曝光台 注意防骗
网曝天猫店富美金盛家居专营店坑蒙拐骗欺诈消费者
(11) Engine instruments ..........................................................................................Monitor
(12) APU EGT indications ........................................................................................ Check
(13) Idle speed ......................................................................................................... Check
H. Engine Start Procedure using External Air (with AC electrical power)
(1) APU LCV switch/light................................................................................... Press out
(2) External air................................................................................................. Connected
(3) 10th stage bleed air pressure ................................................. Check 45 psi minimum
(4) L (R) ENG START switch/light........................................................................... Press
When N2 reaches 20% RPM and ITT is below 120°C:
(5) Left or right thrust lever.....................................................................Advance to IDLE
(6) Engine instruments ..........................................................................................Monitor
(7) Fuel system check valve operation (first flight of the
day).................................................................................................................... Verify
NORMAL PROCEDURES
Consolidated Checklists
04−20−5
REV 66, Feb 01/07
▼
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
1. CONSOLIDATED CHECKLISTS (CONT'D)
H. Engine Start Procedure using External Air (with AC electrical power) (Cont’d)
(8) L and R BOOST PUMP switch/lights..................................................................... ON
(9) Other engine ........................................................................................................ Start
I. Engine Start Procedure using External Air (without AC electrical power)
(1) Normal Power-up Check.........................................................................As instructed
(2) APU LCV switch/light................................................................................... Press out
(3) External air................................................................................................. Connected
(4) Manifold pressure .................................................................Confirm 45 psi minimum
On airplanes 5301 to 5330 NOT incorporating SB 604–21–002:
(5) L and R PACK switch/lights ...................................................................... Check OFF
(6) L BOOST PUMP switch/light ................................................................................. ON
(7) IGNITION B switch/light......................................................................................... ON
(8) R ENG START switch/light ................................................................................ Press
When N2 reaches 20% RPM and ITT is below 120°C:
(9) Right thrust lever...............................................................................Advance to IDLE
(10) Engine instruments ..........................................................................................Monitor
(11) GEN 2 switch ......................................................................................................... ON
(12) AC and DC electrical page ............................................................................... Check
(13) Fuel system check valve operation (first flight of the
day).................................................................................................................... Verify
(14) L and R BOOST PUMP switch/lights.......................................................... Check ON
(15) Bleed leak detection test (first flight of the day) ........................................... Complete
(16) R 10TH STAGE switch/light............................................................................Press in
(17) R PACK switch/light........................................................................................Press in
(18) Normal Power-Up Check ............................................................................. Complete
J. Cross-Bleed Engine Start Procedure
(1) APU LCV switch/light................................................................................... Press out
(2) L (R) 10TH STAGE switch/light (of operating engine) ....................................Press in
(3) Thrust lever (of operating engine)..................................................................Advance
(4) 10th stage bleed air pressure ................................................. Check 60 psi minimum
(5) L (R) ENG START switch/light........................................................................... Press
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址：
庞巴迪挑战者604飞机飞行手册CL604 Airplane Flight Manual 1(118)
