01-217-7915
Structural Aircraft Plate
Used on c-5 aircraft. matl 7075-0 per qq-a-250/12; heat treat T6; matl size .250X11.9X9.0; part of -105c & -105d bulkhead assembly-aft ramp station 158.68
01-217-7916
Structural Aircraft Plate
Material per P141-0550
01-217-7917
Structural Aircraft Plate
Material per P141-1600
01-217-7918
Structural Aircraft Plate
Material per P141-1600
01-217-7919
Structural Aircraft Plate
Material per P141-2400
01-217-7920
Aircraft Fairing
Used on T-37. 14.000" overall length 5.000" overall width 0.032" material thickness nha 4012335; opposite -6
01-217-7921
Structural Component Air Support
01-217-7922
Structural Component Air Support
Used on f-5e aircraft. fitting-attach, fwd, cant fus sta. 505.075, nacelle upr longeron, rh
01-217-7923
Structural Component Air Support
Used on f-5e aircraft. fitting-attach, fwd, cant fus sta. 505.075, nacelle upr longeron, lh
01-217-7926
Structural Component Air Support
Used on f-15 acft. aluminum alloy 7075-T7351; supports main landing gear twist link
01-217-7927
Structural Component Air Support
Used on f-15 acft. aluminum alloy 7075-T7351; supports main landing gear twist link
01-217-7928
Structural Component Air Support
01-217-7934
Airfoil Rib
Used on F-15.
01-217-7935
Airfoil Rib
Used on f-15 acft.
01-217-7936
Airfoil Rib
Used on F-15.
01-217-7937
Airfoil Rib
Used on F-15.
01-217-7943
Aircraft Skin
165.000" overall length 65.000" overall width
01-217-9376
Structural Aircraft Plate
Used on acft model f-16c/d usaf. matl qq-a-250/4-T81; finish A442; 36.00 in.long, 1.00 in.wide, 0.090 in.thick; nha 16B4705-1; eff 5c 0001 9999
01-217-9406
Aircraft Skin
Nha 16B6320-1; eff 5c 0001 9999; superseded p/n 16B6320-7 ow per ecn OF871
01-218-0162
Structural Aircraft Plate
01-218-0163
Structural Aircraft Plate
01-218-0164
Structural Component Air Support
01-218-0166
Structural Component Air Support
Used on acft model f-16c/d usaf. nha 16P194-813; eff 5c 0001 9999
01-218-0167
Structural Component Air Support
Used on acft model b-52g/h. opposite p/n -515; nha 35-35470
01-218-0179
Structural Aircraft Panel
01-218-0198
Former
Used on 1560-00-074-3201 and 1560-00-874-7338. 6.797" overall length 4.500" overall width 0.040" material thickness rectangular shape; w/flanges
01-218-0207
Aircraft Skin
14.000" overall length 6.000" overall width outbd lwr fuselage skin
01-218-0495
Structural Aircraft Plate
01-218-0496
Structural Aircraft Plate
01-218-0497
Structural Aircraft Plate
01-218-0503
Airfoil Rib
Used on F-15.
01-218-1000
Aircraft Channel
Used on SH-60B.
01-218-1586
Aircraft Fairing
Used on f-18 aircraft.
01-218-1587
Aircraft Fairing
Used on f-18 aircraft.
01-218-1816
Access Aircraft Door
Used on acft model b-1b. consists of 4 washer, 1 spacer, 1 roller, 2 base, 2 fitting, 4 bushing, 4 shim, 1 pad, 1 door assy, misc hardware; nha L3400302
01-218-1954
Former
Used on 1560-00-074-3201 and 1560-00-874-7338. 5.297" overall length 4.297" overall width 0.040" material thickness rectuangular shape; w/flanges
01-218-2373
Access Aircraft Door
01-218-2662
Structural Aircraft Plate
Material per P141-2400
01-218-2663
Structural Aircraft Plate
5.760" overall length 5.200" overall width 0.140" material thickness splice rudder
01-218-2667
Structural Component Air Support
01-218-2683
Structural Aircraft Panel
Used on acft model b-52g/h. c/o 11 doublers, 1 skin, 6 stiffeners; located w.s. 1303, w.bl. 1071; opposite p/n -501; nha 35-1900
01-218-2709
Aircraft Skin
Used on acft model b-52g/h. plastic-glass fabric reinforced per D3-1300, type ii; finish f-6.10; opposite p/n -10; nha 25-3129-507, -509
01-218-2710
Aircraft Skin
Used on acft model b-52g/h. plastic-glass fabric reinforced per D3-1300, type ii; finish f-6.10; opposite p/n -9; nha 25-3129-508, -510
