01-164-0412
Structural Component Air Support
Used on acft model b-1b. al plate 2024-T851 per qq-a-250/4; c/o 1 fitting, 1 insert; 2.438 in. square, 0.750 in. o/a h; 4 0.228 in. dia mounting holes; base 0.100 in. thk; 0.65 in. h, 0.800 in. dia centered projection
01-164-0413
Structural Component Air Support
2.700" overall length 2.500" overall width 0.063" material thickness
01-164-0423
Thermal Special Purpo Insulation
Tc/o orcon an-20 film cover, 12.750 in.lg; 11.750 in.w; blanket-fiber glass batting per mil-p-5924b, type a, 0.50 lb/cu ft; end item identification:aircraft, model b-1b; functional description:used as cooling air supply insulation cover
01-164-0425
Thermal Special Purpo Insulation
4c/o orcon an-20 film cover, 14.500 in.lg; 11.750 in.w
01-164-0426
Thermal Special Purpo Insulation
0c/o orcon an-20 film cover, 14.750 in.lg; 11.750 in.w; blanket-fiber glass batting per mil-b-5924b, type a, 0.50 lb/cu ft; nha L5340012; end item identification:aircraft, model b-1b; functional description:used as cooling air supply insulating cover
01-164-0427
Thermal Special Purpo Insulation
3c/o orcon an-20 film cover, 17750 in.lg; 11.750 in.w
01-164-0429
Aircraft Door
Opposite -022
01-164-0430
Aircraft Door
Opposite -021
01-164-1351
Structural Aircraft Plate
Used on b-1b aircraft. used on shelf support-blower
01-164-1355
Aircraft Fairing
01-164-1371
Structural Aircraft Plate
14.500" overall length 5.500" overall width 0.063" material thickness opposite to p/n 39-9921-13; used as web aft
01-164-1374
Structural Component Air Support
Used on b-1b aircraft. used on shelf, support-blower
01-164-1375
Structural Component Air Support
Used on b-1b aircraft. used on shelf, support-blower
01-164-1378
Structural Component Air Support
Used on acft model b-1b. c/o rod 1 ea p/n LE275-0009-0020, 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 L5341293-001, 13.080 in.lg, adjustable
01-164-1379
Structural Component Air Support
Used on acft model b-1b. c/o rod 1 ea p/n LE275-0009-0021, 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, 16.680 in.lg, adjustable
01-164-1380
Structural Component Air Support
Used on acft model b-1b. c/o rod 1 ea p/n LE275-0009-0022, 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 L5341293-001, 8.220 in.lg, adjustable
01-164-1381
Structural Component Air Support
Used on acft model b-1b. c/o rod 1 ea p/n LE275-0009-0023, 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, 8.220 in.lg
01-164-1382
Structural Component Air Support
Used on acft model b-1b. c/o rod 1 ea p/n LE275-0009-0024, 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, 10.940 in.lg, adjustable
01-164-2039
Access Aircraft Door
Used on acft model f-16a/b usaf. location-air scoop
01-164-2042
Access Aircraft Door
Lh lower strake access
01-164-2129
Aircraft Fairing
Nha 16B6322-1; effect 61 0007 9999; superseded 16B6322-13 tw per ECN2E128mmac wf
01-164-2172
Structural Component Air Support
Used on acft model f-16c/d usaf. function-strap, antirotation-jet fuel starter; material-AMS5629 like cres PH13-8M0; stock size-1.0 x 2.2 x 10; eff 5c 0001 9999; nha 16B570-5
01-164-2173
Structural Component Air Support
Used on acft model kc-135.
01-164-2174
Structural Component Air Support
Used on acft model b-1b.
01-164-2175
Structural Component Air Support
Used on acft model b-1b. aluminum alloy sheet per 2024-T8511, 3.030 in. lg, 1.780 in. w, 7.500 in. thk
01-164-2176
Structural Component Air Support
Used on acft model b-1b. c/o strut p/n L5341047-003, 2 ea. rod end p/n KB5E1CRWD21, 2 ea. nut p/n LD114-0006-1003, 2 ea. lock p/n LD162-0004-0006
01-164-2177
Structural Component Air Support
Used on acft model b-1b. titanium alloy 6 al-4v per mil-t-9047, 4.150 in.w, 2.220 in.thk, 10.410 in.lg
01-164-2192
Aircraft Skin
Sealant per fms-1044-5, support, -53 plate .100 x 5.6 x 6, -122 skin .100 x 55 x 66, -136 plate .100 x 19 x 25; finish A403 or A717; eff 0001 9999
01-164-3980
Fuel Aircraft Tank
Used on ah-64 airframe, rotary wing aircraft.
01-164-4006
Access Aircraft Door
Used on helicopter model sh-60b.
01-164-4007
Access Aircraft Door
Used on helicopter model sh-60b.
01-164-4008
Access Aircraft Door
Used on aircraft model f-18.
01-164-4009
Access Aircraft Door
Used on aircraft model f-18.
01-164-4144
Structural Component Air Support
Used on uh-60 helicopter.
01-164-4155
Exhaust Aircraft Lip
Used on aircraft model sh-60b. navy-exhaust assembly 70308-23100-044
01-164-4268
Fuselage Section
Used on helicopter model sh-60b.
01-164-4269
Fuselage Section
Used on helicopter model sh-60b.
01-164-4270
Fuselage Section
Used on helicopter model sh-60b.
01-164-4271
Fuselage Section
Used on helicopter model sh-60b.
01-164-4272
Structural Aircraft Panel
Used on sh60b aircraft.
01-164-4273
Fuselage Section
Used on aircraft model sh-60b.
01-164-4274
Fuselage Section
Used on helicopter model sh-60b.
01-164-4341
Fluid Aircraft Manifold
01-164-4709
Access Aircraft Cover
Used on camera access,f-4 aircraft.
01-164-4830
Structural Component Air Support
Used on f-4 aircraft. console, aft cockpit right hand, retrofit
01-164-4831
Structural Component Air Support
Used on acft model kc-135. 7corrossion resistant steel 15-5ph per AMS5659; heat treated to 155-170 ksi per BAC5619; finish f-8.07 plus f-12.108 at contact points with al; 6.05 in. o/a lg, 3.08 in. o/a h; c/o 1 hinge, 2 flanged bushings, 1 spacer; opposite p/n -605; nha 65C18604
01-164-4832
Structural Component Air Support
Used on acft model kc-135. vcorrosion resistant steel 15-5ph per AMS5659; heat treated to 155-170 ksi per BAC5619; finish f-8.07 plus f-12.108 at contact points with al; 5.97 in. o/a lg, 2.66 in. w, 2.56 in. o/a h; nha 65C18604; c/o 1 hinge, 2 flanged bushings
01-164-4833
Structural Component Air Support
Used on acft model kc-135. ccorrosion resistant steel 15-5ph per AMS5659; heat treated to 155-170 ksi per BAC5619; finish f-8.07 plus f-12.108 at contact points with al; c/o 1 hinge, 2 flanged bushings, 1 spacer; nha 65C18604
