Aircraft Miscellaneous Engine Accessories FSG 29 — FSC 2995

NSN
NIIN
Name
Details
01-410-9176
Oil Pump Assembly Engine Housing
01-411-2238
Fluid Aircraft Manifold
Used on pacer dawn.
01-411-2239
Fluid Aircraft Manifold
Used on pacer dawn.
01-411-5022
Metallic Particle Detector
01-411-6014
Dirt And Liquid Deflector
Used on harpoon guide missile simulator for walrus class model 105 mod 0/1.
01-413-2163
Engine Air Turbine Starter
Used on ah-64a helicopter.
01-413-6191
Dirt And Liquid Deflector
01-414-0576
Supervisory Turbine Control Unit
01-414-3359
Supervisory Turbine Control Unit
Used on pacer dawn. 16.000" overall length 5.050" overall width
01-414-4877
Fluid Aircraft Manifold
01-414-6257
Supervisory Turbine Control Unit
Used on pacer dawn. 12.210" overall length 11.890" overall width
01-416-4089
Metallic Particle Detector
01-416-5190
Supervisory Turbine Control Unit
Used on f110ge129 acft engine. 15.970" overall length 12.800" overall width
01-417-0049
Engine Air Turbine Starter
Used on aircraft model f-14.
01-417-2170
Engine Oil Pump Assembly
Used on aircraft model s-3.
01-418-3248
Supervisory Turbine Control Unit
Used on support of pre-provisioning itemswhich aso acts as point of entry.
01-418-4143
Fluid Aircraft Manifold
Used on f100-pw-100/200 aircraft gas turbine engine. manifold, fuel supply, right, assembly of
01-418-4144
Fluid Aircraft Manifold
Used on aircraft, model f-16. manifold-fuel supply, left, assembly of
01-418-8148
Engine Oil Pump Assembly
01-419-0325
Metallic Particle Detector
Used on coast guard hh65a helicopter engine. right-hand 0.360" thread length 2.330" overall length 28 thread quantity per inch there is a light blue rubber o-ring .431" in diameter. it i s .530" from the end of the detector. this detector snaps into the lts/101 engine. unjf thread series
01-419-5062
Valve Cap
01-419-5063
Valve Cap
01-419-9695
Fluid Aircraft Manifold
Used on pacer dawn.
01-420-1752
Engine Oil Pump Assembly
Used on pacer dawn.
01-420-4405
Engine Oil Pump Assembly
Used on turbo-prop engine, alliedsignal inc, model 46.
01-422-1561
Oil Pump Assembly Engine Housing
01-422-4568
Push-pull Control Assembly
01-422-7027
Electronic Eng Regulator-control
01-423-4040
Metallic Particle Detector
01-423-5580
Push-pull Control Assembly
Used on launching system, guided missle, ver mk48, 1440-01-255-2181.
01-425-3935
Engine Spark Ignition Starter
Used on reciprocating gasoline engine.
01-425-4066
Engine Oil Pump Assembly
Used on u/o f100-100,-200,-220,-220e,and -229 engines.
01-425-5348
Power Control Quadrant
Used on ah-64a.
01-426-2843
Heat Suppressor
Used on preprovisioning support navicp is poe.
01-426-2844
Heat Suppressor
Used on preprovisioning support navicp is poe.
01-426-3042
Power Control Quadrant
Used on ah-64a.
01-426-4378
Engine Oil Pump Assembly
01-428-9493
Regulator-control Engine Housing
Used on the tf33 p7a/p100a - exciter.
01-429-4399
Supervisory Turbine Control Unit
Used on u/o f110-100 acft engine. 12.800" overall length 16.710" overall width
01-430-4368
Engine Exhaust System Hanger
01-430-5539
Engine Oil Pump Assembly
Used on j69-t-25a engine. rotation clockwise, involute spline drive, 13 teeth, 32/64 diametral pitch, 30 deg. pressure angle; flow vs speed inlet pressure 25-30 ins hg abs discharge, pressure: 35 psi. oil: mil-l-780, temp:180 deg f, no entrained air.flow vs inlet pressure speed; 4694rpm; discharge pressure 35 psi; oil mil-l-7808; temp 180 deg. f, no entrained air
01-431-8359
Engine Air Turbine Starter
Used on t64 engine.
01-432-7762
Anti-icing Jet En Valve Assembly
Used on F/A18. indicator valve
01-433-4830
Metallic Particle Detector
Used on special support equipment.
01-434-2660
Valve Head
01-435-2788
Engine Oil Pump Assembly
Used on t63-a-700 and t63-a-720 (turbine engine), rotary wing aircraft.
01-435-3732
Supervisory Turbine Control Unit
Used on preprovisioning support navicp is poe.
01-437-0909
Metallic Particle Detector
Used on alf 502l-2c engine.
01-437-1127
Supervisory Turbine Control Unit
Used on f0110ge100 eng. 12.800" overall width
01-437-4584
Fluid Aircraft Manifold
Used on f404 engine.
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