Paul Matt
Scale Airplane
Drawings
Volume 2
3-View Scale Drawings by Paul Matt
Volume 1 contains all airplanes listed from A through G. Volume 2 contains all airplanes listed from H through W.
If you would like individual, large sheets of any of the below listed scale drawings, send request, catalog #,
appropriate fee, and shipping charge of $3.95. If you want your drawing rolled in a tube — add $4.00. Clear, concise,
uncluttered 3- and 4- view engineering presentations, in large (17" x 22"), easy to work with standard scales. Drawing
is highly detailed and is an accurate working print with all dimensions, specifications, airfoils, cross sections,
templates, and color scheme included. These drawings are part of the collection of the internationally acclaimed and
highly honored Historical Aviation Album. All orders are folded unless a tube is ordered. Each has 2 to 6 large sheets.
Rolled in tube — add $4.00 plus $3.95 postage. Send to: Aviation Heritage, P.O. Box 665, Destin, FL 32540.
VOLUME 1 CONTENTS:
RETAIL PRICE VOLUME 2 CONTENTS:
DRAWING SCALE CODf
Last letter of catalog num
indicates scale of drawinc
A = 1:24.... 1/2'= 1'
B= 1:16.......3/4'=	1'
C= 1:48.... 1/4'= Г
D= 1:32.... 3/8'= 1'
E = 1:8....1 1/2'= Г
F= 1:6..........2'=	1'
G= 1:96.... 1/8'= 1'
RETAIL P
Aeromarine 39B..................
Aeronca7AC “Champion”...........
(#9-78A, 3 shts.)......$16.50 _ Heath LNB-4 Parasol
(#AM-41 A, 2 shts.)....15.00 _ Howard DGA-15P 
Aeronca C-2..........................
Aeronca C-3 “Collegian"..............
Aeronca C-3 “Master”.................
Aeronca К............................
Aeronca LB “Low wing”................
AlcorC.6.1 Jr. Transport.............
Anderson-Greenwood AG-14.............
Beechcraft D-18S Twin................
Bell P-39Q “Airacobra”...............
Berkmans “Speed Scout”...............
Berliner-Joyce О J-2.................
Berliner-Joyce XF3J-1................
Boeing 307 “Stratoliner”.............
Boeing F3B-1.........................
Boeing XF7B-1 .......................
Brewster F2A-3 “Buffalo”.............
Cessna 120/140 ......................
Cessna C-37 “Airmaster”..............
Cessna T-50 “Bobcat".................
Consolidated P2Y-2...................
Consolidated PBY-5A “Catalina".......
Curtiss “Carrier Pigeon Г............
(#10-80A, 2 shts.).......
(#10-81 A. 2 shts.)......
(#10-82 A, 2 shts.)......
(#15-103A, 2 shts.)......
(#AM-60A, 2 shts.).......
(#4-33D, 2 shts.)........
(#12-94A, 2 shts.).......
(#6-59A, 3 shts.)........
(#1-7A, 2 shts.)........
(#2-12B, 2 shts.)........
(#AM-48A, 2 shts.).......
(#15-104A, 2 shts.)......
(#7-63C, 2 shts.) .......
(#AM-56A, 2 shts.).......
(#AM-38A, 2 shts.).......
(#5-47A, 2 shts.)........
(#1-9A, 2 shts.)........
(#6-50A, 2 shts.)........
(#17-115A, 2 shts.)......
(#9-71C,3 shts.).........
(#17-114C, 3 shts.)......
(#2-15A, 2 shts.)........
Curtiss 1st Milit. Tract. S.C. No. 21/22 1913.(#6-55A, 2 shts.).
Curtiss A-3B “Falcon”.................(#AM-39A,	2 shts.).....
15.00 _ Howard DGA-3 “Pete”.............
15.00 _ Howard DGA-4 “Mike".............
15.00 _ Howard DGA-5 “Ike”..............
15.00 _ Howard DGA-6 “Mr. Mulligan”.....
15.00 _ Hughes 1B Longwing Racer........
15.00 _ Hughes 1В Shortwing Racer.......
15.00 _ Laird LC-DW-300 “Solution"......
16.50 _ Laird LC-DW-500 “Super Solution”
15.00 _ Laird-Turner LTR-14.............
15.00 _ Lavochkin LA-7..................
15.00 _ Lockheed P-80B “Shooting Star”...
15.00 _ Lockheed Model 9 “Orion”........
15.00 _ Lockheed PV-1 “Ventura”.........
15.00 _ LWF Cato Model L “Butterfly"....
15.00 _ LWF Model G-2...................
15.00 _ LWF Model H-1 “Owl”.............
15.00 _ Martin BM-1 and 2...............
15.00 _ Martin T4M-1, Great Lakes TG-1 ..
15.00 _ Martin TT, 1913 Trainer.........
16.50 _ Messerschmitt Me 109 E-3........
18.00 _ Morehouse 2 Cyl. Aero Engine ...
15.00 _ Navy-Wright NW-1 Mystery Racer
15.00 _ Navy-Wright NW-2 Mystery Racer
15.00 _ North American 0-47A............
Curtiss AT-9 “Jeep"..................
Curtiss B-2 Condor Bomber............
Curtiss B-20 Condor Transport........
Curtiss F Boat.......................
Curtiss F92 “Sparrowhawk”............
Curtiss MF-K-6 “Seagull”.............
Curtiss P-36 “Hawk”..................
Curtiss P-6E “Hawk”..................
Curtiss PW-8..........................
Curtiss R-6 Racer....................
Curtiss SC-1 “Seahawk”...............
Curtiss SNC-1 “Falcon”...............
Curtiss SO3C-1 “Seagull”.............
Curtiss Twin JN.......................
Curtiss-Cox “Texas Wildcat”..........
Curtiss-Wright T-32 "Condor".........
Curtiss-Wright CW-1 “Jr.”............
Douglas 0-2...........................
Douglas 0-2H..........................
Douglas 0-38..........................
Douglas 0-38E........................
Douglas M-2..........................
Douglas A-20G “Havoc”................
Etrich 1913 Taube..........................
Fairchild FC-1.............................
Fairchild FC-2.............................
Fairchild FC-2W “Stars & Stripes”..........
Fairchild M-62, PT-19 “Cornell”............
(#2-18A, 2 shts.).......15.00 _ North American AT-6D “Texan”.....
(#18-116C, 2 shts.).....15.00 _ North American XB-70-1 “Valkyrie”
(#18-117C, 2 shts.).....15.00 _ Packard-Le Pere LUSAC-11 ........
(#1-1 A, 2 shts.)....... 15.00	_ Pfitzner 1910 Monoplane.........
(#18-118A, 2 shts.).....15.00 _ Piper J-3 “Cub”..................
(#AM-37A, 2 shts.)......15.00 _ Piper J-4 “Cub Coupe”............
(#7-62A, 2 shts.).......15.00 _ Piper PA-12 “Super Cruiser”......
(#5-42A, 2 shts.).......15.00 _ Republic RC-3 Seabee.............
(#10-79A, 2 shts.).......15.00	_ Rover Inverted Aero Engine.....
(#HS-73A, 2 shts.)......15.00 _ Ryan B-5 “Brougham”..............
(#1-8A, 2 shts.)........ 15.00	_ Rylfo FR-1 “Fireball”...........
(#AA-65A, 2 shts).......15.00 _ Ryan SCW Low Wing................
(#AM-34A, 2 shts.)......15.00 _ Ryan ST-A........................
(#3-21 A, 2 shts.)......15.00 _ Seversky BT-8....................
(#2-14B, 2 shts.).......15.00 _ Seversky P-35....................
(#1-6C, 2 shts)......... 15.00 _ Sikorsky S-39B..................
(#11 -88A, 3 shts.).....16.50 _ Standard J-1 ....................
(#11-86A, 3 shts.)......16.50 _ Taylor E-2 “Cub".................
(#11-87A, 2 shts.)......15.00 _ Taylor J-2 “Cub”.................
(#12-92A, 2 shts.)......15.00 _ Thomas-Boeing MB-ЗА and
(#12-93A, 2 shts.)......15.00 Thomas-Morse MB-3..................
(#14-68A, 2 shts.)......15.00 _ Timm TC-170 “Collegiate”........
(#15-102D, 6 shts.).....20.00 _ Verville R-3 Racer...............
(#TB-105D, 3shts.)......
(#17-111 A, 2 shts.)....
(#17-112A, 2 shts.).....
(#17-11 ЗА, 2 shts.)....
(#AA-69A, 2 shts.)......
16.50 _ Vought F4U-1 “Corsair
15.00 _ Vought SBU-1........
15.00 _ Vought XF5U.........
15.00 _ Vultee V-1A Transport.
15.00 _ Waco UMF/YMF-5......
Fokker T.5 Netherlands Bomber........(#AA-61C, 2 shts.).......15.00 _ Waco UPF-7.........
Gallaudet D-1........................(#3-20A, 2 shts.)........15.00 _ Waco YKS-6 Cabin
General Aviation Clark GA-43....
Grumman F-11F-1 “Tiger”.........
Grumman FF-1....................
Grumman G-44 “Widgeon”..........
Grumman J2F-5 “Duck”............
(#13-95D, 2 shts.)......15.00
(#2-19D, 2 shts.).......15.00
(#AA-77A, 2 shts.)......15.00
(#AM5-30A, 2 shts.).....15.00
(#6-53A, 3 shts.).......16.50
Waterman “Arrowbile”.......
Waterman “Gosling" Racer
Wright F2W-1 Racer.........
Wright F2W-2 Racer.........
Wright Brothers 1903 Flyer
Wright-Martin V............
(#4-35B, 2 shts.).......
(#AM-52A, 2 shts.)......
(#12-89A, 2 shts.)......
(#13-90A, 2 shts.)......
(#13-91 A, 2 shts.).....
(#14-99A, 3 shts.)......
(#16-108A, 3shts.)......
(#16-107A, 3 shts.).....
(#7-64A, 2 shts.).......
(#8-74A, 2 shts.).......
(#10-83A, 2 shts.)......
(#AA-46A, 4 shts.)......
(#2-1OA, 2 shts.).......
(#3-22A, 2 shts.).......
(#E-1O1C, 3 shts.)......
(#10-84A, 2 shts.)......
(#2-1 ЗА, 2 shts.)......
(#11-85C, 2 shts.)......
(#1-5A, 2 shts.)........
(#4-29D, 2 shts.) ......
(#5-40A, 2 shts.).......
(#AA-75A, 2 shts.)......
(#3-27E, 1 sht.)........
(#4-31 A, 2 shts.)......
(#4-32A, 2 shts.).......
(#13-98A, 3 shts.)......
(#16-106A, 3 shts.).....
. (#7-66G, 3 shts.)......
(#1-3A, 2 shts.)........
(#2-11 A, 2 shts.)......
(#18-121 A, 2 shts.)....
(#18-122A, 2 shts.).....
(#4-36A, 2 shts.).......
(#16-109A, 3 shts.).....
(#5-45F, 1 sht.)........
(#RB-96A, 2 shts.)......
(#3-26A, 2 shts.).......
(#AM9-49A, 2 shts.).....
(#9-76A, 2 shts.).......
(#3-23A, 2 shts.).......
(#AA-57A, 2 shts.)......
(#14-100A, 5 shts.).....
(#17-110A, 2 shts.).....
(#18-119A, 2 shts.).....
(#18-120A, 2 shts.).....
(#4-28B, 2 shts.).......
(#8-72A, 2 shts.).......
(#6-58A, 2 shts.).......
(#AA-51A, 3 shts.)......
(#3-24A, 2 shts.).......
(#8-70A, 3 shts.).......
(#2-16A, 2 shts.).......
(#13-97A, 3 shts.)......
(#8-67A, 2 shts.).......
.(#2-17A, 2 shts.)......
(#3-25A, 2 shts.).......
(#1-4B, 2 shts.)........
(#5-43A, 2 shts.).......
(#5-44A, 2 shts.).......
(#0-123A, 2 shts.)......
(#1-2A, 2 shts.)........
All of Paul Matt Drawings are soon to be released on ”CD” In TIFF and PCX Format! Reserve your copy Today!! The Paul Matt Scale Dra
listed on this page are all being compiled for the first time on CD-ROM in IBM compatible TIFF and PCX formats especially for the CAD mo
You can have ALL of these internationflly acclaimed drawings on one CD for an incredibly low price? 522 Files available (261 TIFF & 261
Cat. No. WS-PMCD-1................NEW.................$99.95	+ $3.95 SHIPPING
Heath LNB-4 Parasol
Heath Parasol and Henderson converted
motorcycle engine installation.
Heath Parasol on floats. Ed Heath by aircraft.
Heath LNB-4 Parasol.
\	/ \A \ A х . А 1-9'/г“ \/ \	\ ХХХ\ \ ? 4 \\~ \ Х---^	13 2'-1” \	/А	у' \\\\\л\	/ SPECIFICATIONS	\ \А ^у"	\X\W\a\	А^ А\ HEATH LNB-4 (АТС 456)	\Z \ A	\	\	А	А^ \ ENERAL	A	\v\ \ А\\ А^	А\ WINGSPAN	ЗГЗ"(9.5т)	ХЧХХХХХХх	А^ \ А" LENGTH О.A	I7'3"(5.3m)	\\\\\xXvX	/\	/ ' WING AREA	135 5 SO FT. (12.6т2)	\\\\\\\А/	\ А/Х WING LOADING	5.16 LBS/SQ FT(25.2kg/m2 )	\\\\\\z4	Az" \z POWER LOADING	28 LBS/H P. (12.7 kg/hp)	\\\\jr	/А	Az WEIGHT EMPTY	450 LBS.(204 1 kg)	PYRALIN SKYLIGHT	\	\\z\	A/ \ /у GROSS WEIGHT	700 LBS (317.5 kg)	AJ\	\ AzX	/ FUEL CAPACITY	10 GAL. (37.9 litres)	A^X< VSAX A 4^^ OILCAPACITY	I.50GAL (5 7 litres)	^A	xAART У ERFORMANCE	^A \	ЛЖЛ f J \ZA A MAX SPEED	73 MPH. (117.5 kph)	у	\ A^AC'W /X F	Xх CRUISE SPEED	63 M PH. ( 99.8 kph )	A\	/z A A"	A LANDING SPEED	32M.P.H(5I 5 kph)	\	\ \ SERVICE CEILING	11,000 FT. (3,352.8m)	^A\	AA^^X	JrA X ' RATEOFCLIMB	500 FT /MIN (152 4 m/min )	^A	\ X ^\\ CRUISE RANGE	330 MILES(53I 1 km)	^A\	All/ A\	УГА^ЖAx Жт / V \	\А$Л \ ж /	V \	\\Х>У\ A^ ENGINE (APPROVAL E4-3) /	A\ AX	>	HEATH B4, VERTICAL 4CYL. IN-LINE	/ /	\л/	к	1	\A^X \ A^	HORSEPOWER	25HP@2800RPM \	J \Al	\	1	ЧСаГ \ A^	FUEL CONSUMPTION	64LB/H P/HR \	\	\ f \	t	A\ \ A^	OIL CONSUMPTION	.02 LB/H.P /HP \	\	XI	\ ^A	MFGR'S H P RATING 27 H.P02700R PM \	\	\ \	\ \ A^	TAKE-OFF H P AVAILABLE ЗОН РОвООО R P M. \	\	\ \1 \ \	ENGINE WEIGHT	109 LBS \	\	X/\ \ A^	METAL PROPELLOR AVAILABLE AS OPTIONAL	'X	TW. А/X \ ХаУаХ , X Xz \	\ /	\ 12/2 TYP 7 Va^AA^ X^^AAz 	FUEL TANK- 5 GAL CAPACITY PER TANK /		4'- 6”	— 8" p  2'-6"—• CLARK ” Y" SECTION V • j/ S'	TYPICAL PROPELLER, WOOD OR METAL 0	1	2	3	4	5	6 FEET METERS IIktowcal	HEATH LNB-4 parasol 1 A VIATION	(1931) 1 Л Ai Dini	SCALE L32
FUEL TANK CAP
2°DIHEDRAL
1HOKE
4-0
METERS
FEET
RUSSELL CORD
RING SHOCKS
ZENITH
\LTIMETER
INSTRUMENT PANEL DETAILS
REF’ HEATH AIRCRAFT CO. DWG. 183
UPPER FUS. LONGERON
THROTTLE
(SHAKESPEARE MODEL AA)
OILTEMP (MOTO-METER)
IGNITION SWITCH
OIL PRESSURE(MOTO-METER)
TACHOMETER
AILERON "PUSH-PULL
CONTROL ROD
FUEL STRAINER
ACCESS HOLE
173” 0 A LGTH --------------------------------------------------—I
b—— Г-Ю3/4"--НН—Г-10" —
COLOR SCHEME
(FACTORY BUILT)
ENTIRE AIRCRAFT FINISHED IN LIGHT
CREAM REGISTRATION LETTERS,
NUMERALS 8 OPTIONAL TRIM FINISH
WERE BLACK.
6-2"
KNOWN REGISTRATION NUMBERS OF
FACTORY BUILT LNB-4 AIRCRAFT ARE
LISTED AS FOLLOWS:
NC 10739- BELIEVED TOBE PROTOTYPE.
NC 10740
NC 12874 - AIRCRAFT SHOWN IN THESE DWGS
NC 13375
NC 13646
NC 15621
Howard DGA 15P
12' 2'4
2’ O'a
WING 3-Ply MAHOGANY
SHEATHED. FABRIC COVERED,
DOPED & POLISHED TO GLASS
SMOOTH FINISH
I2“- 5’5"
GRIMES RETRACTABLE
LANDING LIGHT
ALUMINUM
FAIRING
SCALE BAR. feet
LEAR ADF
LOOP ANTENNA
HOUSING
2
SCALE BAR, meters
ALUMINUM
FAIRING
ALUMINUM
INSPECTION PLATES -
6 ll'4“
GENERAL SPECIFICATIONS
DGA-I5P АТС 7i7
WEIGHT EMPTY
USEFUL LOAD
GROSS WEIGHT
MAX SPEED
LANDING SPEED
RATE OF CLIMB. INITIAL. S L
SERVICE CEILING
FUEL CAPACITY
OIL CAPACITY
FUEL CONSUMPTION
CRUISING RANGE
CRUISING SPEED
WING LOADING
ROWER LOADING
2.725 lbs
1,625 lbs incl 125 lbs BAGGAGE
4 350 lbs
201 mph of 6,000 ft. 186 of S L
62 mph
1560 ft /min
21,500 feet
120/150 gois
8 gols
24 go Is /hr
785/920 miles
186/191 mph ot 9.600 ft
20.7 lbs Zsq ft
10 9 lbs/ bp
SERVICE STEP BAR
INSTRUMENT PANEL
WOOD GRAIN FINISH
(DRAWING No AM-52-a] PLATE ' of 2
HOWARD DGA-I5P
______________1939 - 41___________
DRAWN BY- PAUL R. MATT
from the files of
HISTORICAL AVIATION ALBUM
for
AMERICAN Aircraft MODELER
________ SCALE - ORIGINAL I 24
HOWARD DGA-I5P
______________1939 -41__________
DRAWN BY- PAUL R MATT
from the files of
HISTORICAL AVIATION ALBUM
for
AMERICAN A/raaft, MODELER
__________SCALE - ORIGINAL I 24
GENERAL SPECIFICATIONS
EMPTY WEIGHT
USEFUL LOAD
GROSS WEIGHT
WING AREA (including oilerons)
MAXIMUM SPEED
LANDING SPEED
CRUISING SPEED
CRUISING RANGE
8-0"
FUEL FILL
CAP FARING
NOTE ALL FULL RIBS, WINGS AND
TAIL SURFACES ARE SPACED
6" ON CENTER
28
8"
6 ft
2 meters
NACA M-6 AIRFOIL
HOWARD DGA-3 "PEI
____________1930-35__________
SCALE-ORIGINAL В 24
REPRO. 148
DRAWN BY- PAUL R. MATT
635 lbs
2 65 lbs
900 lbs
67 sq. ft.
163 5mph
60mph
l50mph
250miles
POWER WRIGHT 4 CYLINDER "GYPSY," 326cu.in
85HP @ 1900RPM
90HP (a) 25OORPM
95HP @ 26OORPM
LICENSE GOLD OUTLINED
IN BLACK 24" HIGH
1/16" PLYWOOD COVERED
LEADING EDGE AND TIP
COLORING NOTES:
AIRCRAFT ALL GLOSS WHITE
LETTERING AND DETAILS AS NOTED
InDAVUIKin 19 - QQ-Л I
"37й SOLID BLACK
16" HIGH
48"
24"
EXPOSED
OVERHEAD
OIL LINE
SCALE BARS
M-6 AIRFOIL USED
ON AXLE FAIRING
PITOT TUBE
ISTORKAL
iVIAItoN
AAlbum
© HISTORICAL AVIATION ALBUM
P.O BOX 33
TCMDI Г CITV ГЛ1 If QI7ЙП
DATUM
Q
---------------------17'-9’
"PETE" IN ORIGINAL 1930 CONFIGURATION
R2Y
HIGH SOLID BLACK
RACING NUMBER
18'x3" RAC MG WHEELS
(2O"x4n SPORT & TESTMG WHEELS)
HORIZONTAL STABILIZER
FIXED AT O* INC.
ALL LETTERING SOLID
BLACK DURING LATE YEARS,
NAME “PETE" ELIMINATED
ONCE JACOBSON PURCHASED
AIRCRAFT.
SCALE BARS
2 meters
JPREME" WOOD
PROPELLER
PETE", GOLD LETTERING,
BLACK OUTLINED
"PETE" WHEN OWNED AND
FLOWN BY JOE JACOBSON,
1935 ON.
FIXED PITCH
METAL PROPELLER
-----4" HIGH GOLD LICENSE
BLACK OUTLINE
ISTORKAL
Wl/WON
AAlbum
HOWARD DGA-3 "PETE"
____________1930-35_____________
SCALE-ORIGINAL 1-24
REPRO. 148
DRAWN BY- PAUL R. MATT
© HISTORICAL AVIATION ALBUM I973
RO, BOX 33
GENERAL SPECIFICATIONS
EMPTY WEIGHT
USEFUL LOAD
GROSS WEIGHT
MAXIMUM SPEED
CRUISING SPEED
LANDING SPEED
8’-О
COCKPIT COAMING
HINGED OUTBOARD
NOTE:
THIS ISA REVISED DRAWING
AND SUPERSEDES DWG No. I2-9O-A
FIXED METAL
TRIM TAB
9 x 12 BLACK NUMBERS,
SAME STENCIL USED FOR
NUMBERING DGA-5 "IKE"
NOT USED ON FUSELAGE
OF MIKE THOUGH.
COLORING NOTES
ENTIRE AIRCRAFT GLOSS WHITE
LETTERING & DETAILS AS NOTED
8 VENT HOLES
PIANO HINGE
meters
2 inc.
AIRFOIL
NACA M-6
7" R.
OIL TANK
FILL ACCESS
919 lbs.
275 lbs.
1194 lbs.
24l.6mph
175 mph
70 mph
POWER: MENASCO C-6-S "BUCCANEER"
6 CYLINDER INLINE ENGINE
489 cu. in. DISPLACEMENT ’
NORMAL RATING 160 HP
SUPERCHARGED TO APPROX
200 HP FOR RACING
FUEL FILL-
SCALE BARS
SINGLE HEAVY
BRACING WIRE--
‘/i6 PLYWOOD COVERED
Д—LEADING EDGE & TIP
DRAW LINE (WIRE)
COWL LOCK
CARBURETOR
LICENSE - GOLD, OUTLINED
IN BLACK,
18" HIGH, 3 "STROKE
Z—MOISTURE DRAIN
GROMETS
isTom
Aviatfjn
/(Album
HOWARD DGA-4
________1932-37
SCALE-ORIGINAL 1:24
REPRO. 148
DRAWN BY-PAUL R. MA
[DRAWING No. 13-90-a]
PLATE I of?
© HISTORICAL AVIATION ALB
RO. BOX 33
TCkitX E-
20’-I
SCALE BARS
THRUST
FRL
0* DIHEDRAL
PITOT ASSEMBLY
THRU3T
CARBURETOR
DATUM
SHEET METAL
COVERING OVER
ORIGINAL LARGE
AIR EXIT DEPRESSION
4” HIGH GOLD LICENSE,
OUTLINED IN BLACK
COCKPIT ADJUSTABLE
STABILIZER
NOTE
THIS IS A REVISED DRAWING
AND SUPERSEDES DWG. No. I2-9C
14 x 6 GOODRICH SILVERTOWN
BALLOON TIRES
SCALE-ORIGINAL I 24
REPRO I 48
DRAWN BY - PAUL R. MAT
NO SHOCK ABSORBING SYSTEM
EMPLOYED IN LANDING GEAR
EXPOSED RETURN OIL
LINE -----------
COOLING, OIL TANK
BEHIND----------
FOR ADDED
PILOT SEAT
THRUST
HILL STREAMLINERS"
WHEEL PANTS & FAIRINGS
SMITH GROUND
ADJUSTABLE METAL
PROPELLOR

6-10

2
. meters
|7._2>г.._АяРЯ«с
’MIKE", GOLD LETTERING
BLACK OUTLINE 7
8"x 10” BLACK NUMBERS
ISTOWCAL
AViAIK>N
ftAlBUM
HOWARD DGA-4 "M.
________1932-37____
© HISTORICAL AVIATION ALBI
RO. BOX 33
GENERAL SPECIFICATIONS
ГУ WEIGHT
rUL LOAD
SS WEIGHT
IMUM SPEED
DING SPEED
SING SPEED
COLORING NOTES
FUEL FILL
COCKPIT COAMING
HINGED OUTBOARD
FIXED STUT
BRACE
feel
J2 meters
2 INC
AIRFOIL NACA M-6
PIANO
HINGE
CHEVROLET EMBLEM
DARK BLUE, WHITE
BORDER & LETTERS,
GOLD PINSTRIPE
OUTLINED
MOISTURE DRAIN
GROMETS
AIRCRAFT ALL GLOSS WHITE,
LETTERING AND DETAILS AS NOTED
GOLD LICENSE, OUTLINED
IN BLACK, 18“ HIGH, 3 STROKE
© HISTORICAL AVIATION ALBUN
RO. BOX 33
HOWARD DGA-5 '7
__________1932-37______
SCALE- ORIGINAL ~
REPRO. 1'48
DRAWN BY - PAUL R. MATT
f—•
919 lbs.
275 lbs
1194 lbs.
241.6 mph
70 mph
175 mph
ER MENASCO C-6-S "BUCCANEER”
6 CYLINDER INLINE ENGINE,
489 cu.in. DISPLACEMENT,
SUPERCHARGED TO APPROX 200 HP,
NORMAL RATING 160 HP
FIXED METAL
TRIM TAB
A9
SCALE BARS
DR/W WIRE
COWL LOCK
CARBURETOR AIR NTAKE
(FLUSH WITH EXT. SURFACE)
SPLAYED FLYING WIRES
’/ю" PLYWOOD COVERED
9"x 12" BLACK NUMBERS,
SAME STENCIL, WITH VARIATIONS,
USED ON FUSELAGE. ALSO USED
ON DGA-4 “MIKE”
NOTE:
THIS IS A REVISED DRAWING
AND SUPERSEDES DWG. No. 12-91-A
ISTOWCAL
AAlbum
У DIHEDRAL
THRUST
Ж5О
SCALE BAR, meters
APPROX
17'- 214'
THRUST
DATUM
6-10
DDOO
DfiDI
080D
DDDP
COCKPIT ADJUSTABLE
STABILIZER.
4" HIGH GOLD LICENSE,
— BLACK OUTLINE.
NOTE:
THIS IS A REVISED DRAWING
AND SUPERSEDES DWG NoJ2-9l-A
© HISTORICAL AVIATION ALBUM 19
PO. BOX 33
14"хб" GOODRICH "SILVERTOWN
BALLOON TIRES.
96(9 ~
96(6’
9Ш
flfl fill
QQQO
(9(9696
lillil QQ8Q6QQ
«98111fl
ORIGINAL TANDEM LANDING G
EMPLOYED DURING FIRST, 19
RACING SEASON ONLY. II x 5"
TREADED HIGH PRESSURE 7
STYLE OF ALL BLACK
NUMBERS WITH CHAMFERED
HORIZONTAL EDGES USED
ON "Miss CHEVROLET" ONLY.
SCALE-ORIGINAL	I 24
REPRO.	I 48
DRAWN BY-PAUL R. MATT
PITOT ASSEMBLY
NO SHOCK ABSORBING SYSTEM
EMPLOYED IN LANDING GEAR
9999999
999999 jHUflu
9999999
Ш8
9988
flflflfl.
80S

3ERED STYLE OF NUMBERING
:d on original "ike"
EDITION OF RACER WHEN
NED BY BEN HOWARD, 1932-34
D FLOWN AT THE NATIONAL
I RACES
AITH GROUND ADJUSTABLE
ETAL PROPELLER.
SCALE BAR, feet
HILL STREAMLINERS
WHEEL PANTS & FAIRINGS
M/ss CHEVROLET
GOLD, BLACK OUTUNE-

ISTORKM
IVIAHON
AAlbum
AT LEFT IS "IKE" IN ITS MOS
POPULAR CONDITION, WHEN
OWNED BY HAROLD NEUMA
1935-36, AND THEN ACQUIRE
BY THE FORDEN-BROWN
AIRSHOWS, INC. 1936-38.
HOWARD DGA-5 "IKE
________1932-37_______
Howard DGA-6 Mister Mulligan
10‘ - 3’—
ZJ
OIL DRAIN
ACCESS
FABRIC
COVERED
USEFUL LOAD
GROSS WEIGHT
WING AREA
WING LOADING
POWER LOADING
STRUT FAIRING, AIRFLOW
DIRECTIONAL & CONTAIN-
MENT CONTROL
1500 lbs.
41 00 lbs.
150 7 sq ft.
30 7 Ibs/sq ft
7.65lbs/h p
POWER - PRATT & WHITNEY WASP SE SPECIAL
s/n 5640. COMPRESSION RATIO 6 4
SUPERCHARGER RATIO 14:1
NORMAL RATING -500 H P at 2200 R PM
USING DESIGNATED 87 OCTANE FUEL
2700lbs
5300 lbs
I 50 7 sq ft.
39 Ibs/sq ft
3	4
66"
AIRFOIL NACA 2412
COL ORING NOTES
METAL COVERING
isrmt
NUMBER ON
SURFACE OF
FLARE
TUBES (2)
ENGINE COWL BUILT-
IN ONE PIECE.
PROPELLER WAS
WING PANELS COVERED
WITH .0781 INCH 3-PLY
HASKELITE SPRUCE
PLYWOOD, THEN COVERED
WITH DOPED FABRIC
FUEL FILL CAP '
FLUSH WITH SURFACE
OF WING. 25 GALS CAP
IN EACH WING, 92 OCT.
FUEL
9-5
10’- 6'A
RACING
UNDER
RIGHT WING ONLY
SCALE-ORIGINAL Г24
REPRO. 1-48
DRAWN BY-PAUL R MATT
MAXIMUM SPEED- 287mph,S.L.. 830h p , 100 OCTANE FUEL
(THOMPSON TROPHY RACE, 1935)
TOP SPEED, NORMAL, 25lmph, S.L., 550 h p., 92 OCTANE
CRUISING SPEEDS, PULLING 550 h p & USING 87 OCT. FUEL
at 17,000 feet - 292 mph
at II, 000 feet - 262 mph
at Sea Level - 23 I mph
LANDING SPEED. WITH FLAPS - 64 mph
RATE OF CLIMB. INITIAL. S L - 2800 ff/mtn
(550h.p , 92 OCTANE FUEL)
- 4450 ff./min
(830h p , 100 OCTANE FUEL )
SCALE BARS
OIL TANK
FILL ACCESS
feet
meters
3772'
WING TANK OVER-
FLOW AND
BREATHER TUBE
FUSELAGE
FUEL TANKS
DRAIN
ACCESS
ANTI-FLUTTER
BRACE WIRE,
TOP & BOTTOM
NUMBER 3 HAS EXTENDED WIDTH
IN ORDER TO COMPENSATE FOR
SLANT OF FAIRING
5’- IO"
5-10"
MY SINCERE APPRECIATION IS
EXTENDED TO PETER M BOWERS,
MRS BEN. O. "MIKE" HOWARD, NICK
REZICH, TOM VERZY AND MAJOR
TRUMAN WEAVER USAF, FOR THEIR
PERSONAL TIME AND INTEREST IN
HELPING TO MAKE THESE DRAWINGS
AS AUTHENTIC AS POSSIBLE
ENTIRE AIRCRAFT-GLOSS WHITE
ALL LICENSE NUMBERS - GOLD,
OUTLINED IN BLACK
'MISTER MULLIGAN' NAME-GOLD,
OUTLINED IN BLACK
RACING NUMBER - SOLID BLACK
GULF OIL CO. INSIGNIA-ORANGE DISC,
OUTLINED IN DARK BLUE, 'GULF'
DARK BLUE, SHADOW SHADED ON
RIGHT LOWER QUADRANTS IN
WHITE
HOWARD DGA-6
Mister Mulligan
___ 1934-36
LYCOMING-SMITH
CONTROLLABLE
PITCH PROPELLER
VISIBILITY CUTOUTS. THIS WAS A
WOOD SUPPORT AND NOT THE WING
SPAR NOR PART OF IT.
0° DIH.
У-б" АРИ°Х
DATUM
4 SHOCK ABSORPTION
HILL STREAMLINERS'
7;50x Ю GOODRICH SILVERTOWN TIRES
INSET NAVIGATION
LIGHT (CLEAR)
30 SPLINE
SHAFT
LICENSE, GOLD
OUTLINED IN BLACK
SCALE-ORIGINAL 1:24
REPRO. Г48
DRAWN RY- PAUI R MATT
ON FLAT SIDE OF FUSELAGE
FABRIC WAS DOUBLE TAPED,
STITCHED AND GLUED TO
EVERY OTHER STRINGER
FUEL TANKS
DRAIN ACCESS
---PITOT ASSEMBLY
ALL WINDOWS
PLASTICYL

