01-113-6996
Aircraft Channel
Used on f-15a/tf-15a. 7.400" overall length 4.600" overall width 0.063" material thickness function-rib-rear, forward; matl-6al-4v per mil-t-9046 type iii comp-c, cond-annealed
01-113-6998
Aircraft Channel
Used on f-15a/tf-15a. 9.000" overall length 5.480" overall width 0.056" material thickness function-spar to rib-intermediate, lower aft; matl-6al-4v per mil-t-9046 type iii comp-c, cond-annealed
01-113-7011
Structural Aircraft Panel
Used on c-5a aircraft. 79.750" overall length 20.000" overall width
01-113-7017
Aircraft Former
14.650" overall length 3.350" overall width 0.080" material thickness do not use cadmium plated tools on this item
01-113-7020
Airfoil Rib
4.000" overall length 4.000" overall width 0.040" material thickness
01-113-7021
Airfoil Rib
4.000" overall length 4.000" overall width 0.040" material thickness
01-113-7022
Airfoil Rib
4.000" overall length 4.000" overall width 0.040" material thickness
01-113-7023
Airfoil Rib
4.000" overall length 4.000" overall width 0.040" material thickness
01-113-7024
Airfoil Rib
4.000" overall length 4.000" overall width 0.040" material thickness
01-113-7025
Airfoil Rib
4.000" overall length 4.000" overall width 0.040" material thickness
01-113-7026
Airfoil Rib
20.150" overall length
01-113-7027
Airfoil Rib
20.150" overall length
01-113-7337
Structural Aircraft Panel
C/o 6 doublers
01-113-7338
Structural Aircraft Panel
C/o 6 doublers; opposite -707a
01-113-7373
Structural Component Air Bracket
2.000" overall length 1.800" overall width 0.063" material thickness finish f-8.07; matl aisi 321/347
01-113-7404
Aircraft Latch Assembly
Used on f-115 acft.
01-113-7405
Aircraft Latch Assembly
Used on f-15 acft.
01-113-7406
Aircraft Latch Assembly
Used on f-15 acft.
01-113-7460
Structural Aircraft Plate
Used on c-5 acft. matl al alloy, qq-a-250/5, 2024-T3; used on slat
01-113-7461
Structural Aircraft Plate
Used on c-5 acft. matl al alloy, qq-a-250/5, 2024-T3; used on slat
01-113-7462
Structural Aircraft Plate
Used on c-5 acft. 11.000" overall length 6.000" overall width 0.050" material thickness
01-113-7463
Structural Aircraft Plate
81.000" overall length 8.000" overall width 1.180" material thickness function-splice plate; mms-149; T851
01-113-7464
Structural Aircraft Plate
81.000" overall length 8.000" overall width 1.180" material thickness function-splice plate; mms-149; T851
01-113-7465
Structural Aircraft Plate
81.000" overall length 8.000" overall width 1.180" material thickness mms-149; cond T851
01-113-7466
Structural Aircraft Plate
81.000" overall length 8.000" overall width 1.180" material thickness mms-149; cond T851
01-113-7467
Structural Component Air Support
Used on c-5 acft. used as edge member on upper panel assy p/n 4J12293; opposite to p/n 4J10046-108b
01-113-7468
Structural Component Air Support
Used on c-5 acft. used as a shim on a slat
01-113-7469
Structural Component Air Support
Used on c-5 acft. used as a shim on a slat
01-113-7471
Structural Component Air Support
Used on c-5 acft. matl al alloy, qq-a-250/17, 7079-T6; matl size 0.020 by 1.000 by 36.000 in. lg; opposite to p/n 4J10046-703a; used on slat
01-113-7472
Structural Component Air Support
Used on c-5 acft. matl al alloy, mil-a-8923, 7079-T6; matl size 0.012 by 2.000 by 24.000 in. lg; opposite to p/n 4J10046-711a; used on slat
01-113-7473
Structural Component Air Support
Used on c-5 acft. matl al alloy, mil-a-8923, 7079-T6; 0.020 by 2.000 by 24.000 in. lg; opposite to p/n 4J1004l-709a; used on slat
01-113-7477
Structural Component Air Support
Used on f-15 acft. used as a splice, spar to rib main lower aft
01-113-7478
Structural Component Air Support
7.900" overall length 4.420" overall width 0.056" material thickness opposite to p/n 68A112187-2002
01-113-7493
Aircraft Skin
Used on c-135 and kc-135 airplane.. 30.000" overall length 14.000" overall width matt; clad sheet, heat treat per T4, finish srf-2.130
01-113-7494
Aircraft Skin
Used on c-135 and kc-135 airplane.. 30.000" overall length 14.000" overall width matt; clad sheet, finsh srf-2.130, heat treat per T4
01-113-7496
Aircraft Skin
Used on F-111. 40.000" overall length 40.000" overall width
01-113-8161
Structural Component Air Bracket
Used on uh-60l helecopter. 3.000" overall width 0.100" material thickness u/osupport instl vibration absorber forward lh 70219-02109-013; includes 2 bushings
01-113-8227
Access Aircraft Door
01-113-8388
Aircraft Trailing Edge
01-113-8390
Access Aircraft Cover
Used on acft e3a.
01-113-8433
Aircraft Latch Assembly
Used on f-15 acft.
01-113-8435
Aircraft Latch Assembly
Used on f-15 acft.
01-113-8535
Structural Aircraft Plate
01-113-8536
Structural Aircraft Plate
01-113-8537
Structural Aircraft Plate
81.000" overall length 12.000" overall width 0.750" material thickness
01-113-8538
Structural Component Air Support
Used on acft model f-16. c/o support p/n 16F1661-7, bracket p/n 16F1661-9, bracket p/n 16F1661-11, spacer p/n 16F1661-13, spacer p/n 16F1661-15, bracket p/n 16F1661-17
01-113-8544
Airfoil Rib
51.000" overall length 25.000" overall width 3.500" material thickness
01-113-8549
Aircraft Spar
01-113-9371
Access Aircraft Door
Pressure sealed
01-113-9403
Structural Aircraft Panel
C/o outer skin, inner skin, doublers, core, channel, edge member, cap, closure, plug; opposite -169c
