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Figure 2. Aircraft hydraulic test stand, three-quarter, left rear view.
Up
TM-55-4920-226-15 Test Stand Aircraft Hydraulic AHT-5A-1 Type D-5A Manual
Next
Figure 5. Shipping dimensions.
5. Deviations in Models
This manual covers only the Sun Electric
Corporation, Model AHT5A1, Type D5A.
No known unit differences exist for the model
covered by this manual.
6. Tabulated Data
a. Aircraft Hydraulic Test Stand.
Manufacturer-------------------------Sun  Electric  Corporation
Figure 3. Aircraft hydraulic test stand
Model------------------------------------AHT-5A-1
identification plate.
Operating range:
Altitude. ------------------------- Sea level to 6000 ft.
Ambient temperature ------20 F. to 130 F.
Humidity ------------------------95 to 100 percent
Deflection ---------------------- 8 in any plane from
horizontal.
b. Engine.
Manufacturer----------------------Wisconsin  Motor  Corp.
Model------------------------------MVG4D
Cycle----------------------------------4
stroke
Cylinders-------------------------4
Cooling-------------------------Air
Cylinder  bore---------------------3  in.  (inch)
Stroke--------------------------------4
in.
Piston displacement--------------l54 cu in (cubic inch)
Horsepower------------- -----------36 at 2200 rpm
Firing  order--------------------1 - 3 - 4 - 2
c. Hydraulic Pump.
Figure 4. Engine identification plate.
Manufacturer------------------------Denisen
Engineering
Company
4. Identification
Model----------------------------------PA072-564X201J
Type-----------------------------------Axial
piston,
variable
a. The manufacturer's identification plate
volume
(fig. 3), is located in the lower right rear cor-
Pressure output----------------------0 to 6000 psi
ner of the housing assembly and specifies type,
Volume output------------------------0 to 10 gpm
specification, contract number, Federal stock
d. Capacities.
number, manufacturer's part number, serial
Engine crankcase------------------5 qt (quart)
number, weight, towing speed, and rating of
Engine fuel tank-----------------13 gal. (gallon)
the hydraulic test stand.
Hydraulic reservoir---------------------26.8 gal.
b. The engine identification plate (fig. 4),
e. Dimensions and weight.
mounted on the engine air shroud inside the
Overall length ---------------------76 in.
engine compartment, specifies the make, model,
Overall width-----------------------57 in.
serial number, and operating instructions of
Overall height----------------------53 in.
the engine.
Weight--------------------------------2200  lb.
(pound)
AGO 5742A

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