SERVICE STEP।
BAR
LETTERING-
GOODRICH
SILVERTOWN
TIRES
SCALE BARS
©-WORDING REPLACED BY P&W "EAGLE" LOGO
DECAL FOR 1936 RACING SEASON
ACCESS TO FUEL FILLER NECK 1
FOR TANKS LOCATED IN BELLY 1
OF PLANE	I
LETTERING “WHEEL PANTS £ COWL
ON LEFT
WHEEL
STRUT
25'-I
A/R INTAKE TUBES BETWEEN CYLINDERS
TWO TOP INTAKES - MAGNETO COOLERS
TWO ON RIGHT SIDE-CABIN FRESH AIR
TWO AT BOTTOM, WITH FUNNEL INTAKE
LEAD - CARBURETOR AIR INTAKE
ONE ON LEFT - OIL COOLER INTAKE
meters
38^'
OXYGEN
BOTTLES
iSTORML
iVlAIlON
/\Album
STYLE AND PLACEMENT
OF NAME ON ENGINE COWL.
GOLD, OUTLINED IN BLACK.
SCALE, 4X SCALE OF G A
HOWARD DGA-6
Mister Mulligan
1934-36____
FLAP OPERATING
г-TORQUE TUBE
X TANK
’PORT
MBERS
>00)
INTERIOR OF CABIN - NATURAL MAHOGANY PLY-VENEER
FLOORBOARD - PAINTED DARK GRAY
SHADED AREA,
LONG RANGE FUEL TAi
(BENDIX RACE)
'mister mulligan" wing tip layout
ON 6 INCH INCREMENTS
LEVER
5-10
5‘-10
DATUM
6^
DATUM
СТОЙ
DATUM____
EXACT DIMENSIONS CANNOT BE GIVEN ON
PROPOSED
REAR SEATII
OVERHEAD METAL PLATE
FOR STABILIZER ADJUSTMENT
CRANK
THIS TUBE OMITTED
ON RIGHT SIDE TO
ALLOW FOR CABIN DOOR
INTERMEDIATE AUXIl
FORMERS
TAIL WHEEL SHOCK ASSEMBLY.
RUBBER DISCS
© HISTORICAL AVIATION ALBUM
P 0. BOX 33
steel compress.on WAG W,RES
SCALE-ORIGINAL 1’24
RE PRO. 1’48
DRAWN BY-PAUL R. MATT
L TANK —UL_
3Al CAP
OCT. FUEL
13. THROTTLE *
MIXTURE C
14. IGNITION SWI
15 ALTIMETER
.MULTI POSIT
'•( ON ENGINE И
17\temperatu
IB OIL PRESSUR
19. OIL TEMPERA
BAGGAGE
□OMPART -
MENT
DRAG WIRES WERE USED IN
’RUCTION OF WING IN CONJUNC-
WITH THE .0781 INCH 3-PLY
ELITE SPRUCE PLYWOOD
SSEMBLY WAS THEN COVERED
FABRIC. DOPED, SANDED AND
HED TO A SMOOTH FINISH
WING
RADIO A
HEADPHONES
OIL
DRU*
LANDING GEAR SHOCK
ABSORBERS, RUBBER
DISCS IN PAIRS,
IN COMPRESSION
ILERON
JSH-PULL TUBE
i3-
INTER-
CONNECT
PIPING
FUSELAGE FUEL
TANKS, «7 OCTANE,
100 GALS TOTAL CAP
INSTRUMENT PANEL, BLACK
CENTER FLIGHT
INSTRUMENT SQUARE,
CRINKLE FINISH
IN CONSTRUCTION ALLOWANCE
SHOULD BE GIVEN FOR TUBE
THICKNESS, FITTINGS & FORMERS
IN ORDER TO ATTAIN EXTERIOR SHAPE
SHEET
/1ETAL
PLYWOOD
FORMERS
(TYPICAL )
I. PROP PITCH
CONTROL INDEX	_______
2 ARTIFICIAL HORIZON 12 ENGINE PRIM
3. CLOCK
AIRSPEED
TURN INDICATOR
COMPASS
BALL A BANK
RATE OF CLIMB
TACHOMETER
HOWARD DGA-6'
Mister Mulligan
______1934-36_____
INTERIOR STRUCTURES AS THEY ARE NO LONGER
AVAILABLE. DRAWINGS ARE RECONSTRUCTED
FROM SURVIVING TECHNICAL DATA, PHOTOS
AND PERSONAL REMEMBERANCES OF THOSE
MORE CLOSELY ASSOCIATED WITH THE
ACTUAL AIRCRAFT
WEIGHT EMPTY
TOP SPEED, APPROX.
WING AREA
WING LOADING
POWER LOADING
FUEL CAPACITY
OIL CAPACITY
4097.40 lbs.
330 mph
191 sq.ft.
32.5 Ibs/sq.ft
8.86lbs/H.R
280 gals
30 gals
FUSELAGE PROPER-FLAT SHEET, BUTT JOINED,
FLUSH, SHAVED, BURNISHED & POLISHED RIVETING.
CONTROL SURFACES- METAL FRAMEWORK, FABRIC
COVERED, WING FLAPS - WOOD FRAMEWORK,
PLYWOOD COVERED.
WINGS- WOOD SPARS AND RIBS, PLYWOOD COVERED,
SHAVED, CLOTH COVERED, DOPED AND POLISHED.
LANDING GEAR-ALUMINUM BOX CONSTRUCTION,
RIGID EXCEPT FOR SHORT 5" SHOCK STRUT AT
WHEEL AXEL.
н‘-о!$'
meters
ROOT AT STA. 18
2/-8'
47>2"
NACA 23006
14 5° IN AT TIP
FUEL FILL
TWO TANKS)
HYDRAULIC
BRAKE LINE
OIL FILL
30 GALS.
LICENSE NUMBERS
16" x 30"-5" STROKE
HUGHES IB RACER
JAN. 19, 1937
AS MODIFIED FOR U.S. TRANSCONTINENTAL
SPEED RECORD-BURBANK, CALIF. TO
NEWARK. N.J. 7hrs. 28min. 25sec
FUEL FILL
80 GALS
FUEL FILL
70 GALS
FUEL FILL
65 GALS
(TWO TANKS)
POWER : PRATT & WHITNEY SA5-G (R-1535),
TWIN WASP Jr., s/n 27, (Redesignated s/n281)
700 HP at 25OOrpm. PROPELLER REDUCTION
GEARING 4:3. POWER BOOSTED TO APPROX.
900 HP THROUGH "DOPED" FUEL AND
CARBURETION ADJUSTMENTS.
NACA 23012
SPRING LOADED
FLUSH ENTRY
STEPS
STA. 18-
FIN OFFSET I
SCALE BARS
АУ SINCERE APPRECIATION IS EXTENDED TO THE
ALLOWING MEN FOR THEIR SPECIAL INTEREST AND
•ERSONAL HELP IN MAKING THESE DRAWINGS AS
ACCURATE AND COMPLETE AS POSSIBLE -
MESSERS. RICHARD "DICK ' PALMER, GLENN ODEKIRK,
ARL MARTYN, VAN STORM, ROBERT HIRSCH, JOEY
'EINLEIR AND WAITER ROYNF AND RHRFRT миггсы
COLORING NOTES
FUSELAGE, FIXED TAIL SURFACES - NATURAL ALUMINUM
ELEVATORS AND RUDDER - SILVER DOPED.
WINGS- DARK ROYAL BLUE,( Hughes Tool Co. blue)
(MUNSELL 5PB 2/4)
LICENSE NUMBERS ON WINGS - DEEP YELLOW,
(Hughes Tool Co. yellow)
(MUNSELL 75 Y 8/12)
ALL SURFACES WERE EXTREMELY SMOOTH IN FINISH.
3414"
FWD. SPAR
ISTOWCAL
iVIAHON
AAlbum
GOVERNOR
CARBURETOR AIR INTAKE
BEHIND ENGINE AND
UNDER COWLING
IO'-О
SCALE BAR, meters
1*50'
10-0
T
THRUST
STEEL)
14*45 Approx.
20X11” LOW PRESSURE
BRAKE
SCALE-ORIGINAL 124
REPRO. 1-48
RUDDER. FABRIC
COVERED
LICENSE, BLACK
4"x6"- I” STROKE
HUGHES IB RACER
JAN. 19, 1937
AS MODIFIED FOR U.S. TRANSCONTINENTAL
SPEED RECORD - BURBANK, CALIF. TO
NEWARK, N J 7 hrs. 28 min 25 sec.
RIGHT SIDE
EXHAUST PORTS
SCALE BAR, feet
32/2"
I7"DEPTH OF
I SPAR AT £
OIL COOLER
INTAKE
27-8'
SHOCK STRUT, 5 MAX. TRAVEL
HYDRAULIC BRAKE LINE
HAMILTON-STANDARD
HYDROMATIC CONTROLLABLE
PITCH PROPELLER
PITOTS
RADIO ANTENNA—x
258Y
ISTORKAL
Aviation
\ Album
53/2
AFT STRUT IS SHOCK STRUT
AND TORQUE LINKAGE
TAIL SKID MECHANICALLY
RETRACTED, NON STEERABLE
HUGHES TOOL CO. STEEL SHOE
( DRILLING BIT
TUBE
AILERON,
FABRIC COVERE
ELEVATORS,
FABRIC COVERED
FIXED METAL
TRIM TABS
FLUSH HOLE,
RELIEF-----
28l 50
вк- -в>2 -e/2
j~ THRUST
SPRING LOADED
FAIRING DOORS
COLOR LINE
BLUE OUTBOARD
\ 3 - W' GAPS -
\RETRACTION
ACTIVATING
ARMS
PITOT
STRAIGHT KEEL LINE
STA. 56 TO STA 129
FLAPS MECHANICALLY OPERATED
BY LEVER IN COCKPIT,
DIRECT TORQUE LINKAGE
EMERGENCY FUEL
DUMP PORTS, ALL TANKS.
COLD SOLDERED PLATES
INSET, FLUSH
INSPECTION PAI
210.50	233.50
COCKPIT CANOPY SHOWN
IN OPEN POSITION, WINDSHIELD
SLIDES FORWARD, SIDE PANELS
SLIDE DOWN INTO FUSELAGE
ALL DIMENSIONS IN PROFIE VIEW ARE INCHES
1ST0RKAL
iVIATON
/\Album
HUGHES IB RA<
JAN. 19, 1937
AS MODIFIED FOR U.S. TRANSCC
SPEED RECORD- BURBANK, CZ3
NEWARK, N.J. 7 hrs 28min
SCALE - ORIGINAL 124
REPRO. I 48
DRAWN BY-FAUL R. MAT'
© HISTORICAL AVIATION ALE
Hughes IB Racer, " Longwing" under construction in 1937.

Hughes Shortwing Racer
OWER LOADING
UEL CAPACITY
IL CAPACITY
PLYWOOD COVERED.
WINGS- WOOD SPARS AND RIBS, PLYWOOD COVERED,
SHAVED, CLOTH COVERED, DOPED AND POLISHED.
LANDING GEAR- ALUMINUM BOX CONSTRUCTION,
RIGID EXCEPT FOR SHORT 5" SHOCK STRUT AT
WHEEL AXEL.
2_7’-O*' LINE
7.85 lbs /Н.Р
feet
7'-9%"
47Z
250 gals
30 gals.
THE
AS
STA. 0
ODEKIRK,
JOEY
MIKESH
LICENSE NUMBERS
l6"*3O"-5" STROKE
|2 meters
SCALE BARS
OWER; PRATT & WHITNEY SA1-G (R-1535),
TWIN WASP Jr., s/n 22, 700 HP at 2500rpm
PROPELLER REDUCTION GEARING 4:3
POWER BOOSTED TO APPROX. 900 HP
THROUGH "DOPED" FUEL AND
CARBURETION ADJUSTMENTS.
FIN OFFSET I
COLORING NOTES
FUSELAGE, FIXED TAIL SURFACES - NATURAL ALUMINUM.
ELEVATORS AND RUDDER - SILVER DOPED.
WINGS- DARK ROYAL BLUE ,( Hughes Tool Co. blue)
(MUNSELL 5PB 2/4)
LICENSE NUMBERS ON WINGS-DEEP YELLOW,
(Hughes Tool Co. yellow)
(MUNSELL 7.5 Y 8/12)
ALL SURFACES WERE EXTREMELY SMOOTH IN FINISH.
0* INC
NACA ’2416 (MOD A3I2R)

SPRING LOADED
FLUSH ENTRY
STEPS
ROOT AT STA 18
50 GALS
FUEL FILL-1
L70GAL
STA. 18
FUEL FILL
80 GALS
27^2 22%"
ISTORKAL
I VIATON
UlBUM
SINCERE APPRECIATION IS EXTENDED TO
LOWING MEN FOR THEIR SPECIAL INTEREST AND
SONAL HELP IN MAKING THESE DRAWINGS
URATE AND COMPLETE AS POSSIBLE -
HESSERS. RICHARD "DICK" PALMER, GLENN
L MARTYN, VAN STORM, ROBERT HIRSCH,
ILEIB, AND WALTER BOYNE AND ROBERT
'HE NATIONAL AIR AND SPACE MUSEUM.
HUGHES IB RACER
SEPT. 13, 1935
I 3 Km SPEED RECORD 352.388 mph
(567.155 Kmph)
SCALE - ORIGINAL L24
RE PRO. I 48
DRAWN BY - PAUL R. MATT
HUGHES IB RACER
SEPT. 13, 1935
FAI 3 Km. SPEED RECORD 352.388 mph
(567.155 Kmph)

Laird LC-DW-300 "Solution"
8-0"---
COLORING NOTES
OIL FILL
О
2 meters
SCALE BAR
FRANKLIN GOTHIC
STYLE NUMERALS
FLAT SHEET
ALUMINUM "A
FOLDED FOR
FILLET
SHOED SING
LEAF SPRIN
^-SKID
STABILIZER
ADJUSTABL
FROM
\ COCKPIT
POWER - PRATT a WHITNEY
WASP JR. 300 HP. MAX
2nd PROTOTYPE
WEIGHT EMPTY .... 1380 lbs
GROSS WEIGHT__1845 lbs.
FUEL CAPACITY___50 gallons
OIL CAPACITY____ 7 gallons
— TAIL SURFACES WELDED
STEEL TUBING, FABRIC
COVERED
42"
— 18-0
UPPER WING
LOWER WING
ULlli
1ST PLACE WINNER THOMPSON TROPHV
RACE,CHICAGO,ILLINOIS, SEPT 1,1930
20 LAPS AROUND A FIVE MILE COURSE
100 MILE TOTAL,-ELAPSED TIME:29:43
201.91 M.P.H.- PRIZE MONEY $5,000
1:24
I 48
MATT
LUEVANO
SCALE - ORIGINAL
REPRO.
DRAWN BY: PAUL R
INKED BY1 HERMAN
HAMILTON-STANDARD GROUND
ADJUSTABLE PROPELLER,
UNPAIN TEO.
© HISTORICAL AVIATION ALBUM 1969
P 0. BOX 33
LAIRD LC-DW-300 "SOLUTIOl
WINNER I930TH0MPS0N TROPHY RACE
FUSELAGE В ALL STRUTS
GLOSS BLACK
WINGS & TAIL SURFACES
METALLIC GOLD
LETTERING a NUMBERS
WHITE ON BLACK,
BLACK ON GOLD
LAIRD INSIGNIA DESCRIBED
ELSEWHERE
CONTROL
STICK
CONNECTED
DIRECTLY TO
AILERON
TORQUE TUBE
о 0
21'-0"
ALUMINUM SHEET EXTERIOR
CENTER SECTION LEADING EDGE
AIRFOIL NACA M-12
(DEVELOPED INTO NACA 2212)
ORDINATES UPON REQUEST
I
15*
24'
BALSA WOOD HEADREST,
PLYWOOD DECK FORMERS,
FABRIC COVERED
ENTIRE COCKPIT AREA
PYROLIN COVERED
SIDES FOLD DOWN FOR
COCKPIT ENTRANCE
76"—
5
WINDSCREEN
SLIDES^
FORWARD
APPROX
WINGS CONSTRUCTED OF
WOOD SPARS AND RIBS,
WIRE TIE RODS, FABRIC
COVERED
,3	4	5	6 feet
SCALE BAR
NO SHOCK ABSORBING SYSTEM
EMPLOYED ON LANDING GEAR,
LOW PRESSURE BALLOON
TIRES TOOK SHOCK.
INC
M-12 AIRFOIL
SAME SCALE AS DRAWING
OUR SINCERE APPRECIATION IS EXTENDED TC
MAJ. TRUMAN S WEAVER, USAF RET, MAJ ROE
HIRSCH, USAF RET, E M MATTY LAIRD, KEN. <
WILSON, HARVEY LIPPINCOTT AND EVE.
CASSENGERES OF THE CONNECTICUT AVIATI
HISTORICAL ASSC FOR THEIR ASSISTANCE
THE PREPARATIONS OF THESE DRAWINGS.
1ST0RK
AviATl
AAlb
Laird LC-DW-500
"Super Solution"
Jimmy Doolittle in front
of Laird Super Solution,
September, 1931.
INTERNAL TUBULAR
STEEL CONSTRUCTION
FAIRED RUDDER
HORNS
ALL RIBS, 6" ON CENTER
(DRAWING No8-74-a|
PLATE 2 of 2
(LEFT ROCKER ARM
HOUSING OF »----
EACH CYLINDER)
VIRIDIAN GREEN
LICENSE
VIRIDIAN GREEN
NUMERALS
SAME STENCIL USED ON
FUSELAGE "400"
SCALE BAR, meters

Laird. Super Solution
COLORING NOTES
FUSELAGE, STRUTS, WHEEL PANTS, VERTICAL TAIL
SURFACES - BRIGHT VIRIDIAN GREEN
WINGS, HORIZONTAL TAIL SURFACES, WHEEL PANTS
TRIM, No. 400 - "KODAK" YELLOW
"Skyways krc.? FLAMINGOS DECOR, - DEEP RED
LICENSE ON RUDDER & FIN - BLACK
FOR LAIRD EMBLEM DETAILS SEE HISTORICAL
AVIATION ALBUM, VOL VII, LAIRD "SOLUTION?
BACKGROUND OF DECAL BEING CLEAR VARNISH
CHANGES THIS AREA, AND THIS ALONE, TO
SUPER SOLUTION GREEN
SCALE BAR, feet
ISTWAL
1VIADON
/Ulbum
LAIRD LC-DW-500
"super solution"
WINNER 1931 BENDIX TROPHY RACE
SCALE- ORIGINAL 124
REPRO I 48
DRAWN BY PAUL R MATT
© HISTORICAL AVIATION ALBUM 1970
P 0. BOX 33
TEMPLE CITY., CALIF. 9(780
91%
ANKLIN GOTHIC
YLE LETTERING.
RIDIAN GREEN
GENERAL SPECIFICATIONS
BENDIX TROPHY CONDITION
GHT EMPTY
)SS WEIGHT
L CAPACITY
CAPACITY
/ER - PRATT a
ю --
42
36
meters
SCALE BARS
£_Q1H
1____l'// DIH.
18-0
4-5
LER S/N 36382-36385
SIGN No. 2IAI-7
6 50x10
B.F GOODRICH
TIRES -----
CARBURETOR INTAKE a OIL COOLER
BEHIND BOTTOM CYLINDER WITHIN
COWL.
COwL
FIREWALL
1,580 lbs.
2,160 lbs. (Approx.)
112 gals.
II gals.
WHITNEY WASP JR.
ENGINE USED IN BOTH BENDIX AND
THOMPSON RACES WAS THE
DIRECT DRIVE WASP Jr., S/N
X-27 "YELLOW JACKET."
COMPRESSION RATIO 61, BLOWER
GEAR RATIO 10*.I, BOOSTED TO
APPROX. 525 H P. (NORMAL 435/450H.P)
AIRFOIL M-12 (TWICE SCALE)
DEVELOPED INTO NACA 2212
METAL FILLET
SLIDING FUEL HATCH
NAVIGATION
AIR INTAKE
OIL GAUGE
OIL FILL
HAND FORMED COWL &
WHEEL PANTS BY—
HILL STREAMLINERS OF
CINCINNATI, OHIO
2l'-0
I
2 3
4
эИ»‘
эК
8-3
1ST
INSET NAV
LIGHT
ON-STANDARD
D ADJUSTABLE
LLER
l7-972
PYROLIN WINDSCREEN
I LEATHER STRAP,
CANOPY HANDLE
HISTORICAL AVIATION ALBUI\
RO BOX 33
")TE~ YELLOW STRIPE
APPLIED FOR THE
SCALE- ORIGINAL I 24
REPRO I 48
DRAWN BY- PAUL R. MATT
WINNER BENDIX TROPHY RACE, BURBANK, CAI
TO CLEVELAND, OHIO, SEPT 4, 1931, THENSE
TO NEWARK, N J , 2,882 MILES IN II HRS-, 16 I
FOR FULL TRANSCONTINENTAL SPEED RECOF
AVERAGE SPEED FOR BENDIX RACE 223.038
AND 217 MPH AVERAGE FOR ENTIRE FLIGHT
ENTIRE AMIDSHIP COCKPIT
ENCLOSURE SWINGS OPE
SIDE PANELS HINGED ON
EITHER SIDE ON TOPSIDE
LONGERON, ALLOWING SIC
TO FOLD OUTWARD. CLEX
TO WINDSCREEN SLIDES
PARALLEL SIDE TRACK:
OUR SINCERE APPRECIATION Ц
EXTENDED TO MAJ. ROBERT H
USAF RET., MAJ. TRUMAN C. W
USAF RET., E. M."MATTY" LAIRI
EV. CASSENGERES (САНА) FO
THEIR ASSISTANCE IN THE PF
TION OF THESE DRAWINGS
LAIRD LC-DW-5C
"SUPER SOLUTION
WINNER 1931 BENDIX TROPHY RX
I AIRSPEED INDICATOR
2	ALTIMETER
3	TURN AND BANK
4	COMPASS
5
VERTICAL SPEED INDICATOR
6
(RATE OF CLIMB)
COURSE INDICATOR
(RIGHT/LEFT OF BEAM)
8
9
IO
II
REVERSING SWITCH, C.l.
REVOLUTION, ENGINE R PM
BOOST INDICATOR
THREE NEEDLE INDICATOR
FUEL LEVEL
12 COCKPIT ILLUMINATION
13 CHECK UGHT, BOMB RELEASE
14 AMPERE METER
15	DIRECTION FINDER
16	FREQUENCY REVERSING SWITCH
17	CYLINDER HEAD TEMP.
18	IGNITION SWITCH
19	STARTER SWITCH
20	CLOCK
21	UNDERCARRIAGE INDICATOR
22	SWITCHES
23	HYDRAULICS PRESSURE GAUGE
24	BRAKE PRESSURE GAUGE
25	AIR INSTALLATION PRESSURE
26	UNDERCARRIAGE CONTROL
27	LANDING FLAP INDEX
28	AIR CANNON CHARGING
29	DIRECTION FINDER
30	MANUAL CHARGING OF CANNON^.
31	DATA PLATE	W
32	LANDING FLAP CONTROL
33	THROTTLE
34	PROPELLER PITCH CONTROL
35	ENGINE STOP
36	BOOSTER CONTROL
37	OIL CONTROL CONTROL
38	RUDDER CONTROL, TRIM TAB
39	ELEVATOR TRIM CONTROL
40	BOMB BLOCKING, ARMING
41	MAIN AIR VALVE
42	COCKPIT AERATION
43	COCKPIT CLOSING LEVER
44	COCKPIT AERATION, CZECH
VERSION ONLY
45	MIXING VALVE, FUEL TO OIL
46	FUEL PUMP
47	FUEL INJECTION PUMP
48	FUEL COCK
49	HYDRAULICS MAIN VALVE
50	OXYGEN PRESSURE	23
51	OXYGEN REGULATOR
52	EMERGENCY CANOPY RELEASE
53	SIDE LOUVRES CONTROL
54	FRONTAL LOUVRE CONTROL
55	BRAKE LEVER
56	CANNON TRIGGER
57	BOMB TRIGGER, RELEASE
SCALE-SEE SCALE BAR
DRAWN BY- JOSEF KRYBUS
PRAGUE,
CZECHOSLOVAKIA
___________________________

