Help
Options
Didn't know it?
click below
click below
Knew it?
click below
click below
Don't Know
Remaining cards (0)
Know
retry
shuffle
restart
0:00
Embed Code - If you would like this activity on your web page, copy the script below and paste it into your web page.
Normal Size Small Size show me how
Normal Size Small Size show me how
CE750 Limitations
Aircraft Limitations for the Citation X
| Question | Answer |
|---|---|
| Max Operating Altitude | FL510 |
| Max Altitude for Takeoff & Landing | 14,000 Ft |
| Max OAT°C for Takeoff & Landing | ISA +39 C |
| Min Temperature for Takeoff | -54 C |
| Lowest Alt with A/P Engaged | Enroute 1000 AGL, ILS 180 AGL, NonPrec 300 AGL |
| A/P & Yaw Damp Restriction | Must be off for all Takeoff & Landings |
| Max ITT°C for ground start | 800°C |
| Max Oil Pressure | 95 PSI (Max 155 PSIG for 2 minutes) |
| Max ITT°C for Takeoff | 907°C for 5 minutes, then 857°C Continuously |
| Min Oil Temp°C for start | -40 C |
| Airstart N2 & ITT° Limits | 10% Min, 25% Max, 888° ITT |
| APU Starter Cycle Limitation | 6 starts per hour, 1 hour off |
| Start limits using Battery | 2 attempts 30 sec On / 30 min Off |
| GPU Output Requirements | 28 Volts, 1000 Amps |
| APU Generator limits | 0 to 200 Green (Ground or Inflight), 200 to 300 Yellow (Ground only), 300 Redline |
| Requirement for elevator trim | Must be operational |
| Antiskid requirement | Must be Operational for Takeoff |
| Is Prist required | No |
| Approved Surfaces for Takeoff & Landing | Paved surfaces only |
| Mmo | Above 30,650' is .92 MACH (.82 MACH Trim Off) |
| Vmo | < 8000 ft = 270 KIAS, > 8000 ft = 350 KIAS |
| Max Crosswind using Manual Flight Controls | 10 KTS |
| Vfe-15° | 210 KIAS |
| Vfe-35° | 180 KIAS |
| Vlo & Vle | 250 KIAS (Operating/Extend speed) |
| Turbulent Air Penetration Speed | 300 KIAS / .90 MACH |
| Tire Limit Speed | 182 KTS / 210 MPH |
| Min Speed in Sustained Icing | 200 KIAS (Slats/Flaps Up except during App/Ldg) |
| Vmca | 90 KIAS |
| Max N1 Using TR's | 50% N¹ in Max Rev (Throttle limted to ∠28°) |
| Min TR Speed During Rollout | 65 KTS (70 KTS = 1-Eng, NoseSteering Inop, or Slippery) |
| Are T&G's Authorized | No |
| When must the TR's be Preflighted | First flight, Required for Ldg Conditions, or TR Mx |
| Is TR Backing Approved | No |
| Max Ramp Weight | 36,400 lbs (*750-173 and after) |
| Max Takeoff Weight | 36,100 lbs (*750-173 and after) |
| Max Landing Weight | 31,800 lbs |
| Max Zero Fuel Weight | 24,400 lbs |
| Max Fuel Imbalance | 400 lbs |
| Max Tailcone Baggage Weight | 700 lbs |
| Max Tailwind Component | 10 KTS |
| Max Crosswind Component | 21 KTS (Demonstrated) |
| Maximum Altitude for APU Operation | FL310 or above |
| Emergency Fuel Imbalance | 800 lbs (limited by wingtip clearance) |
| Max Weight in Ski Tube | 170 lbs |
| Max Floor Loading in Aft Closet | 60 lbs |
| Ballast Fuel | Unusable fuel that cannot be used without exceeding aft CG limits |
| 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 |
| Conditions Anti-Icing is Required | +10°C or below (RAT) in Visible Moisture |
| 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) |
| Nosewheel Turning Limits | Rudder pedals = 12°, Tiller = 80°, Rudder+Tiller = 90° |
| Max Cabin Differential Pressure | 9.7 PSI (9.3 Normal / Relief Opens 9.5) |
| Minimum Air Pressure Required for Start | APU = 25 PSI (EICAS), GPU = 30 PSI (EICAS) |
| How many FADEC's must be Operational for Takeoff | All 4 Required |
| How many Air Data Computers (MADC) must be Operational for Takeoff | Both Required |
| Engine Make/Model | Allison AE-3007C Turbofan |
| Max Fuel Pressure for Single-Point Refueling | 55 PSI |
| Max Defuel Pressure | -10 PSI |
| Unusuable Fuel Quantity | Wing/Hopper = 4.81 gal, Center = 2.2 gal |
| Max Wing Fuel Prior to Initiating Center-to Wing Transfer | 3100 lbs (per side) |
| Min Fuel Quantity for Simultaneous Crossfeed and Center-to-Wing Transfer | 2900 lbs (each wing) |
| Min Fuel Temp°C for Takeoff | +4°C |
| Max Fuel Temp°C for Takeoff | +98.9°C |
| Are Both Rudder Limiters Required for Takeoff | Yes |
| MACH Trim must be Operational above what Speed | .82 Mach |
| Hydraulic Pumps may NOT be Intentionally Unloaded Above What Altitude | 15,000 MSL (Exception- Ab/Emer Procedures) |
| Aircraft Category | Transport |
| Stage ____ Noise Certification | Stage 3 (Reference AFM) |
| Aircraft Generator Output Limits | ≤FL410= 0-400 Amps, >FL410= 0-300 Amps |
| Unsuccessful Starts using GPU | 2 Attempts 15 sec On / 20 min Off (4 per hour max) |
| Operating Limits with PAC's in High | Takeoff, Landing, & Above FL450 |
| Max Alt with single PAC | FL410 |
| Max Turbulent Air Speed | 300 KIAS / .90 MACH |
| Max Crosswind with Slat Assymetry | 10 KTS |
| Min Battery Volts for APU Start | 22 Volts |
| Min Voltage to Close Batt Relay | 18 Volts |
| Min Voltage to Keep Batt Contactor Closed | 11-12 Volts |
Created by:
tailwheel
Popular Aviation sets