Engine Alternate Air Failure - Cessna U206G STATIONAIR Pilot Operating Handbook

SOLOY TURBINE PAC
POHS CESSNA U/TU206G
9. Use a 10º to 20º landing flap setting for ice accumulations of 1
inch or less. With heavier ice accumulations, approach with
flaps retracted to ensure adequate elevator effectiveness in the
approach and landing.
10. Power Control – As required (FLIGHT IDLE minimum 14 psi
torque).
11. Approach at 90 to 100 KIAS with 20 flaps and 105 to 115 KIAS
with 0 to 10 flaps.
12. Land on main wheels first, avoiding the slow and high type of
flare-out.
13. Missed approaches should be avoided.

ENGINE ALTERNATE AIR FAILURE

ALTERNATE AIR LIGHT DOES NOT ILLUMINATE:
1. Visually check that the ram inlet doors are raised.
2. If doors are not raised, cycle the alternate air control and check
for reverse operation.
3. If system has failed in the NORMAL mode, leave the icing
condition or snow as soon as possible.
ALTERNATE AIR LIGHT ILLUMINATES IN FLIGHT:
1. Check that the alternate air control is in the NORM position.
2. Visually check that the ram inlet doors are raised.
3. If the ram inlet doors are raised, cycle the alternate air control
and check for reverse operation.
4. If system has failed in the alternate position, land as soon as
practicable and check the inlet and the pneumatic lines.
F.A.A. Approved
CAUTION
SIGNIFICANT
OCCUR WHILE OPERATING IN THE
ALTERNATE AIR MODE.
CAUTION SHOULD
MAINTAIN A MINIMUM OF 14 PSI
TORQUE IN FLIGHT ON APPROACH TO
LANDING.
During takeoff or steep climbs at low air-
speeds and high power, the alternate air
light can illuminate intermittently when in
the normal air mode.
3-10
EMERGENCY PROCEDURES
POWER LOSS
EXTREME
BE USED
NOTE
SECTION 3
WILL
TO
October 4, 2005