P&M Aviation QUIK GT450 Operating Instructions Manual page 45

Stalls
At 450kg max AUW & 270kg min Auw
Wings level stall, power off, MAUW
Height loss during recovery, MAUW
Max. pitch down below horizon
Wings level stall, power on, MAUW
Height loss during recovery, MAUW
Max. pitch down below horizon, MAUW
30 degree banked stalls, power on, @ Max AUW
Wings level stall, power off, @ Min AUW
Height loss, during recovery @ Min AUW
Max. pitch down below horizon @ Min AUW
Wings level stall, power on, @ Min AUW
Max. pitch down, power on recovery, @ Min AUW
30 degree banked stalls, power off, @ Min AUW
(See also Section 7.5 paragraph on Stall Characteristics.)
It is important to understand that the data recorded during wings level
stall tests were ascertained using the CAA requirement of a reduction of
airspeed of not more than 1 knot per second.
therefore unauthorised stalls are undertaken, the aircraft may then lose
significant height before recovery is made, or in extreme cases, may
become unstable to the extent of being unrecoverable.
Quik & Quik GT450 Aircraft Operating Instructions
th
29 March 2007
Issue 1
NOTE
WARNING
!
All Models
38mph
60ft
o
30
39mph
0ft
o
0
40mph
30mph
50ft
o
30
30mph
o
0
31mph
If accelerated and
Page 45 of 68