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886 2 minutes
Normal take-off 96.2 98.3 842 5 minutes
864 2 minutes
Maximum continuous 98.6 99.2 838 −
Start/relight 930
889
16 seconds
50 seconds
Minimum idle in icing conditions
(cowl anti-ice only)
− 64.0 − −
N O T E
1. The above take-off and maximum continuous
limits for N1, N2 and ITT are engine limits
and are not presented for purposes of
setting power. The pilot must observe the
take-off and maximum continuous power
settings for the appropriate pressure
altitude, ambient temperature and bleed air
extraction as presented in the PERFORMANCE
section of this manual.
2. Above 40,000 feet one ACU or cowl anti-ice
must be selected on for each engine.
MODEL CL−600−2A12
AIRPLANE FLIGHT MANUAL
PSP 601−1A−1
MODEL CL-600-2A12
AIRPLANE FLIGHT MANUAL
PSP 601-1A-1
4. POWER PLANT LIMITATIONS (Coni/d)
C. AUTOMATIC PERFORMANCE RESERVE (APR)
(1) If take-off performance is predicated upon the use of APR, take-off
with the APR system armed must not be attempted until satisfactory
static and dynamic APR system tests have been achieved.
(2) The APR system must be selected OFF for take-off if:
(a) Pre-flight static or dynamic tests fail.
(b) Ambient temperature is below -20°C (-4°F).
D. OIL TEMPERATURE
Minimum for starting: -40°C
Maximum permissible: +163°C (15 minutes maximum)
Maximum for single engine climb: +155°C (60 minutes maximum)
Maximum continuous: +150°C
E. OIL PRESSURE
Transient cold start:
(Six minutes maximum)
Minimum at steady state idle:
Minimum at take-off (power):
Maximum continuous:
F. ENGINE AIRSTART
100 psi (transmitter limit)
(Engine must remain at idle until oil
pressure returns to normal range.)
25 psi
40 psi
95 psi
Engine starting in flight is permitted only within the envelope defined
in Figure 3.
AIR TURBINE STARTER
The starter must not be used if indicated N2 rpm exceeds 55%.
Starter Duty Cvcie
Normal engine start
Motoring and engine
start at -30°C (-22°F)
and below
Motoring with engine
fuel and ignition OFF
JMITWriONS
r'age 8
Three consecutive engine start cycles
with 5 minutes cooling between
additional cycles.
Motor engines for 60 seconds and assure
fan rotation. Then two consecutive
engine start cycles with 5 minutes
cooling between additional cycles.
90 seconds with 5 minutes cooling
between additional cycles of 30 seconds.
DOT Approved
Apr 20/98
44,600/45,100
LIMITATIONS
Page 9
Start Envelope
Figure 3
DOT Approved
Jan 30/07
44,600/45,100
ASSOCIATED CONDITIONS
For air turbine starts in flight: For air turbine starts on the ground:
At initiation of thrust lever movement: At initiation of thrust lever movement:
1) ITT is to be 90C or less. 1) ITT is to be 120C or less.
2) N2 must be 28% or greater. 2) N2 must be 20% or greater.
For windmill starts:
At initiation of thrust lever movement:
1) ITT must be 120C or less.
2) Above 10,000 feet, N2 must be 13% and
stable or increasing.
At or below 10,000 feet, N2 must
be 12% and stable or increasing.
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