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(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.
END
SUPPLEMENTARY PROCEDURES
Steep Approaches up to 5.5 Degrees
Vol. 1 06−26−8
REV 70, Jun 08/07
CL−604 Operating Manual
PSP 604−6
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 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.
If go-around was due to engine failure during approach:
(7) In-Flight Engine Failure/Shutdown .............. Accomplish Refer to Chapter 5 –
ABNORMAL PROCEDURES
– POWER PLANT – In-Flight
Engine Failure/Shutdown.
END
7. SUPPLEMENTARY PROCEDURES
The supplementary procedures in Chapter 6 are applicable.
SUPPLEMENTARY PROCEDURES
Steep Approaches up to 5.5 Degrees
Vol. 1 06−26−9
REV 70, Jun 08/07
CL−604 Operating Manual
PSP 604−6
8. PERFORMANCE
The performance data in Chapter 6 of the Airplane Flight Manual are applicable, except as
modified by the following:
The data in this supplement are applicable to steep approaches from 4.5 to 5.5 degrees
(inclusive), except for this section, which is applicable only for approaches conducted at
5.5 degrees. For all other approach angles, the performance data in Chapter 6 of the Airplane
Flight Manual is applicable.
A. Landing Performance
The reference screen height used for landing is 50 feet.
The reference steep approach glide slope angle is 5.5 degrees.
(1) LANDING FIELD LENGTH AND SPEED
The landing field length required for 5.5 degree approach operations for varying
conditions of airplane landing weight, airport pressure altitude and wind is provided by
Figure 06−26−2. The actual landing distance required is also given within this chart.
The landing approach speed (VREF) for varying airplane landing weights and airport
pressure altitude for steep approach operations is also given by Figure 06−26−2.
The actual landing distance given on Figure 06−26−2 is the distance from a 50 foot
height at VREF with flaps 45°, to a full stop on a smooth, dry, level, hard-surfaced runway
and ISA temperature for steep approach operations.
NOTE
1. The landing field length derived from Figure 06−26−2 includes
factors for operational rules which require use of 60% of the available
runway (landing field length required).
2. Operational rules may require that for wet or slippery runway surfaces,
the runway length available be at least 115% of the landing field length
derived from Figure 06−26−2 .
Example:
Associated Conditions:
Landing gross weight = 15,000 kg (33,069 lb)
Airport pressure altitude = 4,000 feet
Wind = 20 knots, headwind
The example in Figure 06−26−2, shows that for the above conditions, the actual landing
distance is 705 meters (2,313 feet) and the landing field length is 1,175 meters
(3,855 feet).
VREF for the same conditions as above is 126 KIAS.
　
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