GENERAL SPECIFICATIONS
CONSTRUCTION NOTES
FUSELAGE - WELDED STEEL TUBULAR STRUCTURE,
WOOD AND METAL FORMERS, IRISH
LINEN COVERED AMIDSHIP, ALUMINUM
COVERED FORWARD AND AFT PORTIONS
WING- ONE PIECE, TWO LAMINATED FULL SPAN SPRUCE
SPARS, REINFORCED PLYWOOD RIBS,
SINGLE WIRE MACWHITE TIE LINES,
3/32" THREE PLY HASKELITE VENEER
COVERING AND IRISH LINEN FINISHED
AILERONS & FLAPS -SAME CONSTRUCTION AS WING,
ALL TORQUE TUBE OPERATED
HORIZONTAL STABILIZER - SAME AS WING, ADJUSTABLE
FROM COCKPIT
ELEVATORS & RUDDER - WELDED STEEL TUBING, LINEN
COVERED
FIN- STEEL TUBE , ALUMINUM FAIRED, LINEN COVERED
3,195 lbs
3,300 lbs.
4,923 lbs.
330/350 m.p.h-
з'-ю'
PATCH
COCKPIT WINDOWS
PART AT CENTER
LINE, SLIDE DOWN
INTO FUSELAGE
WALLS ON CHANNEL
GUIDES
PLACE
PLACE
PLACE
AT
AT
AT
253-802
283.419
282.536
3,765 lbs.
3,765 lbs.
412 m.p.h. (i939)
87 m.p.h.
m.p.h. 1937
mph. 1938
m.p.h. 1939
95 sq.ft.
lbs./sq.ft.
4.92 Ibs./hp
9'- 5
$ feet
0
2
meters
SCALE BAR
PITOT
TUBE
FLAT BLACK
ANTI-GLARE
FINISH
RACING NUMBER ON
UNDERSURFACE OF
RIGHT WING IN SAME
POSITION.
!’.£* |NC._
25'- 2‘/2
WEIGHT EMPTY
(WHEN AIRCRAFT ORIGINALLY
LEFT THE LAIRD FACTORY)
WEIGHT EMPTY
(IN LATER MODIFICATIONS)
GROSS WEIGHT, LIGHT LOAD
GROSS WEIGHT, FULL LOAD
(LAIRD CONSTRUCTION LIMITS)
GROSS WEIGHT, OVERLOAD
(turner's Figure)
WING AREA
WING LOADING, full load cono.
POWER LOADING
MAX. SPEED, ESTIMATED STRAIGHT
AWAY FLIGHT AT S. L.
(LAIRD CO & UNITED AIRCRAFT
COMPUTATIONS)
ROSCOE TURNER’S PERSONAL
CLAIM
LANDING SPEED, with flaps
POWER. PRATT & WHITNEY
SIB3-G, s/n 177
14 cyl. TWIN ROW WASP Sr, 1830 cu. in.
DISPLACEMENT. MFGR. RATING
900 hp AT 2450 RPM AT 6,500 FEET
1,000 hp AT 2600 RPM, S.L, TAKEOFF
USING 87 OCTANE FUEL
THOMPSON TROPHY RACE RECORD
3rd
1st
1st
AE93XN
5-9
AIRFOIL NACA 23000 SERIES
(EXACT SECTION UNKNOWN)
ROOT AND THEORETICAL TIP
AIRFOIL NOT SYMMETRICAL, NO
WASH-IN OR WASH-OUT, ROOT SECTION
SAME AS TIP
4'-CT
FABRIC _____
OVER ABANDONED
NAVIGATION LIGHT
FITTING, SIMILAR
TREATMENT ON LEFT
WING AND ON THE FIN
OIL FILL
ACCESS
UNDER LOUVERED
COWLING
372
SWEEPBACK
SCALE BAR
3‘4’at M.A.C.
TWIN OIL COOLER
AIR INTAKES
CARBURETOR AIR INTAKE AND BLEED
DUCTING OF AIR DOWN THROUGH DUCT
BUILT IN THE OIL TANK SKIN OF TANK
ANO DUCTING WAS ACCORDIAN PLEATED
FOR ADDITIONAL COOLING.
NOTE
OUR
TAKEN
BLUEPRINTS AND A REVIEW OF SURVIVING
LAWRENCE BROWN AIRCRAFT CO. MATERIAL
COLORING NOTES
BASIC AIRFRAME DIMENSIONS WERE
FROM THE E.M. LAIRD AIRPLANE CO.'s
ENTIRE AIRCRAFT- SILVER DOPED
NUMBERS & LETTERING-BLACK
(NO PIN STRIPING)
SPONSOR'S ADVERTISING LOGO-AS NOTED
Ino лилмг ki л ir'i _ a a _ л I
COILED CAPILARY
FOR OUTSIDE AIR
TEMP GAUGE
(COVERED OVER FOR
1938 RACES)
ISTOkKaL
iVIADON
LAIRD- TURNER LTR-14
LAIRD-TURNER RACER - 14 CYLINDER ENGINE
_________1939 CONFIGURATION___________
SCALE - ORIGINAL I 24
REPRO. I 48
DRAWN BY- PAUL R MATT
TFMPI F PITY ГЛ1 IF Э17ЯГ)
© HISTORICAL AVIATION ALBUM 1971
P.O. BOX 33
GENERAL SPECIFICATIONS
9'- 5
3,195 lbs.
3,300 lbs.
4,923 lbs.
330/350 m.ph
з'-ю'
5'-9'
ON THE FIN
2
meters
SCALE BAR
BASIC AIRFRAME DIMENSIONS WERE
FROM THE E.M. LAIRD AIRPLANE CO.s
COCKPIT WINDOWS
PART AT CENTER
LINE, SLIDE DOWN
INTO FUSELAGE
WALLS ON CHANNEL
GUIDES
AT
AT
AT
3,765 lbs.
3,765 lbs.
412 m.p.h. G939)
87 m.p.h.
AIRFOIL NACA 23000 SERIES
( EXACT SECTION UNKNOWN)
ROOT AND THEORETICAL TIP
AIRFOIL NOT SYMMETRICAL, NO
WASH-IN OR WASH-OUT, ROOT SECTION
SAME AS TIP
253.802 m.p.h.
283.419 m.p.h.
282.536 m.p.h.
95 sq. ft.
lbs./sq.ft.
4.92 Ibs./hp
24
6 feet
0
COLORING NOTES
FLAT BLACK
ANTI-GLARE
FINISH
RACING NUMBER ON
UNDERSURFACE OF
RIGHT WING IN SAME
POSITION.
LAIRD-TURNER LTR-14
LAIRD-TURNER RACER - 14 CYLINDER ENGINE
________1939 CONFIGURATION____
ENTIRE AIRCRAFT- SILVER DOPED
NUMBERS & LETTERING - BLACK
(NO PIN STRIPING)
SPONSOR'S ADVERTISING LOGO-AS NOTED
SCALE - ORIGINAL H24
REPRO. 1-48
DRAWN BY- PAUL R MATT
WEIGHT EMPTY
(WHEN AIRCRAFT ORIGINALLY
LEFT THE LAIRD FACTORY)
WEIGHT EMPTY
(IN LATER MODIFICATIONS)
GROSS WEIGHT, LIGHT LOAD
GROSS WEIGHT, FULL LOAD
(LAIRD CONSTRUCTION LIMITS)
GROSS WEIGHT, OVERLOAD
(turner's figure)
WING AREA
WING LOADING, full load cond.
POWER LOADING
MAX. SPEED, ESTIMATED STRAIGHT
AWAY FLIGHT AT S. L.
(LAIRD CO & UNITED AIRCRAFT
COMPUTATIONS)
ROSCOE TURNER'S PERSONAL
CLAIM
LANDING SPEED, with flaps
POWER PRATT & WHITNEY
SIB3-G, s/n 177
14 cyl. TWIN ROW WASP Sr, 1830 си. in.
DISPLACEMENT. MFGR. RATING
900 hp AT 2450 RPM AT 6,500 FEET
1,000 hp AT 2600 RPM, S.L, TAKEOFF
USING 87 OCTANE FUEL
THOMPSON TROPHY RACE RECORD
1937
1938
1939
3rd
1st
1st
PLACE
PLACE
PLACE
PATCH
FABRIC _____
OVER ABANDONED
NAVIGATION LIGHT
FITTING, SIMILAR
TREATMENT ON LEFT
WING AND
PITOT
TUBE
NOTE
OUR
TAKEN
BLUEPRINTS AND A REVIEW OF SURVIVING
LAWRENCE BROWN AIRCRAFT CO. MATERIAL
ISTOWCAL
iVIAHON
AE93XN
3'/2’
SWEEPBACK
OIL FILL
ACCESS
UNDER LOUVERED
COWLING
TWIN OIL COOLER
AIR INTAKES
COILED CAPILARY
FOR OUTSIDE AIR
TEMP. GAUGE
(COVERED OVER FOR
1938 RACES)
CONSTRUCTION NOTES
FUSELAGE - WELDED STEEL TUBULAR STRUCTURE,
WOOD AND METAL FORMERS, IRISH
LINEN COVERED AMIDSHIP, ALUMINUM
COVERED FORWARD AND AFT PORTIONS
WING- ONE PIECE, TWO LAMINATED FULL SPAN SPRUCE
SPARS, REINFORCED PLYWOOD RIBS,
SINGLE WIRE MACWHITE TIE LINES,
3/32" THREE PLY HASKELITE VENEER
COVERING AND IRISH LINEN FINISHED
AILERONS & FLAPS - SAME CONSTRUCTION AS WING,
ALL TORQUE TUBE OPERATED
HORIZONTAL STABILIZER - SAME AS WING, ADJUSTABLE
FROM COCKPIT
ELEVATORS & RUDDER - WELDED STEEL TUBING, LINEN
COVERED
FIN- STEEL TUBE , ALUMINUM FAIRED, LINEN COVERED
5-9
1’4* INC.
SCALE BAR
25'-2/2
CARBURETOR AIR INTAKE ANO BLEED
DUCTING OF AIR DOWN THROUGH DUCT
BUILT IN THE OIL TANK. SKIN OF TANK
AND DUCTING WAS ACCORDIAN PLEATED
FOR ADDITIONAL COOLING
3’4’at M.A.C.
© HISTORICAL AVIATION ALBUM 1971
P.O. BOX 33
36"
METAL GAP
COVER STRIPS
(TWICE SCALE)
CHAMPION SPARK PLUG LOGO
YELLOW BACKGROUND, DARK BLUE
PINCHED BAR, 'CHAMPION'WHITE,
SPARK PLUG WHITE WITH TONE OF
GRAY, BLACK & COPPER.ALL
LETTERING & OUTLINES - BLACK
SCALE BARS
WASP
15 k/ Approx.
TAKEOFF CLEARANCE
UNDER NORMAL CONDITIONS
RETRACTABLE
STEP BAR
OIL DRAIN
TUBE
ALUMINUM FAIRING OVER
TUBULAR STRUTS.
"STEELITED" STEEL
SHOE SKID
CHROME PLATED
HAMILTON STANDARD
CONTROLLABLE PITCH
PROPELLER. 9'-6”DIA.
3'-IO"
4-10'
CANOPY LOCK, SIDE
PANELS COULD BE
LOCKED IN ANY POSITION
ACCESS HOLE FOR
SCREW DRIVER TO
REMOVE LOUVERED
FUEL FILL, TWO TANKS, COWL AND OIL CAP
105 GALS-EACH
WASP
------^-THRUST
FAIRING BUMP OVER FUEL
LINE AT FIREWALL JUNCTURE
SCARS FROM 1937 ABANDONED-7
CORE TYPE BELLY OIL
COOLER.
ETHYL CORP. LOGO
WHITE 12" DISC, RED TRIANGLE,
YELLOW 'ETHYL' & RADIATING
SUN BURST, OTHER LETTERING
& OUTLINING - BLACK

HEAT FROM EXHAUST STACKS
BASIC LANDING
GEAR WAS A SINGLE
STEEL TUBULAR STRUT,
BALSA WOOD FAIRED &
WRAPPED WITH DOPED FABRIC
(x) FAIRING BUMP
OVER NUT & BOLT
FULCRUM ATTACH-
MENT
24 X 8 " LOW
PRESSURE
GOODYEAR TIRES
23- 4
OUR SINCERE THANKS ГО E.M. "MATTY"LAIRD
AND MAJ. ROBERT HIRSCH FOR THEIR VALUABLE
ASSISTANCE IN THE PREPARATION OF THESE DRAWINGS
[DRAWING No- Ю-83-Д~|
PLATE 2 of 2
9-6
£ THRUST _______
DATUM


EMERGENCY FUEL
DUMP TUBE
METAL ACCESS PANELS
TO CONTROL LINKAGE
6 feet
2
I meters
IO
AIR OUTLET,
FOR DUCTING
THROUGH
OIL TANK
ISTOWCAL
WiAHON
iUlbum
LAIRD-TURNER LTR-14
LAIRD-TURNER RACER - 14 CYLINDER ENGINE
_________1939 CONFIGURATION__________
SCALE- ORIGINAL 1-24
REPRO. I 48
DRAWN BY - PAUL R MATT
© HISTORICAL AVIATION ALBUM 1971
PO. BOX 33
TEMPLE CITY, CALIF. 91780
GENERAL SPECIFICATIONS
RUDDER MOVEMENT t22
0 NATIONAL INSIGNIA
MPLOYED ON TOP
URFACE OF WINGS
ABRIC COVERED
AILERONS
FABRIC COVERED ELEVATORS,
METAL TRIM TAB
HE ТРОГАТЬ (no push)
WHITE
LB
UNPAINTED
E B.
SCALE, feel
SLAT OPEN
(K) LANDING FLAPS DEFLECTION -30
TWO 20 mm
SHWAK CANNON
ACCESS TO FUEL
FILLER CAP
32' l%"
27’ Ю’Чб
8' I l3A"
188. 37 sq ft.
5,512.5 lbs
7,497 lbs
413.2 m ph.
WING SPAN
LENGTH
HEIGHT
WING AREA
WEIGHT EMPTY
TAKE-OFF WEIGHT
MAX. SPEED at S.L
MAX. SPEED at 16,405 ft 392.47m p h
CEILING	32,180 feet
RANGE	434.7miles
POWER - ASH-82 FNU TWIN ROW RADIAL,
14 CYLINDER, 1,775 H P. (metric rating)
ARMAMENT - La 7, MOSKWA BUILT, 2 SCHWAK 20mm
(9.8m )
(8,5m)
(2,8m )
(17,5 М2)
(2.500 kg.)
(3.400 kg.)
(665 km/h)
(632 km/h)
(10.000 m)
( 700 m)
D.G.
E.B.
D.G.
D.G.
E.B.
CANNON
La 7, JAROSLAV BUILT, 3 SCHWAK 20mm CANNON
La 7U, 2 SEAT TRAINER, I SCHWAK 20mm CANNON
La 7, WITH ROCKET ENGINE ADDED FOR TEST
ONLY, 1947
ALL AIRCRAFT CAPABLE OF CARRYING IN ADDITION,
TWO 120 OR 150 kg ( 264.5/330.7 lbs )
BOMBS OR SIX RS-82 ROCKETS.
AIRCRAFT ALL METAL CONSTRUCTION, ALUMINUM
COVERED, INCLUDING LANDING FLAPS,
EXCEPT CONTROL SURFACES, WHICH
WERE FABRIC COVERED
(j) AILERON MOVEMENT

D.G.
INSPECTION
PANELS
HO 25 lbs BOMB
(50 kg ) TYPICAL (block)
SCALE, meters
E.B.
NAV.
LIGHT
VENTURI
FUSELAGE
FUEL TANK
ACCESS PANEL
LAVOCHKIN LA-7
SCALE - 148
DRAWN BY- JOSEF KRYBUS
PRAGUE,
CZECHOSLOVAKIA
INKED & TRANSLATED FOR
REPRODUCTION BY- PAUL MATT
Q ELEVATOR MOVEMENT *
DRAWING No AA-46-A
PLATE I of 4
7c)AERO ALBUM 1968
P.O, BOX 33
TEMPLE CITY, CALIF. 91780
VISUAL MECHANICAL
FLAG MOVES UPAS
LANDING GEAR IS EXTENDED -
32‘l'V (9.8m)
RED
DARK BLUE
BLACK
OTHER COLORS AS NOTED
WHITE
SCALE, meters
DATUM__
137/ Approx.
FABRIC
COVERED
RUDDER,
METAL TRM TAB
FAIRING OVER BOMB
RACK FITTINGS
COMPRESSED
ACCESS
OIL COOLER FLAP,
FULLY DEFLECTED
l'A* ABOARD CANT
W OF MAIN STRUT
ACCUMULATOR
ACCESS PANEL
AIR
E.B.
D.G.
L.B.
EARTH BROWN
DARK GREEN
LIGHT BLUE
X)- BACK ARMOUR GLASS-75 mm
Y)- BACK ARMOUR PLATE - 8 mm
AIR TO
CABIN
FRONTAL LOUVRES CONTROLLABLE
FROM COCKPIT, RING COMPRESSOR-
BLADE FAN BEHIND AND FORWARD
OF ENGINE TO ASSIST IN COOLING
DURING WARM WEATHER OPERATIONS
COLORING NOTES
2 7/ M.A.C.
AIR TO
COMPRESSOR ,
CANNON COOLING . j'J
INTAKE	! 1 !|
8' 8” (2i7ml
2	3	4
SCALE, feet
zrioV-IM!!!)
LIGHT GRAY
COLOR
LAVOCHKIN LA-7
SCALE - Г-48
DRAWN BY-JOSEF KRYBUS
PRAGUE.
CZECHOSLOVAKIA
INKED & TRANSLATED FOR
REPRODUCTION BY- PAUL MATT
(DRAWING No AA-46-a|
PLATE 2 of 4
© AERO ALBUM 1968
P 0. BOX 33
TEMPLE CITY, CALIF. 91780
I	2
। METERS
PORT PROFILE OF POST WAR
LA-7 IN SERVICE OF CZECH
AIR FORCE
?	? FEET
SCALE BARS
NATIONAL INSIGNIA ALSO
ON WINGS. BOTH UPPER
& LOWER SURFACES
LOOP ANTENNA
CABIN AIR VENT
WHITE
BLUE RED
S97-860
DATUM
WHITE LETTERS
& NUMBERS
NON RETRACTING
STEERABLE TAIL
WHEEL
RED ARROW OUTLINED IN YELLOW-
2nd PURSUIT REGIMENT ONLY
MAIN LANDING GEAR DETAILS
TWICE SCALE (Approx.)
LAVOCHKIN LA-7
SCALE- 148
DRAWN BY-JOSEF KRYBUS
PRAGUE,
CZECHOSLOVAKIA
INKED & TRANSLATED FOR
REPRODUCTION BY- PAUL MATT
"© AERO ALBUM 1968
P.O. BOX 33
(DRAWING No. АА-46-д)
PLATE 3 of 4
TEMPLE CITY, CALIF. 91780
AIRCRAFT NATURAL ALUMINUM FINISH,
EXCEPT COLOR DECORE AS SHOWN-
15*7" span _
N-6 GUN —
CAMERA
TRIM TRAVEL
RELIEF VENTS li
BOUNDARY LAYER BLEED DUCTING
466.50" SPAN
ROYAL BLUE
NOSE TO
COLOR LINE-----
3*50’----------------
AT TRAILING EDGE
ON WING REF. LINE
'HAT-IN-THE-RING' INSIGNIA, RED-RING,
HAT BRIM-WHITE, STRIPES-RED, WHITE BACKGRD
STARS-WHITE, DARK BLUE BACKGROUND.
LANDING LIGHTS
TOTAL TAB
SERVO
TAB TRAVELS
ELEVATOR TRIM
34'6" FUSE. LGTH.
FIXED
12'0
AIRSPEED
PITOT
PLENUM CHAMBER
PRESSURE RELIEF
DOORS i
CO&ASS SENSE
ANTENNAE
IFF, VHF COMMAND & VHF HOMING ANTENNAES
ENCLOSED WITHIN FIN	_____
SCALE BAR (feet)
PN
26x6.6", 10 ply TIRE
& LETTERS
DIVE FLAPS IN
EXTENDED
POSITION-
78*30'
TAIL SECTION,RED-AFT OF COLOR LINE-
LETTERS, BLACK ON NATURAL ALUMINUM
BACKGROUND PANEL.
RED 'DANGER'
STRIPE
RED STAR
YELLOW STRIPES & ARROW
BLACK OUTLINE “---------
22x7, 8 ply
TIRE, SHOCK TRAVEL 8',
NOSE & MAIN GEAR
FUSELAGE AFT SECTION
ATTACH POINT, COVER
PLATE OVER LATCH
REMOTE
COMPASS
6 .50 Cal. M-3 M.G.'s,
300 Rounds Each
1200 r.rm.
BOUNDARY
LAYER BLEED
VENTS
ISTOWCAL
iVIARON
((Album
ALTERNATE WINGTANK,'KOREAN WAR'
(FLETCHER, 260 go Is. capacity)
ALL TIP TANKS CYLINDRICAL
IN CROSS SECTION
PLATE 2
Shooting Star
|:48
R. MATT © 1965
LOCKHEED P-80B
SCALE-’
BY; PAUL
BY= ROBLIN LAMBERT
DRAWN
INKED

42' 9.25"
OVER ALL SPAN
PROPELLER, HAMILTON
STANDARD GROUND
ADJUSTABLE
THIN TUBING IS
BRACING FOR WHEEL
FAIRING
® UNIVERSAL
JOINTS
OIL FILLER
NORTH
WIND
RED
WHITE
BLUE
GREEN TIN
SUNSHADE
EMERGENCY
EXIT DOOR
LEATHER PADDED
HEADREST
TWO TUBES BETWEEN
UPPER CYLINDERS ARE
CARBURETOR INTAKES.
LOWER TUBES ARE FOR
OIL COOLING
METERS
NOTE
THIS DRAWING PORTRAYS VARNEY
SPEED LANES "NORTH WIND" MODEL
9 "ORION”, OTHER VARNEY ORIONS
DIFFERED ONLY SLIGHTLY WHILE
OTHER ORIONS, IN PARTICULAR THE
LATE VERSIONS a SPECIAL MODELS,
HAD
OLEO
STRUT
WITHIN
WING
SHOCK
HOUSED
19.5'
12* APPROX
6 OLEO TRAVEL
FULLY EXTENDED DURING
RETRACTION
DULL
BLACK
9.50x12 WHEEL
11.00x12 TIRE
(33xll"0.A.)
VARNEY'S
12223
12224
12225
12226
12227
12228
'PRIONS'
’WEST WIND"
'SOUTH WIND"
'NORTH WIND
'EAST WIND"
WINTER WIND
'SPRING WIND
" NORTH WIND" WAS THE ONLY
VARNEY ORION NOT TO HAVE
FIN LEADING EDGE TRIM PAINT
4—— \ LEATHER
\ BOOT
12 X 5" TIRE
FULL SWIVEL a CASTER
1ST0WCM.
Aviatfjn
Mlbum
MANY MODIFICATIONS.
VARNEY "ORION" COLOR
SCHEME
ENTIRE AIRCRAFT, HIGH GLOSS
INSIGNIA WHITE -ALL
TRIM a ALL LETTERING,
INCLUDING NUMBERS,
VERMILLION OUTLINED
WITH A BLACK PIN STRIPE.
ONLY---------------- **
USED
TWO BASIC COLORS
LOCKHEED INSIGNIA
RED/STAR, STRIPES
DATUM
PLATE
BUMPER a
TIE DOWN
RING
LOCKHEED
ORION
MODEL 9
1931-34
SCALE 148
DRAWN BY- PAUL R. MATT
© PAUL R MATT 1966
Lockheed Vega PV-1
"Ventura"

65-6"-
н-----------22 - О"--
MEAN CHORD
LINE - SPAR
SCALE-ORIGINAL	Г 48
RE PRO.	I .'96
DRAWN BY- PAUL R. MATT
(£) HISTORICAL AVIATION ALBUM 1976
P O. BOX 33
(drawing No. E E ~ 101 -~F|
PLATE 2 of 3
TEMPLE CITY, CALIF. 91780
ii-k.aTIONS
GENERAL SPECIFICATIONS
WEIGHT EMPTY
USEFULL LOAD
GROSS WEIGHT
DESIGN OVERLOAD
SERVICE OVERLOAD
WING AREA
SERVICE CEILING
TOP SPEED
CRUISING SPEED (economcal) 170
CRUISING SPEED (combat)
LANDING SPEED
STALL SPEED, clean
12,500 lbs.
10,000 lbs.
22,500
31,000
34,000
551
27,000
322
SPEED SUPERCHARGERS.
FOWLER FLAPS EXTEND OUT ANO
REARWARD ON TRACKS, LOWERS
BY MEANS OF CABLES * PULLEYS
CAMERA HATCH
(VERTICAL)
250
90
105
knots)
knots)
knots)
knots)
POWER-TWO PAW TWIN-ROW R-2800-31 WASP
ENGINES, 2,000 HP EACH, AT 2700 RPM,
(100 OCTANE FUEL). SINGLE STAGE,
TWO
(28Oknots)
(145
(218
( 78
( 91
RADAR SCANNER DOME
-12-9
[DRAWING No. EE-IOI-c]
PLATE 3 of 3
мпв
ACCESS PANELS,
PAINTED BLACK
STA.
225
MY SINCERE APPRECIATION IS EXTENDED TO
CHARLES SCRIVNER FOR TECHNICAL MATERIAL
SUITABLE TO MAKE THESE DRAWINGS AS
ACCURATE AS POSSIBLE AT THIS TIME.
NOTE:
ONLY MAJOR PANELING AND RIVET LINES
ARE SHOWN ON THESE DRAWINGS ALL
SUCH DETAILING WAS NOT NECESSARILY
TRANSFERED FROM ONE VIEW TO ANOTHER.
TWIN 30 CAL. BROWNING MACHINE
GUNS, 2000 ROUNDS TOTAL,
50’HORIZONTAL , 78’ VERTICAL
ARC OF FIRE
RECOGNITION LIGHTS (3)
RED (FWO.), AMBER, GREEN (AFT)
FLAT PLATE GLASS
BOMBARDIER WINDOW
SCALE - ORIGINAL Г48
REPRO.	1.96
DRAWN BY-PAUL R. MATT
ANTI-STALL SLOTS
42“ DIA. NATIONAL INSIGNIA
LANDING LIGHT-
RETRACTED POSITION
BLACK RUBBER DE-ICING BOOTS,
FITTED FOR COLD WEATHER
OPERATIONS.
□
□
n
J
lbs
lbs.
lbs.
sq. ft.
feet
mph I
mph I
mph i
mph
mph
FLARE TUBE
METERS
SCALE BARS
STA
STA.
REFERANCE
FROM FUSE. STA 0
STA
104
STA STA
STA
STA.
255
STEEL RftNEL
OIL COOLER
HOT AIR EXIT
DOORS
REPRESENTATIVE
INTERIOR
ISTORJCAL
iVIATbJN
AAlbum
COLORING NOTES
U.S. NAVY PV-I MODELS
1942-43, BLUE GRAY-PLAN VIEW AND
UPPER SURFACES.
LIGHT GRAY- UNDERSURFACES.
1944-45, TRI-COLOR, DARK SEA BLUE
UPPER AND PLANVIEW SURFACES
BLENDING TO INTERMEDIATE
ON SIDE VIEW SURFACES-
WHITE UNDERSURFACES.
ALL COLORS WERE NON-
SPECULAR, DULL FINISH.

LOCKHEED-VEGA PV-I
"VENTURA"
_________1941-45________
© HISTORICAL AVIATION ALBUM 1976
R 0. BOX 33
TEMPLE CITY, CALIF. 91780
GENERAL SPECIFICATIONS
STEEL TUBE COI
INTERNAL
DRAG WIRES
MASTER DRAG
WIRE
WINGS OF I BEAM SPRUCE SPARS,
WOOD RIBS, WIRE BRACED, FABRIC
COVERED
=>0WER CATO AIR COOLED 2-CYL.
HORIZONTALLY OPPOSED ENGINE
5’’B0RE 6" STROKE
NORMAL RATING 68 h.p.
MAX. RATING 72 h.p. AT 1825 r.p.m-
WEIGHT EMPTY
USEFUL LOAD
GROSS WEIGHT
TOP SPEED
CRUISING SPEED
LANDING SPEED
CLIMB 4,800 FT. IN 10 MIN.
RANGE AT CRUISE	240 miles
WING AREA, INCL AILERONS 187 sq. ft.
WING LOADING	5.2 Ibs./sq. ft
POWER LOADING	13 5 Ibs./h.p.
IO' R
37*
SCALE BARS
12" R
8'/2"a
19V
ALUMINUM NOSE COWL
0. A. OPERATING CLEARANCE
OF ENGINE
AILERON "THROUGH
CABLE
CATO No. 4 AIRFOIL
(MODIAED U.S.A 6 SECTION)
ORDINATES UPON REQUEST
© HISTORICAL AVIATION ALBUM 1972
P.O. BOX 33
SCALE - ORIGINAL H24
REPRO. 1-48
DRAWN BY- PAUL R MATT
595 lbs.
383 lbs
978 lbs.
72 mph.
60 mph.
30 mph.
FIN OFFSET I
AILERON
RETURN CABLE
JURY STRUTS
SHORT
VENTRAL
STRUTS
4 INC
FUEL FILL ft GAUGE
(12 gals CAP.)
ISTORKAL
Aviation
AAlbum
LWF-CATO Model L
“BUTTERFLY"
1919- 1920
P.O. BOX 33
TEMPLE CITY, CALLE. 91780
COLORING NOTE
20'-10'
ENTIRE AIRCRAFT SILVER DOPED
______DRAWN BY- PAUL R, MATT______
© HISTORICAL AVIATION ALBUM 1972
RO. BOX 33
TEMPLE CITY, CALIF, 91760
DRAWING No. II-84-A
PLATE 2 of 2
GENERAL SPECIFICATIONS
RUDDER AT
Г INC.
PERF FIGURES,
FULL LOAD-NO BOMBS
..CHORD
WING AIRFOIL L-W-F No. I
METERS
INBOARD RIBS
OUTBOARD
CD A KI
WEIGHT EMPTY
PILOT & GUNNER
WATER (14 gals.)
FUEL (90 gals ) & OIL (6 gals.)
ARMAMENT, 7 GUNS
3R0SS WEIGHT
ГОР SPEED
SERVICE CEILING
CLIMB to 10,000 feet
WING AREA
ENDURANCE at FULL SPEED
CRUISING SPEED
LANDING SPEED	______.....
CRUISE , as BOMBER, 90m.p h. - 4 hr. duration
ENGINE, LIBERTY 12 rated 435 B.H.P. at 2,100r.p.m.
CRUISE, at 1,800 r.p.m
2,675 lbs.
330 "
118 "
598 “
302 ••
4,023 "
134 “
24,000 ft.
9 min 20 sec
516 sq.ft.
3 hrs.
90 m p h.
50 m.p.h.
STAB. AT Z____|
AIRFOILS TWICE SCALE
STAGGER
FEET
GUNNER'S STOOL
12’ З1/-'
24" !
COLORING NOTES
ALL PLAN VIEW SURFACES -DARK EARTH BROWN
(UPPER SURFACES OF WINGS, TAIL SURFACES
& TOP OF FUSELAGE TO COLOR LINE______________
UNDER SURFACES- PALE SKY BLUE
STRUTS-CLEAR VARNISHED
UPPER & LOWER WINGS ARE OF THE SAME
BASIC DESIGN & CONSTRUCTION. INSIGNIA
ON UNDER SURFACE OF LOWER WING IN
SAME POSITION AS UPPER
1ST0WCAL
I VIATON
Ulbum
L.W.F. model g
1918
SCALE - Г 24 REPRO I 48
DRAWN BY PAUL R MATT
INKED BY HERB KELLEY
PLATE
© HISTORICAL AVIATION ALBUM 1965
P. O. BOX 33
TEMPLF CUTY CALIF. 917 80

GENERAL
SPECIFICATIONS
12,400 LBS.
7,600 LBS
20,000 LBS
BALL
SOCKET
INTERPLANE BRACING REF
® STRUTS
28 - О"
0123456789 10feet
SAME
AILERON CABLE AND
GUIDE SLEEVES
PLY VEENER
LEADING EDGE
© HISTORICAL AVIATION ALBUM 1972
P. O. BOX 33
SCALE - ORIGINAL 1-48
REPRO. V96
DRAWN BY- PAUL R. MATT
UPPER AND LOWER WINGS OF
PHYSICAL SHAPE, SIZE AND
CONSTRUCTION
AILERON CABLE PULLEY *-60 NATIONAL INSIGNIA
HOUSING & SLIP GUIDES
CENTER VERTICAL, RUDDER ONLY, NO FIN EMPLOYED
io-о
PITOT VENTURI MAST
CUTOUT FOR
SINGLE VENTRAL
.30 CAL. LEWIS
M. G. ON SOCKET
SWIVEL
WEIGHT EMPTY
USEFUL LOAD
GROSS WEIGHT
WING AREA (INCL. AILERONS) 2,000 SQFT.
POWER LOADING
TOP SPEED, S. L.	110 M P H.
CRUISE ENDURANCE, COMPUTED 10 HRS
CLIMB, INITIAL, S.L.
SERVICE
LANDING
POWER:
650 FT/MIN
CEILING, COMPUTED 17,000 FT
SPEED	55M.P.H.
3 LIBERTY 12s 400 HP
@ 1700 RPM
COLORING NOTES
ENTIRE AIRCRAFT GLOSS OLIVE DRAB
(GREEN)
A.S. NUMBER 8 WHEEL COVERS-WHITE
NATIONAL INSIGNIA, RED, WHITE 8 BLUE
FUSELAGE POD & OUTBOARD
BOOMS OF 3-PLY WOOD
MONOCOOUE CONSTRUCTION
EXCEPTIONALLY SMOOTH AND
FREE OF IMPERFECTIONS.
OUTER WING PANEL-
ERECTION LUGS
FLACHBAR
WOOD PROPELLER
CAL.
UNS ON
SCARFF MOUNT
3 meters
SCALE BARS
MAIN FUEL TANKS
UNKNOWN)
-AUX.
FUEL
TANKS
(CAPACITY
UNKNOWN)

1Q6'-8" Q:A_Sf»N_________
---------------------53* -4'
CENTER
i SECTION PLY , .
; VENEER COVEFi h
' ED LOWER \ Il
WING ONLY V |i
*. ii
ENGINE SERVICE
'CATWALK'
BOMBARDIERS
WINDOW
WIND DRIVEN
GENERATORS
SLATTED OPENING FOR
IMPROVED DOWNWARD
VISION FROM COCKPIT
ISTORKAL
1VIAIK)N
Mlbum
LWF Model H-l
“OWL"
__________1919-23_______
HISTORICAL AVIATION ALBUM 1971
P.O. BOX 33
10- 0м-
CfDIH.
PITOT VENTURI MAST
-------------20*- O"
8-10.5
26-0
DATUM _
DATUM (BOOMS)
DATUM (Boom)
AILERON RETURN CABLE
PROPOSED 2,000 LBS BOMB
10 /2 Approx.
45-8%
----LWF DIAMOND
TRADE MARK
DRAWING REF: LWF NO. 3822 ANO RELATED,
WITH MODIFICATIONS PER FINAL REVISIONS
OF 9-5-22	,
Юб'-в” 0 A SPAN
RUBBER SHOCK CORD ENCLOSED
IN STREAMLINED STRUT HOUSING
43 X 9" TIRES
FUSELAGE POD
TEMPLATES
MAXIMUM WIDTH OF
FUSELAGE 48W
DATUM (Fu*e.)[



