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NOTE
For wet grass, an additional 10 % increase in take-off roll must be expected.
NOTE
An uphill slope of 2 % (2 m per 100 m or 2 ft per 100 ft) results in an increase in the take-off distance of approximately 10 %. The effect on the take-off roll can be greater.

Conditions: Flaps: UP, Power: both MAX @ 2300 RPM, vR: 70 KIAS, Airspeed: 77 KIAS, Runway: hard, paved Conditions: Flaps: UP, Power: both MAX @ 2300 RPM, vR: 72 KIAS, Airspeed: 79 KIAS, Runway: hard, paved

Conditions: Flaps: UP, Power: both MAX @ 2300 RPM, vR: 72 KIAS, Airspeed: 79 KIAS, Runway: hard, paved

5.3.7 CLIMB PERFORMANCE - TAKE-OFF CLIMB
Conditions:
-Power lever ......................... both MAX @ 2300 RPM -Flaps .............................. UP -Landing Gear ........................ retracted -Airspeed
     up to 1700 kg (3748 lb).............. 77 KIAS

above 1700 kg (3748 lb) ............. 79 KIAS

NOTE
The charts on the following pages show the rate of climb. The gradient of climb cannot easily be determined with a chart, but it can be calculated using the following formulae:
ROC fpm ]
[
Gradient [%] =. 095
.TAS KTAS ]
[
ROC ms
[/]
Gradient [%] =. 190
TAS KTAS ]
[
Doc. No. 7.01.05-E  Rev. 5  15-Nov-2007  Page 5 - 17 

5.3.8 CLIMB PERFORMANCE - CRUISE CLIMB
Conditions:
-Power lever ......................... both MAX @2300 RPM -Flaps .............................. UP -Airspeed
 up to 1700 kg (3748 lb) .............. 85 KIAS

 above 1700 kg (3748 lb) ............. 86 KIAS

NOTE
The graphs on the following pages show the rate of climb. The gradient of climb cannot easily be determined with a graph, but it can be calculated using the following formulae:
ROC fpm ]
[
Gradient [%] =. 095
.TAS KTAS ]
[
ROC ms
[/]
Gradient [%] =. 190
TAS KTAS ]
[
Page 5 - 20  Rev. 5  15-Nov-2007  Doc. No. 7.01.05-E 

5.3.9 ONE ENGINE INOPERATIVE CLIMB PERFORMANCE
Conditions:
-Remaining Engine (RH)................ MAX @2300 RPM
-Dead Engine ........................ featheredand secured
-Flaps .............................. UP
-Airspeed............................ 82 KIAS
-Landing Gear ........................ retracted
-Zero Sideslip ........................ established

NOTE
With respect to handling and performance, the left-hand engine (pilots view) is considered the "critical" engine.
NOTE
The graphs on the following pages show the rate of climb. The gradient of climb cannot easily be determined with a graph, but it can be calculated using the following formulae:
　
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