01-164-4834
Structural Component Air Support
Used on b-1b aircraft.
01-164-4838
Structural Component Air Support
Used on acft model b-1b. c/o bracket 1 ea p/n L5800943-003, 0.071 in.thk, 3.500 in.w, 5.960 in.lg, al alloy 2024-T3 per qq-a-250/5; nutplate 2 ea p/n MS21076L3, located at yf 932
01-164-4841
Structural Component Air Support
Used on acft model kc-135. corrosion resistant steel 301 per mil-s-5059, surface cond 2b, 1/4 hard; finish f-1.108; 1.900 in. lg, 0.9 in. w, 0.025 in. thk; opposite p/n -2; nha 65C18604
01-164-4842
Structural Component Air Support
01-164-4843
Structural Component Air Support
01-164-4844
Structural Component Air Support
Used on acft model kc-135. fitting made from 9-61248; c/o 1 fitting, 2 nutplate assemblies, 2 bearings, 2 bolts, 2 lubricators; nha 5-87841
01-164-4856
Aircraft Former
44.000" overall length 3.400" overall width 0.063" material thickness opposite -4
01-164-4857
Aircraft Former
44.000" overall length 3.400" overall width 0.063" material thickness opposite -3
01-164-4862
Thermal Special Purpo Insulation
End item identification:aircraft, model b-1b
01-164-5921
Access Aircraft Cover
Used on b-1b aircraft.
01-164-5922
Access Aircraft Cover
Used on b-1b aircraft.
01-164-5923
Access Aircraft Cover
Used on b-1b aircraft.
01-164-5925
Access Aircraft Door
Used on f-16 aircraft. spring loaded self-closing
01-164-5973
Structural Aircraft Plate
Used on f-16 aircraft. c/o-frame assy, cover, rubber sheet, support, sealant, adhesive; replaces -19; location-from fs 427.00 to fs 436.50; part of-dorsal insl-fs 368.10 to 444.40
01-164-5974
Structural Aircraft Plate
Used on f-16 aircraft. c/o-frame, rubber sheet, hardware; replaces -17; location-fs 417.40 to fs 427.00; part of dorsal installation, fs 368.10 to 444.40
01-164-5975
Structural Aircraft Plate
Used on b-1b acft. matl al alloy, qq-a-250/4, 2024-T4; 4.680 in. lg; 5 holes, countersink 100 deg by 0.302 in. dia; used as retainer, seal-crew ram air scoop
01-164-5976
Structural Aircraft Plate
Used on b-1b acft. matl al alloy, 2024-T4; 10.250 in. lg; 9 holes, countersink 100 deg, 0.302 in. dia; used as retainer, seal-crew ram air scoop
01-164-5977
Structural Aircraft Plate
Used on b-1b acft. matl al alloy, 2024-T4; 10.250 in. lg; 9 holes, countersink 100 deg, 0.302 in. dia; opposite to p/n L5340092-005; used as retainer, seal-crew air scoop
01-164-5978
Structural Aircraft Plate
Used on b-1b acft. gmatl al alloy, qq-a-250/4, 2024-T851; matl size 0.312 in. thk by 1.090 in. w by 4.750 in. lg; rectangular shaped; 5 holes, 100 deg countersink by 0.302 in. dia; used as retainer seal crew ramp air scoop
01-164-5979
Structural Aircraft Plate
Used on acft model b-1b. al clad 2024-T81 per qq-a-250/5, 0.090 in.thk, 2.000 in.w, 17.000 in.lg, located from yvs 135.890 to yvs 152.841, left hand
01-164-5981
Aircraft Fairing
0.071" material thickness nha 2-3--3579
01-164-5983
Structural Component Air Support
Used on acft model b-1b. located at YF290.00 lh, al alloy 2024-0 per qq-a-250/4, 0.050 in.thk, 3.420 in.w, 5.880 in.lg
01-164-5984
Structural Component Air Fitting
1.900" overall length 1.000" overall width
01-164-5985
Structural Component Air Support
Used on acft model b-1b. steel casting per ams 5343 17-4ph
01-164-5986
Structural Component Air Support
Used on acft model b-1b. commercially pure titanium bar per mil-t-9047 comp. 6 cond. a type iii, 6.000 in. lg, 1.500 in. w, 1.500 in. thk
01-164-5988
Structural Component Air Support
Used on acft model b-1b. commercially pure titanium bar per mil-t-9047 comp. 6 cond. a, alloy 6al-4v, 4.750 in. lg, 3.500 in. w, 1.750 in. thk
01-164-5989
Structural Component Air Support
Used on acft model b-1b. steel ST0160LB0013, cres rect bar, alloy ph-8mo cond a, 7.500 in. lg, 2.750 in. w, 2.000 in. thk
01-164-5990
Structural Component Air Support
Used on acft model b-1b. titanium bar alloy per mil-t-9047comp. 6 cond. a, 6al-4v, 7.750 in. lg, 6.250 in. w, 2.750 in. thk
01-164-5991
Structural Component Air Support
Used on b-1b aircraft.
