Ov-10a Aircraft Support Equipment Parts

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Part Number
NSN
NIIN
0-001-366-010 Engine Starter Motor
012151733
0-10106 Float Carburetor
000803454
0-10149 Float Carburetor
000803454
0-11193 Float Carburetor
003584516
0-12236 Float Carburetor
000803454
0-12290 Float Carburetor
006839806
0-12354 Float Carburetor
006839806
0-12522 Float Carburetor
000803454
0-12613 Float Carburetor
000803454
0-12658 Float Carburetor
000803454
0-13309 Float Carburetor
002370528
0-307 Ammeter
004586371
000117-1064 Spark Plug
002317256
00323-0339 Electrical Fuel Pump
008479250
00625379 Quick Disconnect Coupling Half
003694593
0095056 Fluid Filter Element
004603222
01-P14803C01 Power Supply Test Set
011075055
010-0161-00 Test Probe-lead Assembly
004386777
010-161 Test Probe-lead Assembly
004386777
0109-0057 Ammeter
000661278
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Support Equipment, Ov-10a Aircraft

Picture of Ov-10a Aircraft Support Equipment

The North American Rockwell OV-10 Bronco is an American turboprop light attack and observation aircraft. It was developed in the 1960s as a special aircraft for counter-insurgency (COIN) combat, and one of its primary missions was as a forward air control (FAC) aircraft. It can carry up to three tons of external munitions, internal loads such as paratroopers or stretchers, and can loiter for three or more hours.

The aircraft was initially conceived in the early 1960s through an informal collaboration between WH Beckett and Colonel KP Rice, U.S. Marine Corps, who met at Naval Air Weapons Station China Lake, California, and who also happened to live near each other. The original concept was for a rugged, simple, close air support aircraft integrated with forward ground operations. At the time, the U.S. Army was still experimenting with armed helicopters, and the U.S. Air Force was not interested in close air support.

The concept aircraft was to operate from expedient forward air bases using roads as runways. Speed was to be from very slow to medium subsonic, with much longer loiter times than a pure jet. Efficient turboprop engines would give better performance than piston engines. Weapons were to be mounted on the centerline to get efficient unranged aiming like the Lockheed P-38 Lightning and North American F-86 Sabre aircraft. The inventors favored strafing weapons such as self-loading recoilless rifles, which could deliver aimed explosive shells with less recoil than cannons, and a lower per-round weight than rockets. The airframe was to be designed to avoid the back blast.

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