رقم الجزء
تجريد
صلاحيه
UOM
NIIN
معلومات الجزء
T.O. 2j-f100-14, fig 130, ind 9; interim blade replaces p/n 4067004 and is replaced by p/n 4084804 per ecp 95-na027
TXT
وصف:
Aircraft Gas Turbine Rotor Blade
MRC:
The dimension measured along the longitudinal axis with terminated points at the extreme ends of the item.ABHP
Overall Length:
Between 6.771 inches and 6.781 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 29.004 inches and 29.404 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-100 aircraft gas turbine 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:
Fir tree
MRC:
A numeric value that reflects the hardness of an item when used in conjunction with a hardness rating scale.CQFM
Hardness Rating:
45.0 rockwell c and 55.0 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 abmz and abhp and czbj
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:
4
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:
Pwa658 mfr ref single material response
