Aircraft Limitations for the Citation X
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Max Operating Altitude | show 🗑
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show | 14,000 Ft
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Max OAT°C for Takeoff & Landing | show 🗑
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Min Temperature for Takeoff | show 🗑
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show | Enroute 1000 AGL, ILS 180 AGL, NonPrec 300 AGL
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A/P & Yaw Damp Restriction | show 🗑
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show | 800°C
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Max Oil Pressure | show 🗑
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Max ITT°C for Takeoff | show 🗑
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Min Oil Temp°C for start | show 🗑
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show | 10% Min, 25% Max, 888° ITT
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show | 6 starts per hour, 1 hour off
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show | 2 attempts 30 sec On / 30 min Off
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show | 28 Volts, 1000 Amps
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show | 0 to 200 Green (Ground or Inflight), 200 to 300 Yellow (Ground only), 300 Redline
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show | Must be operational
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Antiskid requirement | show 🗑
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Is Prist required | show 🗑
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show | Paved surfaces only
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Mmo | show 🗑
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Vmo | show 🗑
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show | 10 KTS
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Vfe-15° | show 🗑
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show | 180 KIAS
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show | 250 KIAS (Operating/Extend speed)
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show | 300 KIAS / .90 MACH
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Tire Limit Speed | show 🗑
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Min Speed in Sustained Icing | show 🗑
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Vmca | show 🗑
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show | 50% N¹ in Max Rev (Throttle limted to ∠28°)
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show | 65 KTS (70 KTS = 1-Eng, NoseSteering Inop, or Slippery)
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Are T&G's Authorized | show 🗑
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When must the TR's be Preflighted | show 🗑
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show | No
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show | 36,400 lbs (*750-173 and after)
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show | 36,100 lbs (*750-173 and after)
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show | 31,800 lbs
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Max Zero Fuel Weight | show 🗑
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Max Fuel Imbalance | show 🗑
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show | 700 lbs
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show | 10 KTS
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show | 21 KTS (Demonstrated)
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Maximum Altitude for APU Operation | show 🗑
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Emergency Fuel Imbalance | show 🗑
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show | 170 lbs
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show | 60 lbs
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show | Unusable fuel that cannot be used without exceeding aft CG limits
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Approved Kinds of Operation | show 🗑
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show | +10°C or below (RAT) in Visible Moisture
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show | On the Ground (except preflight) or Above Idle Power with Temp >20°C (SAT)
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Nosewheel Turning Limits | show 🗑
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show | 9.7 PSI (9.3 Normal / Relief Opens 9.5)
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Minimum Air Pressure Required for Start | show 🗑
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How many FADEC's must be Operational for Takeoff | show 🗑
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How many Air Data Computers (MADC) must be Operational for Takeoff | show 🗑
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Engine Make/Model | show 🗑
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show | 55 PSI
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show | -10 PSI
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show | Wing/Hopper = 4.81 gal, Center = 2.2 gal
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Max Wing Fuel Prior to Initiating Center-to Wing Transfer | show 🗑
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show | 2900 lbs (each wing)
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show | +4°C
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Max Fuel Temp°C for Takeoff | show 🗑
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show | Yes
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show | .82 Mach
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Hydraulic Pumps may NOT be Intentionally Unloaded Above What Altitude | show 🗑
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Aircraft Category | show 🗑
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Stage ____ Noise Certification | show 🗑
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show | ≤FL410= 0-400 Amps, >FL410= 0-300 Amps
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Unsuccessful Starts using GPU | show 🗑
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show | Takeoff, Landing, & Above FL450
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Max Alt with single PAC | show 🗑
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Max Turbulent Air Speed | show 🗑
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Max Crosswind with Slat Assymetry | show 🗑
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show | 22 Volts
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show | 18 Volts
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Min Voltage to Keep Batt Contactor Closed | show 🗑
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