رقم الجزء
تجريد
صلاحيه
UOM
NIIN
معلومات الجزء
6turbine mid frame assembly; new frame to reduce number of liner saddle and blipper cracks; g10 frame has new liner, 1820m83g01, which incorporates a redesigned blipper, higher in strength/temperature; intergal with the liner foward out ring instead of being welded to the ring as of now; turbine mid frame not affected in physical interchangeability; new liner and current liner are physically interchangeable; functional interchangeability is affected in that the new liner has higher strength/temperature
TXT
وصف:
Aircraft Gas Turbi Turbine Frame
MRC:
The dimension measured along the longitudinal axis with terminated points at the extreme ends of the item.ABHP
Overall Length:
Between 13.165 inches and 13.205 inches
MRC:
The length of a straight line which passes through the center of a circular figure or body,and terminates at the outside circumference.ABKV
Outside Diameter:
Between 16.160 inches and 16.200 inches
MRC:
The national stock number or the identification information of the end equipment for which the item is a part.AGAV
End Application:
Tf-39 aircraft gas turbine engine
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:
Abhp and abkv and feat
MRC:
The chemical compound or mechanical mixture properties of which the item is fabricated.MATT
Material:
Nickel alloy
MRC:
Literature and references available for information pertaining to the item.RDAL
Reference Data And Literature:
T.O. 2j-tf39-4, fig 63 ind 1
