رقم الجزء 6051T95G01

Aircraft Gas Turbine Rear Frame

الأسعار والتوافر

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رقم الجزء:
كم:
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التسعير التاريخي لهذا المنتج هو بين 31606.12 and 41331.08 USD. اعتمادا على الكمية والتوافر والحالة والمهلة الزمنية والتوقف المحتمل للعنصر ، لا يمكننا ضمان التسعير حتى نقدم لك عرض أسعار محدث.

رقم الجزء
تجريد
صلاحيه
UOM
NIIN
رقم الجزء:
6051t95g01
تجريد:
Yes - DEMIL/MLI
صلاحيه:
N/A
وحدة القياس:
1 EA
NIIN:
012639333

معلومات الجزء
Original name frame assembly, turbine

NSN
رقم المخزون الوطني:
2840-01-263-9333 2840012639333
TXT
وصف:
Aircraft Gas Turbine Rear Frame
INC
INC
رمز اسم العنصر:
52347
INC
COM
امتثال:
MRC:
The length of a straight line which passes through the center of a circular figure or body,and terminates at the inside circumference.AARX
Inside Diameter:
Between 15.495 inches and 15.535 inches
MRC:
The dimension measured along the longitudinal axis with terminated points at the extreme ends of the item.ABHP
Overall Length:
Between 4.517 inches and 4.531 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 16.995 inches and 17.005 inches
MRC:
The national stock number or the identification information of the end equipment for which the item is a part.AGAV
End Application:
Acft.Eng. J85
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 aarx and czlb
MRC:
The number of variable guide vanes included as part of the strut.CZLB
Number Of Variable Guide Vanes:
6
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:
Mainframe compressor section
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-j85-54, fig 13, ind 1

{lang[cimilar]} Aircraft Gas Turbine Rear Frames

« Gas Turbines and Jet Engines, Aircraft, Prime Moving; and Components {lang[catalog]}
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