부품 정보
Original name frame, front, aircraft gas turbine engine
TXT
묘사:
Aircraft Gas Turbine Rear Frame
MRC:
The national stock number or the identification information of the end equipment for which the item is a part.AGAV
End Application:
Aircraft eng tf39
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:
Feat
MRC:
The number of variable guide vanes included as part of the strut.CZLB
Number Of Variable Guide Vanes:
8
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:
Used on the rear turbine frame; rwkd from p/n 9686m32g23; not an assembly
MRC:
The chemical compound or mechanical mixture properties of which the item is fabricated.MATT
Material:
Steel
MRC:
Literature and references available for information pertaining to the item.RDAL
Reference Data And Literature:
T.O. 2j-tf39-4, fig 69, ind 17
