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99 Cards in this Set
- Front
- Back
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Approved Operations
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Day, night, VFR, IFR, icing, and ditching when required equipment is installed
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Max Ramp/taxi weight
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48,300 lb (21,909 kg)
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Max Takeoff weight
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48,200 lb (21,863 kg)
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Max Landing weight
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38,000 lb (17,237 kg)
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Max Maximum zero fuel weight
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32,000 lb (14,515 kg)
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Minimum flight weight
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26,000 lb (11,794 kg)
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Minimum operating weight
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22,150 lb (10,047 kg)
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Airplane center of gravity...
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... must be maintained within specified limits at all times
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Maximum pressure altitude for takeoff and landing
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10,000 ft (except if 5367 and subsequent or SB 604-21-004, then 14,000 ft)
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Maximum operating altitude
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41,000 ft
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Maximum temperature for takeoff and landing
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ISA +35°C
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Minimum temperature for takeoff
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-40°C
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Safety harness must be worn by at least one pilot...
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... above 25,000 ft
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Maximum runway slope for takeoff/landing
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±2%
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Maximum takeoff/landing tailwind component
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10 kt
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Minimum flight crew
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1 pilot and 1 copilot
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Maximum occupants
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22 with no more than 19 passengers or maximum passenger seating
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Cold weather takeoff is prohibited...
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... 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)
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Warning: Even small amounts of frost, ice, snow, or slush on the wing leading edges and forward upper wing surface may...
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... adversely change the stall speeds, stall characteristics and the protection provided by the stall protection system, which may result in loss of control on takeoff
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In addition to a visual check...
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... a tactile check of the wing leading edge, wing forward upper surface, and rear upper surface is required during the external walk around inspection to determine that the wing is free from frost, ice, snow, or slush when one of the following is present: Outside air temperature (OAT) is ≤5°C (41°F), Wing fuel temperature is ≤0°C (32°F), Atmospheric conditions have been conducive to frost formation
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Cowl Anti-ice Ground Operations...
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...Must be on when OAT is ≤10°C (50°F) and visible moisture in any form is present including fog with visibility of ≤1 mile. Must also be on when OAT is ≤10°C (50°F) and ground surfaces are contaminated with snow, ice, standing water, or slush
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Wing Anti-ice System Ground Operations...
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... Icing conditions exist on the ground when the OAT is ≤5°C (41°F) and: - Visible moisture in any form (such as clouds, fog, or mist) is present below 400 ft AGL, or Runway is wet or contaminated, or In the presence of any precipitation (i.e., rain, snow, sleet, or ice crystals)
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Wing anti-ice system (ground operation) must be selected ON...
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... for final taxi prior to takeoff if the OAT is ≤5°C (41°F), unless Type II, III, or IV anti-icing fluids have been applied. Single engine taxi operations are prohibited in these conditions
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L(R) WING A/ICE caution messages may be posted or L(R) HEAT lights may go out during taxi, but...
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... caution messages must be verified off and WING A/ICE ON or WING/COWL A/ICE ON advisory message and L(R) HEAT lights must be verified on prior to takeoff. If wing anti-ice is not required for takeoff, it should be selected OFF just prior to takeoff
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To prevent wing contamination from reverse jet blast...
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... operating thrust reversers during taxi operations on wet and contaminated surfaces should be avoided
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Wing anti-ice system must be selected and confirmed ON for takeoff...
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... when ground icing conditions exist
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If wing anti-ice is selected ON for takeoff...
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... the cowl anti-ice must also be selected ON
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Engine Type
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General Electric CF34-3B
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EICAS limit indications must be used...
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... to determine compliance with maximum/minimum limits and caution ranges
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If above 40,000 feet...
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... one air-conditioning unit or cowl anti-icing must be selected on for each engine
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Before the first flight of the day, if the aircraft is cold-soaked below -30 deg C (-22 deg F) for more than 8 hours...
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Motor engines 60 seconds; check fan rotation before engine start is initiated
Actuate thrust reversers until deploy and stow cycles are < 5 seconds |
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Minimum starting oil temperature
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-40 deg C (-40 deg F)
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Maximum continuous oil temperature
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155 deg C (311 deg F)
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Maximum permissible oil temperature
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163 deg C (325 deg F)
(15 minutes maximum) |
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Minimum idle oil pressure
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25 psi
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Minimum Takeoff oil pressure
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45 psi
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Maximum continuous oil pressure
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110 psi
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Maximum transient oil pressure after cold start (10 minutes maximum; engine must remain at idle until pressure returns to normal range)
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115 psi
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Maximum oil consumption
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6.4 oz/0.2 qt/0.05 gal per hour
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Engine oil must be checked within...
