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钻石40系列飞机维护手册 DA 40 SERIES AIRPLANE MAINTENANCE MANUAL 1(17)

时间:2011-10-28 13:36来源:蓝天飞行翻译 作者:admin
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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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