Quantcast Section III. TECHNICAL PRINCIPLES OF OPERATION - TM-55-4920-426-13-P0022

 

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Table 1-1. Leading Particulars (Cont)
Up
TM-55-4920-426-13-P Gasoline Engine Driven Hydraulic Systems Test Stand Type Type D5-D P/N 79009-100 NSN
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Chapter 2. OPERATING INSTRUCTIONS - TM-55-4920-426-13-P0023
TM 55-4920-426-13&P
Section Ill. TECHNICAL PRINCIPLES OF OPERATION
1-10
1-10
HYDRAULIC OPERATIONS
a.
Hydraulic fluid, taken from the test stand reservoir or the aircraft reservoir, is forced under pressure by
the test stand high pressure pump (directly driven by the gasoline engine), first through a relief valve,
check valve, high pressure filter and a two way selector valve to the supply port on the test stand and
then to the aircraft being tested through one of the external hoses provided.
The fluid is then returned to the test stand. Complete instrumentation is provided on the control panel
b.
to indicate test stand engine rpm, oil pressure and alternator output, plumbing system pressure, return
flow gpm, hydraulic fluid temperature, hydraulic fluid reservoir level and fuel level.
1-11
1-11.
HOSE
Hose assemblies are furnished with the test stand to connect the stand to the aircraft. The hoses are stored on
two hooks, located on the front of the test stand.
1-12

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