L
21-7.50
OUTBOARD
BOOMS
<t THRUST
OUTBOARD
О I 2 3 4 5 6 7 8 9 10 feet
SCALE BARS
|3 meters
INC. 3 V
MAXIMUM WIDTH
OF BOOM 38"
55'-9
CENTER COCKPIT FOR MECHANIC
OBSERVER, BOMBARDIER,
3 ABREAST SEAT
UPPER STABILIZER SET AT + 4
LOWER STABILIZER SET AT +1-1/2°
6-9.75
[DRAWING No. 11-85-Cl
PLATE 2 of 2
U.S.A. 6 AIRFOIL AT 4.7%
MAXIMUM THICKNESS
SCALE: TWICE GENERAL ARRANGEMENT DWGS.
NOTE UPPER WING SET AT +4®
LOWER WING 1/2* LESS OR 13-1/2*
ISTOWCAL
VIATION
Album
LWF Model H-l
"OWL"
1919-23_________________
SCALE-ORIGINAL 1-48
REPRO. I196
DRAWN BY-PAUL R. MATT
© HISTORICAL AVIATION ALBUM 1972
P. 0. BOX 33
TEMPLE CITY, CALIF, 91780
14'0'
GENERAL SPECIFICATIONS
WEIGHT EMPTY	3700 lbs
USEFUL LOAD	2049 "
WEIGHT GROSS	5749 "
FUEL CAPACITY (INTERNAL) 100 gals.	
OIL CAPACITY	12 "
MAXIMUM SPEED	145 mph
LANDING SPEED	59 "
CRUISING SPEED	95 ”
WING AREA	4 17 sq.ft.
SERVICE CEILING	16,500 feet
RANGE AT CRUISE	400 miles
COLOR NOTES	FOR AIRCRAFT
(GROSS WHT
INT FUEL)
PORTRAYED
ALL EXPOSE METAL AREAS, (FUSELAGE, STRUTS,
FILLET,) - LIGHT GRAY
FABRIC COVERED WINGS - SILVER, (TOP OF UPPER
WING,-CHROME YELLOW)
ALL LETTERING & DETAILS - BLACK
SEATS, CONTROLS, PANEL, SIGHT, GUN - BLACK
INTERIOR AREAS - ZINC CHROMATE (LIGHT GREEN)
UPPER WING CHEVRON & TOP HALF OF ENGINE
NOSE PLATE - WHITE
FAIL SURFACES-RED (AS NOTED)
7'8'
FORMATION
LIGHT (White)
NAVIGATION -
LIGHT (White)
.30 CAL.
LEWIS GUN,
'HORSE-SHOE”
MOUNT\
FOLDING SEAT
(TYPE OPTIONAL)
WING WALK
(Black)
7' 6
HAND HOLD (BLA^)
RED ' BLUE
WHITE
STRUT
ATTACHMENT
POINTS
SERIAL NUMBERS
(BU NOS)
BM-I
BM-2
XBM-I
BM-I
A-8879-8890
A-9I70-9I85
9212
9214-9217
HAMILTON STANDARD ।-----------
10' DIA., ADJUSTABLE
PITCH PROPELLER
(XBM-I TO NACA.
FOR TESTS)
BLUE-
YELLOW
RED-
FABRIC COVERED
ELEVATORS-ENTIRE HORIZONTAL
STABILIZER, TO FUSELAGE JOINT, RED (ABOARD
U.S.S. LANGLEY)
ALUMINUM
LEADING EDGES
0	12	3	4	5	6
11111
SCALE BAR (feet)
6’57'
DULL BLACK PANEL
BACK SIDE OF BLADE
CARBURETOR
INTAKE
ALUMINUM PANEL,
FLOATATION BAG
COMPARTMENT.
TIE ROD /
ALUMINUM
FILLET
STEP PLATE^
FLARE -
TUBE (2)
DARK BLUE
RED
WHITE
CTORKAL
iVIAnON
/(Album
MARTIN BM-I and-2
(1931)
SCALE I 48

GENERAL SPECIFICATIONS
18’11^
9' OV-
4’ 10“
BU. NO. ASSIGNMENTS
AILERON MOVEMENT 1 20
54
48
HINGE
FLIPS
MAIN
PLANVIEW UPPER
WING REMOVED
A 8458 - 8475
A8697-8728
R-I69O
525
18
32
A 7566
A 7596-7649
A 7852-7899
VERSIONS
LAKES AS
UNDERSURFACE
VIEW
ELEVATOR MOVEMENT
TOTAL 153
BLACK WALKWAY
AREAS
21 4
FEET
METERS
20’4
^z’lNC
WINGS
HOISTING A
LANYARD
COMPARTMEN”
DRAWINGS COMPLETED FROM THE
GLENN L. MARTIN CO., CLEVELAND,
OHIO PRINTS R-47600 No.2200,
R-47601 No 2065 AND 4340 OF
9/10/28
LOWER WINGS	”^'GA™N
ONLY	LIGHT POSITION OR
FORMATION LIGHTS
AUX.
STRUT,
BRACE
FOR FOLDEDI
WING ONLY
MARTIN T4M-I
1928-31
SCALE’ L64
DRAWN BY: PAUL R. MATT
_____________ __________| DRAWING No. 4-29-D | PLATE I of 2___________© HISTORICAL AVIATION ALBUM, 1967
-------	SPAN	।	-------
RING! F STAY STRUT Я TIP ОЛП	<	______ __ _	П
LANDPLANE TYPE
WEIGHT EMPTY
USEFUL LOAD
CREW
EQUIPMENT
ORDNANCE
FUEL (104 gals, normal)
OIL (8 gals.)
GROSS WEIGHT (Scout)
GROSS WEIGHT (With Torpedo)
WING LOADING (Full Load)
POWER LOADING (Full Load)
CLIMB IN 10 min.
SERVICE CEILING
ENDURANCE “	’
ENDURANCE
RANGE
RANGE
MAXIMUM
CRUISING
LANDING
FUEL CAPACITY (Normal)
FUEL CAPACITY (Maximum)
POWER, PRATT & WHITNEY
lbs
lbs
lbs.
lbs
lbs.
lbs.
lbs
lbs. /sq ft.
lbs /H P
MARTIN SPECS R-47600
3890 lbs.
347 lbs
400
308
20 79
624
60
6547
7309
I I 0
140
3850 ft.
10,150 ft.
3 5 hrs.
7.5 hrs
435 miles
650 miles
113.2 m.p.h. SL.
98 mph
l*9kl6
(Full Power)
(Cruise)
(Full Power)
(Cruise)
SPEED (Military load)
SPEED	__
SPEED (Light Condition) 56 m.p.h.
104 gals
200 gals
HORNET
H P. at
T4M-I (XT4M-I)
T4M-I
T4M-I
TWIN SISTER
BUILT BY GREAT
THE TG SERIES
TG-I
TG-2
EXACT AIRFOIL UNKNOWN
(PROJECTED FROM AVAILABLE INFORMATION)
з’оЭД
1900 r.p.m.
HCLEAR
JNAV. &
- FORMATION
LIGHTS
DRAG
WIRE
SPAN-WINGS FOLDED
TWIN 30 CAL.-
LEWIS M.G.s
HAND
GRIPS
LINE-SMALL WING PANEL
OVER ON TOP OF OUTER
PANEL DURING WING FOLD
PROCEDURES
FUEL TANK
VENT TUBE
HATCH FOR HOISTING /
SLING, LOWERED
THROUGH WING TO
HOOK ON "A” LANYARDS
ATTACHED TO FUSE.
AT CABANE STRUT
FITTINGS, & CARRIED
WITH AIRCRAFT.
LSKMAL
AviAT}ON
jUlbum
CONTROLS IN
FRONT &
CENTER COCK-
PITS, PILOTS
USE CENTER-
MINIMUM OF
CONTROLS IN
FORWARD PIT.
USED FOR
RELIEF AND
EMERGENCY
MAINLY.
6 6 /j2
I DRAWING No. 4-29-D
© HISTORICAL AVIATION ALBUM, 1967
PLATE I of 2
A
PROPELLER COLOR TIPPED
RED AT TIP, YELLOW
THEN DARK BLUE
FEET
J METERS
I'A inc.
—<t
№
	
SUPPORT
CLAMP
TORPEDO
STARTING
MECHANISM
ZfLOATION BAG
COMPARTMENT
i3*/2’
RUDDER _л.
MOVEMENT -30
STABILIZER
SETTING O*TO*2'
18 x 18 NAVAL
ORDNANCE AERIAL
TORPEDO
39x9" TIRE-
SPOKE WHEEL,
ALUMINUM DISC COVERED
-----IPaH .
SINGLE STAY STRUT & TIE ROD
AT FORWARD SPAR LINE ONLY.
SINGLE STAY ROD AT REAR SPAR

COLOR SCHEME
(AIRCRAFT PORTRAYED)
ALL FABRIC AREAS,	SILVER
ALUMINUM AREAS,	LIGHT GRAY
TAIL SURFACES.	RED
TOP SURFACE OF UPPER
WING,	CHROME	YELLOW
12 llz2
GUIDE HOOKS FOR
FORE & AFT CARRIER
ARRESTING CABLES.
ABANDONED IN I92§
FOLLOWING TESTS WITH SUCH
CABLES ABOARD THE U.SS LANGLEY WING CHEVRON &
WITH A T4M, 5/8/29	LOWER HALF OF
ENGINE NOSE PLATE, BRIGHT MED.
GREEN
all lettering a details, black
INTERIOR: METAL, ZINC CHROMATE GREEN
FABRIC, SILVER
FIXTURES. BLACK
FUSELAGE FABRIC COVERED
AFT OF TEMPLATE 4, ALUMINUM
FORWARD AS WELL AS FAIRINGS
AND INSPECTION PLATES-
HAMILTON STANDARD GROUND
ADJUSTABLE PROPELLER
35'2'
26' 5
HOISTING
XING
16"
WINDOWS
ADJUSTABLE
WINDSCREEN
VT-2B
(TORPEDO SQUADRON TWO)
FIRE BREATHING FLYING DRAGON
DRAGON - RED
SPINE - GREEN
CLAWS & TAIL TIP-YELLOW
TORPEDO - BLACK
REF. U.S. NAVY AIRCRAFT, 1921-1941
by W.T. LARKINS &
artist W MclNTYRE
NIMH
I TORPEDO/
1 ARMING -
MECHANISM
TORPEDO SLING,
CLEVIS & СОТТЁ
[drawing No. 4-294)]
PLATE 2 of 2
TIE DOWN RINGS
FULL SWIVEL TAIL WHEEL
6 SOLID RUBBER TIRE
LEATHER STRUT COVERING
1STOWCAL
iVIAnON
(Ulbum
MARTIN T4M-I
1928-31
SCALE- I:64
DRAWN BY; PAUL R. MATT

© HISTORICAL AVIATION ALBUM, 1967
GENERAL SPECIFICATION
10’5''------
9
COLORING NOTES
AILERON PIVOT LINE
HARDWOOD STRIPS
AS STEP PLATES
BRACE WIRE
TO RUDDER
POST
POWER- CURTISS OX-2 90 hp
gals
min.
lbs. (land plane version)
mp.h
mp.h
m p h
AILERON CONTROL
LINES
ALUMINUM ENGINE COWLING AREA, COCKPIT COMBING-
MEDIUM GRAY
BALANCE OF AIRCRAFT- CLEAR DOPED FABRIC
INTER-PLANE STRUTS - CLEAR VARNISHED ASH
MAIN LANDING GEAR METAL STRUTS - BLACK
UPPER WHIG. OMITTED
Incidence, all wings
AIRFOIL, TWICE SCALE
METAL STRUT SOCKET
& SPAR TIE BRACKET
EXACT ORDINATES UNKNOWN, BELIEVED TO
BE A MARTIN BASED ON AN EARLY
1320 lbs
400 lbs APPROX
1720
96
80
45
12 U
50
10
WEIGHT EMPTY
USEFUL LOAD
GROSS WEIGHT
TOP SPEED
CRUISING SPEED
LANDING SPEED
GLIDE RATIO
FUEL CAPACITY
CLIMB TO 3500 FEET
RECORD CLIMB, 1915, - 5,200 feet in 10 mm I5sec (MARTIN TT No 31)
SERVICE CEILING, 2 PERSONS ABOARD, 9,500 feet
WING AREA	379 sq ft (not incl ailerons)
PULLEY
ELEVATOR
CONTROL LINE
RUDDER
CONTROL LINE
12" WHEEL, ROTATES
FOR RUDDER CONTROL,
MOVES FORE & AFT
FOR ELEVATOR
CONTROL —
5' 2
REMOVABLE
SHEET ALUMINUM FORWARD
OF THIS LINE -
UNDER SURFACE ONLY
О
2
UPPER
UPPER WING LINE
LOWER WING CUT OUT
3	4
METERS
DRAG
WIRES
PARTIALLY EXPOSED
WATER / RADIATOR
PIPES
5	6 FEET
AXLE BAR PIVOT
POINT FOR SHOCK
ABSORBING SYSTEM
SCALE BARS
ISTONGAL
i VIATON
MARTIN model TT
1913-14
SCALE - 1:48

AILERON CONTROL LINES
AILERON PULLEY
(SAME ON LOWER WWG)
© HISTORICAL AVIATION ALBUM 1967
___________P. 0. BOX 33___
6' 6—4-
-<-23 —
57? °inc
DATUM
| DRAWING No. 5 -40-a]
PLATE 2 of 2
FORWARD J
DRAG WIRE
No.37, FITTED
CURTISS MARINE
MILES IN LESS
CLEAR VARNISHED
ASH STUT
OAK TAIL SKID,
BUNGEE CORD SPRUNG
SIGNAL CORPS
AIRCRAFT
PROCUREMENT
NUMBER (BLACK)
AFT DRAG
WIRE
O’ DIH.
BOTH
WINGS
WHITE RUBBER" WAS LIGHT GRAY IN COLOR
ALL SPOKES WERE STRAIGHT, UNCROSSED AT RIMS
OR HUBS
TRIPOD TAIL SKID
BRACE, TUBULAR STEEL
TO STABILIZER AT POINT
(Y) ON PLAN VIEW
THIS AIRCRAFT, MARTIN TT
WITH FLOATS WON THE 1915
TROPHY BY FLYING 443.72 ______________
THAN IO CONSECUTIVE HOURS IN ONE DAY.
PILOT WAS OSCAR A BRINDLEY
27 x 4” - WHITE RUBBER
TIRES. 36 SPOKES,
MARTIN model TT
1913-14
SCALE- 1-48
DRAWN BY- PAUL R- MATT
22 x2.5"- "WHITE RUBBER"
TIRES 20 SPOKES,
© HISTORICAL AVIATION ALBUM 1967
P. 0. BOX 33
TEMPLE CITY, CALIF. 91780

38’ 8“
Please NOTE. TAIL SURFACE BRACE WIRES
OMITTED ON THIS SIDE FOR CLARITY
HEAVY CABLE CENTER SECTION
TIE STRAPS
NOTE FLYING WIRES ARE DOUBLED, ALL
OTHERS SINGLE WIRES
34 O'!---------------
COMPRESSION SPRING SHOCK
ABSORBING SYSTEM HOUSED
IN STRUT FAIRING
SCALE BAR (feet)
SCALE BAR (meters)
24‘ 4 !/2
AILERON CONTROL
CABLE
штпшш
аштошш
1ST0RKAL
AVIATION
AAlbum
GENERAL SPECIFICATIONS
IO'-2-----1—
14,800 ft
330
Г-3"
\TE OF CLIMB to
)WER - 12 CYL. 60
D.B 601 ENGINE, 1,100 HP
BRIC COVERED
.ERONS, SLOTTED,
VEMENT *25* - 13.6
EIGHT EMPTY
SEFUL LOAD
?OSS WEIGHT
OP SPEED of 16,400 ft
MARKED HEAVY -z
CAMBERED RIGHT
SIDE OF FIN TO
COUNTERACT
PROPELLER TORQUE
10 min 2 sec
13 min. 35 sec.
ft
sq. ft
lbs /sq ft
DATA FROM BRITISH RAF (RAE) HANDLING AND
MANEUVERABILITY------—.........
(BAUCH HEMMICHUH) KEEL MATING LINE
BELLY SKID	1
, FABRIC COVERED ELEVATORS,
! MOVEMENT, ♦ or-31 6*
DEG. INVERTED V, GLYCOL
COOLED,GEAR REDUCTION, FUEL INJECTION,
DAIMLER BENZ
TESTS OF AN Me 109, SEPT. 1940
4550
1030
5 580
355
AIR EXIT DOOR
SCALE BARS
3.42'
3.4?‘
OIL FILL (8.5 GALS.)
BLACK OVERALL
NACA 2315
© HISTORICAL AVIATION ALBUM 1970
32-4
GLYCOL ENGINE
COOLANT RADIATORS
EXACT AIRFOIL UNKNOWN, RAE ENGINEERS
FOUND SECTION TO BE NEAR IDENTICAL TO
THE NACA 2300 SERIES
1:24
I 48
SCALE - ORIGINAL
REPRO.
DRAWN BY-PAUL R MATT
INC I 75*
FUEL EMERGENCY
DUMP TUBE
3S0LUTE CEILING
ING AREA
ING LOADING
)WER LOADING
ALLING SPEED
>PROACH SPEED
ENDING SPEED
✓ ING SPEEDS
lbs.
lbs.
lbs
mph,2400rpm
RADIATORS CLOSED T
mph, 2400 r.p m
RADIATORS OPEN
2,430 ft in I min. 16 sec
(2,740 ft /min INITIAL,S.L )
23,000 ft in “
26,300 ft in
32,000
174
32
5 07 Ibs/BHP
61 mph
90 mph
75-80 mph
370-400 mph
2-1
6 feet
2
I rntrs
FABRIC COVERED
SLOTTED FLAPS, MOVEMENT
3 SETTINGS, 0*. 20
L E. SLOT AT MAX. EXTENSION
FAIRING OVER
MAIN SPAR PIN
JOINT
NACA 2310 at tip
----------7.03’ BOOT CHORD
7.9 mm F F
GUN -
EMPTY GUN
SHELLS
RETAINER —
LEAD WEIGHT
MASS BALANCE
IN EAR OF AERODYNAMIC
"HORN” BALANCE. SIMILAR
TREATMENT GIVEN TO RUDDER
FUEL FILL, 88 GALS.,
RED & WHITE TRIANGLE
IDENTIFICATION SYMBOL
OIL COOL AIR
INTAKE
COOLANT HEADER TANK
AIR INTAKE
VISUAL COOLING-DOOR POSITION
INDICATOR, METAL PEG-^
FIXED METAL TRIM TAB
5'-б"_
7.03'
13.35'
AIR EXIT
- DOOR
BRIDGE
HINGE
AILERON
MASS
BALANCEJ
SUPERCHARGER
AIR INTAKE
GUN COOLING VENTS
TWIN SYNCRONIZED
79 mm GUNS
PROPELLER,DULL
MESSERSCHMITT MelO9E-3
________1939-40____________
38' 8"
AILERON CONTROL LINES
HEAVY CABLE CENTER SECTION
TIE STRAPS
AILERON PULLEY
(SAME ON LOWER WNG)
Please NOTE. TAIL SURFACE BRACE WIRES
----------- OMITTED ON THIS SIDE FOR CLARITY
6 6
SCALE BAR (meters)
SCALE BAR (feet)
THAN IO CONSECUTIVE
PILOT WAS OSCAR A
No.37, FITTED
CURTISS MARINE
MILES IN LESS
COMPRESSION SPRING SHOCK
ABSORBING SYSTEM HOUSED
IN STRUT FAIRING
O’ DIH.
BOTH
WINGS
THIS AIRCRAFT, MARTIN TT
WITH FLOATS WON THE 1915
TROPHY BY FLYING 443.72 ______ ______
---- --------------HOURS IN ONE DAY.
BRINDLEY
NOTE FLYING WIRES ARE DOUBLED, ALL
OTHERS SINGLE WIRES
34’0
24' 4,/2‘
♦ 23
- 40
AILERON CONTROL
CABLE
57g*iNC
4’0'
__ —DATUM
CLEAR VARNISHED-^ —
ASH STUT
| DRAWING No. 5-40-a]
PLATE 2 of 2
OAK TAIL SKID,
BUNGEE CORD SPRUNG
SIGNAL CORPS
AIRCRAFT
PROCUREMENT
NUMBER (BLACK)
WHITE RUBBER" WAS LIGHT GRAY IN COLOR
ALL SPOKES WERE STRAIGHT, UNCROSSED AT RIMS
OR HUBS
27 x 4 - WHITE RUBBER
TIRES. 36 SPOKES,
MARTIN model TT
1913-14
SCALE- H48
DRAWN BY- PAUL R. MATT
TRIPOD TAIL SKID
BRACE,TUBULAR STEEL
TO STABILIZER AT POINT
© ON PLAN VIEW
FORWARD J
DRAG WIRE
22 * 2.5 - ' WHITE RUBBER
TIRES 20 SPOKES,
© HISTORICAL AVIATION ALBUM 1967
P. 0. BOX 33
TEMPLE CITY, CALIF 91780
) ]) ])! !h

