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4920-01-388-0154

Aircraft Engine Maintenance Stand

4920013880154 013880154 PWA80345

A structure designed for overhauling, assembling, disassembling and repairing aircraft engines. See also STAND, AIRCRAFT ENGINE; TEST STAND, AIRCRAFT ENGINE and STAND, MAINTENANCE, RAIL TYPE. View more Aircraft Engine Maintenance Stand

4920-01-388-0154 STAND,MAINTENANCE,AIRCRAFT ENGINE 4920013880154 013880154

Managed by United States
NSN Created on 17 Mar 1994
Data Last Changed
January 2023
NATO Update Count
2
NATO Data Quality
4920-01-388-0154 STAND,MAINTENANCE,AIRCRAFT ENGINE 4920013880154 013880154 1/1
NSN 4920-01-388-0154 (Generic Image) 1/1

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Aircraft Engine Maintenance Stand 013880154 United States (US) 4. 4920-01-388-0154 Marketplace Restrictions

4920-01-388-0154 Demil Restrictions 4920-01-388-0154

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

IUID Required

4920-01-388-0154 is a Aircraft Engine Maintenance Stand 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.

4920-01-388-0154 HTS and ScheduleB Import and Export 4920-01-388-0154

4920-01-388-0154 End Users End Users 4920-01-388-0154

US Air Force (FBB5)
Effective Date:
1 May 2000
Former MOE Rule:
FECX

4920-01-388-0154 Manufacturers Approved Sources 4920-01-388-0154

4920-01-388-0154 Technical Data Datasheet 4920-01-388-0154

Characteristic
Specifications
FIIG
T361-C
Assembly Form [AFPM]
Rigid
Work Holding Device Position Adjustability [CGYB]
Adjustable
Overall Diameter [ADAV]
4.166 Feet Nominal
Overall Height [ABKW]
2.800 Feet Nominal
Functional Description [FTLD]
Required To Support The Lpc Rotor And Stator Assy,Rear End Down; Also Supports The Balance Arbor During Installation
End Item Identification [AGAV]
F117-Pw-100 Aircraft Engine

4920-01-388-0154 Management Data Management Data 4920-01-388-0154

Effective Date
Organization
Unit of Issue
Unit Price
Qty Unit Pack
May 2010
Department of the Air Force (DF)
EA
Subscribe

Air Force Air Force

Budget:
S
57X3010 - Aircraft Replenishment Spares
Aggregation Code:
BA
C-17 PROGRAM
Price Validation Code:
N
The current standard price in Catalog Management Data (CMD) has not analyzed or coded for LP/LM.
The price has not been analyzed or reviewed for accuracy.
ZOP or Standard price challenges are permissible but must be supported with adequate justification. However, if coded for Local Purchase (LP) or Fabrication/Manufacture as indicated with an (LM) Acquisition Advice Code of ā€œLā€ or ā€œFā€, then it must be evaluated locally where purchased or fabricated.
Expendability
Recoverability
Repairability:
P
Expendable. Reparable. Condemn at Intermediate. Stock Fund (except Munitions).

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4920-01-388-0154 Freight Data Freight Information 4920-01-388-0154

4920-01-388-0154 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. 4920-01-388-0154 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. 4920-01-388-0154 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. 4920-01-388-0154 is not classified as a special type of cargo when transported by water. 4920-01-388-0154 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.