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4920-01-393-1721

Aircraft Engine Maintenance Machining Fixture

4920013931721 013931721 PWA81943

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

4920-01-393-1721 FIXTURE,MACHINING,AIRCRAFT ENGINE MAINTENANCE 4920013931721 013931721

Managed by United States
NSN Created on 15 Jul 1994
Data Last Changed
January 2023
NATO Update Count
2
NATO Data Quality
4920-01-393-1721 FIXTURE,MACHINING,AIRCRAFT ENGINE MAINTENANCE 4920013931721 013931721 1/1
NSN 4920-01-393-1721 (Generic Image) 1/1

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United States (US) 4. 4920-01-393-1721 Marketplace Restrictions Approved Sources Datasheet Management
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4920-01-393-1721 Demil Restrictions 4920-01-393-1721

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

IUID Required

4920-01-393-1721 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.

4920-01-393-1721 HTS and ScheduleB Import and Export 4920-01-393-1721

4920-01-393-1721 End Users End Users 4920-01-393-1721

US Air Force (FBB4)
Effective Date:
1 Dec 2000
Former MOE Rule:
FXX4

4920-01-393-1721 Manufacturers Approved Sources 4920-01-393-1721

4920-01-393-1721 Technical Data Datasheet 4920-01-393-1721

Characteristic
Specifications
FIIG
A505C0
Functional Description [FTLD]
Used To Perform The Honeycomb Replacement, The Snap Diameter-And-Matingfaces Repair, And The Scallop Change Repair To The Turbine Ring Airseal Assembly
End Item Identification [AGAV]
C-17 Aircraft Engine F117-Pw-100
Nominal Overall Diameter [CZDH]
26.000 Inches
Nominal Overall Height [CYAG]
6.300 Inches
Reference Data And Literature [RDAL]
Serd No. 1116; T.O. 32-1-294
Special Features [FEAT]
C/O A Steel Base Ring, A Locating Ring, A Clamping Ring, And Six Stud-And-Nut Assemblies

4920-01-393-1721 Management Data Management Data 4920-01-393-1721

Effective Date
Organization
Unit of Issue
Unit Price
Qty Unit Pack
Dec 2012
Department of the Air Force (DF)
EA
Subscribe
1

Air Force Air Force

Budget:
Q
57X3010 - Aircraft Weapon Systems and Peculiar Support Equipment
Aggregation Code:
BE
C-17 ENGINE
Price Validation Code:
P
The current standard price is the initial negotiated provisioned price.
This is the price paid by DoD for the item as the result of price negotiation of the Provisioned Item Order (PIO) or other initial negotiated price.
ZOP or Standard Price challenges are permissible but should be supported with adequate justification.
Expendability
Recoverability
Repairability:
U
Reparable. Condemn at Intermediate. AF Equipment Management System (AFEMS).

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4920-01-393-1721 Freight Data Freight Information 4920-01-393-1721

4920-01-393-1721 has freight characteristics.It has a National Motor Freight Classification (NMFC) of 147650. A Sub NMFC of X. It has a NMFC Description of OUTFITS MILITARY EQUIP FOR REPAIR. 4920-01-393-1721 is rated as class 77.5 when transported by Less-Than Truckload (LTL) freight. It has a Uniform Freight Classification (UFC) number of 73790 which rates the freight between FCL and LCL. 4920-01-393-1721 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 671 for ocean manifesting and military sealift. 4920-01-393-1721 is not classified as a special type of cargo when transported by water. 4920-01-393-1721 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.