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Required Flight Crew
Pilot, Co-Pilot (Captain, First Officer)
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Types of Aircraft Operations
- Day and Night
- VFR and IFR
- Flight in Icing Conditions
- RVSM
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Maximum differential pressure
8.1 psi
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Auto Mode normal maximum differential pressure
7.8 psi
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Maximum negative differential pressure
-0.3 psi
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Maximum Altitude for operation after an in flight depressurization
10,000 MSL (unless MEA or other constraints require a higher altitude)
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Maximum altitude when aircraft is dispatched unpressurized flight
10,000 ft.
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Maximum Speed for SL
250 KIAS / .50 mach
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Maximum Speed for 10,000 ft
320 KIAS / .78 mach
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Maximum Speed for 26,000 ft
320 KIAS / .78 mach
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Maximum Speed for 30,000 ft
320 KIAS / .78 mach
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Maximum Speed for 35,000 ft
296 KIAS / .78 mach
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Maximum Speed for 37,000 ft
350 KIAS / .78 mach
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Maximum Operation (VMO/MMO)
320/.78
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Maximum operating (KIAS) 8,000 to 10,000 ft. MSL VMO
Red Line
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Maximum operating (KIAS) up to -8,000 ft. MSL VMO
250
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Maximum turbulence penetration VB/MB
250/.63 whichever is lower, 200 at or below 10,000
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Maximum manuevering speed VA
200
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VLOE (Landing gear extention)
250
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VLE (landing gear extended)
250
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VLOR (landing gear retration)
200
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Flap 9 Vfe airspeed limit
250
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Flap 22 Vfe airspeed limit
200
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Flap 45 Vfe airspeed limit
145
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Maximum wiper operation speed
160
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Momentary airspeed excursions that are due to wind gusts or turbulence are allowed up to 155 kts.
with no crew or matinenance action required
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Steady state operation over 145 kts
is not allowed and must be entered into the AML
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Maximum Operating Altitude
37,000 ft
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Minimum takeoff and landing pressure altitude
-1,000 ft
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Maximum takeoff and landing pressure altitude
8,000 ft
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Minimum takeoff and landing temperature
-40C SAT
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Maximum takeoff and landing temperature (-1,000 pressure altitude)
52C SAT
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Maximum takeoff and landing temperature (8,000 pressure altitude)
34C SAT
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In the even of a landing below -40C SAT, the aircraft:
may not takeoff without further maintenance inspection
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TAT in cruise flight above 25,000 ft. is
limited to -45C
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(on ground) Icing condition exist when:
OAT 10C or below and visible moisture is present
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(on ground) Icing condition exist also exist when:
OAT 10C or below when operating on ramps, taxiways or runways where surface snow, ice, standing water or slush may be ingested by engines, or freeze on engines, nacelles or engine sensor probes.
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(in flight) Icing conditions exist whenever the TAT is 10C or below and:
visible moisture in any form is present
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Minimum temperature for manual Anti-Ice Operation
-40C
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Maximum temperature for manual Anti-Ice Operation
10C
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SAT (or static air temperature)
to be used on the ground
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TAT (or Total Air Temperature)
to be used in flight
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There is no temperature limitation for:
automatic Anti-Ice System operation
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Takeoff is Prohibited when:
frost, snow, ice or slush is adhereing to the wings conrol surfaces, stabilizers, pitot static ports or AOA vanes
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Takeoff with frost on the fuel tank underwing surfaces is permitted:
provided it does not exceed 1/8 inch
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A runway is considered contaminated when more than 25% of the required field length within the width being used is cover by:
- More than 1/8 inch of
- standing water
- slush
- wet snow
- More than 3/4 inch or Dry snow
- Compacted snow
- Ice
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Pre-Takeoff Tactile check is required whenever the outside temperature is 5C or below and:
- there is visible moisture
- water is present on the wing
- temp/dew point difference is 3C or less
- atmospheric conditions have been condusive to frost formation
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APU shall not be used as a:
pneumatic source for anti-icing system
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Minimum altitude during Coupled CAT I ILS Approach
200 ft
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Minimum [autopilot] engagement height after takeoff
500 ft
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Decent below minimum decent altitude on a non-precision approach with auto pilot engaged is:
prohibited
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Single engine go-around go-around with autopilot engaged is:
prohibited
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Approach mode selection during a localizer capture is allowed only when:
aircraft is inbound
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When crossing the Outer Marker on glideslope, the altitude:
must be verified with the value on the published procedure
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For aircraft with a single operating glideslope receiver:
the approach may be flown using normal procedures no lower than LOC only MDA
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Yaw Damper operation is not authorized for:
- Takeoff to 500 ft AFL
- landing
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(APU) Operation altitude limit
37,000 ft
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(APU) Altitude for start
30,000 ft
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(APU) Continuous EGT
680 C
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(APU) Min Start Temp
-54C
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Minimum Battery temperature for APU start is:
-20 C
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The APU (continuous) EGT may be exceeded up to
717 C for five minutes maximum
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(APU) Cooling Period
- Between Three Consecutive Attempts - 1 minute OFF
- Between Two series of Three Consecutive Attempts - 30 min. OFF
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