01-513-8396
Structural Aircraft Panel
Used on f/a-22 raptor. panel, access-fuel tank, aft centerline made from 1 5HF46509-127 panel; 1 5HF46848-113 gasket
01-513-8397
Structural Aircraft Plate
Scuff plate pacer spical; nurclear hardnessandsmoothness critical item
01-513-8398
Structural Aircraft Plate
Scuff plate
01-513-8401
Structural Aircraft Panel
Used on f-22a raptor. panel
01-513-8913
Structural Component Air Bracket
Used on aircraft, osprey, v-22a, marine corps.
01-513-8916
Window Aircraft Frame
01-513-8929
Access Aircraft Cover
Used on f/a-22 raptor. cover access aircraft c/o 1 cover, 35 rings, 35 screws
01-513-8984
Structural Aircraft Panel
Used on i-cap ii peculiar aircraft (ea-6b). navy-mounting base, aircraft
01-513-9183
Structural Aircraft Plate
Gusset gusset right hand only
01-513-9554
Structural Aircraft Plate
Aeb scuff plate form, fit, function
01-513-9558
Aircraft Fairing
Aeb, blade seal nuclear hardness critical
01-513-9559
Structural Aircraft Panel
Used on f/a-22 raptor.
01-513-9560
Structural Aircraft Panel
Used on f/a-22 raptor. 29.659" overall length panel, access-fuel tank, aft centerline made from (1) 5HF46509-127 panel
01-513-9562
Structural Aircraft Panel
Used on f/a-22 raptor. panel
01-513-9576
Winglet
Winglet assy, complete same as -504 except where ecn states; c/o 1 strl assy; nha 17N6W0637
01-513-9577
Winglet
Winglet assy, complete same as -503, except ecn chg; c/o 1 strl assy; nha 17N6W0637-505; effectivity 17A117-17A999
01-513-9901
Structural Aircraft Plate
Used on pacer special. scuff, plate
01-513-9946
Structural Component Air Fitting
Fitting assy
01-513-9948
Structural Component Air Fitting
Fitting assy
01-514-0177
Structural Component Air Bracket
Used on p53 harrier ii. 0.050" overall length 2.030" overall width
01-514-0319
Structural Component Air Bracket
Used on helicopter. bracket assembly
01-514-0350
Aircraft Stringer
Used on next higher assembly 145s2577-171, ch-47d chinook helicopter.
01-514-0414
Horizontal Stabilizer
Horizontal stab. box-assy of box assy of; nha 16T7461
01-514-0580
Stiffener Aircraft Rib
01-514-0590
Stiffener Aircraft Rib
01-514-0598
Aircraft Stringer
01-514-0604
Aircraft Stringer
01-514-0685
Aircraft Floor
Used on next higher assembly 145s2554-29,ch-47d chinook helicopter.
01-514-0687
Aircraft Floor
Used on next higher assembly 145s2554-29 & 30; ch-47d chinook helicopter.
01-514-0817
Structural Aircraft Panel
Used on f-22 raptor. panel-apu access, aft assy c/o 19 gasket, 50 ring, 50 bolt
01-514-0820
Access Aircraft Cover
Used on f/a-22 raptor. panel-apu access, aft assembly made from 1 5HF42511-107 cover; 1 each 5HF45823-147, -149, -151, -153, -157 gaskets; 12 5HF45823-159 gaskets; 1 each 5HF45823-161, -169, -171, -173 gaskets; 39 CA21037-4r rings; 11 CA21037-5r rings; 9 CA21359-4-2tx stud bolts; 14 CA21359-4-4tx stud bolts; 2 CA21359-4-6tx stud bolts; 14 CA21359-4-8tx stud bolts; 2 CA21359-5-10tx stud bolts; 2 CA21359-5-12tx stud bolts; 1 CA21359-5-16tx stud bolt; 2 CA21359-5-6tx stud bolts
01-514-0832
Structural Component Air Bracket
Used on f-22 raptor. 2.000" overall length
01-514-0835
Structural Component Air Bracket
01-514-1079
Structural Component Air Support
01-514-1088
Structural Component Air Support
01-514-1256
Aircraft Skin
Used on k135 aircraft. R22 (rh) ; fig. 68, index no. 3
01-514-1257
Aircraft Skin
Used on kc135 aircraft. skin, R26 (upper) ; fig. 133, index no. 4
01-514-1259
Structural Component Air Support
Used on kc135 aircraft. fig. 61, index no. 4
01-514-1262
Aircraft Skin
Used on kc135 aircraft. R8; fig. 44, index no. 2
01-514-1263
Structural Component Air Support
Used on kc135 aircraft. fig. 59, index no. 4
01-514-1271
Access Aircraft Cover
Used on kc135 aircraft. next higher assembly, access, boom, fig. 89
01-514-1272
Aircraft Skin
Used on kc135 aircraft. skin, R25, lower; fig. 137, indexno. 3
01-514-1273
Aircraft Skin
Used on kc135 aircraft. R21 (lh) ; fig. 67, index 3
01-514-1274
Structural Aircraft Panel
Used on kc135 aircraft. fairing assembly, R6 (rh) ; fig. 8index no. 1
01-514-1290
Structural Component Air Support
01-514-1326
Aircraft Fairing
20.000" overall length 20.000" overall width 0.063" material thickness fairing, sensor-fwd sheet clad, heat treat 0; replaces -1; effectivity 17A117-17A999; nha 17P1A2713
01-514-1450
Aircraft Stringer
01-514-1452
Structural Component Air Support
01-514-1602
Access Aircraft Door
Used on f/a-22 raptor. door installation-avionics
01-514-1603
Access Aircraft Door
Used on f/a-22 raptor. door door access lru
