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• Twenty two (22), or
• The number for which seating accommodation approved for take-off and landing is
provided.
G. Cold Weather Operations
Airplane operation in cold weather conditions is to be conducted in accordance with Flight
Crew Operating Manual, Volume 1, Chapter 7, SUPPLEMENTARY PROCEDURES − Cold
Weather Operations. The minimum ambient temperature approved for take-off is −40 °C
(−40 °F).
Take-off is prohibited with frost, ice, snow or slush adhering to any critical surface (wings,
horizontal stabilizer, vertical stabilizer, control surfaces, engine inlets and upper surface of the
fuselage).
WARNING
Even small amounts of frost, ice, snow or slush on the wing leading
edges and forward upper wing surface may adversely change the
stall speeds, stall characteristics and the protection provided by the
stall protection system, which may result in loss of control on take
off.
NOTE
1. Comprehensive procedures for operating in cold weather are
provided in Flight Crew Operating Manual, Volume 1, Chapter 7;
SUPPLEMENTARY PROCEDURES − Cold Weather
Operations.
2. Take-off is permitted with frost adhering to the underside of the
wing that is caused by cold soaked fuel, in accordance with the
instructions provided in Flight Crew Operating Manual, Volume
1, Chapter 7; SUPPLEMENTARY PROCEDURES − Cold
Weather Operations − Pre-flight Preparation, External Safety
Inspection.
LIMITATIONS
OPERATING LIMITATIONS
Flight Crew Operating Manual REV 13, Nov 10, 2006
CSP 700−5000−6
Volume 1
02−04−4
1. OPERATING LIMITATIONS (CONT'D)
H. Runway Surface Condition
Operations from unprepared (i.e. gravel, grass, etc.) runways are prohibited.
I. Minimum Enroute Climb Gradient and Clearance
It is recommended that the minimum enroute net climb gradient with one engine inoperative is
positive and all terrain and/or obstacles be cleared by at least 1,300 feet along the enroute
flight path.
LIMITATIONS
OPERATING LIMITATIONS
REV 13, Nov 10, 2006 Flight Crew Operating Manual
CSP 700−5000−6
Volume 1
02−04−5
LIMITATIONS
OPERATING LIMITATIONS
Flight Crew Operating Manual REV 11, Apr 17, 2006
CSP 700−5000−6
Volume 1
02−04−6
THIS PAGE INTENTIONALLY LEFT BLANK
1. ENGINE OPERATING LIMITS
A. Type
BR700−710A2−20, quantity two.
B. Engine Operating Limits Table
CONDITION CORE RPM N2 % FAN RPM N1 % ITT°C
Start N/A N/A 700 (on ground)
850 (in flight)
Idle 58.0 (minimum) N/A 860
TakeOff
* 99.6 102.0 900 *
Max Continuous 98.9 102.0 860
− 99.8 (20 seconds) 102.5 (20 seconds) 905 (20 seconds)
Reverse Thrust − 70.0 (30 seconds) −
* Takeoff
thrust for 5 minutes with all engines operating.
Takeoff
thrust for 10 minutes in the event of an engine failure.
NOTE
Static ground operation in the range of 66% to 80% N1 is
prohibited. Acceleration/deceleration thru this range is permitted.
This limitation does not apply to reverse thrust.
C. Cold Weather Operations
Airplane operations in cold weather conditions must be conducted in accordance with
Chapter 7; SUPPLEMENTARY PROCEDURES − Cold Weather Operations.
D. Thrust Management Data
Thrust management information is advisory only. Thrust setting data presented on EICAS /
FMS must be checked for accuracy prior to use. Refer to Airplane Flight Manual, Chapter 6;
PERFORMANCE − THRUST SETTINGS.
E. Maximum Wind Speed and Direction
Engine starts are not permitted when the tailwind component exceeds 20 knots. Anytime
there is an external or EICAS indication of N1 rotation due to tailwinds, the engine must be
cranked for 30 seconds and must be followed immediately by an AUTO start.
When winds exceed 20 knots, do not exceed the minimum thrust required for taxi. When the
takeoff
crosswind component exceeds 20 knots, do not exceed 66% N1 below 30 KIAS.
There are no limits for a headwind within 10 degrees of the airplane centreline.
Refer to Chapter 4; NORMAL PROCEDURES − TAXIING AND TAKEOFF
− HIGH
CROSSWIND TAKEOFF.
LIMITATIONS
POWER PLANT
Mar 12, 2004 Flight Crew Operating Manual
CSP 700−5000−6
Volume 1
02−05−1
2. STARTER CRANKING LIMITS (GROUND AND AIR)
A. General
The starter must not be used if indicated RPM exceeds 42% N2.
B. Engine Start
Normal engine start − 3 consecutive engine start cycles of 3 minutes each with 15 seconds
　
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