رقم الجزء
تجريد
صلاحيه
UOM
NIIN
معلومات الجزء
T.O. 2j-f100-54; 4-9th stages; 58units per assembly; rear compressor, variable inlet
TXT
وصف:
Aircraft Gas Tur Compressor Vane
MRC:
The dimension measured along the longitudinal axis with terminated points at the extreme ends of the item.ABHP
Overall Length:
Between 4.721 inches and 4.733 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 means by which the blade is attached to the item.BGLW
Blade Attachment Method:
Pin
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 chemical compound or mechanical mixture properties of which the item is fabricated.MATT
Material:
Titanium alloy vane
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:
Ams4928 assn standard single material response vane
MRC:
The metallic,nonmetallic,and/or chemical properties with which the item is plated,dipped,and/or coated.the treatment is designed to protect the surface(s) and cannot be wiped off.SFTT
Surface Treatment:
Nickel vane
MRC:
The specification,standard,or manufacturers reference,and the classification designation,such as type,class,grade,and the like,that identifies the surface treatment material.STDC
Surface Treatment Specification:
Ams2433 assn standard single treatment response vane
