Figure 1. Aircraft hydraulic test stand, three-quarter, right front view.

lutions per minute) by a centrifugal fly-weight

door assembly (2), front right door assembly

governor which adjusts the throttle to compen-

(10), and left front door assembly (1, fig. 2)

sate for changes in engine load. A handcrank,

are opened to gain access to the engine com-

for manually cranking the engine, is secured

partment.

to the frame in the engine compartment of the

d. Hydraulic Reservoir. The hydraulic reser-

test stand. Controls for operating the engine

voir is mounted in the upper left rear corner

are made accessible by opening the control

of the housing assembly with the reservoir fill

panel door assembly (1, fig. 1). The f rent top

cap (4, fig. 2) extending through the rear top

Front panel assembly

Control panel door assembly

9 Pneumatic tire

10 Right front door assembly

Front top door assembly

Thumbscrew

Frame assembly

11 Spring

Drawbar assembly

Brake lever assembly

Housing assembly

Figure 1. Aircraft hydraulic test stand, three-quarter, right front view.

AGO 5742A