JS-MD 1C Aircraft Flight Manual
MD01-AFM-00-001
Issue: 02
Rev. 00
Rev. Date: 14.09.2017
Page 3–3
3.4 Stall recovery
The JS-MD 1C has a very mild stall with ample warning. Stalls can
easily be recognised by the following:
•
The nose is in a higher than normal attitude relative to the
horizon
•
A slight shudder approximately 2 km/h before the stall
•
Airspeed indicator starts fluctuating near the stall
•
A slight increase in the sink rate
•
Aileron effectiveness decreases considerably
The stall recovery procedure is to release the back pressure on the
control stick and move it towards the neutral position.
CAUTION:
During stalled flight if the angle of attack is increased
by further pulling back on the stick, a wing drop may
occur. This asymmetric stall may result in a spin if
incorrect stall recovery procedures are used.
NOTE
:
When a stall is initiated by pulling with the nose to a
high pitch angle (in excess of 30° above the horizon),
the nose may pitch down well below the horizon during
the recovery and the altitude loss during recovery may
exceed 60 m or 200 ft.
NOTE
:
When a stall is initiated with 45° bank, and the resulting
roll is not prevented with the use of opposite rudder, a
loss of altitude exceeding 100 m or 330 ft may ensue.