01-538-0241
Structural Aircraft Plate
1.800" overall length 1.800" overall width 0.220" material thickness filler taper cadmium surface treated
01-538-0243
Structural Component Air Bracket
Used on b-52 stratofortress. gap cover lnha 520-13599; -3 opposite; -4 consists of 1ea 26-2001 slide assy; 1 ea 26-2002-801 fitting; 1 ea 520-13601-4 bracket; 1 ea 520-13602-10, -11, -12, -8, clip; 4 ea MS20426D4-7 rivet solid; 8 ea MS20470D5-6 rivet solid
01-538-0255
Structural Component Air Bracket
Used on b-52 stratofortress. gap cover nha 520-13599; -6 opposite; -5 consists of 1 ea 26-5312 slide assy; 1 ea 26-5313 retainer; 1 ea 520-13601-5 bracket; 1 EA520-13602-13, -15, -17, -18, clip; 4 ea MS20426D4-7 rivet solid; 8 ea MS20470D5-6 rivet solid
01-538-0265
Structural Component Air Support
01-538-0269
Structural Component Air Support
01-538-0278
Structural Component Air Support
01-538-0308
Structural Component Air Bracket
Used on b-52 stratofortress. gap cover nha 520-13599; -5 opposite; -6 consists of 1ea 26-5312 slide assy; 1ea 26-5313 retainer; 1 ea 520-13601-6 bracket; 1 ea 520-13602-14, -16, -17, -18, clip; 4 ea MS20426D4-7 rivet solid, 8 ea MS20470D5-6 rivet solid
01-538-0320
Structural Component Air Bracket
Used on b-52 stratofortress. gap cover nha 520-13599; consists of gap cover assy, slide asswmbly, fitting, bracket, clips
01-538-0340
Aircraft Skin
Skin
01-538-0346
Structural Component Air Bracket
Used on b-52 stratofortress. gap cover nha 520-13599; consists of gap cover assy, slide assembly, fitting, bracket, clips
01-538-0360
Structural Component Air Bracket
Used on nose gear aft closure assembly for harrier. clip
01-538-0380
Structural Aircraft Plate
Used on upper bulkhead.
01-538-0381
Aircraft Fairing
Fairing-assy of
01-538-0382
Aircraft Fairing
Fairing assy of
01-538-0388
Aircraft Bulkhead
Used on aft fuselage. 9.180" overall length
01-538-0537
Structural Aircraft Panel
Used on f-22 raptor. ref cover assy, 4 coating appl, 2 label
01-538-0538
Aircraft Door
Used on f-22 raptor.
01-538-0539
Aircraft Door
Door instl c/o 4 coatings, 2 labels, 1 filler
01-538-0749
Thermal Aircraft Insulation
Insul covering film spec douglas dms 2450 c type 2, boeing bms 8-360 type 1
01-538-0855
Aircraft Windshield Panel
Main windshield, rh
01-538-0862
Aircraft Stiffener
Used on p3 orion aircraft. next higher assembly lower internal structure; extrusion aluminum alloy; technical document navair 01-75paa-3-1
01-538-0871
Aircraft Windshield Panel
Main windshield, lh
01-538-0884
Structural Aircraft Panel
01-538-0896
Structural Component Air Bracket
01-538-0905
Aircraft Door
Used on f-22 raptor. c/o ref door assy, 3 coating, 2 label, 1 filler
01-538-0907
Aircraft Door
Used on f-22 raptor. c/o ref door assy; 4 coating appl; ref filler/fair seams; ref gap
01-538-0986
Airfoil Rib
Rib support
01-538-1011
Airfoil Rib
Rib rib wing pylon, nha 16W041, make from -8
01-538-1017
Wing Parts Kit
Used on B-1B. L1201051
01-538-1402
Structural Component Air Support
Used on uh-60m blackhawk helicopter, utility nsn 1520-01-492-6324. 0.750" overall length 0.750" overall width 0.125" material thickness
01-538-1575
Aircraft Hinge
01-538-1660
Aircraft Door
Used on f-22 raptor. door
01-538-1661
Structural Aircraft Plate
01-538-1662
Structural Aircraft Plate
Used on f-22 raptor. plate
01-538-1665
Access Aircraft Door
Used on f-22 raptor. door-service
01-538-1666
Structural Aircraft Plate
Used on f-22 raptor. seal
01-538-1667
Structural Aircraft Plate
Used on f-22 raptor. seal
01-538-1694
Aircraft Door
01-538-1737
Structural Component Air Support
01-538-1755
Structural Component Air Support
01-538-1770
Structural Component Air Support
01-538-1776
Structural Component Air Support
01-538-1794
Structural Component Air Support
Used on b-52 stratofortress. gap cover support for spares replacement, 520-13599-1 optional to 25-2781-1; -2 is opposite; includes 24 ea 23-1627 washer, 1 ea 520-13600-1, -3, -5, -6, -7-8 gap covers, 24 ea BACB30LM3-11 bolt, 24 ea MS21042L3 nut
01-538-1870
Airfoil Rib
Used on c/kc-135 stratotanker. 8.600" overall length 5.100" overall width 0.040" material thickness nose rib matl al aly 7075 T73 per ams-qq-a-250/12, dim are stock matl
01-538-1874
Airfoil Rib
Used on KC-135. 8.600" overall length 5.800" overall width 0.040" material thickness nose rib used on 5-88190
01-538-1946
Structural Aircraft Panel
Used on tristar aircraft. edge assembly, elevator sta technical document da P101b-5100-3a
01-538-1976
Structural Component Air Bracket
01-538-1977
Structural Component Air Support
