부품 정보
T.O. 2j-f100-54, fig 99, ind 21; repl p/n 4074864 once tcto has been accomplished; retaining plate damper is symmetrical in shape and has 6 retention tabs forward and aft to preclude possible reverse installation and resulting cut-off of cooling air to the 2nd stage blades
TXT
묘사:
Aircraft Tu Turbine Blade Damper
MRC:
The dimension measured along the longitudinal axis with terminated points at the extreme ends of the item.ABHP
Overall Length:
Between 0.565 inches and 0.571 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:
16.788 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:
A numeric value that reflects the hardness of an item when used in conjunction with a hardness rating scale.CQFM
Hardness Rating:
34.0 rockwell c and 44.0 rockwell c
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 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:
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:
Ams5544 assn standard single material response
