01-595-4838
Structural Component Air Fitting
01-595-4848
Aircraft Stiffener
Used on c130 amp cmb.
01-595-4860
Structural Component Air Fitting
01-595-4863
Structural Component Air Fitting
01-595-4865
Structural Component Air Fitting
01-595-4866
Structural Aircraft Plate
01-595-5042
Structural Aircraft Panel
01-595-5048
Aircraft Spar
18.000" overall length spar, front spoiler no. 2
01-595-5054
Aircraft Spar
18.000" overall length spar, front spoiler no. 2
01-595-5068
Aircraft Spar
18.000" overall length spar, front spoiler no. 2
01-595-5085
Aircraft Spar
18.000" overall length 18.000" overall width spar, front spoiler no. 2
01-595-5091
Access Aircraft Door
Used on T38.
01-595-5095
Aircraft Spar
24.5000" overall length spar, front spoiler no. 2
01-595-5102
Aircraft Spar
24.500" overall length spar, front spoiler no. 2
01-595-5123
Aircraft Spar
8.000" overall length spar, front spoiler no. 2
01-595-5130
Structural Aircraft Plate
Used on C-5. plate u/o linear actr, elmech
01-595-5134
Aircraft Spar
8.000" overall length spar, front spoiler no. 2
01-595-5143
Aircraft Spar
18.000" overall length spar, front spoiler no. 2
01-595-5146
Structural Component Air Bracket
6.000" overall length 2.250" overall width 1.500" material thickness actuator bracket assy heat treat T351; finish srf-2.30
01-595-5152
Aircraft Spar
18.000" overall length spar, front spoiler no. 2
01-595-5188
Aircraft Spar
67.700" overall length 3.000" overall width 2.000" material thickness spar, rear --spoiler no. 2 -003 opp -004
01-595-5201
Aircraft Spar
67.700" overall length 3.000" overall width 2.000" material thickness spar -004 opp -003
01-595-5218
Aircraft Skin
01-595-5239
Aircraft Skin
13.440" overall length 12.500" overall width
01-595-5240
Structural Component Air Support
Used on cap repair c-5 galaxy. 13.000" overall length 2.000" overall width 0.125" material thickness strap u/o -102a
01-595-5248
Aircraft Skin
13.440" overall length 12.500" overall width
01-595-5371
Structural Component Air Fitting
7.030" overall length 4.590" overall width aft cockpit doubler -2 opp -1; manufacture from al 2124-T851 or al 7075-T73; material thickness is not to be less than .100";
01-595-5382
Structural Component Air Fitting
7.030" overall length 4.590" overall width aft cockpit doubler -1 opp -2; manufacture from al 2124-T851 or al 7075-T73; material thickness is not to be less than .100"
01-595-5474
Stiffener Aircraft Rib
12.750" overall length 4.620" overall width 0.050" material thickness rib, closeout--spoiler no. 2
01-595-5493
Stiffener Aircraft Rib
12.750" overall length 4.620" overall width 0.050" material thickness rib, closeout--spoiler no. 2
01-595-5517
Aircraft Frame
Used on b-2 aircraft.
01-595-5527
Stiffener Aircraft Rib
11.500" overall length 4.500" overall width 0.050" material thickness rib, closeout--spoiler no. 2
01-595-5539
Stiffener Aircraft Rib
11.500" overall length 4.500" overall width 0.050" material thickness rib, closeout--spoiler no. 2
01-595-5625
Access Aircraft Door
Used on c-130 aircraft. door-access, liquid oxygen fill, rh u/o mlg fwd fairing assy
01-595-5651
Aircraft Truss Assembly
01-595-5668
Stiffener Aircraft Rib
12.400" overall length 4.000" overall width 0.080" material thickness rib, intmd, spoiler no. 2 -001 opp -002
01-595-5683
Stiffener Aircraft Rib
12.400" overall length 4.000" overall width 0.080" material thickness rib, intmd, spoiler no. 2 -002 opp -001
01-595-5697
Stiffener Aircraft Rib
11.900" overall length 4.000" overall width 0.080" material thickness rib, intmd, spoiler no. 2 -011 opp -012
01-595-5713
Stiffener Aircraft Rib
11.900" overall length 4.000" overall width 0.080" material thickness rib, intmd, spoiler no. 2 -012 opp -011
01-595-5725
Structural Aircraft Plate
Used on B-52. 1.700" overall length 1.200" overall width 0.080" material thickness filler finish cadmium plate per qq-p-416, type ii class ii; ht-tr 10-200 ksi; bms 7-34 anld cadmium surface treated
01-595-5870
Stiffener Aircraft Rib
11.750" overall length 4.000" overall width 0.080" material thickness rib, intmd, spoiler no. 2 -021 opp -022
01-595-5879
Stiffener Aircraft Rib
11.750" overall length 4.000" overall width 0.080" material thickness rib, intmd, spoiler no. 2 -022 opp -021
01-595-5890
Stiffener Aircraft Rib
11.250" overall length 4.000" overall width 0.080" material thickness rib, intmd, SP0iler no. 2 -031 opp -032
01-595-5891
Aircraft Stiffener
Used on b-52 aircraft. 23.000" overall length 6.000" overall width 0.050" material thickness channel stiffener fin. f-2.16; ht alum to T42 per AMS2770.opposite -19; 0 al alloy clad sh
01-595-5914
Stiffener Aircraft Rib
11.250" overall length 4.000" overall width 0.080" material thickness rib, intmd, spoiler no. 2 -032 opp -031
01-595-5918
Aircraft Stiffener
Used on b-52 acft. 23.000" overall length 6.000" overall width 0.050" material thickness channel stiffener finish f-2.16; ht al to T42 per AMS2770; 0 al alloy clad sh; opposite -20
01-595-5973
Structural Aircraft Panel
01-595-5984
Access Aircraft Door
01-595-5986
Access Aircraft Cover
01-595-5991
Aircraft Trailing Edge
Trailing edge, no. 2---spoiler -011 opp -012
