Questions and Answers
What is the Max Ramp Weight for the Falcon 2000 Classic?
What is the Max Takeoff Weight for the Falcon 2000 Classic?
What is the Max Landing Weight for the Falcon 2000 Classic with SB F2000-186?
What is the Max Zero Fuel Weight for the Falcon 2000 Classic?
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Above what temperature should Engine & Wing A/I not be used?
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What is the Max Differential Pressure for the Falcon 2000 Classic?
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What is the Max Negative Differential Pressure for the Falcon 2000 Classic?
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What is the Max Voltage of the DC system?
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What is the Max Generator Output in flight?
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What is the Max Generator Output on the ground?
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At what temperature does the Amber WARM light for battery temperature illuminate?
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At what temperature does the Red HOT light for battery temperature illuminate?
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What is the Max APU Operating Altitude?
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What is the Max APU Starting Altitude?
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What is the Max N1 Speed?
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What are the EGT limits for starting?
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What is the Max APU Generator Output Transient?
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What are the stabilized max APU generator outputs at various altitudes?
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Inflight fuel tank temperature must be maintained at least how many degrees Celsius above the freezing point of the fuel being used?
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What is the Max Fuel Imbalance for flight?
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What is the Max Operating Altitude for the Falcon 2000 Classic?
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For a ground start, what is the maximum time from start to light-off?
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What is the maximum time from light-off to idle during a ground start?
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What are the times for airstart from light-off to idle for assisted and windmilling starts?
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What are the thrust ratings for takeoff and maximum continuous?
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What is the maximum time limit for takeoff thrust rating?
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What are the ITT limits for ground start and airstart?
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What is the max temp for restart and takeoff?
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What is the windmilling max temp for the Falcon 2000?
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What is the maximum baggage weight for the Falcon 2000 Classic?
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What is the payload capacity for the Falcon 2000 Classic?
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What is the M.A.C (Mean Aerodynamic Chord) of the Falcon 2000 Classic?
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What is the fuel quantity in the left tank plus half the center wing box?
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What is the total fuel quantity for the Falcon 2000 Classic?
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What is the windshield wiper operating speed?
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What is the direct vision window opening speed?
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What is the tire max operating speed?
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What is the Vmcg (Minimum Control Speed on the ground)?
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What is the Vmca (Minimum Control Speed in the air)?
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What is the Vmcl (Minimum Control Speed during landing approach)?
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What is the Vle (Max Landing Gear Extended Speed)?
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What is the Mle (Max Landing Gear Extended Speed)?
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What is the Vlo (Max Landing Gear Operating Speed)?
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What is the Mlo (Max Landing Gear Operating Speed)?
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What is the speed for Slats Extended + Flaps 10°?
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What is the speed for Slats Extended + Flaps 20°?
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What is the speed for Slats Extended + Flaps 40°?
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What is the Va (Max Maneuvering Speed)?
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What are the checklists for handling an engine fire?
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What are the steps for handling an APU fire?
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What are the criteria for a Main Wheel Well Overheat situation?
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What are the actions for handling an Electrical Fire or Smoke situation?
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What are the actions to remove smoke and unusual odors?
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What should you do in a Two-Engine-Out Condition Above 35,000 Feet?
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What actions should be taken in a Two-Engine-Out Condition Below 35,000 Feet?
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What should you do when both generators are inoperative?
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What is the procedure for loss of both hydraulic systems?
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What are the actions to take during rapid depressurization?
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What steps to take during emergency descent?
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What should you do in a forced landing scenario?
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What should be done during an emergency evacuation?
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What should you do in a ditching scenario?
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What actions to take during an unreliable airspeed situation?
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What should be done in case of a TCAS RA-Resolution Advisory?
