5340-20-002-1232

Shock Strut End Cap

5340200021232 200021232 21262-1 21262

5340-20-002-1232 END CAP,SHOCK STRUT 5340200021232 200021232

Managed by Canada
NSN Created on 15 Jun 2005
Data Last Changed
January 2023
NATO Update Count
1
NATO Data Quality
5340-20-002-1232 END CAP,SHOCK STRUT 5340200021232 200021232 1/1
NSN 5340-20-002-1232 (Generic Image) 1/1

5340-20-002-1232 Stock and Availability Marketplace 5340-20-002-1232

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Approved Sources 1450-00-817-4146 Part NumberManufacturerStatus29-21262-1 08903 - The Boeing Company
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5305-00-484-6225 Socket Head Cap Screw 5305004846225,FFS86
5305-00-484-6225 5305004846225 004846225 is an externally threaded fastener whose threaded portion is of one nominal diameter. the head has an internal socket or multiple spline for use with an inserted driver. a locking feature may be incorporated in the design of the head or threads. excludes items with bevel (conical) heads. see bolt, internal wrenching. excludes screw, shoulder; and screw, machine.

5340-20-002-1232 Demil Restrictions 5340-20-002-1232

DEMIL: | DEMILI: | CRITICALITY: | HMIC: | PMIC: | EDC: | ADPEC:

5340-20-002-1232 is a Shock Strut End Cap

5340-20-002-1232 End Users End Users 5340-20-002-1232

United Kingdom (ZK)

5340-20-002-1232 Manufacturers Approved Sources 5340-20-002-1232

Part Number
Manufacturer
Status
21262-1
35962 - Safran Landing Systems Canada Inc. (Active)
Primary Buy
RNCC 3 RNVC 2 DAC 2
21262
35962 - Safran Landing Systems Canada Inc. (Active)
Informational Drawing
RNCC D RNVC 9 DAC 2

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