AFT DRAG
WIRE
ISTtWAL
W1ATON
AAlbum
GENERAL SPECIFICATIONS
14,800 ft
330
l‘-3"
ATE OF CLIMB to
)WER - 12 CYL. 60
D В 601 ENGINE, 1,100 HP
NACA 2315
BRIC COVERED
_ERONS, SLOTTED,
IVEMENT *25* - 13.6
HEIGHT EMPTY
SEFUL LOAD
ROSS WEIGHT
OP SPEED at 16,400 ft.
10 min 2 sec
13 min 35 sec.
ft
sq ft
lbs /sq. ft
DATA FROM BRITISH RAF (RAE) HANDLING AND
MANEUVERABILITY-------—.........—
75*
к
(BAUCH HEMMICHUH) KEEL MATING LINE
BELLY SKID	‘
DEG INVERTED V, GLYCOL
COOLED .GEAR REDUCTION. FUEL INJECTION,
DAIMLER BENZ
13.35'
\ AIR EXIT
- DOOR
FABRIC COVERED ELEVATORS,
• MOVEMENT, ♦ or- 31 6’
IO'-2"—
TESTS OF AN Me 109, SEPT. 1940
4550
1030
5 580
355
AIR EXIT DOOR
2
GLYCOL ENGINE
COOLANT RADIATORS
SCALE - ORIGINAL 124
REPRO. 148
DRAWN BY- PAUL R MATT
BSOLUTE CEILING
ING AREA
ING LOADING
)WER LOADING
FALLING SPEED
3PR0ACH SPEED
ENDING SPEED
VING SPEEDS
lbs.
lbs.
lbs
mph,2400rpm.
RADIATORS CLOSED T
mph, 2400 r.p m
RADIATORS OPEN
2,430 ft in I min 16 sec.
(2,740 ft/min INITIAL, S L )
23,000 ft in *
26,300 ft tn
32,000
174
32
5 07 Ibs/BHP
61 mph
90 mph
75-80 mph
370-400 mph
SCALE BARS
6 feet
FABRIC COVERED
SLOTTED FLAPS, MOVEMENT,
3 SETTINGS, 0*. 20
L E. SLOT AT MAX EXTENSION
FAIRING OVER
MAIN SPAR PIN
JOINT
INC 175
NACA 2310 at tip
------7 03* -R00T CHORD
EXACT AIRFOIL UNKNOWN. RAE ENGINEERS
FOUND SECTION TO BE NEAR IDENTICAL TO
THE NACA 2300 SERIES
MARKED HEAVY
CAMBERED RIGHT
SIDE OF FIN TO
COUNTERACT
PROPELLER TORQUE
7.9 mm FF
GUN-----
EMPTY GUN
SHELLS
RETAINER
LEAD WEIGHT
MASS BALANCE
IN EAR OF AERODYNAMIC
"HORN” BALANCE, SIMILAR
TREATMENT GIVEN TO RUDDER
/FUEL FILL, 88 GALS.,
.RED & WHITE TRIANGLE
IDENTIFICATION SYMBOL
VISUAL COOLING-DOOR POSITION
INDICATOR, METAL PEG-?-
SUPERCHARGER
AIR INTAKE
GUN COOLING VENTS
TWIN SYNCRONIZED
79 mm GUNS
OIL FILL (8 5 GALS )
PROPELLER,DULL
BLACK OVERALL
FUEL EMERGENCY
DUMP TUBE
OIL COOL AIR
INTAKE
COOLANT HEADER TANK
AIR INTAKE
FIXED METAL TRIM TAB
5-6"
7.03'
3.4 2’
13'
BRIDGE
HINGE
AILERON
MASS
BALANCE
MESSERSCHMITT MelO9E-3
_________1939-40___________
© HISTORICAL AVIATION ALBUM 1970
32’- 4 м-
MASS
BALANCE
COCKPIT CANOPY HINGED ON RIGHT
SIDE, ENTIRE CENTER SECTION FLIPS
OVER FOR OPENING. FOWARD SIDE
WINDOWS SLIDE AFT FOR ADDED
PILOT VISIBILITY AND VENTILATION.
at MAC ,
( % CHORD LINE
SWEEPBACK AT
THIS LINE IS I’
FOUND SECTION TO BE NEAR IDENTICAL TO
THE NACA 2300 SERIES
VDM VARIABLE PITCH PROPELLER.
ELECTRICALLY CONTROLLED. PITCH
ADJUSTMENT 22 5е THRU 90*(FULL
FEATHERING) SPUR GEAR REDUCTION
RATIO 14:9
(C) HISTORICAL AVIATION ALBUM 1970
P.O BOX 33
JLEMPL_K_.fU.r_r. ПА! IF Qivan
6-8
2-1%''
— 2-11%
LIFT BAR HOLE
RADIO COMPARTMENT
FULL SWIVEL
TAIL WHEEL
60 lbs. PERMANENT BALLAST
CARRIED WITHIN AFT FUSELAGE
STABILIZER TRIM FROM
COCKPIT, ♦ 3.4° THRU - 8.4
ADJUSTMENT
FABRIC COVERED
RUDDER, MOVEMENT
or - 33.8*
SCALE - ORIGINAL Г 24
REPRO Г48
DRAWN BY PAUL R MATT
5 75'
AILERON
T,E DOW4
CASING RING-----1
HYDRAULIC
BRAKE LINE
PROPELLER SPINNER WAS A HOLLOW, FORME D AIR INTAKE,
TO COOL PROPELLER GEARING AND ENGINE GENERATOR
IT WAS CALLED A KULLERSCHNAUZE (KILLER SNOUT), A
POSSIBLE GUN POSITION. THIS NEVER FITTED AS A
COMBAT FEATURE.
SCALE BAR, feet
SCALE BAR. meters
28'- 8‘
PITOT
IO'-2
DATUM
16 Approx.
DRAWING No AA-75-A
PLATE 2 of 2
MESSERSCHMITT MelO9E-3
________1939-40___________
(c) HISTORICAL AVIATION ALBUM 1970
P.O. BOX 33
TEMPLE CITY, CALIF. 91780
Morehouse 29.IH.P. Aircraft Engine
1925
Top left: Front view
Top right: Top view
Middle left: Right rear view
Middle right: Direct rear view
Bottom right: Bottom view
^1 CYLINDER
OVERFLOW LINE
17 375
2 CYLINDER
5 125
30 250
.. _1_ 6.750
9 750
OIL FILLER
BREATHER
PROP HUB
7.625
OVERFLOW AREA
(SEE LUBRICATION SYSTEM NOTES)
6 00DIA
2 812
WIDTH (REF)
THROTTLE LEVER
OIL LEVEL FLOAT
FUEL CONNECTION
CHOKE LEVER
5.187
5 187
- MATERIALS -
CRANKCASE • ALUMINUM ALLOY CASTING
CRANKSHAFT: S A E. 3240 STEEL FORGING
CONNECTING RODS- FORGED DURALUMINUM
WITH BRONZE PISTON PIN BUSHINGS
PISTONS: MACHINED ALUM WITH 4 125 TEE TOR
RINGS.
CYLINDERS CAST IRON WITH INTEGRAL FINS& VALVE SEATS.
VALVES: COBALT CHROME.
CAMSHAFT & VALVE GEARS: S A E 6120 STEEL.
- LUBRICATION SYSTEM CONT-
TUBES IN CRANKSHAFT CARRY OIL FROM MAIN
BEARINGS TO CRANKPIN BEARINGS THE OVER-
FLOW FROM THE RELIEF VALVE FLOWS THRU
THE COMPARTMENTS AROUND THE CYLINDERS
SKIRTS.
THE OIL SUMPIS PROVIDEDWITH AN OIL LEVEL
INDICATOR. FILTERS & A THERMOMETER FITTING.
- SPECIFICATIONS -
THE FOLLOWING DATA & PERFORMANCE FIGURES ARE
AS REPORTED BY THE POWER PLANT SECTION, MCCOOK
FIELD. ENGINEERING DIVISION, JUNE 15,1925
BORE : 3.750
STROKE: 3.625
DISPLACEMENT : 80.10 CU. IN
COMPRESSION RATIO: 5.10 I
RATED H P. 29.1 AT 2500 RPM AT SEA LEVEL
WEIGHT DRY 89 50LBS.
OIL PRESSURE AT CRUISE RPM: 12.16LB /SQ IN.
FUELCONSUMPTION 5I3LBS./H P. / HR .
THE FOLLOWING H P. RATINGS ARE AT SEA LEVEL:
24 О H P.
24.8 H P
26 OH P.
27 2 H P
28 3 H P
29 I H P
29.6 H P
29.8 H P
CARBURETION•• STROMBERG MODEL OX-2
IGNITION SCINTILLA MAGNETO, DELCO SYSTEM & CHAMPION
SPARK PLUGS.
LUBRICATION SYSTEM: SINGLE GEAR PUMP IN REAR COVER
SUPPLIES OIL THRU DRILLED CRANKSHAFT PASSAGES TO
MAIN BEARINGS, IDLER & CAMSHAFT GEAR BEARINGS
CONT. BELOW
RPM
RPM
RPM
RPM
a 2,050
о 2,100
о 2,200
о 2,300
О 2,400 RPM.
о 2,500 R PM.
о 2,600 R PM
a 2,650 R P M
MAGNETO
MAGNETO ADVANCE LEVER
TACHOMETER CONNECTION
OIL PRESSURE CONNECTION
ISTORKM
Aviation
AAlbum
MOREHOUSE 29.1 H R AIRCRAFT ENGINE
1925
SCALE: 1:16(3/4'« Г)
DRAWN BY: ROB LAMBERT
© HISTORICAL AIRCRAFT ALBUM 1966
NW-2
OVER ALL
RUSTIC BRASS
2480
520
3000
209
56
WEIGHT EMPTY
USEFUL LOAD
GROSS WEIGHT
MAXIMUM SPEED
FUEL CAPACITY
TUBE
RUNNING
FUSELAGE
OIL CAPACITY
LANDING SPEED
WING AREA
NO NATIONAL
MARKINGS OR
INSIGNIA EMPLOYED
ON WINGS
AILERONS TORQUE
OPERATING WITH TUBE
WITHIN WING AND INTO
COLORING NOTES
RACING VERSION, SECOND T-2 BUILT,
NW-I A-6543, RATED 650 H Pat 2000rpr
A-6544 AS SESQUI-PLANE USED T-2
SERIAL NUMBER 6140
GENERAL SPECIFICATIONS
POWER-WRIGHT T-2,SPECIAL HIGH COMPRESSION
RATIO 6-5
lbs.
lbs.
lbs.
m.p.h DURING RACE
gols. ( 337 lbs. incl. in
useful lood)
gals.
71.2 m.p.h
180 sq.ft., incl. ailerons
3 9
MAIN WING PLANES ARE
PLY WOOD COVERED TO
REAR SPAR LINE, FABRIC
AFT. SESQUI-WING ALL
PLY COVERED.
FABRIC AREAS AND PLY COVERED
WING AREAS - SILVER
METAL AREAS - ENGINE COWLING. COCKPIT COMBING,
STRUTS, FAIRINGS, AFT FUSELAGE AREA
BATTLESHIP GRAY (DARK)
ALL LETTERING & DETAILS - BLACK
LAMBLIN RADIATORS
SCALE BAR (meters)
SCALE BAR (feet)
ALL RIB SPACING
6" ON CENTER
8' 10
LAMBLIN WATER
RADIATOR —
OIL COOLING
RADIATOR
CLEARANCE FAIRING
OVER ENGINE PIPING
CARBURETOR INTAKE
negative
INCIDENCE
AIRFOIL M-80 (1921) TWICE SCALE
4
30' 6
ISTORKM
Aviation
AAlbum
PJ-4TE—i_ o<_ ?
NAVY WRIGHT NW-I
1922
SCALE:148
DRAWN BY PAUL R. MATT
TQRICAL AVIATION ALBUM 1967
1
0	12	3	4	5	6
SCALE BAR (feet)
____________________241 n" (approx.)______________
(к1 q"	3x CHORD____________
TO C.G. AT GROSS WEIGHT
RUDDER STRIPES
NOTE •• THESE DRAWINGS AND THE COMPANION NW-2
MODEL WERE COMPLETED FROM ORIGINAL
FACTORY BLUEPRINTS THROUGH
THE COOPERATION AND
RESEARCH OF
THOMAS G. FOXWORTH
ISTOWCAL
iVIATlON
NAVY WRIGHT NW-I
1922
SCALE:148
DRAWN BY PAUL R. MATT
| DRAWING No.4-3I-A~]
PLATE 2 of 2© HISTORICAL AVIATION ALBUM 1967
SPECIFICATIONS
GENERAL
19 */2
£ HINGE
COLORING NOTES
UPPER
WING
RADIATOR
AILERON CONTROL
HORN, UNDER SIDE
ONLY, PUSH ROD
ASSEMBLY.
AILERONS
FABRIC COVERED
POWER-WRIGHT T-2
SPECIAL,
COMPLETE PERFORMANCE TESTS
NOT CARRIED OUT
(bs- ESTIMATED
lbs.
lbs-
m.p.h. DURING RACE
sq ft incl. oilerons
UPPER
aileRon----6’0V
LOWER
. . и AILERON
4 7/.e------
STRUTS
6 FEET
2 METERS
SCALE BARS
NW-2
MOORING
CLEAT
LOWER
WING
RADIATOR
WATER
COOLER TO
COOL THE
OIL
7'6 DIA. SPECIAL HAMILTON PROPELLER CO.
GROUND ADJUSTABLE FORGED DURALUMIN BLADES, STEEL HUB,.
AS EMPLOYED ON NW-2 IN ITS FINAL CONFIGURATION
NO TRUSS ;
WIRES
EMPLOYED
BETWEEN
THESE
‘“—CARBURETOR INTAKE
FAIRING OVER WATER PIPES
__POSITION OF CARBURETOR
INTAKE IN FINAL CONFIGURATION
---27‘ IIV
С FA I Pl МП OVFR PI HMRINH
WEIGHT EMPTY
USEFUL LOAD
GROSS WEIGHT
MAXIMUM SPEED
WING AREA
WING LOADING
POWER LOADING
FUEL CAP. 106 gals.
OIL CAR 8.5 gals.
3565
882
4447
204
26 6
I 6.7 lbs/sq. ft.
6.85 lbs / H P.
(COMPUTED ON BASIS
OF MAX. POWER OUTPUT
OF 650 H.P )
HIGH COMPRESSION
650 H.P AT 2000 R.P M
29‘/41
OVER ALL FABRIC AREAS AND PLY COVERED
WING AREAS - SILVER DOPED
METAL AREAS - ENGINE COWLING, COCKPIT COMBING,
STRUTS, FAIRINGS, AFT FUSELAGE AREA -
BATTLESHIP GRAY (DARK)
FLOATS - BATTLESHIP GRAY DOPED MAHOGANY VENEER
ALL LETTERING AND DETAILS - BLACK
WING RADIATORS - RUSTIC BRASS
6'9
HAND HOLD
TIE DOWN
RING
SERVICE WALKWAY
WINGS
PLY WOOD
COVERED
BOTH UPPER & LOWER WINGS
OF THE SAME PHYSICAL
CONSTRUCTION & DIMENSIONS
1STOWCAL
iVIABON
AAlbum
NAVY WRIGHT
1923
SCALE I 48
DRAWN BY- PAUL R MATT
FROM ORIGINAL MATERIAL SUPPLIED
BY THOMAS G. FOXWORTH
I nvjrviMO—U—rUAWUtt I H
North American 0-47A
General profile and cut-a-way sketches In
block form of prominent details. NAA 0-47
aircraft.
ADJUSTABLE METAL
TRIM TAB, LEFT
WING ONLY
ELEVATORS, METAL FRAMEWORK,
FABRIC COVERED,
TAB, LEFT
ONLY
FIXED METAL
TRIM------ “
WING
STEP PLATE
HAND HOLD
GENERAL SPECIFICATIONS
220.5 MPH
COLORING NOTES
POWER WRIGHT R-1820-49
48
[DRAWING No 13-98-A]
PLATE I of 3
5900 LBS.
I 7 36 LBS
7636 LBS
ENTIRE AIRCRAFT HIGHLY BUFFED
AND POLISHED NATURAL ALUMINUM,
INTERIOR- GREEN ZINC CHROMATE,
DETAILING BLACK OR AS NOTED
COCKPIT
WARM AIR-
COOL AIR MIXING
CHAMBER
STANDARD 36" NATIONAL
INSIGNIA
30 CAL. FIXED BROWNING MACHINE GUN
200 ROUNDS. DOTTED LINE INDICATES
ALUMINUM BARRELL COVER
FLAT ANTI-GLARE
BLACK
FUEL FILL, 3 TANKS IN EACH
WING STUB, 45 GALS TOTAL
PER WING
XO-47 (GA-15) I
0-47A (NA-25) 64
HAMILTON STANDARD HYDROMATIC CONSTANT SPE ED
PROPELLER, REDUCTION RATIO 1611
0-47B (NA-51) 24
50
QUANTITY 23B
NOTE—
ONLY PROMINENT RIVETING AND
PANELING SHOWN ON THESE DWGS.,
ALL WERE NOT NECESSARILY
TRANSFERED FROM ONE VIEW
TO ANOTHER
NORTH AMERICAN 0-47 PRODUCTION
ANO MILITARY SERIAL NUMBERS
BUILT A.C. 36-145
A.C. 37-260 / 323
N G. 37-324/ 368
N.G 38 - 271 / 318
A C. 38-319 / 325
A C. 39-065 / 088
N.G. 39-089/ 138
HORSESHOE "U '
GUN MOUNT, ONE
.30 CAL FLEXIBLE
BROWNING M-2 GUN.
NORMAL ARMAMENT,
WITH 600 ROUNDS.
WEIGHT EMPTY
USEFUL LOAD
GROSS WEIGHT
TOP SPEED, 4,000 FT.
2I00RPM
OPERATING SPEED
1840 RPM
RANGE AT 74 THROTTLE
LANDING SPEED, 45еFLAPS
CLIMB, INITIAL, S.L.
WING AREA (WINGS ONLY)
WING LOADING
POWER LOADING
SERVICE CEILING
ABSOLUTE CEILING
197 MPH
640 MILES
75.6 MPH
1720 MPH
31 3.6 SQ.FT.
2 1.6 LBS/SQ. FT.
9.4 LBS / HP
23,200 FT
24,600 FT.
"cyclone"
RATINGS- S.L. 805 HP at 2100 RPM
835 HP, 3900 FT. at 2100 RPM
975 HP, 5000 FT of 2200 RPM
(TAKEOFF MAXIMUM)
COMPRESSION RATIO 6.45: I
BLOWER RATIO 7: I
MY SINCERE APPRECIATION IS EXTENDED TO
THE REV BOARDMAN C REED FOR HIS
PERSONAL INTERESTAND HELP IN THE
PREPARATION OF THESE DRAWINGS AND
RELATED TECHNICAL FACTS REGARDING
THE 0-47 TYPE AIRCRAFT
ISTOWCAL
WlABON
WBUM
NORTH AMERICAN 0-47A
NAA MODEL 25
1937-39
SCALE-ORIGINAL 124
REPRO. Г-48
DRAWN BY-PAUL R. MATT
© HISTORICAL AVIATION ALBUM 1974
P 0. BOX 33
______TEMPLE CITY, CALIF. 91780
GUNNER'S SEAT PIVOTED ABOUT A
HORIZONTAL AXIS ANO ADJUSTED
TO DESIRED INCLINATION FOR
GUN OPERATION. SEAT BACK
HINGED WITH AN A-3 GUNNER'S
BELT ATTACHED TO THE
FLOORBOARD.
N“2 OPTICAL GUNSIGHT
-TURN-OVER BRACE
* ANTENNA SUPPORT,
ALSO INCORPORATES
HOISTING HOOK FITTING
i- CARBURETOR
AIR INTAKE
ACCESS, COCKPIT INSTRUMENTS
VENTURI (2)
FOR GYRO INSTRUMENTS
— 23
SCALE BAR, feet
DATUM___
12
RETRACTABLE
© HISTORICAL AVIATION ALBUM 1974
OLE OS
OVERLOAD
DEPRESS!
FLARES(2)
AND CONTROLS
RUDDER, METAL FRAMEWORK,
FABRIC COVERED,
METAL TRIM TAB
RETRACTABLE
GROUND SERVICE
STEP BAR
BAGGAGE
COMPARTMENT
OIL COOLER
INTAKE
GROUND LINE
ANTI-STATIC WIRE
BATTERY 1
DRAIN
IQItt OBSERVATION SQUADRON INSIGNIA
WHITE GULL, MED BLUE SKY BACKGROUND,
ENCIRCLED IN A WHITE BAND AND OUTER
RING OF LEMON YELLOW.
12-2
C THRUST_______FRL
® OIL FILL, (9.5 GALS NORMAL)
S) ACCESS, FUEL LINE CONNECTIONS
© FUEL FILL, MAIN TANK. (60 GALS )
© MAIN ELECTRICAL FUSE PANEL
© ACCESS, TRIM CABLES
£) ACCESS, PULLEYS
Г- B-2 LIFERAFT
STOWAGE
AIRFOIL
NACA 2210 AT ROOT
2^-inc
SYMMETRICAL RADIO
BEACON ANTENNA
UHF WITH COAXIAL
FEED LINES -----
SCALE BAR, meters
REEL TYPE ANTENNA
WITH DRAG LEAD &
REAR GUIDE FAIRLEAD
33’-7'
12 Approx
L.E. TO RUDDER HINGE
»— AFT CANOPY EMERGENCY
RELEASE BUTTON
. - FIRE EXTINGUISHER
RED PANEL
AIRCRAFT PORTRAYED-
»1h AIRCRAFT OF THE 101 »f OBSERVATION
SQUADRON, 26th DIVISION AVIATION,
MASSACHUSETTS NATIONAL GUARD-
S/N N.G. 38-307, C/N 25-584
COMPLETED JUNE 9, 1939. FLIGHT
DELIVERED TO lOlet SOON ARRIVING AT
BOSTON MUNICIPAL AIRPORT JUNE 15,1939
ISTORKAL
JVIATON
AAlbum
OIL TANK
BREATHER
TUBE
BAFFLE PLATE,
WINO A DEBRIS
DEFLECTOR
""--CAMERA BAY DOORS
IN OPEN POSITION, ALSO
USED FOR TOW TARGET
SLEEVE LEAD OPERATIONS
ALTERNATING
STRIPES
6'4" «co
7>2" WHITE
ACCESS, TAILWHEEL INSPECTION
- Ю" STEERABLE TAILWHEEL SHOWN
IN 3-POINT GROUND POSITION.
OLEO DROP 6" IN FLIGHT
12.5"TIRE OPTIONAL.
NORTH AMERICAN 0-47A
NA A MODEL E5
___ \ьът-ъъ
SCALE-ORIGINAL 124
REPRO Г48
DRAWN BY-PAUL R MATT
CITY,
North American AT-6D
"Texan"
North American AT-6D, September 6,1948.
North American AT-6. Rear cockpit.
66
GENERAL SPECIFICATIONS
12-llV-
5'-9^
4-0
0* inc.
NACA 4412
— 7-6
meters
7-5^
HOUSING OVER
M G BREECH-:
STAINLESS
STEEL PANEL
INBOARD
L.G. STRUT
GUN
SHELL
EJECTION -
COVER PLATE
RED & WHITE
WARNING
PLAQUE -
FABRIC COVERED
ELEVATORS, METAL
TRIM TABS
RIGHT SIDE PROFILE,
ENGINE EXHAUST DETAIL
FUEL CAPACITY (2 wing tanks)
OIL CAPACITY (incl. expansion
SPACE - 2 GAL.)
POWER- PRATT & WHITNEY R-I340-AN-I
RATED- 600 HP at 2250 RPM at S.L.
550 HP at 2200 RPM at 5,000 ft.
USING 91 OCTANE FUEL
J— £ HINGE
BAGGAGE COMPARTMENT
STEP
FIXED
EXTINGUISHER PANEL (RED)
AIR
7- II’/
150.89
35
120.713
10*18 16
90.139
PITOT TUBE
60357
| DRAWING No. I6-I06-a]
PLATE I of 3
34" DIA. INSIGNIA
SIMILAR AT ALL
FOUR POSITIONS
SCALE- ORIGINAL Г.24
REPRO. Г-48
DRAWN BY- PAUL R. MATT
15.089
29 074
© HISTORICAL AVIATION ALBUM 1979
P.O. BOX 33
TEMPLE CITY, CALIF 91780
WEIGHT EMPTY
USEFUL LOAD
GROSS WEIGHT
TOP SPEED
CRUISING SPEED
LANDING SPEED (with flaps)
RANGE (AT 70% POWER)
WING AREA (incl. ailerons)
WING LOADING
POWER LOADING
SERVICE CEILING
38%
SCARFF MOUNT FOR
.30 Cal. M-2 BROWNING
FLEXIBLE M G., 500 Rds.
(when employed)
DYNAMOTOR COMPARTMENT
(RADIO POWER)
NACA 2215
feet
FIRE
SCALE BARS
INTAKE DOOR (rear cockpit)
FABRIC COVERED
AILERONS, METAL L E.
FORWARD OF THIS LINE
METAL TRIM TAB-x
lbs
lbs.
lbs
mph
mph
mph
miles
4250
905
5155
210
146
67
629
253.73 sq.ft
22.2 lbs /sq ft.
9. 37 lbs/HP
24,700 ft.
110 U.S GALS.
12.2 U.S. GALS
23 км
fuel! FILL ( 55.2 GALS. /SIDE)
NOTE
RIVET LINES ARE DRAWN ON THE
SIDE VIEW AND RIGHT SIDES ON PLAN-
VIEWS ONLY. SIMPLIFIED PANELING IS
SHOWN ON THE LEFT SIDE PLANVIEWS.
ALL LINE WERE NOT NECESSARILY
TRANSFERED FROM ONE VIEW TO
ANOTHER.
WING PANELS DRAWN IN FLAT PLANE.
OIL FILL I
(12.2 GAL.)| lqck PINS
1 STRUT OLEO FILLER
CARBURETOR AIR INTAKE
AMMON
/Ulbum
SHOCK STRUTS
BENDIX
HAYES HYDRAULIC BRAKES
18 DIA
SPINNER
USED ON
REMANUFACT-
URED MODEL
AS T-6G
.30 Cal. SYNCRONIZED
MG., (when employed)-
200 ROUNDS
NORTH AMERICAN AT-6D
"TEXAN” <u-s-navy SNJ-5)
1939-1945___________________________
42’-О V
7" CLEAR LANDING LIGHT, 450 WATT, INBOARD
4" RED PASSING LIGHT, 50 WATT, OUTBOARD
(ONLY LANDING UGHT IN RIGHT WING, ALL LENSES
CONFORM TO WING L E CONTOUR, LIGHT WELLS
PAINTED FLAT BLACK)
x- 8'-6%
GEAR RETRACTION
RADUS
О	VI	2
h— I	I
SCALE BAR meters
5е II' DIH.
IAMILT0N-STANDARD
ONSTANT SPEED
’ROPELLER,
’itch-low nk2e
HIGH 27*
(prop dia on some
NJ-5s WAS 8'-4" TO
LEAR CARRIER DECK
ANDING WIRES)
9-0’
L
a trust
4”i
12 75"
_!____
<8>
ADF SENSING ANTENNA
45.62	31 0
28'- 11%"—
I DRAWING No. 16-IOG-Al
IГ 55' Approx.
t
27” TIRE
OLEO TRAVEL 8.8"
242.188
12.5" TIRE
STEERABLE,
WITH LOCK
34 —
29%“
70 %"
78%"
II'
FABRIC COVERED
RUDDER, COCKPIT
ADJUSTABLE METAL
TRIM TAB
8*4’
F.ft.L.
ISTWAL
IVIADON
/(Album
t~	^4
I I NORTH AMERICAN AT-6D
J- "TEXAN" (US navy SNJ-5)
HYDRAULIC FLUID TANK
GROUND LINE (R 4 L SIDE) COOED BLACK
CARTRIDGE STARTER ACCESS
HAND STARTER CRANK PIN
SERVICE STEP BAR (RETRACTED)
1939 1945
SCALE- ORIGINAL 1:24
REPRO. 148
DRAWN BY- PAUL R. MATT
© HISTORICAL AVIATION ALBUM 1979
PO BOX 33
GENERAL SPECIFICATIONS
— 5’-9%
HINGE
O’ INC
meters
7-53
HOUSING OVER
M G BREECH-?
STAINLESS
STEEL PANEL
INBOARD
L.G. STRUT
GUN
SHELL
EJECTION
COVER PLATE
RED & WHITE
WARNING
PLAQUE----
FABRIC COVERED
ELEVATORS, METAL
TRIM TABS
RIGHT SIDE PROFILE,
ENGINE EXHAUST DETAIL
12'-11^'
FUEL CAPACITY (2 wing tanks)
OIL CAPACITY (incl EXPANSION
SPACE - 2 GAL.)
POWER- PRATT & WHITNEY R-I340-AN-I
RATED- 600 HP at 2250 RPM at S.L.
550 HP at 2200 RPM at 5,000 ft
USING 91 OCTANE FUEL
23 кзг
NACA 2215
BAGGAGE COMPARTMENT
FIXED
FIRE
INTAKE DOOR (REAR cockpit)
AIR
10’18 16
90.139
PITOT TUBE
I DRAWING No. I6-IO6-A~|
PLATE I of 3
SCALE- ORIGINAL 1.24
RE PRO. Г-48
DRAWN BY- PAUL R. MATT
STEP*
EXTINGUISHER PANEL (RED)
© HISTORICAL AVIATION ALBUM 1979
P.O. BOX 33
TEMPLE CITY, CALIF 91780
WEIGHT EMPTY
USEFUL LOAD
GROSS WEIGHT
TOP SPEED
CRUISING SPEED
LANDING SPEED (with flaps)
RANGE (at 70% power)
WING AREA (incl. ailerons)
WING LOADING
POWER LOADING
SERVICE CEILING
lbs
lbs.
lbs
mph
mph
mph
miles
4250
905
5155
210
146
67
629
253.73 sq.ft
22.2 lbs /sq ft.
9. 37 lbs/HP
24,700 ft.
HO U.S GALS.
12.2 U.S. GALS.
feet
SCALE BARS
38^
7-6
SCARFF MOUNT FOR
.30 Cal. M-2 BROWNING
FLEXIBLE M G., 500 Rds.
(when employed)
DYNAMOTOR COMPARTMENT
(RADIO POWER)
FABRIC COVERED
AILERONS, METAL L E.
FORWARD OF THIS LINE
METAL TRIM TAB^

fuel! FILL ( 55.2 GALS. /SIDE)
NOTE
RIVET LINES ARE DRAWN ON THE
SIDE VIEW AND RIGHT SIDES ON PLAN-
i/IEWS ONLY SIMPLIFIED PANELING IS
SHOWN ON THE LEFT SIDE PLANVIEWS.
ALL LINE WERE NOT NECESSARILY
fRANSFERED FROM ONE VIEW TO
ANOTHER.
WING PANELS DRAWN IN FLAT PLANE.
OIL FILL !
(12.2 GAL.)| lqck PINS
1 STRUT OLEO FILLER
’ ^ CARBURETOR AIR INTAKE
ISTORKM
WlATFJN
AAlbum
SHOCK STRUTS
BENDIX
HAYES HYDRAULIC BRAKES
I 18 DIA
SPINNER
USED ON
REMANUFACT-
URED MODELS
AS T-6G
15.089
I STA 0
35
34" DIA. INSIGNIA
SIMILAR AT ALL
FOUR POSITIONS
.30 Cal. SYNCRONIZED
M.G., (when employed) -
200 ROUNDS
NORTH AMERICAN AT-6D
"TEXAN " (US. NAVY SNJ-5)
1939-1945______________________________________

GENERAL SPECIFICATIONS AND DATA
MAXIMUM GROSS WEIGHT - 550,000 lbs.
TOP SPEED- MACH 3 (2,000 m.p.h. ) AT 7Q ООО FEET
POWER- SIX GENERAL ELECTRIC YJ-93 TURBO JETS, 30,000 lbs.THRUST EACH
FUEL- II TANKS, 47,000 gals. TOTAL CAPACITY
TAKEOFF AT 500,000 lbs , 200 knots IN 7,000 feet
AT 400,000 lbs., 180 knots IN 4,000 feet
LANDING APPROACH SPEED’ 270 knots
AREAS,
TOTAL WING (INCLUDES 2,482 34 sq.ft COVERED BY FUSELAGE BUT NOT 33-53sq-ft
OF WING RAMP AREA) - 6,297.15 sq ft
CANARD (INCLUDES 150-31 sq.ft- COVERED BY THE FUSELAGE) - 415 -59 sq-ft
VERTICAL TAIL SURFACES (INCLUDES 8 96 sq.ft BLANKETED AREA)- 233-96sq.ft
ENGINEERING AND DESIGN COST, REPORTED FIGURE - 1-3 BILLION DOLLARS
CONSTRUCTION COSTS, APPROX., REPORTED - 750 MILLION DOLLARS
ACCURATE AND TRUE TOTALS WILL PROBABLY NEVER BE KNOWN
COLORING NOTES
ENTIRE AIRCRAFT - GLOSS WHITE
ENGINE BAYS AREA - NATURAL STEEL FINISH
TIRES - ALUMINUM PAINTED
ANTI-GLARE PANEL - FLAT BLACK
TURBOJET ENGINES- BLACK
ALL LETTERING - BLACK
WING TIP FOLD FAIRING - GLOSS BLACK
NATIONAL INSIGNIA - RED, WHITE & BLUE
HATCHES FOR
ESCAPE CAPSULES
PITOT
в
U.S.AIR FORCE
STA. 870
urmi
jVlADON
.1BLM
VARIABLE INTAKE
OUTLINE
STA. 0
24.60' АРРГОХ-
GROUND ESCAPE
HATCHES-
28 81*
□ 0 □
ООО
—g—
ODO
□ 0 □
□ DO
ODO
PROB
STA 56 A
FUSE. STA. 0
FRL DATUM
KwW«t-’
WINDOW & WINDSHIELD RAMP
IN SUBSONIC POSITION
NORTH AMERICAN XB-70-1
Valkyrie*
_____________1964-69_______________
SCALE: ORIGINAL L96 ('/e“« l‘)
REPRO. 1192 ('/!«= Г)
DRAWN BY - PAUL R. MATT______
© HISTORICAL AVIATION ALBUM 1969
P. 0- BOX 33
TEMPLE CITY, CALIF. 91780
7 26 " WING ENTWANCE
84'-11	INTAKE ENTRANCE
-----------------107 '-1
THROAT ТЕ
PLATES I & 2 of 3
I DRAWING No. 7-66-Gl
65 57
32- 1.2
HINGE MECHANISM
COVER FAIRING-
GLOSS BLACK
WING
STA. 385.2 WING FOLD LIN
ГТ
—t
105-0'
□
17 - II.0I31
□
'ООО
FLAP
meters
15-0
_DATUM
THRUST
ЗО'-tf
STA 1285
STA. 2328
O.A. LENGTH OF AIRCRAFT - TECH. TERM
------ I94'-O
PARALLEL RED
DANGER STRIPES
STA
2277.5
BRAKING SYSTEM
REFERENCE WHEEL
ENGINE—
REMOVAL
DOORS
DRAG CHUTE
COMPARTMENT,
3 CHUTE
DEPLOYMENT
46.21 WHEEL-BASE.
! (7 I WING ROOT CHORD BASED ON C-L. OF AIRCRAFT
PROMINENT
INSTRUCTION &
ENGINE BLEED
AIR BYPASS DOORS
ADJUSTABLE
CANARD FORWARD
SURFACE
О 2 4 6 8 10
SCALE BARS
feet
Е
□
□
о.
ООО
52-6*
STRUT
DOORS
STA 1019.4
RHINAL SHOCK LINE
WING LEADING POINT
AT WING STA.
о
USAF
LETTERING
POSITION-
SEC. 7
FUSE.
STA.
INDEPENDENT
FLAP
MOVEMENT
WINDOWS & WINDSHIELD RAMP
IN SUPERSONIC POSITION
PIVOT
AND/OR
CANARD
Lir,t TRIM
SEC 7
HINGE LINE
FIXED VERTICAL FIN
thrust
SCALE BARS
2	3 meters
RADOM
COLOR SEPARATION
LINE, FLAT BLACK
ANTI-GLARE PANEL
Л RUDDER
S/N POSITION (2000U
23.17
HIGH SPEED
TRANSITION
FULL DOWN TIP
POSITION AT
SUPERSONIC
SPEEDS
ALL TIRES SAME
SIZE, HEAT DETERENT
ALUMINUM PAINTED,
WING
FRl^ DATUM
WING STA 0
AT FUSE. 870
SCULPTURED WING
AND LEADING EDGE
DROOP
£_Rk_
SINGLE POINT
REFUELING
\ RED DANGER
'---STRIPE
OUTBOARD ELEVONS DISENGAGE
AND HAVE NO CONTROL FUNCTION
IN TIP FOLD SUPERSONIC POSITION
WING AIRFOIL^ECTION FROM "О" AT ENTRY DOWN BUTT STUB LINE TO ® ON PLANVIEW
— -----------------------------j———------------------>-----------
2 4 6 8 IO feet
MAIN GEAR
ROTATES 90
FOR STOWAGE
105-0
RUDDER
MOVEMENT
LANDING GEAR
DOORS NORMALLY
OPEN ONLY DURING
BRIEF EXTENSION
OR RETRACTION
SEQUENCE
NORTH AMERICAN XB-70-1
I DRAWING Мл 7-ftA-Gl
ISTORKAL
i VIATON
AAlbum
Valkyrie
1964-69
SCALE: ORIGINAL Г96 ('/q^^TT
REPRO 1-192 С/Г6"»Г)
DRAWN BY - PAUL R MATT
© HISTORICAL AVIATION ALBUM 1969
P.O. BOX 33
North American XB-70-1 "Valkyrie"


GENERAL SPECIFICATIONS
WEIGHT EMPTY
PILOT & GUNNER
FUEL & OIL
ARMAMENT
GROSS WEIGHT
TOP SPEED at
2468
360
475
352
3655
(136) 132 mph
127
102
23,000 ft.
415.6 sq ft.
84 lbs./sq.ft.
5 hrs.
112 mph
50
lbs.
-------13'2'4
8'2%
STEP PLATE
GUNNERS FOLDING STOOL
AIRFOIL (TWICE SCALE)
SEA LEVEL
10,000 ft.
20,000 ft.
PARALLEL" FLAT STEEL
TENSION STRAPS
TELESCOPIC
SIGHT
TWIN LEWIS .30 CAL.
MACHINE GUNS ON
SCARF MOUNT
31 7g
-WE
В О
1%
W-E
BO
----W-E
COLOR REVERSED ON SOME MODELS
STEEL BINDING
STRAPS (SOME MODELS)
METAL 'OVER-SF^R' CLAMP
FOR INTER-PLANE STRUT
WHITE
BLUE
RED
COCADE ON UNDERSURFACE OF
LOWER WING, IN SAME POSITION
SERVICE CEILING
WING AREA (INCL. AILERONS)
WING LOADING
ENDURANCE, CRUISE at 10,000 ft.
DRUISING SPEED
.ANDING SPEED
65 A CHORD
23/e
7' 10%
35'/4
ENTIRE
FUSELAGE
VENEER
COVERED
(ENGINE AREA
ALUMINUM COVERED)
COLOR NOTES
INITIAL DESIGN - IRREGULAR, OLIVE DRAB & MEDIUM ‘EARTH* BROWN,
UNDERSURFACES, CLEAR DOPED-
EXPERIMENTAL DAY CAMOUFLAGE (POST WW-I), BLACK & WHITE, CLEAR
DOPED UNDERSURFACES.
LATE VERSION- OLIVE DRAB FUSELAGE & EMPANAGE , CLEAR DOPED
WINGS AND STRUTS.
COLOR CODE
PATTERN ONE: 0-
E -
C -
PATTERN TWO: В -
W-
OLIVE DRAB
EARTH BROWN
CLEAR DOPED
BLACK
WHITE
BASIC CAMOFOUFLAGE PATTERN AND OUTLINE DID NOT CHANGE
COLOR LINE-------------
RADIATOR
TWIN MARLIN .30 CAL.
MACHINE GUNS,
SYNCHRONIZED TO
FIRE--------------
ARC.
(ON
THROUGH PROP.
RIGHT SIDE ONLY)
SCALE BAR (feet)
ISTOWCAL
1 VIATON
/(Album
PACKARD-LE PERE LUSAC-II
(1918)
SCALE: 148
39* ок»
WATER
FIREWALL
9В'/2
ALUMINUM
VENEER
ENGINE
BEARER & BRACE
LANDING GEAR
STEEL STRAP
CROSS BRACE
CABANE STRUTS
EXTENDS TO LOWER
LONGERON
ALUMINUM
INSULATION
PLATE
О’ DIH.
6О?В
О’ DIH
ALUMINUM FAIRING
RADIATOR
ALUMINUM
у FAIRING
MARLIN GUNS
ON OTHER (RIGHT)
SIDE, IN POSITION
SHOWN
94^

