01-541-1428
Structural Aircraft Panel
Panel
01-541-1429
Structural Aircraft Panel
Panel
01-541-1430
Structural Aircraft Panel
Panel assy matl consist of honeycomb polyamide paper, cloth glass fiber resin impregnated b-stage low heat release, foam polyurethane riged, dms 1937 type 1 grade a class 1 density 25 pcf
01-541-1431
Aircraft Fairing
Used on C-17A. 46.000" overall length 10.000" overall width 0.063" material thickness fairing c/o 1 (-32 fairing) ; make from 17P293952-18; temp T3; sheet, alclad
01-541-1433
Aircraft Fairing
Lh used on 17P2A3997-511; t.o. 1c-17a-4-53, fig 139, indx 44d
01-541-1434
Aircraft Fairing
Used on C-17A. 46.000" overall length 10.000" overall width 0.063" material thickness fairing make from 17P2A3952-18; c/o 1 (-17fairing) ; alclad sheet; temp T3
01-541-1436
Aircraft Fairing
39.000" overall length 10.000" overall width 0.063" material thickness u/o 17P2A3997-1
01-541-1437
Structural Component Air Bracket
Bracket
01-541-1760
Airfoil Rib
Rib
01-541-1779
Aircraft Fairing
01-541-1780
Aircraft Fairing
46.000" overall length 10.000" overall width 0.063" material thickness heat treat T3; m/f 17P2A3952-19
01-541-1781
Aircraft Fairing
34.000" overall length 10.000" overall width 0.063" material thickness m/f 17P2A3952-20; c/o 1 fairing; 2 clips; alt rivet; ar rivet-solid
01-541-1969
Structural Aircraft Panel
Used on AWACS.
01-541-1970
Structural Aircraft Panel
Used on AWACS.
01-541-1971
Structural Component Air Support
Used on AWACS.
01-541-1973
Structural Component Air Support
Used on AWACS.
01-541-1992
Supplemental Small Arms-fr Armor
Used on ch-47 chinook helicopter. parts for ch-47 chinook crew seat
01-541-1993
Supplemental Small Arms-fr Armor
Used on ch-47 chinook helicopter. parts for ch-47 chinook crew seat
01-541-2037
Aircraft Fairing
Used on predator. fairing
01-541-2038
Cowling
Used on predator. cowling
01-541-2045
Structural Aircraft Panel
Effectivity 17A071-124; nha 17P9B4020-1
01-541-2048
Structural Aircraft Panel
Panel assy effectivity 17A071-124; nha 17P9B4020-1
01-541-2434
Door Aircraft Parts Kit
Used on C-17A. kit used to repair or modify otbd mlg door hinges; kit consists of patch assys, 7X12 ply fabric carbon fiber woven b-stage epoxy impregnated dms TYPE2 class 2 grade c; tape patch; hinge assys; washers; nuts; bolts
01-541-2436
Access Aircraft Door
Used on C-17A. door instl hyd access; sta Y1137.500 to sta Y1160.500; -221 opp
01-541-2457
Structural Aircraft Panel
Used on C-17A. panel assy nha 17P1B1245-505; u/o-503; c/o 1 facing (.010 x noted, sheet, ALCLAD7075-0) , 1 channel (84X3x.050, cloth, glass fiber, resin impregnated b-stage, low heat release) , 16 insert, 8 insert
01-541-2458
Aircraft Door
Composite constuction
01-541-2459
Aircraft Door
Carbon/epoxy composite
01-541-2460
Door Aircraft Hinge
6.600" overall length 4.200" overall width hinge hinge assy, plate alum al 7075-T745; dim are stock matl
01-541-2461
Door Aircraft Hinge
8.800" overall length 4.250" overall width hinge plate alum al 7075-T7451; dim are stock matl
01-541-2463
Door Aircraft Hinge
7.820" overall length 4.000" overall width hinge matl plate alum al 7075-T7451; dim are stock matl
01-541-2464
Aircraft Fairing
01-541-2471
Aircraft Fairing
58.000" overall length 10.000" overall width 0.063" material thickness heat treat T3; m/f 17P2A3952-16
01-541-2472
Aircraft Fairing
Fairing make from 17P2A3952-17
01-541-2473
Aircraft Fairing
Used on C-17A. 39.000" overall length 10.000" overall width 0.063" material thickness fairing make from 17P2A3952-14; c/o 1 (-14 fairing) ; temp T3; sheet alclad
01-541-2474
Aircraft Fairing
58.000" overall length 10.000" overall width 0.063" material thickness u/o 17P2A3997-512; heat treat T3; m/f 17P2A3952-16
01-541-2607
Aileron Balance Weight
0.465" overall width m/o tungsten alloy, zinc-nickol plate per AMS2417e
01-541-2611
Aileron Balance Weight
0.645" overall width m/o tungsten alloy, zinc-nickel plate per AMS2417e
01-541-2626
Structural Component Air Support
Used on KC-135. support-assy of c/o 1 (-5 support make from 9-61176) , 2 bushing (90-9173-6, ; finish srf 2.30
01-541-2738
Aircraft Door
Door, assy
01-541-2740
Aircraft Door
Door assy
01-541-2746
Aircraft Fairing
Used on C-17A. 12.000" overall length 6.000" overall width 0.063" material thickness fairing make from -23; heat treat 0
01-541-2747
Aircraft Fairing
Used on C-17A. 12.000" overall length 6.000" overall width 0.063" material thickness fairing make from -22; heat treat 0
01-541-2754
Aircraft Fairing
Used on mh60s knighthawk. navy - fairing assembly, lh, aircraft
01-541-2784
Structural Component Air Support
Used on end item nsn: 1520-01-492-6324.
01-541-2798
Explosion Suppressa Foam Segment
Void filler matl ballistic foam thermarest AX5052-2.5, avco spec M10462
01-541-2840
Explosion Suppressa Foam Segment
Used on A-10A. 9.700" overall length 5.700" overall width void filler station 365 - 524.30
01-541-2848
Explosion Suppressa Foam Segment
Used on A-10A. 13.600" overall length 4.100" overall width void filler
01-541-2852
Explosion Suppressa Foam Segment
Void filler material to be ballistic foam thermarest AX5052-2.5 avco spec M10462
01-541-2860
Explosion Suppressa Foam Segment
Used on A-10A. 7.900" overall length 4.500" overall width void filler
01-541-2863
Explosion Suppressa Foam Segment
Void filler material to be ballistic foam, thermarest AX5052-2.5, avco spec M10462
