01-270-3093
Structural Component Air Support
0.050" material thickness
01-270-3094
Structural Component Air Support
0.063" material thickness primer epoxy-polyamide surface treated
01-270-3095
Structural Component Air Support
0.063" material thickness primer epoxy-polyamide surface treated
01-270-3096
Structural Component Air Support
0.063" material thickness primer epoxy-polyamide surface treated
01-270-3097
Structural Component Air Support
0.050" material thickness primer epoxy-polyamide surface treated
01-270-3099
Structural Aircraft Panel
0.250" overall width c/o kickskield, thermoplastic sheets; liner, aluminum foil tape; furn w/clip, aluminum alloy, qq-a-250/13, alloy 7075-T6; 20.130 in. lg; 13.210 in.
01-270-3784
Structural Component Air Support
0.050" material thickness
01-270-3785
Structural Component Air Support
0.063" material thickness primer epoxy-polyamide surface treated
01-270-3786
Structural Component Air Support
0.040" material thickness primer epoxy-polyamide surface treated
01-270-3890
Airframe Modification Kit
Used on uh-60 series helicopter.
01-270-3919
Structural Component Air Support
01-270-3920
Structural Aircraft Panel
20.130" overall length 13.210" overall width oc/o kickshield, thermoplastic sheet, lexan F60061 genreal electric, color dark gull gray; liner, aluminum foil tape; clip, aluminum alloy, alloy 7075-T6. 0.250 in min., 0.250 in max dia three holes; opposite of item shown
01-270-4366
Aircraft Fairing
53.700" overall length
01-270-4383
Airfoil Rib
Used on aircraft,f-14. 0.025" material thickness
01-270-4384
Airfoil Rib
Used on aircraft,f-14. 0.025" material thickness
01-270-4385
Airfoil Rib
Used on aircraft,f-14. 0.025" material thickness
01-270-4386
Airfoil Rib
0.050" material thickness primer epoxy-polyamide surface treated
01-270-4387
Airfoil Rib
0.050" material thickness primer epoxy-polyamide surface treated
01-270-4388
Airfoil Rib
Used on F-14. 0.025" material thickness c/o epoxy, polyamide primer mil-p-23377
01-270-4781
Aircraft Fairing
01-270-4782
Aircraft Fairing
01-270-4783
Structural Component Air Support
Used on acft model b-1b. functional description:used on nose landing gear uplock installation; nuclear hardness critical item; nha L3400303-001;
01-270-4788
Structural Aircraft Panel
Identical to L1200923-021 except 0.250 excess on inbd, outbd & aft
01-270-4853
Radome
Nha L3005999; used on fuslg lower tailcone radome assy; acft model b-1b
01-270-4990
Structural Aircraft Plate
6.800" overall length 2.600" overall width 0.156" material thickness
01-270-5680
Structural Component Air Support
Used on acft model f-16. located at fuselage station 492.44 on horizonal tail
01-270-6013
Aircraft Fairing
Used on KC-135. 44.100" overall length 20.000" overall width 0.040" material thickness opposite -27; nha 5-71743; TEMPER0, class d, finish f-2.130
01-270-6066
Aircraft Windshield Panel
Used on aircraft,e-6a.
01-270-6781
Structural Component Air Support
Aluminum alloy 6061 bar temp T6 per qq-a-250/11, finish chemical film class 3 per mil-c-5541, 0.720 in. min 0.780 max thk, 2.000 in. lg, 0.750 in. w, 2 holes 0.344 in. dia
01-270-6782
Structural Component Air Support
Used on acft,model f18. consist of 1 bracket p/n 74A670686-1001, 2 rivets p/n MS20470AD4; bracket material: aluminum qq-a-250/13 cond-0; 0.071 in. x 2.40 in. x 5.20 in.
01-270-6783
Structural Component Air Support
Used on acft,model f18. consist of 1 bracket p/n 74A670686-2002, 2 rivet p/n MS20470AD4; bracket material: aluminum qq-a-250/13; 0.071 in. x 2.40 in. x 5.20 in.
01-270-7672
Structural Component Air Support
Used on c-141 acft. fitting u/o aft cowl
01-270-7673
Structural Component Air Support
Used on c-141 acft. fitting u/o aft cowl
01-270-8590
Structural Component Air Support
0.063" material thickness primer epoxy-polyamide surface treated
01-270-9059
Aircraft Fairing
01-270-9060
Aircraft Fairing
01-270-9077
Fuel Aircraft Tank
01-270-9961
Aircraft Skin
01-271-0063
Control Surface Aircraft Fairing
Used on acft,model av8.
01-271-0064
Control Surface Aircraft Fairing
Used on acft,model av8.
01-271-0067
Former
Used on acft,model av8. 22.000" overall length 11.600" overall width 0.040" material thickness
01-271-0068
Former
Used on acft,model av8. material:aluminum qq-a-250/13 cond-0; 0.040 in. x 10.90 in. x 21.55 in.;
01-271-0069
Former
Used on acft,model av8. 22.000" overall length 11.150" overall width 0.040" material thickness
01-271-0071
Wing Rib
Used on acft,model av8. 9.750" overall length 7.200" overall width 0.032" material thickness
01-271-0072
Wing Rib
Used on acft,model av8. 9.750" overall length 7.200" overall width 0.032" material thickness
01-271-0073
Aircraft Skin
Used on acft,model av8. 27.000" overall length 21.000" overall width
01-271-0717
Airframe Modification Kit
Used on uh-60 series helicopters.
01-271-0718
Airframe Modification Kit
Used on uh-60 series helicopter.
01-271-1145
Structural Aircraft Plate
Used on aircraft model av-8. aluminum alloy; 35.480 in. lg; 6.360 in. w
01-271-1146
Structural Aircraft Plate
35.480" overall length 6.360" overall width
