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With a reputation for being the world’s best training aircraft, the CESSNA is the most popular single-engine aircraft ever built.
Engine : Thielert Aircraft Engines GmbH
Propeller : MT Propeller Entwicklung GmbH
Number of blades : 3
Fuel : JET A-1/JET A
Total capacity of fuel : 180.2 litres
Maximum Takeoff Weight : 1111 kg
Maximum Landing Weight : 1111 kg
Aircraft is certified up to an altitude of : 18000 ft
Take-off and Max continuous RPM : 2300
Engine Control : FADEC System
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Marking
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KIAS Range
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Significance
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|---|---|---|
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White Arc
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33 - 85
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Full Flap Operating Range. Lower limit is maximum weight VS0 in landing configuration. Upper limit is maximum speed permissible with flaps extended
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Green Arc
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44 -129
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Normal Operating Range. Lower limit is maximum weight VS1 at most forward C.G. with flaps retracted. Upper limit is maximum structural cruising speed.
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Yellow Arc
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129-163
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Operations must be conducted with caution and only in smooth air.
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Red Line
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163
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Maximum speed for all operations.
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Engine : Avco Lycoming (VT-AAY), Textron Lycoming (VT-RBM)
Propeller : McCauley Accessory Division
Number of blades : 2
Fuel :100LL Grade Aviation Fuel(Blue)/100 Grade Aviation Fuel(Green
Total capacity of fuel : 211.6 litres
Maximum Takeoff Weight : 1088.6 kg
Maximum Landing Weight : 1088.6 kg
Aircraft is certified up to an altitude of : 14000 ft
Take-off and Max continuous RPM : 2700
Engine Type: Carburetor (VT-AAY)
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Marking
|
KIAS Range
|
Significance
|
|---|---|---|
|
White Arc
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33 - 85
|
Full Flap Operating Range. Lower limit is maximum weight VS0 in landing configuration. Upper limit is maximum speed permissible with flaps extended
|
|
Green Arc
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44 -127
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Normal Operating Range. Lower limit is maximum weight VS1 at most forward C.G. with flaps retracted. Upper limit is maximum structural cruising speed.
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Yellow Arc
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129-158
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Operations must be conducted with caution and only in smooth air.
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Red Line
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158
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Maximum speed for all operations.
|
|
Marking
|
KIAS Range
|
Significance
|
|---|---|---|
|
White Arc
|
33 - 85
|
Full Flap Operating Range. Lower limit is maximum weight VS0 in landing configuration. Upper limit is maximum speed permissible with flaps extended
|
|
Green Arc
|
44 -129
|
Normal Operating Range. Lower limit is maximum weight VS1 at most forward C.G. with flaps retracted. Upper limit is maximum structural cruising speed.
|
|
Yellow Arc
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129-163
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Operations must be conducted with caution and only in smooth air.
|
|
Red Line
|
163
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Maximum speed for all operations.
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