2-21
Systems and Equipment Limits
2-21-1
Stall Warning / Stick Pusher System
Preflight function test required before takeoff.
System is required to function properly in normal mode for all flights and in ice mode for flight
into known icing conditions.
2-21-2
Brakes
To allow adequate cooling of the wheels and brakes the aircraft must remain on the ground for
at least 45 min following the two events:
−
Rejected takeoff with brake on speed greater than V
R
-20 kts and heavy brake usage
−
0° flap full stop landing and heavy brake usage.
2-21-3
Trim Systems
Stabilizer normal and alternate, and rudder trim systems must function properly for all flights.
2-21-4
Heated Windshield
Left Hand and Right Hand Heated Windshields must function properly for all flights. Exception,
for IFR flights conducted into no known or forecast icing conditions at least one heating zone of
the windshield on the side of the pilot in command must function properly.
2-21-5
Fire Detection System
Preflight Function Test is required for takeoff.
System must function properly for all flights.
2-21-6
Engine Ice Protection
Preflight Function Test is required for takeoff.
2-21-7
Oxygen System
A minimum oxygen supply of 10 minutes duration for each occupant is required for dispatch for
pressurized flight above FL250.
Note
Some National Operating Requirements may require that a larger quantity of oxygen be
carried on the aircraft.
The oxygen system shutoff valve handle in the cockpit must be selected to ON prior to engine
start and throughout the duration of flight.
The oxygen masks for the crew must be connected for all flights.
Section 2 - Limitations (EASA Approved)
Systems and Equipment Limits
Pilot's Operating Handbook
Report No: 02406
Issue date: Dec 18, 2020
Page 2-21-1
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