Originally with open
tandem cockpits, the NA-16 was of metal construction with a
fabric-covered fuselage, and was provided with fixed tailwheel type
landing gear. Powered by an non-cowled 400 hp (298 kW) Wright R-975
Whirlwind engine, the prototype was first flown on 1 April 1935 in
Dundalk, Maryland by test pilot Eddie Allen. After evaluation at Wright
Field, was selected for production for training under the designation
BT-9, albeit with some modifications which were to include enclosed
cockpits.
Although the prototype,
as the NA-18, was so modified and fitted with a 550 hp (410 kW ) Pratt
& Whitney R-1340-41 Wasp air-cooled 9-cylinder radial engine, the 400
hp (298 kW) Wright R-975 Whirlwind 9-cylinder radial engine was
retained for the production BT-9. The first of 42 BT-9s produced was
flown at Inglewood, Los Angeles (North American's new factory) in April
1936. Forty BT-9As, with one fixed forward-firing gun, and another on a
flexible mounting in the rear cockpit, were then built for the USAAC
Reserve, followed by 117 BT-9Bs with detail improvements, and the
series ended with 67 similarly armed BT-9Cs with only equipment
changes. The first of the BT-9Cs was, in fact, completed as the sole
Y1BT-10, with a 550 hp (410 kW) Pratt & Whitney R-1340-41 radial
engine, and another single aircraft was designated BT-9D to signify a
change, namely the substitution of the more angular outer wing panels
and rudder which had, by then, been developed for the BC-1A.
The US Navy received 40
aircraft designated NJ-1, which were basically BT-9s with the 550 hp
(410 kW) Pratt & Whitney R-1340-41 Wasp 9-cylinder engine instead of
the 400 hp (298 kW) Wright R-975 Whirlwind radial engine.
The single BT-9D
prototype led to the improved BT-14 which introduced a metal-covered
fuselage and a 450 hp (336 kW) R-985-25 Wasp Junior engine and
production of these for the USAAC totalled 251, of which 27 were later
in 1941, fitted with an 400 hp (298 kW) R-985-11 engine and
redesignated BT-14A.
Flight Training:
On the Eve of World War II
During the 1930s Depression the
number of pilots the Air Corps trained decreased until 1937 only 184
graduated from advanced pilot training. Facing a resurgent German
militarism and an aggressive Japanese military in 1939, the Air Corps
planned to graduate 4,500 pilots in the following two years. Lacking
facilities to train such a large number of cadets, in mid-1939 the Air
Corps contracted with nine of the best civilian flying schools to begin
training pilots. When France fell to Germany in 1940 the Air Corps
increased the number of pilots to be trained to 7,000 per year. By
December 1941 the Air Corps had contracted with 45 civilian flying
schools and by 1943 the number increased to 63. In the first class at
Randolph Field in 1939 only 257 pilots graduated. By the end of 1941
over 2,000 were enrolled in each class. At the end of World War II the
Army Air Forces Training Command had graduated 250,000 pilots from its
schools.
Training Fields
Before World War II
During the 1930s the Army Air
Corps conducted primary and basic flying training at Randolph and
Brooks Fields, and advanced training at Kelly Field. These fields were
just outside of San Antonio, Texas. In 1940 the Army Air Corps planned
the expansion of pilot training and began offering basic flight
instruction at additional fields. By 1944 there were 31 fields involved
in basic training. Advanced training was originally given at Kelly and
Brooks Fields; however, when the program expanded and was divided into
single- and twin-engine instruction, other fields began to offer
advanced instruction. Soon after, Brooks and Kelly Fields conducted
only twin-engine training. Eventually, single- and twin-engine training
fields spread across the country from coast to coast.
BT-9B SPECIFICATIONS
Span: 42 ft.
Length: 28 ft.
Height: 13 ft. 7 in.
Weight: 4,470 lbs. loaded
Armament: None
Engine: Wright R-975-53 of 400 hp.
Crew: Two - Instructor pilot and Student pilot
Cost: $20,000
PERFORMANCE
Maximum speed: 170 mph / 148 knots
Cruising speed: 146 mph / 127 knots
Range: 877 statute miles / 762 nautical miles
Service Ceiling: 19,750 ft.