01-516-7723
Structural Aircraft Panel
01-516-7724
Exhaust Heat Shield
Used on ch47c helicopter cabin crown access tunnel. shield
01-516-7864
Structural Aircraft Plate
0.025" material thickness doubler
01-516-8035
Structural Aircraft Plate
3.400" overall length 2.000" overall width 0.500" material thickness block dims are stock material; u/o -31; nha 160D111000
01-516-8044
Structural Aircraft Plate
1.500" overall length 1.500" overall width block u/o -31; nha 160D111000
01-516-8045
Structural Aircraft Panel
Honeycomb core u/o -31; nha 160D111000
01-516-8046
Structural Aircraft Plate
5.500" overall length 1.900" overall width block u/o -31; nha 160D111000
01-516-8165
Aircraft Windshield Panel
Used on a109, ab206, ab212, and ab412 helicopters.
01-516-8217
Structural Aircraft Plate
Used on f-22 raptor. 7.000" overall length 5.000" overall width splice-hinge support, inlet bypass
01-516-8231
Structural Aircraft Plate
Used on f/a-22 raptor. 6.000" overall length 5.000" overall width splices-hinge support, inlet bypass
01-516-8232
Structural Aircraft Plate
Used on f-22 raptor. 4.440" overall length 6.710" overall width 2.110" material thickness splice-hinge support, inlet bypass
01-516-8234
Structural Aircraft Plate
Used on f/a-22 raptor. 6.000" overall length 5.000" overall width 2.500" material thickness splices-hinge support, inlet bypass
01-516-8235
Structural Aircraft Plate
Used on f-22 raptor. 7.000" overall length 5.000" overall width splice dim. are stock material, ti 6al-4v ann titanium, opposite -121
01-516-8236
Structural Aircraft Plate
Used on f-22 raptor. 6.200" overall length 4.310" overall width 2.220" material thickness splice-hinge support, inlet bypass
01-516-8240
Structural Component Air Support
19.380" overall length strut finish per mil-std-1516; strut assy consists of 2ea rivets univ hd MS20470AD4-15, 1 ea nut hex AN316-6, 1 ea bearing, rod end MS21152-1, 1ea bearing rod end MS21151-8, 1ea rod -05 matl al 7075-T73
01-516-8241
Structural Component Air Support
19.250" overall length strut finishper mil-std-1516; consists of 2ea rivets univ hd MS20470AD4-15, 1ea nut hex AN316-6, 1ea bearing rod end MS21152-1, 1ea bearing rod end MS21151-81 ea rod -07
01-516-8300
Structural Component Air Fitting
01-516-8387
Structural Component Air Support
22.500" overall length 2.000" overall width support next higher assy, L3050021; ST0170LB0052, al aly shape, alloy 2024-T3, shape AND10134-2006
01-516-8458
Aircraft Frame
Used on rotary wing aircraft, sikorsky.
01-516-8486
Aircraft Window Panel
Used on a109, ab206, ab212, and ab412 helicopters.
01-516-8487
Aircraft Window Panel
Used on a109, ab206, ab212, and ab412 helicopters.
01-516-8492
Aircraft Windshield Panel
Used on a109, ab206, ab212, and ab412 helicopters.
01-516-8500
Aircraft Stiffener
Used on a109, ab206, ab212, and ab412 helicopters.
01-516-8650
Aircraft Stiffener
Used on a109, ab206, ab212, and ab412 helicopters. used on fin assy of bht model 412
01-516-8657
Structural Component Air Support
Used on a109, ab206, ab212, and ab412 helicopters.
01-516-8744
Structural Component Aircr Patch
Material is weave style 51789 nylon 6.6 fiber with bismaleimade resin; cure temp 177 deg c +/- 5 deg (350 deg f +/- 5 deg) for 4 hours at 177 deg c (350 deg f) ; item shall be stored at or below -18 deg c (0 deg f) for six months after date of shipment, when stored at this temp item doesn't need retesting prior to 720 days from date of shipment
01-516-8762
Aircraft Floor
01-516-8804
Aircraft Windshield Assembly
Used on ea-6b aircraft. glass assembly ckpt encl-fus fwd sect-windshiled-bullet resistant
01-516-8927
Access Aircraft Cover
Used on B-1B. ground plane ground plane aft equipment bay door 1122 antenna; matl qq-a-250/4 al bare sheet alloy 2024-0, 30.85 lg x 0.032 thk x 43.90 wd, heat treat al aly per ST0111LA0009 to temper T62, hardness crtl item
01-516-9109
Structural Aircraft Plate
0.025" material thickness doubler
01-516-9178
Access Aircraft Door
01-516-9280
Aircraft Latch Assembly
Hook-aft, fwd. canopy cond "c", ams 6427; nha 32-35202; same as 32-35226-3 except
01-516-9283
Aircraft Latch Assembly
Hook-aft, fwd canopy cond "c"ams 6427; nha 32-34202; same as 32-35226-4 except
01-516-9348
Aircraft Skin
48.000" overall length 10.000" overall width c/o p/n's 160D177101-1, -3, -5, -7, -9, -13, ; heat treat 0
01-516-9438
Aircraft Skin
48.000" overall length 10.000" overall width c/o pn's 160D177101-1, -3, -5, -7, -9, -13, -15; heat treat 0
01-516-9492
Structural Component Air Fitting
Used on f/a-22 raptor. 5.295" overall length fitting-spring beam, keel lns made from 1 5HP78272-113 fitting; 1 5HP78284-105 bushing
01-516-9493
Structural Component Air Fitting
Used on f-22 raptor. 3.000" overall length 3.000" overall width 0.200 centimeters material thickness fitting-spring beam, keel lns consists of 1 5HP78272-107 fitting; 2 5HP78284-105 bushings
01-516-9494
Structural Component Air Fitting
Used on f-22 raptor. 6.000" overall length 2.000" overall width 0.100 centimeters material thickness fitting-spring beam, keel lns consists of 1 5HP78272-115 fitting; 1 5HP78284-107 bushing
01-516-9495
Structural Component Air Fitting
Used on f-22 raptor. 6.000" overall length 2.000" overall width 0.150 centimeters material thickness fitting-spring beam, keel lns consists of 1 5HP78272-103 fitting; 1 5HP78284-109 bushing, 5
01-516-9563
Structural Component Air Fitting
01-516-9564
Structural Component Air Fitting
Used on f-22 raptor. fitting-sidewall, aft, aft keel
01-516-9570
Structural Component Air Fitting
01-516-9573
Structural Component Air Fitting
01-516-9574
Structural Component Air Fitting
Used on f-22 raptor. fitting
01-516-9583
Structural Component Air Bracket
Used on f/a-22 raptor. bracket-titanium sustem, support upper skin, forward boom
01-516-9587
Structural Component Air Bracket
Used on f/a-22 raptor. bracket-frame
01-516-9592
Structural Component Aircraf Web
Used on f-22 raptor. web-aft, keel
01-516-9594
Structural Component Air Fitting
Used on f-22 raptor. 5.000" overall length 4.000" overall width aft uplock, arresting gear dim. are stock material; nha: 5HL71029-101; see note on drawing 5HL71031-101; c/o: 1 fitting, 2 bushing
01-516-9595
Structural Component Air Fitting
Used on f-22 rapter. 5.000" overall length fitting assy, fairing contains (1) bracket with (2) MS14239A04-009 bushing, (1) MS14238A06-010 bushing
01-516-9596
Structural Component Air Fitting
