Miscellaneous Aircraft Accessories And Components FSG 16 — FSC 1680

NSN
NIIN
Name
Details
01-521-4414
Indicator Panel
Used on breguet 1150 atlantic maritime patrol aircraft.
01-521-5122
Rigid Foam Insulation-ballistic
01-521-5125
Rigid Foam Insulation-ballistic
01-521-5131
Rigid Foam Insulation-ballistic
01-521-5192
Webbing Strap
Used on mv-22 tilt rotor aircraft. (navy) lanyard, aircraft, ma belly skin rhs/lhs sta 187 to sta 202 access pannel assy interim support items list (isil) per (77272) 901-031-193; made from 0.090 max thickness x 0.50 inch wide x 12" long plus or minus 0.12 inch tubular webbing per mil-w-5625, natural color nylon material
01-521-5205
Gasket And Seal Set
Used on kc-130j aircraft engines. (navy) seal, aircraft material
01-521-5211
Gasket And Seal Set
Used on kc-130j aircraft engines. (navy) seal, aircraft material
01-521-5610
Aircraft Control Panel
Used on astor airborne radar.
01-521-5611
Aircraft Control Panel
Used on astor airborne radar.
01-521-5612
Aircraft Control Panel
Used on astor airborne radar.
01-521-5613
Aircraft Control Panel
Used on astor airborne radar.
01-521-6272
Control Electrical-electro Panel
01-521-6595
Control Panel Aircraft Chassis
Chassis assy, electrical equipt
01-521-7158
Control Electrical-electro Panel
Used on c-130j hercules aircraft. panel assembly, electrical control
01-521-7159
Control Electrical-electro Panel
Used on c-130j hercules aircraft. panel, edge lighted, electrical control
01-521-7225
Control Panel Aircraft Chassis
Chassis assy, electrical equipt
01-521-7840
Air Conditioning-heating Adapter
Used on fwd fuselagf. 8.680" overall length 9.850" overall width adapter assy - plenum nose wheel well
01-521-7854
Aircraft Control Panel
Used on c130j hercules aircraft. panel assembly, propeller control
01-521-8393
Compartment Division Curtain
01-521-8474
Control Electrical-electro Panel
Used on c-17 acft. panel assy, built in test c/o 1ea cca-bit panel, p/n 195D1469G1; 1ea pad card 768-702019-21; 1ea pad card, p/n 768-702019-16; 1ea front panel, p/n 780-301001-2; 1ea jumper, p/n 4990097-1; 4ea switches, p/n 5090012-1; 1ea ptd wrg bd, p/n 780-704005-2; misc hardware
01-521-8480
Mechanical Aircraft Actuator
Used on c-17 acft. control assy-aeileron load feel, fwd fus
01-521-8533
Interior Lining Aircraft Panel
01-521-8542
Seat Frame Aircraft Cover
01-521-8545
Seat Frame Aircraft Cover
01-521-8555
Seat Frame Aircraft Cover
01-521-8569
Aircraft Compon Modification Kit
01-521-8598
Interior Lining Aircraft Panel
01-521-8823
Mechanical Aircraft Actuator
01-521-8824
Mechanical Aircraft Actuator
01-521-8825
Aircraft Gearbox Assembly
01-521-8826
Mechanical Aircraft Actuator
01-521-8827
Aircraft Gearbox Assembly
01-521-8828
Aircraft Gearbox Assembly
01-521-8829
Aircraft Gearbox Assembly
01-521-8830
Aircraft Gearbox Assembly
01-521-8831
Aircraft Gearbox Assembly
01-521-8832
Mechanical Aircraft Actuator
01-521-8833
Mechanical Aircraft Actuator
01-521-9104
Bell Crank
Used on c-130j hercules aircraft. 0.6250" bore diameter used on left side ramp lock mechanism - actuating; from center of fulcrum bore to center of hole first arm is 6.500" ; from center of fulcrum bore to center of hole second arm is 6.000"
01-521-9107
Bell Crank
Used on c-130j hercules aircraft. 0.6250" bore diameter used on right side ramp lock mechanism - actuating; from center of fulcrum bore to center of hole first arm is 6.500" ; from center of fulcrum bore to center of hole second arm is 6.000"
01-521-9375
Bell Crank
Used on c-130j hercules aircraft. 0.6250" bore diameter efor right side ramp hook mechanism; from center of fulcrum bore to center of hole first arm is 4.000" ; from center of fulcrum bore to center of hole second arm is 6.000"
01-521-9377
Bell Crank
Used on c-130j hercules aircraft. 0.6250" bore diameter efor right side ramp hook mechanism; from center of fulcrum bore to center of hole first arm is 3.680" ; from center of fulcrum bore to center of hole second arm is 6.000"
01-521-9379
Bell Crank
Used on c-130j hercules aircraft. 0.6250" bore diameter dfor left side ramp hook mechanism; from center of fulcrum bore to center of hole first arm is 4.000" ; from center of fulcrum bore to center of hole second arm is 6.000"
01-521-9380
Bell Crank
Used on c-130j hercules aircraft. 0.6250" bore diameter dfor left side ramp hook mechanism; from center of fulcrum bore to center of hole first arm is 3.680" ; from center of fulcrum bore to center of hole second arm is 6.000"
01-521-9381
Fire Aircraft Extinguisher
19.910" overall length 5.950" overall width fire ext assy hfc-227 drawing number 10659065, general dynamics
01-521-9603
Aircraft Seat Track
01-521-9648
Mechanical Aircraft Actuator
01-521-9649
Mechanical Aircraft Actuator
01-521-9650
Mechanical Aircraft Actuator
01-521-9651
Mechanical Aircraft Actuator
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