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stick shaker activation, for a load factor of 1.0 g.
PERFORMANCE
General
06−01−26
REV 66, Feb 01/07
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
4. FLIGHT CAPABILITIES (CONT'D)
DFM0601_013 buffet_afm_uni
PERFORMANCE
General
06−01−27
REV 66, Feb 01/07
Maneuvering Capabilities
Figure 06−01−13
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
5. PERFORMANCE CONDITIONS AND CONFIGURATIONS
A. Minimum Control Speed, Air (VMCA)
VMCA in the take-off configuration = 116 KIAS
B. Minimum Control Speed, Ground (VMCG)
The minimum control speed on the ground, for varying conditions of ambient temperature and
airport pressure altitude, is shown on Figure 06−01−14.
DFM0601_014 VMCG604DKC−13JUN96
Minimum Control Speed, Ground (VMCG)
Figure 06−01−14
C. Minimum Control Speed, Landing (VMCL)
VMCL in the approach and landing configuration = 116 KIAS
D. Demonstrated Crosswind (Take-Off and Landing)
The maximum demonstrated crosswind component for take-off and landing [at 33 feet (10
meters) tower height] is 24 knots and is not considered limiting for take-off and landing. When
using reverse thrust, this speed is limiting.
Landings have been performed at an approach speed of VREF +1/2 of the steady state wind
plus all of the gust up to a maximum of VREF + 20 knots.
PERFORMANCE
General
06−01−28
REV 66, Feb 01/07
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
5. PERFORMANCE CONDITIONS AND CONFIGURATIONS (CONT'D)
E. Maximum Tailwind (Take-Off and Landing)
The maximum tailwind component for take-off and landing [at 33 feet (10 meters) tower
height] is 10 knots.
F. Configurations and Thrusts
PHASE OF FLIGHT ENGINE THRUST
SETTING
FLAPS
(DEGREES) LANDING GEAR
Take - Off Take-off thrust,
2 engines to VEF, then
1 engine at automatic
performance reserve
(APR), or take-off thrust
if APR is not armed.
20 Down
First Segment Climb Automatic performance
reserve (APR), or
take-off thrust if APR
not armed, 1 engine.
20 Down
Second Segment Climb Same as First Segment. 20 Up
Final Take-Off Climb Maximum continuous
thrust, 1 engine 0 Up
Enroute Climb Maximum continuous
thrust, 1 engine 0 Up
Approach Climb Single engine climb
(APR rating) thrust,
1 engine, set manually.
FAA Certified
Airplanes
Normal take-off
thrust, 1 engine
20 Up
Landing Climb Normal take-off thrust,
2 engines 45 Down
Landing Idle, 2 engines 45 Down
Take-off performance data are presented allowing for the use of the APR system and for
situations where APR is not used. The effects of 10th stage engine bleeds (for Packs) open
and closed, and cowl and wing anti-ice systems on and off, are also presented.
NOTE
Flaps 30° is an intermediate flap position and no procedures or performance
data are predicated on its use.
PERFORMANCE
General
06−01−29
REV 66, Feb 01/07
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
PERFORMANCE
General
06−01−30
REV 66, Feb 01/07
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
THIS PAGE INTENTIONALLY LEFT BLANK
1. THRUST SETTINGS
A. General
This section presents normal take-off thrust settings, single engine climb thrust (APR rating)
settings and single engine maximum continuous thrust (MCT) settings for various ambient
temperatures, pressure altitudes and engine bleed configurations.
Normal take-off thrust settings are used during the following conditions:
(1) Normal take-off, set statically;
(2) Go-around with all engines operating (landing climb).
FAA Certified Airplanes:
(1) Normal take-off, set statically;
(2) Go-around.
Single engine climb thrust (APR rating) settings are used during the following conditions:
(1) Manual readjustment of thrust setting during the second segment climb, for a take-off
with one engine inoperative;
(2) Go-around with one engine inoperative (approach climb).
FAA Certified Airplanes:
(1) Manual readjustment of thrust setting during the second segment climb, for a take-off
with one engine inoperative.
Single engine maximum continuous thrust (MCT) settings are used during the following
conditions:
(1) Level flight acceleration from V2 to VFTO ;
(2) Final segment/enroute climb.
PERFORMANCE
Thrust Settings
　
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