通航信息_通航_通用航空_General Aviation

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Doc. No. 6.01.05-E  Revision 3  26-May-2003  Page 5 - 10 

Doc. No. 6.01.05-E  Revision 3  26-May-2003  Page 5 - 11 

5.3.8 CLIMB PERFORMANCE -TAKE-OFF CLIMB
Conditions: -Power lever ............... MAX

-Flaps ....................  T/O

- Airspeed.................. 66 KIAS (1150 kg, 2535 lb) 60 KIAS (1000 kg, 2205 lb) 54 KIAS (850 kg, 1874 lb)
-Altitude...................  0 up to8500 ft pressure altitude

NOTE
The graph on the following page shows 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]
[
%

Doc. No. 6.01.05-E  Revision 3  26-May-2003  Page 5 - 12 

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Doc. No. 6.01.05-E  Revision 3  26-May-2003  Page 5 - 13 

5.3.9 CLIMB PERFORMANCE -CRUISE CLIMB
Conditions: -Power lever ............... MAX

-Flaps ....................  UP

- Airspeed.................. 73 KIAS (1150 kg, 2535 lb) 68 KIAS (1000 kg, 2205 lb) 60 KIAS (850 kg, 1874 lb)
-Altitude...................  0 up to8500 ft pressure altitude

NOTE
The graph on the following page shows 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]
[
%

Doc. No. 6.01.05-E  Revision 3  26-May-2003  Page 5 - 14 

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Doc. No. 6.01.05-E  Revision 3  26-May-2003  Page 5 - 15 

5.3.10 CRUISING (TRUE AIRSPEED TAS)

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Doc. No. 6.01.05-E  Revision 3  26-May-2003  Page 5 - 16 

5.3.11 LANDING DISTANCE -FLAPS LDG
Conditions: -Power lever ............... IDLE

-Flaps ....................  LDG

- Approach speed............ 71 KIAS (1150 kg, 2535 lb) 63 KIAS (1000 kg, 2205 lb) 58 KIAS (850 kg, 1874 lb)
-Runway ..................  level, asphalt surface

values for ISA and MSL, at 1150 kg (2535 lb) 
Landing distance over a 50 ft (15 m) obstacle  744 m (2441 ft) 
　
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