Bearings » Sleeve Bushings

014416-1
0144161

3120-01-520-7455

015207455

0.2650" overall length passivate body surface treated 22e blank, external flange one end

014416-501
014416501

3120-01-520-7748

015207748

0.2020" overall length passivate body surface treated 22e blank, external flange one end

029685-1
0296851

3120-01-521-0471

015210471

1.0000" overall length bushing, support passivate surface treated 22c solid, external flange one end

1211245-205
1211245205

3120-01-520-5223

015205223

Used on ecp n-244-r1.

1211245-206
1211245206

3120-01-520-5218

015205218

Used on ecp n-244-r1.

128968
128968

3120-01-521-0431

015210431

2049AS010-01
2049AS01001

3120-01-520-6705

015206705

Used on block iii rf. 0.3500" overall length navy: bushing, yoke flange end inside diameter is countersunk 0.410 x 90 degrees. 0.060 inch stepped length extension x 0.260 inch diameter beyond main body of bushing. 22c solid, external flange one end

21-026C25
21026C25

3120-01-520-9421

015209421

Used on mv-22 aircraft. 0.3910" overall length cadmium surface treated

334-007-056-0
3340070560

3120-01-521-0250

015210250

Used on cfm-56 engine. bushing

347-7771
3477771

3120-01-520-8792

015208792

Used on 2320014950110 cargo truck.

496-0041
4960041

3120-01-520-8265

015208265

Used on 2320014950110.

4D0004P04-032
4D0004P04032

3120-01-520-9851

015209851

4M43CP26-022
4M43CP26022

3120-01-521-1472

015211472

Used on bushing, sleeve-press fit. 0.6875" overall length navy: bushing, sleeve passivate surface treated 17c solid, plain, no outside flanges

4M43CP30-022
4M43CP30022

3120-01-521-1095

015211095

Used on bushing, sleeve-press fit, corossion resistant steel. 0.6875" overall length navy: bushing, sleeve cadmium surface treated 17c solid, plain, no outside flanges

5HA47222-103
5HA47222103

3120-01-519-8936

015198936

Used on f/a-22 raptor. 2.2100" overall length bearing recoil fwd 22c-1 solid, external flange one end, internal flange one end

60-0344-1
6003441

3120-01-520-5363

015205363

629064
629064

3120-01-521-1920

015211920

Used on f16 aircraft.

63SH0125
63SH0125

3120-01-520-4350

015204350

Used on bushing, q.c. vds transfer hoist. 1.8900" overall length plated steel. fits q.d. sprokets with bushing "sh"., installation torque: 125 ft lbs., max transmissible torque: 4380 lbs. next assembly ej-42180, final assembly ej-52046. 22c solid, external flange one end

83309-36 4IN PART 12
83309364INPART12

3120-01-521-1836

015211836

Used on gate valve.

83309-36 4IN. PART 27
83309364INPART27

3120-01-521-1832

015211832

Used on gate valve. yoke busing

BACB28AK03-011
BACB28AK03011

3120-01-520-9325

015209325

Used on f-22 raptor. 0.1100" overall length bushing, plain (for clamped installation) chromium outside diameter surface of body surface treated 17c solid, plain, no outside flanges

BACB28AK09-049
BACB28AK09049

3120-01-520-3466

015203466

Used on RAPTOR. 0.4850" overall length bushing plain (for clamped installation) chromium outside diameter surface of body surface treated 17c solid, plain, no outside flanges

BACB28AK09-055
BACB28AK09055

3120-01-520-8987

015208987

0.5450" overall length chromate surface treated 17c solid, plain, no outside flanges

BACB28AP04P020
BACB28AP04P020

3120-01-520-9285

015209285

0.2600" overall length cadmium surface treated 22c solid, external flange one end

BACB28AP04P022
BACB28AP04P022

3120-01-520-9284

015209284

0.2200" overall length cadmium surface treated 22c solid, external flange one end

BACB28AT06B024C
BACB28AT06B024C

3120-01-520-9283

015209283

0.3000" overall length cadmium surface treated 22c solid, external flange one end

BACB28W12E049
BACB28W12E049

3120-01-520-7788

015207788

Used on f-22 aircraft. 0.4850" overall length bushing, plain, spacer 22c solid, external flange one end

BACB28W28J081
BACB28W28J081

3120-01-520-4412

015204412

Used on f-22 aircraft. 0.8050" overall length bushing, plain, spacer 22c solid, external flange one end

