01-204-3678
Structural Aircraft Plate
1.200" overall length 1.000" overall width 0.125" material thickness
01-204-3679
Aircraft Fairing
01-204-3681
Structural Component Air Support
Used on acft model b-1b. functional description:used as overwing fairing position indicator switch support; nuclear hardness critical item; al alloy 2024-T8511 per qq-a-200/3; opposite p/n -003; nha L3223628;
01-204-3682
Structural Component Air Support
Used on acft model b-1b. al alloy 2024-T851 per qq-a-225/6; 4.470 in. lg, 2.500 in. w, 2.000 in.h; opposite p/n -004; nha L5351642-001
01-204-3683
Structural Component Air Support
Used on f-15 acft. titanium; sidewall closure-engine fairing
01-204-3684
Structural Component Air Support
Used on f-15 acft. outboard-forward, engine upper nozzle fairing
01-204-3685
Structural Component Air Support
Used on f-15 acft. empennage, support beam; fuselage station 738.870
01-204-3686
Structural Component Air Support
Used on f-15 acft. former-empenage, support beam; fuselage station 738.870
01-204-3687
Structural Component Air Support
Used on f-15 acft. titanium; sidewall closure-engine fairing
01-204-3688
Structural Component Air Support
Used on f-15 acft. titanium; sidewall closure-engine fairing
01-204-3689
Structural Component Air Support
Used on f-15 acft. inboard side panel; fuselage station 672.680
01-204-3690
Structural Component Air Support
Used on f-15 acft. inboard side panel; fuselage station 672.680
01-204-3700
Aircraft Former
36.000" overall length 22.000" overall width 0.125" material thickness part of -5 assy; eff on -5c 0001 -9999; nha 16B6105-5
01-204-3701
Aircraft Former
17.300" overall length nuclear hardness critical item; shape 4E148 by 17.30 in lg; nha L3206642-001
01-204-3702
Aircraft Former
01-204-3703
Aircraft Former
01-204-3704
Aircraft Former
01-204-3735
Thermal Special Purpo Insulation
End item identification:aircraft, model b-1b; nha L3227345-101
01-204-3736
Thermal Special Purpo Insulation
B-1b acft; p/n nha L3227345-031
01-204-3737
Thermal Special Purpo Insulation
B-1b acft; p/n nha L3227345-031
01-204-3738
Thermal Special Purpo Insulation
B-1b acft; p/n nha L3227345-071
01-204-3739
Thermal Special Purpo Insulation
B-1b acft; p/n nha L3227345-101
01-204-3740
Thermal Special Purpo Insulation
B-1b acft; p/n nha L3227345-202
01-204-3742
Thermal Special Purpo Insulation
B-1b acft; p/n nha L3227345-202
01-204-3743
Thermal Special Purpo Insulation
B-1b acft; p/n nha L3227345-122
01-204-3744
Thermal Special Purpo Insulation
B-1b acft; c/o--015 facesheet inner, cres foil alloy 321 cond a, spec qq-s-766, 17 in. l x 19 in. w x .002 in. thk; -017 facesheet outer, same dims
01-204-3745
Thermal Special Purpo Insulation
B-1b acft; c/o--015 facesheet inner, cres foil alloy 321 cond a, spec qq-s-766, 30 in. l x 17 in. w x .002 in. thk; -029 facesheet outer, same dims
01-204-3746
Thermal Special Purpo Insulation
B-1b acft; c/o--029 facesheet inner, cres foil alloy 321 cond a, spec qq-s-766, 30 in. l x 9 in. w x .002 in. thk; -043 facesheet outer, same dims
01-204-3747
Thermal Special Purpo Insulation
B-1b acft; c/o--053 facesheet inner, cres foil alloy 321 cond a, spec qq-s-766, 28 in. l x 18 in. w x .002 in. thk; -055 facesheet outer, same dims
01-204-3749
Thermal Special Purpo Insulation
C/O227 facesheet, inner qq-s-766 cres foil alloy 321 cond a, 26.000 in, by 0.002 in.by 23.000 in.w, 229 facesheet, outer qq-s-766, 26.000 in.l by 0.002 in.thk by 23.000 in.w, 233 retainer, qq-s-766 cres foil ribbon, 140.000 in.l by 0.0005 in.thk by 1.000 in.w, 235 batt crf-800 blanket 8 lb/FT3-26.000 in.l by 0.125 in.thk by 23.000 in.w, 237 ident plate, grommet (27) ; location nac, apu compt, yn 216.5-265.24, ctd; end item identification:aircraft, model b-1b
01-204-3750
Thermal Special Purpo Insulation
