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(2) Operating engine.............................................. Increase thrust as required.
(3) FLIGHT SPOILER lever .......................................Select to RETRACT.
Check EICAS indicates
spoilers retracted.
(4) FLAPS ..................................................................Select to 20° for landing.
(5) Airspeed ........................................................... Increase to VREF (Flaps 45°) + 14 KIAS
(6) Airplane ............................................................... Retrim and continue approach, or
go-around at pilot’s discretion
(Refer to Single Engine
Go-Around, in this section).
If required, autopilot may be
re-engaged, if above 800 feet
AGL.
If continuing the approach:
(7) AIR-CONDITIONING, L and R
PACKs.............................................................. Transfer to APU bleed air.
(8) Go-Around thrust........................................... Determine applicable single engine climb
thrust (APR rating) (Refer to
the Airplane Flight Manual,
Chapter 6; PERFORMANCE –
THRUST SETTINGS).
(9) GPWS/FLAP OVRD switch
(if installed) ...........................................................Select to OVRD (to mute flap aural
warning).
(10) Final approach speed....................................... Maintain VREF (Flaps 45°) + 14 KIAS.
(11) Actual landing distance .................................... Increase by a factor of 1.55 (55%), for a
flap 20° landing without the
use of reverse thrust.
NOTE
Use remaining thrust reverser carefully upon landing.
After landing:
(12) Affected engine ..............................................Shutdown
END
ABNORMAL PROCEDURES
Single Engine Procedures
Vol. 1 05−03−2
REV 74, Nov 07/08
CL−604 Operating Manual
PSP 604−6
1. SINGLE ENGINE PROCEDURES (CONT'D)
C. Single Engine Procedure
(1) Affected thrust lever ................................... Confirm and
SHUT OFF
(2) BLEED AIR, 10TH STAGE L (R)
switch/light .......................................................Press out to select affected 10th-stage
SOV closed.
Check L (R) 10TH CLOSED
light on.
(3) AIR-CONDITIONING, L (R) PACK
switch/light .........................................................Press in to turn on operative engine
pack.
Check L (R) PACK OFF light
out.
(4) Land at the nearest suitable airport.
END
ABNORMAL PROCEDURES
Single Engine Procedures
Vol. 1 05−03−3
REV 66, Feb 01/07
CL−604 Operating Manual
PSP 604−6
1. SINGLE ENGINE PROCEDURES (CONT'D)
D. Single Engine Approach and Landing
(1) AIR-CONDITIONING, L and R
PACKs.............................................................. Transfer to APU bleed air.
NOTE
Bleed air extraction from the APU is not permitted above
15,000 feet.
On airplanes 5301 to 5630 NOT incorporating Service Bulletin 604–49–006 or
604–49–009:
NOTE
Bleed air extraction from the APU is not permitted above 14,500 feet.
(2) Go-Around thrust........................................... Determine applicable single engine climb
thrust (APR rating) (Refer to
the Airplane Flight Manual,
Chapter 6; PERFORMANCE –
THRUST SETTINGS).
(3) GPWS/FLAP OVRD switch
(if installed) ...........................................................Select to OVRD (to mute flap aural
warning).
(4) FLAPS ..................................................................Select to 20° for landing. Verify
proper indication.
(5) Final approach speed....................................... Maintain VREF (Flaps 45°) + 14 KIAS.
(6) Actual landing distance .................................... Increase by a factor of 1.55 (55%), for a
flaps 20° landing without the
use of reverse thrust.
NOTE
If required, use remaining thrust reverser carefully upon landing.
END
ABNORMAL PROCEDURES
Single Engine Procedures
Vol. 1 05−03−4
REV 66, Feb 01/07
CL−604 Operating Manual
PSP 604−6
1. SINGLE ENGINE PROCEDURES (CONT'D)
E. Single Engine Go-Around
NOTE
1. The minimum fuel for go-around is 230 kg (500 lb) per wing with a
maximum airplane climb attitude of 5° nose up.
2. Single engine go-around capability is not assured with flaps greater
than 20°.
(1) FLIGHT SPOILER lever
(If extended) .........................................................Select to RETRACT.
Check EICAS indicates
spoilers retracted.
(2) Single Engine Climb Thrust
(APR rating).............................................................. Set immediately (Refer to the
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庞巴迪挑战者604操作手册 Operating Manual 1(113)
