1851M34P02

1851M34P02 Supervisory Turbine Control Unit

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Datasheet. 1851M34P02 specification

Overall Length
The dimension measured along the longitudinal axis with terminated points at the extreme ends of the item.

12.800in. ⁓12-13/16"

Overall Height
The distance measured in a straight line from the bottom to the top of an item.

6.590in.

Overall Width
An overall measurement taken at right angles to the length of an item,in distinction from thickness.

16.710in.

End Item Identification
The national stock number or the identification information of the end equipment for which the item is a part.

u/o F110-100 acft engine

Features Provided
Those features,not otherwise specified,which may be required for proper functioning of the item.

electrostatic sensitive

Special Markings
Markings included on an item for the purpose of offering instructions or warnings or to indicate the purpose,function,or application of the item.excludes manufacturers part numbers,symbols,or the like.

high voltage to be printed on a red or yellow background; caution this equipment contains parts and assemblies susceptible to danage by electrostatic discharge (esd) . use esd precautionary procedures when touching removing or inserting parts or assemblies

Reference Number Differentiating Characteristics
A feature of the item of supply which must be specifically recorded when the reference number covers a range of items.

as differentiated by source control drawing

Answers.

What quantity is this sold in?

1EA

What is the overall width?

16.710 inches maximum

What is the NSN for 1851M34P02?

2995-01-429-4399

How is this classified for shipping?

Schedule B number: 8411997050
nmfc 061700
Parts of gas turbine aircraft engines, other than for use in civil aircraft

What's the federal classification of 1851M34P02?

FSC 2995 ⁓ Miscellaneous engine accessories, aircraft

Note-items classified in this class must be specifically designed for use with aircraft or quided missile primemovers only.

Excluding exhaust system; (fsc 1560); jet engine hydraulic reservoirs (fsc 2840); jet engine oil tanks (fsc 2840); electrical starters (fsc 2925); cockpit mounted control quadrants (fsc 1680); aircraft engine covers (fsc 1730).

NSN 2995-01-429-4399 CONTROL UNIT,SUPERVISORY,TURBINE

Used on u/o f110-100 acft engine. 16.710" overall width 12.800" overall length

NIIN
014294399
NIIN Date
04/10/96
Schedule B
8411997050 
Name Code
47093
FIIG
A23900
Item Weight
50.500lbs
Item Dimensions
250 X 190 X 165
QUP
Historical Price
$233,972.40 EA
DEMIL / ITAR
USML/ITAR controlled item (Code: D)
Hazmat
No hazard information available from HMIRS.
MSDS
N/A
Precious Metals
No precious metals
Enviromental
N/A
Electrostatic ESD & EMI
No ESD or EMI sensitivity

Other Part Numbers Parts with same form, fit, and function by other manufacturers

1. 105E7475G201 Cage 89954
2. 1851M34 Cage 07482

Major End Users Countries and entities

  • - Department of The Air Force  DSOR Oklahoma city air logistics complex (afsc), oc-alc, tinker afb, ok
  • - Greece 

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Shipping Information

Special Handling
Other or no special handling required (sh) 
LTL (less than a truck load rating)
Rating variable 
LCL (less than a car load rating)
85.0
Special Cargo
No special type of cargo code applicable 
Air Freight (Minimum cargo door size required)
Shipment is not a consolidation and does not exceed 84 inches in any dimension. 
Customs Requirement Classification
Instruments/equipment/supplies for radio, communications, electrical, laboratory, etc. (includes signal corps) 
Commodity (for shipments via water)
Communications/electronics, other than sigint/ew or comsec repair parts and components 
NMFC (national motor freight code)
061700 ELEC APPLIANCES/INSTRUMENTS NOI 
UFC (universal freight code)
34580 

Similar by Design Other control units with similar characteristics

Nothing similar to this part number was found in our inventory

1851M34P02 / Control unit,supervisory,turbineWhat is the formal definition of this item?

An electronic unit that continously monitors engine speed, temperature, and air flow and adjusts the fuel control, main, turbine engine to compensate for changes. features may include load sharing capabilities, rotor speed governing, loss-of-load protection and analog or manual backup modes. it may contain automatic start capability or self-diagnostic circuitry.