01-174-0744
Structural Component Air Support
Used on f-4 acft. matl AMS5520; 1.375 in. od; 0.500 in. lg; 0.030 in. thk; used as cup to repair stabilator inboard trailing edge panel
01-174-0745
Structural Component Air Support
Used on f-4 acft. matl al alloy, qq-a-367, 7075-T6; 5.620 in. lg; 0.165 in. dia holes, 8 places; used as fitting on lower longeron cfs 28.630
01-174-0746
Structural Component Air Support
Used on f-4 acft. matl AMS5520; 0.1875 in. od; 3.000 in. lg; 0.020 thk wall; clindrical shaped; used as a pin-tubular to repair stabilator inboard trailing edge panel
01-174-0747
Structural Component Air Support
Used on f-4 acft. matl AMS5520; clindrical shaped; 2.250 in. lg; 0.250 in. od; 0.030 in. thk wall; used as pin-tubular to repair stabilator inboard trailing edge panel
01-174-0748
Structural Component Air Support
Used on acft model b-1b. cres bar PH13-8M0, per ST0160LB0013; heat treat per ST0111LA0008 to cond h 1100; finish per 60HA02; 8.50 in. long, 2.50 in. wide, 2.00 in. thick; nha L3300150
01-174-0749
Structural Component Air Support
Used on acft model b-1b.
01-174-0750
Structural Component Air Support
Used on acft model b-1b. al alloy die forging 7075-T73 per ST0170LB0043; finish 10AB02; nha L3300316
01-174-0751
Structural Component Air Support
Used on acft model b-1b.
01-174-0752
Structural Component Air Support
Used on acft model b-1b. anl steel forging HP9-4-20 per LB0160-180; finish per 31AB02; nha L3300316
01-174-0753
Structural Component Air Support
Used on acft model b-1b.
01-174-0754
Structural Component Air Support
Used on acft model b-1b. cres bar PH13-8M0, per ST0160LB0013; heat treat per ST0111LA0008 to cond h 1100; finish per 60HA02; 8.50 in. long, 2.50 in. wide, 2.00 in. thick; nha L3300150
01-174-0765
Structural Aircraft Panel
C/o panel assy, p/n 4F11062-101a
01-174-0766
Structural Aircraft Panel
C/o panel assy, p/n 4F11079-101a
01-174-0767
Structural Aircraft Panel
6.000" overall length 6.000" overall width c/o panel assy, p/n 4F11070-101a; doubler, 2; doubler
01-174-0768
Structural Aircraft Panel
11.000" overall length 11.000" overall width c/o panel assy, p/n 4F11063-101a; doubler, 2, p/n 4F11052-213a; doubler
01-174-0769
Structural Aircraft Panel
C/o panel assy, p/n 4F11056-101a; doubler, 2, p/n 4F11052-209a; doubler matl titanium, mil-t-9046a; ti-6al-4vannealed; doubler matl size 0.063 by 6.000 by 11.000 in. lg
01-174-0770
Structural Aircraft Panel
C/o panel assy, p/n 4F11072-101a
01-174-0771
Structural Aircraft Panel
C/o core; face sheet, lower; face sheet, upper; reinforcement, 2; face sheet matl al alloy, qq-a-250/18, 7075-T6 clad 1 side; core matl mil-c-7438; 23.950 in. wi; 59.910 in. lg
01-174-0772
Structural Aircraft Panel
C/o core; face sheet, upper; face sheet, lower; reinforcement, 3; doubler; core matl mil-c-7438; face sheet, alalloy, qq-a-250/18, 7075-T6 clad 1 sheet; 19.910 in. lg; 11.950 in. w
01-174-0773
Structural Aircraft Panel
Used on C-5B. c/o core; face sheet, upper; face sheet, lower; reinforcement, 4; face sheet matl al alloy, qq-a-250/18 7075-T6 clad 1 side; core matl mil-c-7438; 39.910 in. lg; 30.010 in. w
01-174-0774
Structural Aircraft Panel
Used on c-5b acft. c/o doubler, 8; panel assy p/n 4F11057-101a; doubler matl al alloy, qq-a-250/12, 7075-T6 bare; used as panel assy-floor relief crew compartment
01-174-0775
Structural Aircraft Panel
Used on c-5b acft. c/o doubler 4F11051-179a; panel assy p/n 4F11056-101a; doubler matl al alloy qq-a-250/12, 7075-T6 bare; used as panel assy, floor, relief crew compartment
