01-155-6392
Aircraft Former
3.200" overall length 2.500" overall width 0.040" material thickness as channel
01-155-6393
Aircraft Former
As channel
01-155-6394
Aircraft Former
32.000" overall length 2.200" overall width 0.032" material thickness as angle
01-155-6601
Structural Component Air Bracket
Used on s-70c-2 aircraft.
01-155-6610
Bell Crank
0.2495" bore diameter
01-155-6613
Bell Crank
0.2500" bore diameter fork at bb arm end has 3 prongs, distance between forks
01-155-6787
Access Aircraft Door
01-155-6788
Access Aircraft Door
01-155-6789
Access Aircraft Door
01-155-6876
Structural Aircraft Plate
12.000" overall length 11.000" overall width 0.040" material thickness
01-155-6877
Structural Aircraft Plate
Used on B-52. 2.200" overall length 0.600" overall width 0.120" material thickness material BAC1521-120
01-155-6878
Structural Aircraft Plate
Used on b-52 acft. matl al alloy, qq-a-287, 7075-0; matl size 0.063 by 2.100 by 3.600 in. lg; opposite to p/n 26-1922-2; used as stiffener angle frame station 85.27, nose cowl
01-155-6879
Structural Aircraft Plate
Used on b-52 acft. matl al alloy, qq-a-287, 7075-0; matl size 0.063 by 2.100 by 3.600 in. lg; opposite to p/n 26-1922-1; used as stiffener angle on frame station 85.27, nose cowl
01-155-6880
Structural Aircraft Plate
Used on b-52 acft. matl al alloy, qq-a-287, 7075-0; matl size 0.063 by 2.100 by 4.100 in. lg; opposite to p/n 26-1922-4; used as stiffener angle on frame station 85.27, nose cowl
01-155-6881
Structural Aircraft Plate
Used on b-52 acft. matl al alloy, qq-a-287, 7075-0; matl size 0.063 by 2.100 by 4.100 in. lg; opposite to p/n 26-1922-3; used as stiffener angle on frame station 85.27, nose cowl
01-155-6882
Structural Aircraft Plate
Used on b-52 acft. matl al alloy, qq-a-318, 5052-0; 0.040 by 5.000 by 5.000 in. lg; opposite to p/n 25-2617-5; used as collar on doubler installation nose cowl
01-155-6883
Structural Aircraft Plate
Used on b-52 acft. matl al alloy, qq-a-362, 2024-0; matl size 0.063 by 5.000 by 6.000 in. lg; opposite to p/n 25-2617-1; used as doubler on nose cowl
01-155-6884
Structural Aircraft Plate
9.100" overall length 2.500" overall width 0.020" material thickness used as doubler
01-155-6885
Structural Component Air Support
2.800" overall length 2.400" overall width 0.040" material thickness opp 39-14611-11; used as gusset on cowl body panel
01-155-6886
Structural Component Air Support
3.100" overall length 2.100" overall width 0.063" material thickness opp 39-14611-14; used as gusset on cowl body panel
01-155-6887
Structural Component Air Support
3.100" overall length 2.100" overall width 0.063" material thickness opp 39-14611-13; used as gusset on cowl body panel
01-155-6888
Structural Component Air Support
2.600" overall length 1.400" overall width 0.040" material thickness opp 39-14611-18; used as frame attachment on cowl body panel
01-155-6889
Structural Component Air Support
2.600" overall length 1.400" overall width 0.040" material thickness opp 39-14611-17; used as frame attachment on cowl body panel
01-155-6890
Structural Component Air Support
2.500" overall length 1.400" overall width 0.040" material thickness opp 39-14611-20; used as frame attachment on cowl body panel
01-155-6891
Structural Component Air Support
2.000" overall length 1.400" overall width 0.040" material thickness opp 39-14611-1; used as frame attachment on cowl body panel
01-155-6892
Structural Component Air Support
2.000" overall length 1.400" overall width 0.040" material thickness opp 39-14611-19; used as frame attachment on cowl body panel
01-155-6903
Aircraft Former
20.300" overall length 1.900" overall width 0.020" material thickness
01-155-6904
Aircraft Former
Opposite pn 35-8227-881
01-155-6906
Fuselage Section
01-155-6908
Aircraft Pylon
01-155-6909
Aircraft Pylon
01-155-7014
Aircraft Windshield Panel
01-155-8195
Structural Aircraft Panel
Used on B-52. 33.000" overall length 24.400" overall width
01-155-8196
Structural Aircraft Plate
2.000" overall length 1.300" overall width 0.025" material thickness
01-155-8197
Structural Aircraft Plate
2.200" overall length 1.600" overall width 0.032" material thickness
01-155-8198
Structural Aircraft Plate
2.200" overall length 1.600" overall width 0.032" material thickness
01-155-8199
Structural Aircraft Plate
2.200" overall length 0.600" overall width 0.032" material thickness
01-155-8200
Structural Aircraft Plate
31.800" overall length 5.700" overall width 0.020" material thickness
01-155-8201
Structural Aircraft Plate
31.800" overall length 5.700" overall width 0.020" material thickness
01-155-8202
Structural Aircraft Plate
31.000" overall length 1.100" overall width 0.032" material thickness
01-155-8203
Structural Aircraft Plate
21.200" overall length 0.900" overall width 0.025" material thickness
01-155-8204
Structural Aircraft Plate
Used on B-52. 2.000" overall length 2.000" overall width 0.060" material thickness stock BAC1524-62
01-155-8205
Structural Aircraft Plate
Used on B-52. stock size BAC1511-161 x 24.600 in lg
01-155-8206
Structural Aircraft Plate
Used on B-52. stock size BAC1511-161 x 24.500 in. lg
01-155-8207
Structural Aircraft Plate
2.900" overall length 1.600" overall width 0.040" material thickness
01-155-8208
Structural Aircraft Plate
22.800" overall length 1.900" overall width 0.020" material thickness
01-155-8209
Structural Aircraft Plate
2.400" overall length 0.600" overall width 0.032" material thickness
01-155-8210
Structural Aircraft Plate
3.600" overall length 0.800" overall width 0.040" material thickness
