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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
Vol. 1 02−05−17
REV 71, Oct 31/07
CL−604 Operating Manual
PSP 604−6
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
RED
(MAX 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
LIMITATIONS
Power Plant
Vol. 1 02−05−18
REV 71, Oct 31/07
CL−604 Operating Manual
PSP 604−6
12. AUXILIARY POWER UNIT (CONT'D)
LIMITATIONS
Power Plant
Vol. 1 02−05−19
REV 71, Oct 31/07
APU In-Flight Envelope
Figure 02−05−6
CL−604 Operating Manual
PSP 604−6
12. AUXILIARY POWER UNIT (CONT'D)
On airplanes 5301 to 5630 NOT incorporating Service Bulletin 604–49–006 or 604–49–009:
15
20
25
10
5
0
0 100
141
200
290
300
KIAS (KNOTS)
ALTITUDE X 1000 FT.
15,000 feet
Maximum starting envelope 20,000 feet.
In-flight starting is guaranteed up to 15,000 feet
and has been demonstrated up to 20,000 feet.
Ground starting permitted up to 15,000 feet.
APU Operation is permitted up to 20,000 feet.
DFM0205_004
In-flight start guaranteed
APU In−Flight Envelope (Airplanes 5301 to 5630 NOT incorporating
SB 604−49−006 or 604−49−009)
Figure 02−05−7
LIMITATIONS
Power Plant
Vol. 1 02−05−20
REV 71, Oct 31/07
CL−604 Operating Manual
PSP 604−6
1. MAXIMUM OPERATING SPEED AND MACH NUMBER
Maximum operating limit speeds as given in Figure 02−06−1, must not be deliberately exceeded
in any regime of flight (climb, cruise or descent), unless a higher speed is specifically authorized
for flight test or training operations.
DFM0206_001
Maximum Operating Speed and Mach Number
Figure 02−06−1
2. RVSM MAXIMUM OPERATING SPEED
On airplanes incorporating Service Bulletin 604–34–012:
The maximum cruise mach number during flight in RVSM airspace is 0.83.
LIMITATIONS
Operating Speeds
Vol. 1 02−06−1
REV 66, Feb 01/07
CL−604 Operating Manual
PSP 604−6
3. DESIGN MANEUVERING SPEED
Full application of rudder and aileron controls as well as maneuvers that involve angles of attack
near the stall, must be confined to speeds below VA. Values of VA are given in Figure 02−06−2,
for varying pressure altitudes and airplane weights.
CAUTION
Avoid rapid and large alternating control inputs, especially in
combination with large changes in pitch, roll, or yaw (e.g. large side slip
angles), as they may cause structural failure at any speed, including
below VA .
DFM0206_002
Design Maneuvering Speeds
Figure 02−06−2
LIMITATIONS
Operating Speeds
Vol. 1 02−06−2
REV 66, Feb 01/07
CL−604 Operating Manual
PSP 604−6
4. FLAPS EXTENDED SPEED
The maximum speeds at which the flaps may be extended are:
Flaps to 20 degrees: 231 KIAS
Flaps to 30 degrees: 197 KIAS
Flaps to 45 degrees: 189 KIAS
　
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