01-215-0927
Aircraft Skin
Used on aircraft model av-8. aluminum alloy
01-215-0928
Aircraft Stringer
Used on acft model av-8.
01-215-0986
Bell Crank
0.257" bore diameter
01-215-1689
Structural Component Air Support
Used on c-5 aircraft. fitting-track support, ctr cargo door, fs 2657; matl 7075-T6 alum alloy per qq-a-367; opposite -104a; nha 4F41266
01-215-1690
Structural Component Air Bracket
01-215-1697
Structural Aircraft Panel
Used on f-5 aircraft. aft panel assembly; c/o: -9 panel (1) , washer (8) , stud assembly (4) ; part of -501 panel instl-interior trim lh, front cockpit
01-215-1706
Aircraft Former
8.250" overall length 5.700" overall width 0.032" material thickness former installation-nose
01-215-1715
Aircraft Skin
Used on acft model kc-135. al alloy clad sheet 2024-0 per qq-a-362; 0 temper; heat treated to cond. T4; 72.80 in. lg, 34.40 in. w, 0.040 in. thk; nha 5-95602
01-215-2287
Structural Aircraft Plate
01-215-2288
Structural Aircraft Plate
01-215-2291
Structural Component Air Support
01-215-2292
Structural Component Air Support
01-215-2293
Structural Component Air Support
01-215-2311
Aircraft Skin
01-215-2717
Aircraft Rudder
01-215-2718
Aircraft Fairing
01-215-2719
Structural Component Air Support
Used on c-5b aircraft. bracket-hinge, rear beam, wing box ail. sta 122.15, aileron; make from 4J53009-993a; opposite -104c; nha 4J50014
01-215-2720
Structural Component Air Bracket
Opp 103c; nha 4J50014
01-215-2721
Structural Component Air Bracket
Opposite -104e
01-215-2722
Structural Component Air Bracket
Opposite -103e
01-215-2723
Structural Component Air Support
Used on acft model c-5a. consists of 1 bracket, 2 nut; nha 4F73133
01-215-2724
Structural Component Air Support
Used on acft model c-5a. 7075-T651 per qq-a-250/12; heat treat T6; 4.00 long, 4.00 wide, 2.000 thick; nha 4F72218
01-215-2725
Structural Component Air Support
Used on acft model f-16. A356-T61 per mil-a-21180, class 1 or 2; nha 2-300-48150
01-215-2726
Structural Component Air Support
01-215-2735
Wing Aircraft Spoiler
Nuclear hardness critical item; nha L1600000; opposite -022
01-215-2736
Wing Aircraft Spoiler
Flight control surface end item; opposite -021
01-215-2737
Wing Aircraft Spoiler
Fnuclear hardness critical item; nha L1600000; opposite -021; c/o 3 fitting assy, 4 front spar, 2 rear spar, 4 lower skin, 1 shim, 1 horn, 2 closeout rib, 1 trailing edge, 4 rib, 1 sensor fitting, misc hardware
01-215-2738
Wing Aircraft Spoiler
Nuclear hardness critical item; nha L1600000; opposite -021
01-215-2745
Aircraft Former
01-215-2749
Aircraft Skin
01-215-3644
Structural Component Air Bracket
Opp -102d
01-215-3645
Structural Component Air Bracket
Opposite -101d
01-215-3646
Structural Component Air Support
Used on c-5b aircraft. bracket-hinge, rear beam, wing box, ail sta 272.953, aileron; make from 7075-T6 alum alloy per qq-a-367; opposite -102d
01-215-3647
Structural Component Air Bracket
Opposite -101d
01-215-3648
Structural Component Air Support
C/o 2 fitting, 2 bushing, misc hardware; opp -2; nha 35-34256
01-215-3649
Structural Component Air Support
C/o 2 fitting, 4 bushing, misc hardware; opp -1; nha 35-34256
01-215-3650
Structural Component Air Support
Used on acft model b-52. consists of 2 fitting, 2 bushing, misc hardware; opp p/n -1; nha 35-34256
01-215-3651
Structural Component Air Support
Used on acft model b-1b. consists of 1 support, 5 bearing, 2 bushing, 2 insert; nha L3400134
01-215-3660
Aircraft Former
51.000" overall length 24.000" overall width 3.000" material thickness stock size-3.00X24X51 in; material per fms 3002-T851; location-lower, fs 446.10; superceded -41, ni, per ecn 4H362; eff on-5c 0091, 0093-0117, 0129-0135, 0137-177, 0179, 0181, 0195-0201, 0203, 0205, 0207, 0219, 0221, 0223, 0225, 0183-0187, 0189, 0119, 0121, 0123, 0125-0127; nha-16B610- 5
01-215-3899
Structural Component Air Support
1.610" overall width
01-215-4529
Structural Component Air Support
Used on c-130 aircraft. matl 4340 steel; size 1.50X6.0X20.0; opposite -8; part of -5 top kit instl-mlg beam repair, fs 577; 4130 steel may be substituted for 4340
01-215-4530
Structural Component Air Support
Used on c-130 aircraft. matl 4340 steel; size 1.50X6.0X20.0; opposite -7; part of -6 top kit instl-mlg beam repair, fs 577; 4130 steel may be substituted for 4340
01-215-4936
Structural Aircraft Plate
Type/model designation:f-4e/gy/ steel comp 301 mil-s-5059, 1/2 h; matl 0.040 in. thk by 1.547 in. w by 2.625 in. lg; right appl; 2 mtg holes
01-215-4937
Structural Aircraft Plate
Used on 1560-00-113-0077. type/model designation:f-4e/gy/ steel comp 301 mil-s-5059, 1/2 h, matl 0.040 in. thk by 0.781 in. w by 1.156 in. lg, 2 slotted aperatures
01-215-4938
Structural Aircraft Plate
Used on 1560-00-113-0077. type/model designation:f-4e/gy/ steel comp 301 mil-s-5059, 1/2 h; matl 0.040 in. thk by 0.680 in. w by 1.400 in. lg; aperature centrally located
01-215-4939
Structural Component Air Support
Used on 1560-00-113-0077 and 1560-00-179-9187. type/model designation:f-4e/gy/ aluminum alloy 2024 qq-a-250/5, T0; matl 0.040 in. thk by 3.203 in. w by 10.797 in. lg; l cross section; right appl
01-215-4940
Structural Component Air Support
Used on mcdonnell p/n 53-42001-305 door assy. type/model designation:f-4e/gy/ aluminum alloy 7075 qq-a-250/13, to; matl 0.025 in. thk by 6.400 in. w by 14.500 in. lg; z cross section; right appl
01-215-4941
Structural Component Air Support
Used on mcdonnell p/n 53-42001-306 door assy. type/model designation:f-4e/gy/ aluminum alloy 7075 qq-a-250/13, to; matl 0.025 in. thk by 6.400 in. w by 14.500 in. lg; z cross section; left appl
01-215-4942
Structural Aircraft Panel
01-215-5461
Access Aircraft Door
Used on aircraft model f-14a.
