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庞巴迪挑战者605公务机机组操作手册 CL605-CHAPTER 2 -限制 LIMITATIONS(7)

时间:2011-10-31 11:51来源:蓝天飞行翻译 作者:公务机
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CL.605 Flight Crew Operating Manual
PSP 605.6


 LIMITATIONS Operating Limitations  Vol. 1  02.04.6 
Oct 05/06 

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CL.605 Flight Crew Operating Manual
PSP 605.6


 LIMITATIONS Power Plant  Vol. 1  02.05.1 
Oct 05/06 

1. ENGINES
Type: General Electric CF34–3B, quantity two.
2. ENGINE INDICATIONS
The engine limit display markings on EICAS must be used to determine compliance with the maximum/minimum Limits and precautionary ranges. If EICAS markings show more conservative Limits than those specified below, the limit markings on the EICAS must be used.

INDICATION RED AMBER GREEN
(MAX/MIN LIMITS) (CAUTION RANGE) (NORMAL RANGE) N1 % RPM 0 to 98.5 ITT °C:
900
– 0 to 900(for first 2 min.)
– APR not operating
884 0 to 884
(for next 3 min.) 928 0 to 928(for first 2 min.)
– APR operating
900 0 to 900
(for next 3 min.) – Maximum
Continuous Thrust 900 – 0 to 900
(MCT)

 

N2 % RPM:
– wing anti-ice on 99.3 78 to 99.2
– wing anti-ice off 99.3 – 0 to 99.2
OIL TEMP °C –40 to 154 OIL PRESS psi
0 to 25 116 to 156 26 to 115


 LIMITATIONS Power Plant  Vol. 1  02.05.2 
Oct 05/06 

3. ENGINE OPERATING LIMITS
A. Engine Operating Limits Table

 

 

CONDITION CORE RPM N2 % FAN RPM N1 % ITT °C
Start 20 903 (50 seconds) Acceleration 930 (5 seconds) Max Continuous 99.2 98.6 899 884 (5 minutes)*
Normal Take-Off 98.3 96.2 900 (2 minutes out of 5 total transient)* 899 (5 minutes)*
Maximum Take-Off
99.4  98.6 928 (2 minutes out of
(APR operating)
5 total transient)*
* Transient limits
NOTE
1.  
The take-off, go-around and maximum continuous thrust N1 values for the CF34-3B engine are presented on the appropriate engine thrust setting charts contained in Chapter 6; PERFORMANCE – THRUST SETTINGS of the Airplane Flight Manual .

2.  
If above 40,000 feet, one air-conditioning unit or cowl anti-ice must be selected on for each engine.


B. Airplane Cold Soak
Before the first flight of a day, when the airplane is cold-soaked at an ambient temperature of –30°C (–22°F) or below for more than 8 hours, the engines must be motored for 60 seconds, and fan rotation must be verified, before the engine start is initiated.
Thrust reversers must be actuated until the deploy and stow cycles are less than 5 seconds.
C. Oil Temperature
Minimum for starting –40°C
Maximum Continuous +155°C
Maximum Permissible +163°C (15 minutes maximum)

D. Oil Pressure
 
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