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side slip angles), as they may cause
structural failure at any speed, including
below VA.
DOT Approved
Jul 16/04
44,600/45,100
LIMITATIONS
Page 17
MODEL CL-600-2A12
AIRPLANE FLIGHT MANUAL
PSP 601-1A-1
Weight
Ob)
Weight
(kg)
Altitude
(feet)
Sea Level
10,000
15,000
20,000
25,000
30,000
35,000
40,000
45,000
24,525
11,124
172
174
179
186
194
203
211
218
225
31,000
14,061
193
201
209
219
229
238
245
248
-
36,000
16,329
Design ^
211
224
234
245
255
264
268
-
-
38,000
17,237
lanoeuveri
(KIAS
217
232
243
254
265
274
276
-
-
43,100
19,550
ng Speed
)
236
256
267
278
289
294
-
-
-
44,600
20,230
(VA)
241
263
275
286
297
304
-
-
-
45,100
20,457
(SB 601-0360)
243
265
278
290
299
304
-
-
-
LIMITATIONS
Page 18
Design Manoeuvering Speed - VA
Figure 5
DOT Approved
Sep 25/90
44,600
cacnhaacufeanirQer
MODEL CL-600-2A12
AIRPLANE FLIGHT MANUAL
PSP 601-1A-1
5. MAXIMUM OPERATING LIMIT SPEEDS (Cont'd)
D. FLAPS EXTENDED SPEED (VFE) |
The maximum speeds at which the flaps may be extended are:
flaps to 20 degrees: 232 KIAS
flaps to 30 degrees: 198 KIAS
flaps to 45 degrees: 190 KIAS
E. MAXIMUM LANDING GEAR OPERATING SPEED (VL0) |
The maximum airspeed at which the landing gear may be lowered or raised is
197 KIAS/0.7 M L
F. MAXIMUM LANDING GEAR EXTENDED SPEED (VLE) |
The maximum airspeed at which the airplane may be flown with the landing
gear extended and locked is 250 KIAS/0.7 Mi.
On airplanes incorporating Canadair Service Bulletin 601-0329 Part B(3),
Special Check/Modification - Main Landing Gear Door - Hinge and
Fasteners, but not Part C, the maximum airspeed at which the airplane may
be flown with the landing gear extended and locked is 197 KIAS.
G. TIRE LIMIT SPEED |
The tire limit speed is 183 knots ground speed.
H. MAXIMUM AIRSPEED FOR ADG OPERATION |
The maximum airspeed for continuous operation of the air driven generator
following automatic or manual deployment is 250 KIAS. When operationally
necessary, speeds up to 330 KIAS are permitted for a period of twelve (12)
minutes reducing to a period of four (4) minutes at VMO with linear
interpolation. For flight test or pilot training deployment, the maximum
airspeed is 215 KIAS.
I. TURBULENCE PENETRATION SPEED |
Turbulence penetration speed is 280 KIAS or 0.75 Mi, whichever is lower.
DOT Approved
Mf 27/97 LIMITATIONS
44,600/45,100 Page- 19
MODEL CL-600-2A12
AIRPLANE FLIGHT MANUAL
PSP 601-1A-1
6. 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.
7. MANOEUVERING LIMIT LOAD FACTORS
These load factors limit the permissible angles of bank in turns and the
　
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