01-260-6332
Structural Component Air Support
Used on f-15 acft.
01-260-6333
Structural Component Air Support
Used on f-15 acft.
01-260-6342
Aircraft Former
01-260-6351
Aircraft Skin
8.000" overall length 3.000" overall width nuclear hardness critical item; TA0108-016 type i covering
01-260-6355
Aircraft Skin
8.000" overall length 3.000" overall width nuclear hardness critical item; TA0108-016 type i covering
01-260-6356
Aircraft Skin
Used on b-1 bomber airplane.. 8.000" overall length 3.000" overall width nuclear hardness critical item TA0108-016 type i
01-260-6360
Aircraft Skin
Used on F-15.
01-260-6361
Aircraft Skin
Used on C-130.
01-260-6362
Aircraft Skin
Used on f-15e aircraft.
01-260-6630
Structural Component Air Support
01-260-7855
Structural Component Air Support
01-260-7856
Structural Component Air Support
0.080" material thickness chromate zinc surface treated
01-260-7857
Structural Component Air Support
0.071" material thickness chromate zinc surface treated
01-260-7858
Structural Component Air Support
0.050" material thickness chromate zinc surface treated
01-260-7859
Structural Component Air Support
0.050" material thickness chromate zinc surface treated
01-260-7860
Structural Component Air Support
0.050" material thickness chromate zinc surface treated
01-260-7889
Thermal Special Purpo Insulation
01-260-9010
Structural Aircraft Plate
01-260-9011
Structural Aircraft Plate
Used on acft model a-6e. 0.040" material thickness
01-260-9012
Aircraft Fairing
Used on acft model a-6a and a-6e.
01-260-9013
Structural Component Air Support
0.071" material thickness chromate zinc surface treated
01-260-9014
Structural Component Air Support
0.050" material thickness primer zinc chromate surface treated
01-260-9015
Structural Component Air Support
0.020" material thickness primer zinc chromate surface treated
01-260-9016
Structural Component Air Support
Aluminum alloy, qq-a-200/11 or qq-a-225/9, alloy 7075-T6511/T651, anodize, mil-a-8625, ty 2, cl 1; 2.000 in. thk, fitting; aluminum alloy, qq-a-250/13, alloy 7075-T6, chromate, mil-c-5541, cl 1a; 0.080 in. thk, plate; opposite of p/n 123CSM10015-501
01-260-9917
Structural Component Air Support
Aluminum alloy, qq-a-250/3 alloy 2014 T6, primer, zinc chromate, mil-p-6808; 0.050 in. material thickness
01-260-9918
Structural Component Air Support
Aluminum alloy, qq-a-250/5 alloy 2024 T3, primer, zinc chromate, mil-p-6808
01-261-0276
Structural Aircraft Panel
Used on pacer special. smoothness critical item; c/o: bracket, sealants, shims, panel, ftg assy, edges, pins, bolts, collars, & retaining rings
01-261-0277
Structural Aircraft Panel
Used on pacer special. smoothness critical item; c/o: bracket, sealants, shims, sleeves bolts, bolts, washers, nuts, nut collars, & retaining rings
01-261-0326
Structural Component Air Fitting
C/o: 1 fitting, 1 ball, 1 retainer, 2 pin; nha L3227003; opposite -001
01-261-0327
Structural Component Air Support
C/o: 1 fitting, 1 ball, 1 retainer, 2 pin; nha L3227003; used on fwd pin latch engine access door fitting assembly
01-261-0328
Structural Component Air Fitting
C/o: 1 fitting, 1 ball, 1 retainer, 2 pin; opposite -011; nha L3227003; used on fwd pin latch engine access door fitting assembly
01-261-0330
Structural Component Air Support
Fitting assembly-engine access door, forward pin latch
01-261-0331
Structural Component Air Fitting
C/o: 1 fitting, 1 ball, 1 retainer, 2 pin; opposite -031; nha L3227003; used on fwd pin latch engine access door fitting assembly
01-261-0335
Structural Aircraft Panel
Used on acft model b-1b. consist of 4 adhesive pile, 1 panel; nha L5338806; located on YF335 to YF344
01-261-0336
Structural Aircraft Panel
Used on acft model b-1b. consist of 4 adhesive pile, 1 panel; nha L5338806; located on YF335 to YF344
01-261-0348
Aircraft Skin
8.000" overall length 3.720" overall width nuclear hardness critical item; TA0108-016 type i
01-261-0656
Movable Canopy
Haz class div 1.4; storage comp gps; dot class exempt 1; un serial number 0349; dot marking xx; dot label 3; net xpl weight 250.0 lbs
01-261-1220
Aircraft Ramp Assembly
Fwd ramp assembly; nha 4F51000
01-261-1233
Aircraft Door
C/o 2 sheet, 19 frame, 1 blanket, 31 clip, 1 house assy, 2 bracket assy, 6 block, 4 stiffener, 1 stop, 1 skin, 2 plate, 1 retainer, 2 fitting, 6 support, 1 bracket, misc hardware
01-261-1248
Structural Aircraft Plate
Used on F-15.
01-261-1249
Structural Component Air Fitting
01-261-1250
Structural Component Air Support
Used on f-15 acft. aluminum alloy 7075-T7351; support-valve, landing gear selector
01-261-1251
Structural Component Air Support
Used on f-15 acft. aluminum alloy 7075-T7351; support-valve, landing gear selector
01-261-1254
Structural Aircraft Panel
Used on acft model b-1b. consist of 1 strip, 3 spacer; nha L1202397; located at xrs 188.515 to xrs 215.515
01-261-1255
Structural Aircraft Panel
Used on acft model b-1b. consist of 1 strip, 3 spacer; nha L1202397; located at xrs 188.515 to xrs 215.515
01-261-1256
Structural Aircraft Panel
Used on acft model b-1b. consist of 1 strip, 3 spacer; nha L1202397; located at xrs 188.515 to xrs 215.515
01-261-1257
Structural Aircraft Panel
Used on acft model b-1b. consist of 1 strip, 3 spacer; nha L1202397; located at xrs 188.515 to xrs 215.515
01-261-1258
Structural Aircraft Panel
Used on acft model b-1b. consist of 1 strip, 2 spacer; nha L1202397; located at xrs 188.515 to xrs 215.515
01-261-1259
Structural Aircraft Panel
Used on acft model b-1b. consist of 1 strip, 2 spacer; nha L1202397; located at xrs 188.515 to xrs 215.515
01-261-1260
Structural Aircraft Panel
Used on acft model b-1b. consist of 1 strip, 2 spacer; nha L1202397; located at xrs 188.515 to xrs 215.515
