Sleeve Bushings. 98,451 part numbers in this category

Home » Catalog » Bearings » Sleeve Bushings (Page 93)
Part Number
NSN
NIIN
1-060-167-01
106016701
3120-01-501-4503
015014503
Used on t-53 aircraft gas turbine engine inlet guide inner fairing assy outboard side.
1-060-167-02
106016702
3120-01-501-4506
015014506
Used on t-53 aircraft gas turbine engine inlet guide outer forward fairing inboard side.
12364288
12364288
3120-01-502-2516
015022516
Used on fighting vehicle system, bradley, (bfvs). 0.1800" overall length roller 17c solid, plain, no outside flanges
12-847638
12847638
3120-01-501-8377
015018377
Used on gimble ring and steering lever; stern overdri.
12L369-7
12L3697
3120-01-502-2208
015022208
0.4200" overall length blank, plain, no outside flanges
160D920111-15
160D92011115
3120-01-501-5084
015015084
Used on spacer and bushings-primary flight controls;aircraft a-10. 0.2430" overall length cadmium surface treated 17c solid, plain, no outside flanges
18048-0012
180480012
3120-01-502-3578
015023578
180-6984440-132
1806984440132
3120-01-501-8757
015018757
180-6984440-400
1806984440400
3120-01-501-8761
015018761
22-006B15-23-16
22006B152316
3120-01-502-4209
015024209
Used on helicopter. bushing
221-0749-17
221074917
3120-01-501-3458
015013458
Used on a310-222 airbus.
221-0749-5
22107495
3120-01-501-3464
015013464
Used on a310-222 airbus.
23051314
23051314
3120-01-502-4084
015024084
Used on engines t406-ad-400 and ae2100a, c and ae2100d2, d3, j and ae3007a, c, h, rolls-royce corporation. bushing sleeve flanged
23058366
23058366
3120-01-502-1729
015021729
used on C130j aircraft; AE2100a, c engine
23060891
23060891
3120-01-502-1734
015021734
used on C130j aircraft; AE1107 engine; T406-ad-400 engine; AE2100a, c, engine; AE3007a, c, h engine; AE2100D2, D3, j engine
23060892
23060892
3120-01-502-0699
015020699
Used on models ae1107 and t406-ad-400 andae2100a,c and ae3007a,c,h and ae2100d2,d3,j aircraft engines. bushing, sleeve - flange inner .439 x 1.44
23060893
23060893
3120-01-502-0697
015020697
Used on models ae1107 and t406-ad-400 andae2100a,c and ae3007a,c,h and ae2100d2,d3,j aircraft engines. bushing, sleeve - flange, stages 1-5
23-807073
23807073
3120-01-502-0599
015020599
Used on mercruiser, trim cylinders & hydrulic hoses,stern overdri.
23-847637
23847637
3120-01-501-8382
015018382
Used on bell housing; stern overdri.
2613157
2613157
3120-01-501-5894
015015894
2613158
2613158
3120-01-501-5896
015015896
342-7067321-110
3427067321110
3120-01-501-8640
015018640
342-7067321-77
342706732177
3120-01-501-8631
015018631
4529-001
4529001
3120-01-501-6938
015016938
4529-002
4529002
3120-01-501-7299
015017299
4529-003
4529003
3120-01-501-7297
015017297
512-7409900-36
512740990036
3120-01-502-2942
015022942
531-7069980-60
531706998060
3120-01-501-9462
015019462
596-7409665-7
59674096657
3120-01-502-3315
015023315
601-APPC2
601APPC2
3120-01-502-3865
015023865
803-1400051 PC 2
8031400051PC2
3120-01-501-8616
015018616
803-1400051 PC 20
8031400051PC20
3120-01-501-8614
015018614
805-1400053 PC 4
8051400053PC4
3120-01-501-8357
015018357
881534-11
88153411
3120-01-501-7851
015017851
Used on aircraft,mc-130h. 0.3770" overall length nickel surface treated 22c solid, external flange one end
881534-13
88153413
3120-01-501-7847
015017847
Used on aircraft,mc-130h. 0.3140" overall length flange has been ground flat on two sides; measurement accross flats, is 0.320 to is 0.350" nickel surface treated 22c solid, external flange one end
881534-9
8815349
3120-01-501-7777
015017777
Used on aircraft,mc-130h. 0.5205" overall length nickel surface treated 17c solid, plain, no outside flanges
BACB28W10E058
BACB28W10E058
3120-01-502-4359
015024359
passivate surface treated
BACB28X12E050
BACB28X12E050
3120-01-502-4419
015024419
passivate surface treated
D767563-1
D7675631
3120-01-502-1671
015021671
JE3055-4
JE30554
3120-01-501-8326
015018326
Used on hatch, wt.
JE3055-5
JE30555
3120-01-501-8324
015018324
Used on hatch, wt.
NAS72-7E010
NAS727E010
3120-01-502-0380
015020380
NAS74A4-003
NAS74A4003
3120-01-501-4618
015014618
Used on f/a-18e/f acft hydraulic system hand pump. 0.1920" overall length 17c solid, plain, no outside flanges
S4922798-6A019
S49227986A019
3120-01-501-6451
015016451
Used on c-17a acft. 0.2914" overall length bushing, sleeve-press fit, undersize id, reamable cadmium surface treated 17c solid, plain, no outside flanges
S5005-4-200
S50054200
3120-01-501-5501
015015501
Used on f10 thunderbolt. cadmium surface treated
S700B0444
S700B0444
3120-01-501-3456
015013456
Used on a310-222 airbus.
S700Y0619
S700Y0619
3120-01-501-3461
015013461
Used on a310-222 airbus.
ST4M130-05042
ST4M13005042
3120-01-501-4614
015014614
Used on f18 e/f. 0.1950" overall length bushing-sleeve-flanged, special passivate surface treated 22c solid, external flange one end
ST4M144-03018
ST4M14403018
3120-01-502-4859
015024859
0.7350" overall length 17c solid, plain, no outside flanges
U72-14-34
U721434
3120-01-501-7742
015017742
Used on brake,metal f. bushing, clamp, handle
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