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4920-01-199-0507

Aircraft Engine Maintenance Machining Fixture

4920011990507 011990507 PWA70168

A fixture designed to hold aircraft engine or auxiliary power unit individual parts, subassemblies, or assemblies in position for machining to design tolerances during modification or repair. View more Aircraft Engine Maintenance Machining Fixture

4920-01-199-0507 FIXTURE,MACHINING,AIRCRAFT ENGINE MAINTENANCE 4920011990507 011990507

Managed by United States
NSN Created on 17 Jan 1985
Data Last Changed
January 2023
NATO Update Count
11
NATO Data Quality
4920-01-199-0507 FIXTURE,MACHINING,AIRCRAFT ENGINE MAINTENANCE 4920011990507 011990507 1/1
NSN 4920-01-199-0507 (Generic Image) 1/1

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,PWA70168 United States (US) 4. 4920-01-199-0507 Marketplace Restrictions Approved Sources Datasheet
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381-1710 Part NumberManufacturerStatus49474 78753 - Te-Co (Active) Primary Buy RNCC 3 RNVC 2 DAC E PWA70168

4920-01-199-0507 Demil Restrictions 4920-01-199-0507

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

4920-01-199-0507 is a Aircraft Engine Maintenance Machining Fixture that does not have a nuclear hardened feature or any other critical feature such as tolerance, fit restriction or application. 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.

4920-01-199-0507 HTS and ScheduleB Import and Export 4920-01-199-0507

4920-01-199-0507 End Users End Users 4920-01-199-0507

Netherlands (ZN01)
Effective Date:
1 Apr 1991

4920-01-199-0507 Manufacturers Approved Sources 4920-01-199-0507

4920-01-199-0507 Technical Data Datasheet 4920-01-199-0507

Characteristic
Specifications
FIIG
A505C0
Functional Description [FTLD]
Used To Hold And Locate The Convergent Flap During The Machining Of The Link Tower Assembly Pads
End Item Identification [AGAV]
F100-Pw-220/220E
Nominal Overall Length [CWFR]
35.000 Inches
Nominal Overall Height [CYAG]
15.500 Inches
Nominal Overall Width [CXRQ]
11.500 Inches
Reference Data And Literature [RDAL]
Serd No. 5090; T.O. 2J-F100-94
Special Features [FEAT]
Aluminum; Company Item Name Fixture Machining Convergent Flap Link Tower; Item Supercedes Pwa55772

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4920-01-199-0507 Freight Data Freight Information 4920-01-199-0507

4920-01-199-0507 has freight characteristics.It has a National Motor Freight Classification (NMFC) of 186630. A Sub NMFC of X. It has a NMFC Description of TOOLS:NOI O/T PLSTC IN BBLS/BXS. 4920-01-199-0507 is rated as class 77.5 when transported by Less-Than Truckload (LTL) freight. 4920-01-199-0507 is rated as class 77.5 when transported by Less-Than Carload (LCL) rail or ocean freight. It has a Uniform Freight Classification (UFC) number of 91810 which rates the freight between FCL and LCL. 4920-01-199-0507 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 576 for ocean manifesting and military sealift. 4920-01-199-0507 is not classified as a special type of cargo when transported by water. 4920-01-199-0507 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.