BACB28W6B029
BACB28W6B029

3120-01-520-8993

015208993

0.2900" overall length cadmium surface treated 22c solid, external flange one end

BACB28Y11C050
BACB28Y11C050

3120-01-520-8715

015208715

0.5000" overall length anodize surface treated 17c solid, plain, no outside flanges

BACB28Y4D285
BACB28Y4D285

3120-01-520-8714

015208714

2.8500" overall length anodize surface treated 17c solid, plain, no outside flanges

BACB28Y8M020
BACB28Y8M020

3120-01-520-8713

015208713

0.2000" overall length anodize surface treated 17c solid, plain, no outside flanges

BACB28Z4-036
BACB28Z4036

3120-01-520-8711

015208711

0.3600" overall length 17c solid, plain, no outside flanges

BACB28Z4-334
BACB28Z4334

3120-01-520-8712

015208712

3.3400" overall length 17c solid, plain, no outside flanges

MS14237A08-037
MS14237A08037

3120-01-520-6728

015206728

Used on f-22 aircraft. 0.3650" overall length bushing sleeve, plain, press fit, ream type 17c solid, plain, no outside flanges

MS14237B08-037
MS14237B08037

3120-01-520-7075

015207075

Used on f-22 aircraft. 0.3650" overall length bushing, sleeve plain, press fit, ream type 17c solid, plain, no outside flanges

MS14237C04-100
MS14237C04100

3120-01-520-9025

015209025

Used on f-22 aircraft. 0.9950" overall length bushing, sleeve plain, press fit, ream type passivate surface treated 17c solid, plain, no outside flanges

MS14237C05P036
MS14237C05P036

3120-01-520-5476

015205476

0.3600" overall length cadmium surface treated solid, plain, no outside flanges

MS14237C06P011
MS14237C06P011

3120-01-520-5472

015205472

0.1100" overall length cadmium surface treated solid, plain, no outside flanges

MS14237C06P012
MS14237C06P012

3120-01-520-5470

015205470

0.1200" overall length cadmium surface treated solid, plain, no outside flanges

MS14237C07P044
MS14237C07P044

3120-01-520-5473

015205473

0.4400" overall length cadmium surface treated 17c solid, plain, no outside flanges

MS14238A05P024
MS14238A05P024

3120-01-521-1034

015211034

Used on bushing, sleeve flanged, press fit, ream type;. 0.3020" overall length navy: bushing, sleeve, aircraft material is aluminum-nickel-bronze per AMS4640; bushing, sleeve flanged, press fit, ream type. cadmium surface treated 22c solid, external flange one end

MS14238C04P012
MS14238C04P012

3120-01-520-5469

015205469

0.1820" overall length cadmium surface treated solid, external flange one end

MS14238C06P039
MS14238C06P039

3120-01-520-5471

015205471

0.3900" overall length cadmium surface treated solid, external flange one end

NAS537-4P042
NAS5374P042

3120-01-520-7428

015207428

Used on mh-60r reman. 0.4150" overall length navy: bushing bushing, sleeve-press fit undersize inside diameter. .013 lbs./piece cadmium surface treated 17c solid, plain, no outside flanges

NAS537-4P055
NAS5374P055

3120-01-520-7453

015207453

Used on mh-60r reman. 0.5450" overall length navy: bushing bushing, sleeve-press fit undersize inside diameter. 0.017 lbs./piece cadmium surface treated 17c solid, plain, no outside flanges

NAS77A6-045
NAS77A6045

3120-01-520-6729

015206729

Used on f-22 aircraft. 0.5420" overall length bushing-flanged, press fit steel, bronze & copper 22c solid, external flange one end

ST4M130-10036
ST4M13010036

3120-01-521-0866

015210866

Used on F/A-18. 0.7500" overall length cadmium surface treated 22c solid, external flange one end

ST4M130-12039
ST4M13012039

3120-01-521-0500

015210500

Used on item fighter aircraft (f18 e/f). 0.6775" overall length cadmium surface treated 22c solid, external flange one end

ST4M130-12040
ST4M13012040

3120-01-521-0494

015210494

Used on item fighter aircraft (f18 e/f). 0.6870" overall length cadmium surface treated 22c solid, external flange one end

Sleeve Bushings. 98,451 part numbers in this category