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On airplanes 5301 to 5630 NOT incorporating Service Bulletin 604−49−006 or
604−49−009:
Below 60% rpm − maximum 20 seconds
Between 60% and 95% rpm − maximum 10 seconds
(5) APU starting and operation is permitted within the following operating envelope:
Temperature − Refer to Figure 02−04−1.
Altitude and Airspeed − Refer to Figure 02−05−4 or 02−05−5.
(6) In-flight start:
In-flight starting is guaranteed at altitudes below 20,000 feet.
On airplanes 5301 to 5630 NOT incorporating Service Bulletin 604−49−006 or
604−49−009:
In-flight starting is guaranteed at altitudes below 15,000 feet and has been demonstrated
at altitudes up to 20,000 feet.

CL-604 Airplane Flight Manual
PSP 604−1
DOT Approved
REV 59, Jan 30/06
LIMITATIONS
Power Plant
02−05−13
12. AUXILIARY POWER UNIT (CONT’D)
E. APU Bleed Air
(1) Engine-start during ground operations up to 15,000 feet:
(a) No bleed air extraction limitation. Each engine may be started using the APU as
a bleed air source.
(b) If both engines are to be started using the APU bleed air, then the operating
engine’s thrust must not exceed 70 % N2.
(2) Engine-start during flight:
(a) During single engine operations, APU bleed air extraction for an engine start is
not permitted.
(b) During double engine failure conditions, APU bleed air extraction for engine
starts is permitted.
In-flight APU main engine starts have been demonstrated to 15,000 feet
On airplanes 5301 to 5630 NOT incorporating Service Bulletin 604−49−006 or
604−49−009:
In-flight APU main engine starts have been demonstrated to 10,000 feet.
(3) Air-conditioning:
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:
Bleed air extraction from the APU is not permitted above 14,500 feet.
APU bleed air extraction is not permitted in flight whenever standby electrical power is
required from the APU.
F. APU Generator
The maximum permissible load on the APU generator in flight is 30kVA.
On airplanes 5301 to 5630 NOT incorporating Service Bulletin 604−49−006 or
604−49−009:
Use of the APU generator in flight is not permitted unless both main generators have failed
or are off-line.
G. APU Indications
The APU limit display markings on the EICAS must be used to determine compliance with
the maximum/minimum limits and precautionary ranges. If EICAS markings show more
conservative limits than those specified below, the limit markings on the EICAS should be
used.
Indication Red
(max / min limitations)
Amber
(caution range)
Green
(normal range)
APU
EGT C
start scale 974 and above 680 to 973 0 to 679
normal scale 731 and above 680 to 730 0 to 679
APU RPM % 110 and above 105 to 109 0 to 104

CL-604 Airplane Flight Manual
PSP 604−1
DOT Approved
REV 59, Jan 30/06
LIMITATIONS
Power Plant
02−05−14
ALTITUDE X 1000 FT.
APU start and generator operation guaranteed − 20,000 feet
0 100 200 300
KIAS (KNOTS)
25
20
15
10
0
141 290
APU in-flight starting is guaranteed up to 20,000 feet.
APU Operation is permitted up to 20,000 feet.
pneumatic operation guaranteed − 15,000 feet
APU In-Flight Envelope
Figure 02−05−4
Main engine starting is guaranteed up to 15,000 feet.
APU generator operation is guaranteed up to 20,000 feet.
APU pneumatic operation is guaranteed up to 15,000 feet.
5
Main engine start and

CL-604 Airplane Flight Manual
PSP 604−1
DOT Approved
REV 59, Jan 30/06
LIMITATIONS
Power Plant
02−05−15
On airplanes 5301 to 5630 NOT incorporating Service Bulletin 604−49−006 or 604−49−009:
APU In-Flight Envelope
Airplanes 5301 to 5630 NOT incorporating SB 604−49−006 or 604−49−009
Figure 02−05−5
ALTITUDE X 1000 FT.
Maximum starting envelope 20,000 feet.
0 100 200 300
KIAS (KNOTS)
25
20
15
10
5
0
141 290
In-flight starting is guaranteed up to 15,000 feet
APU Operation is permitted up to 20,000 feet.
Ground starting permitted up to 15,000 feet.
and has been demonstrated up to 20,000 feet.
In-flight start guaranteed
　
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