부품 정보
P/n not to be procured; p/n taken off engine and put into supply then reworked up to p/n 753538 (01-160-6504); depending on repair it will get assigned a different p/n; if this p/n has cracks in the tie rod holes will be assigned p/n 784473; if this item has nocracks, is reworked to p/n 774659
TXT
묘사:
Aircraft Gas Turb Compressor Hub
MRC:
The dimension measured along the longitudinal axis with terminated points at the extreme ends of the item.ABHP
Overall Length:
12.726 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 16.741 inches and 16.743 inches
MRC:
The national stock number or the identification information of the end equipment for which the item is a part.AGAV
End Application:
Tf-33 aircraft gas turbine engine
MRC:
Indicates the design type of the item.APGF
Design Type:
Axial compressor
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 and abhp and abmz and czbj
MRC:
Indicates the location of the item on the engine section.CZBJ
Engine Section Location:
Compressor
MRC:
The chemical compound or mechanical mixture properties of which the item is fabricated.MATT
Material:
Steel
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:
Ams6415 assn standard single material response
MRC:
Literature and references available for information pertaining to the item.RDAL
Reference Data And Literature:
T.O. 2j-tf33-34, fig 6, ind 51
