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Max TO/LDG Alt
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CE560XL Lims
| Question | Answer |
|---|---|
| Max Oper Alt | 45,000 |
| Max TO/LDG Alt | 14,000 |
| Max Temp TO/LDG | ISA +39 |
| Min Temp TO/LDG | -54 |
| Max Ramp Wght | 20,400 |
| MTOW | 20,200 |
| Max Ldg Weight | 18,700 |
| Max Zero Fuel Weight | 15,100 |
| Min Flight Weight (gust loading) | 12,400 |
| Max Fuel Imbalance (Normal) | 400 |
| Max Fuel Imbalance (Emergency) | 800 |
| Tailcone Baggage Compartment | 700 |
| Mmo (above 26,515) | .75Mach (indicated) |
| Vmo (below 8,000) | 260 KIAS |
| Vmo (8000 to 26,515) | 305 |
| Auotopilot Operation | 305KIAS or .75Mach indicated |
| Va (varies w/wght and alt) | Refer to AFM Fig. 2-8 |
| Vfe (flaps 7 or 15) | 200 KIAS |
| Vfe (flaps 35, fully extend) | 175 KIAS |
| Vle | 250 KIAS |
| Vlo retracting/extending | ret=200kias ext=250kias |
| Vsb | No Limit |
| Turbulent Air Penetration | 180 kias |
| Max Tire Grd Spd | 165 kias |
| Min Speed in Icing (except app & ldg) | 160 kias |
| Vmcg | 81 kias |
| Vmca | 90 kias |
| Vortex Generators | up to 3vg may be missing provided alt=/<41k52 installed, 26/wing |
| Boundary Layer Energizers | All must be present 22 installed 11/wing |
| Tire Pressure | Main: Loaded 218+2or-5 Unloaded 210+2or-5Nose: Loaded 135 +/-5 Unloaded 130+/-5 |
| Engines | Pratt Whitney PW545B Turbofan |
| Max ITT (starting only) | 740C |
| Min Oil Temp (ground eng start) | -40C |
| Oil Pressure | 160 (250Psi for 400 seconds) |
| N1 indication by | 25% N2 |
| Takeoff pwr limited to | 5 min, 10 min for single engine |
| L and R ignition switches | ON prior to reducing pwr to less than 70%N2(Acft Config code AC only) |
| Max Oil Consumption | 1qt per 8 hour period |
| Dispatch with engine display in revisionary mode is prohibited | true |
| Aviation Gas | Not Approved |
| Prist | Approved but not required |
| Boost Pumps | ON, for FUEL LOW LEVEL lights or 400lbs or less indic fuel |
| Gen Assist Start Equals | 1/3 battery start |
| Battery Limit | 3 Eng starts per hour |
| Starter Limitation | 3 in 30 min with 90 sec rests |
| GPU amperage set | 28 volts, 800 to 1000 max |
| Electrical Load | 300 amps in flt, 200 gnd w/250 transient up to 4 min |
| Primus 1000 CDS | must ne verified to be operational by a satisfactory preflight check |
| AOA System | Operable and preflight check prior to dispatch |
| PFD Reversionary Modes | P and CP PFDs must be installed and operational in the normal mode for TO |
| Reversion of Both PFDs to the MFD | Prohibited |
| Avionics Ground Operation | Time Limits refer to AFM pg2-9 |
| Standby Flight Display | sat preflight test, must be functioning prior to TO, only one source req’d for TO |
| Autopilot | Pilot in seat w/SB fastened AP prohibited if comparison mon illumsMin Hgt: Enr=1000', Non Prec=300', cat I=180',catII=80', AP/YD=OFF for TO/LDG |
| Portable Elect Devices | All PED's, laptop,handheld, cell phones, wireless devices, radios, games must be off and stowed during term ops, ie taxi, climb, app and ldg phase. Includes items pwrd by cabin electrical inverters |
| APU Prohibited | Until Satisfactory Test has been accomplishedWhile applying deiceTR deployment for more than 30 secIf unattendedAbove FL300 |
| APU Start Attempts Prohibited | When APU FAIL light illumAfter dual gen failureAfter shutdown until 30 sec after RPM=0%Above FL200 |
| APU Starter Limits | Same as main engine start lims9 APU start cycles/hour- Main Batt(APU batt starts =1/3 of main eng start |
| Rain Ice Airframe Contamination | TO from wet rwy using TR in Perf credit lim to 75' wide rwyGrd Op of pitot/static heat to 2 min |
| Tail Deice Syst | Min Temp for use arspd<150KIAS=-40CMin Temp for use arspd>150KIAS=-35C |
| Tail Deice Syst CAUTION | Do Not Op TDB in flwing conditions, boots may crack: Arspd at/above 150KIAS and RAT-35C or colderArspd<150KIAS at RAT -40C or colder |
| TO Proh with flwng Contamination 1 Frost | Frost Adhering to:Wing Leading EdgeUpper wing surfaceWindshield |
| TO Proh with flwng Contamination 2 Ice, snow, slush | Wng ldg edge and Upper wng surf, Flt Ctrl Sfcs inc all hinge gaps, Hor Stab, Vert Stab, Eng inlet, Top Eng Pylon, Top Fuselage, Wndshld, All Static Ports, Ang Atk Vanes, Upper sfc of nose fwd of wdshd |
| TO Proh with flwng Contamination 3 Vis/Tactile check | V/T check wle and upper ws must be perf to ensure wng is free of frost, ice, snow, or slush when oat<10C or if it cannot be det wng fuel temp is>0C and vis moist, water on upwng, dew pt oat spread =<3C, atmos conducive to frost |
Created by:
dssully310