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is 5 C (41 F) or less, or it cannot be determined that the wing fuel temperature is above 0 C
(32 F); and:
There is visible moisture (rain, drizzle, sleet, snow, fog, etc); or
Water is present on the wing; or
The difference between the dew point temperature and the OAT is 3 C (5 F) or less; or
The atmospheric conditions have been conducive to frost formation.
NOTE
Ice and frost may continue to adhere to wing surfaces
for some time even at outside air temperatures above
5 C (41 F).
15/05/95
CL-604 Airplane Flight Manual
PSP 604−1
DOT Approved
REV 61, Jun 29/06
TEMPORARY REVISION 604/19−1
Page 4 of 4
Jul 03/06
INSERT IN LIMITATIONS
FACING PAGE 02−04−5
REASON FOR ISSUE
Temporary revision to advise the flight crew of the following:
Additional operational limitations for SAA of Ukraine registered airplanes.
ACTION
Add paragraph 8. as follows:
8. MAXIMUM CROSSWIND COMPONENT
The maximum crosswind component for take-off and landing on a dry runway is 24 knots
(12 meters/sec).
The maximum crosswind component for take-off and landing on a wet runway with water depth
no more than 3.00 mm (0.125 inch) is defined in the following table for different values of the
coefficient of friction:
Reported Coefficient of Friction Maximum Crosswind Component
0.3 (poor braking) 10 knots (5 meters/sec)
0.4 (average braking) 15 knots (8 meters/sec)
0.5 (good braking, equivalent to dry) 24 knots (12 meters/sec)
The maximum crosswind component for take-off and landing on a contaminated runway is
10 knots (5 meters/sec).
Operation on runways with a coefficient of friction less than 0.3 is prohibited.
15/05/95
CL-604 Airplane Flight Manual
PSP 604−1
DOT Approved SAAU
LIMITATIONS
Operating Limitations
02−04−5
4. RUNWAY SLOPES
The maximum runway slopes approved for take-off and landing are:
+2% (uphill)
−2% (downhill)
5. TAILWIND CONDITIONS
The maximum tailwind component approved for take-off and landing is 10 knots.
6. MINIMUM FLIGHT CREW
The minimum flight crew is one pilot and one copilot.
7. MAXIMUM OCCUPANTS
The total number of occupants, including no more than nineteen passengers, must not exceed
the lesser of the following:
Twenty-two or,
The number for which seating accommodation approved for take-off and landing is
provided.
15/05/95
CL-604 Airplane Flight Manual
PSP 604−1
DOT Approved
REV 61, Jun 29/06
LIMITATIONS
Operating Limitations
02−04−6
THIS PAGE INTENTIONALLY LEFT BLANK
15/05/95
CL-604 Airplane Flight Manual
PSP 604−1
DOT Approved
REV 61, Jun 29/06
LIMITATIONS
Operating Limitations
02−04−5
4. RUNWAY SLOPES
The maximum runway slopes approved for take-off and landing are:
+2% (uphill)
−2% (downhill)
5. TAILWIND CONDITIONS
The maximum tailwind component approved for take-off and landing is 10 knots.
6. MINIMUM FLIGHT CREW
The minimum flight crew is one pilot and one copilot.
7. MAXIMUM OCCUPANTS
The total number of occupants, including no more than nineteen passengers, must not exceed
the lesser of the following:
Twenty-two or,
The number for which seating accommodation approved for take-off and landing is
provided.
8. MAXIMUM CROSSWIND COMPONENT
The maximum crosswind component for take-off and landing is 24 knots (12 meters/sec).
15/05/95
CL-604 Airplane Flight Manual
PSP 604−1
DOT Approved
REV 61, Jun 29/06
AR
LIMITATIONS
Operating Limitations
02−04−6
THIS PAGE INTENTIONALLY LEFT BLANK
15/05/95
CL-604 Airplane Flight Manual
PSP 604−1
DOT Approved
REV 61, Jun 29/06
LIMITATIONS
Power Plant
02–05–1
1. ENGINES
Type: General Electric CF34–3B, quantity two.
2. ENGINE INDICATIONS
The engine limit display markings on 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 must be used.
Indication Red
(max / min limits)
Amber
(caution range)
Green
(normal range)
N1 % RPM 98.6 – 0 to 98.5
ITT °C:
– APR not
i
900
(for first 2 min.)
– 0 to 900
operating
884
(for next 3 min.)
–
0 to 884
– APR operating 928
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