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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
02−05−18
REV 71, Oct 31/07
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
12. AUXILIARY POWER UNIT (CONT'D)
LIMITATIONS
Power Plant
02−05−19
REV 71, Oct 31/07
APU In-Flight Envelope
Figure 02−05−6
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
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
02−05−20
REV 71, Oct 31/07
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
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
02−06−1
REV 66, Feb 01/07
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
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
02−06−2
REV 66, Feb 01/07
DOT Approved
CL−604 Airplane Flight Manual
PSP 604−1
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
5. MAXIMUM LANDING GEAR OPERATING SPEED
The maximum airspeed at which it is safe to extend the landing gear is 197 KIAS / 0.6 MI.
The maximum airspeed at which it is safe to retract the landing gear is 197 KIAS / 0.6 MI.
6. MAXIMUM LANDING GEAR EXTENDED SPEED
The maximum airspeed at which the airplane may be flown with the landing gear extended and
locked is 250 KIAS / 0.7 MI.
Flight at altitudes above 20,000 feet with the landing gear extended is prohibited.
7. TIRE LIMIT SPEED
The tire limit speed is 182 knots ground speed.
8. MAXIMUM AIRSPEED FOR ADG OPERATION
On airplanes 5301 to 5407:
The maximum airspeeds for continuous operation of the air-driven generator are as follows:
• Following automatic or manual deployment, the maximum airspeed is 250 KIAS.
• When operationally necessary (e.g. windmill airstarts), speeds up to 330 KIAS are permitted
for a period of twelve (12) minutes, and speeds between 330 and 348 KIAS are permitted for
a period of four (4) minutes.
• For flight test or pilot training deployment, the maximum airspeed is 215 KIAS.
9. TURBULENCE PENETRATION SPEED
Maximum air speed for turbulence penetration is 280 KIAS or 0.75 Mach, whichever is lower.
10. MINIMUM OPERATING LIMIT SPEED
Intentional speed reduction below the onset of stall warning, as defined by stick shaker operation,
is prohibited unless a lower speed is specifically authorized for flight test or training operations.
　
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