01-151-5912
Aircraft Former
2.700" overall length 1.700" overall width 0.032" material thickness opposite -850
01-151-5913
Aircraft Former
2.700" overall length 1.700" overall width 0.032" material thickness opposite -849
01-151-5914
Aircraft Former
11.600" overall length 1.500" overall width 0.500" material thickness opposite -856
01-151-5915
Aircraft Former
11.600" overall length 1.500" overall width 0.500" material thickness opposite -855
01-151-5916
Aircraft Former
4.200" overall length 3.400" overall width 0.032" material thickness opposite -858
01-151-5917
Aircraft Former
4.200" overall length 3.400" overall width 0.032" material thickness opposite -857
01-151-5918
Aircraft Former
4.700" overall length 1.500" overall width 0.032" material thickness opposite -860
01-151-5919
Aircraft Former
4.700" overall length 1.500" overall width 0.032" material thickness opposite -859
01-151-5921
Aircraft Leading Edge
01-151-5923
Aircraft Skin
Used on B-52. 12.000" overall length 8.500" overall width
01-151-5924
Aircraft Skin
Used on B-52. 34.000" overall length 24.000" overall width annealed
01-151-5925
Aircraft Skin
Used on B-52. 34.000" overall length 24.000" overall width annealed
01-151-6547
Access Aircraft Door
Used on rf-4c aircraft. used for camera access, forward, retrofit
01-151-6586
Aircraft Engine Build- Parts Kit
Used on uh-60a helicopter.
01-151-6604
Aircraft Fairing
01-151-6605
Aircraft Bulkhead
31.000" overall length 14.000" overall width 0.040" material thickness
01-151-6606
Aircraft Bulkhead
24.000" overall length 19.000" overall width 0.040" material thickness
01-151-6607
Aircraft Bulkhead
01-151-6626
Structural Aircraft Plate
Used on f-4 aircraft. used as doubler on trailing edge assembly, aileron; matl-7075-T6 qq-a-250/12 cond T6; dimensions-12.900 in. lg, 1.400 in. w, 0.032 in. thk
01-151-6627
Structural Aircraft Plate
Used on f-4 aircraft. used as doubler on trailing edge assembly, aileron; matl-7075-T6 qq-a-250/12 cond T6; dimensions-14.500 in. lg, 1.400 in. w, 0.032 in. thk
01-151-6628
Structural Aircraft Plate
Used on f-4 aircraft. used as doubler on trailing edge assembly, aileron; matl-7075-T6 qq-a-250/12 cond T6; dimensions-54.100 in. lg, 1.800 in. w, 0.032 in. thk
01-151-6629
Structural Aircraft Plate
2.600" overall length 0.500" overall width 0.032" material thickness optional spec bms 7-7c
01-151-6630
Structural Aircraft Plate
2.500" overall length 0.600" overall width 0.032" material thickness optional spec bms 7-7c
01-151-6631
Structural Aircraft Plate
25.000" overall length 2.000" overall width 0.025" material thickness
01-151-6632
Structural Aircraft Plate
Used on acft model b52. do not use cadmium plated tools on this item, 0.025 in.thk, 1.500 in.w, 10.100 in.lg, used on tail fairing, left hand, inboard strut
01-151-6633
Structural Aircraft Plate
11.800" overall length 2.500" overall width 0.050" material thickness
01-151-6634
Structural Aircraft Plate
3.900" overall length 3.800" overall width 0.050" material thickness
01-151-6635
Structural Aircraft Plate
Used on B-52. opposite pn 25-2345-47
01-151-6636
Structural Aircraft Plate
3.900" overall length 3.800" overall width 0.050" material thickness
01-151-6637
Structural Aircraft Plate
Used on B-52. opposite pn 25-2345-53
01-151-6638
Structural Aircraft Plate
22.000" overall length 9.600" overall width 0.050" material thickness finish f-2.115; tempered to T3; functions as shear plate
01-151-6639
Structural Aircraft Plate
7.300" overall length 1.600" overall width 0.040" material thickness used on -516, -522
01-151-6640
Structural Aircraft Plate
10.500" overall length 1.700" overall width 0.040" material thickness used on -516, -522
01-151-6641
Structural Aircraft Plate
6.500" overall length 1.500" overall width 0.040" material thickness functions as doubler; finish f-2.115; tempered to T3
01-151-6642
Structural Aircraft Plate
3.000" overall length 1.700" overall width 0.012" material thickness opposite pn -879
01-151-6643
Structural Aircraft Plate
39.000" overall length 2.500" overall width 0.012" material thickness opposite -518; finish f-8.05; functions as seal
01-151-6644
Structural Aircraft Plate
45.800" overall length 32.000" overall width 0.016" material thickness used on -522
01-151-6645
Structural Aircraft Plate
Used on B-52. matl BAC1530 .4 x 9.4 in.; used on -545
01-151-6646
Structural Aircraft Plate
9.500" overall length 1.000" overall width 0.025" material thickness annealed, class 6 optional; finish f-10.10; commercially pure
01-151-6647
Structural Aircraft Plate
12.000" overall length 8.500" overall width 0.040" material thickness
01-151-6648
Structural Aircraft Plate
3.400" overall length 1.200" overall width 0.050" material thickness
01-151-6649
Structural Aircraft Plate
3.000" overall length 1.700" overall width 0.012" material thickness opposite p/n -878
01-151-6650
Aircraft Fairing
C/o 293 component parts
01-151-6651
Aircraft Fairing
C/o 293 component parts
01-151-6653
Structural Component Air Support
4.200" overall length 3.300" overall width 0.063" material thickness
01-151-6654
Structural Component Air Support
4.200" overall length 3.300" overall width 0.063" material thickness
01-151-6655
Structural Component Air Support
Used on acft model b52. al clad 2024-0 per qq-a-250/5, 0.071 in.thk, 1.800 in.w, 10.000 in.lg, left hand, used on tail fairing, station 245.30
01-151-6656
Structural Component Air Support
5.900" overall length 2.800" overall width 0.050" material thickness AISI301 per mil-s-5059, 1/4 hard
01-151-6657
Structural Component Air Support
4.100" overall length 2.300" overall width 0.020" material thickness do not use cadmium plated tools on this item, titanium ams 4901
01-151-6658
Structural Component Air Support
4.100" overall length 2.300" overall width 0.020" material thickness do not use cadmium plated tools on this item, titanium ams 4901
