부품 번호 26002

Hydraulic System Comp Test Stand

가격 및 가용성

이 NSN의 현재 가격 및 가용성에 대해 이 양식을 제출하십시오.
부품 번호:
양:
이메일 주소:
전화:
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이름:

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All major credit cards accepted as well as gov. p-cards

이 제품의 과거 가격은 82990.7 and 108526.3 USD. 수량, 가용성, 상태, 리드 타임 및 품목 중단 가능성에 따라 최신 견적을 제공할 때까지 가격을 보장할 수 없습니다.

부품 번호
비무장화
수명
UOM
NIIN
부품 번호:
26002
비무장화:
No
수명:
N/A
측정 단위:
1 EA
NIIN:
014341081

부품 정보
Diesel driven powered dual sub-system test stand

NSN
국가 주식 번호:
4920-01-434-1081 4920014341081
TXT
묘사:
Hydraulic System Comp Test Stand
INC
INC
아이템 이름 코드:
11017
MRC:
The national stock number or the identification information of the end equipment for which the item is a part.AGAV
End Application:
Multi-acft
MRC:
Indicates the designed use of the item.ALBY
Usage Design:
Aircraft hydraulic system
MRC:
The installation for which the item is designed.AMQY
Installation Design:
Portable
MRC:
The source of power which drives the item.ATJK
Power Source:
Gasoline engine
MRC:
An indication of whether or not an accumulator is included.AYJM
Accumulator:
Included
MRC:
The pressure at which an item is designed to operate.BGST
Pressure Rating:
Between 3000.0 pounds per square inch and 6000.0 pounds per square inch
MRC:
An indication of whether or not a design feature for testing engine driven hydraulic pumps is included.CGYK
Engine Driven Hydraulic Pump Testing Design Feature:
Not included
MRC:
An indication of whether or not a filtering system is included.CHGQ
Filtering System:
Included
MRC:
An indication of whether or not a pressure and suction hose are included.CHGR
Pressure/suction Hose:
Included
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:
Used for type iii; the drive system is the only primary difference fromthe electric counterpart
MRC:
Describes the capabilities,intended use,and/or purpose for which the item is provided.FTLD
Functional Description:
Used to pressurize aircraft hydraulic system without having to use aircraft engine or auxilary power unit; this pressurization allows functional check of flight control system/landing gear operation prior to aircraft flightto ensure no malfunctions are occuring
MRC:
Literature and references available for information pertaining to the item.RDAL
Reference Data And Literature:
Mil-prf-38381

{lang[cimilar]} Hydraulic System Comp Test Stands

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