Dimensional_Data.htm

Dimensional Data and Principle Characteristics

The tables below show a summary of the dimensional and principle characteristics data that I have collected for US Single Engine WWII era aircraft, from the References listed on the Introduction page.

Caveats

Please note all units are in pounds and that I am still in the process of filling in and confirming some of the information for these tables and graphs.
Because References 1, 2 and 3 sometimes provide data for the same aircraft, this data has been entered in separate, adjacent columns so that the data can be compared.

USAAC Pursuit/Fighter Aircraft - Radial Engine

		Boeing	Seversky	Curtiss	Curtiss	Curtiss	Curtiss	Curtiss	Curtiss	Curtiss	Curtiss	Curtiss	Curtiss	Republic	Republic	Republic	North American	North American
		P-26A	P-35	P-36A	H-75A (CW)	H-75A (P&W)	P-40E	P-40E	P-40F	P-40K	P-40L	P-40M	P-40N-25	P-47D (early)	P-47D-RE	P-47D-25	P-51B & P-51C	P-51D
Reference Sources		2, 3, 5	2, 3, 5	2, 3, 5	3, 4, 5	3, 4, 5	1, 3, 5	2, 3, 5	1, 3, 5	1, 3, 5	1, 3, 5	1, 3, 5	1, 3, 5	2, 3, 5	1, 3, 5	1, 3, 5	1, 3, 5	2, 3, 5
No of Crew		1	1	1	1	1	1	1	1	1	1	1	1	1	1	1	1	1
Engine:
Qty		1	1	1	1	1	1	1	1	1	1	1	1	1	1	1	1	1
Model		R-1340-27	R-1830-9	R-1830-13	R-1820-G105A	P&W S3C3G	V-1710-39	V-1710-39	V-1650-1	V-1710-73 (F4R)	V-1650-1	V-1710-81	V-1710-99	R-2800-63		R-2800-59	V-1650-3	V-1650-7
Displacement	(cu in)	1340	1830	1830	1820	1830	1710	1710	1650	1710	1650	1710	1710	2800	2800	2800	1650	1650
Power
Military	(HP)					1100	1150	1150	1240	1150			1125	2000		2000	1600	1720
War Emergency	(HP)						1490	1490		1580	1435		1360
Normal	(HP)	570	850	900	900	950								1625		1625
Take Off	(HP)	500	950	1050	1100	1100	1150	1150	1390	1325	1385	1360	1200	2000		2000	1280	1315
Eng Dims
Length	(ft)	3.60	4.64	4.94	4.01	5.13								6.31		6.31
Width/Dia	(ft)	4.29	4	4.005	4.59	4.01								4.375		4.375
Height	(ft)
Base Engine Wt	(lb)	715	1292	1292	1287	1463	1310	1310		1345	1510		1355	2265		2290	1700	1715
Propeller
# Blades		2	3	3	3	3	3	3	3	3	3	3	3	4	4	4	4	4
Dia	(ft)			10	10.5	10.125	11	11	11	11	11	11	11	13	13	13	11.17	11.17
Manufacturer		Hamilton Std			Curtiss (Elec)	Curtiss (Elec)	Curtiss (Elec)	Curtiss (Elec)	Curtiss (Elec)	Curtiss (Elec)	Curtiss (Elec)	Curtiss (Elec)	Curtiss (Elec)					Hamilton Std
