C
IRRUS
D
ESIGN
S
ECTION
4: N
ORMAL
P
ROCEDURES
SR20
S
TALLS
P/N 11934-005
4-23
Shutdown
Stalls
Aircraft stall characteristics are conventional. Power-off stalls may be
accompanied by a slight nose bobbing if full aft stick is held. Power-on stalls
are marked by a high sink rate at full aft stick. Power-off stall speeds at
maximum weight for both forward and aft CG positions are presented in
Section 5 -
When practicing stalls at altitude, as the airspeed is slowly reduced, you will
notice a slight airframe buffet, hear the stall speed warning horn sound
between 5 and 10 knots before the stall, and see the Crew Alerting System
display a STALL Warning annunciation. Normally, the stall is marked by a
gentle nose drop and the wings can easily be held level or in the bank with
coordinated use of the ailerons and rudder. Upon stall warning in flight,
recovery is accomplished by immediately reducing back pressure to reduce
the angle of attack and to maintain safe airspeed, adding power if necessary
and rolling wings level with coordinated use of the controls.
• WARNING •
Extreme care must be taken to avoid uncoordinated, accelerated or
abused control inputs when close to the stall, especially when close to
the ground.
1. Fuel Pump.................................................................................................OFF
2. Throttle.................................................................................................... IDLE
• CAUTION •
If the engine hesitates as the switch cycles through the “OFF” posi-
tion. If the engine does not hesitate, one or both magnetos are not
grounded. Prominently mark the propeller as being “Hot,” and
contact maintenance personnel immediately.
3. Ignition Switch ................................................................................... CYCLE
4. Mixture............................................................................................. CUTOFF
5. All Switches...............................................................................................OFF
6. Magnetos...................................................................................................OFF
• N
OTE
•
After a hard landing, ELT may activate. if this is suspected, press the
RESET button.
7. ELT.......................................................................TRANSMIT LIGHT OUT
8. Chocks, Tie-downs, Pitot Covers ...................................... AS REQUIRED
Reissue A
Содержание 2220
Страница 12: ...SECTION 1 GENERAL CIRRUS DESIGN SR20 1 2 P N 11934 005 Reissue A Intentionally Left Blank ...
Страница 120: ...SECTION 4 NORMAL PROCEDURES CIRRUS DESIGN SR20 4 2 P N 11934 005 Reissue A Intentionally Left Blank ...
Страница 188: ...SECTION 6 WEIGHT AND BALANCE CIRRUS DESIGN SR20 6 2 P N 11934 005 Reissue A Intentionally Left Blank ...
Страница 198: ...SECTION 7 AIRPLANE AND SYSTEMS CIRRUS DESIGN SR20 7 4 P N 11934 005 Reissue A Intentionally Left Blank ...
Страница 326: ...SECTION 10 SAFETY INFORMATION CIRRUS DESIGN SR20 10 2 P N 11934 005 Reissue A Intentionally Left Blank ...