65V--
SERIAL NUMBER ASSIGNMENT
40013-40029
42129-42141
(42130-42133 TO FRANCE, A.E.F )
INTERPLANE STRUTS SAME COLOR AS
CONTACT AREA OF LOWER WING,
FOLLOWING CAMOUFLAGE PATTERN.
ALUMINUM FAIRINGS LEFT NATURAL.
PLATF I
(1918)
SCALE; 148
RADIATOR FILLER & EXPANSION TANK
RIGHT SIDE, CAMOUFLAGE PATTERN
(HALF SCALE)
PACKARD -LE PERE LUSAC - 11
PLATE 2	(1918) SCALE: 1.48 DRAWN BY’ PAUL R. MATT © 1965
GENERAL
WEIGHT EMPTY
USEFUL LOAD
GROSS WEIGHT
TOP SPEED
WING AREA
WING LOADING
POWER LOADING
ASPECT RATIO
ENGINE - 25 H.R (at
SPECIFICATIONS
370 lbs (approx.)
190-230 lbs
560-600 lbs.
42 mp h (est.)
186 sq. ft.
3 2 Ibs./sq ft.
24 Ibs/H.P.
5.7 to I
1,200 r.p.m.) CURTISS
4 cyl., W.C.
TYPICAL CROSS SECTIONS
AUX. STRUT	MAIN STRUT
18'0"
DETAIL of RUDDER
DRAWING No. 2-11- A
к------5’6”
LIGHT RIB - HEAVY RIB WIRE T. E. ’/z* 2" GUIDES FASTENED TO
ALTERNATE^X ribs AND SPARS
INSIDE OF
FUEL LINE
SHUT OFF
VALVE
FIXED
STABILIZER
CONTROL LINES
PULLEY
& BRACKET
Iм DIA STEEL
TUBE STRUCTURE
PULLEY
Note-, wings
DRAWN IN TRUE
PLANFORM NOT
AS 5* DIHEDRAL
PROJECTION
Pfitzner i9io Monoplane
PLATE I of 2
ISKHIKAL
iVlAIWN
] Album
SCALE - ORIGINAL I 24
REPRO. I 48
DRAWN BY:HERB KELLEY
© HISTORICAL AVIATION ALBUM 1965
PO BOX 33
tempi c r»r *—c  1 ,g	I
4‘0
3‘0 —
ANTI-VIBRATION
LOOP IN FUEL
LINE \
Note: wing panels
DELETED FOR
CLARITY IN
SIDE VIEW
2 x 20" TIRES
/	10
=-------F
2 x2"ASH
STRUT
DRIP RAN TO CATCH
OIL FROM ENGINE
ENGINE BED DETAILS
l“x p/4" ash
RUDDER
PULLEY
I x |?4" SPRUCE BEAMS
I" DIA STEEL
TUBING
TENSION WIRES
ELEVATOR CONTROL
LINES
RUDDER CONTROL
LINES
CONTROL HORN
RIGHT SIDE ONLY
ELEVATOR
CONTROL HORN
RUDDER HORN
ELEVATOR
RUDDER
ALL CONTROLS OPERATED BY
CENTRAL CONTROL COLUMN. WHEEL
TURNED FOR WING TIP "EQUALIZERS',’
TWISTED ON AXIS FOR RUDDER CONTROL
& MOVED FORE a AFT ON LOWER PIVOT
LINE FOR ELEVATOR CONTROL
FRONT FRAMEWORK DETAIL
“ AL0UM
___________QI 7 on
GASOLINE TANK, 9" DIA (at largest point)
г »/e" DIA. STEEL
w TUBE BRACES,
FORE a AFT -
SCALE
BAR
TSTEEL
FERRULE
FEET
METERS
’/в" HOLE
DRILLED (.
THROUGH^ i
NOTES
VARNISHED
V DIA. STEEL TUBE
- AXLE, (no shock
ABSORBING__________
SYSTEM	<
EMPLOYED.)
FACING PROPELLER,
LOOKING FOREWARD
ALL WOOD, 6'0" DIA-4 ' PITCH
ROTATION - C W.
=? 0
3/i6" LACING HOLES,
/ I" APART
HEAVY RIB-SIX ’A" SPRUCE
LAMINATIONS
----4' 8
: \ % STEEL
X FERRULE,
J 3/32 " HOLE
:	. DRILLED
THROUGH.
COLORING
WOOD - CLEAR
METAL TUBULAR STRUCTURE,
FITTINGS, FUEL TANK,-BLACK
FABRIC - BLACK, UNEVEN MOTTLED
FINISH
ALL SURFACES WERE COVERED ON THE TOP SURFACE ONLY,
WITH REMNANT BALDWIN BALLOON RUBBERIZED FABRIC
LIGHT RIB - THREE 14 " SPRUCE
LAMINATIONS - fe" THICK
RIBS-TWICE SCALE
WINGS SET AT
10 5* INCIDENCE (Approx.)
1STOWCAL PFITZNER ^MONOPLANE
IVJADON
/\Album
(1910)
SCALE: 1.48
DRAWN BY: H Kelley
© PAUL R. MATT 196
GENERAL SPECIFICATION
WEIGHT EMPTY	680	lbs
USEFUL LOAD	540	lbs
GROSS WEIGHT	1100	lbs
WING AREA	178.5 sq.ft.
WING LOADING	6l6lbs/sqft
POWER LOADING	22.0 lbs/HP
TOP SPEED	87	mph
CRUISING SPEED	73	mph
LANDING SPEED	38	mph
RANGE AT CRUISE	220	miles
MAXIMUM CEILING	12,000	feet
FUEL CAPACITY	12 gals
OIL CAPACITY	I gal
FUEL CONSUMPTION 4.46 gals/hr
POWER CONTINENTAL A-65-8
LYCOMING 0-145
FRANKLIN 4AC-65
ALL 65 HP AT 2500/2550rpm
COLORING NOTES
STANDARD FACTORY ISSUE-OVERALL CUB YELLOW
(DEEP RED-YELLOWJ, BLACK TRIM
OTHER COLORS AT CUSTOMERS REQUEST
SCALE ORIGINAL- l‘24
REPRO. - 1:48
DRAWN BY: PAUL R MATT
PIPER J-3 "CUB"
1937-47
[DRAWING No. I8-I2l-~A~|
PLATE I of 2
(c) HISTORICAL AVIATION ALBUM 1986
P 0 BOX 33
TEMPLE CITY, CALIF. 91780
[drawing No 18-121-4]
PLATE 2 of 2
PIPER J-3 "CUB"
1937-47
SCALE : ORIGINAL - I 24
REPRO. - I 48
_______DRAWN BY: PAUL R. MATT
© HISTORICAL AVIATION ALBUM 1986
P. 0. BOX 33
TEMPLE CITY, CALIF. 91780
WEIGHT EMPTY
USEFUL LOAD
GROSS WEIGHT
WING AREA
WING LOADING
POWER LOADING
TOP SPEED
CRUISING SPEED
LANDING SPEED
SERVICE CEILING
RANGE AT CRUISE
FUEL CAPACITY
OIL CAPACITY
FUEL CONSUMPTION
GENERAL SPECIFICATIONS
CONTINENTAL A 75-8, 75 HP LYCOMING 0-145, 65 HP
880
520
1400
183 sq ft
7. 65 Ibs/sq ft
18 66 Ibs/HP
96 mph
83 mph
38 mph
12,000 feet
382 miles
25 gals
1.25 gols.
5 gal at S.L
lbs.
lbs
lbs
800
401
1301
I 83
HINGE
meters
METAL TRIM TAB
— COCKPIT CONTROLLED
COLORING NOTES
STANDARD FACTORY SCHEME- FUSELAGE,
POWER CONTINENTAL 4-75*8,
75 HP AT S, LAI 2600 rpm
OR LYCOMING 0-145,
65 HP AT S.L. AT 2550 rpm
MAXIMUM POWER, TAKE OFF & EMERGENCY
SCALE BARS
1027
AIRFOIL USA 35B MODIFIED
30"
2'z, inc.
aluminum
LEADING EDGE
L ICENSE NUMBERS - CREAM
ON RED BACKGROUND
N'CRAL
METAL SPARS
lbs.
lbs
lbs
sq ft
Ibs/sq.ft
20.0 Ibs/HP
87 mph
73 mph
35 mph
12,000 feet
34 0 miles
16 gals
1.25 gals.
4 gals at S.L.
, VERTICAL
TAIL SURFACES & LANDING GEAR - CREAM.
HORIZONTAL TAIL SURFACES, WINGS & PROFILE
TRIM - RED- . OR REVERSE COLORS.
OTHER COLORS USED - BLUE & CREAM AS WELL AS
SOLID COLORS OVERALL
COLOR SEPARATION LINE
INNER - RED, OUTBOARD
CREAM
fuel| fill —
—63"
JURY STRUT
CLAMPS TO
LIFT STRUTS
SINCERE THANKS TO PAUL
McDANIEL, JOHN UNDERWOOD
AND PIPER AIRCRAFT FOR
THEIR HELP IN THE PREPARA-
TIONS OF THESE DRAWINGS „
----------------------
DRAWING No. 18-122-aI
PLATE I of 2
ISTORKAL
i viaton
\ Album
PIPER J-4E "CUBCOUPE
1941 MODEL
SCALE ORIGINAL - L24
REPRO - 1-48
DRAWN BY PAUL R MATT
© HISTORICAL AVIATION ALBUM 1986
P.O- BOX 33
TEMPLE CITY, CALIF. 91780___

------36 -2й----------
DATUM
2^" ’V
FUEL TANK
25 GALS
SPAR 45
feet
SCALE BARS
22'-6
278Б6
DATUM__
14 Approx
RED LICENSE ON
CREAM RUDDER
UNILOY STEERABLE
TAIL WHEEL
8.00x4" TIRES
PALMER HYDRAULIC BRAKES
HAYES WHEELS
CARBURETOR
I N ТА К E
WING WASHOUT
FRONT SPAR 1“
REAR
SIDE BY SIDE
BENCH SEAT
50 lbs BAGGAGE
COMPARTMENT
CHROME
TRIM
2 meters
SENSENICH WOOD
PROPELLER
53^
76
THRUST
ISTCMAL
AVIATION
\Album
PIPER J-4E "CUB COUPE
1941 MODEL
SCALE: ORIGINAL - 1=24
REPRO. - Г48
DRAWN BY: PAUL R. MATT
[DRAWING No-18-122-a]
PLATE 2 of 2
© HISTORICAL AVIATION ALBUM
P.O- BOX 33
TEMPLE CITY, CALIF. 91780
GENERAL SPECIFICATIONS
WEIGHT EMPTY
GROSS WEIGHT
POWER LOADING
WING LOADING
BAGGAGE CAPACITY
CRUISING SPEED
LIMITED TOP SPEED
RED LINE DIVING SPEED
STALLING SPEED
RATE OF CLIMB ’
BEST CLIMB SPEED
CRUISING RANGE
SERVICE CEILING
ABSOLUTE CEILING
GLIDING RATIO
FUEL CAPACITY (73/80
OIL CAPACITY
NORMAL
950
1750
17.5
9.8
lbs
lbs.
Ibs./H.P
lbs./sq. ft.
. . lbs.
103 m.ph.
110 m.ph.
138 m.p.h.
49 m.p.h.
600 ft /min.
75 m ph.
600 miles
12,600 feet
15,500 feet
ll:|
octane) 38 gals.
6 quarts
UTILITY
950 lbs.
1500 lbs.
15 Ibs./H.P.
8.36 lbs. /sq.ft.
HORIZONTAL TAIL
SURFACES, TOP &
BOTTOM, RED
TYPICAL INSTRUMENT PANELlSTANDARD PIPER PA-12
------------------- SUPER CRUTSER---------
OIL PRESSURE &	------- ~	~	~
TEMPERATURE

COMPASS
AIR SPEED
AMMETER
ALTIMETER
PARKING BRAKE
— HANDLE
S.L.
2600 r.p.m.
POWER- LYCOMING
at
2600r.p.m.
LYCOMING
at
THE
CHORD
--- 5'3
AIRFOIL USA 35 В
8'6*4"
19 GAL.
TANK
MIXTURE
CONTROL-
POSITION
FOR
RADIO
LEFT SIDE, FORWARD OF
INSTRUMENT PANEL UNDER
COWLING
CHORD, UNDER SURFACE
OF AILERON
0-235-C 100 H P
OR LATER
0-235-CI 108 H.R
PRIMER
CABIN
HEAT
103 m.p.h.
138 m.p.h.
148 mp.h.
CARBURETOR
HEAT
IGNITION
SWITCH
-Cl ENGINE BOOSTED CRUISING SPEED
TO 105 m.p h.
OFF/ON
RIGHT AUX-/-
- OFF/ON
left man
ZZZZJ |9 GAL. TANK
9’6
SCALE BAR (feet)
INC
TOTAL
PONCA CITY. OKLA.
TOTAL
1946-48
PLAN VIEW SURFACES, RED
LICENSE NUMBERS, CREAM
PIPER PA-12
LOCK HAVEN, PA. S.N.
SCALE- l:48
750 ft. /min
70 m.p.h
600 miles
15,700 feet
18,000 feet
II.I
38 gals.
6 quarts
LIFT HANDLE
RIGHT SIDE
ONLY---
SCALE BAR (meters)
METAL FAIRING
18%
26'W
MASTER7
SWITCH BREAKERS
RIGHT SIDE FORWARD
OF DOOR, UNDER
WINDSHIELD
POSITION
AND
PANEL
LIGHTS
COLOR
LINE
SEE RIGGING'NOTE, PLATE 2
CHORD ON TOP
SURFACE,
AILERON
5'
SUPER CRUISERS BUILT
12- I to 12 - 1900,
12- 2001 to 12-3625, 3,525
S.N. 12-1901 to 12-2000,
12-3901 to 12-4039,	239
DRAWING No 4-36-A
PLATE I of 2
TWICE SCALE
ЯЯ
THREE PIPER PA-12 s
STATE OF MAIN, 1946 - 50.
AIRCRAFT PORTRAYED IS ONE OF
USED BY THE GAME WARDENS, _
AIRCRAFT WERE ALSO EQUIPPED WITH SKIIS AND
PONTOONS. NOSE SPINNERS WERE REMOVED WHEN
KOPPERS AEROMATIC PROPELLERS WERE INSTALLED
IN 1947.
ISTORKAL
1 VIATON
ЛДивим
PIPER PA-12 SUPER CRUISER
DRAWN BY; PAUL R MATT
© HISTORICAL AVIATION ALBUM 1967
- 35* 5.5'
FUEL GAUGE TUBE
DIH.
PITOT TUBE
COLORING NOTES
FWD MAIN
SPAR -
2’AT REAR
SPAR
CARBURETOR
INTAKE, EARLY MODELS,
POSITION OF INTAKE ON LATE
MODELS AND MODIFICATIONS
CUT OUT-----
SPINNER---
RIGGING
NOTE:
SURFACES OF
WINGS AND HORIZONTAL TAIL SURFACES, FUSELAGE
DOWN TO COLOR SEPARATION LINE, WING STRUTS -
TENNESSEE RED (SLIGHTLY DEEPER THAN VERMILLION)
BALANCE OF AIRCRAFT, VERTICAL FIN & RUDDER,
FUSELAGE BELOW COLOR SEPARATION LINE - CREAM
LICENSE NUMBERS - BLACK ON RUDDER,
CREAM ON WINGS
ALL PLAN VIEW SURFACES, UNDER
74'4
DATUM
2
6 О
SCALE BAR (meters)
SCALE BAR (feet)
WITH SPINNER
22’ IO
COLOR SEPARATION LINE,
RED ABOVE, CREAM BELOW
2	3
DATUM
PIPER NAMEPLATE &
BEAD TRIM STIFFENERS
CARBURETOR
SCOOP INTAKE
LATE MODELS
ALUMINUM
FWD OF THIS
LINE
ENTRANCE STEP & DOOR
RIGHT SIDE ONLY
STEERABLE TAIL WHEEL
LINKED TO RUDDER
IO 25
FIXED PITCH WOOD
SENSENICH PROPELLER
STANDARD EQUIPMENT
3404M
ISTOWCAL
iVIATON
(Ulbum
PIPER PA-12 SUPER CRUISER
1946 -48
SCALE: Г 48
DRAWN BY PAUL R. MATT
[ DRAWING No. 4-36-~A~]
PLATE 2 of 2
© HISTORICAL AVIATION ALBUM 1967

GENERAL SPECIFICATIONS
I4%"
CONTROLLABLE
-TRIM TABS
CUSTOMIZED, $200 EXTRA
ENTIRE AIRCRAFT PAINTED CREAM
TRIM, AS MARKED, RED
POWER: FRANKLIN "500", 6-CYLINDER,
215 H.P at 2500 r.p.m ,
MODEL 6A8-2I5-B9F
COLORING NOTES
ENTIRE AIRCRAFT PAINTED SILVER
TRIM, AS MARKED, FOREST GREEN
l2‘-6
25%
6,-7^,,ai^ron
PITOT TUBE
STEP & SPLASH PLATE
AIR VENTS
PIVOT POINT
BOW DOOR
MOORING CLEAT
48 STIFFENERS
PER PANEL,
4" ON CENTER
OVERHEAD ENGINE
CONTROL LINES COVERING
INSTRUMENT PANEL
DECKING
MY SINCERE APPRECIATION IS EXTENDED
TO MR. CHARLES A 'SEABEE' CARY FOR
HIS UNTIRING HELP IN THE PREPARATION
OF THESE DRAWINGS.
© HISTORICAL AVIATION ALBUM 1980
P. 0. BOX 33
KOPPERS "AEROMATIC", GROUND ADJUSTABLE
PROPELLER, 84“ DIA.
(HARTZELL HYDRO-SELECTIVE HC-I2«2O, 84" DIA.,
VARIABLE & REVERSIBLE - OPTIONAL)
SCALE - ORIGINAL I 24
REPRO. 1:48
DRAWN BY; PAUL R. MATT
—    ——.г । ———
REPUBLIC RC-3 'SEABEE
__________1946-47_______
6 7e DIA
INSPECTIO
PLATES
[DRAWING No. I6-IQ9-a]
PLATE I of 3
TEMPLE CITY, CALIF. 91780
WEIGHT EMPTY
USEFUL LOAD
GROSS WEIGHT
WING AREA
WING LOADING
POWER LOADING
TOP SPEED
CRUISING SPEED
LANDING SPEED
CRUISING RANGE
RATE OF CLIMB, INITIAL, S.L.
SERVICE CEILING
FUEL CAPACITY
OIL CAPACITY
2,100 lbs.
1,050 lbs.
3, 150 lbs.
196 sq. ft
15.3 lbs./sq.ft.
14.2 lbs./H P
120 mph
103 mph
58 mph
520 miles
700 ft./mm.
12,000 ft
75 gals.
13 qts.
SCALE BARS
287*
,2 meters
OIL FILL ACCESS
NACELLE OUTLINE
9’.6«/8‘!_flap
1STOWCAL
WlATON
HAlbum

----------37’- 8
----RUNNING (ANCHOR) LIGHT
REPRO. I 48
DRAWN BY: PAUL R. MATT_______
© HISTORICAL AVIATION ALBUM 1980
P.O. BOX 33
TEMPLE CITY, CALIF. 91780_____
PLATE 2 of_3
I ГЛ D A LAZ. M/— Мп 1£-1Г>а-"л1
WATER DRAIN PLUG
LICENSE
FOREST GREEN, 16"* 24"
4" STROKE, 4" SEPARATIONS
RO. BOX oo
TEMPLE CITY, CALIF. 91780
CABIN LINES
p meters
BOW DOOR OPEN
TIE DOWN RING
| DRAWING No. 16-Ю9-д|
PLATE 3 of 3
16 STIFFENERS,
4" ON CENTER
FIXED TRIM TAB
PORT SIDE ONLY
©HISTORICAL AVIATION ALBUM 1980
PO BOX 33
TEMPLE CITY, CALIF 91780
REPUBLIC RC-3 SEABEE
____________1946-47_________
SCALE - ORIGINAL 1: 24
REPRO. Г-48
DRAWN BY PAUL R MATT
TAIL WHEEL ROTATES
90е FOR "RETRACTION
SCALE BARS
ISTORKAL
iVIAIlON
AAlbum
Rover Aviation Engine
CARBURETOR AIR
CONTROL LEVER
COLD AIR INLET
COLORING NOTES
GENERAL SPECIFICATIONS
АТС No. I42
TAIL SURFACES METAL
FRAMEWORK, FABRIC
COVERED
OVERALL SILVER DOPED,
DETAILING BLACK.
ALUMINUM NOSE AREA, BURNISHED
CABIN WINDOWS AND DOORS,
STAMPED ALUMINUM SHEET
POWER - WRIGHT J-6-9 "WHIRLWIND
RATED 300/330 HP
CARBURETOR AlR INTAKE
Yr0
7-0
AIRFOIL, CLARK Y
PITOT TUBE
ToRAWINg
3-LAM IN AT IONS
SPRUCE SPARS
GREEN TINTED
PYROLIN SKYLIGHT
5Ogol. FUEL TANK
(2 TANKS, lOOgol
TOTAL CAPACITY)
30" *2 Г GOTHIC LETTERING,
5" STROKE
© HISTORICAL AVIATION ALBUM I974
P. O. BOX 33
TSMPLf CITY GA!.IF.	I
SCALE-ORIGINAL 1:24
REPRO. I-48
DRAWN BY - PAUL R. MATT
WEIGHT EMPTY
USEFULL LOAD
(PAYLOAD
GROSS WEIGHT
TOP SPEED
CRUISING SPEED
CRUISING RANGE
LANDING SPEED
CLIMB, INITIAL, S.L.
SERVICE CEILING
ABSOLUTE CEILING
WING AREA
WING LOADING
POWER LOADING
2250 lbs
I 750 lbs.
935 lbs)
4000 lbs
I38
I I2
750
55
I000
18,000
25,000 feet
224 sq.ft
14.5 Ib./sq f t.
13.3 Ibs/HP
mph
mph
miles
mph
ft./min.
feet
FUEL
FUEL LINIES-5
ALUMINUM L E
DIMENSIONS APPROXIMATE,
ARRIVED AT THROUGH
MECHICANICAL ANO
PROJECTION PROCESS
PIVOT LINE OF STABILIZER
ADJUSTMENT, JACKSCREW
ON TAILPOST STABILIZER
ADJUSTMENT + 4° thru -5'
INERTIA STARTER
CRANK FITTING
CORO WRAPPED
NON-SKID
SERVICE STEP
AREA
02 INC
WING BUILT IN ONE PIECE, CONSTRUCTED OF WOOD WITH
METAL TUBE COMPRESSION MEMBERS AND STEEL TIE WIRES,
FABRIC COVERED. AILERONS METAL FRAMEWORK, FABRIC
COVERED
ISTORICAL
VIATON
Album
MAHONEY-RYAN B-5
"BROUGHAM"
______1929-30___
drawing No. RB-96-а'
PLATE I of 2
FUEL TANK FILL,
CAP & BREATHER TUBE
42’ - 4” WINGSPAN
p. 0. BOX 33
TEMPLE citv; CALIE, 91780
10-0
RYAN В 5
FRL
14* Approx.
32"* 6" HIGH PRESSURE TIRES
FLAT BLACK
BAGGAGE COMPARTMENT
(73lbs. TOTAL ALLOWANCE)
LIFT HANDLE
(BOTH SIDES)
EMERGENCY STEEL SKID
LEATHER DUST BOOT
FULL SWIVEL, 8" FLANGED
MICARTA TAILWHEEL
SCALE-ORIGINAL Г.24
REPRO 148
DRAWN BY - PAUL R. MATT
HAMILTON STANDARD
GROUND ADJUSTABLE
PROPELLER
(OPTIONAL 9‘-4"
MAX. DIAMETER)
THRUST ----

ENCASED
OLEO SHOCK ABSORBERS
STATIC GROUND LINE
NORMAL LOAD ABOARD
FUSELAGE OF WELDED STEEL
TUBING, WOOD FORMERS AND
STRINGERS, FABRIC COVERED
O* DIH.
SCALE BAR, feet
SCALE BAR, meters
28'-3'
_________DATUM .
ISTORKAL
iVlAITON
/\Album
[DRAWING No. RB-96-A]
MY APPRECIATION IS EXTENDED
TO WILLIAM WAGNER AND THE
RYAN AERONAUTICAL LIBRARY
FOR SUITABLE RESEARCH MATERIAL
SO ESSENTIAL IN THE PREPARATION
OF THESE DRAWINGS
PLATE 2 of 2
MAHONEY-RYAN B-5
"BROUGHAM"
_____1929-30____
© HISTORICAL AVIATION ALBUM 1974
R 0. BOX 33
______TEMPLE CITY, CALIF, 91780
SCALE METERS
XF2R-I
39661 ONLY
WIDTH
YELLOW ROPE
WHITE INNER RING
VF-66
OUR SINCERE APPRECIATION TO MR. ED MALONEY, DIRECTOR OF THE
AIR MUSEUM, ONTARIO INTERNAT'L AlRPORT,ONTARIO, CALIF FOR
HIS ASSISTANCE WITH MATERIAL FOR PREPARATION OF THESE DWGS
7,635 LBS.
9,958 LBS
10,595 LBS
YELLOW
ORANGE
YELLOW
ORANGE
BLACK BEAK
.	, — NAVY BLUE
iM Z—LIGHT GRAY BODY & WINGS
50 CALIBER MACHINE GUNS ( IN WING CENTER SECTION )
1,000 LB BOMB & 8 60LB HVAR'S
NAVY BLUE	U —
FIREBIRD INSIGNIA
SERIAL NO. ASSIGNMENTS,RYAN FR-I	0
MODEL SERIAL	DESCRIPTION
XFR-I ---- 48232-48234 ----PROTOTYPES
FR-I ----- 39647-39712 ----PROD SERIES (VF-66 )
XFR-2----- 104572-105175 --IMPROVED VERSION(NONE BUILT)
XFR-3---- NOT ASSIGNED ---- HIGHER H P PROP NOT BUILT	MAIN	FUSELAGE
XFR-4 --- 39665 ONLY-------HIGHER H P, FLUSH AIR	FUEL TANK CAP
INTAKES, MODIFIED TAIL.
'DARK SHARK" TURBO-PROP,
TURBO-JET COMBINATION
GENERAL SPECIFICATIONS-
PERFORMANCE DATA
MAX SPEED (BOTH ENGINES)^ I8.000FT---- 425 MPH
MAX SPEED(BOTH ENGINES)@ SEA LEVEL----- 399MPH
MAX SPEED( PISTON ENGINE ONLY)----	-320MPH
CRUISE SPEED( PISTON ENGINE ONLY) -- -153 MPH
MAX SPEEDf JET ENGINE ONLY) —	300MPH
CLIMB TO 20,000 FT. (BOTH ENGINES)----- 5.6 MIN
INITIAL CLIMB RATE (BOTH ENGINES)---4,800 FPM
SERVICE CEILING--------------------40,000 FT*
RANGE (PISTON ENGINE ONLY(<0 153 MPH)	-1,030 MILES
WEIGHTS
EMPTY-----------
NORMAL LOADED
MAX GROSS A U.W
3QWER PLANT
I WRIGHT CYCLONE RI820-72W------------ 1,350 HP
I GENERAL ELECTRIC I-16(J-31)--1,600 LB THRUST
ARMAMENT (WITH AUX FUELTANK)
21 80
RYAN FR-I FIREBALL
( 1945-1948)
SCALE I 48
DRAWN BY ROB LAMBERT



GENERAL SPFC! F "Л1 IONS
ST-A, MENASCO 04, 125 hp ENGINE
9'-5
HINGE
24 ST ALCLAD LEADING EDGE
POWER-MENASCO C"4 FOUR
О
FLAP
CYLINDERS COOL
AIR INTAKE
NOTE
NC 14985, c/n 117 WAS BUILT AS A 95 H P
MENASCO B-4 POWERED ST MODEL ORIGINALLY.
IT BECAME AN ST-A LATER WHEN A 125 H P.
MENASCO D-4 ENGINE WAS INSTALLED
FUEL FILL
(24 gals.)
CYLINDER
INVERTED INLINE AIRCOOLED
ENGINE RATED 125 H P AT 2,175 RPM
5 7г
$ feet
SCALE BARS
COLORING NOTES
CONSTRUCTION NOTES
FORMED TAIL CONE
HOUSES RUDDER
CONTROL HORN
COCKPIT CONTROLLED
METAL TRIM TABS
MOISTURE
DRAIN
1—GROMETS
2
j meters
WEIGHT EMPTY
USEFUL LOAD
GROSS WEIGHT (MAY
MAXIMUM SPEED Al S-L.
CRUISING SPEED AT <000 FT
RANGE AT CRUISE
CLIMB AT S.L (MAX. EFFORT)
SERVICE CEILING
LANDING SPEED, WITH FLAPS
LANDING SPEED, FLAPS UP
TAKEOFF RUN, FULL LOAD
WING AREA
POWER LOADING
WING LOADING
1,035
565
1,600
150
127
38 r
1,200
17,500
60
70
175
124
12.8 lbs /hp
.12.9 Ibs/sq. ft
b
I bs
mob
mp h
mile.'
t! /min.
feet
mph
mph
yards
sq ft
24>2"
6”
T
LANDING ___
ADJUSTMENT 0°THRU-45
84у PRE c/n 121
675/1бТТГГ11Га
ONWARD
ZIPPER*
INSPECTION
FLAP
-4k—67^’
METAL-
INSPECTION PLATES
3o£
OIL FILL
(2.0 gals )
AIR SCOOP
CARBURETOR AIR
INTAKE
INTAKE FOR
CYLINDER
HEADS
ENTIRE AIRCRAFT NATURAL ALUMINUM
FABRIC COVERED AREA, MATCHING SILVER DOPE
LICENSE NUMBERS & DETAILS, BLACK
INTERIOR OF COCKPIT AREA UPHOLSTERED IN
RED OR BLACK LEATHERETTE, INSTRUMENT
PANEL BLACK "CRINKLE” FINISH, CONTROL
STICK AND WING FLAP CONTROL LEVER
CHROME PLATED
MY SINCERE APPRECIATION IS EXTENDED TO
MESSERS. T. CLAUDE RYAN, WILLIAM WAGNER,
AND MAC CATRELL OF THE RYAN AERONAUTICAL
CORP, EV. CASSAGNERES AND FLOYD CARTER
FOR THEIR VALUABLE AND UNSELFISH HELP
IN THE PREPARATION OF THESE DRAWINGS
FUSELAGE - ALL METAL, MONOCOQUE, ALCLAD 24 ST SKIN.
WINGS - SPRUCE SPARS, STAMPED ALUMINUM ALLOY RIBS,
STEEL TUBE COMPRESSION MEMBERS, STEEL
CABLE TIE LINES, FABRIC COVERED
AILERONS & WING FLAPS - STEEL TUBE SPAR, ALUMINUM
ALLOY RIBS, FABRIC COVERED
TAIL SURFACES- RIVETED 24 ST ALUMINUM TUBING AND
ALLOY RIBS, FABRIC COVERED.
RYAN ST-A
c/n 117 NC 14985
1936
1ST0RKAL
AVIATION
AAlbum
SCALE-ORIGINAL 124
REPRO. I 48
DRAWN BY - PAUL R MATT
© HISTORICAL AVIATION ALBUM 1971
P. o. BOX 33
2Г-5?в
SMALL LOUVRES ON BOTH
SIDES OF COWL USED ON FIRST
FEW STs. DISCONTINUED
ON LATER MODELS
OF NOSE SCOOPS^
SENSENICH WOOD
PROPELLER-^
—309/,; 4-21'V*
IN FAVOR
GLASS VISUAL
FUEL GAUGE
THRUST LINE____]
on
EXHAUST STACKS VARIED
IN LENGTH AND END
ANGLE CUT OFF
12’-38' Approx
FIXED, GROUND
ADJUSTABLE METAL
TRIM TAB
DATUM
FULL SWIVEL FORKED TAIL
WHEEL, STEERABLE LINKAGE
OPTIONAL 8" GOODYEAR
PNEUMATIC TIRE. OLEO
OR BUNGEE SYSTEM SHOCK
ABSORBER.
18 x 8"x 3” GOODYEAR BALLOON TIRES,
WHEELS & DISC BRAKES, RYAN AEROL
SHOCK ABSORBERS.
ISKMAL
iVIATION
AAlbum
| DR AWING No 9- 76-A~|
PLATE 2 of 2
RYAN ST-A
c/n 117 NC 14985
1936
SCALE - ORIGINAL I 24
REPRO- I 48
_______DRAWN BY- PAUL R. MATT
© HISTORICAL AVIATION ALBUM 1971
P 0. BOX 33
TEMPLE CITY, CALIF 91780
J
WEIGHT EMPTY	2730	lbs.
USEFUL LOAD	1320	•1
GROSS WEIGHT	4050	I
TOP SPEED	168	mph
CRUISING SPEED	120	•I
LANDING SPEED, WITH FLAPS 60		11
RATE OF CLIMB	650	ft. /min.
FUEL CAPACITY	200	gols
OIL CAPACITY	12	II
SERVICE CEILING	15,000	ft.
WING AREA, incl. ailerons	220	sq ft
R MATT
bCALE I 48“
DRAWN by PAUL
GENERAL SPECIFICATIONS
I
.24
Г Inc Approx
POWER - P & W R-1830-9 TWIN WASP
950 h.p max.
ARMAMENT - TWO 30 col. OR ONE .30 cal &
ONE .50 cal BROWNING MACHINE GUNS
FUEL
METERS
STANDARD 30'
DIA NATIONAL
INSIGNIA
WEIGHT EMPTY
USEFUL LOAD
GROSS WEIGHT
WING AREA
MAXIMUM SPEED
CRUISING SPEED
STALLING SPEED
CLIMB, INITIAL
SERVICE CEILING
FUEL CAPACITY
OIL CAPACITY
RANGE AT CRUISE
4,318 lbs
I, 284 lbs.
5,602 lbs
220 sq ft
281 mph at 10 000 feet
200 mp h approx
78 m.ph.
3,175 ft/min.
29,685 ft
200 gols
12 gals
1,000 miles
METAL TRIM TABS,
FABRIC COVERED CONTROL
SURFACES v
OIL COOLER
INTAKE
EXHAUST STACK
FAIRING
CARBURETOR AIR
INTAKE
— FUEL TANK
INTEGRAL WITH
WING CENTER
SECTION
FIN OFFSET 2
TO LEFT
BATTERY
COMP
BAGGAGE
FLARE TUBES
DOORS
INDIAN HEAD INSIGNIA, P-35 AIRCRAFT,
94 th PURSUIT SQUADRON
FACE BROWN WITH BLACK, BLUE & RED MARKINGS,
WAR BONNET WHITE FEATHERS TIPPED WITH
BLUE, YELLOW & BLUE HEAD BANDS,
RIBBONS RED & BLUE
NOTE?
/ ELEPTICAL TRAILING
EDGE STARTS AT OUTER
WING PANEL
PROTRUDING
HANDLE
METAL
FLAPS,
ELECTRICALLY
OPERATED
- 7-3“ —
7'-5
FEET
W-l
AIRFOIL AT W-l
(TYPICAL)
SPECIAL SEVERSKY SECTION
ONLY MAJOR PANELING AND
PROMINENT RIVET LINES ARE
SHOWN. ALL WERE NOT NECESSARILY
TRANSFERED FROM ONE VIEW TO
ANOTHER
PIANO HINGE
SEVERSKY P-35
The Farmingdale flash
SCALE-ORIGINAL 1-24
REPRC 148
DRAWN BY- PAUL R MATT
© AERO ALBUM 1968
P O. BOX 33
PLATE 2 of 2
DRAWING No AA-5 7-A~"|
© AERO ALBUM 1968
PO. BOX 33
TEMPLE CITY, CALIF. 91780
Sikorsky S-39B
Sikorsky S-39B interior.
[DRAWING No I4-IOQ-A~|
GENERAL SPECIFICATIONS
EMPTY
LOAD


WEIGHT
USEFUL
GROSS WEIGHT
TOP SPEED
CRUISING SPEED
LANDING SPEED
RATE OF CLIMB, S.L., INITIAL
SERVICE CEILING
CRUISING RADIIS
WING AREA (INCL AILERONS)
WING LOADING
POWER LOADING
POWER- P&W WASP JR. A (R-985)
300 h p MAX. AT 2,000 r p m.

