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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(9)

时间:2011-10-31 11:51来源:蓝天飞行翻译 作者:公务机
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Use of the ATS during go-around is prohibited. Pilot must manually set thrust to override ATS. ATS may be used to trim final N1, once manually set.

.  
If flaps are selected to less than 45° for landing, ATS must be disengaged prior to reaching 100 feet AGL.

 


 LIMITATIONS Power Plant  Vol. 1  02.05.4 
Oct 05/06 


6. AUTOMATIC PERFORMANCE RESERVE (APR)
If take-off performance is predicated upon the use of APR, the APR system must be verified
operative prior to take-off.
The APR system must be selected off, if an APR INOP caution message is displayed on EICAS.
APR OFF Performance must be used if an APR INOP caution message is displayed.


7. STARTER CRANKING LIMITS (GROUND AND AIR)
The starter must not be used if indicated N2 rpm exceeds 55%.
A. Engine Start
Normal engine start – Three consecutive engine start cycles with 5 minutes cooling between additional cycles.
B. Associated Conditions
At initiation of thrust lever movement from SHUT OFF to IDLE:
(1)
ITT must be 120°C or less for all ground starts.

(2)
ITT must be 90°C or less for all air starts.


C. Dry Motoring Cycle
Dry motoring is performed with ignition OFF and thrust levers at SHUT OFF.
Dry motoring may be used for engine ground starts and engine airstarts.

 

8. ENGINE RELIGHT
Engine starting in-flight is only permitted within the envelope defined in Figure 02.05.1:

Vol. 1
02.05.5
LIMITATIONS
Power Plant
Oct 05/06
8.  ENGINE RELIGHT (CONT'D) 
RELIGHT TYPE Windmilling  ENVELOPE (FIGURE 02–05–1) Altitude from 21,000 to 10,000 feet: Airspeed from 300 to 348 KIAS, and from 12 to 55% N2. Altitude from 10,000 to 8,000 feet: Airspeed from 300 to 348 KIAS, and from 10 to 55% N2. Altitude from sea level to 8,000 feet: Airspeed 300 KIAS, and from 10 to 55% N2. 
NOTE 
Starter-assisted Cross Bleed  N2 should be stable or increasing. Altitude from 21,000 feet to 15,000 feet: Airspeed from 200 KIAS up to 300 KIAS, and from 0 to 55% N2. Altitude from 15,000 feet to sea level: Airspeed from 140 KIAS up to 300 KIAS, and from 0 to 55% N2. 
25 
200  21,000 ft  300  348 
20 

ALTITUDE X 1000 FT.
N2 >12%
15,000 ft
15
W’MILL
10,000 ft
10
STARTER
N2 >10%
ASSISTED
W’MILL
8,000 ft
N2 >10%
5

0  100  200  300 
KIAS (KNOTS)  350 

DFM0205_001
Engine Air Start Envelope (In Flight)
Figure 02.05.1

CL.605 Flight Crew Operating Manual
PSP 605.6


 LIMITATIONS Power Plant  Vol. 1  02.05.6 
 
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