01-534-8087
Exhaust Heat Shield
Used on F/A-22. heat shield
01-534-8159
Structural Aircraft Plate
Used on C-130. angle plate nha 02032389; heat treat T6, al sae ams
01-534-8329
Airfoil Rib
Used on harrier aircraft. next higher assembly 75A23001007
01-534-8331
Airfoil Rib
Used on harrier aircraft. next higher assembly 75A23001007
01-534-8363
Aircraft Skin
Used on p-3c orion aircraft.
01-534-8436
Structural Component Aircraf Web
Used on c130k hercules.
01-534-8448
Structural Aircraft Panel
01-534-8449
Structural Aircraft Panel
01-534-8453
Structural Aircraft Panel
01-534-8456
Aircraft Stiffener
01-534-8461
Access Aircraft Cover
01-534-8469
Bleed Air Duct Assembly
Used on p-3c orion aircraft. 47.500" overall length 0.040" material thickness
01-534-8566
Aircraft Pylon
Per e/o no. 2004C0083, nha 35-8273; same as 35-8201-506 after 520-182852-3 harness installation, u/o b-52h all; opposite -511
01-534-8576
Structural Aircraft Panel
Used on C-17A. 144.000" overall length 48.000" overall width 6aromatic polymide paper honeycombdms 1974, type 3, CLASS2, grade a, 1/8in. cell size, 8.0lb/cu ft or greater for type 1, type 2 is 4.0lb/cuft. unidirectional carbon fiber/phenolic resin laminate; t.o. 1c-17a-4-25, fig.124, ind 3/dwg 9D0207
01-534-8617
Aircraft Frame
01-534-8780
Structural Aircraft Panel
01-534-8861
Exhaust Heat Shield
Used on f/a-22 raptor. sidewalls - nozzle aircraft mounted
01-534-8864
Exhaust Heat Shield
Used on f/a-22 raptor. sidewalls - nozzle aircraft mounted
01-534-8871
Tubing Aircraft Support
Used on f/a-22 raptor.
01-534-8965
Structural Component Air Support
Used on B-52. 0.025" material thickness airplane serial number 60-001
01-534-8976
Structural Component Air Support
15.500" overall length support assy matl steel type 321 or 347 mil-s-6721 annealed; p/n 35-10725 consist of 1-3 lwr flange, 1 -2 upper flange, 1-1 duct
01-534-9003
Aircraft Channel
Used on jet engine test facility. 108.000" overall length 1.624" overall width 0.125" material thickness channel, overhead cable support, cva engine stest facility chromate zinc surface treated
01-534-9262
Explosion Suppressa Foam Segment
Used on filler for f-16.
01-534-9266
Explosion Suppressa Foam Segment
Used on filler for f-16.
01-534-9267
Explosion Suppressa Foam Segment
Used on filler for f-16.
01-534-9268
Explosion Suppressa Foam Segment
Used on filler for f-16.
01-534-9269
Explosion Suppressa Foam Segment
Used on filler for f-16.
01-534-9272
Structural Component Air Fitting
01-534-9279
Aircraft Windshield Panel
01-534-9298
Aircraft Door
01-534-9427
Door Aircraft Hinge
01-534-9428
Structural Aircraft Plate
Used on F-16.
01-534-9429
Vertical Stabilizer
Used on F-16.
01-534-9430
Vertical Stabilizer
Used on F-16.
01-534-9431
Vertical Stabilizer
Used on F-16.
01-534-9433
Vertical Stabilizer
Used on F-16.
01-534-9434
Vertical Stabilizer
Used on F-16.
01-534-9435
Structural Aircraft Panel
Used on F-16.
01-534-9436
Structural Aircraft Panel
Used on F-16.
01-534-9437
Structural Aircraft Panel
Used on F-16.
01-534-9474
Structural Component Air Fitting
For diesel engine components
01-534-9479
Structural Component Air Fitting
For diesel engine components
01-534-9509
Structural Aircraft Panel
Used on p-3 orion, aircraft.
01-534-9510
Aircraft Fireseal
Used on p-3 orion, aircraft. seal
01-534-9674
Aircraft Skin
01-534-9678
Structural Component Air Bracket
0.071" material thickness
01-534-9725
Airfoil Rib
8.100" overall length 4.900" overall width 0.040" material thickness rib NHA65-48584, matl sheet clad 2024-0, qq-a-362; heat treat to T42 per bac 5602; -2 opp; -1 includes 1 -3 rib
01-534-9726
Airfoil Rib
9.400" overall length 5.500" overall width 0.051" material thickness rib matl AL7075-0 clad sheet, qq-a-2370 temper; -2 opp; -1 includes -7 rib, -5 splice plate, -6 splice plate, 90-2200-2nose rib; dim are stock matl
01-534-9727
Airfoil Rib
9.300" overall length 5.400" overall width 0.025" material thickness rib matl AL7075-0 clad sht, qq-a-287 0temper; -2 opp; -1 includes 1 -3 rib, 1 90-1599-2 nose rib; dim are stock matl
01-534-9998
Trim Aircraft Tab
