01-188-1605
Structural Component Air Support
01-188-1802
Access Aircraft Door
Used on b-1b aircraft. nuclear hardness critical item; p/o: door, avionics bay-fuselage; sta YF737.000 to sta YF875.500; c/o: lru door, channels, supports, door hinges, emp shield, stud nuts, retaining rings, rivets, clip & corner clip, shield, spacer; opposite -181; n/a: L3002656-232
01-188-2001
Aircraft Skin
Used on c/kc-135. 17.000" overall length 7.000" overall width srf 2.130; nha 65-13772-15
01-188-3542
Access Aircraft Door
Used on b-1b aircraft. nuclear hardness critical item; p/o: door, avionics bay-fuselage; sta YF737.000 to sta YF875.500; c/o: lru door, channels, supports, door hinges, emp shield, stud nuts, retaining rings; rivets, clip & corner clip, shield, spacer opposite -192; n/a: L3002656-241
01-188-3727
Structural Aircraft Plate
39.000" overall length internal heat shield
01-188-3728
Structural Aircraft Plate
39.000" overall length internal heat shield
01-188-3729
Structural Aircraft Plate
39.000" overall length 34.000" overall width 0.020" material thickness eff on 5c 0178, 0180, 0182, 0188, 0190, 0192, 0194; opposite -83; replaces -82 shield; nha 16B6312-8-07
01-188-3730
Aircraft Fairing
01-188-3734
Structural Component Air Support
Used on c-5 aircraft. matl-al alloy, comp 6061-T651 per qq-a-250/11; location-fitting, mounting beam, nose radome; finish-chromate per mil-c-5541, cl 3
01-188-3745
Structural Aircraft Panel
01-188-4116
Fuel Aircraft Tank
Used on acft model av-8.
01-188-5647
Attachment Molded Tank Flange
01-188-5945
Structural Component Air Fitting
1.680" overall width hanger
01-188-5953
Structural Component Air Support
Used on c-141 acft. 7075-T6 aluminum alloy per qq-a-225/9; 16.800 in. lg; 1.650 in. w; 1.600 in. h
01-188-5954
Structural Component Air Support
Used on f-15 acft.
01-188-5962
Aircraft Skin
Used on c/kc-135. 17.000" overall length 7.000" overall width srf 2.130; nha 65-13772-11
01-188-7107
Structural Aircraft Plate
Used on acft model b-1b. corrosion resistant steel type 302, annealed per qq-s-766; 2.63 in. dia, 0.030 in. thk; center section bent 45 deg, 1.63 in. dia; 2 0.383 in. dia holes in hex compresions, 0.440 in. accross flats; contain spot welded lug
01-188-7109
Structural Aircraft Plate
5.000" overall length 2.700" overall width 1.000" material thickness
01-188-7117
Structural Component Air Support
Used on f-5f acft. rear canopy mechanism support
01-188-7118
Structural Component Air Support
Used on acft model a-10a. made from 160D611603-11, 56.000 in. lg
01-188-7119
Structural Component Air Support
Used on acft model a-10a. made from 160D611603-11, 56.000 in. lg
01-188-7130
Stiffener Aircraft Rib
23.400" overall length 7.100" overall width 0.040" material thickness
01-188-7131
Airfoil Rib
23.500" overall length 7.000" overall width 0.040" material thickness heat treat T4; finish f-2.115; opposite -2; nha 5-84477
01-188-7233
Thermal Insulation Pipe Covering
F-15, eagle aircraft
01-188-8672
Structural Component Air Support
Nha L1201050; made from -009
01-188-8673
Structural Component Air Bracket
Nha L1201050; make from -009
01-188-8674
Structural Component Air Bracket
Make from -009 per PH13-8mo; nha L1201050; opp -018
01-188-8675
Structural Component Air Bracket
Make from -009; nha L1201050; opp-018
01-188-8676
Structural Component Air Bracket
Make from -009 per PH13-8mo; nha L1201050; opp -017
01-188-8677
Structural Component Air Bracket
Make from -009; nha L1201050; opp-017
01-188-8687
Structural Component Air Support
Used on c-5b acft. crank-inner door, mlg
01-188-8688
Structural Component Air Support
Used on c-5a acft.
01-188-8690
Structural Component Air Support
Used on c-5a acft.
01-188-8692
Structural Component Air Support
Used on c-5a acft.
01-188-8693
Structural Component Air Support
01-188-8694
Structural Component Air Support
Used on c-5a acft.
01-188-8695
Structural Component Air Support
Used on c-5a acft.
01-188-8696
Structural Component Air Support
Used on c-5a acft.
01-188-8698
Structural Component Air Support
Used on c-5a acft.
01-188-8699
Structural Component Air Support
Used on c-5a acft.
01-188-8705
Structural Aircraft Panel
01-188-8706
Structural Aircraft Panel
Used on c-5b acft. upper wing to fuselage fairing, fuselage station 1418 1453
01-188-8707
Structural Aircraft Panel
Used on c-5b acft. upper wing to fuselage fairing, fuselage station 1399 to 1418
01-188-8708
Structural Aircraft Panel
Used on c-5b acft. upper wing to fuselage fairing, fuselage station 1399 to 1418
01-188-8763
Radome
Used on c-5b acft.
01-188-9615
Aircraft Boom
01-189-1448
Structural Component Air Bracket
Nha L1201050; opp -020
01-189-1450
Structural Component Air Bracket
Nha L1201050; opp -019
01-189-1482
Aircraft Fairing
01-189-1484
Aircraft Fairing
