رقم الجزء
تجريد
صلاحيه
UOM
NIIN
معلومات الجزء
Original name duct segment, compressor
TXT
وصف:
Aircraft Gas Tur Compressor Duct
MRC:
The dimension measured along the longitudinal axis with terminated points at the extreme ends of the item.ABHP
Overall Length:
12.130 inches
MRC:
An overall measurement taken at right angles to the length of an item,in distinction from thickness.ABMK
Overall Width:
Between 2.320 inches and 2.326 inches
MRC:
The length of a straight line which passes through the center of a circular figure or body,and terminates at the circumference.ABMZ
Diameter:
Between 27.647 inches and 27.659 inches
MRC:
The national stock number or the identification information of the end equipment for which the item is a part.AGAV
End Application:
F100-pw-229 aircraft gas turbine engine
MRC:
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.CRTL
Criticality Code Justification:
Abmk and abhp and abmz and feat
MRC:
Indicates the location of the item on the engine section.CZBJ
Engine Section Location:
Compressor
MRC:
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.FEAT
Special Features:
No 3. Bearing real seal assembly, rear compressor stator variable inlet vanes, exit fan stator and compressor intermediate case assembly; stage 4; replaces p/n 4081682-01; corrosion resistant segments
MRC:
The chemical compound or mechanical mixture properties of which the item is fabricated.MATT
Material:
Nickel alloy duct
MRC:
The specification,standard,or manufacturers reference,and the classification designation,such as class,condition,temper,and the like,that identifies the material.MDCL
Material Specification:
Ams5771 assn standard single material response duct
MRC:
Literature and references available for information pertaining to the item.RDAL
Reference Data And Literature:
T.O. 2j-f100-54, fig 84, ind 16 and 17