Type		Fixed Pitch		Const Speed	Const Speed	Const Speed	Const Speed	Const Speed	Const Speed	Const Speed	Const Speed	Const Speed	Const Speed	Const Speed	Const Speed	Const Speed	Const Speed	Const Speed
Wing
Span	(ft)	27.96	36	37.3	37.3	37.3	37.3	37.3	37.3	37.3		37.3	37.3	40.8				37.03
Root Thickness	(%)	10.0%	18.0%	15.0%			15.0%	15.0%						14.0%				15.8%
	(in)	7.2	16.4	16.2			16.2	16.2						15.2				15.8
Total Area	(sq ft)	149.5	220	236	236	236	236	236	236	236	236	236	236	300	300	300	233.19	236
Wing (less Ail & Flaps)	(sq ft)				182.79	182.79			182.8				182.9				188.24
Ailerons	(sq ft)				18.41	18.41			18.4				18.3			25.7	12.73
Flaps	(sq ft)				34.8	34.8			34.8				34.8				32.22
Tail Area	(sq ft)	37.2	54.2	68.74	68.74	68.74	69.04	69.04	69.04	71.22	69.74	69.74	69.04	86.1	86.1	80.8	61.05
V Tail Area	(sq ft)	12.5	19.1	20.74	20.74	20.74	20.74	20.74	20.74	22.92	21.74	21.74	20.74	26.5	26.5	25.8	20.02
Fin	(sq ft)				7	7			7	9.18			7			13.9	9.61
Rudder	(sq ft)				13.74	13.74			13.74	13.74			13.74			11.9	10.41
H Tail Area	(sq ft)	24.7	35.1	48	48	48	48.3	48.3	48.3	48.3	48	48	48.3	59.6	59.6	55	41.03
Stabilizer	(sq ft)				28.8	28.8			30.86	30.86			30.86			33	27.98
Elevator	(sq ft)				19.2	19.2			17.44	17.44			17.44			22	13.05
Total Control Surf Area	(sq ft)				86.15	86.15			84.38				84.28				68.41
Length
Overall	(ft)	23.83	25.3	28.85	28.8	28.8	31.7	31.7	31.6	33.31	33.31	33.31	33.31	35.34	35.34	35.34
Fuselage	(ft)	20.9	23.2	24.4	26.8	26.8	27	27					27.96	31				27.8
Body	(ft)	22.81	24.2	26.8			31.6	31.6	31.6	33.31	33.31	33.31	33.31	33.43	33.43	33.43
Body Depth	(ft)						5.48	5.48	4.8	5.81	5.81	5.81	4.82					11.13
Body Width	(ft)						3.3	3.3	3.08	3.21	3.21	3.21	3.19				2.92	2.92
Fuel Tank Volume	(gal)			163	163	163	143	144	145	146	147	148	154					269.8
Wing Tanks	(gal)			105	105	105	85.5	85.5	85.5	85.5	85.5	85.5	88.0					184.8
FuselageTanks	(gal)	50/106		58	58	58	57.5	58.5	59.5	60.5	61.5	62.5	66.0					85
Oil Tank Volume	(gal)						13.3	13.3	13.3	13.3		13.3	10.0					13.8
Water Fluid Tank Vol	(gal)
Wetted Area (sqf)	(sq ft)																	862.12
Pwr Ldng	(lb/HP)	4.89	5.89	5.27	5.17	5.38		7.33						6.69				7.70
Wing Ldng	(lb/sqft)	19.63	25.45	23.44	24.11	25.08		35.71						44.58				42.88
Struct. Des. GW	(ib)						7400	7400										8000
Ultimate Ld Factor	(G's)				12	11.5	12	12						12				12
Design Speed	(mph)				445	445		496										537
Not to Exceed Speed	(mph)			403

