Sleeve Bushings. 98,451 part numbers in this category

Home » Catalog » Bearings » Sleeve Bushings (Page 72)
Part Number
NSN
NIIN
209-032-167-001
209032167001
3120-01-524-3968
015243968
4320536
4320536
3120-01-524-2414
015242414
Used on f119 engine. unique
5231-A101-307
5231A101307
3120-01-523-9571
015239571
5231-A101-309
5231A101309
3120-01-524-1850
015241850
5231-A101-310
5231A101310
3120-01-524-4738
015244738
5231-A101-320
5231A101320
3120-01-524-4685
015244685
5231-A101-322
5231A101322
3120-01-524-4721
015244721
5231-A101-467
5231A101467
3120-01-523-9509
015239509
6071-A101-132
6071A101132
3120-01-524-3387
015243387
6071-A102-727
6071A102727
3120-01-523-9542
015239542
6071-A103-755
6071A103755
3120-01-524-4700
015244700
69-34905-8
69349058
3120-01-524-4513
015244513
752-7068420-158
7527068420158
3120-01-524-4294
015244294
92107-15102-103
9210715102103
3120-01-523-9595
015239595
Used on h-60 helicopter. navy: bushing next higher assembly: 707107-08404-047
BACB28AK03-017
BACB28AK03017
3120-01-524-2096
015242096
Used on boeing aircraft b757. 0.1700" overall length chromium surface treated 17c solid, plain, no outside flanges
BACB28AK03-031
BACB28AK03031
3120-01-524-2097
015242097
Used on boeing aircraft b757. 0.3100" overall length chromium surface treated 17c solid, plain, no outside flanges
BACB28AK03-042
BACB28AK03042
3120-01-524-2093
015242093
Used on boeing aircraft b757. 0.4200" overall length chromium surface treated 17c solid, plain, no outside flanges
BACB28AK03-084
BACB28AK03084
3120-01-524-2095
015242095
Used on boeing aircraft b757. 0.8400" overall length chromium surface treated 17c solid, plain, no outside flanges
BACB28AK04-020
BACB28AK04020
3120-01-524-2087
015242087
Used on boeing aircraft b757. 0.2000" overall length chromium surface treated 17c solid, plain, no outside flanges
BACB28AK04-022
BACB28AK04022
3120-01-524-2086
015242086
Used on boeing aircraft b757. 0.2200" overall length chromium surface treated 17c solid, plain, no outside flanges
BACB28AK04-031
BACB28AK04031
3120-01-524-2088
015242088
Used on boeing aircraft b757. 0.3100" overall length chromium surface treated 17c solid, plain, no outside flanges
BACB28AK04-033
BACB28AK04033
3120-01-524-2090
015242090
Used on boeing aircraft b757. 0.3300" overall length chromium surface treated 17c solid, plain, no outside flanges
BACB28AK04-035
BACB28AK04035
3120-01-524-2091
015242091
Used on boeing aircraft b757. 0.3500" overall length chromium surface treated 17c solid, plain, no outside flanges
BACB28AK04-036
BACB28AK04036
3120-01-524-2100
015242100
Used on boeing aircraft b757. 0.3600" overall length chromium surface treated 17c solid, plain, no outside flanges
BACB28AT09B014A
BACB28AT09B014A
3120-01-524-2425
015242425
Used on f-22 raptor. 0.2025" overall length bushing flanged, undersize bore, 22c solid, external flange one end
BACB28AT09B019A
BACB28AT09B019A
3120-01-524-2424
015242424
Used on f-22 raptor. 0.2525" overall length bushing flanged, undersize bore, 22c solid, external flange one end
BACB28AT17B040C
BACB28AT17B040C
3120-01-524-2342
015242342
0.4000" overall length cadmium surface treated 22c solid, external flange one end
BACB28U14B037
BACB28U14B037
3120-01-524-2336
015242336
0.3700" overall length 17c solid, plain, no outside flanges
BACB28U3F015
BACB28U3F015
3120-01-524-2333
015242333
0.1500" overall length 17c solid, plain, no outside flanges
BACB28W10C037
