01-145-0226
Aircraft Skin
Used on B-52. 130.000" overall length 0.050" overall width opposite p/n 35-10702-8
01-145-0227
Aircraft Skin
Used on B-52. 130.000" overall length 37.200" overall width opposite p/n 35-10702-7
01-145-0228
Aircraft Skin
01-145-0229
Aircraft Skin
Used on acft model b-52. magnesium alloy sheet AZ31b-H24 per qq-m-44, condition H24; 70.200 in. lg, 39.000 in. w, 0.050 in. thk; opposite p/n 35-10703-806
01-145-0230
Aircraft Skin
Used on acft model b-52. magnesium alloy sheet, AZ31b-H24 per qq-m-44, condition H24; 70.200 in. lg, 39.000 in. w, 0.050 in thk; opposite p/n 35-10703-805
01-145-1773
Solid Plain Disk
01-145-1795
Structural Component Air Support
01-145-2279
Aircraft Spar
49.200" overall length temper T6; finish f-2.30; alter BAC1509-100121; nha 5.84479-1, -2, -29, -30
01-145-2571
Aircraft Tip
Aluminum alloy; 12.727 in. lg
01-145-2667
Aircraft Window Panel
24.000" overall length 18.000" overall width
01-145-2676
Access Aircraft Door
Used on f/a-18 acft.
01-145-3843
Structural Aircraft Plate
Used on acft model b52g. al clad 2024-0 per qq-a-362, 0.050 in.thk, 4.250 in.w, 7.000 in.lg, left hand
01-145-3844
Structural Component Air Support
Used on acft model c/kc-135. tube body 6061-T6 al per ww-t-700/6, rod end 4340 steel alloy per mil-s-5000, latch end 303 corrosion resistant steel per ams 5640; 10.670 in. functional length; latch end contains a positive lock pin to hold 3/8 in. dia pin when in operational position
01-145-3846
Structural Component Air Support
Used on acft model f-111.
01-145-3852
Airfoil Rib
7.600" overall length 5.000" overall width 0.032" material thickness
01-145-3853
Aircraft Skin
Used on F-111. 20.000" overall length 3.000" overall width fms 1053, type i, T6
01-145-3861
Aircraft Door
01-145-4503
Fuselage Aircraft Fairing
Used on eh-60a;uh-60a.
01-145-5085
Structural Aircraft Plate
2.000" overall length 1.800" overall width 0.060" material thickness matl: cres laminated; u/a: shim
01-145-5086
Structural Component Air Support
Used on c-141 acft. matl al alloy tubing, ww-t-785, 2024, type 1; 64.050 in. lg; 3.500 in. dia; includes miscellaneous hardware; used as brace, lower stabilizing, main landing gear support structure
01-145-5090
Aircraft Skin
Used on acft model b-52. al clad sheet 2024-0 per qq-a-362, heat treated to condition T4; 130.000 in. lg, 48.000 in. w, 0.050 in. thk
01-145-5866
Structural Component Air Support
01-145-5871
Fuselage Aircraft Fairing
01-145-5946
Aircraft Pylon Section
C/o support instl, beam assy, bulkhead assy, fairing instl, actuator instl, 2 support, 2 blowout door instl, panel assy, misc hardware
01-145-5960
Structural Component Air Support
Used on h-53 acft. matl al alloy, qq-a-367, 7075-T73; surface treatment of epoxy primer
01-145-5961
Structural Component Air Support
Used on h-53 acft. matl al alloy, qq-a-367, 7075-T73; surface treatment of epoxy primer
01-145-8787
Structural Aircraft Panel
Used on uh-60 blackhawk airframe. panel assy ceiling STA327 115-STA360
01-145-9622
Structural Aircraft Plate
Used on acft model c/kc-135. zal alloy 2024-t per qq-a-3556 or qq-a-362, heat treated to min hardness of 92 on rockwell e scale; oval shaped; 4.546 in. lg, 2.866 in. w, 0.156 in. o/a thk; end radius 1.433 in., 4 holes centered along lg, 2 0.313 in. dia, 2 0.140 in. dia
01-145-9646
Aircraft Trailing Edge
C/o rub strip p/n 12W8151-13, rub strip p/n 12W8151-15, rub strip p/n 12W8151-17, rub strip p/n 12W8151-17, rub strip p/n 12W8151-27, stiffener p/n 12W8042-9, skin p/n 12W8150-9, 3 ea. nut p/NC068-02-2, 8 ea. nut p/n C2949-02, as required rivet p/n C088-4
01-145-9647
Aircraft Trailing Edge
0c/o rub strip p/n 12W8044-15, rub strip p/n 12W8044-25, rub strip p/n 12W8044-27, rub strip p/n 12W8044-29, stiffener p/n 12W8042-119, skin p/n 12W8043-9, nut p/n C068-02-2, 12 ea. nut C2949-02, as required rivet p/n C088-4
01-145-9972
Structural Component Air Fitting
01-146-0307
Fuselage Aircraft Fairing
Used on acft model f-18. cognizant service:navy;
01-146-0308
Structural Component Air Support
Used on acft model f-18. aluminum per mil-a-21180, class 11; cond T61
01-146-0739
Aircraft Fairing
C/o 3 seal, 3 retainer, 2 angle, bracket, zee
01-146-0755
Structural Aircraft Plate
Matl size LS7237 by 3
01-146-0756
Structural Aircraft Plate
Matl size LS7237 by 16
01-146-0757
Structural Component Air Support
7.000" overall length 1.000" overall width 0.016" material thickness titanium, AMS4901; u/a:retainer, box structure; opp to p/n 3P61500-109
01-146-0758
Structural Component Air Support
7.000" overall length 1.000" overall width 0.016" material thickness u/a: retainer, box structure; opp to p/n 3P61500-110
01-146-0759
Structural Aircraft Plate
7.680" overall length c/o:2 holes, 0.385in dia; distance from c to c 2.900 in; 2 holes, 0.322in dia; temper T4; opp to p/n 3P38902-103; u/a: spacer
01-146-0760
Structural Aircraft Plate
7.680" overall length c/o:2 holes, 0.385in dia; distance from c to c 2.900 in; 2 holes, 0.322in dia; temper T4; opp to p/n 3P38902-104; u/a: spacer
01-146-0774
Airfoil Rib
Used on F-111. 42.000" overall length 8.000" overall width 0.063" material thickness
01-146-0775
Aircraft Skin
Used on acft model c-135. aal clad sheet 7075-T6 per qq-a-250/13, finish f-2.10 for -15 doubler
