부품 정보
Original name frame assembly, turbine
TXT
묘사:
Aircraft Gas Turbine Rear Frame
MRC:
The length of a straight line which passes through the center of a circular figure or body,and terminates at the inside circumference.AARX
Inside Diameter:
Between 15.495 inches and 15.535 inches
MRC:
The dimension measured along the longitudinal axis with terminated points at the extreme ends of the item.ABHP
Overall Length:
Between 4.517 inches and 4.531 inches
MRC:
The length of a straight line which passes through the center of a circular figure or body,and terminates at the outside circumference.ABKV
Outside Diameter:
Between 16.995 inches and 17.005 inches
MRC:
The national stock number or the identification information of the end equipment for which the item is a part.AGAV
End Application:
J85 aircraft 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:
Abhp and abkv and aarx and czlb
MRC:
The number of variable guide vanes included as part of the strut.CZLB
Number Of Variable Guide Vanes:
6
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:
Mainframe compressor section; must conform to as367 safety wire, key washers and cotter pin
MRC:
The chemical compound or mechanical mixture properties of which the item is fabricated.MATT
Material:
Nickel alloy
MRC:
Literature and references available for information pertaining to the item.RDAL
Reference Data And Literature:
T.O. 2j-j85-54, fig 13, ind 1
