01-159-4529
Access Aircraft Door
01-159-4530
Access Aircraft Door
01-159-4531
Access Aircraft Door
01-159-5243
Access Aircraft Cover
Used on b-52 aircraft.
01-159-5244
Access Aircraft Door
01-159-5245
Access Aircraft Door
01-159-5307
Elevator Balance Weight
Used on acft model c/kc-135. 1020 or 1025 steel bar per mil-s-7952; finish cadmium plate per qq-p-416; 21.300 in. lg, 5.500 in. w, 0.375 in. thk; weight 30.0-30.5; opposite p/n -3018; used as balance weight on elevator panel
01-159-5308
Elevator Balance Weight
Used on acft model c/kc-135. 1020 or 1025 steel bar per mil-s-7952; finish cadmium plate per qq-p-416; 24.400 in. lg, 5.500 in. w, 0.375 in. thk; weight 30.5-31.0; opposite p/n -3019; used as balance weight on elevator panel
01-159-5309
Elevator Balance Weight
Used on acft model c/kc-135. 1020 or 1025 steel bar per mil-s-7952; finish cadmium plate per qq-p-416; 27.000 in. lg, 5.500 in. w, 0.375 in. thk; weight 31.0-31.5; opposite p/n -3020; used as balance weight on elevator panel
01-159-5310
Elevator Balance Weight
Used on acft model c/kc-135. antimony lead per mil-l-18331; finish cadmium plate per qq-p-416, type ii or iii; 21.400 in. lg, 5.500 in. w, 0.375 in. thk; weight 32.0-32.5; opposite p/n -3024; used as balance weight on elevator panel
01-159-5311
Elevator Balance Weight
Used on acft model c/kc-135. antimony lead per mil-l-18331; finish cadmium plate per qq-p-416, type ii or iii; 23.400 in. lg, 5.500 in. w, 0.375 in. thk; weight 32.5-33.0; opposite p/n -3025; used as balance weight on elevator panel
01-159-5312
Elevator Balance Weight
Used on acft model c/kc-135. antimony lead per mil-l-18331; finish cadmium plate per qq-p-416, type ii or iii; 25.700 in. lg, 5.500 in. w, 0.375 in. thk; weight 33.0-33.5; opposite p/n -3027; used as balance weight on elevator panel
01-159-5336
Aircraft Former
Used on acft model f-111. material per fms 1010-T851, may be used as an alternate if -19, -20 are not available
01-159-5340
Structural Component Air Support
Used on acft model ef-111. restrictor-union, 2.047 in. lg o/a
01-159-5355
Structural Aircraft Panel
Used on b-1b aircraft. 26.000" overall length 22.000" overall width
01-159-5356
Structural Aircraft Panel
Used on b-1b aircraft. 26.000" overall length 22.000" overall width
01-159-5357
Structural Aircraft Plate
Used on acft model c/kc-135. 6/6 wear resistant nylon sheet per l-p-410; 4.400 in. lg, 4.400 in. w, 0.125 in. thk; contains 4 irregular holes; 6 holes for attachment
01-159-5358
Structural Aircraft Plate
Used on acft model c/kc-135. 6/6 wear resistant nylon sheet per l-p-410; 5.600 in. lg, 4.300 in. w, 0.125 in. thk; 5 irregular holes; 9 holes for attachment
01-159-5359
Structural Aircraft Plate
1.600" overall length 1.600" overall width 0.125" material thickness
01-159-5364
Structural Component Air Support
Used on acft model ef-111. 1.180 in. lg o/a, 1.000 in. w. o/a
01-159-5366
Aircraft Former
16.000" overall length 11.000" overall width 0.040" material thickness 0 temp; heat treat T4; finish f-2.115
01-159-5367
Aircraft Former
4.300" overall length 1.000" overall width 0.625" material thickness temper T4; finish f-2.30; opp -4
01-159-5368
Aircraft Former
4.300" overall length 1.000" overall width 0.625" material thickness opposite -3
01-159-6099
Access Aircraft Door
Used on acft model f-18.
01-159-6646
Access Aircraft Door
01-159-6724
Structural Aircraft Panel
Used on c/kc-135 aircraft. consist of one cowl fastener pin; one cowl fastener stud; one attach strap
01-159-6725
Structural Aircraft Panel
Used on c/kc-135 aircraft.
01-159-6747
Structural Aircraft Panel
Used on c/kc-135. opposite p/n -3124
01-159-6749
Structural Aircraft Panel
Used on c/kc-135 aircraft. opposite p/n -3126
01-159-6750
Structural Aircraft Panel
Used on c/kc-135.
01-159-6796
Structural Aircraft Plate
1.800" overall length 1.100" overall width 0.080" material thickness
01-159-6799
Structural Component Air Support
Used on acft model c/kc-135. al clad 2024-T3 per qq-a-362, T3 temper; finish f-2.115; BAC1501-1545 by 11.100 in. lg; nha 5-86308-5 outboard main landing gear door; opposite p/n -28
01-159-6800
Structural Component Air Support
Used on acft model c/kc-135. al clad 2024-T3 per qq-a-362, T3 temper; finish f-2.115; BAC1501-1545 by 11.100 in. lg, nha 5-86308-5 outboard main landing gear door; opposite p/n -30
01-159-6801
Structural Component Air Support
Used on c-141 acft. matl al alloy, qq-a-200/11, 7075-T6; matl size 2.500 by 3.000 by 7.000 in. lg; used on no. 6 spoiler drive roller
01-159-6805
Aircraft Former
01-159-6806
Aircraft Former
01-159-6807
Aircraft Former
01-159-6809
Aircraft Former
01-159-6811
Airfoil Rib
5.000" overall length 1.050" overall width 0.500" material thickness phen cot. sheet per mil-p-15035, type fbg; opposite p/n -1; nha 215-40066-2
01-159-6812
Airfoil Rib
5.000" overall length 1.050" overall width 0.500" material thickness phen cot. sheet per mil-p-15035, type fbg; opposite -2; nha 215-40066-1
01-159-6813
Airfoil Rib
Nha 215-40066-4
01-159-6814
Airfoil Rib
Nha 215-40066-3
01-159-6815
Airfoil Rib
Nha 215-40066-4
01-159-6816
Airfoil Rib
Nha 215-40066-3
01-159-6817
Airfoil Rib
Nha 216-40063-19 fairing assembly
01-159-6818
Aircraft Skin
Nha 216-4-0063-19
01-159-6819
Aircraft Skin
Nha 215-40067-4
01-159-6966
Structural Component Air Support
Used on 1520-00-859-2670. type/model designation:uh-1d aluminum alloy 7075 qq-a-250/13, T6; 0.020 in. matl thk by 1.800 in. w by 30.300 in. lg; l cross section; w/o rivet holes
01-159-6967
Structural Component Air Support
Used on 1520-00-859-2670. type/model designation:uh-1d aluminum alloy 7075 qq-a-250/13, T6; 0.032 in. matl thk by 2.000 in. w by 30.300 in. lg; l cross section; w/o rivet holes
01-159-7262
Structural Component Air Fitting
