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58 Cards in this Set
- Front
- Back
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Max Ramp Weight
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65,400 lbs
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Max T.O. Weight
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65,200 lbs
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Max Landing Weight
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62,000 lbs
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Max Zero Fuel Weight
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58,000 lbs
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Min Structural Design Weight
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31,753 lbs
CFM VOL 1 Ch 2 |
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Max AFT Baggage Load
C2 Limitation |
2,560 lbs total weight with 1,000 lbs on C2
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Max FWD Baggage Load
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910 lbs
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Max/Min Load Factors with Flaps Up
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Flaps Retracted: +2.5g to -1.0g
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Max/Min Load Factors with Flaps Down
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Flaps Extended: +2.0g to 0.0g
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Max Altitude We May Accept From ATC
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25,000 ft. ASL
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Max T/O and Landing Alt.
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10,000 Ft. ASL
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Max/Min Rwy Slopes
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+/- 2%
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May We Takeoff with a Rwy Slope of 2.5%?
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No, +/- 2% slope is the limitation
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Max Crosswind for T/O and Landing
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32 Knots, Hard,Dry or Wet Rwy
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Max Crosswind for Landing with a Wet Rwy
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32 Knots
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Max/Min Operating Temp Limits
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Min= -54c
Max= +50c or ISA +35c whichever is lower |
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Max Operating Speeds
0 - 8,000 ft |
245 KIAS
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Max Operating Speeds
10,000 ft |
282 KIAS
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Max Operating Speeds
18,000 ft |
286 KIAS
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Max Operating Speeds
20,000 ft |
275 KIAS
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Max Operating Speeds
25,000 ft |
248 KIAS
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Q 400 Maneuvering Speed
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VA: 204 KIAS
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Q 400 Rough Air Penetration Speed
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VRA: 210 KIAS
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Max Speed We May Operate the Landing Gear Handle
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VLO: 200KIAS
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If Required to Fly With the Landing Gear Down, What Would be Our Max Speed We May Fly at and Stay Within Limitations?
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VLE: 215 KIAS
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Max IAS for Alternate Gear Extension? Why?
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VALT gear: 185 KIAS, Due to Main and Nose Hydraulic Gear Doors Remaining Open.
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VFE @ Flaps 5
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200 KIAS
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VFE @ Flaps 10
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181 KIAS
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VFE @ Flaps 15
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172 KIAS
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VFE @ Flaps 35
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158 KIAS
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Max Alt for Air-Start
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20,000 ft
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Max ITT for Start
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920 C
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Once an Engine has Stabilized After a Start, What is the Min NH That the Display Should Indicate?
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64.2 %
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How Long May MTOP be Utilized Per Engine Operating Limitations?
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5 Minutes
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Min Oil Temp for Inlet Ice Protection on the Ground
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55 C
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Min Oil Temp for Inlet Ice Protection Airborne
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65 C Within 3 Minutes of Setting Takeoff Power
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Starter Cranking Limits
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1st start, 70 Secs on, 2 Mins off
2nd Start, 70 Secs on, 2 Mins off 3rd Start, 70 Secs on, 30 Mins off |
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After an Aborted Engine Start Sequence, How Long Must a Crew Wait Until Attempting Another Start? (1st Attempt)
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2 Mins
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Max Usable Fuel Load
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11,724 lbs
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Max Lateral Fuel Imbalance
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600 lbs
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When Must the Tank Aux Pumps be on During Normal Operations?
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Tank 1 and Tank 2 Auxiliary Pumps must be on for T.O. and Landing.
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Fuel Temp Operating Range
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0 - 71 C Normal Operations
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Max Battery Load for T/O
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0.1 on the Stby, Aux and Main Batts
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Min Battery Temp for T/O
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-20 C
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May we Extend the Gear at FL250 to aid an Emergency Descent?
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No, 15,000 ft is the Max Alt. for Extending the Landing Gear
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Max Tire Speed
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182 Knots Ground Speed
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Max Cabin Differential Pressure Airborne
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5.95 psi
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Max cabin Differential Pressure on the Ground
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0.5 psi
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Normal Cabin Differential Pressure Airborne
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5.46 psi +/- 0.1 psi
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Max Cabin Alt.
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8,000 ft
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When May We NOT Conduct a T/O With Bleeds On?
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Tailwind component exceeds 10 kts,
Reported OAT Exceeds 39 C (100 F) When Performance Data Dictates we Must Conduct a bleed off T/O |
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When May We NOT Conduct a Landing with Bleeds On?
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Tailwind Component Exceeds 10 Kts,
Reported OAT Exceeds 39 C (100 F) When Performance Data Dictates We Must Conduct a Bleed Off Landing |
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AutoPilot Coupled Approach Limitations
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AFCS is Approved for Autopilot Approaches to CAT 1 Limits Only
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Autopilot Coupled Approaches are approved for
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Flap 0 (Min Alt: 1000 AGL)
Flap 5, 10, 15, 35 |
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Autopilot Minimum Engagement Height
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After T/O or Go Around the Minimum Height for Autopilot Engagement is 1,000 ft AGL
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Is Autopilot Use in Severe Turbulence and/or Severe Icing Permitted?
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Autopilot must be disengaged in Severe Icing and turbulence
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Reasons Why Flight Must be Conducted no Further Than 1 Hour Flying Time From a Suitable Landing Airport for Landing
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Due to the One Hour Limitation on the Integrated Standby Instrument and the Fire Protection Requirements of the Forward and Aft Baggage Compartment
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Is the Q400 Certified for Ditching?
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Yes
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