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... 15 minutes to 2 hours after shutdown; engine must be motored if period exceeded
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Maximum oil replenishment without dry motering
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2 qt
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Continuous Ignition must be on for
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Takeoff and landing on contaminated runway
Takeoff with high crosswind component Flight in moderate or greater rain and/or turbulence Flight in vicinity of thunderstorms |
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Maximum N2 for starter use or engagement
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55%
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Starter operation is limited to...
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... three consecutive start cycles with 5 minutes cooling between additional cycles
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Maximum ITT for ground starts
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120 deg C
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Maximum ITT for air starts
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90 deg C
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Dry motoring permitted for ground and air starts?
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Yes
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Dry motoring limit, first cycle
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Maximum 90 seconds, then 5 minutes off
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Dry motoring limit, subsequent cycles
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Maximum 30 seconds, then 5 minutes off
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Maximum fuel imbalance for taxi, takeoff and landing
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400 lb
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Maximum fuel imbalance in flight
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800 lb
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Maximum fuel quantity each main tank
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4860 lb
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Maximum fuel quantity auxiliary tank
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7168 lb
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Maximum fuel quanity tail tank
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3112 lb
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Maximum fuel quantity total
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20,000 lb
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If gravity fueling, reduce maximum fuel quantity by...
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7%
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Takeoff with up to 500 lb in auxiliary tank permitted if at least...
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... 1500 lb in each wing and no fuel in tail tank
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For takeoff weights up to 42,200 lb with more than 500 lb in the auxiliary tank, each wing tank must have at least...
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1500 lb
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For takeoff weights above 42,200 lb with more than 500 lb in the auxiliary tank...
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... consult the AFM limitations section
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Minimum fuel quantity for go around
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500 lb each wing with maximum 10 deg noseup attitude
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Takeoff prohibited with fuel temperature below
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5 deg C
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Bulk fuel temperature must be at least how many degrees above fuel freezing point for takeoff, and remain above fuel freezing point in flight
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10 deg C
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Approved fuels
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Jet A, Jet A1, Jet B, JP-4, JP-5, JP-8. Mixing of fuel grades is permitted
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What position must fuel transfer valves be in for takeoff
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Closed
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In normal operations, the tail tank transfer system must not be used for center of gravity control; it must remain in what mode?
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Automatic
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During manual mode operations: Auxiliary tank quantity must be at least xxx times the tail tank quantity if tail tank quantity >= 1200 lb, and at least yyy times the tail tank quantity if tail tank quantity is < 1200 lb
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2.75, 2.2
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Maximum speed in RVSM airspace
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0.83 Mach
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Vfe 20
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231 KIAS
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Vfe 30
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197 KIAS
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Vfe 45
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189 KIAS
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Vlo
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197 KIAS/0.6 Mach
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Vle
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250 KIAS/0.7 Mach
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Tire limit speed
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182 knots ground speed
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Maximum Gear Extended Altitude
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20,000 ft
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Maximum speed with ADG deployed (5301 - 5407)
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250 KIAS normally
330 KIAS for 12 minutes 330 KIAS to 348 for 4 minutes 215 KIAS for flight test or pilot training |
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Turbulence penetration speed
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280 KIAS or 0.75 Mach, whichever is lower
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Load factors flaps up
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-1.0 to +2.5 g
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Load factors flaps down
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0.0 to +2.0 g
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Maximum relief differential pressure
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9.2 psi
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Maximum negative differential pressure
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-0.5 psi
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Maximum differential during taxi, takeoff and landing
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0.2 psi
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Airplane must be completely depressurized...
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... prior to opening any doors
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Minimum AP engage altitude after takeoff
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320 ft AGL
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Minumum AP use height for visual and non-precision approaches
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320 ft AGL
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Minimum AP use height for precision (ILS) approaches with glidepath angle of 3.5 deg or less
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80 ft AGL
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If post SB 604-32-012, the ADC source coupled to the active autopilot must be the same as...
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... that coupled to the ATC transponder during flight in RVSM airspace
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During takeoff and landing with the cowl and/or wing anti-ice systems on, the 10th stage bleed valves must be...
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Closed
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If above 40,000 feet, one air-conditioning pack or cowl anti-icing system for each engine must be...
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On
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Maximum APU generator load
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30 kVA
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APU (100E) generator use not permitted in flight unless...
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... both IDGs are offline
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Maximum IDG load below 35,500 ft
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30 kVA
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Maximum IDG load above 35,000 ft
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25 kVA
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Maximum load on each TRU
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100 amp
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Enroute use of flaps is...
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... prohibited
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Flight with flaps extended above 15,500 ft is...
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... prohibited
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Flight below 300 AGL with flight spoilers extended is...
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... prohibited
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Minimum speed for flight spoiler extension is...
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... Vref + 10 KIAS
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For all phases of flight, both stick pusher switches must be...
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... On
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Stall protection test indicator must only be used for...
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... system testing
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