SCHEMPP-HIRTH FLUGZEUGBAU GmbH., KIRCHHEIM/TECK
Ventus-2cM
FLIGHT MANUAL
(4)
a)
Check fuselage for damage, especially on its lower side.
b)
Check that the Static pressure ports for the airspeed indicator on
the tail boom are clear (0.8 m / 2.62 ft forward of the base of the fin)
Visual inspection of the power plant
(See also Engine Manual, page 3)
CAUTION:
IGNITION TO BE SWITCHED OFF !
c)
Check propeller pylon during extension for sufficient clearance to the
rim of the engine compartment
d)
Check propeller for damage
e)
Check power plant for loose bolt and nuts,
check all locks and stops
f)
Check exhaust system, engine pylon and propeller mounting structure
for cracks (check metal parts especially at the welding joints)
g)
Check all components, lines, hoses, pipes and wires etc. for chafing
marks
h)
Check engine arresting wires and their attachment for proper condition
i)
Check engine door actuating mechanism for proper function
j)
Check for proper function: Throttle control, manual primer
(when squeezing rubber bulb, air must be expelled through hole in lid of
carburetors)
and
prop arresting device
Note: With the prop arresting device open check that there is a
clearance of about 1 mm (0.039 in.) through 2 mm (0.0787 in.)
between ball bearing and propeller hub
k)
Check ignition system, ignition harness and lead ends for proper
seating
l)
Check drive belt for wear
m) Rotate propeller by hand repeatedly and listen for abnormal noise.
Check for engine binding.
n)
Depress fuel drain (at the bottom of the fuselage, aft of the under-
carriage) and discharge condensed water.
Check that the drain outlet is clear
November
2003
LBA-app.
Revision --
4.3.3
Summary of Contents for Ventus-2cM
Page 11: ......