0
2,678 lbs.
1,322 lbs
4,000 lbs
I I 9 mph
100 mph
54 mph
750 ft./min.
18,000 feet
400 miles
350 sq.ft.
11.43 Ibs./sq ft
13.33 Ibs/H.P
COLORING NOTES (NC803W)
DARK NAVY BLUE - HULL, FLOATS, STRUTS AND
ENGINE COWL
SILVER- WINGS,TAIL SURFACES, BOOMS, ENGINE
NACELLE & TRIM STRIPE ON HULL
BLACK- LETTERING & DETAILS
COLORING DURING USE BY CIVIL AIR PATROL
DURING WORLD WAR П
DARK NAVY BLUE- LOWER PORTION OF HULL TO TRIM LINE UNDER
WINDOWS, TOPSIDE HULL OVER CABlNE AREA
DOWN TO TRIM LINE JUST ABOVE WINDOWS,
ALL STRUTS, ENGINE NACELLE, LOWER
PORTION OF FLOATS
CHROME YELLOW- WINGS, BOOMS, EMPENNAGE , TOPSIDE BOW
DECKING, PANEL DOWN WINDOWS & TOPSIDE
FLOATS
RED - ENGINE COWL______________________________

PLATE I of 5
ISTMAL
AViATKJN
A Album
SIKORSKY S-39B
_______1930-32________
SCALE ORIGINAL 1:24
REPRO 148
DRAWN BY - PAUL R MATT
© HISTORICAL AVIATION ALBUM 1975
P 0. BOX 33
TEMPLE CITY, CALIF. 91780
STABILIZER ADJUSTMENT WHEEL
LANDING GEAR PUMP
PARKING BRAKE
WHEEL BRAKES
ENGINE CONTROLS
HATCH LOCK BAR * CATCH
BOAT HOOK
FOLDING STEP 4 PART OF SEAT BACKREST
INSIDE STEP
COMPASS
BATTERY BOX
HANDHOLD
LANDING GEAR VALVES
BAGGAGE COMPARTMENT
FIXED HATCH LOCK ARMS
IDRAWING No 14-lQO-A)
HAMILTON STANDARD
GROUND ADJUSTABLE
METAL PROPELLER
г ' 1
©
NC 803w
63'732
GROUND LINE
ALL DIMENSIONS IN WING PANEL LAYOUT APE IN INCHES
OUTRIGGER
OIL TANK
(CAP. 6 GAL.
GAL EXPANSION)
(c) HISTORICAL AVIATION ALBUM 1975
R О BOX 33
TEMPLE CITY, CALIF. 91700	_
SCALE-ORIGINAL 1-24
REPRO I 48
DRAWN BY - PAUL R. MATT

CABIN ENTRANCE
DECK HATCH
C THRUST, PARALLEL
’ WITH GROUND LINE
42-4-
32-6"-----
SCALE
BARS
meters


TELESCOPIC HAND
-'-HOLD TUBE
SILVER TRIM STRIPE
DOWN HULL
INTERIOR FINISH -
NATURAL MAHOGANY
VENEER, LEATHER
COVERED REAR BENCH
SEAT, INSTRUMENT
PANEL, CONTROLS, FRONT
BUCKET SEATS-BLACK
18" HIGH PRESSURE
TIRE, STEERABLE
TAILWHEEL, WIRE
WHEEL. ALUMINUM
DISC COVERED ALSO
USED AS WATER
RUDDER
22 -1
ISTORKAL
Aviation
AAlbum
SIKORSKY S-39B
1930-32
ADJUSTABLE
CABLE LOCK —
AILERON
CABLE -
PLAN VIEW
STABILIZER
ADJUSTMENT
BLKD
13
BICYCLE CHAIN
SPROCKET
GUIDES
SPRING KEEPS
PEDALS NEUTRAL
AILERON
PUSH ROD
STABILIZER
ADJUSTMENT
POST
FWD- SPAR
£ PROPELLER
40*>32'L
e’ze
HULL REF.
ELEVATOR
CABLES
C ENGINE
v CYLINDERS
@ - STABILIZER ADJUSTMENT
WHEEL & CABLES
244 Pq____(20,-^y4,>
58’46---------
5 ..
- 355z,
3i'/2"
PULLEYS
GROUND LINE
GROUND LINE
26” DIA.
(22-l“)
51
3'/г USING 18 TAILWHEEL
| AIRCRAFT EMPTY
0° REF
390”	"2 apprqx.
®@©
WATERTIGHT
COMPARTMENTS
STABILIZER PARALLEL TO
GROUND LINE
NEUTRAL, ©"SETTING
SCALE BARS
NON STRUCTURAL
FAIRING (OPTIONAL )
1 9”
Ы^^/\7Х7
KEYS
OLEO STRUT
meters
6iv
STABILIZER
ADJUSTMENT
SPROCKET
SPINDLE
DATUM
267/4',g

S-39 LANDING GEAR
THE OLEO STRUT HAS TWO HYDRAULIC ONES ONE ATГ THE TOP'AND
ISIWAL
IVimi
SIKORSKY S-39B
______1930-32_____
SCALE-ORIGINAL 1-24
REPRO. Г-48
DRAWN BY-PAUL R MATT
(c) HISTORICAL AVIATION ALBUM 1975
P. o. BOX 33
f
HYDRAULIC SHOCK ACCUMULATOR
FOR RAISING AND LOWERING _
LANDING
ONE FOR
INATES
BILGE CHINE LINE (side view)
(GROUND LINE - 0* REF, FOR FINAL ERECTION)
HULL PROFILE
GEAR DOWN
LINE
SCALE - ORIGINAL K24
REPRO. I 48
DRAWN BY PAUL R MATT
2^
12’4-4-12%

(LOCK PINS)
TA
I 5 A
OLEO STRUT
SPRINGS
GEAR UP
LINE-.
CYLINDER
PISTON
-r~
GEAR. TWO REQUIRED,
RIGHT & ONE FOR LEFT GEAR
ALL DIMENSIONS ARE IN INCHES
UNLESS OTHERWISE NOTED
S-39 LANDING GEAR
THE OLEO STRUT HAS TWO HYDRAULIC LINES, ONE AT THE TOP AND
ONE AT THE BOTTOM OF THE CYLINDER TWO SHOCK ACCUMULATORS,
ONE FOR EACH LANDING GEAR, WHICH ARE MOUNTED IN THE FORWARD
BAGGAGE COMPARTMENT AT STATION No. 8
ON THE CENTER INSTRUMENT PANEL IS A GEAR-UP OR GEAR-DOWN
SELECTOR HANDLE A HAND PUMP, BETWEEN THE PILOT’S SEATS, IS
USED TO PUMP FLUID FROM A RESERVOIR TANK, THROUGH THE PUMP AND
OUT TO THE OLEO STRUT. IF THE SELECTOR HANDLE IS UP, THE FLUID
WILL BE PUMPED TO THE BOTTOM OF THE CYLINDER; IF DOWN, THE
FLUID GOES TO THE TOP OF THE CYLINDER, EFFECTIVELY EXTENDING
OR PUSHING THE LANDING GEAR DOWN
UPON LANDING ON LAND, THE INITIAL SHOCK IS TAKEN BY THE TIRES,
THEN TRANSFERRED TO THE HYDRAULIC SHOCK ACCUMULATOR. THE
IMPACT FORCES THE FLUID OUT OF THE STRUT INTO THE ACCUMULATOR-
COMPRESSING THE SPRINGS AND RESULTING ABSORBTION.
HULL BOTTOM & LONGITUDINAL STRINGERS
D£CK CHINE ORDi
ISTOWCAL
IVIAIION
/Ulbum
SIKORSKY S-39B
1930-32	___
[DRAWING No ^-lOO7^]
PLATE 5 of 5
© HISTORICAL AVIATION ALBUM 1975
R 0. BOX 33
TEMPLE CITY, CALIF. 91780
xA
J
21*-II
43--Ю—
,	• -la'-o1
'|5,’4~ ^э-О
18" STEEL KINGPOST
PRAWN BY: PAUL R, MATT____
©HISTORICAL AVIATION ALBUM 1984
3
GENERAL SPECIFICATIONS
WEIGHT EMPTY	525 lbs.
USEFUL LOAD	400 lbs.
GROSS WEIGHT	925 lbs
WING AREA
WING LOADING
POWER LOADING
MAXIMUM SPEED
CRUISING SPEED
LANDING SPEED
RANGE AT CRUISE
SERVICE CEILING
FUEL CAPACITY
OIL CAPACITY
FUEL CONSUMPTION
I 84 lbs
6 Ibs/sq.ft
22 Ibs/HP
80 mph at 3000 feet
68 mph
28 mph
204 miles
12,000 feet
9 gals.
4 quarts
3 gal/hr
J--9-6
6" RADIUS
6"RAOIUS-
RED
A-40-2,
35-37 HP at 2,550rpm
POWER: CONTINENTAL
IO^2” RADIUS
12 ' RADIUS
7^2 RADIUS
T
16'
£ HINGE
26”
-7%
8x SCALE OF DRAWING
WHITE ON RED FIN
SILVER, LICENSE BLACK
AIRFOIL USA-35B
63'
ILVER
0
2	3	4	5
6
SCALE BARS
DIAGONAL STEEL TUBE
CABIN SWAY BRACE—\
NOSE AREA,
RED —
о
27? IN]
AT ROOT
\ FALSE SPRUCE
— SPAR
CLAMP AROUND
LIFT STRUTS AT
JURY STRUTS
И
T
SKYLIGHT & WINDOWS
OF PYRALIN
ONE PIECE WINDSHIELD
OIL FILL AND
ENGINE BREATHER
WING MOUNT
FITTINGS
CABIN SWAY-BRACE WING T E ANTI-FLUTTER
"N” STRUT	BRACE
CARRY THROUGH
TUBE
CABIN DETAIL
2 meters
9’-0k2'
T
I31/,
63"
32 Ц"
Z ALUMINUM
LEADING EDGE
eV
I
1ST0RICAL
Aviation
Album
MY SINCERE APPRECIATION
TO RICHARD C. "DICK " HILL AND
BILL KNEPP FOR THEIR HELP IN
THE PREPARATION OF THESE
DRAWINGS	г
---------------------T“**A	----
TAYLOR E-2 "CUB
1931-36
SCALE •• ORIGINAL - 1-24
REPRO. - 148
DRAWN BY PAUL R MATT
(c) HISTORICAL AVIATION ALBUM 1986
HI5IORICAL AVIATION ALBUM ЗбГ
RO. SOX 33
GENERAL SPECIFICATIONS
WEIGHT EMPTY
USEFUL LOAD
GROSS WEIGHT
WING AREA
WING LOADING
POWER LOADING
MAXIMUM SPEED
CRUISING SPEED
LANDING SPEED
RANGE AT CRUISE
SERVICE CEILING
FUEL CAPACITY
OIL CAPACITY
FUEL CONSUMPTION
563 lbs.
407 ibS
9 70 lbs
I 78 sq ft
5 44 lbs /sq ft
25 5
85
70
29
200
12,000
9
4
3
Ibs/HP
mph
mph
miles
feet
gals
quarts
gal /hr.
А-40-4,
POWER - CONTINENTAL
37 HP at 2550 rpm
40 HP at 2575 rpm LIMITED
COLORING NOTES
OVERALL SILVER WITH THREE DARK BLUE
OR RED FUSELAGE STRIPES
OPTIONAL-RED, BLUE OR GREEN FUSELAGE,
VERTICAL, STRUTS & LANDING GEAR WITH
SILVER OR YELLOW WINGS 8 HORIZONTAL
TAIL SURFACES
CUSTOM COLORS AVAILABLE INCLUDING
OVERALL METALLIC BRONZE-GOLD
WITH RED TRIM
CABIN DETAIL
|2 meters
SCALE BARS
35'-2‘/2
SKYLIGHT A WINDOWS
OF PYRALIN
3-PIECE WINDSHIELD
MY SINCERE APPRECIATION
TO RICHARD C. “DICK “ HILL AND
BILL KNEPP FOR THEIR HELP IN
THE PREPARATION OF THESE
DRAWINGS
SWAY-BRACE
"N'STRUT
© HISTORICAL AVIATION ALBUM 1986
BOX 33
TAYLOR J-2 CUB
"THE SILVER CUB" 1937
SCALE  ORIGINAL- L24
REPRO. - 148
DRAWN BY PAUL R. MATT
WING MOUNT
FITTINGS
CARRY THROUGH
TUBE
26 л
102'/
OIL FILL ANO
ENGINE BREATHER
ALUMINUM
LEADING EDGE
zsezioN
AIRFOIL USA-35B MODIFIED
---63
AT ROOT
CLAMP AROUND
LIFT STUTS AT
JURY STRUTS
ISTOkhaI
iVIATFJN
WBUM
© HISTORICAL AVIATION ALBUM 1986
GENERAL SPECIFICATIONS MB-ЗА
138
------------5’ O'/2 "---------
TAIL SURFACES USED ON LAST
50 BOEING BUILT MB -3As
I' 11%
I 2'4
2'0
AUX. FUEL TANK GAUGE
FIXED HOISTING PIN
PILOTS KNEES)
KELLEY
26'0
INC. AT TIP
INC. - CENTER LINE TO FIRST STRUTS
3. 2’ 20
THOMAS-MORSE
MB-3
1919-29
SCALE - Г-32
DRAWN BY- HERB
INKED BY- HERMAN LUEVANO
PAUL R MATT
to 141 mph.
125m. ph.
55 mp.h.
1230 ft/min. S.L.
19,500 ft.
1716 lbs.
823 lbs.
2539 lbs.
2 hrs. 15 min. (45 gals, fuel)
TOP SPEED
CRUISING SPEED
LANDING SPEED
INITIAL CLIMB
SERVICE CEILING
WEIGHT EMPTY
USEFUL LOAD
GROSS WEIGHT
ENDURANCE
POWER- 300 kp. WRIGHT-HISPANO H-3 ENGINE
FEET
2 METERS
PLY VENEER
AREAS
LOWER WING PLANFORM
” FALSE" SPARS
MAGNETIC
COMPASS
PLY VENEER LEADING EDGE
AIRFOIL TWICE SCALE
AUX. FUEL TANK. (MAIN TANK
IN FUSELAGE BETWEEN HU
WATER TANK, FWD.
.50 col. M.G. BLAST TUBE
(.30 cal. ON RIGHT)
PITOT LEAD LINES (2)
CARBURETOR INTAKE
BOEING
MB-ЗА
ISTWAL
iVIABON
RAlbum
»--------4’ 5й-----------1
PLANFORM PROTOTYPES a
MAJOR PRODUCT-
ION MACHINES
PLY VENEER
LEADING EDGES
COLORING NOTES
ENTIRE AIRCRAFT. OLIVE DRAB,-
BLACK MARKINGS
EXPOSED STRUTS, CLEAR
VARNISHED SPRUCE
4 BLADED PROPELLER
USED ON LATE MB-3As
ONLY 4 WITHOUT A
SPINNER
METAL
LEADING EDGE
SHEATHING
-----7’6
BOTH PROPELLERS, SAME DIAMETER
MAHAGONY WOOD


DRAWING No. 4-28-Bj
Т7И»
ukawn BY- HERB KELLEY-
INKED BY-HERMAN LUEVANO
4 PAUL R. MATT

PLATE I of 2
26'0
HEX CORE RADIATOR
ADJUSTABLE SHUTTERS
RIGGING NOTE:
INCIDENCE, BOTH WINGS,
3’ CENTER SECTION TO
FIRST STRUT, WASH-OUT
TO 2* 20' AT TIP
FUEL TANK VENT
WATER EXPANSION TANK
INTAKE WATER PIPES
SERIAL NUMBER ASSIGNMENTS
40092-40095
4
BOEING
254
2’2
[drawing No. 4-28-B~]
PLATE 2 of 2
63331 - 63365
64124- 64138
68237-68436
35
15
200
WHEEL IN GROSS WEIGHT
GROUND POSITION
FIXED BOMB RACK
FITTINGS (FWD. AFFIXED
AS NEEDED)
BLUE
WHITE
RED
ABOVE IS VERTICAL TAIL
SURFACES USED ON LAST
50 BUILT BY BOEING
Thomas Morse
PROTOTYPES
T.M. PRODUCTION
3* DIH.
AT FWD. SPAR LINE
MAJOR PRODUCTION
VERTICAL TAIL SURFACES
4 6 GAP AT
INBOARD
CENTER
SECTION
KELLEY
_______	. LUEVANO
& PAUL R. MATT
© HISTORICAL AVIATION ALBUM 1967
24' 5" LOWER SPAN
3е DIH.
5* MAXIMUM
4‘ 9%
®EMPTY GUN SHELLS
EJECTION CHUTE AND
DEFLECTION PLATE
SCALE BARS
20'0'
FEET
J METERS
PROTOTYPE
FIN OUTLINE

~l’ 9411
IST0R1CAL
Aviation
/\Album
3’0>2
THOMAS-MORSE
MB-3
1919-29
SCALE- 1 = 32
DRAWN BY- HERB
INKED BY-HERMAN
BOEING
MB-3A
GENERAL SPECIFICATIONS
PRODUCTION STAB ,
RETRO-FITTED TO
PROTOTYPE AFTER
SMALLER AREA WAS
FOUND UNSATISFACTORY
WINGS-WOOD SPARS & RIBS, STEEL TUBE
COMPRESSION MEMBERS, CABLE TIE BRACING
FABRIC COVERED. ALL FULL RIBS 12" ON
CENTER, FALSE NOSE RIBS 6"
mph
ft /min at S L
feet
miles
sq ft
COLORING NOTES
EXACT COLORING OF NC 887E IS NO LONGER
REMEMBERED, BUT BELIEVED TO HAVE BEEN
SILVER WINGS & TAIL SURFACES, DARK BLUE
FUSELAGE AND BLACK DETAILS
8- ift
33/я
36
NC337
I DRAWING No. 8-72-A |
PLATE I of 2
END RIB SLANTED OUTBOARD
TO FORM CONTOURED TIP
ENLARGED AND MODIFIED VERTICAL TAH_
SURFACES AS EMPLOYED ON COLLEGIATE
C/N 101 IN LATE SERVICE	I
BOW TIP TO
MATCH EDGE
RADIUS
FWD CYLINDER BANKS
AFT CYLINDER BANKS
FAGE & COLLINS AIRFOIL No. 4
NACA REPORT 124
( DRAWN TWICE SCALE)
© HISTORICAL AVIATION ALBUM 1970
R О BOX 33
TEMPLE CITY, CALIF 91780
SCALE- ORIGINAL I 24
REPRO. Г48
DRAWN BY - RftUL R MATT
WEIGHT EMPTY
USEFUL LOAD
GROSS WEIGHT
TOP SPEED
CRUISING SPEED
LANDING SPEED
RATE OF CLIMB, INITIAL
SERVICE CEILING
CRUISE RANGE
WING AREA (incl ailerons)
1663 lbs (Model C-185)
702 lbs.
2365 lbs
118 mph (100hp Kinner powered)
92 mph
35
640
18,000
500
236
CARBURETOR INTAKE
OIL COOLING INTAKE VENT
21 к»
COLLEGIATE NC 887E, PORTRAYED,
WAS COMPLETED MARCH 12, 1929
POWER-CURTISS R-600 CHALLENGER
6-CYL RADIAL, 170 hp at l800rpm
185 hp at 2000 rpm
OUR SINCERE APPRECIATION IS
EXTENDED TO MR OTTO TIMM FOR HIS
PERSONAL HELP AND INTEREST IN
MAKING THESE DRAWINGS POSSIBLE.
A SPECIAL THANKS ALSO TO REVEREND
BOARDMAN C. REED FOR HIS UNTIRING
PERSONAL INTEREST IN THE TIMM
COLLEGIATE PROJECT-_______________
AILERON BELL CRANK
INSPECTION HATCH
LANDING GEAR
4774
-INTERNAL STRUCTURE,
ENTIRE HORIZONTAL
TAIL SURFACES OF WELDED
STEEL TUBING. FABRIC
COVERED
STEP PLATE, CAST ALUMINUM
STEEL STIRRUP
SCALE BARS
FUEL FILL, 39 gals.
OIL FILL, 4 gals.
2 meters
TUBE MEMBERS
TIE CABLES
ззЧ
84
1ST0MCAL
iwmoN
AAlbum
TIMM С-Г70 COLLEGIATE
_________1928-31__________
СОЛ Ki
35- 3"" SPAN---1-
0* DIH
LIGHT
HAMILTON STANDARD PROPELLER
l5’.6».-PANEL
W"JURY STRUTS
8-6
m ж mm
л =
mom
? дэт
НСВБ/с
DATUM
_L1
II72
4672
DRAWING No. 8-72-A
PLATE 2 of 2
TOOL & BAGGAGE
COMPARTMENT (30 lbs.)
FULL SWIVEL TAIL
WHEEL, 10" BALLOON
TIRE
STABILIZER ADJUSTABLE FROM
COCKPIT, 0* THROUGH -3*
DRAWINGS PREPARED FROM TIMM AIRCRAFT CORR
BLUEPRINTS M-150, TC-165, F MASTER AND RELATED
FUEL LINE
-PUSH PULL AILERON
RODS, TO BELL
WITHIN CENTER
SECTION
© HISTORICAL AVIATION ALBUM 1970
R 0. BOX 33
TEMPLE CITY, CALIE 91780
SCALE - ORIGINAL I 24
REPRO U48
DRAWN BY-PAUL R- MATT
I
GLASS TUBE
FUEL GAUGE
PITOT
ASSEMBLY
PRODUCTION LANDING GEAR,
RETRO-FITTED TO PROTO-
TYPE AFTER ORIGINAL
CONFIGURATION WAS
DISCARDED.
26" x 9.5"
BALLOON TIRES---
2	3
SCALE BAR, feet
8-0"
WOOD FAIRING
LONGERONS
datum
2
SCALE BAR, meters
22' -4'/2'
STANDARD PRODUCTION VERTICA
TAIL SURFACES, THREE OTHER
SIMILAR SHAPES WERE USED, ALL
DIFFERING FROM FACTORY DWGS
NON-SKID ALUM
STEP PLlATES
ISTORKAL
iVlATION
/\Album
TIMM C-170 COLLEGIATE
_________1928-31___________
GENERAL SPECIFICATIONS
R-3 IN FINAL CONFIGURATION
THREE R-3s WERE BUILT, AS22-326, 22-327 AND 22-323 (t922). DESIGNED
BY ALFRED к VERV/LLE, CHIEF OF PURSUIT AND RACING PLANE DESIGN
WEIGHT EMPTY
USEFUL LOAD
2032
47 1
lbs.
lbs
GROSS WEIGHT
MAXIMUM SPEED
2503
219
WITH WATER
INCLUDING 271 lbs OF
DISPOSABLE WEIGHT
LANDING SPEED
STALLING SPEED
FUEL CAPACITY
OIL CAPACITY
WING AREA
POWER - CURTISS
lbs
m p h. I.A.S. at 2400 r.p.m.
OVER MEASURED TRIANGLE
COURSE (T.A.S. 235mph)
73. 2 m p h	«*
78
40
4
146.5
D-12 500
507
(NOT HIGH COMPRESSION ENGINE)
mp.h.
ga Is.
gals.
sq ft
h p at 2200 r.p.m
h p. at 2380 r p m
CONSTRUCTION NOTES
WINGS - WOOD, PLYWOOD RIBS, TAPERED SPRUCE
BOX SPARS, PLYWOOD COVERED
FUSELAGE - WELDED STEEL TUBING, FABRIC COVERED
AFT PORTIONS, ALUMINUM COVERED
FORWARD
EMPENNAGE - WELDED STEEL TUBING, FABRIC COVERED
COLORING NOTES
ENTIRE AIRCRAFT - SILVER
LETTERING- BLACK
RUDDER STRIPES - RED, WHITE & BLUE,
BLUE TO TAILPOST
WING RADIATORS - RUSTIC BRASS
WINGS PLYWOOD
COVERED
FUEL FILL
94n at root
FAIRING OVER
LANDING GEAR
MAIN JACKSTAY
RETRACTION
TlNcJ
8-4"	!
TAIL CONE HOUSES
RUDDER CONTROL
SINGLE CAMBERED
AIRFOIL-LEFT SIDE
TO COUNTERACT
ENGINE TORQUE
DIRECTIONALLY
WORM GEAR,
UPPER ADJUSTMENT
---- LUGS
WING THICKNESS ORDINATES REDUCED 25%
ABOUT AIRFOIL MEDIAN LINE
WING SET AT NEGATIVE -I* INCIDENCE THROUGHOUT
PROJECTS, USAS ENGINEERING DIVISION, McCOOK FIELD, DAYTON, OHIO BY
DIRECTION OF BRIG. GEN. WILLIAM MITCHELL, ASST CHIEF U.S. ARMY AIR SERVICE.
LAWRENCE SPERRY AIRCRAFT CO., FARMINGDALE, LONG ISLAND WAS AWARDED
THE CONTRACT TO CONSTRUCT THE AIRCRAFT. FINAL MODIFICATION OF R-3
AS 22-328 WAS MADE IN 1923 AND IT'S ULTIMATE DESIGN FEATURES
BECAME P-362 IN 1924 AND IS PORTRAYED ON THESE DRAWINGS.
RACING NUMBER
UNDERSURFACE LEFT
WING ONLY-7
INSPECTION
PLATE
I
I
SCALE BARS
2 METERS
—---------68 -
-7-6"
FAIRING OVER GEAR
RETRACTION UNIVERSAL
LINKAGE
CURTISS REED
DURALUMIN PROPELLER
ALUMINUM
FAIRING
PLYWOOD
15.5”
60‘
36.5"
WE WISH TO EXPRESS OUR
SINCERE APPRECIATION TO MR
ALFRED V. VERVILLE FOR HIS
PERSONAL ASSISTANCE AND
INTEREST IN THE PREPARATION
OF THESE DRAWINGS
ISTORICAL
iVIATlON
Ulbum
[drawing No. 6-58-A |PLATE I of 2
WHEEL FAIRING
OMITTED TO SEE
CONSTRUCTION
IN EXTENDED
POSITION
SHEET,
BURNISHED
ALUMINUM
WRAPING
SPUN, POLISHED
ALUMINUM SPINNER
VERVILLE-SPERRY R-3
WINNER 1924 PULITZER RACE
A S. 22-328
U.S. AIR SERVICE ENGINEERING DIVISION
McCOOK FIELD PROJECT 362
__________DAYTON, OHIO_________
SCALE - ORIGINAL Г24
REPRO I- 48
______DRAWN BY - PAUL R. MATT__
© HISTORICAL AVIATION ALBUM 1969
P.O. BOX 33
TEMPLE CITY, CALIF. 91760_
.GENERAL-SPECIFICATIONS.
R-3 IN FINAL CONFIGURATION
2032
471
WEIGHT EMPTY
USEFUL LOAD
LANDING SPEED
STALLING SPEED
FUEL CAPACITY
OIL CAPACITY
WING AREA
POWER - CURTISS
lbs. WITH WATER
lbs INCLUDING 271 lbs OF
DISPOSABLE WEIGHT
lbs
m ph. I.A.S. at 2400 r.p.m.
OVER MEASURED TRIANGLE
COURSE (TA S. 235mph)
73. 2 mph
78
40
4
146.5
D-12 500
507
(NOT HIGH COMPRESSION ENGINE)
8'-4”
PLYWOOD
TAIL CONE HOUSES
RUDDER CONTROL
ALUMINUM
FAIRING
2503
219
RACING NUMBER
UNDERSURFACE LEFT
WING ONLY—у
GROSS WEIGHT
MAXIMUM SPEED
INSPECTION
PLATE
T
20”
---7-6
AT ROOT
[DRAWING No. в-58-A |
WHEEL FAIRING
OMITTED TO SEE
CONSTRUCTION
IN EXTENDED
POSITION
FAIRING OVER GEAR
RETRACTION UNIVERSAL
LINKAGE
CURTISS REED
DURALUMIN PROPELLER
© HISTORICAL AVIATION ALBUM 1969
P.O. BOX 33
TEMPLE CITY. CALIF. 91780
WORM GEAR,
UPPER ADJUSTMENT
---- LUGS
SCALE - ORIGINAL 1-24
REPRO 1-48
DRAWN BY - PAUL R. MATT
mp.h.
ga Is.
gals,
sq. ft.
h p. at 2200 r.p.m
h p. at 2380 r p m
CONSTRUCTION NOTES
WINGS - WOOD, PLYWOOD RIBS, TAPERED SPRUCE
BOX SPARS, PLYWOOD COVERED
FUSELAGE - WELDED STEEL TUBING, FABRIC COVERED
AFT PORTIONS, ALUMINUM COVERED
FORWARD
EMPENNAGE - WELDED STEEL TUBING, FABRIC COVERED
COLORING NOTES
ENTIRE AIRCRAFT - SILVER
LETTERING- BLACK
RUDDER STRIPES - RED, WHITE & BLUE,
BLUE TO TAILPOST
WING RADIATORS - RUSTIC BRASS
WINGS PLYWOOD
COVERED
FUEL FILL-
FAIRING OVER
LANDING GEAR
MAIN JACKSTAY
RETRACTION
SPECIAL VERVILLE AIRFOIL
MODIFIED NACA 81
WING THICKNESS ORDINATES REDUCED 25%
ABOUT AIRFOIL MEDIAN LINE
WING SET AT NEGATIVE -Iе INCIDENCE THROUGHOUT
THREE R-3s WERE BUILT, AS22-326, 22-327 AND 22-328 0922). DESIGNED
BY ALFRED V. VERVILLE, CHIEF OF PURSUIT AND RACING PLANE DESIGN
PROJECTS, USAS ENGINEERING DIVISION, McCOOK FIELD, DAYTON, OHIO BY
DIRECTION OF BRIG. GEN. WILLIAM MITCHELL, ASST CHIEF U.S. ARMY AIR SERVICE.
LAWRENCE SPERRY AIRCRAFT CO., FARMINGDALE, LONG ISLAND WAS AWARDED
THE CONTRACT TO CONSTRUCT THE AIRCRAFT. FINAL MODIFICATION OF R-3
AS 22-328 WAS MADE IN 1923 AND IT'S ULTIMATE DESIGN FEATURES
BECAME P-362 IN 1924 AND IS PORTRAYED ON THESE DRAWINGS.
SINGLE CAMBERED
AIRFOIL-LEFT SIDE
TO COUNTERACT
ENGINE TORQUE
DIRECTIONALLY
METERS
SCALE BARS
68"—
FLAT SHEET,
BURNISHED
ALUMINUM
WRAPING
SPUN, POLISHED
ALUMINUM SPINNER
WE WISH TO EXPRESS OUR
SINCERE APPRECIATION TO MR
ALFRED V. VERVILLE FOR HIS
PERSONAL ASSISTANCE AND
INTEREST IN THE PREPARATION
OF THESE DRAWINGS
I СТЖА1
4 Aviation
AAlbum
PLATE I of 2
VERVILLE-SPERRY R-3
WINNER 1924 PULITZER RACE
A S. 22-328
U.S. AIR SERVICE ENGINEERING DIVISION
McCOOK FIELD PROJECT 362
_________DAYTON, OHIO_______

Vought F4U-1
"Corsair"
F4U-1D "Corsair", June 6, 1944.


