01-561-7717
Structural Component Air Support
01-561-7721
Structural Component Air Support
01-561-7729
Structural Component Air Support
44.000" overall length 6.000" overall width 0.040" material thickness closure member dim. are stock material
01-561-7737
Airfoil Rib
Used on f-16 acft. rib -12 opp B24
01-561-7758
Structural Component Air Bracket
2.400" overall length 1.600" overall width 0.063" material thickness bracket ams qq-a-250/5; opposite -25; 2024-0 bare al sh or 2024-0 clad al sh; dim. are stocksize matl.
01-561-7766
Structural Component Air Bracket
Used on f-15 a-e acft. 2.900" overall length 1.300" overall width 0.063" material thickness bracket 2024-0 bare al sh or 2024-0 clad al sh; -10 opposite; lh bracket; dim. are stocksize matl; or qq-a-250/5
01-561-7806
Aircraft Fairing
Used on ch47 chinook. curtain assembly fwd crown of the aft pylong, fairing assembly
01-561-7807
Aircraft Latch Assembly
Used on ch47 chinook. race; cargo door trolley, wheel assy
01-561-7809
Structural Component Air Fitting
Used on ch47 chinook. fitting assembly fuel tank vent
01-561-7810
Structural Component Air Fitting
Used on ch47 chinook. fitting assembly fuel tank vent
01-561-7871
Structural Component Air Support
01-561-7872
Aircraft Latch Assembly
01-561-7928
Structural Component Air Bracket
Used on f-15 a-e acft. 2.900" overall length 1.300" overall width 0.063" material thickness bracket opposite -9 per p/l; 0 bare al sh or clad al sh; or qq-a-250/5; dim. are stocksize matl.
01-561-7965
Aircraft Fairing
Used on f-15 a-e acft. 26.000" overall length 2.500" overall width 0.050" material thickness fairing lh 2024-0 bare al sh or 2024-0 clad al sh; or ams qq-a-250/5; dim. are stocksize matl; -8 opposite
01-561-8022
Structural Component Air Bracket
Used on f-15 a-e acft. 6.000" overall length 2.500" overall width 0.050" material thickness bracket lh qq-a-250/5; dim. are stocksize matl; 2024-0 bare al sh or 2024-0 clad al sh; lh
01-561-8080
Structural Component Air Bracket
3.000" overall length 2.100" overall width 0.125" material thickness angle dim. are stock material
01-561-8084
Structural Component Air Bracket
Angle
01-561-8091
Aircraft Leading Edge
01-561-8104
Structural Component Air Bracket
Used on f-15 a-e acft. 1.900" overall length 1.900" overall width 0.063" material thickness bracket lh dim. are stocksize matl; lh, ams qq-a-250/5; 2024-0 bare al sh or 2024-0 clad al sh; opposite -20
01-561-8149
Structural Component Air Bracket
Used on f-15 a-e acft. 2.100" overall length 1.600" overall width 0.063" material thickness bracket lh 2024-0 bar al sh or 2024-0 clad al sh; qq-a-250/5 also; dim. are stocksize matl; opposite -14
01-561-8204
Structural Component Air Support
01-561-8271
Tubing Aircraft Support
Used on ch47 chinook. support, hydraulic tube
01-561-8344
Aircraft Fairing
Low observable
01-561-8467
Access Aircraft Cover
Used on ea-18g (f/a-18g) electronic attack ftr gse. (navy) cover assembly, airc
01-561-8507
Access Aircraft Door
A door designed to provide access for inspection
01-561-8509
Access Aircraft Door
A door designed to provide access for inspection
01-561-8576
Structural Component Air Bracket
Used on f-15 a-e acft. 1.700" overall length 1.700" overall width 0.063" material thickness bracket lh 2024-0 bare al sh or 2024-0 clad al sh; qq-a-250/5; dim. are stocksize; opposite -22
01-561-8608
Structural Component Air Bracket
1.440" overall length 0.750" overall width clip includes MS21060-08k nut
01-561-8613
Structural Component Air Bracket
1.810" overall length 1.360" overall width 0.063" material thickness anodize surface treated
01-561-8754
Structural Component Air Support
Used on c-5 acft. 8.000" overall length 2.000" overall width 0.025" material thickness angle annealed 321; no heat treat; dim. are stocksize matl; used on 102b; nha 4P50006
01-561-8928
Aircraft Fairing
Used on f-22 raptor acft. nozzle fairing right; carbon/bmi composite construction w/titanium supports
01-561-8970
Aircraft Stiffener
13.500" overall length 2.200" overall width 0.051" material thickness dim. are stock material
01-561-8973
Aircraft Stiffener
11.500" overall length 2.200" overall width 0.051" material thickness dim. are stock material
01-561-8978
Aircraft Stiffener
7.300" overall length 1.500" overall width 0.051" material thickness dim. are stock material
01-561-8983
Aircraft Channel
9.200" overall length 3.300" overall width 0.063" material thickness dim. are stock material
01-561-8988
Structural Component Aircraf Web
01-561-9116
Aircraft Stiffener
01-561-9118
Radome
Used on ec-135t2. 3.000" overall length 2.000" overall width 3 x 2 x 2 feet. plastic painted cover for radom
01-561-9119
Radome
Used on ec-135t2. 3.000" overall length 2.000" overall width 3 x 2 x 2 feet. plastic painted cover for radom
01-561-9195
Aircraft Window Panel
Window panel, aircraft
01-561-9421
Cowling
Used on interframe adapter. 14.500" overall length 12.000" overall width (navy) ifaa cowling cushion assembly engine cowling is a double angle bracket, made of steel having a foam cushion adhesively attached; bracket has two mounting holes at the top portion
01-561-9434
Aircraft Fairing
Used on a-10 acft. 26.000" overall length 9.000" overall width 0.071" material thickness fairing assy alcd sh; heat treat 0; dim. are stocksize matl; opposite -28; used on 160D611108-11
01-561-9448
Cowling
Used on interframe adapter. 14.500" overall length 12.000" overall width navy) ifaa cowling cushion assembly engine cowl is a double angle bracket, made of steel with a foam cushion adhesively attached; bracket has two mounting holes in the upper portion
01-561-9463
Structural Component Air Bracket
Used on f-16 acft. 8.000" overall length 7.000" overall width 0.080" material thickness bracket assy c/o 1 bracket, 2 cover, rivets (ar) , adhesive (ar) , nuts, grommet (ar) ; fnsh A578; dim. are stocksize matl.
01-561-9480
Aircraft Leading Edge
Used on a-10 acft. le assy mid outbd opposite -21; used on 160D513101-18
01-561-9485
Structural Component Air Support
Used on interframe adapter. 53.170" overall length 9.940" overall width (navy) ifaa gearbox support assembly consists of 3 support sub weldments, 1 block, 1 slide key, 4 capscrews, 4 locknuts, 8 flat washers, 4 hex head bolts, r flange lock nuts,
01-561-9489
Structural Component Air Support
Used on interframe adapter. 50.457" overall length 3.890" overall width (navy) ifaa forward cross member consists of 3 channels, 1 boss, 1 plate, 1 hex head bolt, 2 inserts,
01-561-9761
Structural Component Air Support
Used on kc-135 acft. 28.700" overall length chord alter bac 1506-1058; dim. are stocksize matl; T6 extru; T6 temp; fnsh srf-2.30; used on 5-94410-3000
01-561-9767
Aircraft Intercostal
7.000" overall length 4.000" overall width 0.050" material thickness dim. are stock material
