D IAMOND AIRCRAFT
HK 36 TS
FLIGHT MANUAL
Emergency
Procedures
3 .4
STALL RECOVERY
3 . 4 . 1 Behavior with
off
Under a l l l oading conditions , air brakes appl i ed or retracted , wings
level f l ight or banked f light , the HK 36 TS goes through a horizontal
sta l l . The a i l erons keep their effectiveness even with maximum
elevator deflection .
A partial l oss of posi ti ve control in the stick and pedals, buffeting ,
and pitch angle of 2 0" to 3D" occur during this condition .
NOTE
During the horizontal stal l , lAS rises to approximately
8 5 km/h ( 46 kts . / 53 mph ) .
3 . 4 . 2 Behavior with
on
See behavior with power off .
Only at 5 0
%
to 1 0 0
%
power , wings level f l ight , and maximum rearward
center of gravity , the airplane may perform a sta l l dive over the
left or right wing after entering the hor i zontal sta l l i f the control
stick is pulled even further .
3 . 4 . 3
The hori zontal stall can be terminated immediately by r e l axing the
force on the e levator control .
NOTE
I f the airplane performs a stal l dive , immedi ately r e l ax
the force on the e levator control and pull
out the
airplane smoothly .
I f the stick i s pull ed further, the airplane may start
to spin .
Altitude loss resulting froIrI. stationary hor i z ontal stall
described above : approximately 1 0 - 2 0 m ( 33-65 ft . ) .
Altitude loss resulting from stal l dive over a wing :
approximately 4 0 m ( 130 ft . ) .
Revision No .
Date
Source
Doc . No .
I ssue
Page
3 . 01 . 0 6
Jan 1 9 9 6
3-3
No .
