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Aircraft Limitations for the Citation X

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Question
Answer
Max Operating Altitude   FL510  
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Max Altitude for Takeoff & Landing   14,000 Ft  
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Max OAT°C for Takeoff & Landing   ISA +39 C  
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Min Temperature for Takeoff   -54 C  
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Lowest Alt with A/P Engaged   Enroute 1000 AGL, ILS 180 AGL, NonPrec 300 AGL  
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A/P & Yaw Damp Restriction   Must be off for all Takeoff & Landings  
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Max ITT°C for ground start   800°C  
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Max Oil Pressure   95 PSI (Max 155 PSIG for 2 minutes)  
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Max ITT°C for Takeoff   907°C for 5 minutes, then 857°C Continuously  
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Min Oil Temp°C for start   -40 C  
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Airstart N2 & ITT° Limits   10% Min, 25% Max, 888° ITT  
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APU Starter Cycle Limitation   6 starts per hour, 1 hour off  
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Start limits using Battery   2 attempts 30 sec On / 30 min Off  
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GPU Output Requirements   28 Volts, 1000 Amps  
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APU Generator limits   0 to 200 Green (Ground or Inflight), 200 to 300 Yellow (Ground only), 300 Redline  
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Requirement for elevator trim   Must be operational  
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Antiskid requirement   Must be Operational for Takeoff  
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Is Prist required   No  
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Approved Surfaces for Takeoff & Landing   Paved surfaces only  
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Mmo   Above 30,650' is .92 MACH (.82 MACH Trim Off)  
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Vmo   < 8000 ft = 270 KIAS, > 8000 ft = 350 KIAS  
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Max Crosswind using Manual Flight Controls   10 KTS  
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Vfe-15°   210 KIAS  
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Vfe-35°   180 KIAS  
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Vlo & Vle   250 KIAS (Operating/Extend speed)  
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Turbulent Air Penetration Speed   300 KIAS / .90 MACH  
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Tire Limit Speed   182 KTS / 210 MPH  
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Min Speed in Sustained Icing   200 KIAS (Slats/Flaps Up except during App/Ldg)  
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Vmca   90 KIAS  
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Max N1 Using TR's   50% N¹ in Max Rev (Throttle limted to ∠28°)  
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Min TR Speed During Rollout   65 KTS (70 KTS = 1-Eng, NoseSteering Inop, or Slippery)  
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Are T&G's Authorized   No  
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When must the TR's be Preflighted   First flight, Required for Ldg Conditions, or TR Mx  
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Is TR Backing Approved   No  
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Max Ramp Weight   36,400 lbs (*750-173 and after)  
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Max Takeoff Weight   36,100 lbs (*750-173 and after)  
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Max Landing Weight   31,800 lbs  
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Max Zero Fuel Weight   24,400 lbs  
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Max Fuel Imbalance   400 lbs  
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Max Tailcone Baggage Weight   700 lbs  
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Max Tailwind Component   10 KTS  
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Max Crosswind Component   21 KTS (Demonstrated)  
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Maximum Altitude for APU Operation   FL310 or above  
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Emergency Fuel Imbalance   800 lbs (limited by wingtip clearance)  
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Max Weight in Ski Tube   170 lbs  
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Max Floor Loading in Aft Closet   60 lbs  
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Ballast Fuel   Unusable fuel that cannot be used without exceeding aft CG limits  
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Approved Kinds of Operation   Day/Night (VFR & IFR), Icing, Overwater, B-RNAV, RVSM Airspace, RNP-10 (Enroute), RNP-3 (Approach), NAT-MNPS Airspace, Cat II  
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Conditions Anti-Icing is Required   +10°C or below (RAT) in Visible Moisture  
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Conditions Wing Anti-Icing System (Bleed Air) can NOT be Used   On the Ground (except preflight) or Above Idle Power with Temp >20°C (SAT)  
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Nosewheel Turning Limits   Rudder pedals = 12°, Tiller = 80°, Rudder+Tiller = 90°  
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Max Cabin Differential Pressure   9.7 PSI (9.3 Normal / Relief Opens 9.5)  
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Minimum Air Pressure Required for Start   APU = 25 PSI (EICAS), GPU = 30 PSI (EICAS)  
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How many FADEC's must be Operational for Takeoff   All 4 Required  
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How many Air Data Computers (MADC) must be Operational for Takeoff   Both Required  
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Engine Make/Model   Allison AE-3007C Turbofan  
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Max Fuel Pressure for Single-Point Refueling   55 PSI  
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Max Defuel Pressure   -10 PSI  
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Unusuable Fuel Quantity   Wing/Hopper = 4.81 gal, Center = 2.2 gal  
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Max Wing Fuel Prior to Initiating Center-to Wing Transfer   3100 lbs (per side)  
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Min Fuel Quantity for Simultaneous Crossfeed and Center-to-Wing Transfer   2900 lbs (each wing)  
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Min Fuel Temp°C for Takeoff   +4°C  
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Max Fuel Temp°C for Takeoff   +98.9°C  
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Are Both Rudder Limiters Required for Takeoff   Yes  
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MACH Trim must be Operational above what Speed   .82 Mach  
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Hydraulic Pumps may NOT be Intentionally Unloaded Above What Altitude   15,000 MSL (Exception- Ab/Emer Procedures)  
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Aircraft Category   Transport  
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Stage ____ Noise Certification   Stage 3 (Reference AFM)  
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Aircraft Generator Output Limits   ≤FL410= 0-400 Amps, >FL410= 0-300 Amps  
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Unsuccessful Starts using GPU   2 Attempts 15 sec On / 20 min Off (4 per hour max)  
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Operating Limits with PAC's in High   Takeoff, Landing, & Above FL450  
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Max Alt with single PAC   FL410  
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Max Turbulent Air Speed   300 KIAS / .90 MACH  
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Max Crosswind with Slat Assymetry   10 KTS  
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Min Battery Volts for APU Start   22 Volts  
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Min Voltage to Close Batt Relay   18 Volts  
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Min Voltage to Keep Batt Contactor Closed   11-12 Volts  
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