부품 정보
Original name seal brush, combustion chamber, outer assembly
TXT
묘사:
Aircraft Gas Turbine En Air Seal
MRC:
The dimension measured along the longitudinal axis with terminated points at the extreme ends of the item.ABHP
Overall Length:
Between 0.258 inches and 0.268 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 25.004 inches and 25.008 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:
Czbj and abhp and abmz and feat
MRC:
Indicates the location of the item on the engine section.CZBJ
Engine Section Location:
Combustion chamber
MRC:
The number value that reflects the stage where the item is used.CZCJ
Stage Number:
1
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:
T.O. 2j-f100-54, fig 86, ind 19f; use only on p/ns 4083194, 4083560, and 4083565; contains wire brush, 2250-2650 wires per circumferential inch; located near the rear compressor drive turbine rotor and stator assembly; turbine stator support and combustion chamber
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:
Ams5599 assn standard 1st material response or ams5666 assn standard 2nd material response