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Study Notes
Weight Limitations
- Max Ramp Weight: 36,000 lbs
- Max Takeoff Weight: 35,800 lbs
- Max Landing Weight:
- 33,000 lbs
- 34,500 lbs with SB F2000-186
- Max Zero Fuel Weight: 28,660 lbs
Engine & Pressure Limits
- Engine and Wing Anti-Ice should not be used above 10°C
- Max Differential Pressure: 9.3 PSI
- Max Negative Differential Pressure: -0.3 PSI
Electrical System Limits
- Max Voltage of DC System: 29.5 Volts
- Max Generator Output in Flight: 400 AMPS
- Max Generator Output on Ground: 300 AMPS
Battery Temperature Limits
- Amber Warm illuminates at or above 120°F
- Red Hot illuminates at or above 160°F
Auxiliary Power Unit (APU) Limits
- Max APU Operating Altitude: 35,000 ft
- Max APU Starting Altitude: 35,000 ft
- Max APU Generator Output:
- Transient (one minute maximum): 350 AMPS
- Stabilized: 300 AMPS at 0-10,000 ft, 250 AMPS at 10,000-25,000 ft, 200 AMPS at 25,000-35,000 ft
Fuel and Temperature Requirements
- In-flight fuel tank temperature must be maintained at least 3°C above freezing point of the fuel
- Max Fuel Imbalance for Flight: 2,200 lbs
- Total Fuel Quantity: 12,155 lbs
Maximum Operating Altitude
- Max Operating Altitude: 47,000 ft
Engine Start Procedures
- Ground Start (from Start to Light-off): 10 seconds max after 22% N2
- Ground Start (from Light-off to Idle): 60 seconds max
- Airstart (from Light-off to Idle): 90 seconds assisted, 180 seconds windmilling
Thrust Ratings
- Takeoff Thrust: 5,888 lbs
- Max Continuous Thrust: 5 minutes time-limited
- Max ITT for ground start: 815°C
- Airstart ITT: 890°C
- Max Restart ITT: 150°C
- Max Takeoff (APR) ITT: 890°C for 5 minutes max
- Normal Takeoff ITT: 864°C
- Max Continuous ITT: 861°C
- Windmilling Max Temp: 970°C for 10 seconds max, 1,000°C for 2 seconds max
Payload Capacities
- Max Baggage: 1,600 lbs
- Payload: 5,990 lbs
- Mean Aerodynamic Chord (MAC): 113.69 inches
- Fuel Quantity for left + half center wing box: 6,070 lbs
Speed Limitations
- Windshield Wiper Operating Speed: 215 KIAS
- Direct Vision Window Opening Speed: 215 KIAS
- Tire Max Operating Speed: 195 KTS (ground speed)
- Vmcg (Minimum Control Speed on Ground): 98 KIAS
- Vmca (Minimum Control Speed in Air): 90 KIAS
- Vmcl (Minimum Control Speed during Landing Approach): 90 KIAS
- Vle (Max Landing Gear Extended Speed): 245 KIAS
- Vlo (Max Landing Gear Operating Speed): 190 KIAS
Control and Configuration Speeds
- Max Maneuvering Speed (Va): 198 KIAS
- Slats Extended + Flaps 10°: 200 KIAS
- Slats Extended + Flaps 20°: 160 KIAS
- Slats Extended + Flaps 40°: 160 KIAS
Emergency Procedures
- Engine Fire: Immediate steps include moving Power Lever to IDLE, turning off fuel switches, and activating fire extinguishers based on warning persistence.
- APU Fire: APU fuel shut-off switch must be actuated and airspeed maintained below 250 KIAS.
- Special conditions like main wheel well overheat, electrical fire, smoke and unusual odors all require crew oxygen masks to be donned.
Critical Conditions
- Two Engine-Out Condition Below 35,000 feet: Use best glide speed and ensure APU is started if not inoperative.
- Loss of Both Hydraulic Systems: Closures and disengagements as necessary for safety.
- Rapid Depressurization: Immediate use of crew oxygen masks and initiating emergency descent.
Ditching and Evacuation
- Ditching: Similar protocols to forced landing; emphasize on instructing passengers and maintaining safety measures.
- Emergency Evacuation: Set parking brake, communicate distress to ATC, and ensure passenger instructions are clear.
Unreliable Airspeed Management
- Disconnect autopilot, disengage yaw damper, maintain smooth control inputs, and stabilize pitch between 0° and 3° nose up with full engine power.
TCAS Resolution Advisory
- Promptly perform evasive maneuvers while maintaining situational awareness and following the appropriate procedures for stall, GPWS, or windshear alerts.
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Test your knowledge of the Falcon 2000 Classic's weight limitations and operational guidelines with these flashcards. Each card provides key definitions and figures essential for understanding the aircraft's performance parameters. Ideal for pilots and aviation enthusiasts alike.