FAA Approved Airplane Flight Manual Supplement

190-00716-03 Rev. 1 Hawker Beechcraft B300 and B300C King Air
FAA APPROVED Page 23 of 141
AUTOPILOT OPERATION LIMITS
One pilot must remain seated at the controls, with seatbelt fastened, during all autopilot operations.
Do not use autopilot or yaw damper during takeoff and landing.
The GFC 700 AFCS preflight test must complete successfully prior to use of the autopilot, flight director or
manual electric trim.
The maximum fuel imbalance with the autopilot engaged is 300 pounds.
Minimum speed for autopilot operation is 100 KIAS.
Maximum speed limit for autopilot operation is unchanged from the airplane’s maximum airspeed limit
(V
MO
/M
MO
).
Autopilot coupled ILS, LOC, LPV, or LNAV/VNAV approaches with the yaw damper inoperative or not
engaged is prohibited.
Do not use autopilot below the following altitudes:
1. On takeoff, do not engage the autopilot below ....................................................... 400 feet AGL
2. Cruise .................................................................................................................... 1000 feet AGL
3. Approach (GP or GS mode) .................................................................................... 200 feet AGL
4. Approach (FLC, VS, PIT or ALT mode) .................... Higher of 400 feet AGL or Approach MDA
5. Steep Approaches (GP or GS mode) ..................................................................... 286 feet AGL
SYNTHETIC VISION AND PATHWAYS LIMITS
Use of the Synthetic Vision system display elements alone for aircraft control without reference to the
G1000 primary flight instruments or the aircraft standby instruments is prohibited.
Use of the Synthetic Vision system alone for navigation, or obstacle or terrain avoidance is prohibited.
Use of the SVS traffic display alone to avoid other aircraft is prohibited.