01-198-4938
Structural Component Air Support
Used on acft model kc-135. consists of 1 rod, 2 rod end-fork, 1 rod end-connector, 2 bolt, 2 collar, 1 nut; finish f-8.05; nha 458-52215
01-198-4964
Aircraft Former
Used on aircraft c-18a.
01-198-4965
Aircraft Former
Used on aircraft c-18a.
01-198-4966
Aircraft Former
Used on aircraft c-18a.
01-198-4967
Aircraft Former
Used on aircraft c-18a.
01-198-6277
Access Aircraft Door
7.400" outside diameter
01-198-6338
Aircraft Former
8.500" overall length
01-198-7061
Vertical Stabilizer
Used on acft model f-16.
01-198-7430
Structural Aircraft Plate
Used on acft model c-18a. nha 50-11379-5
01-198-7431
Structural Aircraft Plate
Used on acft model c-18a. nha 50-7954
01-198-7432
Structural Aircraft Plate
Used on acft model c-18a. nha 69-24929-3
01-198-7433
Structural Aircraft Plate
Used on acft model c-18a. nha 50-7990-156
01-198-7434
Structural Aircraft Plate
Used on acft model c-18a. nha-50-7990-156; used as aft side strip on center cargo door
01-198-7435
Structural Aircraft Plate
Used on acft model c-18a. nha 50-3777-3007
01-198-7436
Structural Aircraft Plate
Used on acft model kc-135. inconel 625 casting per BMS7-193; finish f-4.10; nha 65C18566
01-198-7437
Structural Aircraft Plate
Used on acft model c-18a. nha 50-7944-92; used as forward cargo door angle retainer
01-198-7439
Structural Aircraft Plate
Used on acft model kc-135. 9.1 in lg, 4.0 in wd. 0.020 in thk; finish srf 2.115; clad 2024-T3 sheet per qq-a-362, , T3 temper; nha 65-31682
01-198-7440
Structural Aircraft Plate
Used on acft model kc-135. nha 65-31682
01-198-7441
Aircraft Fairing
Nha 65-31682, 65-31683
01-198-7445
Structural Component Air Support
Used on acft model kc-135. consists of 2 guide plate, 2 tee, 2 clip, 1 support, 1 clamp, 2 nut, 2 spacer; nha 458-52215
01-198-7446
Structural Component Air Support
Used on acft model kc-135. titanium sheet commercially pure alloy spec mil-t-9046, class 6 annealedfinish srf-10.15
01-198-7457
Aircraft Former
38.000" overall length 1.800" overall width 0.032" material thickness
01-198-7458
Aircraft Former
29.000" overall length 1.900" overall width 0.032" material thickness nha 65-31682
01-198-7459
Aircraft Former
32.000" overall length 1.800" overall width 0.032" material thickness
01-198-8953
Outer Wing Section
Used on 1550-01-199-5050. 37.750 in.lg; 26.780 in.w; 3
01-198-9157
Structural Aircraft Plate
Used on acft model c-18a. nha 50-7944-92; used as forward cargo door angle retainer
01-198-9158
Structural Aircraft Plate
Used on acft model c-18a. nha 50-7944-92; used as forward cargo door angle retainer
01-198-9159
Structural Aircraft Plate
Used on acft model c-18a. nha 50-7944-92
01-198-9160
Structural Aircraft Plate
Used as: hinge arm
01-199-0326
Access Aircraft Cover
Used on f-5a aircraft. cover, electrical connector-pylon, wg sta 114.50; c/o: -3 plate (1) , pad (1) , latch-nut (2) , anchor block (2) , shim plate (2) , screw (2) , rivet (4) ;
01-199-0519
Aircraft Bulkhead
01-199-0571
Structural Aircraft Plate
2.590" overall length 0.880" overall width 0.125" material thickness
01-199-0572
Structural Aircraft Plate
Used on acft model c-18a. nha 65-29260-1; used as door bearing plate on emergency exit frame instl
01-199-0573
Structural Aircraft Plate
Used on acft model c-18a. nha 65-3300-27; used as reveal on 9.0 x 12.50 inner
01-199-0574
Structural Aircraft Plate
Used on acft model c-18a. nha 69-10768-2; used as fan cowl guide block on fan cowl support insl
01-199-0575
Aircraft Fairing
01-199-0577
Structural Component Air Support
Used on acft model c-5b. consists of 1 pad, 14 screw, 14 nuts, 1 support, 1 hinge assy, 1 trim; nha 4E32015; located at bl 2.50
01-199-0578
Structural Component Air Support
C/o 1 tubular rod, 2 rod end, 2 nut
01-199-0580
Structural Component Air Support
Used on acft model c-18a.
01-199-0582
Structural Component Air Support
Used on acft model c-18a. used as rh stabilizer elevator control crank instl
01-199-0584
Structural Component Air Support
Used on acft model c-18a.
01-199-0587
Structural Component Air Support
Used on acft model c-18a. attaching parts 2 bolts, 2 nuts; nha 65-18483-30; located at section 15
01-199-0588
Structural Component Air Support
Used on acft model c-18a.
01-199-0591
Structural Component Air Support
Used on acft model c-18a.
01-199-0598
Structural Aircraft Panel
Used on c-5b aircraft. c/o: -103a panel, size per LS60204v-a-a X22.0X42.0; nha 4E23227
01-199-0599
Structural Aircraft Panel
Used on c-5b aircraft. c/o: -103a panel, size per LS60204v-a-a X35.0X42.0; nha 4E23227
01-199-0600
Structural Aircraft Panel
Used on c-5b aircraft. c/o: -103a panel, size per LS60204v-a-a X16.0X22.0, insert (12) ; nha 4E23227
01-199-0601
Structural Aircraft Panel
Used on c-5b aircraft. c/o: -103a panel, size per LS60204v-a-a X16.0X35.0; nha 4E23227
01-199-0603
Structural Aircraft Panel
Used on c-5b aircraft. c/o: -103a panel, size LS60204v-a-a X3.0X24.0, -105a edge, matl spruce, size 1.0X1.0X24.0, insert (3) ; nha 4E23227
01-199-0604
Structural Aircraft Panel
Used on c-5b aircraft. c/o: -103a core (1) , -105a face sheet (2) , -107a doubler (2) , insert (5) ; nha 4E23227
