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A. Type:
36–150 (CL)
On airplanes 5301 to 5630 NOT incorporating Service Bulletin 604–49–006 or
604–49–009:
GTCP-36-100(E)
B. Maximum RPM: 110%
The APU overspeed control will automatically shutdown the APU at 107% rpm.
On airplanes 5301 to 5630 NOT incorporating Service Bulletin 604–49–006 or
604–49–009:
The APU overspeed control will automatically shutdown the APU at 110% rpm.
C. Maximum EGT: 731°C
LIMITATIONS
Power Plant
02−05−15
REV 71, Oct 31/07
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
12. AUXILIARY POWER UNIT (CONT'D)
D. Starting:
(1) Minimum ambient temperature for starting a cold soaked APU on the ground is –40°C.
(2) The following APU start cycles are permitted:
(a) Using airplane batteries on the ground or for normal in-flight start:
• Three start attempts, each of 30 seconds continuous cranking
• Followed by a 20-minute off-time
• Followed by two further attempts each of 30 seconds continuous cranking.
(b) Using ground power:
• Two start attempts, each of 15 seconds continuous cranking
• Followed by a 20-minute off-time
• Followed by two further attempts each of 15 seconds continuous cranking.
(c) If, in either case (2)(a) or (2)(b) a successful start is not obtained, a further start must
not be attempted for a period of at least 35 minutes.
(3) Maximum EGT:
974°C (not to be exceeded under any operating conditions)
(4) Hung start:
If not greater than 30% rpm within 60 seconds
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 02−05−6 or Figure 02−05−7.
(6) In-flight start:
In-flight starting is guaranteed at altitudes up to 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 up to 15,000 feet and has been demonstrated
at altitudes up to 20,000 feet.
LIMITATIONS
Power Plant
02−05−16
REV 71, Oct 31/07
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
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.
LIMITATIONS
Power Plant
02−05−17
REV 71, Oct 31/07
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
12. AUXILIARY POWER UNIT (CONT'D)
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
　
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