105
FAIRING OVER
GUN BUTT-^.
SPLIT HINGE
12V* 4'/г" SOLID RUBBER TIRE,
PNEUMATIC ON EARLY MODELS
INC
2 INC
-------71 4
NACA23OQO
THEORETICAL TIP
NACA 23015 ДТ OUTER PANEL ROOT
CONTROL HORNS
FOR INBOARD
TRIM TABS,
TOPSIDE
CONTROLLED
OUTBOARD
TABS
CARRIER HOOK
CONTROL ROD
SCALE BAR feet
NACA 23018 AT ROOT
2* INC.
GENERAL SPECIFICATIONS
WEIGHT EMPTY
USEFUL LOAD. NORMAL
GROSS WEIGHT, NORMAL
OVERLOAD
WING AREA
MAXIMUM SPEED AT 23,000 feet
CRUISING SPEED
STALLING SPEED
CLIMB. INITIAL, S L.
SERVICE CEILING
FUEL CAPACITY, NORMAL
RANGE -AT CRUISE, INTERNAL FUEL
POWER - PRATT & WHITNEY R-2800-8
8,982 lbs.
3,057 lbs
12,039 lbs
14,009 lbs
314 sq. ft
395 /417 m p h.
180/185 mph
87 m.p.h.
2,890 feet/min
36,800 feel
225 gals.
1,015 miles
2,000 h p. of TAKEOFF
l,800h.p at 15,500 fee!
R-2800-8W (water injection), 2,100h.p.
-ALRfQlL SECTION -
CENTER SECTION NACA 23018
AT ROOT TO 23015
OUTER PANEL NACA 23015 AT
ROOT TO 23000 AT TIP
TAIL SURFACES C V SPECIAL
SYMMETRICAL
ARMAMENT - 6 .50 CALIBRE BROWNINGS, 39lr.pg
2000 lb BOMB LOAD OR EQUIVELENT
DRAWING No AA-
EMPTY SHELL EJECTION CHUTES
MACHINE GUNS 7” ON CENTER
FIXED AT 0* 44‘ POINTING INBOARD
SCALE BAR meters
PLATE 3 of 3
6 SPOILER BOARD, CORRECTED
NOTICABLE TWITCH TO RIGHT
UNDER CERTAIN CONDITIONS
GREEN
AMBER
RED
RECOGNITION
LIGHTS
SOCKET FITTING FOR MECHANICS
SERVICE STAND
© AERO ALBUM 1968
P. 0. BOX 33
TEMPLE CITY, CALIF. 91780
0
О
ORIGINAL AREA USED FOR MECHANICAL ft TECHNICAL
DATA RECORDING, LATER EMPLOYED FOR AIRCRAFT
STATUS NUMBER
TRAP DOOR VENT, COOLERS
BOMB RACK
CATAPULT HOOK
TRAP DOOR VENT. ENGINE COMPONENTS
О
О
о © •[
©ffi
NATIONAL INSIGNIA VARIED IN SIZE
AND POSITION, STANDARD 50" STAR
ON 54" DISC. POSITION VARIED AS
MUCH AS 9" INBOARD AND 16 "OUTBOARD
VOUGHT F4U-ID "CORSAIR
TYPICAL F4U-I, FG-I, F3A-I SERIES
SCALE - ORIGINAL I 24
REPRO. I 48
DRAWN BY- PAUL R. MATT

33' 3"-
CLEAR FORMATION
LIGHT
(A) BOTH WING PANELS OF SAME
PHYSICAL LENGTH S OUTLINE
(500 lbs. GP BOMB ON £ )
31 I %
9756
2* INC
METAL
T
27’ DIA. STREAMLINE TIRE
SBU-I
© HISTORICAL AVIATION ALBUM 1966
FABRIC
COVERED
RUDDER
INCIDENCE
N-69
PLATE 2
NOTE; PORT SIDE BAGGAGE COMPARTMENT
SUFFICIENT FOR OVERNIGHT SUITCASE
AND 4 FIFTHS OF SCOTCH
L’_
UNDER
SURFACE
TAPER
2
J7 METERS
w SOLID RUBBER TIRE
6x 2.5"
HORIZONTAL STABILIZER
FIXED AT *5*
AIRFOIL NAVY
CHANCE VOUGHT
1936-39
SCALE: 148
DRAWN BY: HERB KELLEY
S PAUL MATT
5' 67/e
TIE DOWN RING
0* DIH. AT 30%
CHORD
10' 3'
NOTE BOMB
CAPACITY LIMITED
TO EITHER WING
STORES OR C
500 lbs.
FEET
RED
YELLOW
BLUE
FLAT BLACK
27'9%
METAL
FIN
46
T.E. AT
FUSELAGE
STA. 7
ISTOWCAL
AVIATION
\Album
INSIGNIA COLORS VS-3B
INDIAN HEAD, BLACK SILHOUTTE
DETAILED IN RED
OUTER CIRCLE, BLACK
INNER DISC, RED
TEETH a HAIR CLASPS, WHITE
Vought XF5U-1
Vought XF5U-1, mock up completed.
Vought XF5U-1 airplane under ground run conditions, August 21,1947.





Waco YMF-5
1	Glove Compartment	12	Tachometer
2	Cylinder Head Temp.	13	Compass
3	Oil Temp.	14	Airspeed
4	Climb Indicator	15	Clock
5	Turn & Bank	16	Engine Primer
6	Altimeter	17	Throttle and
7	Manifold Pressure		Mixture Control
8	Electrical Fuses	18	Service Step
9	Parking Brake Lock	19	Brake Line
10	Ignition Switches	20	Rudder Pedal
11	Oil Pressure		


	
	
29308 thru	29363	-	55
299 06 "	30179	- 273
32014 "	32195	’ 181
	TOTAL	509
	WACO UPF-7 1937-42
	SCALE-ORIGINAL	1:24 REPRO	1 : 48
	DRAWN BY: PAUL R. MATT
PLATE 1 OF 2	© HISTORICAL AVIATION ALBUM 1970 P 0 BOX 3 3 TEMPLE CITY, CALIF. 91780
23’-6
RED DATA PLACARD
DATUM_____
8*63/4
15*30 APPROX.
SCALE BARS
0
TIRES OPTIONAL -
8.50 x 10 STANDARD
CURTISS-REED
FORGED STEEL
PROPELLER,
FIXED PITCH
FUSELAGE CONSTRUCTION.—
WELDED STEEL TUBING, WOOD FAIRING,
FABRIC AFT COVERED, ALUMINUM DECKING,
HEADREST, FORWARD ENGINE AREA AND
ALL FILLETING
2	3
FLAT
BLACK
EXTERNAL
I CARBURETOR
LINKAGE

0
FEET
2
J METERS
DRAWING NO. 8-67-A
PLATE 2 OF 2
WHITE LICENSE NUM^ERS
65 3/4'
GROUND ADJUSTABLE
METAL TRIM TAB
STEERABLE TAIL WHEEL THROUGH
LINKAGE WITH RUDDER, 10"
BALLOON PNUEMATIC TIRE
। I’STOWCAL
MVlAnON
WACO UPF-7
1937-42
SCALE - ORIGINAL
REPRO.
1: 24
1: 48
DRAWN BY: PAUL R. MATT
LBUM
© HISTORICAL AVIATION ALBlJM 1970
P.O BOX 33	,	b
TEMPLE CITY, CALIF, 91780______✓
YKS-6 PLACARD SPEEDS - LEVEL FLIGHT 140 m.p. h. Indicated
GENERAL SPECIFICATIONS
WEIGHT EMPTY	1945 lbs.
USEFUL LOAD	767 lbs.
GROSS WEIGHT	2745 lbs.
TOP SPEED	144 m.p.h at S.L.
CRUISING SPEED	135 m.p h.
LANDING SPEED	55 m ph
RATE OF CLIMB	850 ft /min -initial
FUEL CAPACITY	70 gals
OIL CAPACITY	5 gals.
CRUISING RANGE	518 miles
SERVICE CEILING	12,500 ft.
WING AREA	244 sq ft.
WING LOADING	13.32 lbs /sq f t
POWER LOADING	14.44 Ibs /H.P
GLIDE or DIVE 168 m.p.h.
TRIM TAB ADJUSTMENT PLATE
FILLETS
ON ALL SOCKET LINKAGE
METERS
CORRUGATED ALUMINUM
AILERONS-34 STIFFENERS
LINKAGE & CABLES TO CONTROL
AT PILOT POSITION.
DATA APPROX, a APPLIES TO BASIC YKS-6
IN CLASS II CATEGORY UNDER А.ТС.-533
BALL JOINT
POINTS
10'8
NC-16592 HAS BEEN FLYING
PITOT
6"4
29
TWICE SCALE
WHEN O.A, COLOR
SCHEMES WERE USED-WEIGHT
BRAKE LINKAGE
FAIRING COVER
YKS-6.
REGULARLY FOR OVER 29 YEARS
24 5
AILERON CONTROLS-BELL CRANK SYSTEM TO
PUSH-PULL ROD RUNNING THROUGH LOWER WING
AND INTO FUSELAGE UNDER REAR SEAT, THENSE
SIMILAR .............  “	------
COLUMN
Note: this drawing is typical of the
ENTIRE -KS SERIES (UKS , VKS, YKS, ZKS, VKS-7F).
MINOR CHANGES WERE INCORPORATED DURING
VARIOUS YEARS OF PRODUCTION. DIMENSIONS а
DESIGN VARIED LITTLE THROUGHOUT THESE YEARS
O.A. LENGTH WITH PROPELLER USED, FUEL
CAPACITY 50 to 70 gals-. GEAR TREAD ACCORDING TO
MODIFICATION a WEIGHT CLASS CATEGORY UNDER
АТС PERMIT. GROSS WEIGHT a USEFUL LOADS
VARIED ACCORDING TO OPTIONAL EQUIPMENT (INCL.
ENGINE INSTALLATION) UNDER CLASS PERMIT ISSUED-
ALUM. FILLET
WINGS LINEN COVEREDj
BALANCE MUSLIN COTTON FABRIC
COVERED, TITANINE DOPED-
BERRYLOID COLORS
1 AIRFOIL CLARK Y
COLORING NOTES:
AIRCRAFT PORTRAYED, O.A. SILVER , BLACK TRIM,
NO PIN STRIPING-S/N4526
STANDARD COLORS FOR -KC.-KS SERIES:
GUNMETAL GRAY, SILVER, INSIGNIA BLUE
WITH BLACK, VERMILLION, WHITE OR
FRENCH GRAY TRIM
INSPECTION
PLATES
(metal)
OIL FILLER
ACCESS
FEET
GRIMES
RETRACT-
ABLE LAND
ING LIGHT
(optional)
35 gal
FUEL TANK
(25 gal. normol)
35 gal BECAME STANDARD
ON 1937 MODELS a ALL
SUBSEQUENT ”s" TYPES
PENALTY WAS AS FOLLOWS;
SILVER	NONE
DARK BLUE	7 lbs.
BLACK	36	lbs.
VERMILLION	40 lbs.
WHITE	48	lbs.
FRENCH GRAY	5 1 lbs.
OTHER COLORS a COMBINATIONS WERE AVAILABLE
ISTOMCAL
iVIATFJN
AAlbum
UPON CUSTOMER REQUEST
PLATE I
WACO YKS-6
(1936)
SCALE1 148
DRAWN BY PAUL R. MATT
© PAUL R. MATT, 1965


38*0'
WINGS TWISTED, SPARS REMAIN
PERPENDICULAR TO CHORD LINE
ALUMINUM COVERED
CENTER SECTION
POSITION OF PROPELLER FOR
SAFEST SURFACE TRAVEL
12 —
INC.*5
SCALE BARS
INC. * I at tip
10-
9 -
"AEROBILE" N0.6-N54P • DARK BLUE$ &US^HITE
(LATE POST WAR П DEVELOPMENT)
OVERHEAD CONTROL COLUMN-
STEERING WHEEL (AIR & SURFACE
MANEUVERS), OPERATED INTERCONNECTED
ELEVONS, RUDDERS & NOSE WHEEL
„ WHEEL-PANTS,
AS FENDERS REQUIRED
FOR SURFACE TRAVEL
4* WASHOUT
AT CHORD LINE
TRAILING EDGE
PROGRESSIVE DEVELOPMENT
OF FUSELAGE
FWD. OF 6
AFT OF 7
THRUST LINE
DATUM
COLORING NOTES
"ARROWBILE" No.l - X 262Y-ORIGINALLY ALL SILVER (PROTO.
AS NR 262Y, DARK GRAY & WHITE
No.2- NR 16332 - DARK BUICK BLUE & WHITE
No. 3 - NR 18932 - RED & WHITE
К°Д'йо	ASSIGNED, MACHINES NOT
No.5-NR 18934-J COMPLETED TO POINT
WHERE APPLICATION
5'10
DATUM
FEET
AIRFOIL NACA 23012
METERS
2 V
5&6
<t HINGE
2 3
FAIRINGS OVER
WING FITTINGS
RADIATOR
FILL---
DECORATIVE
GRILL
FUEL FILLER
NECK
20 0
WATERMAN ARROWBILE
tltllOHIIIH-
PLATE 2
BENDIX-
BRAKES
STEERING \
CONTROL RODS
AIR INTAKE
FOR COOLING
OIL PAN
/	—----------13'7
DASH & FLOOR
BOARD OUTLINE
(1937-38)
SCALE I 48
DRAWN BY PAUL R. MATT
AIR EXHAUST2^
FROM RADIATOR
-9’2.5-—
ENGINE
EXHAUST
BATTERY
CAP VENT
CARBURETOR
INTAKE
EXHAUST WHEN
MUFFLER IS CUT
IN FOR ROAD
OPERATION
THRUST
CLEARANCE
FAIRINGS
DATUM LINE
FORKED
NOSE
GEAR
STRUT



ISIWAL
Aviation
Ulbum
© PAUL R. MATT 1966
WEIGHT EMPTY	885 lbs.
USEFUL LOAD	245 "
GROSS WEIGHT	1130 "
FUEL CAPACITY	10 gals.
OIL CAPACITY	3 •'
SPEED, MAX.	136 mph
LANDING SPEED	60 "
CRUISING SPEED	110 ”,
WING AREA	112 4'q.ft.
WING LOADING	Il.l Ibs/sq.ft
POWER LOADING	12.5 Ibs/H.R
RANGE AT CRUISING	135 miles






л
lbs
SLEEVE
6'2^'
3'5
SECTIONS BELOW, TWICE SCALE
SECTION S-l
15 %"
SECTION R-l
<-IO
ALUMINUM
SEATS
WEIGHT
USEFUL
GROSS
FUEL FILLER,
TANK ON FLOOR
BETWEEN SEATS
AILERON CONTROL CABLE -
ON TOP OF LOWER WING, ENTERS
UNDER FLOOR BOARD TO CONTROL
STICK. SIMILARLY ON UNDER SURFACE
OF TOP WING, RUNNING FULL SPAN
GENERAL SPECIFICATIONS
MAIN CONSTRUCTION,
ASH, SPRUCE & POPLAR,
LINEN COVERED & DOPED
2’9
OUTER RIBS
RED
WHITE
BLUE
UPPER & LOWER PANELS
IDENTICAL EXCEPT AT
CENTER SECTION AREA.
COCADES ON
UNDER SURFACE
OF LOWER WINGS
IN SAME POSITION.
INBOARD
RIBS
^-ALUMINUM COWL
FABRIC AFT
EMPTY	1725
LOAD	595
_____ WEIGHT	2320
ENDURANCE AT	CRUISE-63mph	6
WING AREA (AILERONS	EXCLUDED) 430
AREA OF AILERONS (4)
WING LOADING
POWER LOADING
TOP SPEED
hrs
_ _ sq. ft.
64.6 sq.ft.
5.86 Ibs/sq. ft.
16.86 .........
90 mph
STRUT
SOCKET
69
3*INC
VOUGHT AIRFOIL
(MODIFIED RAF- 15)
3-SPAR WING CELLULE, CENTER SPAR (FALSE) NON-BEARING
REMOVABLE
AFT DECKING
FOR ACCESS
TO FUSELAGE
INTERIOR.
ALUMINUM
KNOTTED CORD-
DOPED TO WING, AS
NON-SLIP WALK WAY
ALUMINUM
DECKING
WRIGHT SIMPLEX "A"2’
150 H R AT
(geared) 1400 r.p.m:
SCALE BAR (feet)
LEATHER COWL
TIE DOWN STRAPS
ISTOWCAL
WlATlON
(Album
WRIGHT-MARTIN model V
(1916)
SCALE = 1:48
DRAWN BY - PAUL R. MATT
0 1965
PLATE I
OAK PROPELLEI
5' T/i' PITCH
DEPRESSED
LOUVERS
26 "x 4” TIRE
— 39’8 >2
4'5 kz
1*45'
-5'4
25‘ 8^'
HAND HOLD
2 I ।
IO
INSTRUMENT PANEL, REAR
COCKPIT ONLY
(TWICE SCALE)
I. ALTIMETER
2.SLIP INDICATOR (R.PM.) PROP
3.	AIR SPEED
4.	CLOCK
5.	OIL PRESSURE
6-AIR PRESSURE (FUEL GAUGE)
7. TACHOMETER (R PM.) ENGINE
8-THERMOMETER (WATER)
9.SHUT OFF VALVE (FUEL)
IO. HAND AIR PUMP (FUEL)
II-IGNITION SWITCHES
12. BLANK AREA (OIL TEMP)
SCALE BAR (feet)
27'2
AILERON CONTROL CABLE CROSSES TO PULLEY
ON LOWER WING, ACROSS WING TO FUSELAGE
ENTRY.
CABLE TO PULLEY OF UPPER WING & ACROSS
ENTIRE SPAN.
ISTORKAL
WlATON
(Ulbum
ENTIRE AIRCRAFT - CLEAR DOPED
ALUMINUM AREAS-NATURAL
PLATE 2
WRIGHT-MARTIN model V
(1916)
SCALE- I 48
DRAWN BY: PAUL R. MATT © 1965
3-View Scale Drawings by Paul Matt
Volume 1 contains all airplanes listed from A through G. Volume 2 contains all airplanes listed from H through W.
If you would like individual, large sheets of any of the below listed scale drawings, send request, catalog #,
appropriate fee, and shipping charge of $3.95. If you want your drawing rolled in a tube — add $4.00. Clear, concise,
uncluttered 3- and 4- view engineering presentations, in large (17" x 22"), easy to work with standard scales. Drawing
is highly detailed and is an accurate working print with all dimensions, specifications, airfoils, cross sections,
templates, and color scheme included. These drawings are part of the collection of the internationally acclaimed and
highly honored Historical Aviation Album. All orders are folded unless a tube is ordered. Each has 2 to 6 large sheets.
Rolled in tube — add $4.00 plus $3.95 postage. Send to: Aviation Heritage, P.O. Box 665, Destin, FL 32540.
VOLUME 1 CONTENTS:	retail price VOLUME 2 CONTENTS:
DRAWING SCALE CODE:
Last letter of catalog number
indicates scale of drawing.
A = 1:24.... 1/2"= T
B = 1:16.....3/4"=	Г
C= 1:48.... 1/4"= T
D= 1:32.... 3/8"= T
E= 1:8....1 1/2"= 1'
F= 1:6.........2"=	1'
G= 1:96.... 1/8"= 1'
RETAIL PRICE
_ Aeromarine 39B................
_ Aeronca 7AC “Champion”........
AeroncaC-2...................
_ Aeronca C-3 “Collegian”.......
_ Aeronca C-3 “Master”..........
Aeronca К....................
Aeronca LB “Low wing”........
_ AlcorC.6.1 Jr. Transport......
_ Anderson-Greenwood AG-14 ...
_ Beechcraft D-18S Twin.........
_ Bell P-39Q “Airacobra”........
_ Berkmans “Speed Scout”........
_ Berliner-Joyce О J-2..........
Berliner-Joyce XF3J-1 .......
_ Boeing 307 “Stratoliner”......
Boeing F3B-1.................
Boeing XF7B-1 ...............
Brewster F2A-3 “Buffalo”.....
_ Cessna 120/140 ...............
_ Cessna C-37 “Airmaster”.......
_ Cessna T-50 “Bobcat”..........
_ Consolidated P2Y-2............
_ Consolidated PBY-5A “Catalina’
_ Curtiss “Carrier Pigeon Г.....
_ Curtiss 1st Milit. Tract. S.C. No. 21/22 1913.(#6-55A, 2 shts.)
_ Curtiss A-3B “Falcon”...........
_ Curtiss AT-9 “Jeep”.............
Curtiss B-2 Condor Bomber......
_ Curtiss B-20 Condor Transport ....
Curtiss F Boat....................
_ Curtiss F92 “Sparrowhawk”.......
_ Curtiss MF-K-6 “Seagull”........
_ Curtiss P-36 “Hawk”.............
_ Curtiss P-6E “Hawk”.............
_ Curtiss PW-8....................
_ Curtiss R-6 Racer...............
_ Curtiss SC-1 “Seahawk”..........
_ Curtiss SNC-1 “Falcon”..........
_ Curtiss SO3C-1 “Seagull”........
_ Curtiss Twin JN.................
_ Curtiss-Cox “Texas Wildcat”.....
Curtiss-Wright T-32 "Condor"...
_ Curtiss-Wright CW-1 “Jr.”.......
_ Douglas 0-2.....................
_ Douglas 0-2H....................
Douglas 0-38...................
_ Douglas 0-38E...................
_ Douglas M-2.....................
Douglas A-20G “Havoc”..........
Etrich 1913 Taube..............
Fairchild FC-1.................
Fairchild FC-2.................
_ Fairchild FC-2W “Stars & Stripes’
_ Fairchild M-62, PT-19 “Cornell” ...
_ Fokker T.5 Netherlands Bomber..
_ Gallaudet D-1...................
_ General Aviation Clark GA-43...
_ Grumman F-11F-1 “Tiger”.........
_ Grumman FF-1 ...................
Grumman G-44 “Widgeon”.........
_ Grumman J2F-5 “Duck”............
(#9-78A, 3shts.)....
(#AM-41 A, 2 shts.)
(#10-80A, 2 shts.)..
(#10-81 A, 2 shts.)..
(#10-82A, 2 shts.)..
(#15-103A, 2 shts.)
(#AM-60A, 2 shts.)
(#4-33D, 2 shts.) ...
(#12-94A, 2 shts.)..
(#6-59A, 3 shts.)....
(#1-7A, 2 shts.).......
(#2-12B, 2 shts.)....
(#AM-48A, 2 shts.)
(#15-104A, 2 shts.)
(#7-63C, 2 shts.) ...
(#AM-56A, 2 shts.)
(#AM-38A, 2 shts.)
(#5-47A, 2 shts.)....
(#1-9A, 2 shts.).......
(#6-50A, 2 shts.)....
(#17-115A, 2 shts.)
(#9-71C,3 shts.) ....
(#17-114C, 3 shts.)
(#2-15A, 2 shts.)....
(#AM-39A, 2 shts.) ..
(#2-18A, 2 shts.)..
(#18-116C, 2 shts.) .
(#18-117C, 2 shts.) .
(#1-1 A, 2 shts.)..
(#18-118A, 2 shts.)..
(#AM-37A, 2 shts.)..
(#7-62A, 2 shts.)..
(#5-42A, 2 shts.)..
(#10-79A, 2 shts.)...
(#HS-73A, 2 shts.)...
(#1-8A, 2 shts.)...
(#AA-65A, 2 shts)....
(#AM-34A, 2 shts.) ..
(#3-21 A, 2 shts.).
(#2-14B, 2 shts.)..
(#1-6C, 2 shts) ...
(#11-88A, 3 shts.)....
(#11-86A, 3 shts.)....
(#11-87A, 2 shts.)...
(#12-92A, 2 shts.)....
(#12-93A, 2 shts.)....
(#14-68A, 2 shts.)....
(#15-102D, 6 shts.) .
(#TB-105D, 3 shts.)
(#17-111 A, 2 shts.)..
(#17-112A, 2 shts.)..
(#17-113A, 2 shts.)..
(#AA-69A, 2 shts.)...
(#AA-61C, 2 shts.)..
(#3-20A, 2 shts.)..
(#13-95D, 2 shts.) ...
(#2-19D, 2 shts.) .
(#AA-77A, 2 shts.)...
(#AM5-30A, 2 shts.)
(#6-53A, 3 shts.)..
..$16.50 _ Heath LNB-4 Parasol..............
..15.00 _ Howard DGA-15P....................
..15.00 _ Howard DGA-3 “Pete”...............
..15.00 _ Howard DGA-4 “Mike”...............
..15.00 _ Howard DGA-5 “Ike”................
..15.00 _ Howard DGA-6 “Mr. Mulligan”.......
..15.00 _ Hughes 1В Longwing Racer..........
..15.00 _ Hughes 1В Shortwing Racer.........
..15.00 _ Laird LC-DW-300 “Solution”........
..16.50 _ Laird LC-DW-500 “Super Solution”
.. 15.00 _ Laird-Turner LTR-14..............
..15.00 _ Lavochkin LA-7....................
..15.00 _ Lockheed P-80B “Shooting Star”...
..15.00 _ Lockheed Model 9 “Orion”..........
.15.00 _ Lockheed PV-1 “Ventura”............
.T.. 15.00 _ LWF Cato Model L “Butterfly”...
...15.00 _ LWF Model G-2....................
...15.00 _ LWF Model H-1 “Owl”..............
... 15.00 _ Martin BM-1 and 2...............
...15.00 _ Martin T4M-1, Great Lakes TG-1 ..
...15.00 _ Martin TT, 1913 Trainer..........
...16.50 _ Messerschmitt Me 109 E-3.........
...18.00 _ Morehouse 2 Cyl. Aero Engine.....
...15.00 _ Navy-Wright NW-1 Mystery Racer
...15.00 _ Navy-Wright NW-2 Mystery Racer
...15.00 _ North American 0-47A.............
...15.00 _ North American AT-6D “Texan".....
...15.00 _ North American XB-70-1 “Valkyrie”
...15.00 _ Packard-Le Pere LUSAC-11 ........
... 15.00 _ Pfitzner 1910 Monoplane.........
...15.00 _ Piper J-3 “Cub”..................
...15.00 _ Piper J-4 “Cub Coupe”............
...15.00 _ Piper PA-12 “Super Cruisef.......
...15.00 _ Republic RC-3 Seabee.............
...15.00 _ Rover Inverted Aero Engine.......
...15.00 _ Ryan B-5 “Brougham”..............
... 15.00 _ Ryan FR-1 “Fireball”............
...15.00 _ Ryan SCW Low Wing................
...15.00 _ Ryan ST-A........................
...15.00 _ Seversky BT-8....................
...15.00 _ Seversky P-35....................
... 15.00 _ Sikorsky S-39B..................
...16.50 _ Standard J-1 ....................
...16.50 _ Taylor E-2 “Cub”.................
...15.00 _ Taylor J-2 “Cub”.................
....15.00 _ Thomas-Boeing MB-ЗА and
....15.00 Thomas-Morse MB-3.................
....15.00 _ Timm TC-170 “Collegiate”........
....20.00 _ Verville R-3 Racer..............
....16.50 _ Vought F4U-1 “Corsair”..........
....15.00 _ Vought SBU-1....................
....15.00 _ Vought XF5U.....................
....15.00 _ Vultee V-1A Transport...........
....15.00 _ Waco UMF/YMF-5..................
....15.00 _ Waco UPF-7......................
....15.00 _ Waco YKS-6 Cabin................
....15.00 _ Waterman “Arrowbile”............
....15.00 _ Waterman “Gosling” Racer........
....15.00 _ Wright F2W-1 Racer..............
....15.00 _ Wright F2W-2 Racer..............
....16.50 _ Wright Brothers 1903 Flyer......
 Wright-Martin V................
(#4-35B, 2 shts.)........
(#AM-52A, 2 shts.).......
(#12-89A, 2 shts.).......
(#13-90A, 2 shts.).......
(#13-91 A, 2 shts.)......
(#14-99A, 3 shts.).......
(#16-108A, 3shts.).......
(#16-107A, 3 shts.)......
(#7-64A, 2 shts.)........
(#8-74A, 2 shts.)........
(#10-83A, 2 shts.).......
(#AA-46A, 4 shts.).......
(#2-1OA, 2 shts.)........
(#3-22A, 2 shts.)........
(#E-1O1C, 3 shts.).......
(#10-84A, 2 shts.).......
(#2-1 ЗА, 2 shts.).......
(#11-85C, 2 shts.) ......
(#1-5A, 2 shts.).........
(#4-29D, 2 shts.) .......
(#5-40A, 2 shts.)........
(#AA-75A, 2 shts.).......
(#3-27E, 1 sht.).........
(#4-31 A, 2 shts.).......
(#4-32A, 2 shts.)........
(#13-98A, 3 shts.).......
(#16-106A, 3 shts.)......
(#7-66G, 3 shts.)........
(#1-3A, 2 shts.).........
(#2-11A, 2 shts.)........
(#18-121 A, 2 shts.).....
(#18-122A, 2 shts.)......
(#4-36A, 2 shts.)........
(#16-109A, 3 shts.)......
(#5-45F, 1 sht.).........
(#RB-96A, 2 shts.).......
(#3-26A, 2 shts.)........
(#AM9-49A, 2 shts.)......
(#9-76A, 2 shts.)........
(#3-23A, 2 shts.)........
(#AA-57A, 2 shts.).......
(#14-100A, 5 shts.)......
(#17-110A, 2 shts.)......
(#18-119A, 2 shts.)......
(#18-120A, 2 shts.)......
(#4-28B, 2 shts.)........
(#8-72A, 2 shts.)........
(#6-58A, 2 shts.)........
(#AA-51A, 3 shts.).......
(#3-24A, 2 shts.)........
(#8-70A, 3 shts.)........
(#2-16A, 2 shts.)........
(#13-97A, 3 shts.).......
(#8-67A, 2 shts.)........
.(#2-17A, 2 shts.).......
(#3-25A, 2 shts.)........
(#1-4B, 2 shts.).........
(#5-43A, 2 shts.)........
(#5-44A, 2 shts.)........
(#0-123A, 2 shts.).......
(#1-2A, 2 shts.).........
15.00
15.00
15.00
15.00
15.00
16.50
16.50
16.50
15.00
15.00
15.00
18.00
15.00
15.00
16.50
15.00
15.00
15.00
15.00
15.00
15.00
15.00
8.00
15.00
15.00
16.50
16.50
16.50
15.00
15.00
15.00
15.00
15.00
16.50
12.00
15.00
15.00
15.00
15.00
15.00
15.00
18.50
15.00
15.00
15.00
15.00
15.00
15.00
16.50
15.00
16.50
15.00
16.50
15.00
15.00
15.00
15.00
15.00
15.00
15.00
15.00
All of Paul Matt Drawings are soon to be released on "CD" in TIFF and PCX Format! Reserve your copy Today!! The Paul Matt Scale Drawings
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