1610-01-328-1277

Aircraft Propeller Blade

1610013281277 013281277 RFC11R1-OC

An airfoil, which is the thrust producing and major torque absorbing component of an aircraft propeller. It is provided with a suitable root section for assembly in an aircraft propeller hub. It may include retention hardware, cuff, and/or ice control components. View more Aircraft Propeller Blade

1610-01-328-1277 BLADE,PROPELLER,AIRCRAFT 1610013281277 013281277

Managed by United States
NSN Created on 27 Oct 1990
Data Last Changed
November 2023
NATO Update Count
5
NATO Data Quality
1610-01-328-1277 BLADE,PROPELLER,AIRCRAFT 1610013281277 013281277 1/1
NSN 1610-01-328-1277 (Generic Image) 1/1

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1610-01-328-1277 Related Documents Related Documents 1610-01-328-1277 3+ Documents (More...)

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1610-01-328-1277 Aircraft Propeller Blade 1610013281277
RFC11R1-OC An airfoil, which is the thrust producing and major torque absorbing component of an aircraft
United States (US) 4. 1610-01-328-1277 Marketplace Restrictions Approved Sources Datasheet Management
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1610-01-328-1140 Aircraft Propeller 1610013281140 013281140
www.nsnlookup.com /fsg-16/fsc-1610 Aircraft Propellers and Components from United States (US) 1991 1610-01-328-1277
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Aircraft Propellers and Components from United States (US)
1 Jan 1900 1610-01-332-9049 Diaphram Valve F6204013-1RNCC: 3 | RNVC: 2 | DAC: 6 19 Jan 1991 1610-01-328-1277

1610-01-328-1277 Demil Restrictions 1610-01-328-1277

DEMIL: A | DEMILI: | CRITICALITY: | HMIC: N | PMIC: U | EDC: | ADPEC:

1610-01-328-1277 is a Aircraft Propeller Blade This item is considered a low risk when released from the control of the Department of Defense. The item may still be subject to the requirements of the Export Administration Regulations (EAR) and the Code of Federal Regulations (CFR). This item is not suspected to be hazardous. The precious metals content of this item is unknown.

1610-01-328-1277 Manufacturers Approved Sources 1610-01-328-1277

Part Number
Manufacturer
Status
RFC11R1-OC
4V792 - Rockwell Collins, Inc. (Active)
Primary Buy
RNCC 3 RNVC 2 DAC 6

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