USAAC Pursuit/Fighter Aircraft - Inline Engine

		Consolidated	P-39?	Bell	Bell	Bell	Bell	Bell	Bell	Bell	Bell
		PB-2A		P-39D	P-39D	P-39D-2	P-39Q-1	P-400	XP-63A	P-63A-10	P-63C
Reference Sources		2, 3	3, 4, 5	1, 3, 5	2, 3, 5	1, 3, 5	1, 3, 5	1, 3, 5	1, 3, 5	1, 3, 5	1, 3, 5
No of Crew		2	1	1	1	1	1	1	1	1	1
Engine:
Qty		1		1	1	1	1	1	1	1	1
Model		V-1570-61		V1710-35	V1710-35	V-1710-63	V-1710-85 (E19)	V-1710-E4 (-35)	V-1710-93	V-1710-93	V-1710-117
Displacement	(cu in)	1570		1710	1710	1710	1710	1710	1710	1710	1710
Power
Military	(HP)			1150	1150	1150	1125	1150	1150	1150	1100
War Emergency	(HP)			1490	1490	1580	1410	1490	1825	1825	1800
Normal	(HP)
Take Off	(HP)	700		1150	1150	1325	1200	1150	1325	1325	1325
Eng Dims
Length	(ft)
Width/Dia	(ft)
Height	(ft)
Base Engine Wt	(lb)	1040.76		1375	1375	1435	1452	1375	1613	1613	1660
Propeller
# Blades		3		3	3	3	3	3	4	4	4
Dia	(ft)			10.375	10.375	10.375	11.58	10.375	11	12.17	12.67
Manufacturer		Curtiss (Elec)
Type		Variable Pitch	Const Speed	Const Speed	Const Speed	Const Speed	Const Speed	Const Speed		Const Speed	Const Speed
Wing
Span	(ft)	43.9	34	34	34
Root Thickness	(%)	18.0%		15.0%	15.0%
	(in)	19.7	14.75	15.8	15.8
Total Area	(sq ft)	297		213.22	213.22	213.22	213.22	213.22	248	248	248
Wing (less Ails & Flaps)	(sq ft)		197.7
Ailerons	(sq ft)		15.46	11.82	11.82
Flaps	(sq ft)			26.2	26.2
Tail Area	(sq ft)	58.8		59.05	59.05	60.21	59.01	59.01	69.49	69.49	70.26
V Tail Area	(sq ft)	18.7		19.01	19.01	19.01	18.97	18.97	25.48	25.48	23.73
Fin	(sq ft)			7.94	7.94
Rudder	(sq ft)			11.07	11.07
H Tail Area	(sq ft)	40.1		40.04	40.04	41.2	40.04	40.04	44.01	44.01	46.53
Stabilizer	(sq ft)			23.9	23.9
Elevator	(sq ft)			16.14	16.14
Total Control Surface Area	(sq ft)			65.23	65.23
Length
Overall	(ft)		30.17	30.13	30.13	30.13	30.13	30.13	31.33	31.33	31.33
Fuselage	(ft)	29.5		26.3	26.3
Body	(ft)	28.16		30.38	30.38	30.38	30.38	30.38	31.6	31.6	31.6
Body Depth	(ft)		5.89
Body Width	(ft)		2.90
Fuel Tank Volume	(gal)		120
Wing Tanks	(gal)		120
FuselageTanks	(gal)
Oil Tank Volume	(gal)		13.8	11.7	11.7
Water Fluid Tank Volume	(gal)
Wetted Area (sqf)	(sq ft)
Pwr Ldng	(lb/HP)	7.97			6.44
Wing Ldng	(lb/sq ft)	17.5			34.73
Struct. Des. GW	(lb)		7496	7406	7406
Ultimate Load Factor	(G's)		12	12	12
Design Speed	(mph)				530
Not to Exceed Speed	(mph)

