01-508-7694
Structural Component Air Fitting
01-508-7695
Structural Component Air Fitting
01-508-7696
Structural Component Air Fitting
01-508-7698
Structural Aircraft Panel
01-508-7724
Structural Component Air Support
7.400" overall length 7.000" overall width 1.500" material thickness block NHA68A324910, u/o f-15c cum 239-253, f-15d cum 40-41, f-15dj cum 9-10; honeycomb core per mms-703 typeiii, hrp-3/8-GF11-2.2 lb/cu ft fully cured, thickness 1.50 porm .03; dim are stock matl
01-508-7725
Structural Component Air Support
7.400" overall length 7.000" overall width 1.500" material thickness block nha, 68A324910, u/o f-15c cum 239-253, f-15d cum 40-41, f-15dj cum 9-10; honeycomb core per mms-703 type iii, hrp-3/8-GF11-2.2 lb/cu ft fully cured, thickness 1.50 porm .03; dim are stock matl
01-508-7727
Wing Landing Flap
Panel instl-structural, inbd trailing edge, inbd flap eff from 17A001-004; c/o 2 support assy, 4 spar assy; 4 washer (AN9604l) (limited eff) ; rivet as required; 3 rib assy; 1 skin assy; 1 spare assy; 1 channel assy; 2 support assy
01-508-7863
Radome Cover
Used on an/tmq-44a(v).
01-508-7948
Structural Component Air Bracket
01-508-7957
Structural Component Air Bracket
01-508-7963
Structural Component Air Bracket
01-508-8175
Structural Component Air Fitting
01-508-8176
Structural Component Air Fitting
01-508-8177
Structural Component Air Fitting
01-508-8178
Structural Component Air Fitting
01-508-8184
Structural Component Air Fitting
01-508-8185
Structural Component Air Fitting
01-508-8199
Structural Component Air Support
1.600" overall length 0.085" overall width 0.035" material thickness block NHA68A321400, u/o f-15c CUM1
01-508-8200
Structural Component Air Support
10.800" overall length 4.400" overall width 1.500" material thickness block nha, 68A324910 u/o f-15c CUM239-253, f-15d CUM40-41, f-15dj CUM9-10; honeycomb core per mms-703 type iii, hrp-3/8-GF11-2.2 lb/cu ft, fully cured, thickness 1.50 porm .03; dim are stock matl
01-508-8201
Structural Component Air Bracket
7.000" overall length 3.000" overall width 2.000" material thickness c/0 1 -7 bracket, 4 bushing; effeect 17A117-184; nha 17P3A1600; -501 same as -1 except; heat treat T7451-d; matl. spec DMS2233
01-508-8203
Structural Component Air Support
14.020" overall length 2.000" overall width 1.100" material thickness block nha 68A321400, u/o f-15c CUM1-214, f-15d CUM1-35, f-15dj CUM1-6, f-15j CUM1and up, fmf-15c CUM1-9, fmf-15d CUM1-6, saf-15c CUM1-24, saf-15d CUM1-11; hh-i-530 type i grade 2 class 1 polyurethane foam; dim are stock matl
01-508-8315
Structural Component Air Bracket
3.100" overall length 3.000" overall width 0.080" material thickness bracket dimensions are stocksize; heat treat 0
01-508-8337
Structural Component Air Support
01-508-8342
Structural Component Air Support
01-508-8377
Structural Component Air Bracket
3.700" overall length 2.700" overall width 0.080" material thickness bracket dimensions are stocksize; heat treat 0
01-508-8379
Structural Aircraft Plate
1.800" overall length 5.000" overall width 0.050" material thickness jeat treat 6
01-508-8386
Structural Component Air Bracket
3.700" overall length 2.700" overall width 0.080" material thickness bracket dimensions are stocksize; heat treat 0
01-508-8390
Structural Component Air Support
3.000" overall length 2.000" overall width 0.050" material thickness angle dimensions are stocksize; heat treat T6
01-508-8393
Structural Component Air Support
3.300" overall length 1.200" overall width 0.060" material thickness doubler heat treat 6
01-508-8395
Structural Component Air Support
3.000" overall length 2.000" overall width 0.050" material thickness angle dimensions are stocksize; heat treat T6
01-508-8401
Structural Component Air Support
7.000" overall length 3.000" overall width 0.063" material thickness angle dimensions are stocksize; heat treat 0
01-508-8407
Structural Component Air Support
2.750" overall length 2.000" overall width 0.050" material thickness angle dimensions are stocksize; heat treat T6
01-508-8412
Structural Component Air Support
7.000" overall length 3.000" overall width 0.063" material thickness angle dimensions are stocksize; heat treat 0
01-508-8417
Structural Component Air Support
4.500" overall length 1.750" overall width 0.063" material thickness angle heat treat 0
01-508-8420
Structural Component Air Support
2.750" overall length 2.000" overall width 0.050" material thickness angle dim.are stocksize; effect from 1 thru on; heat treat T6
01-508-8470
Structural Component Air Support
0.060" material thickness housing plastic glass fiber reinforced, light gray number 9685 per bac 5427; optional plastic glass fabric reinforced per bac 5419 light gray number 3W95 per bac 5427
01-508-8482
Structural Component Air Support
5.000" overall length 2.000" overall width 0.063" material thickness angle heat treat 0; dimensions are stocksize
01-508-8490
Structural Component Air Support
5.000" overall length 2.120" overall width 0.063" material thickness angle
01-508-8527
Structural Aircraft Plate
1.500" overall length 1.400" overall width 0.050" material thickness clip dim are stock matl
01-508-8532
Structural Aircraft Plate
1.500" overall length 1.400" overall width 0.050" material thickness clip dim are stock matl
01-508-8536
Structural Component Air Support
7.000" overall length 3.000" overall width 0.0630" material thickness angle 32 opp -31; dims are stock material
01-508-8538
Structural Component Air Support
5.000" overall length 2.000" overall width 0.063" material thickness angle heat treat 0
01-508-8548
Structural Component Air Support
10.000" overall length 5.000" overall width 2.000" material thickness angle heat treat 0; alt for p/n 160J610103-66
01-508-8568
Structural Component Air Support
5.000" overall length 2.120" overall width 0.063" material thickness angle
01-508-8685
Structural Component Air Support
10.000" overall length 5.000" overall width 2.000" material thickness angle heat treat 0; alt for p/n 160J610103-37
01-508-8895
Structural Component Air Support
5.000" overall length 0.062" material thickness heat treat T6511; shp; dimensions are stocksize
01-508-8900
Structural Component Air Support
5.000" overall length 0.062" material thickness heat treat T6511; shp; dimensions are stocksize
01-508-8903
Structural Aircraft Panel
Louvered vent proof test requirements, fit assemblies in bleed air exhaust duct, cstg 35-12538-2, for acceptance
01-508-8965
Structural Component Air Support
3.600" overall length 1.000" overall width 0.053" material thickness support heat 6; c/o p/n's (1 each) 160D610103-1, -133, -3
01-508-9012
Structural Component Air Support
3.600" overall length 1.000" overall width 0.053" material thickness support heat treat, 6, c/o pl/n's 160D610103-1, -133, -137, -3 (1 ea)
