5.7 Recovery from Unintentional Spin
If unintentional spin occurs, the following recovery procedure should be used:
Throttle: ..................................................................................... IDLE
Flap:........................................................................................... UP
Rudder: ...................................................................................... FULL, IN THE OPPOSITE DIRECTION OF THE SPIN
Stick: ......................................................................................... FORWARD
As the spin stops:
Rudder: ...................................................................................... SET NEUTRAL
Attitude: ..................................................................................... SMOOTLHY RECOVER AVERTING SPEEDS IN
EXCESS OF VNE AND MAXIMUM LOAD FACTOR
(n=+3.8)
Throttle: ..................................................................................... AS REQUIRED
NOTE
Use elevator control to recover to straight and level or a climbing attitude
5.8 Airplane Alerts
The annunciations colors located on the annunciator panel can be:
GREEN: to indicate a SAFE OPERATION
RED: to indicate a FUTURE CORRECTIVE ACTION must be performed
5.8.1 Alternator failure
The annunciation (ALT) located on the annunciator panel may activated when a fault is detected on alternator or the
alternator is disconnected.
Generator switch: ...................................................................... OFF
Master switch: ........................................................................... OFF
Generator switch: ...................................................................... ON
Master switch: ........................................................................... ON
If the problem persists:
Generator switch: ...................................................................... OFF
Non-vital electric equipment: .................................................... SHED
5.8.2 Electrical fuel pump failure
If the annunciation FUEL PUMP ON located on the annunciator panel is deactivated, apply the following procedure:
Electrical fuel pump switch: ...................................................... OFF
Electrical fuel pump switch: ...................................................... ON
Fuel pressure: ............................................................................ CHECK RAISE
If fuel pressure does not build up:
Land as soon as possible monitoring fuel pressure