01-542-8915
Aircraft Intercostal
6.500" overall length 3.500" overall width 0.050" material thickness dim. are stock material
01-542-8919
Aircraft Intercostal
6.250" overall length 4.000" overall width 0.063" material thickness dim. are stock material
01-542-8925
Access Aircraft Door
Used on a-10 acft. form, fit, function
01-542-8931
Structural Component Air Support
Support, lanyard
01-542-8936
Structural Component Air Support
Support, lanyard
01-542-8957
Structural Component Air Support
Used on mv-22 aircraft. (navy) clip
01-542-8965
Structural Component Air Support
Used on mv-22 aircraft.
01-542-8969
Aircraft Door
01-542-8993
Structural Component Air Support
Cap used on -1, -77, -501
01-542-8997
Aircraft Floor
Used on C-130. 43.000" overall length 15.000" overall width panel assy nha 389091; wl 146.00; fin. per LAC0483; 5/16 in. thk; group 1; dim. are stocksize matl.
01-542-9023
Structural Component Air Bracket
Used on mv-22 aircraft. navy: bracket assy
01-542-9050
Structural Component Air Support
83.000" overall length 10.000" overall width 0.040" material thickness edge member matl al cd sh qq-a-250/13 7075-0; dim are stock matl
01-542-9056
Aircraft Door
01-542-9060
Structural Component Air Fitting
01-542-9064
Aircraft Channel
54.000" overall length 10.000" overall width 0.040" material thickness channel matl al cd sh qq-a-250/13 7075-0; dim are stock matl
01-542-9112
Structural Component Air Support
Used on e3a aircraft.
01-542-9177
Structural Component Air Support
Used on f-22 raptor.
01-542-9190
Aircraft Latch Assembly
01-542-9206
Structural Aircraft Panel
Used on C-17A. 76.000" overall length 31.000" overall width panel assy u/o -509, -511; dim. are stocksize, c/o 1 (-183 panel) , 24 plug, 24 insert; matl.aromatic polyamide paper honecomb, DMS974, type 3 class 2, grade a, 1/8 in. cell size
01-542-9207
Aircraft Fairing
Used on C-17A. fairing u/o 17P2A3997-512; make from 17P2A3952-39; heat treat T3; alclad; c/o 1 (-39 fairing) ; dim.are stocksize matl
01-542-9208
Structural Aircraft Panel
Used on f-22 raptor.
01-542-9209
Structural Aircraft Panel
Used on f-22 raptor.
01-542-9226
Structural Aircraft Panel
01-542-9227
Structural Aircraft Panel
01-542-9390
Aircraft Hinge
Used on f/a-18e/f pse: gsu test set. 21.250" overall length 2.000" overall width hinge, test point unit nha test set electronic power; test point unit
01-542-9525
Aircraft Former
Former, rib, outer wing flap
01-542-9552
Structural Component Air Support
01-542-9566
Structural Component Air Support
01-542-9862
Structural Component Air Support
3.500" overall length plug closeout plug, matl ams 4975 titanium alloy, dim are stock matl
01-542-9939
Structural Component Air Fitting
Used on ah-1w; fitting-tripod, strut, engine mount. navy-clevis
01-542-9981
Structural Component Air Fitting
Used on ah-1w;fitting-strut, tripod engine mount. navy-clevis
01-543-0079
Bleed Air Duct Assembly
Used on chinook ch-47d. duct assembly technical document 21-24-00-099
01-543-0131
Aircraft Windshield Panel
Copilot windshield technical document 56-11-10-099
01-543-0132
Aircraft Windshield Panel
Pilot windshield technical document 56-11-10-099
01-543-0180
Aircraft Fairing
Fairing
01-543-0637
Trim Aircraft Tab
Used on KC-135. stab tab, lh new design
01-543-0644
Structural Aircraft Panel
Used on f-22 raptor. panel assy, fwd lh nha 5HF71005-109; unique for air vehicle 96
01-543-0646
Access Aircraft Door
Used on C-17A. aft mount fairing pylon
01-543-0730
Aircraft Intercostal
6.250" overall length 4.000" overall width 0.050" material thickness latch back-up instl - inboard door nacelle
01-543-0742
Aircraft Former
Used on f/a-18c/d former-seal, leading edge. 7.600" overall length 3.500" overall width 0.071" material thickness navy-former
01-543-0744
Aircraft Former
Used on f/a-18c/d former-seal, leading edge. 7.600" overall length 3.500" overall width 0.071" material thickness navy-former
01-543-0746
Aircraft Former
Used on f/a-18c/d former-esal, leading edge. 5.200" overall length 3.400" overall width 0.071" material thickness navy-former
01-543-0793
Structural Aircraft Plate
Used on latch back-up instl. 4.750" overall length 1.440" overall width 0.063" material thickness latch back-up instl - inboard door nacelle heat treat T6
01-543-0834
Structural Component Air Support
Latch back-up instl inboard door nacelle heat treat T6511
01-543-0852
Structural Component Air Fitting
Used on apache helicopter, ah-d64.
01-543-0853
Structural Component Air Fitting
Used on apache helicopter, ah-d64.
01-543-0856
Aircraft Fairing
Used on apache helicopter.
01-543-0857
Aircraft Fairing
Used on apache helicopter.
01-543-0893
Airframe Modification Kit
Used on velivolo av8b.
