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vNO Max. structural cruising speed 155 KIAS Do not exceed this speed except in smooth air, and then only with caution.
vNE Never exceed speed in smooth air 194 KIAS Do not exceed this speed in any operation.
2.3 AIRSPEED INDICATOR MARKINGS
Marking KIAS Significance
White arc 56 - 111 KIAS Operating range with flaps fully extended.
Green arc 62 - 155 KIAS Normal operating range.
Yellow arc 155 - 194 KIAS ‘Caution range’ - “Only in smooth air”.
Blue radial 82 KIAS Best rate of climb speed, single engine.
Red radial 68 KIAS Minimum control speed, single engine.
Red radial 194 KIAS Maximum speed for all operations - vNE.
2.4 POWER-PLANT LIMITATIONS
a) Number of engines : 2
b) Engine manufacturer : Thielert Aircraft Engines
c) Engine designation : TAE 125-01 Centurion 1.7 ' or ' TAE 125-02-99 (if M.M 42-198 is carried out)
(P/N see Equipment List in Chapter 6)
d) RPM limitations (shown as propeller RPM)
Maximum : 2300 RPM
Maximum overspeed : 2500 RPM (max. 20 sec)
e) Engine power Max. take-off power : 99 kW (135 DIN-hp) at 2300 RPM (100 % load) Max. continuous power : 99 kW (135 DIN-hp) at 2300 RPM (100 % load)
' f) Fuel temperature:
'
'
' '
'
TAE 125-01 TAE 125-02-99 (M.M 42-198 carried out)
Minimum -30 oC -30 oC
Maximum +75 oC +75 oC
g) Oil pressure (indicated values are corrected for pressure altitude)
Minimum : 1.0 bar
Maximum : 6.5 bar
h) Oil quantity (per engine)
Minimum : 4.5 liters (appr. 4.8 US qts)
Maximum : 6.0 liters (appr. 6.3 US qts)
Maximum oil consumption : 0.1 liters/hr (appr. 0.1 US qts/hr)
Page 2 - 6 Rev. 5 15-Nov-2007 Doc. No. 7.01.05-E
' i) Oil temperature:
' '
' '
'
TAE 125-01 TAE 125-02-99 (M.M 42-198 carried out)
Minimum -32 oC -30 oC
Maximum +140 oC +140 oC
j) Gearbox temperature
Maximum : 120 °C
' ' k) Coolant temperature:
'
' '
'
l) Voltage Minimum Maximum
m) Amperage Maximum
n) Propeller manufacturer
o) Propeller designation
p) Propeller diameter
q) Prop. pitch angle (@ 0.75 R) : 24.1 V : 32.0 V
TAE 125-01 TAE 125-02-99 (M.M 42-198 carried out)
Minimum -32 oC -30 oC
Maximum +105 oC +105 oC
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