01-226-9044
Thermal Insulation Pipe Covering
Acft c-130
01-227-0724
Structural Component Air Support
01-227-0733
Bleed Air Duct Assembly
C/o 1 tube, 2 doubler, 2 support, 1 band, 1 nameplate, 1 boss assy, 2 flange
01-227-0739
Structural Aircraft Panel
Consist of 1 panel, 126 insert; nha 204-40182
01-227-0740
Structural Aircraft Panel
Consist of 1 panel, 1 foam block, 1 perforated vinyl, 75 insert; nha 204-40182
01-227-0741
Structural Aircraft Panel
Consist of 1 panel, 1 foam block, 1 perforated vinyl, 75 insert; nha 204-40182
01-227-0742
Structural Aircraft Panel
Consist of 1 panel, 2 insert; nha 204-40182
01-227-0743
Structural Aircraft Panel
Consist of 1 panel, 1 perforated vinyl, 51 insert; nha 204-40181
01-227-0744
Structural Aircraft Panel
Consist of 1 panel, 1 insert; nha 204-40182
01-227-0745
Structural Aircraft Panel
Used on acft model e-3a. consist of 1 panel, 13 insert; nha 204-40182; located at sta 881 to 951.5
01-227-0746
Structural Aircraft Panel
Used on acft e-3a. consist of 1 panel, 6 insert; nha 204-40182; located at sta 881 to 951.5
01-227-0747
Structural Aircraft Panel
Used on acft model e-3a. consist of 1 panel, 26 inserts; nha 204-40182; located at sta 881 to 951.5
01-227-0749
Structural Aircraft Panel
Used on acft model e-3a. consist of 1 panel, 28 insert; nha 204-40182; located at sta 881 to 951.5
01-227-0750
Structural Aircraft Panel
Used on acft model e-3a. consist of 1 panel, 18 insert; nha 204-40182; located at sta 881 to 951.5
01-227-0755
Aircraft Floor
Includes 1 rug p/n 906492-5; 1 panel p/n 906492-7; 1 batt assy p/n 906492-9; 3 straps p/n 906492-15; 1 batt assy p/n 906492-101
01-227-0759
Thermal Special Purpo Insulation
01-227-0760
Thermal Special Purpo Insulation
01-227-0761
Thermal Aircraft Insulation
Used on acft model b-1b. consist of 2 facesheet, 1 batt blanket, 1 plate, 3 grommet; located at yan 25.93 to yan 81.50
01-227-0762
Thermal Aircraft Insulation
Used on acft model b-1b. consist of 2 facesheet, 1 batt blanket; located at yan 25.93 to yan 81.50
01-227-0846
Access Aircraft Door
Anodize surface treated
01-227-1591
Structural Component Air Support
Used on c-5 aircraft. fitting, end-lower side panel frame, fus sta 1884.00; opposite -101a; nha 4F41262
01-227-1597
Aircraft Pylon
01-227-1598
Aircraft Pylon
01-227-2042
Structural Aircraft Plate
01-227-2050
Structural Component Air Support
Used on c-5 aircraft. fitting assembly-rear beam, elev actr, inbd, sta 95.56; c/o: -703a fitting (1) , bushing (2) ; opposite -702a; nha 4T31023
01-227-2073
Airfoil Rib
C/o approximately 18 components
01-227-2074
Airfoil Rib
C/o approximately 18 components
01-227-2077
Aircraft Skin
Used on F-111. 60.000" overall length 15.000" overall width fms 105, type i T6, A032
01-227-3519
Structural Component Air Support
01-227-3520
Structural Component Air Support
01-227-4911
Access Aircraft Cover
Used on acft model b-1b. consist of 1 plate, 5 helicoil insert; nha L1203369; used on wing outer panel fuel transfer pump access cover
01-227-4913
Access Aircraft Door
Used on acft model b-1b. nha L3022126; located at YF686.50
01-227-4914
Access Aircraft Door
Used on acft model b-1b. nha L1203350; lwr wing outer panel
01-227-4915
Access Aircraft Door
Used on acft model b-1b. nha L1203350; lwr wing outer panel
01-227-4916
Access Aircraft Door
Used on acft model b-1b. nha L1203350; lwr wing outer panel
01-227-4917
Access Aircraft Door
Used on acft model b-1b. nha L1203350; lwr wing outer panel
01-227-4977
Aircraft Fairing
Used on f-14 aircraft.
01-227-4978
Structural Component Air Support
26.000" overall length 6.000" overall width 0.018" material thickness
01-227-4979
Structural Component Air Support
0.018" material thickness
01-227-4980
Structural Component Air Support
01-227-4986
Structural Aircraft Panel
Used on acft model e-3a. consist of 1 beaded doubler, 1 skin, 1 lwr doubler, 1 upp doubler; nha 65-3495; located at sta 146.78 to 169.08; opposite p/n -2
01-227-4987
Structural Aircraft Panel
01-227-4988
Structural Aircraft Panel
01-227-4995
Aircraft Leading Edge
96.000" overall length 4.000" overall width 0.010" material thickness
01-227-4996
Aircraft Leading Edge
96.000" overall length 4.000" overall width 0.010" material thickness
01-227-6612
Fuel Tank Aircraft Regulator
01-227-6651
Structural Aircraft Plate
01-227-6652
Structural Aircraft Plate
01-227-6656
Structural Component Air Support
Used on acft model kc-135. 7075-T73 aluminum die forging per BMS7-186; finish f-2.20; nha 458-58024
01-227-6657
Structural Component Air Support
Used on acft model kc-135. 2024-0 extruded aluminum per qq-a-200/3; heat treat T42; finish f-2.59; stock alter AND10134-2405 by 1.1
