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时间:2010-09-27 07:35来源:蓝天飞行翻译 作者:admin
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When N2 reaches 20% RPM and ITT is below 120°C:
(6) Thrust lever (of starting engine)........................................................Advance to IDLE
(7) Engine instruments ..........................................................................................Monitor
NORMAL PROCEDURES
Consolidated Checklists
04−20−6
REV 66, Feb 01/07

DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
1. CONSOLIDATED CHECKLISTS (CONT'D)
J. Cross-Bleed Engine Start Procedure (Cont’d)
(8) Thrust lever (of first engine).................................................................................IDLE
(9) Idle speed ......................................................................................................... Check
K. Failure to Start Procedure
(1) Thrust lever (of starting engine).................................................................SHUT OFF
(2) Ignition ....................................................................................................................Off
(3) Dry motor until ITT is below 120°C
(maximum 90 seconds) ............................................................................ Accomplish
L. After Engine Start Check
(1) GEN 1 and 2 switches ........................................................................................... ON
On airplanes 5301 to 5320 NOT incorporating SB 604–33–002:
(2) STBY INSTR circuit breaker (1P9) ................................................................... Check
(3) AC and DC electrical page ............................................................................... Check
(4) APU GEN switch..................................................................................... OFF/RESET
(5) APU .......................................................................................................... As required
(6) IGNITION A (B) switch/light ......................................................................... Press out
(7) L and R PACK switch/lights ............................................................................Press in
(8) ANTI-ICE, WING switch....................................................................................NORM
(9) Wing anti-ice/isolation valve check
(first flight–of the day) .................................................................................. Complete
(10) Wing anti-ice ............................................................................................. As required
(11) Anti-Ice cowl check (first flight of the day) ................................................... Complete
(12) Cowl anti-ice ............................................................................................. As required
(13) Flight controls ................................................................................................... Check
(14) Ground spoilers check (first flight of the day) .............................................. Complete
(15) Flight spoilers check (first flight of the day).................................................. Complete
(16) NOSE STEER switch......................................................................................ARMED
(17) APR check ................................................................................................... Complete
(18) ADG AUTO DEPLOY CONTROL switch............................................................ UNIT
M. Taxi Check
(1) Brakes............................................................................................................... Check
(2) FLAPS ................................................................................................................... 20°
(3) Thrust reversers check (first flight of the day).............................................. Complete
(4) Aileron and rudder trims .................................................................................. Neutral
NORMAL PROCEDURES
Consolidated Checklists
04−20−7
REV 74, Nov 07/08

DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
1. CONSOLIDATED CHECKLISTS (CONT'D)
M. Taxi Check (Cont’d)
(5) Stabilizer trim ....................................................................................... Set for take-off
(6) Flight instruments ....................................................................................... Check/Set
(7) Fuel balance ..................................................................................................... Check
N. Take-Off Check
(1) Ignition ...................................................................................................... As required
(2) Wing anti-ice ............................................................................................. As required
 
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