01-164-5992
Structural Component Air Support
Used on acft model b-1b. aluminum alloy per mil-a-21180 sand casting alloy A356
01-164-6015
Aircraft Skin
Used on F-16. 17.000" overall length 12.000" overall width
01-164-6016
Aircraft Skin
Used on F-16. 17.000" overall length 12.000" overall width
01-164-6017
Horizontal Stabilizer
01-164-6018
Horizontal Stabilizer
01-164-6508
Airframe Modification Kit
Used on f-5e/f acft.
01-164-6510
Movable Canopy
Haz/class div 1.4; warning label 1.4s; un sern 0349; dot regis 8808499a; n.e.w. 0.023 lbs
01-164-6560
Radome
Used on f-5 acft.
01-164-6785
Fuel Aircraft Tank
Used on oh-58d kiowa warrior helicopter.
01-164-8981
Access Aircraft Cover
Used on b-1b aircraft. nuclear hardness critical item
01-164-8982
Access Aircraft Cover
Used on b-1b aircraft. nuclear hardness critical item
01-164-8984
Access Aircraft Door
01-164-9040
Structural Component Air Fitting
C/o 4 plate, 2 shim, 1 bushing, 1fitting
01-164-9041
Structural Component Air Fitting
C/o 1 fitting, 1 spacer, 1 plate, 2 shim, 2 bearing
01-164-9042
Structural Component Air Fitting
C/o 1 fitting, 1 spacer, 1 plate, 1 shim, 2 bearing
01-164-9047
Structural Component Air Support
12.500" overall length 0.028" material thickness
01-164-9061
Structural Component Air Support
Used on acft model b-1b. c/o rod 1 ea p/n LE275-0009-0007, nut-check 2 ea p/n LD114-0006-10002, lock-rod end 2 ea p/n LD162-0004-00005, bearing 2 ea fscm 97613 p/n KBDE4crw, 14.980 in.lg, adjustable
01-164-9063
Structural Component Air Support
C/o: rod (1 ea) LE275-0009-0010, nut-check (2 ea) LD114-0006-1002, lock-rodend (2 ea) LD162-0004-0005, clevis (1 ea) L5341262-003, bearing (1 ea) cage 97613 KBDE4crw; 10.130 lg adjustable
01-164-9064
Structural Component Air Support
Used on acft model b-1b. bc/o rod 1 ea p/n LE275-0009-0006, nut-check 2 ea p/n LD114-0006-1002, lock-rod end 2 ea p/n LD162-0004-0005, clevis 1 ea p/n L5341263-005, bearing 1 ea fscm 97613 p/n KBDE4crw, 8.050 in.lg, adjustable
01-164-9078
Aircraft Former
5.800" overall length 4.200" overall width 0.025" material thickness finish no.18/no. 20- ict; opp -99; nha 215-40060-139
01-164-9079
Aircraft Former
5.800" overall length 4.200" overall width 0.025" material thickness finish N18/N20-ict; opp -100; nha 215-40060-139
