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4920-01-079-6143
Aircraft Engine Test Stand
4920010796143 010796143 289445-3
A device designed to test the performance and/or operational characteristics of aircraft engines. For mobile items, see TEST STAND, ENGINE, SEMITRAILER MOUNTED. See also STAND, AIRCRAFT ENGINE; and STAND, MAINTENANCE, AIRCRAFT ENGINE. View more Aircraft Engine Test Stand
January 2023
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Restrictions 4920-01-079-6143
IUID Required
4920-01-079-6143 is a Aircraft Engine Test Stand 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.
Import and Export 4920-01-079-6143
- Schedule B
- Subscribe to View Schedule B
- HTS Code
- Subscribe to View HTS Code
End Users 4920-01-079-6143
- US Air Force (FXX4)
- Effective Date:
- 1 Apr 1991
- US Navy (NAXS)
- Effective Date:
- 1 Mar 2005
- Supplementary Receivers:
- GG
Approved Sources 4920-01-079-6143
- Part Number
- Manufacturer
- Status
- 289445-3
- Manufacturer
- 59364 - Honeywell International Inc. (Active)
- Primary Buy
- Primary Buy
- 289445-3
- 99193 - Honeywell International Inc. (Active)
- Canceled/Obsolete
- Canceled/Obsolete
Datasheet 4920-01-079-6143
- Characteristic
- Specifications
- FIIG
- Specifications
- T361-D
- End Item Identification [AGAV]
- Starter, Engine, Air Turbine
- Engine Model Tested [CGYD]
- Wide Variety Of Jet Engine Starters
- Functional Description [FTLD]
- Provides A Test Facility With Capability For Functionally Testing A Wide Variety Of Pneumatic Turbine-Type, Turbofan Or Turbojet Engine Starters
- Reference Data And Literature [RDAL]
- T.O. 33D4-6-594-1
- Special Features [FEAT]
- O/A Dim: 64.000 In. Lg., 26.000 In. H., 36.000 In. W.; 28 Vdc; 15 Amps; C/O Base Which Supports An Overspeed Drive Assy With Mounting Flange And Muffler, A Disconnect Assy, Load Cell And Spot Disk Brake Assy.; Pneumatic Supply: 15Lb/Min Max At 200 Psig Max
- Test Type For Which Designed [AQXY]
- Engine Air Turbine Starter
Management Data 4920-01-079-6143
Air Force
- Budget:
- Y
- Centrally procured equipment items. They are separate, primary end items (other than the weapon system itself) needed by a user to perform an assigned mission. They are non-expendable items (ERRC NF or ND) which are not consumed in use, and they do not lose their original identity during periods of use by incorporation into, or attachment to another assembly
- Aggregation Code:
- YQ
- ENGINE ACCESSORIES, AIRCRAFT
- Price Validation Code:
- X
- The current standard price has been validated and the previous price was erroneous.
The item was overpriced and the contractor has refunded the overcharge or DoD activities did not actually pay the previous price. The price paid is within the analyzed acceptable range.
If the difference from the previous price exceeds $99.99 or if the price change exceeds 500 percent and the extended value of any affected transaction exceeds $99.99, then reverse-post procedures will apply where the stock fund has overcharged unit O&M Funds. These corrections will be limited to the current fiscal year.
ZOP or Standard Price challenges are permissible but should be supported by adequate justification.
- Expendability
Recoverability
Repairability: - U
- Reparable. Condemn at Intermediate. AF Equipment Management System (AFEMS).
Navy
- Cognizance:
- 6R
- Bypass
- Special Material ID:
- VH
- MARK III Helicopters (SH-60B)
- Issue, Repair, Requisition Restriction Code:
- BS
- Submit/refer requisitions to NAVICP PHIL
- Special Material Content:
- 9
- Non-Hazardous or Non-Sensitive Item
NATO Stock Numbers Related to 4920-01-079-6143
Freight Information 4920-01-079-6143
4920-01-079-6143 has freight characteristics.. 4920-01-079-6143 has a variance between NMFC and UFC when transported by rail and the description should be consulted.