USN Fighter Aircraft - Fixed Wing

		Brewster	Brewster	Brewster	Brewster	Brewster	Brewster	Brewster	Brewster	Brewster	Brewster	Brewster	Brewster	Grumman	Grumman
		X F2A-1	F2A-1 #1	F2A-1	XF2A-2	F2A-2	F2A-3	F2A-3	F2A-3	B239	339B	339D	339E	F4F-3	F4F-3
Reference Sources		1, 3, 8	1, 3, 8	1, 3, 8	1, 3, 8	1, 3, 8	1, 3, 8	1, 3, 8	2, 3, 8	1, 3, 8	1, 3, 8	1, 3, 8	1, 3, 8	1, 3, 5	3, 4, 5
No of Crew		1	1	1	1	1	1	1	1	1	1	1	1	1	1
Engine:
Qty		1	1	1	1	1	1	1	1	1	1	1	1	1	1
Model		XR-1820-22	R-1820-34	R-1820-34	R-1820-40	R-1820-40	R-1820-40	R-1820-40	R-1820-40	R-1820-G5(-34)N548A	R-1820-G105	R-1820-G205	R-1820-G105	R-1830-86	R-1830-76
Displacement	(cu in)	1820	1820	1820	1820	1820	1820	1820	1820	1820	1820	1820	1820	1830	1830
Power
Military	(HP)
War Emergency	(HP)
Normal	(HP)	850	850	850	1000	1000	1000	1000	1000	850	900	1000	900	1100	1100
Take Off	(HP)	950	950	950	1200	1200	1200	1200	1200	950	1100	1200	1100	1200	1200
Eng Dims
Length	(ft)	3.59	3.59	3.59	4.03	4.03	4.03	4.03	4.03	3.59	4.01	4.17	4.01	5.62	5.94
Width/Dia	(ft)	4.52	4.52	4.52	4.59	4.59	4.59	4.59	4.59	4.52	4.59	4.59	4.59	4.02	4.01
Height	(ft)
Base Engine Wt	(lb)	1105	1114	1114	1315	1315	1315	1315	1315	1114	1272	1302	1272	1560	1550
Propeller
# Blades		3	3	3	3	3	3	3	3	3	3	3	3	3	3
Dia	(ft)	9	9	9				10.25	10.25	9			10.08	9.75	9.75
Manufacturer
Type
Wing
Span	(ft)	35	35	35	35	35	35	35	35	35	35	35	35	38	38
Root Thickness	(%)	18.0%	18.0%	18.0%	18.0%	18.0%	18.0%	18.0%	18.0%	18.0%	18.0%	18.0%	18.0%	15.0%	15.0%
	(in)	16	16	16	16	16	16	16	16	16	16	16	16	14.7	14.7
Total Area	(sq ft)	208.9	208.9	208.9	208.9	208.9	208.9	208.9	208.9	208.9	208.9	208.9	208.9	260	260
Wing (less Ail & Flaps)	(sq ft)	177.16	177.16	177.16	177.16	177.16	177.16	177.16	177.16	177.16	177.16	177.16	177.16	218.82	218.82
Ailerons	(sq ft)	15.3	15.3	15.3	15.3	15.3	15.3	15.3	15.3	15.3	15.3	15.3	15.3	11.48	11.48
Flaps	(sq ft)	16.44	16.44	16.44	16.44	16.44	16.44	16.44	16.44	16.44	16.44	16.44	16.44	29.7	29.7
Tail Area	(sq ft)	58.7	58.7	58.7	58.7	58.7	58.7	58.7	58.7	58.7	58.7	58.7	58.7	71.63	71.63
V Tail Area	(sq ft)	19.2	19.2	19.2	19.2	19.2	19.2	19.2	19.2	19.2	19.2	19.2	19.2	22.58	22.58
Fin	(sq ft)	10.3	10.3	10.3	10.3	10.3	10.3	10.3	10.3	10.3	10.3	10.3	10.3	13.2	13.2
Rudder	(sq ft)	8.9	8.9	8.9	8.9	8.9	8.9	8.9	8.9	8.9	8.9	8.9	8.9	9.38	9.38
H Tail Area	(sq ft)	39.5	39.5	39.5	39.5	39.5	39.5	39.5	39.5	39.5	39.5	39.5	39.5	49.05	49.05
Stabilizer	(sq ft)	22.6	22.6	22.6	22.6	22.6	22.6	22.6	22.6	22.6	22.6	22.6	22.6	30.43	30.43
Elevator	(sq ft)	16.9	16.9	16.9	16.9	16.9	16.9	16.9	16.9	16.9	16.9	16.9	16.9	18.62	18.62
Total Control Surf Area	(sq ft)	57.54	57.54	57.54	57.54	57.54	57.54	57.54	57.54	57.54	57.54	57.54	57.54	69.18	69.18
Length
Overall	(ft)	25.61	25.61	25.61	25.61	25.61	26.36	26.36	26.36	26.01	26.01	26.01	26.01	28.78	28.78
Fuselage	(ft)	26.1												26.92	26.92
Body	(ft)	24.12	24.12	24.12	24.12	24.12	24.12	24.12	24.40	24.12	24.12	24.12	24.12	25.94	25.94
Body Depth	(ft)													25.94	25.94
Body Width	(ft)
Fuel Tank Volume	(gal)													147	147
Wing Tanks	(gal)
FuselageTanks	(gal)
Oil Tank Volume	(gal)													11	11
Water Injection Tank Vol	(gal)
Wetted Area (sqf)	(sq ft)
Pwr Ldng	(lb/HP)				4.51	4.52	5.43		6.02						5.75
Wing Ldng	(lb/sq ft)	23.93	24.19	24.20	25.89	25.94	31.20		34.61		26.03	29.17	29.26		26.52
Struct. Des. GW	(lb)								6510
Ultimate Load Factor	(G's)								11.3
Design Speed	(mph)
Not to Exceed Speed	(mph)

