Bearings » Sleeve Bushings

129-A-805-1
129A8051

3120-01-522-3202

015223202

Used on braiding machine. bronze bushing 17c solid, plain, no outside flanges

15861010 FIND NO. 17
15861010FINDNO17

3120-01-522-0588

015220588

Used on ramp,self-deploying. 2.1820" overall length 22a split, external flange one end

15861010 FIND NO. 18
15861010FINDNO18

3120-01-522-0591

015220591

Used on ramp self-deploying. 4.1770" overall length 22a split, external flange one end

16105A ITEM NO 3
16105AITEMNO3

3120-01-522-3199

015223199

Used on valve drain, 1.00 ips 150 psi.

2050M22P01
2050M22P01

3120-01-522-1336

015221336

Used on f-110-ge-100c/129b engine hpc fwd stator case/f16. submitted name is bushing, igv

2050M23P01
2050M23P01

3120-01-522-1339

015221339

Used on f-110-ge-100c/129b engine hpc fwd stator case/f16. submitted name is bushing, vane

2050M23P02
2050M23P02

3120-01-522-1341

015221341

Used on f-110-ge-100c/129b engine hpc fwd stator case/f16. submitted name is bushing, vane

2050M24P01
2050M24P01

3120-01-522-1344

015221344

Used on f-110-ge-100c/129b engine hpc fwd stator case/f16. submitted name is bushing, vane

2050M24P02
2050M24P02

3120-01-522-1345

015221345

Used on f-110-ge-100c/129b engine hpc fwd stator case/f16. submitted name is bushing, vane

21-010A16-8
21010A168

3120-01-522-0209

015220209

Used on hv 22 aircraft. 0.2500" overall length navy) bushing - press fit 17c solid, plain, no outside flanges

70209-26007-164
7020926007164

3120-01-522-2657

015222657

0.4100" overall length 22c solid, external flange one end

74A328960-2005
74A3289602005

3120-01-522-2202

015222202

Used on f/s-18 e/f. 0.0800" overall length bushing one edge of top of flange is chamfered 45 degrees x 0.015-0.025 inch cadmium surface treated 22c solid, external flange one end

74D110608-2027
74D1106082027

3120-01-522-2038

015222038

Used on f-18 e/f fighter aircraft. bushing, cover, aircr used on cover, protective ec

908-03
90803

3120-01-522-3542

015223542

AS14238B05P008
AS14238B05P008

3120-01-521-9054

015219054

0.0800" overall length material - beryllium copper cadmium body surface treated 21c solid, external flange

BACB28X5C040
BACB28X5C040

3120-01-522-3398

015223398

Used on B757.

BACB28X5E011
BACB28X5E011

3120-01-522-3830

015223830

Used on B757.

BACB28X5F016
BACB28X5F016

3120-01-522-3829

015223829

Used on B757.

BACB28X5M010
BACB28X5M010

3120-01-522-3828

015223828

Used on B757.

BACB28X5M011
BACB28X5M011

3120-01-522-3826

015223826

Used on B757.

BACB28X5M012
BACB28X5M012

3120-01-522-3824

015223824

Used on B757.

BACB28X5N031
BACB28X5N031

3120-01-522-3820

015223820

Used on B757.

BACB28X6C017
BACB28X6C017

3120-01-522-3819

015223819

Used on B757.

BACB28X6C019
BACB28X6C019

3120-01-522-3397

015223397

Used on B757.

BACB28X6M012
BACB28X6M012

3120-01-522-3816

015223816

Used on B757.

BACB28X6M020
BACB28X6M020

3120-01-522-3810

015223810

Used on B757.

BACB28X6M033
BACB28X6M033

3120-01-522-3807

015223807

Used on B757.

BACB28X6N012
BACB28X6N012

3120-01-522-3805

015223805

Used on B757.

BACB28X6N023
BACB28X6N023

3120-01-522-3803

015223803

Used on B757.

BACB28X6N027
BACB28X6N027

3120-01-522-3401

015223401

Used on B757.

BACB28X6P017
BACB28X6P017

3120-01-522-3400

015223400

Used on B757.

BACB28X7M020
BACB28X7M020

3120-01-522-3399

015223399

Used on B757.

BACB28X8C017
BACB28X8C017

3120-01-522-3812

015223812

Used on B757.

BACB28X9F017
BACB28X9F017

3120-01-522-3395

015223395

Used on B757. bushing, flange, press fit

BACB28X9M023
BACB28X9M023

3120-01-522-3817

015223817

Used on B757.

BACB28X9M024
BACB28X9M024

3120-01-522-3396

015223396

Used on B757. bushing, flange, press fit

BACB28Y3C043
BACB28Y3C043

3120-01-522-2322

015222322

BACB28Y4C025
BACB28Y4C025

3120-01-522-2321

015222321

BACB28Y4C127
BACB28Y4C127

3120-01-522-2320

015222320

BACB28Y5M016
BACB28Y5M016

3120-01-522-2306

015222306

BACB28Y6C032
BACB28Y6C032

3120-01-522-2319

015222319

LS2326-10S-0.435
LS232610S0435

3120-01-522-0729

015220729

Used on c-130j hercules aircraft. 0.4350" overall length inside diameter after installation 0.6247 to 0.6261 inch cadmium left end surface surface treated 17c solid, plain, no outside flanges

LS35206B4-1
LS35206B41

3120-01-522-2334

015222334

Used on c-130j, aircraft.

MS14238B04P016
MS14238B04P016

3120-01-521-9063

015219063

0.1600" overall length material - beryllium copper cadmium body surface treated 21b segmented, external flange

NAS75-6-028
NAS756028

3120-01-521-9917

015219917

0.0280" overall length inside diameter to be parallel cadmium surface treated 18b segmented, external flanges both ends

P817F5-65
P817F565

3120-01-522-0241

015220241

P817H5-65
P817H565

3120-01-522-0236

015220236

PT3604L1
PT3604L1

3120-01-522-1008

015221008

Used on 10 inch lathe with d1-4 camlock.

S7080-11500-106
S708011500106

3120-01-522-1797

015221797

Used on new man mh-. 0.1800" overall length chamferred 50 degrees all around on one end 17c solid, plain, no outside flanges

S7080-11500-107
S708011500107

3120-01-522-2126

015222126

Used on new man mh-. 0.1800" overall length chamferred 50 deg all around on one inside edge; hole is oval shaped with length being 0.2260-0.2310 17c solid, plain, no outside flanges

Sleeve Bushings. 98,451 part numbers in this category