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15,000 feet

CL-604 Airplane Flight Manual
PSP 604−1
DOT Approved
REV 59, Jan 30/06
LIMITATIONS
Power Plant
02−05−16
THIS PAGE INTENTIONALLY LEFT BLANK
15/05/95
CL-604 Airplane Flight Manual
PSP 604−1
DOT Approved
REV 57, Jul 19/05
LIMITATIONS
Operating Speeds
02–06–1
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.
2. RVSM MAXIMUM OPERATING SPEED
On airplanes incorporating Canadair Service Bulletin 604–34–012:
The maximum cruise mach number during flight in RVSM airspace is 0.83.
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.
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.
15/05/95
CL-604 Airplane Flight Manual
PSP 604–1
DOT Approved
REV 53, Jun 04/04
LIMITATIONS
Operating Speeds
02–06–2
Maximum Operating Speed and Mach Number
Figure 02–06–1
15/05/95
CL-604 Airplane Flight Manual
PSP 604–1
DOT Approved
Sep 20/95
LIMITATIONS
Operating Speeds
02–06–3
Design Maneuvering Speeds
Figure 02–06–2
15/05/95
CL-604 Airplane Flight Manual
PSP 604–1
DOT Approved
Sep 20/95
LIMITATIONS
Operating Speeds
02–06–4
7. TIRE LIMIT SPEED
The tire limit speed is182 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.
15/05/95
CL-604 Airplane Flight Manual
PSP 604–1
DOT Approved
REV 37, Oct 12/99
LIMITATIONS
Maneuvering Loads
02–07–1
1. MANEUVERING LIMIT LOAD FACTORS
These load factors limit the permissible angles of bank in turns and the severity of pull-up and
push-over maneuvers:

Flaps up: –1.0 G to 2.5 G

Flaps down: 0.0 G to 2.0 G
2. SIDE SLIP MANEUVERS
Avoid unnecessary and large side-slip maneuvers during low speed high altitude cruise.
15/05/95
CL-604 Airplane Flight Manual
PSP 604–1
DOT Approved
Sep 20/95
LIMITATIONS
Maneuvering Loads
02–07–2
THIS PAGE INTENTIONALLY LEFT BLANK
15/05/95
CL-604 Airplane Flight Manual
PSP 604–1
DOT Approved
Sep 20/95
LIMITATIONS
Systems Limitations
02–08–1
1. AIR-CONDITIONING AND PRESSURIZATION

The maximum relief differential pressure is 9.2 psi.

The maximum negative differential pressure is –0.5 psi.
　
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