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During double engine failure conditions, APU bleed air extraction for
engine starts is permitted.
On airplanes not incorporating Service Bulletin 601−0568 or 601−0581:
In-flight APU main engine starts have been demonstrated to 10,000 feet.
On airplanes incorporating Service Bulletin 601−0568 or 601−0581:
In-flight APU main engine starts have been demonstrated to 15,000 feet.
APU Generator:
The maximum permissible load on the APU generator in flight is 30 kVA.
On airplanes not incorporating Service Bulletin 601−0568 or 601−0581:
(a) With APU supplying bleed air during take-off and landing, the APU
generator must be selected OFF.
(b) In-flight use of the APU generator is intended only if both main
generators have failed. Use of the APU generator is not permitted
unless both main generators are off line.
MODEL CL−600−2A12
AIRPLANE FLIGHT MANUAL
PSP 601−1A−1
DOT Approved
Sep 11/06
44,600/45,100
LIMITATIONS
Page 14A
APU In-Flight Envelope
(Airplanes NOT Incorporating
Service Bulletin 601−0568 or 601−0581)
Figure 4
AIRSPEED: 0 to 290 KIAS
AIRSPEED: 141 KIAS to 290 KIAS
MODEL CL−600−2A12
 

　
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