PILOT’S OPERATING HANDBOOK
SECTION 2
LIMITATIONS
EASA Approved
Edition 0 -- October 31, 2013
Rev. 1
Page 2.6.9
Flight into icing conditions
1) All equipment required for IFR flight
2) Propeller deicing
3) L.H. windshield deicing
4) Airframe, stabilizer and elevator horn deicing
5) Wing leading edge inspection light (if night flight)
6) Stall warning deicing
7) Inertial separator
8) Garmin annunciation ”Airspeed, Airspeed”
ALTITUDE OPERATING LIMITS
Maximum altitude : 31000 ft (9449 m)
Maximum differential pressure : 6.2 psi
Operation in RVSM area
This airplane is approved for operations in Reduced Vertical Separation Minimum (RVSM) airspace when required
equipment (refer to Section ”List of equipment”, § ”List of critical RVSM equipment”) is maintained in accordance
with the airplane Maintenance Manual.
This does not constitute operational approval. Individual airplane and operational approval must be obtained in
accordance with applicable operating rules.
Each operator must ensure compliance with required crew training and operating practices and procedures.
Moreover, the following equipment must be installed and operating normally upon entering RVSM airspace :
-
Pilot and R.H. station primary altimeters
-
Autopilot
-
Altitude Alerter
-
ATC transponder
NOTE
Any changes to the pitot / static, air data computer, autopilot, altitude alerting and / or
transponder systems, or other changes that affect operation of these systems must be
evaluated for impact on the RVSM approval.
The standby altimeter is not approved for RVSM operations.
IN-FLIGHT CIRCUIT BREAKER USE LIMITS
A tripped circuit breaker should not be reset in flight unless deemed necessary for continued safe flight and landing.
Only one reset should be attempted.
