Textron Cessna Grand Caravan Ex 208B Pilot's Operating Handbook And Faa Approved Airplane Flight Manual page 86

SECTION 2 CESSNA
OPERATING LIMITATIONS MODEL 208B (867 SHP)
GARMIN G1000
SYSTEM AND EQUIPMENT LIMITATIONS
(Continued)
G1000 LIMITATIONS
(Continued)
Use of the TERRAIN PROXIMITY information for primary terrain
avoidance is prohibited. The Terrain Proximity map is intended only to
enhance situational awareness. It is the pilot's responsibility to provide
terrain clearance at all times. In addition, Terrain Proximity information
is not available in locations north of 75° North latitude or South of 60°
South latitude due to the absence of terrain data in these geographical
areas.
The COM 1/2 (split COM) function of the Audio Panel is not approved
for use. During COM 1/2 operation, transmission by one crew member
inhibits reception by the other crew member.
Dispatch with GIA1, GIA2, PFD, or MFD cooling advisory message is
prohibited.
Verify the torque gage dynamic redline agrees with the values listed in
Figure 5-8, Maximum Engine Torque For Takeoff, for current altitude
and temperature.
The dynamic redline is a graphical representation of takeoff power
below 16,000 feet MSL and Maximum Rated Power above 16,000 feet
MSL as depicted in Section 5, Performance, Figure 5-8, Maximum
Engine Torque For Takeoff chart and Figure 5-9 Maximum Engine
Torque For Climb. The dynamic redline automatically compensates for
altitude and temperature changes and adjusts displayed takeoff torque
for inertial separator deployment and bleed air heat switch position.
Failure to comply with the dynamic redline indication can result in
accelerated engine wear, unscheduled engine maintenance and
increased operating costs even though no other published engine
limitation has been exceeded.
The maximum cruise torque bug functions of the G1000 engine torque
indicator is advisory information only.
All power settings must be verified by the pilot, refer to Section 5,
Performance, Figure 5-8, Maximum Engine Torque For Takeoff, Figure
5-9, Maximum Engine Torque For Climb and Figure 5-19, Cruise
Performance (with Cargo Pod) or Figure 5-36, Cruise Performance
(without Cargo Pod) for the approved engine power settings.
FAA APPROVED
208BPHCUS-01
2-32
U.S.