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1610-01-652-2115

Aircraft Propeller

1610016522115 016522115 W29F3NL-21FH

A propeller designed to provide thrust for a fixed or tilt wing aircraft. It may be of solid or built-up construction; constant or controllable speed type; adjustable, fixed or variable pitch design with reversing and/or feathering capabilities during aircraft operation. Variable pitch propellers have integral facilities for changing the pitch angle of the blades while aircraft is in flight. Excludes HUB-BLADE ASSEMBLY, PROPELLER, AIRCRAFT. See also TEST CLUB. View more Aircraft Propeller

1610-01-652-2115 PROPELLER,AIRCRAFT 1610016522115 016522115

Managed by United States
NSN Created on 12 Feb 2016
Data Last Changed
January 2023
NATO Update Count
4
NATO Data Quality
1610-01-652-2115 PROPELLER,AIRCRAFT 1610016522115 016522115 1/1
NSN 1610-01-652-2115 (Generic Image) 1/1

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1610-01-652-2115 Related Documents Related Documents 1610-01-652-2115 5+ Documents (More...)

W29F3NL-21FH A propeller designed to provide thrust for a fixed or tilt wing aircraft.
United States (US) 4. 1610-01-652-2115 Marketplace Restrictions Approved Sources Datasheet Management
RQST NE Updated Every Day 1610-01-652-2115 RQST Updated Every Day 1610-01-652-2115 RQST NE Related Documents
Aircraft Propeller 1610016522115 016522115 201-9809 Aircraft Propeller 1610002019809 002019809
001210890 1680993526784 993526784 909-3920 1610-99-719-4467 1610-01-530-8100 1610-01-618-5360 1610-01-652-2115
201-9809 1610001157911 001157911 909-3920 1610-99-719-4467 1610-01-530-8100 1610-01-618-5360 1610-01-652-2115
001210890 1680993526784 993526784 909-3920 1610-99-719-4467 1610-01-530-8100 1610-01-618-5360 1610-01-652-2115
201-9809 1610001157911 001157911 909-3920 1610-99-719-4467 1610-01-530-8100 1610-01-618-5360 1610-01-652-2115
1610-00-201-9809 000309552 1680993526784 993526784 719-4467 1610-01-530-8100 1610-01-618-5360 1610-01-652-2115
1680/uk 1680-99-352-6784 Aircraft Propeller 1680993526784 993526784 530-8100 1610-01-618-5360 1610-01-652-2115
1610/us 1610-00-555-6417 Aircraft Propeller 1610005556417 005556417 530-8100 1610-01-618-5360 1610-01-652-2115
1610/us 1610-00-652-9259 Aircraft Propeller 1610006529259 006529259 530-8100 1610-01-618-5360 1610-01-652-2115
Propeller 1680993526784 993526784 909-3920 1610-99-719-4467 1610-01-530-8100 1610-01-618-5360 1610-01-652-2115
Propeller 1610001157911 001157911 909-3920 1610-99-719-4467 1610-01-530-8100 1610-01-618-5360 1610-01-652-2115
1610-00-201-9809 1610-00-121-0890 909-3920 1610-99-719-4467 1610-01-530-8100 1610-01-618-5360 1610-01-652-2115

1610-01-652-2115 Demil Restrictions 1610-01-652-2115

DEMIL: A | DEMILI: 1 | CRITICALITY: X | HMIC: N | PMIC: A | EDC: A | ADPEC: 0

1610-01-652-2115 is a Aircraft Propeller that does not have a nuclear hardened feature or any other critical feature such as tolerance, fit restriction or application. Demilitarization of this item has been confirmed and is not currently subject to changes. 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. This item does not contain a precious metal.

1610-01-652-2115 HTS and ScheduleB Import and Export 1610-01-652-2115

1610-01-652-2115 End Users End Users 1610-01-652-2115

Republic of Korea (ZH01)
Effective Date:
1 Feb 2016

1610-01-652-2115 Manufacturers Approved Sources 1610-01-652-2115

1610-01-652-2115 Technical Data Datasheet 1610-01-652-2115

Characteristic
Specifications
FIIG
A30700
Special Features [FEAT]
Glass Fabric; Hontek Coating; Propeller Dia 29.0 Inches; Hub Thickness 1.63 Inch; Hub Dia 3.56 Inch

1610-01-652-2115 Related Items NATO Stock Numbers Related to 1610-01-652-2115

1610-01-652-2115 Freight Data Freight Information 1610-01-652-2115

1610-01-652-2115 has freight characteristics managed by the Republic of Korea.. 1610-01-652-2115 has a variance between NMFC and UFC when transported by rail and the description should be consulted.