01-163-6801
Structural Aircraft Plate
88.000" overall length 43.000" overall width 0.020" material thickness
01-163-6803
Structural Aircraft Plate
88.000" overall length 43.000" overall width 0.040" material thickness
01-163-6804
Structural Aircraft Plate
Used on acft model b52. al clad 2024-0 per qq-a-362, 0.020 in.thk, 45.000 in.w, 88.000 in.lg, right hand, used on trailing edge, outboard strut, panel assy
01-163-6805
Structural Aircraft Plate
Used on acft model b52. al clad 2024-0 per qq-a-362, 0.020 in.thk, 45.000 in.w, 88.000 in.lg, left hand, used on trailing edge, outboard strut, panel assy
01-163-6813
Structural Component Air Support
Used on f-5f acft.
01-163-6814
Structural Component Air Support
Used on acft model kc-135. located sta. 360
01-163-6815
Structural Component Air Support
Used on acft model kc-135. located station 287.63
01-163-6816
Structural Component Air Support
Used on acft model b-1b. al alloy 2024-T8511, 1.320 in.thk, 1.640 in.w, 5.870 in.lg, used on central avionics ram air scoop, located at station yf 462
01-163-6818
Structural Component Air Support
Used on acft model b-1b. c/o rod 1 ea p/n LE275-009-0003, lock-rod end 2 ea p/n LD162-0004-0005, bolt eye 2 ea p/n L5341293-001, clevis 1 ea p/n L5341263-007, clevis 1 ea p/n L5341262-005, 16.450 in.lg
01-163-6819
Structural Component Air Support
Used on acft model b-1b. c/o rod 1 ea p/n LE275-0009-0004, nut-check 2 ea p/n LD114-0006-1002, lock-rod end 2 ea p/n LD162-0004-0005, eye bolt 1 ea p/n L5341293-001, clevis 1 ea p/n L5341262-005, 10.720 in.lg
01-163-6820
Structural Component Air Support
Used on acft model b-1b. c/o rod 1 ea p/n LE275-0009-0005, nut-check 2 ea p/n LD114-0006-10002, lock-rod end 2 ea p/n LD162-0004-00005, clevis 1 ea p/n L5341262-005, bearing 1 ea fscm 97613 p/n KBDE4crw, bearing 1 ea fscm 97613 p/n KBDE5crw, 14.710 in.lg, adjustable
01-163-6822
Aircraft Strut
Used on acft model b-1b. 10.450" overall length c/o: rod (1 ea) LE275-0009-0012, nut-check (2 ea) LD114-0006-1002, lock-rodend (2 ea) LD162-0004-0005, clevis (1 ea) L5341263-005, bearing (1 ea) cage 97613 KBDE4crw; size 10.450 adjustable
01-163-6824
Structural Component Air Support
Used on acft model b-1b. c/o rod 1 ea p/n LE275-009-0008, nut-check 2 ea p/n LD114-0006-1002, lock-rod end 2 ea p/n LD162-0004-0005, bearing 2 ea fscm 97613 p/n KBDE4crw, 7.460 in.lg, adjustable
01-163-6825
Structural Component Air Support
Used on acft model b-1b. dc/o rod 1 ea p/n LE275-0009-0006, nut-check 2 ea p/n LD114-0006-10002, lock-rod end 2 ea p/n LD162-0004-00005, clevis 1 ea p/n L5341262-005, bearing 1 ea fscm 97613 p/n KBDE5crw, 7.960 in.lg, adjustable
01-163-6826
Structural Component Air Support
Used on c-130 acft. function-mount beam support; location-aft engine mount; matl-7075 aluminum alloy per qq-a-367 condition 310, make from -999l forging
01-163-6827
Structural Component Air Support
Used on c-130 acft. function-mount beam support; location-aft engine mount; matl-7075 aluminum alloy per qq-a-367 condition 10, make from -999r forging
01-163-6831
Aircraft Former
Used on acft model f-16c/d usaf. stock size-30"; material specs-K14A19T8511; finish-A671; location-fs 217.00 to fs 244.12; eff on 5c-0001-9999; nha 16B4701-5; superseded p/n 16B4450-15 ow per ecn 2E893
01-163-6832
Aircraft Skin
Used on B-52. 88.000" overall length 45.000" overall width
01-163-6833
Aircraft Skin
Used on B-52. 88.000" overall length 45.000" overall width
01-163-6835
Aircraft Skin
Used on B-52. 73.000" overall length 24.000" overall width
01-163-6836
Aircraft Skin
Used on B-52. 73.000" overall length 24.000" overall width
01-163-6839
Aircraft Skin
Used on B-52. 64.000" overall length 28.000" overall width
01-163-6840
Aircraft Skin
Used on B-52. 64.000" overall length 28.000" overall width
01-163-6841
Aircraft Skin
Used on B-52. 65.000" overall length 29.000" overall width
01-163-6842
Aircraft Skin
Used on B-52. 65.000" overall length 29.000" overall width
01-163-7030
Aircraft Door
Used on ah-64 apache helicopter.
