FAA Approved Airplane Flight Manual Supplement

Hawker Beechcraft King Air 300/300LW 190-00716-02 Rev. 1
Page 78 of 137 FAA APPROVED
• With Elevator Tab Wheel in Motion,
AP/YD DISC / TRIM INTRPT Button ....................................................... PRESS AND HOLD
(verify elevator tab wheel motion stops)
• Pilot’s Trim Override ................................................................................................. CHECK
Activate the copilot’s Pitch Trim Switches nose down. Verify elevator tab wheel is
moving nose down. While the tab wheel is moving in the DN direction, activate the
pilot’s Pitch Trim Switches nose up. Verify the elevator tab wheel begins to move in the
UP direction. Release both pilot’s and copilot’s Pitch Trim switches and reset elevator
tab as required.
• Manually Operate Elevator Tab Wheel .................VERIFY Pitch Trim Servo is Not Engaged
c. Press GA Button on Left power lever ......... VERIFY FD Command Bars show Takeoff Attitude
‘TO / / TO’ is Annunciated in Mode Window on Both PFDs
BEFORE TAKEOFF (FINAL ITEMS)
The following procedures supersede the same procedures in the airplane’s AFM BEFORE
TAKEOFF (FINAL ITEMS) checklist items.
1. V
1
, V
2
, Minimum Takeoff Power .......................................................................... SET OR CONFIRM
These procedures should be conducted after completing the airplane’s AFM BEFORE TAKEOFF
(FINAL ITEMS) checklist.
2. PFD Attitude and Heading .................................................................................................. NORMAL
3. GPS Position .................................................................. VALID, ‘LOI’ NOT ANNUNCIATED on HSI
4. Standby Attitude Indicator .......................................... ERECT and NORMAL, Fail Flag not in view
TAKEOFF
This procedure should be conducted after brake release during the takeoff roll but before
becoming airborne.
1. Verify correspondence of PFD airspeed display and standby airspeed.
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.