Cessna 208B - Maximum Performance Climb

CESSNA SECTION 4
MODEL
2088 (675 SHP)
NORMAL PROCEDURES
1 ENROUTE CLIMB (Cont~nued)
NOTE
Engine operations which exceed 740°C ITT may reduce
engine life.
CAUTION
FOR EVERY 10" BELOW -30°C AMBIENT
TEMPERATURE. REDUCE MAXIMUM ALLOWABLE
N,.
MAXIMUM PERFORMANCE CLIMB
1. Ice Protection (if installed) - AS REQUIRED.
1
2 PitoVStatic Heat - ON when OAT is below YC (40°F).
3. Airspeed - 104 KlAS from sea level to 10,000 feet decreasing to
87 KlAS at 20,000 feet.
4. Propeller
- 1900 RPM.
5. Torque - SET (refer to Maximum Climb Torque Chart in Section 5.
I
Observe Maximum Climb ITT and Ng limits).
NOTE
Engine operations which exceed 740°C ITT may reduce
engine life.
.
CAUTION
=
FOR EVERY 10" BELOW -30°C AMBIENT
=,
TEMPERATURE, REDUCE MAXIMUM ALLOWABLE Ng
BY 2.2%.
1 Revision 23
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U.S. 4-23