부품 정보
Original name spool, compressor rotor
TXT
묘사:
Aircraft Gas Tu Compressor Rotor
MRC:
The dimension measured along the longitudinal axis with terminated points at the extreme ends of the item.ABHP
Overall Length:
Between 6.143 inches and 6.163 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:
17.300 inches
MRC:
The national stock number or the identification information of the end equipment for which the item is a part.AGAV
End Application:
F110-ge-100 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:
High pressure compressor
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-f110-14, fig 67, ind 5 under p/n 1559m63g02; includes stage 2; also consists no. 1 disk and no. 2 disk and forward shaft that makes a 1 piece construction that holds both stgs; weighs 40.3 lbs; basic p/n can be used on all engine types, but once used on the f110, it can only be used on an f110 engine; reidentification will consist of adding the engine type as a dash number following the p/n
MRC:
The chemical compound or mechanical mixture properties of which the item is fabricated.MATT
Material:
Titanium 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:
Ti-17 mfr ref single material response