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Airplane Flight Manual,
Chapter 6; PERFORMANCE –
THRUST SETTINGS).
FAA Certified Airplanes
(2) Normal Take-off Thrust ............................................ Set immediately (Refer to the
Airplane Flight Manual,
Chapter 6; PERFORMANCE –
THRUST SETTINGS).
(3) Airplane ............................................................... Rotate smoothly to initial pitch attitude
of 10°, and adjust pitch as
required to achieve the
approach climb speed. (Refer
to the Airplane Flight Manual,
Chapter 6; PERFORMANCE –
APPROACH AND LANDING
CLIMB).
(4) FLAPS ..................................................................Select to 20°, if required.
(5) Landing gear ...................................................... Retract when positive rate of climb is
achieved. Landing gear
symbols (3) indicate up.
At a safe altitude (not below 400 feet AGL):
(6) FLAPS ..................................................................Select to UP at a speed of not less
than VFTO – 5 KIAS.
ABNORMAL PROCEDURES
Single Engine Procedures
Vol. 1 05−03−5
REV 74, Nov 07/08
▼
CL−604 Operating Manual
PSP 604−6
1. SINGLE ENGINE PROCEDURES (CONT'D)
E. Single Engine Go-Around (Cont’d)
Go-around was due to engine failure during approach:
Yes
(7) In-Flight Engine
Failure/Shutdown................................. Accomplish Refer to POWER PLANT –
In-Flight Engine
Failure/Shutdown procedure in
this chapter.
− END −
No
(7) No further action required.
END
ABNORMAL PROCEDURES
Single Engine Procedures
Vol. 1 05−03−6
REV 66, Feb 01/07
CL−604 Operating Manual
PSP 604−6
1. AIR START
NOTE
During single engine operations, APU-assisted air start is not
always possible. Priority is given to a cross bleed start (i.e., highest
bleed air pressure source).
Use air turbine starter whenever possible. Refer to Chapter 2;
LIMITATIONS – POWER PLANT, for starter duty cycle.
A. Windmilling Air Start Procedure
NOTE
1. At thrust lever advance, N2 should be stable or increasing.
2. Windmill airstart efficiency is enhanced by attaining the
highest practical airspeed and N2 within the relight
envelope.
3. 300 knots is a target airspeed only, and may be exceeded to
obtain the minimum required N2 .
(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, 10TH STAGE, L (R)
switch/light .......................................................Press out to close affected shut-off
valve.
Check 10TH CLOSED light
on.
(4) BLEED AIR, 10TH STAGE, ISOL
switch/light .......................................................Press out to close isolation valve.
Check 10TH ISOL OPEN light
out.
(5) BLEED AIR, APU LCV switch/light..................Press out to close load control valve.
Check APU LCV OPEN light
out.
ABNORMAL PROCEDURES
Air Start
Vol. 1 05−04−1
REV 66, Feb 01/07
▼
CL−604 Operating Manual
PSP 604−6
1. AIR START (CONT'D)
A. Windmilling Air Start Procedure (Cont’d)
(6) Start envelope ................................................. Establish
WINDMILLING AIR START ENVELOPE
ALTITUDE AIRSPEED ITT % N2
21,000 feet to
10,000 feet 300 KIAS up to
348 KIAS 90°C or less
12 to 55
10,000 feet to
8,000 feet 10 to 55
8,000 feet to SL 300 KIAS
When ready to start:
(7) 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.
When ITT is 90°C or less and N2 is at least 12% (10% if below 10,000 feet):
(8) Affected engine, thrust lever.................................Select to IDLE when within start
envelope.
(9) Engine indications ..............................................Monitor carefully.
NOTE
1. If engine does not ignite in 25 seconds, retard thrust lever to SHUT
OFF, maintain at least 300 KIAS for 30 seconds and repeat
procedure. After ignition is achieved, monitor N2 acceleration rate.
N2 acceleration should be uninterrupted and positive at all times.
Stable idle must be achieved in 2 minutes of advancing thrust lever
　
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