Vliegclub Schiphol
Version 0.7, March 2013
PH-TDS Procedures Quick Reference Guide Page
17
Power
-‐
On Stalls
•
NOTE:
The power on stall may cause one wing to
be more stalled than the
other (usually due to uncoordinated flight)
causing the wing to drop. Use
coordinated rudder and aileron inputs
to level the wings.
SET UP
•
Find practice area where terrain is appropriate for maneuvering with an
available emergency landing area
•
Perform the maneuver no lower than 1000 AGL
PERFORMANCE
1.
Reduce power to 60%
2.
Clear the area
3.
Pre-‐maneuver check
4.
Slow to V
R
(59 KIAS)
5.
Simultaneously pitch up and increase throttle to 80%
6.
Recognize symptoms of approaching stall
•
Airspeed and noise level decrease
•
High nose attitude
•
Flight controls are less effective and feel “mushy”
•
Stall warning horn activates
•
Aerodynamic buffeting
RECOVERY
1.
Release enough back pressure to break the stall
2.
Simultaneously apply full power
3.
Establish a shallow climb (100 – 200 FPM)
4.
At positive rate of climb and approaching 73 KIAS
5.
Retract flaps to UP
6.
Set climb power
•
NOTE:
This stall may not cause any loss of altitude. In this case, lower the
nose to maintain altitude and set cruise power, and refer to CRUISE checklist.
7.
Climb at 80 KIAS to initial altitude
