TOMARK, s.r.o.
Airplane Maintenance Manual
Chapter 05 Inspection and Maintenance
Issue: 04.APR 2016
Page 59
Max Continues Power Level Flight
Fly the aircraft at full throttle (climb). Build up speed in moderately
into level flight and reduce RPM gradually until MCP (5500RPM) is
reached. Allow the aircraft to stabilize for some time. Fly this
maneuver as stationary as possible. Write down the requested
parameters. Compare this data with the data displayed in the airplane
flight manual. (Fly this maneuver at minimum safe altitude). The
corrected flight data should correlate with the data in the airplane
flight manual.
05-21-20 System Tests
The system tests are meant for checking the systems of the aircraft.
The systems are subdivided into 7 groups. For each group the
relevant systems are indicated on the form. Check their functionality
and indication where relevant. On the form indicate an acceptable
functionality with a “+”. A functionality which is not acceptable should
be indicated with a “-“. Use the reverse of the form to write down
possible comments or complaints. Try to be as accurate as possible in
writing the comments/complaints. This will allow maintenance
personnel to handle this adequately.
05-21-21 Flight Controls
Elevator/Aileron/Rudder/Flap
Check the elevator/aileron/rudder controls for smooth operation and
forces as expected. Do not apply full or abrupt control inputs at
speeds above V
A
(88 KIAS). While increasing speed do not allow the
speed to increase above V
NE
(126 KIAS), keep engine RPM within
limits. While decreasing speed do not stall the aircraft. Check controls
with all possible flap settings. DO NOT spin the aircraft! The
maximum speed with flaps intermediate and full flaps is 79 KIAS.
Longitudinal Trim
Operate the trim through the full range. It should be possible to trim
the aircraft in a speed range above 50 KIAS at Full throttle and flap up
as well as 65 KIAS at 3500 RPM and flap 30°. A larger trim range is