BACB28W10C037
3120-01-524-2405
015242405
0.3700" overall length cadmium surface treated 22c solid, external flange one end
BACB28W22B150
BACB28W22B150
3120-01-524-2085
015242085
Used on fixed wing aircraft, boeing 757. 1.5000" overall length subassembly is mechanism instl nose whl well door fwd operating; refer to boeing i.p.c. BOE2339 32-22-02-01 no. 115 cadmium surface treated 22c solid, external flange one end
BACB28W4C009
BACB28W4C009
3120-01-524-2164
015242164
Used on fixed wing aircraft, boeing 757. 1.5000" overall length subassembly is mechanism instl nose whl well door fwd operating; reference boeing i.p.c. BOE2339 32-22-02-01 no. 115 cadmium surface treated 22c solid, external flange one end
BACB28X5C012
BACB28X5C012
3120-01-524-2094
015242094
Used on boeing aircraft b757. 0.1200" overall length cadmium surface treated 22c solid, external flange one end
BACB28Y10C008
BACB28Y10C008
3120-01-524-2294
015242294
0.0800" overall length cadmium surface treated 17c solid, plain, no outside flanges
BACB28Y10M018
BACB28Y10M018
3120-01-524-2305
015242305
0.1800" overall length cadmium surface treated 17c solid, plain, no outside flanges
BACB28Y10M033
BACB28Y10M033
3120-01-524-2302
015242302
0.3300" overall length cadmium surface treated 17c solid, plain, no outside flanges
BACB28Y14C008
BACB28Y14C008
3120-01-524-2280
015242280
0.0800" overall length cadmium surface treated 17c solid, plain, no outside flanges
BACB28Y3C025
BACB28Y3C025
3120-01-524-2289
015242289
0.2500" overall length cadmium surface treated 17c solid, plain, no outside flanges
L6316217-003
L6316217003
3120-01-524-4366
015244366
MS14238A10P015
MS14238A10P015
3120-01-524-0800
015240800
Used on pre-provisioning support. 0.2440" overall length bushing, sleeve - flanged, press fit, ream type cadmium surface treated 22c solid, external flange one end
NAS77A4-012
NAS77A4012
3120-01-524-0803
015240803
Used on pre-provisioning item which navicp acts as poe. bushing, sleeve, aircraft
P817G3-60
P817G360
3120-01-524-3123
015243123
Used on f-16 aircraft. 0.5900" overall length passivate surface treated 22c solid, external flange one end
P817Y3-20
P817Y320
3120-01-524-3124
015243124
Used on f-16 aircraft. 0.1900" overall length passivate surface treated 22c solid, external flange one end
P817Y3-30
P817Y330
3120-01-524-3125
015243125
Used on f-16 aircraft. 0.2900" overall length passivate surface treated 22c solid, external flange one end
P817Y3-45
P817Y345
3120-01-524-3117
015243117
Used on f-16 aircraft. 0.4400" overall length passivate surface treated 22c solid, external flange one end
P817Y4-20
P817Y420
3120-01-524-3115
015243115
Used on f-16 aircraft. 0.1900" overall length passivate surface treated 22c solid, external flange one end
P817Y5-80
P817Y580
3120-01-524-3116
015243116
Used on f-16 aircraft. 0.7900" overall length passivate surface treated 22c solid, external flange one end
P817Z4-55
P817Z455
3120-01-524-3118
015243118
Used on f-16 aircraft. 0.5400" overall length passivate surface treated solid, external flange one end
P817Z4-75
P817Z475
3120-01-524-3119
015243119
Used on f-16 aircraft. 0.7400" overall length passivate surface treated 22c solid, external flange one end
P817Z4-82
P817Z482
3120-01-524-3120
015243120
Used on f-16 aircraft. 0.8100" overall length passivate surface treated 22c solid, external flange one end
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