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to IDLE.
2. During windmilling airstart, attempt to keep the flight control inputs
to a minimum.
Engine start is successful:
Yes
When the engine is stabilized at Flight Idle:
(10) Thrust levers..................................................... Set as required.
(11) IGNITION, CONT switch/light..................Press out to turn off ignition.
Check the following:
• CONT ON, A and B lights
out.
• IGNITION A/B advisory
message out.
ABNORMAL PROCEDURES
Air Start
Vol. 1 05−04−2
REV 66, Feb 01/07
▼
CL−604 Operating Manual
PSP 604−6
1. AIR START (CONT'D)
A. Windmilling Air Start Procedure (Cont’d)
(12) BLEED AIR, 10TH STAGE,
L (R) switch/light .................................. As required
(13) BLEED AIR, APU LCV
switch/light ........................................... As required
(14) AIR-CONDITIONING, L (R)
PACK switch/light ......................................Press in to start affected pack.
Check L (R) PACK OFF light
out.
(15) ANTI-ICE, COWL, L (R)
switches............................................... As required
(16) AC POWER, GEN 1 (2)
switch............................................................Select affected generator ON.
Check GEN 1 (2) OFF caution
message out.
(17) Affected HYDRAULIC, pump
switch............................................................AUTO Check the following:
• HYD EDP 1A and HYD PUMP
2B caution messages out,
or
• HYD EDP 2A and HYD PUMP
1B caution messages out.
(18) GPWS/FLAP OVRD switch
(if installed) ...................................................Select to NORM.
− END −
No
(10) Single engine procedures............................ Accomplish Refer to SINGLE ENGINE
PROCEDURES in this
chapter.
END
ABNORMAL PROCEDURES
Air Start
Vol. 1 05−04−3
REV 74, Nov 07/08
CL−604 Operating Manual
PSP 604−6
1. AIR START (CONT'D)
B. Engine Cross Bleed − Air Start Procedure
(1) Affected engine, thrust lever.................................Check affected lever SHUT OFF.
(2) FUEL, L (R) BOOST PUMP
switch/light ............................................................Check the following:
• PUMP ON lights on.
• L and R FUEL PUMP ON
advisory messages on.
(3) BLEED AIR, APU LCV switch/light..................Press out to close load control valve.
Check APU LCV OPEN light
out.
(4) BLEED AIR, 10TH STAGE, L (R)
switch/light .........................................................Press in to open operative shut-off
valve.
Check L (R) CLOSED light
out.
(5) Bleed air pressure, operating
engine................................................................... 60 psi Adjust operating engine’s
thrust lever to attain 60 psi
minimum.
(6) Start envelope ................................................. Establish
ENGINE CROSS BLEED AIR START ENVELOPE
ALTITUDE AIRSPEED ITT % N2
21,000 feet to
15,000 feet
200 KIAS up to
300 KIAS
90°C or less 0 to 55
15,000 feet to SL 140 KIAS up to
300 KIAS
On airplanes 5301 to 5330 NOT incorporating Service Bulletin 604–21–002:
(7) AIR-CONDITIONING, L (R) PACK
switch/light .......................................................Press out to shutdown remaining pack.
Check L (R) PACK OFF light
on.
On airplanes 5301 to 5550 NOT incorporating Service Bulletin 604–21–008:
NOTE
It is recommended that the packs be selected off manually.
ABNORMAL PROCEDURES
Air Start
Vol. 1 05−04−4
REV 66, Feb 01/07
▼
CL−604 Operating Manual
PSP 604−6
1. AIR START (CONT'D)
B. Engine Cross Bleed − Air Start Procedure (Cont’d)
When ready to start:
(8) IGNITION , CONT switch/light...........................Press in for continuous ignition.
Check the following:
• CONT ON, A and B lights
on.
• IGNITION A/B advisory
message on.
(9) ENG, L (R) START switch/light .............................Press to cross bleed-air start
affected engine.
Check L (R) START light on.
When ITT is 90°C or less and N2 is 28%:
(10) Affected engine, thrust lever.................................Select to IDLE when within start
envelope.
NOTE
If ITT is above 90°C, dry motor to lower ITT to 90°C before
moving throttle to IDLE.
(11) Engine indications ..............................................Monitor carefully.
NOTE
　
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