USN Fighter Aircraft - Folding Wing


		Grumman	Grumman	Grumman	Grumman	Vought	Vought	Vought	Vought	Grumman	Grumman	Grumman	Grumman	Grumman	Grumman
		F4F-4	F4F-4	F4F-4	FM-2	F4U-1	F4U-1D	F4U-4	F4U-4	F6F-3	F6F-3	F6F-5	F6F-5	F6F-5	F8F-1
Reference Sources		1, 3, 5	2, 3, 5	3, 4, 5	1,3, 8	3, 4, 5	3, 4, 5	2, 3, 5	3, 4, 5	1, 3, 5	3, 4, 5	1, 3, 5	2, 3, 5	2, 3, 5	2, 3, 5
No of Crew		1	1	1	1	1	1	1	1	1	1	1	1	1	1
Engine:
Qty		1	1	1	1	1	1	1	1	1	1	1	1	1	1
Model		R-1830-86	R-1830-86	R-1830-86	R-1820-56	R-2800-8	R-2800-8W	R-2800-18W	R-2800-18W	R-2800-10W	R-2800-10W	R-2800-10W	R-2800-10W	R-2800-10W	R-2800-22W
Displacement	(cu in)	1830	1830	1830	1820	2800	2800	2800	2800	2800	2800	2800	2800	2800	2800
Power
Military	(HP)					2000	2000	2100	2100	2000	2000	2000	2000	2000	2100
War Emergency	(HP)					2250	2250								2750
Normal	(HP)	1100	1100	1100	1200	1675	1675	1700	1700	1675	1675	1675	1675	1675	1700
Take Off	(HP)	1200	1200	1200	1300	2000	2000	2100	2100	2000	2000	2000	2000	2000	2100
Eng Dims
Length	(ft)	5.62	5.62	5.62	3.96	7.81	7.81	7.81	7.81	7.37	7.37	7.37	7.37	7.37	6.51
Width/Dia	(ft)	4.02	4.02	4.02	4.59	4.4	4.4	4.4	4.4	4.375	4.375	4.375	4.375	4.375	4.4
Height	(ft)
Base Engine Wt	(lb)	1560	1560	1560	1333	2560	2560	2560	2560	2460	2460	2460	2460	2460	2359
Propeller
# Blades		3	3	3	3	3	3	4	4	3	3	3	3	3	4
Dia	(ft)	9.75	9.75	9.75	10	13.33	13.08	13.33	13.17	13.08	13.08	13.08	13.08	13.08	12.58
Manufacturer
Type
Wing
Span	(ft)	38	38	38		40.98	40.98	41	40.98	42.83	42.83	42.83	42.83	42.83	35.5
Root Thickness	(%)	15.0%	15.0%	15.0%		18.0%	18.0%	18.0%	18.0%		15.6%		15.6%	15.6%	18.0%
	(in)	15.2	15.2	15.2		18.9	18.9	18.8	18.9		18.63		19.8	19.8	21.9
Total Area	(sq ft)	260	260	260	260	314	314	314	314	334	334	334	334	334	244
Wing (less Ail & Flaps)	(sq ft)	217.04	217.04	217.04		259.5	259.5		259.5		278.5				15
Ailerons	(sq ft)	13.26	13.26	13.26		18.1	18.1		18.1		15.7				18.18
Flaps	(sq ft)	29.7	29.7	29.7		36.4	36.4		36.4		39.8
Tail Area	(sq ft)	71.63	71.63	71.63		79.9	79.9	79.9	79.9	100.1	101.2	100.1	100.1	100.1
V Tail Area	(sq ft)	22.58	22.58	22.58	22.58	22	22	22	22	23.4	23.4	23.4	23.4	23.4	17.7
Fin	(sq ft)	13.2	13.2	13.2		9	9		9		14.4				11
Rudder	(sq ft)	9.38	9.38	9.38		13	13		13		9				6.7
H Tail Area	(sq ft)	49.05	49.05	49.05	49.05	57.9	57.9	57.9	57.9	76.7	77.8	76.7	76.7	76.7	52.27
Stabilizer	(sq ft)	30.43	30.43	30.43		36	36		36		52				33.64
Elevator	(sq ft)	18.62	18.62	18.62		21.9	21.9		21.9		25.8				18.63
Total Control Surf Area	(sq ft)	70.96	70.96	70.96		89.4	89.4		89.4		90.3
Length
Overall	(ft)	28.89	28.89	28.89		33.34	33.34	33.25	33.69	33.83	33.83	33.83	33.83	33.83	27.5
Fuselage	(ft)	25.2	25.2	25.2	25.2				44.69	31.5	31.5	31.5	31.5	31.5
Body	(ft)	25.94	25.94	25.94	25.935	29.83	29.83	29.83	29.83	33.45	33.45	33.45	33.45	33.45	27.3
Body Depth	(ft)
Body Width	(ft)
Fuel Tank Volume	(gal)	144	144	144		178	237	234	250	175	175	175	175	175	185
Wing Tanks	(gal)								250	175	175	175	175	175
FuselageTanks	(gal)														185
Oil Tank Volume	(gal)	11	11	11		20	24.25	23.5	23.5	19	19	19	19	19	17
Water Inj Tank Vol	(gal)						10		13.5		16				16
Wetted Area (sqf)	(sq ft)							404					458
Pwr Ldng	(lb/HP)		6.57	6.19		5.57	5.67	5.83	5.91		5.75		6.13	6.25	4.37
Wing Ldng	(lb/sq ft)		30.30	28.56		35.49	36.12	39.01	39.51		34.45		36.72	37.40	37.60
Struct. Des. GW	(lb)	6436	6436					12036					11000	1000	8551
Ultimate Load Factor	(G's)	13.5	13.5					11.25					13.5	13.5	9.6
Design Speed	(mph)	470	470					555					506	606	477
Not to Exceed Speed	(mph)

