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1560-00-125-4444

Cowling Flap

1560001254444 001254444 175884

A hinged section forming a part of the aircraft engine cowling, usually located aft of the engine. The purpose of the flap is to regulate the flow of air over and around an engine to control the temperature. View more Cowling Flap

1560-00-125-4444 FLAP,COWLING 1560001254444 001254444

Managed by United States
NSN Created on 1 Jan 1963
Data Last Changed
January 2023
NATO Update Count
16
NATO Data Quality
1560-00-125-4444 FLAP,COWLING 1560001254444 001254444 1/1
NSN 1560-00-125-4444 (Generic Image) 1/1

1560-00-125-4444 Stock and Availability Marketplace 1560-00-125-4444

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1560-00-125-4444 Related Documents Related Documents 1560-00-125-4444 3+ Documents (More...)

175884 A hinged section forming a part of the aircraft engine cowling, usually located aft of the engine
United States (US) 4. 1560-00-125-4444 Marketplace Restrictions Approved Sources Datasheet Management
FLAP,COWLING 4 EA NS Request Quotation Updated Every Day 1560-00-125-4444 RQST NE Updated Every Day
enable JavaScript in your web browser . 5340-01-160-1372Rudder Hing Bracket5340011601372 011601372 175884
Every Day 5340-01-160-1372 RQST NE Restrictions https//www.nsnlookup.com /fsg-15/fsc-1560/us 1560-00-125-4444
Cowling Flap 1560001254444 001254444,175884 Documents 1560-00-125-4444 2+ Documents ( More... )
Account Upgrade 5962-01-312-9474Digital-Linear Microcircuit5962013129474 013129474 BUS-65201II-605 175884
Cowling Flap 1560001254444 001254444,175884 https//www.nsnlookup.com /fsg-15/fsc-1560/us 1560-00
-125-4444 Cowling Flap 1560001254444 001254444,175884 1372Rudder Hing Bracket5340011601372 011601372

1560-00-125-4444 Demil Restrictions 1560-00-125-4444

DEMIL: B | DEMILI: | CRITICALITY: X | HMIC: P | PMIC: U | EDC: | ADPEC:

1560-00-125-4444 is a Cowling Flap that does not have a nuclear hardened feature or any other critical feature such as tolerance, fit restriction or application. This item is a US Munitions List Item and must be mutilated to scrap. This item may be hazardous as it is in a Federal Supply Class for potentially hazardous items. A MSDS should be available from the supplier for the end user to evaluate any hazards. The precious metals content of this item is unknown.

1560-00-125-4444 HTS and ScheduleB Import and Export 1560-00-125-4444

1560-00-125-4444 End Users End Users 1560-00-125-4444

Canada (ZC01)
Effective Date:
1 Apr 1991
Republic of Korea (ZH01)
Effective Date:
1 Apr 1991
Portugal (ZP01)
Effective Date:
1 Apr 1991
Greece (ZU01)
Effective Date:
1 Apr 1991

1560-00-125-4444 Manufacturers Approved Sources 1560-00-125-4444

1560-00-125-4444 Technical Data Datasheet 1560-00-125-4444

Characteristic
Specifications
FIIG
A11500
Aircraft Mission Design Series [CZEK]
T-33
Material Document And Classification [MDCL]
Qq-A-383 Fed Spec Single Material Response

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1560-00-125-4444 Freight Data Freight Information 1560-00-125-4444

1560-00-125-4444 has freight characteristics.It has a National Motor Freight Classification (NMFC) of 095290. A Sub NMFC of X. It has a NMFC Description of HINGES/BUTTS NOI METAL O/T I/S. 1560-00-125-4444 is rated as class 70 when transported by Less-Than Truckload (LTL) freight. 1560-00-125-4444 is rated as class 70 when transported by Less-Than Carload (LCL) rail or ocean freight. It has a Uniform Freight Classification (UFC) number of 49840 which rates the freight between FCL and LCL. 1560-00-125-4444 has a variance between NMFC and UFC when transported by rail and the description should be consulted. It has a Water Commodity Code (WCC) of 713 for ocean manifesting and military sealift. 1560-00-125-4444 is not classified as a special type of cargo when transported by water. 1560-00-125-4444 is not a consolidation and does not exceed 84" in any dimension. It should be compatible with a standard 72" Aircraft Cargo Door when transported by air.