부품 정보
T.O. 2j-f100-54, fig 99, ind 42; use only on p/ns 4084517-700 and 4083015-701; located near the rear compressor drive turbine rotor and stator assembly
TXT
묘사:
Aircraft Gas Turbin Turbine Disk
MRC:
The dimension measured along the longitudinal axis with terminated points at the extreme ends of the item.ABHP
Overall Length:
Between 1.809 inches and 1.811 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 36.696 inches and 36.736 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:
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:
Apgf and czbj and abmz and abhp and feat
MRC:
Indicates the location of the item on the engine section.CZBJ
Engine Section Location:
Turbine
MRC:
The number value that reflects the stage where the item is used.CZCJ
Stage Number:
1
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:
Pwa1106 mfr ref single material response