Attack, Dive Bomber & Torpedo Bomber Aircraft

		Northrop	Douglas	Douglas	Curtiss	Douglas	Grumman
		A-17A	SBD-6	AD-7	SB2C-5	XBT2B-1	TBM-3
Reference Sources		2, 3, 8	2, 3, 8	2, 3, 8	2, 3, 8	2, 3, 8	2, 3, 8
No of Crew		2	2	1	2	3	3
Engine:
Qty		1	1	1	1	1	1
Model		R-1535-13	R-1820-66	R-3350-26W	R-2600-20	R-3350-24W	R-2600-20
Displacement	(cu in)	1535	1820	3350	2600	3350	2600
Power
Military	(HP)
War Emergency	(HP)
Normal	(HP)	750	1200	2300	1600	2100	1600
Take Off	(HP)	825	1300	2700	1900	2500	1900
Eng Dims
Length	(ft)	4.44	3.96	6.72	5.51	6.72	5.51
Width/Dia	(ft)	3.68	4.59	4.51	4.51	4.51	4.51
Height	(ft)
Base Engine Wt	(lb)	1130	1333	2822	2045	2822	2045
Propeller
# Blades		3	3	4	4	4	3
Dia	(ft)	9.5	10.83	13.5	12	13.5	13.08
Manufacturer
Type		2-Post
Wing
Span	(ft)	47.8	41.51	50	49.7	50	54.2
Root Thickness	(%)	15.0%	15.0%	17.2%	17.0%	17.2%	15.4%
	(in)	15.7	18.6	22.1	24.5	22.1	22
Total Area	(sq ft)	363	323.8	400	422	400	490
Wing (less Ail & Flaps)	(sq ft)
Ailerons	(sq ft)
Flaps	(sq ft)
Tail Area	(sq ft)	90.86	93.21		153.1		141.4
V Tail Area	(sq ft)	26.8	22.45		45.7		38.75
Fin	(sq ft)
Rudder	(sq ft)
H Tail Area	(sq ft)	64.06	70.76		107.4		102.65
Stabilizer	(sq ft)
Elevator	(sq ft)
Total Control Surf Area	(sq ft)
Length
Overall	(ft)	32.1	31.01	39.17	33.61	39.67	39.9
Fuselage	(ft)	28.6	29.8	34.8	32.5	34.1	35.8
Body	(ft)	30.5375	30.91666667		33.6		37.8583333
Body Depth	(ft)
Body Width	(ft)
Fuel Tank Volume	(gal)		260
Wing Tanks	(gal)		260
FuselageTanks	(gal)
Oil Tank Volume	(gal)
Water Injection Tank Vol	(gal)
Wetted Area (sqf)	(sq ft)		447		652		930
Pwr Ldng	(lb/HP)	9.14	7.43	6.64	8.13	6.13	8.65
Wing Ldng	(lb/sq ft)	20.78	29.84	44.82	36.60	38.32	33.55
Struct. Des. GW	(lb)		7338	15595	17000	15600	14500
Ultimate Load Factor	(G's)		14	10.5	12	10.5	6.2
Design Speed	(mph)		425	500	540	500
Not to Exceed Speed	(mph)

