01-165-6018
Structural Aircraft Panel
Used on acft model b52. al clad 2024-0 per qq-a-250/5, 0.063 in.thk, 7.100 in.w, 13.100 in.lg, right hand, located from station 116 to sta 178
01-165-6019
Structural Aircraft Panel
Used on b-52 aircraft. consist of nineteen component parts
01-165-6020
Structural Aircraft Panel
Used on b-1b aircraft. consist of nine component parts
01-165-6021
Structural Aircraft Panel
Used on b-1b aircraft.
01-165-6022
Structural Aircraft Plate
Used on acft model kc-135. al alloy clad sheet 2024-T3 per qq-a-250/5; finish f-2.31; 12.450 in. lg, 3.560 in. w, 0.090 in. thk; irregular shaped; nha 35-35377
01-165-6023
Structural Aircraft Plate
Used on acft model kc-135. al alloy clad sheet 2024-T3 per qq-a-250/5; finish f-2.31; 11.900 in. lg, 7.330 in. w, 0.063 in. thk; oval shaped; 3.96 in. radius both ends, 10 0.307 in. dia holes; nha 35-35377
01-165-6024
Structural Aircraft Plate
Used on acft model kc-135. al alloy clad sheet 2024-T3 per qq-a-250/5; finish f-2.31; 4.150 in. lg, 3.400 in. w, 0.090 in. thk; irregular shaped; nha 35-35377
01-165-6025
Structural Aircraft Plate
Used on acft model kc-135. al alloy clad sheet 2024-T3 per qq-a-250/5; finish f-2.59; 6.000 in. lg, 3.000 in. w, 0.050 in. thk; nha 35-35377-502
01-165-6026
Structural Aircraft Plate
Used on acft model kc-135. al alloy clad sheet 2024-T3 per qq-a-250/5; finish f-2.59; 4.750 in. dia., 0.032 in. thk; nha 35-35377
01-165-6027
Structural Aircraft Plate
Used on acft model b-1b.
01-165-6028
Structural Component Air Support
Used on acft model kc-135. 5.6 in lg, 2.0 in wd, 0.063 in thk; finish srf-2.115; clad 2024-T3 sheet per qq-a-362, T3 temper; nha 65-12212
01-165-6029
Structural Component Air Support
Used on acft model kc-135. al alloy clad sheet 2024-T3 per qq-a-250/5; finish f-2.59; 3.000 in. lg, 3.000 in. w, 0.050 in. thk; nha 35-35377-501
01-165-6030
Structural Component Air Support
Used on acft model kc-135.
01-165-6031
Structural Component Air Support
Used on acft model kc-135. made from -2.aluminum forging 7075-T73 per BMS7-186; finish f-2.47; 4.670 in. lg, 3.422 in. o/a w, 1.200 in. o/a h; 2 0.416 in. dia holes 1.250 in. apart, counterbored .89 dia by .06 in. depth (inner surface) ; nha 65C18604
01-165-6033
Structural Component Air Support
01-165-6034
Structural Component Air Support
01-165-6035
Structural Component Air Support
Used on acft model kc-135. corrosion resistant steel 15-5ph per AMS5659; heat treated to 155-170 ksi per BAC5619; finish f-8.07 plus f-12.108 on areas with aluminum contact; c/o 1 hinge, 2 flanged bushings, 1 spacer; opposite p/n -604; nha 65C18604
01-165-6036
Structural Component Air Support
C/o 1 fitting, 3 bushing; finish f-2.47; nha 65C18604
01-165-6053
Aircraft Former
01-165-6054
Aircraft Pylon
Used on acft model a-10. c/o 11 components
01-165-6070
Cowling
Used on KC-135. nha p/n 65C18604
01-165-7080
Access Aircraft Door
Used on acft model kc-135.
01-165-7081
Access Aircraft Door
Used on acft model b-1b.
01-165-7082
Access Aircraft Door
Used on acft model b-1b.
01-165-7083
Access Aircraft Door
Used on acft model b-1b.
01-165-7158
Structural Aircraft Plate
Used on acft model b-1b.
01-165-7186
Structural Component Air Support
Used on acft model b-1b.
01-165-7190
Aircraft Skin
32.000" overall length 26.000" overall width finish A783
01-165-7191
Aircraft Skin
C/o skin, plate, rivet, sealant
01-165-9197
Access Aircraft Door
Used on f-16c/d aircraft. has latch buttons
01-165-9242
Structural Aircraft Plate
Used on f-4 aircraft. upper longeron splice fuselage station 203.00 outer; make from p/n 32-31378-7f 7075-T73 mms-136
01-165-9243
Structural Aircraft Plate
Used on f-4 aircraft. used on upper longitude f.s. 203.00 outer; make from p/n 32-31378-8f forging mms-136
01-165-9249
Structural Component Air Support
C/o 4 plate, 2 shim, 1 bushing, 1 fitting
01-166-1007
Access Aircraft Cover
Used on b-1b aircraft.
01-166-1008
Access Aircraft Cover
Used on b-1b aircraft. nuclear hardness critical item
01-166-1009
Access Aircraft Cover
Used on b-1b aircraft. on horizontal stabilizer fairing-tail warning system, yvs 262.630 to yvs 300.870
01-166-1014
Access Aircraft Door
01-166-1015
Access Aircraft Door
01-166-1016
Access Aircraft Door
Used on b-1b aircraft. nuclear hardness critical item
01-166-1017
Access Aircraft Door
Used on b-1b aircraft. nuclear hardness critical item
01-166-1018
Access Aircraft Door
Used on b-1b aircraft. nuclear hardness critical item
01-166-1020
Access Aircraft Door
Used on b-1b aircraft. nuclear hardness critical item
01-166-1134
Structural Component Air Support
Used on b1-b aircraft. oon nose radome hinge; c/o-link, MS14101-4 bearing, LD131-0022-0610 bearing; material of link-al aly plate 2024-T851 per qq-a-250/4; stock size-.320 x 5.450 lgx 1.520 w.; finished length-from centers of bearings-4.500 in.
01-166-1135
Aircraft Trailing Edge
Same as -011; effective on 82-0001
01-166-1138
Structural Aircraft Plate
Used on b-1b aircraft. duct, transition-cold air outlet, fwd instructor; c/o-plate, qq-a-250/5 aluminum clad sheet alloy 2024-781, 2.600 lg, .032 thk, 1.100 wd; nutplate-2, rivet
01-166-1195
Structural Aircraft Panel
Used on b-1b aircraft. aconsist of one panel, p/n L5338339-003; velcro tape 45.000 in. lg, p/n L5338339-005; velcro tape 47.200 in. lg, p/n L5338339-007; velcro tape 6.380 in lg, p/n L5338339-009; velcro tape 6.700 in. lg
01-166-1196
Structural Aircraft Panel
Used on b-1b aircraft. consist of one panel, p/n L5338348-003
01-166-1197
Structural Aircraft Panel
Used on b-1b aircraft. 32.930" overall length 8.220" overall width consist of one panel, p/n L5338373-017; two piles, p/n L5338373-019; two piles, p/n L5338373-023; twenty-eight holes 0.257 in. dia; 13 holes top lg; 13 holes bottom lg; 2 holes left side
01-166-1200
Structural Aircraft Plate
Used on acft model b-1b. al clad 2024-0 per qq-a-250/5, 0.040 in.thk, 3.060 in.w, 3.280 in.lg, used on center box to latch avionic supply, fwd overhead, left hand