C/O415 facesheet, inner, qq-s-766 cres foil, alloy 321, cond a, 23.000 in.l by 0.002 thk by 18.000 w, 417 facesheet, outer, qq-s-766, 23.000 in.lg by 0.002 in.thk by 18.000 in.l; 419 retainer qq-s-766 cres foil ribbon 76.000 in.l by 0.0005 in.thk by 1.000 in.w; 423 batt crf 800 blanket 8 lb/FT3; 425 ident plate, grommet (16) ; location nac, apu compt, yn 216.5-265.25, ctd; end item identification:aircraft, model b-1b
01-204-3751
Thermal Special Purpo Insulation
C/o 267 facesheet, inner, qq-s-766 cres foil, alloy 321, cond a, 16.000 in.l by 0.002 in.thk by 7.000 in.w; 269 facesheet, outer, qq-s-766, 16.000 in.l by 0.002 in.thk by 7.000 in.w; 273 retainer, qq-s-766 cres foil ribbon, 42.000 in.l by 0.0005 in.thk by 1.000 in.w; 275 batt crf 800 blanket 8 lb/FT3; 277 ident plate; location nac, apu compt, yn 216.5-265.25 ctd; end item identification:aircraft, model b-1b
01-204-3752
Thermal Special Purpo Insulation
C/O268 facesheet, inner, qq-s-766, cres foil alloy 321, cond a, 16.000 in.l by 0.002 in.thk by 7.000 in.w; 270 facesheet, outer, qq-s-766 16.000 in.l by 0.002 in.thk by 7.000 in.w; 274 retainer qq-s-766 cres foil ribbon 42.000 in.l by 0.0005 in.thk by 1.000 in.w; 276 batt crf-800 blanket 8 lb/FT3; 279 plate ident, grommet (5) ; location nac, apu comp, yn 216.5-265.25, ctd; end item identification:aircraft, model b-1b
01-204-3753
Thermal Special Purpo Insulation
C/o 283 facesheet, inner, qq-s-766 cres foil; 285 facesheet, outer, outer, qq-s-766 cres foil; 287 retainer qq-s-766 cres foil ribbon; 289 batt crt 800 blanket 8 lb/FT3; 293 ident plate qq-s-766 cres sheet, grommet (7) ; location nac, apu compt, yn 216.5-265.25 ctd; end item identification:aircraft, model b-1b
01-204-3755
Thermal Special Purpo Insulation
C/o 325 facesheet, inner, qq-s-766 cres foil, alloy 321, cond a, 27.000 in.l by 0.002 in.thk by 14.000 in.w; 327 facesheet, outer, same matl, ribbon, 76.000 in.l by 0.0005 in.thk by 1.000 in.w; 333 batt crf-800 blanket 8 lb/FT3 27.000 in.l by 0.125 in.thk by 14.000 w; 335 ident plate, grommet (12) ; location nac, apu compt, yn 216.5-265.25, ctd; end item identfication:aircraft, model b-1b
01-204-3756
Thermal Special Purpo Insulation
Dc/o 370 facesheet, inner, qq-s-766 cres foil, alloy 321, cond a, 20.000 in.l by 0.002 in.thk by 7.000 in.w; 374 facesheet, outer, qq-s-766, 20.000 in.l, 0.002 thk by 7.000 in.w; 376 retainer, qq-s-766 cres foil ribbon, 54.000 in.l by 0.0005 in.thk by 1.000 in.w; 378 batt crf-800 blanket, 8 lb/FT3, 20.000 in.lb/FT3, 20.000 l by 0.125 in, thk by 7.000 in.w; 383 ident plate, grommet (5) ; location nac, apu compt, yn 216.5-265.25, ctd; end item identification:aircraft, model b-1b
01-204-5396
Structural Aircraft Panel
Used on aircraft model f-14.
01-204-5701
Structural Aircraft Panel
Used on uh-60 helicopter.
01-204-5710
Structural Aircraft Plate
Used on uh-60 blackhawk helicopter.
01-204-6244
Structural Aircraft Panel
01-204-6303
Structural Aircraft Plate
Used on acft model b-1b. functional description:used on apu start module mtg serrated plate; nuclear hardness critical item; AMS5520 cres sht per PH15-7mo; 1.90 in.lg, 0.750 in.wd, 0.125 in.thk; nha L5802631;
01-204-6304
Structural Aircraft Plate
Used on f-15 acft. closure: vertical stabilizer-leading edge
01-204-6305
Structural Aircraft Plate
01-204-6307
Structural Component Air Support
Used on acft model kc-135. consist of 2 rod end, 1 tube; nha 458-52033
01-204-6308
Structural Component Air Support
Used on acft model kc-135. consist of 2 rod end, 1 tube; nha 458-52033
01-204-6309
Structural Component Air Support
Used on acft model kc-135. consist of 2 rod end, 1 tube; nha 458-52033
01-204-6310
Structural Component Air Support
Used on acft model kc-135. consist of 1 fitting, 2 bushing; nha 458-53001
01-204-6311
Structural Component Air Support
Used on acft model b-1b. al alloy investment casting A356.0 per LB0170-195 class ii; nha L3400134
01-204-6312
Structural Component Air Support
Used on acft model b-1b. titanium bar alloy 6al-4v per mil-t-9047, comp 6, cond a; 3.40 in. long, 3.50 in. wide, 2.50 in. thick; nha L3206662
01-204-6313
Structural Component Air Support
Used on acft model b-1b.
