2840-99-636-0847
Bellcrank
2840996360847 996360847 1539-2 36DE274
Managed by United Kingdom
NSN Created on 25 Apr 1991
Data Last Changed
January 2023
January 2023
NATO Update Count
1
1
NATO Data Quality
Marketplace 2840-99-636-0847
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Related Documents 2840-99-636-0847 5+ Documents (More...)
215397223 5950-21-539-7223 5950215397223 215397223 https//www.nsnlookup.com /fsg-28/fsc-2840/uk 2840-99-636-0847
Bellcrank 2840996360847 996360847,1539-2 2840-99-636-0847 2840996360847 996360847 BELLCRANK https
Bellcrank 2840996360847 996360847,1539-2 2840-99-636-0847 2840996360847 996360847 BELLCRANK https
Details... 15392 PAD,ENGINE MOUNTING 1 EA NS Request Quotation Subscribe to View Vendor Details... 1539-2
3146Power Transformer5950009593146 009593146 15392 https//www.nsnlookup.com /fsg-28/fsc-2840/uk 2840-99-636-0847
Bellcrank 2840996360847 996360847,1539-2 2840-99-636-0847 2840996360847 996360847 BELLCRANK https
3146Power Transformer5950009593146 009593146 15392 https//www.nsnlookup.com /fsg-28/fsc-2840/uk 2840-99-636-0847
Bellcrank 2840996360847 996360847,1539-2 2840-99-636-0847 2840996360847 996360847 BELLCRANK https
instructions how to enable JavaScript in your web browser . 6650-15-230-4380Magnifier6650152304380 152304380 1539/2
TM 9-2320-366-20-2 TM 9-2320-366-20-2 TM 9-2320-366-20-2 TM 9-2320-366-20-2 TM 9-2320-366-20-2 2-1539 2
-1539 2-1539 2-1539 2-1539 CONTINUITY TEST (1) Remove kick panel (para 16-3). (2) Disconnect connector
TM 9-2320-366-20-2 TM 9-2320-366-20-2 TM 9-2320-366-20-2 TM 9-2320-366-20-2 TM 9-2320-366-20-2 2-1539 2
-1539 2-1539 2-1539 2-1539 CONTINUITY TEST (1) Remove kick panel (para 16-3). (2) Disconnect connector
https//www.nsnlookup.com
/fsg-31/fsc-3120/us
/fsg-31/fsc-3120/us
3120-00-287-6389 Sleeve Bearing 3120002876389 002876389
3120-00-287-6389 3120002876389 002876389 is a tubular shaped item with or without flange(s) designed to reduce friction and carry a kinetic load on the surface(s) parallel to the axis of the bore. it must have a visible or detectable means of lubrication or be self-lubricated. the over all length must exceed 25 percent of the outside diameter or the shortest distance between peripheral flats of the body, except for straight tubular (without flange or shoulder) items having a bearing surface(s) parallel to the axis of the bore only. includes items which are divided into two or more segments which include 180 degrees (3.141 radians) or less of the bearing periphery. see also bushing, sleeve; spacer, sleeve; and washer (as modified). excludes pin, hollow.
TM 9-2320-366-20-2 TM 9-2320-366-20-2 TM 9-2320-366-20-2 TM 9-2320-366-20-2 TM 9-2320-366-20-2 2-1539 2
-1539 2-1539 2-1539 2-1539 CONTINUITY TEST (1) Remove kick panel (para 16-3). (2) Disconnect connector
-1539 2-1539 2-1539 2-1539 CONTINUITY TEST (1) Remove kick panel (para 16-3). (2) Disconnect connector
Restrictions 2840-99-636-0847
Approved Sources 2840-99-636-0847
- Part Number
- Manufacturer
- Status
- 1539-2
- Manufacturer
- K0378 - Rolls-Royce Military Aero Engines (Active)
- Primary Buy
- Primary Buy
- 36DE274
- U1725 - Ministry Of Defence (Air) (Domestic (Active)
- NATO Reference
- NATO Reference
NATO Stock Numbers Related to 2840-99-636-0847
2510-15-209-3009 2520-99-446-6108 6220-15-204-1528 9999-37-515-0085 5310-15-139-2426 9915-15-219-4601 1730-25-105-4112 1220-14-266-0252 4030-15-175-3668 6685-14-380-3542 1560-99-601-1385 1680-99-600-3219 1005-13-103-5661 2540-15-138-4766 4920-14-441-3681 5340-14-436-9248 2910-12-148-8383 5820-15-138-1601