Quik & Quik GT450 Aircraft Operating Instructions
29
th
March 2007
Issue 1
Page 45 of 68
Stalls
At 450kg max AUW & 270kg min Auw
All Models
Wings level stall, power off, MAUW
38mph
Height loss during recovery, MAUW
60ft
Max. pitch down below horizon
30
o
Wings level stall, power on, MAUW
39mph
Height loss during recovery, MAUW
0ft
Max. pitch down below horizon, MAUW
0
o
30 degree banked stalls, power on, @ Max AUW
40mph
Wings level stall, power off, @ Min AUW
30mph
Height loss, during recovery @ Min AUW
50ft
Max. pitch down below horizon @ Min AUW
30
o
Wings level stall, power on, @ Min AUW
30mph
Max. pitch down, power on recovery, @ Min AUW
0
o
30 degree banked stalls, power off, @ Min AUW
31mph
NOTE
(
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. If accelerated and
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.
WARNING
!
