01-507-8888
Exhaust Pipe Flange
Used on av8b harrier aircraft access cover p/n 75a337498.
01-507-8921
Structural Component Air Support
Used on pylon p/n 75a732402.
01-507-8925
Exhaust Pipe
Used on hydraulic installation p/n 75a690030.
01-507-9103
Structural Component Air Support
9.250" overall length 5.450" overall width 1.500" material thickness block nha 68A324960; u/o f-15a CUM236-243, f-15b CUM38, FMF15a CUM1; avco 5052 thermarest polyurethane foam withoutfabric covering
01-507-9174
Structural Component Air Bracket
01-507-9175
Structural Component Air Support
Used on landing gear, main;f/a-18e/f support of ecp 6038. (navy) support assy, air
01-507-9333
Aircraft Beam
01-507-9397
Stiffener Aircraft Rib
16.600" overall length 2.500" overall width 0.040" material thickness rib-rudder nose heat treat 0; clad; dim. stocksize; rudder station 13.75
01-507-9402
Aircraft Skin
57.000" overall length 26.500" overall width skin-side, upper heat treat 0; sheet; dim. are stocksize; upper; this item has been determined to be a critical application item. in-flight failure of this item would create a hazardous condition
01-507-9411
Aircraft Skin
57.000" overall length 26.500" overall width skin-side, upper heat treat 0; sheet; dimensions are stocksize; upper; this item has been determined to be a critical application item. in-flight failure of this item would create a hazardous condition
01-507-9534
Aircraft Door
Used on ch-47d chinook helicopter.
01-507-9535
Structural Aircraft Panel
Used on f-16 aircraft.
01-507-9631
Aircraft Skin
01-507-9711
Structural Aircraft Panel
Used on f/a-22 raptor. panel, access A3 fuel tank rh-assy of
01-507-9718
Structural Component Air Bracket
Used on f-22 raptor. 6.060" overall length 5.570" overall width bracket m/o: 7050-T7451 aluminum plate
01-507-9719
Structural Component Air Bracket
Used on f-22a raptor. 7.000" overall length 6.000" overall width 3.250" material thickness bracket, mount support heat treat T7451; alum plate; dim. are stock material
01-507-9720
Structural Component Air Fitting
7.100" overall length 1.500" overall width 0.180 " material thickness filler dim are stock matl; matl qq-a-250/24 T76, al aly 7075-T76
01-507-9724
Structural Component Air Fitting
7.100" overall length 1.500" overall width 0.180 " material thickness filler dim are stock matl; matl qq-a-250/24, al aly 7075-T76
01-507-9812
Structural Component Air Support
01-507-9983
Structural Component Air Support
01-508-0368
Structural Aircraft Panel
Used on f-22a raptor. panel composite materials m/f: carbon/bmi & epoxy; c/o: -121 (m/f -101) , & gasket
01-508-0369
Structural Aircraft Panel
Used on f-22a raptor. panel, assembly of opposite -130; composite material made from carbon/bmi
01-508-0382
Structural Aircraft Panel
Used on f-22a raptor. panel, assembly of composite material made from carbon/epoxy
01-508-0986
Structural Component Air Fitting
Used on sh-2g seasprite helicopter. guide
01-508-1214
Structural Component Air Bracket
7.150" overall length 3.390" overall width 0.125" material thickness bracket nha L3050015; u/o b-1b modification; ams 5518 ces sheet, alloy 301, cond 1/2 hard; protect per LA0116-020; finis per L0000024 code 60HA02; opp p/n L3050014-003
01-508-1235
Structural Component Air Support
Angle
01-508-1251
Structural Component Air Bracket
Bracket
01-508-1257
Structural Component Air Support
3.600" overall length 2.000" overall width 0.050" material thickness angle, outbd, aft nha 160D611101; dims are stock material
01-508-1290
Structural Component Air Support
Angle
01-508-1587
Rudder Balance Weight
Used on 707 aircraft. 0.500" overall width
01-508-1885
Aircraft Spar
01-508-1902
Aircraft Spar
01-508-2088
Structural Component Air Support
10.870" overall length 5.250" overall width block nha -1001; u/o f-15a, b BLK7-12
01-508-2090
Structural Component Air Support
10.700" overall length 5.250" overall width block nha -1001; u/o f-15a, b BLK13-16
01-508-2217
Access Aircraft Cover
Used on fighter aircraft-first (f18 e/f).
01-508-2498
Structural Aircraft Panel
Panel assy-ceiling, fs 534.14 to 613.55, lh side material
01-508-2807
Aircraft Step
18.000" overall length 9.500" overall width 1.500" material thickness surface-traction serrated surface
01-508-2871
Structural Aircraft Panel
Liner matl lexan f-6006, color no 36231 fed-std-595
01-508-2910
Structural Aircraft Plate
3.200" overall length 0.900" overall width 0.050" material thickness side cowl panel assy-engine nacelle
01-508-2918
Structural Component Air Fitting
12.700" overall length 5.000" overall width 3.200 " material thickness cam support dim are stock matl, 7075 al aly heat treat to T73
01-508-2990
Structural Aircraft Plate
Side cowl panel assy-engine nacelle
01-508-2999
Structural Component Air Support
4.750" overall length 1.000" overall width angle dimensions are stocksize
01-508-3070
Structural Component Air Support
Used on dewar support assembly 21046650-101. dewar support
01-508-3177
Structural Component Air Support
5.900" overall length 2.240" overall width 1.470" material thickness block nha -1001; u/o f-15c BLK23-CUM358, 407-408, f-15d BLK23-CUM59, f-15dj, j CUM1&up; honeycomb core cellsize 3/16 in. density 2.0 lb/cu ft fully cured
01-508-3462
Structural Component Air Fitting
21.700" overall length 13.000" overall width 0.032 " material thickness fitting heat treat 1/2 h
01-508-4005
Structural Aircraft Plate
2.500" overall length 1.800" overall width 0.050" material thickness side cowl panel assy - engine nacelle
01-508-4033
Structural Aircraft Plate
3.000" overall length 1.500" overall width 0.070" material thickness side cowl panel assy - engine nacelle u/o 204-70045-447
01-508-4185
Access Aircraft Cover
Used on RQ-4A.
01-508-4186
Access Aircraft Cover
Used on RQ-4A.
01-508-4196
Access Aircraft Cover
Used on C-17A. replaces -524; c/o 1 bracket assy, 1 door, 4 pins, 4 nuts, 4 washers; effectivity 17A033-100; NHA17N6W0615; closeout-slat no.3
