01-570-5916
Structural Component Air Support
140.010" overall length attach angle finnish per f-1-1
01-570-5918
Aircraft Truss Assembly
01-570-5923
Structural Component Air Support
Cap make from LS60337-1
01-570-5930
Structural Component Air Fitting
01-570-6072
Aircraft Stringer
Used on s-70a, uh-60a, uh-60l, uh-60m. stringer
01-570-6073
Aircraft Stringer
Used on s-70a, uh-60a, uh-60l, uh-60m. stringer
01-570-6074
Aircraft Fairing
Used on s-70a, s-70c, uh-60a. fairing
01-570-6075
Aircraft Stringer
Used on s-70a, uh-60a, uh-60l, uh-60m. stringer
01-570-6076
Aircraft Stringer
Used on s-70a, uh-60a, uh-60l, uh-60m. skin
01-570-6803
Structural Component Air Support
Used on awacs nato e-3a aircraft.
01-570-6807
Structural Aircraft Plate
Used on awacs nato e-3a aircraft.
01-570-7093
Structural Component Air Fitting
Used on RAPTOR.
01-570-7094
Structural Component Air Fitting
Used on RAPTOR.
01-570-7095
Structural Component Air Fitting
Used on RAPTOR.
01-570-7181
Stiffener Aircraft Rib
01-570-7705
Structural Component Air Support
Used on c-130 h acft. 143.000" overall length attach angle u/o MEP15z; next assy 3337825; -2 opposite; final cond-T76; fin code f-19-19; dim. are stocksize matl; matl size or shape LS60374-1 x 143
01-570-7845
Structural Component Air Support
Used on c-130 h acft. 143.000" overall length attach angle opposite 3337877-1; matl size or shape LS60374-1 x 143; next assy 3337825; finial cond T76; u/o MEP15z; fin code f-19-19
01-570-7864
Structural Component Air Fitting
Used on c-130h acft. wing joint fitting 390620-6 opposite; m/f 390617-991
01-570-7918
Structural Component Air Support
Used on c-130h acft. 143.000" overall length attach angle next assy 3337190; matl size/shape LS60374-1 x 143; final cond T76; finish code f-1-1; opposite 3337191-1
01-570-7998
Aircraft Frame
Used on c-130h acft. frame assy finish code f-1-1; c/o shims, reinforcing plate, caps, nuts, pins
01-570-8000
Aircraft Frame
Used on c-130h acft. frame assy finish code f-1-1; c/o shims, reinforcing plate, caps, nuts, pins
01-570-8007
Aircraft Truss Assembly
Used on c-130 acft. truss assy m/f 3336492-992; final cond T74; c/o 1 truss, barrel muts, retainers, insert, bushing; finish per LAC0471
01-570-8280
Fuel Cell Aircraft Plate
Fuel cell graphite plate serpentine flow 50CM2 bi-polar
01-570-8281
Fuel Cell Aircraft Plate
Fuel cell graphite plate serpentine flow 50CM2 inlet
01-570-8282
Fuel Cell Aircraft Plate
Fuel cell graphite plate serpentine flow 50CM2 outlet
01-570-8283
Fuel Cell Aircraft Plate
Fuel cell end plate aluminum end plate for 50CM2
01-570-8284
Fuel Cell Aircraft Plate
Fuel cell end plate gold plated current collector copper plate for 50CM2
01-570-8297
Access Aircraft Cover
01-570-8543
Wing Parts Kit
Used on kc-135 acft. kit, aft terminal fitting used as wing terminal assy
01-570-8891
Structural Component Air Fitting
Used on RAPTOR.
01-570-9153
Structural Component Air Bracket
01-570-9154
Structural Component Air Bracket
01-570-9252
Structural Component Air Fitting
Used on f-22 raptor acft. nha 5HF42064-141
01-570-9502
Structural Component Aircraf Web
01-570-9519
Aircraft Stiffener
01-570-9537
Structural Component Air Support
01-570-9566
Aircraft Stiffener
01-570-9696
Structural Component Air Support
Used on kc-135 acft. support fitting-boom pivot f-2.30; c/o 1 support ftg, 1 bearing plate assy, 2 screw 100 degree hd; m/f 5-89094; penetrant inspect per BAC5423
01-570-9706
Aircraft Skin
Used on 1520013558250. skin goes on stabilator assy
01-570-9797
Aircraft Stiffener
01-570-9801
Aircraft Stiffener
01-570-9803
Structural Component Air Support
Used on kc-135 acft. 27.000" overall length 3.800" overall width 0.064" material thickness support, seal plate used on 5-86025; clad 2024-0 sht; 0 temp; heat treat T4; opposite 90-4540-4; finish srf 2.115
01-570-9806
Aircraft Stiffener
01-570-9813
Structural Component Air Support
Used on kc-135 stratotanker acft. 6.500" overall length 6.000" overall width 0.051" material thickness pan-support finish f-2.115; T4 heat treat; opposite 9-61950-6; clad 2024-0 sht; 0 temp; dim. are stocksize matl.
01-570-9832
Structural Component Air Support
Used on 1520013558250. 11.200" overall length 0.032" overall width vane the vane is an airframe part that is located on top of the engine nacelle, kind of a support rib
01-570-9863
Structural Aircraft Panel
01-570-9971
Aircraft Bulkhead
01-571-0078
Structural Component Air Fitting
Used on f-22 raptor acft. nha 5HF4264-139
01-571-0133
Structural Component Air Support
Used on 1520013558250. 20.700" overall length 0.020" overall width vane the vane sits on top of the engine nacelle
01-571-0419
Structural Aircraft Panel
