TXT
묘사:
Aircraft Turbine Shroud Segment
MRC:
The dimension measured along the longitudinal axis with terminated points at the extreme ends of the item.ABHP
Overall Length:
Between 0.855 inches and 0.865 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 17.954 inches and 17.964 inches
MRC:
The national stock number or the identification information of the end equipment for which the item is a part.AGAV
End Application:
F100pw0229 aircraft 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:
Agav
MRC:
Indicates the location of the item on the engine section.CZBJ
Engine Section Location:
Compressor
MRC:
The number value that reflects the stage where the item is used.CZCJ
Stage Number:
9
MRC:
The chemical compound or mechanical mixture properties of which the item is fabricated.MATT
Material:
Nickel alloy
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:
Ams5536 assn standard 1st material response and ams5666 assn standard 2nd material response
