FAA Approved Airplane Flight Manual Supplement

190-00716-02 Rev. 3 Hawker Beechcraft King Air 300/300LW
FAA APPROVED Page 89 of 167
WARNING
CRUISE WITHIN RVSM AIRSPACE
1. Altimeters ................................................................................................................ CROSS-CHECK
Maximum Difference: 200 Feet
Ensure Matched barometric pressure settings (29.92 inHg, STD BARO, or 1013 mb).
2. Altitude ........................................................................................................... RECORD as Required
Record pilot, copilot and standby altimeter readings upon entering RVSM airspace and as
required thereafter while in RVSM airspace for contingency situations.
3. Autopilot ALT Mode ............................................................ Maximum Altitude Deviation: +/- 65 Feet
During normal operations, the ADC coupled to the autopilot will supply altitude data to the active
transponder.
CLIMB, CRUISE, AND DESCENT
Disengage autopilot and yaw damper and re-trim the airplane in roll and/or yaw, if slight dutch roll
activity is observed. Re-engage the autopilot and yaw damper after trimming the airplane.
ICING FLIGHT
IN FLIGHT
DUE TO DISTORTION OF THE WING AIRFOIL, ICE ACCUMULATION ON THE LEADING EDGES
CAN CAUSE A SIGNIFICANT LOSS IN RATE OF CLIMB AND IN SPEED PERFORMANCE, AS
WELL AS INCREASES IN STALL SPEED. EVEN AFTER CYCLING THE DEICE BOOTS, THE
ICE ACCUMULATION REMAINING ON THE BOOTS AND UNPROTECTED AREAS OF THE
AIRPLANE CAN CAUSE LARGE PERFORMANCE LOSSES. FOR THE SAME REASON, THE
AURAL STALL WARNING SYSTEM MAY NOT BE ACCURATE AND SHOULD NOT BE RELIED
UPON. UNDER THESE CONDITIONS, ESP AND AUTOPILOT UNDERSPEED PROTECTION
MAY ALSO NOT BE ACCURATE AND SHOULD NOT BE RELIED UPON.
SHUTDOWN AND SECURING
These procedures should be conducted after the Battery and Generator Switches have been
turned OFF in the AFM Shutdown and Securing checklist, and before the flight crew vacates the
cockpit.
1. Standby Battery Switch .................................................................................................. PRESS OFF
a. Standby Battery Switch ...................................................... [ARMED] and [ON] EXTINGUISHED
b. Standby attitude fail flag ........................................................................................... DISPLAYED
c. Standby altimeter vibrator should not be heard (BAT – MASTER SWITCH OFF).