01-163-7031
Aircraft Door
Used on ah-64 apache helicopter.
01-163-8391
Structural Component Air Fitting
2.700" overall length 0.620" overall width guide, can hsg, interlock link
01-163-8399
Structural Aircraft Plate
11.000" overall length 7.000" overall width 2.000" material thickness
01-163-8403
Aircraft Former
Used on f-16a/b aircraft. 55.000" overall length 26.000" overall width 1.750" material thickness matl FMS3002-T851; finish A403
01-163-8404
Structural Aircraft Plate
Used on b-1b aircraft. used as radius block on support, blower-forward air recirc loop
01-163-8405
Structural Aircraft Plate
Used on b-1b aircraft. used on support, blower-forward air recirc loop
01-163-8406
Structural Component Air Support
Used on b-1b aircraft. used on support, blower-forward air recirc loop; matl-qq-a-250/5 al clad sheet alloy 2024-T3; dimensions-20.300 in. lg, 9.960 in. w, 0.050 in. thk
01-163-8407
Structural Component Air Support
Used on b-1b aircraft. used on shelf-blower
01-163-8408
Aircraft Strut
C/o 1 tube, 1 clevis assy, 1 rod, end assy, 2 nuts, 2 washers; nha L1000000 or L1000004
01-163-8410
Structural Component Air Support
Used on b-1b aircraft. used as beam, shelf, blower
01-163-8411
Structural Component Air Support
Used on acft model b-1b. c/o rod 1 ea p/n LE275-0009-0008, nut-check 2 ea p/n LD114-0006-1002, lock-rod end 2 ea p/n LD162-0004-0005, eye bolt 2 ea p/n L5341293-011, 6.280 in.lg, adjustable
01-163-8412
Structural Component Air Support
Used on b-1b aircraft. used for control valve YF482-YF492; support matl-aluminum alloy bar 5 alloy 2024-T8511; dimensions-7.940 in. lg, 3.500 in. w, 0.875 in. thk; other components-nutplate 3, rivet as required
01-163-8414
Structural Component Air Support
Used on acft model b-1b. c/o rod 1ea p/n LE275-0009-0019, nut-check 2 ea p/n LD114-0006-1002, lock-rod end 2 ea p/n LD162-0004-0005, eye bolt 1 ea p/n L5341293-001, eye bolt 1 ea p/n L5341293-011, 16.160 in.lg
01-163-8420
Aircraft Former
30.000" overall length matl specs-K14A19T8511; finish A671; superseded p/n 16B4450-17 ow per ECN2E893; nha 16B4701-801; eff 5d-0001-9999
01-163-8421
Aircraft Former
2.500" overall length 1.000" overall width 0.063" material thickness
01-163-8422
Aircraft Former
2.500" overall length 1.000" overall width 0.063" material thickness
01-163-8430
Thermal Special Purpo Insulation
C/o 1 -15 blanket assy; 1 -9 blanket assy; 1 -3 blanket assy; end item identification:aircraft, model b-1b; functional description:used as insulation assy set on crew pack heat exchanger
01-163-9613
Bell Crank
0.749" bore diameter both arms have a recessed area onboth sides which is 0.100 in. from outer edge of arm; arm thickness in recessed area is 0.100 in.; recessed area begins 1.000 in. from center of both arm holes; recessed area ends 0.575 in. from center of fulcrum per hughes dwg 7-211525044; width at fulcrum point is 1.500 in. clevis ends
01-163-9621
Aircraft Windshield Panel
01-164-0189
Structural Component Air Fitting
2.000" overall length 0.687" overall width 0.125 microinch surfaces
01-164-0383
Structural Aircraft Panel
Used on B-52. 65.000" overall length 5.500" overall width
01-164-0410
Structural Aircraft Plate
Used on acft model kc-135r. al alloy bar 2024-T62 per qq-a-225/6; finish f-2.16; 4.000 in. lg, 1.300 in. w, 0.800 in. thk; contains 4 MS21209F4-25 inserts; opposite p/n -16; nha 458-58057-1
01-164-0411
Structural Aircraft Plate
2.600" overall length 1.700" overall width 0.050" material thickness