01-174-0776
Structural Aircraft Panel
C/o doubler, 2, p/n 4F11051-185a; panel assy, p/n 4F11056-101a; doubler matl al alloy, qq-a-250/12, 7075-T6 bare
01-174-0777
Structural Aircraft Panel
C/o doubler, 4; panel assy p/n 4F11062-101a; doubler matl al alloy, qq-a-250/12, 7075-T6 bare
01-174-0778
Structural Aircraft Panel
C/o doubler, 2, p/n 4F11051-159a; panel assy p/n 4F11063-101a; doubler matl al alloy, qq-a-250/12, 7075-T6
01-174-0779
Structural Aircraft Panel
C/o doubler, 4, p/n 4F11051-159a; panel assy, p/n 4F11058-101a; doubler matl al alloy, qq-a-250/12, 7075-T6 bare
01-174-0780
Structural Aircraft Panel
Panel assy, p/n 4F11068-101a
01-174-0781
Structural Aircraft Panel
C/o doubler, 2, p/n 4F11053-187a; panel assy, p/n 4F11071-101a; doubler matl al alloy, qq-a-250/13, 7075-T6 clad
01-174-0782
Structural Aircraft Panel
C/o doubler, 4, p/n 4F11053-189a; panel assy, p/n 4F11071-101a; doubler matl mil-t-9046, T1-6al-4v annealed
01-174-0783
Structural Aircraft Panel
Panel assy p/n 4F11073-101a; doubler, 2; doubler matl al alloy, qq-a-250/13, 7075-T6 clad
01-174-0784
Structural Aircraft Panel
C/o doubler, 2; panel assy, p/n 4F11076-101a; doubler matl mil-t-9046
01-174-0788
Aircraft Former
01-174-0789
Longeron
Used on c-135 acft. location-t/c forward fairing nacelle assy; fsc application data:aircraft structural component;
01-174-0790
Longeron
Used on F-15.
01-174-0791
Longeron
Used on F-15.
01-174-0793
Aircraft Skin
Used on c-135 acft. location-t/c forward fairing nacelle assy, aft
01-174-1458
Inner Wing Section
Used on aircraft model f-18. cognizant service:navy;
01-174-1459
Attachment Molded Tank Flange
01-174-1574
Access Aircraft Door
Used on acft model c-135. used on door assy-trailing edge fairing inbd strut; -603 c/o plate (2) stock sz-.032X4.7X4.7, matl 2024-T3 aluminum bare sh per qq-a-250/4, ht TREATT81; gasket (2) stock sz-.032X4.7X4.7, matl cork-rubber per mil-c-6183 medium type ii-class 1; window (2) stock sz .25X4.7X4.7, plastic sh heat resistant per mil-p-5425a finish a, process plastic per BAC5038; -625 panel assy (1) ; sleeve bolt (23) ; retainer ring (23)
01-174-1624
Structural Aircraft Plate
Used on acft model c-135.
01-174-1625
Structural Aircraft Plate
Used on acft model c-135.
01-174-1626
Structural Component Air Support
Used on f-4 acft. matl AMS5520; 2.250 in. lg; 0.1875 in. od; 0.020 in. thk; clindrical shaped; used as a pin-tubular repair on stabilator inboard trailing edge panel
01-174-1627
Structural Component Air Support
Used on f-4 acft. matl AMS5520; 1.250 in. lg; 0.1875 in. od; 0.020 in. thk; clindrical shaped; used as pin-tubular repair on staabilator inboard trailing edge panel
01-174-1628
Structural Component Air Support
C/o 1 hinge support, 2 bushing
01-174-1629
Structural Component Air Support
C/o 1 hinge support, 2 bushing
01-174-1630
Structural Component Air Support
Used on acft model c-135. c/o channel aluminum alloy per 2024-T3 qq-a-250/5
01-174-1631
Structural Component Air Support
Used on acft model c-135. c/o channel aluminum alloy per 2024-T3 qq-a-250/5
01-174-1632
Structural Component Air Support
Used on acft model c-135. c/o channel aluminum alloy per 2024-T3 qq-a-250/5
01-174-1633
Structural Component Air Support
Used on acft model c-135. c/o channel aluminum alloy per 2024-T3 qq-a-250/5
01-174-1634
Structural Component Air Support
Used on acft model c-135. c/o channel aluminum alloy per 2024-T3 qq-a-250/5