Single Engine Monoplane Trainer Aircraft

		Fairchild	Ryan	Seversky	NAA	Vultee	NAA	NAA	NAA
		PT-19	PT-21	BT-8	BT-9B	BT-13	BC-1	AT-6A	SNJ-5
Reference Sources		2, 3	2, 3	2, 3, 5	2, 3, 8	2, 3, 5	2, 3, 5	2, 3, 5	2, 3, 5
No of Crew		2	2	2	2	2	2	2	2
Engine:
Qty		1	1	1	1	1	1	1	1
Model		L-440-1	R-440-3	R-985-11	R-975-7	R-985-25	R-1340-47	R-1340-49	R-1340-AN-1
Displacement	(cu in)	440	440	985	975	985	1340	1340	1340
Power
Military	(HP)						600	600
War Emergency	(HP)
Normal	(HP)			440	400	450	550	550	550
Take Off	(HP)	175	132	440	400	450	600	600	600
Eng Dims
Length	(ft)	4.43			3.54	3.53	3.58	3.58	4.00
Width/Dia	(ft)	1.83			3.75	3.81	4.29	4.29	4.33
Height	(ft)	2.79
Base Engine Wt	(lb)	376			695	665	854	854	865
Propeller
# Blades		2	2	2	2	2	2	2	2
Dia	(ft)	7.17	7.58	8.5	8	9	9.08	9.00	9
Manufacturer								Hamilton Std	Hamilton Std
Type		Fixed Pitch			Two-Speed	Two-Speed	Two-Speed	Const Spd	Const Spd
Wing
Span	(ft)							42.60	42.02
Root Thickness	(%)
	(in)
Total Area	(sq ft)	200	124	220	248	239	225	258.1	253.73
Wing (less Ail & Flaps)	(sq ft)							218.18	213.47
Ailerons	(sq ft)							11.4	11.4
Flaps	(sq ft)							28.52	28.86
Tail Area	(sq ft)					71.7
V Tail Area	(sq ft)				19.03	18.62		18.54	18.54
Fin	(sq ft)							5.33	5.33
Rudder	(sq ft)							13.21	13.21
H Tail Area	(sq ft)				40.2	53.08		50.11	50.11
Stabilizer	(sq ft)							28.34	28.34
Elevator	(sq ft)							21.76	21.76
Total Control Surf Area	(sq ft)
Length
Overall	(ft)				28	27.8		28.99	28.99
Fuselage	(ft)	28	22.5	24.3	27.6	28.8	27.8	29
Body	(ft)				26.37	27.8		20.54	20.54
Body Depth	(ft)
Body Width	(ft)
Fuel Tank Volume	(gal)							178	110.4
Wing Tanks	(gal)
FuselageTanks	(gal)
Oil Tank Volume	(gal)							15.5	12.2
Water Inj Tank Vol	(gal)
Wetted Area (sqf)	(sq ft)
Pwr Ldng	(lb/HP)	13.77	13.90	9.37	11.11	9.36	8.70	8.69	8.78
Wing Ldng	(lb/sq ft)	12.05	14.80	18.75	17.91	17.62	23.20	20.19	20.75
Struct. Des. GW	(lb)	2450	1825					5246	5280
Ultimate Load Factor	(G's)								8.5
Design Speed	(mph)	132		175	170	180	207	210	251
Not to Exceed Speed	(mph)

Parametric plots of the above data can be found at this link.

Notes: This website has been developed with a number of low cost or free programs including Hot Metal Pro, KompoZer, MicroSoft Designer and Da Button Factory.com

Rev 2-21-25

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