199C6714G1

199C6714G1 Fluid Aircraft Manifold

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Quality Commitment

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Datasheet. 199C6714G1 specification

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

1.720in. ⁓1-47/64"

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

2.990in.

Mounting Hole Quantity
The number of mounting holes provided.

3

Overall Thickness
An overall measurement of the smallest dimension of an item,in distinction from length or width.

0.900in.

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

F110GE129 engine

Connection Quantity
The number of connections furnished.

2

Metering Valves
An indication of whether or not metering valves are provided.

not provided

Mounting Hole Location
Indicates the location of the mounting hole(s) in or on the item.

mounting flange

Criticality Code Justification
The master requirement codes of those requirements which are technically critical by reason of tolerance,fit,performance,or other characteristics which affect identification of the item.

feat

Special Features
Those unusual or unique characteristics or qualities of an item not covered in the other requirements and which are determined to be essential for identification.

nha r/N101E9750G01; 1459M52Xxx

Material
The element,compound,or mixture of which an item is fabricated,excluding any surface treatment.

aluminum alloy

Material
The chemical compound or mechanical mixture properties of which the item is fabricated.

aluminum alloy

Answers.

What quantity is this sold in?

1EA

What material is the fluid aircraft manifold made of ?

Aluminum alloy

What is the overall width?

2.990 inches

What is the NSN for 199C6714G1?

2995-01-325-8612

How is this classified for shipping?

Schedule B number: 8803909060
nmfc 133300
Other parts, for use in other military aircraft, spacecraft and spacecraft launch vehicles (excluding parts of communicat

What's the federal classification of 199C6714G1?

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 2995-01-325-8612 MANIFOLD,FLUID,AIRCRAFT

Used on f110ge129 engine. nha r/N101E9750G01; 1459M52xxx 2.990" overall width 1.720" overall length

NIIN
013258612
NIIN Date
09/12/90
Schedule B
8803909060 
Name Code
27020
FIIG
T261-F
Item Weight
0.000lbs
Item Dimensions
QUP
Historical Price
$5,212.13 EA
DEMIL / ITAR
USML/ITAR controlled item (Code: B)
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

Major End Users Countries and entities

  • - Department of The Air Force 
  • - 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)
Unknown
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
Supplies and equipment for aircraft and aerial targets, including aircraft and maintenance parts, aircraft accessories, aircraft 
Commodity (for shipments via water)
Motors and parts, (machinery and parts),(less than 35 feet) 
NMFC (national motor freight code)
133300 MACHINERY/MACHINES NOI 
UFC (universal freight code)
63220 

Similar by Design Other manifolds with similar characteristics

Nothing similar to this part number was found in our inventory

199C6714G1 / Manifold,fluid,aircraftWhat is the formal definition of this item?

An enclosure with three (3) or more openings designed for use in aircraft de-icing, fuel, hydraulic, oil, pneumatic, and vacuum systems to collect and/or distribute fluids. it may contain valves or metering devices and the like. excludes manifold, aircraft instruments.