01-269-3606
Aircraft Skin
Used on C-141. 30.0000" overall length 24.000" overall width
01-269-3607
Aircraft Skin
25.000" overall length 13.000" overall width NHA3P21600, 3-29004, 3P29013, 3P29027, 3P29064
01-269-3608
Aircraft Spar
01-269-3609
Aircraft Spar
01-269-4094
Structural Aircraft Plate
Used on C-141. 5.000" overall length 3.000" overall width 0.020" material thickness
01-269-4095
Structural Aircraft Plate
Used on C-141.
01-269-4096
Structural Aircraft Plate
Used on C-141.
01-269-4097
Aircraft Fairing
Used on C-141. 35.000" overall length 8.000" overall width 0.040" material thickness
01-269-4098
Structural Component Air Support
60.000" overall length 2.000" overall width 0.063" material thickness
01-269-4099
Structural Component Air Support
01-269-4100
Structural Component Air Support
3.000" overall length 1.000" overall width 0.032" material thickness
01-269-4101
Structural Component Air Support
2.000" overall length 2.000" overall width 0.050" material thickness
01-269-4729
Filler Opening Cap
3a thread class 2.620" outside diameter anodize body surface treated uns thread series
01-269-6106
Structural Aircraft Panel
01-269-6905
Access Aircraft Cover
Used on acft model b-1b. consist of 1 skin, 2 rib; nha L1804003; used on wing panel flap actuator access door
01-269-6906
Access Aircraft Cover
Used on acft model b-1b. consist of 1 skin, 2 rib; nha L1804004; used on wing panel flap actuator access door assy
01-269-6907
Access Aircraft Cover
Used on acft model b-1b. consist of 1 skin, 2 rib; nha L1804005; located wing panel flap actuator access door assy
01-269-6909
Access Aircraft Cover
Used on acft model b-1b. consist of 1 skin, 2 rib; nha L1802004; used on wing panel flap actuator access door assy
01-269-6910
Aircraft Door
Consists of 2 housing, 3 rod assy, 1 lever, 1 spring, 3 support, 2 bushing, 1 strap, 2 retainer, 1 door, 5 plate, 1block, 3 shim; nha L3010050
01-269-6911
Aircraft Door
Consist of 1 retainer, 1 strap, 3support, 1 handle assy, 3 rod assy, 2 bushing, 3 spring, 1 lever, 2 housing, 5 plate, 1 hatch frame, 1 block, 3 shim; nha L3010050
01-269-6942
Structural Aircraft Plate
Used on C-141. 7.000" overall length 11.000" overall width 0.040" material thickness T3 clad
01-269-6943
Aircraft Fairing
C/o 1 panel assy, 1 platform seal, 5 duct, 5 esc
01-269-6944
Aircraft Fairing
Nuclear hardness critical item
01-269-6945
Aircraft Fairing
Nuclear hardness critical item; c/o: panel assy, platform seal, ducts
01-269-6946
Aircraft Fairing
01-269-6947
Fuselage Aircraft Fairing
Used on f-15 acft. al alloy 2024-0 alclad; fairing, arresting hook;
01-269-6948
Structural Component Air Support
Used on f-16 aircraft.
01-269-6949
Structural Component Air Support
Used on f-16 aircraft.
01-269-6950
Structural Component Air Support
Used on acft model b-1b.
01-269-6951
Structural Component Air Support
Used on acft model b-1b.
01-269-6956
Airfoil Rib
6.000" overall length 3.000" overall width 1.500" material thickness
01-269-6996
Fluid Aircraft Manifold
Consist of 1 weld assy, 2 coupling, 1 insert; nha L4802200; used on fwd intmd fuselage cooling fuel temperature sensor manifold; used on b-1b
01-269-7383
Fluid Aircraft Manifold
01-269-7611
Structural Component Air Support
0.050" material thickness
01-269-7612
Structural Component Air Support
0.050" material thickness
01-269-7613
Structural Component Air Support
0.050" material thickness
01-269-7614
Structural Component Air Support
0.063" material thickness
01-269-7615
Structural Component Air Support
0.063" material thickness
01-269-7616
Structural Component Air Support
0.063" material thickness
01-269-7617
Structural Component Air Support
0.063" material thickness
01-269-7618
Structural Component Air Support
0.063" material thickness
01-269-7620
Airfoil Rib
Used on f-14 tomcat. primer epoxy-polyamide surface treated
01-269-8684
Structural Component Air Support
01-269-8840
Structural Component Air Support
0.050" material thickness
01-269-8841
Structural Component Air Support
0.063" material thickness
01-269-8842
Structural Component Air Support
0.050" material thickness
01-269-8843
Structural Component Air Support
0.063" material thickness
01-269-8844
Structural Component Air Support
0.050" material thickness
01-269-8845
Structural Component Air Support
0.063" material thickness
01-269-8846
Structural Component Air Support
Aluminum alloy, qq-a-250/4, alloy 2024, T62; epoxy polyamide primer, mil-p-23377; 0.063 in. thk stock; three holes 0.192 in. min 0.198 in. max dia
