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Use of the FMS approach performance function for steep approach landing is prohibited.
(2) ENHANCED GROUND PROXIMITY WARNING SYSTEM (GPWS)
The GPWS STEEP APPROACH switch/light must be selected ON as directed in the
normal procedures of this supplement.
4. EMERGENCY PROCEDURES
The emergency procedures in Chapter 3 are applicable, except as modified by the following:
Discontinue steep approach landing and divert to the nearest suitable airport if any procedure
necessitates:
• an approach speed greater than VREF,
• a landing with flaps other than 45 degrees,
• an increase in actual landing distance by a factor greater than 1.50 (50%) or
• a landing with gear up or unsafe.
• a landing with any of the systems inoperative as listed in the system limitations of this
supplement.
SUPPLEMENT 12
Steep Approaches up to 5.5 Degrees
07−12−01−2
REV 70, Jun 08/07
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
5. NORMAL PROCEDURES
The normal procedures in Chapter 4 are applicable, except as modified by the following:
NOTE
Use of ILS or FMS VNAV guidance with or without the flight director is
authorized.
A. Before Start Check
(1) GPWS, STEEP APPROACH
switch/light .......................................................Press out Check ON light out.
B. In Range Check
(1) GPWS, STEEP APPROACH
switch/light .........................................................Press in Check ON light on.
C. Before Landing Check
NOTE
The airplane should be fully configured for landing and slowed to VREF
prior to glideslope intercept.
D. Go-Around
(1) GPWS, STEEP APPROACH
switch/light .......................................................Press out Check ON light out.
E. After Landing Check
(1) GPWS, STEEP APPROACH
switch/light .......................................................Press out Check ON light out.
SUPPLEMENT 12
Steep Approaches up to 5.5 Degrees
07−12−01−3
REV 70, Jun 08/07
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
6. ABNORMAL PROCEDURES
The abnormal procedures in Chapter 5 are applicable, except as modified by the following:
Discontinue steep approach landing and divert to the nearest suitable airport if any procedure
necessitates:
• an approach speed greater than VREF,
• a landing with flaps other than 45 degrees or
• an increase in actual landing distance by a factor greater than 1.50 (50%).
• a landing with any of the systems inoperative as listed in the system limitations of this
supplement.
A. Engine Failure During Approach
(1) Operating engine.............................................. Increase thrust as required.
(2) FLIGHT SPOILER lever .......................................Select to RETRACT.
Check EICAS indicates
spoilers retracted.
(3) FLAPS ..................................................................Select to 20°.
(4) Airspeed ........................................................... Increase to VREF (Flaps 45°) + 14 KIAS.
(5) Airplane ............................................................... Retrim and go-around (Refer to
Single Engine Go-Around, in
this section).
If required, autopilot may be
engaged, if above 800 feet
AGL.
Divert to a suitable landing
field that does not require a
steep approach procedure.
NOTE
The height loss during a single engine go-around is no more than
200 feet.
SUPPLEMENT 12
Steep Approaches up to 5.5 Degrees
07−12−01−4
REV 70, Jun 08/07
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
6. ABNORMAL PROCEDURES (CONT'D)
B. 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
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 Chapter 6;
PERFORMANCE –
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庞巴迪挑战者604飞机飞行手册CL604 Airplane Flight Manual 2(100)
