NA-16/BT-9/NJ-1 Harvard I/NA-57/Sk 14 | |
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![]() NA-16-2A/NA-42 "FAH-21" displayed outside at the Honduras Air Museum at Toncontín | |
General information | |
Type | Trainer |
Manufacturer | North American Aviation |
Status | retired |
Primary users | United States Army Air Corps |
Number built | 1,935 |
History | |
Manufactured | 1935 to 1939 |
First flight | 1 April 1935 |
Variants | North American BT-9 CAC Wirraway I.Ae. 21 DL |
Developed into | North American T-6 Texan North American P-64 |
The North American Aviation NA-16 is the first trainer aircraft built by North American Aviation, and was the beginning of a line of closely related North American trainer aircraft that would eventually number more than 17,000 examples, notably the T-6 Texan family.
On 10 December 1934, James Howard "Dutch" Kindelberger, John L. "Lee" Atwood, and H.R. Raynor sketched out the specifications for the NA-16. A key characteristic for the advanced trainer was a closed canopy. [1]
The NA-16 is a family of related single-engine, low-wing monoplanes with tandem seating. [2] Variants could have an open cockpit (the prototype and the NA-22) or be under a glass greenhouse that covered both cockpits. [3] On some variants, the rear of the canopy could be opened for a gunner to fire to the rear. [4] A variety of air-cooled radial engines, including the Wright Whirlwind, Pratt & Whitney Wasp and Pratt & Whitney Wasp Junior of varying horsepowers, could be installed depending on customer preferences. [5] The fuselage was built up from steel tubes and normally fabric covered; however, later versions were provided with aluminum monocoque structures. [6]
During the development of the design, a six-inch stretch was made by moving the rudder post aft. [7] Many versions had a fixed landing gear, but later versions could have retractable gear, mounted in a widened wing center section (which could have either integral fuel tanks or not). [8] Most had a straight trailing edge on the outer wing while again, some had the wing trailing edge swept forward slightly in an attempt to fix a problem with stalls and spins. [9] Several different rudders were used, with early examples having a round outline, intermediate examples having a square bottom on the rudder (Harvard I) and late examples using the triangular rudder of the AT-6 series, due to a loss of control at high angles of attack with the early types. [10] Horizontal and vertical tails were initially covered in corrugated aluminum, but later examples were smooth-skinned, and the horizontal stabilizer was increased in chord near its tips on later versions. [11]
The NA-16 flew for the first time on 1 April 1935, by Eddie Allen. An enclosed cockpit version of the NA-16 was submitted to the United States Army Air Corps for performance tests as a basic trainer on 27 May 1935. [12] The Army accepted the trainer for production but with some detail changes, including a larger engine and faired landing gear modifications. The modified NA-16 was redesignated by North American as the NA-18, with production examples entering Air Corps service as the North American BT-9 (NA-19). The U.S. Army Air Corps ordered 42 BT-9s, equipped with the Wright R-975 Whirlwind engine, and 40 BT-9As, which could be armed with .30 cal. Browning M-1 machine guns. In 1936, an order was placed for 117 BT-9Bs, without armament. A total of 67 BT-9Cs (NA-29) were built, using the same R-975-7 engine. [1] : 20–21, 29–31, 33, 36, 214 Similar aircraft continued to be sold outside the U.S. under the NA-16 designation. [13]
By the time of the U.S. entry into WWII, the NAF had built 1631 N-16 series aircraft. Of that total, 1043 were for foreign countries, while the remainder were for the U.S. Army Air Corps and Navy. [1] : 73
The Commonwealth Aircraft Corporation produced 755 units of a modified version of the NA-16-2K (NA-33) known there as the Wirraway between 1939 and 1946. [14] The units built included 40 CA-1s (Wirraway I), 60 CA-3s, 32 CA-5s, 100 CA-7s, 200 CA-8s, 188 CA-9s, and 135 CA-16s. The CA-16s were called the Wirraway IIIs, while previous models were called Wirraway IIs. [1] : 53–56
Experience with the NA-16-4P and deteriorating political relations with the US led to the local development of the I.Ae. D.L. 21, which shared the NA-16 fuselage structure; however it proved too difficult to produce. As a result of this, an entirely new design (the I.Ae. D.L. 22) was built instead; it had similar configuration, but was structurally different and optimized to available materials. [15]
The NA-16-4RW and NA-16-4R inspired the development of the Kyushu K10W when the Imperial Japanese Navy instructed Kyushu to develop something similar. [16] The resulting aircraft owed little to the NA-16, however Allied Intelligence saw so few examples that the error was not corrected and some drawings show a modified NA-16. [16]
This section needs additional citations for verification .(April 2014) |
Listing includes aircraft built specifically under NA-16 designation for export, and similar aircraft built for use by the United States armed forces.
When the North American NA-16 was first conceived, five different roles were intended for the design, designated NA-16-1 thru NA-16-5: [17]
This section needs additional citations for verification .(April 2014) |
General characteristics
Performance
Related development
Aircraft of comparable role, configuration, and era
Related lists
Media related to North American NA-16 at Wikimedia Commons