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CE650 Limitations
Citation 650/III Limitations
| Question | Answer |
|---|---|
| Vmo (Below 8,000 feet) | 305 KIAS |
| Mmo (Above 36,524 feet)(Indicated) | 0.851 Mach |
| Landing Lights Extended | 250 KIAS |
| Landing Gear Operational (Vlo) | 210 KIAS |
| Flaps (7 or 20)(Partial Vfe) | 210 KIAS |
| Flaps Full (Vfe) | 170 KIAS |
| Maximum Tire Ground Speed | 165 KIAS |
| Speedbrake Extension (Max/Min) | No Limit / Vref + 15 KIAS |
| Spoiler Extension (Max/Min) | (Vmo/Mmo) / 150 KIAS |
| Turbulent Air Penetration | 200 KIAS / 0.75 Mach (whichever is less) |
| Min Speed in Sustained Icing (Except T.O., Appr & Landing) | 180 KIAS |
| Ramp Weight | 22,200 lbs. |
| Takeoff Weight | 22,000 lbs. |
| Landing Weight | 20,000 lbs. |
| Zero Wing Fuel Weight | 16,300 lbs. |
| Maximum Calibrated Operating Altitude | 51,000 feet |
| Maximum Takeoff/Landing Altitude | 14,000 feet |
| Ambient Temperature for Engine Start (Max/Min) | ISA +37C / -54C |
| Maximum Tail Wind Component | 10 Knots |
| Maximum Crosswind with Thrust Reversers | 25 Knots (limiting) |
| Maximum Crosswind with Roll Spoilers INOP. | 10 Knots (limiting) |
| Max Crosswind with Aileron/Spoiler Disc. Handle Pulled | 10 Knots (limitiing) |
| Battery Start Limitation | 3 Starts per Hour |
| Starter Limitation | 3 starts in 30 min; with a 60 second rest |
| Minimum Battery Voltage for Starting | 24 VDC |
| Minimum Battery Voltage for Charing from GPU | 23 VDC |
| Maximum Differential Pressure | 9.3 PSID (Structural 9.7 PSID) |
| Maximum APU Starting Altitude (PATS) | 20,000 feet |
| Maximum APU Operating Altitude (PATS) | 30,000 feet |
| Generator Limits (Dual) | 300 amps(41,000') 250 amps(41-47,000') 200 amps (47,000'+) |
| Generator Limits (Single) | 365 amps (up to 25,000') Above 25,000' same as Dual Limits |
| Fuel Transfer with ZFW CG > 327 | Transfer at or prior to 2,500 lbs per side or gross weight >= 19,000 lbs. |
| Fuel Transfer with ZFW CG < 327 | Transfer at or prior to 2,000 lbs per side or gross weight >= 19,000 lbs. |
| Operate pumps prior to ______ to prevent cavitation. | 30,000 feet |
| Maximum Normal Fuel Imbalance | 200 lbs. |
| Emergency Fuel Imbalance | 800 lbs. |
| If brakes are hot.... | Do not set the brakes |
| No more than ____ vortex generator per wing may be missing to dispatch for flight. | ONE |
| No more than a total of ____ static discharge wicks may be missing from the entire airframe to dispatch for flight. | TWO |
| There cannot be ____ adjacent static discharge wicks missing at one time. | TWO |
| Maximum Baggage Compartment Load Without APU | 700 lbs. |
| Maximum Baggage Compartment Load With APU | 500 lbs. |
| No intentional stalls are permitted above ____ | 20,000 ft |
| Landing Sink Rate should be not greater than | 600 feet per min. |
| Flight above _____ is prohibited with more than _____ passengers on board. | 45,000 ft ; nine |
| Battery charging from EPU prohibited if: | 1. Batteries below 23 volts.2. OAT exceeds 100F (38C)3. Prohibited for more than four hours.4. Must charge both batteries together.5. Voltage must be set at 28.5+/- before charging. |
| Max Water / Slush on Runway | .75 inch |
| Max Crosswind without Thrust Reversers | 25 knots (Not Limiting) |
| Maximum Number of Seats | 15 (pilot, copilot, and 13 pax) |
| The Starter Generator is limited to ____ amps for takeoff and ___ amps for all other ground operations. | 365; 300 |
| The ____ temperature warning must be verified operational by a preflight test. | Battery Temperature |
| If the ______ light illuminates during ground operation, do not takeoff. | BATT O'TEMP |
| Wing Tank Fuel Transfer- The _____ _____ in the receiving tank must be off during wing tank transfer. | Boost Pump |
| Ballast Fuel is _______. | Nonusable Fuel |
| Single Point refueling pressures pos/neg. | 55 psi; -6psi. Max refueling flow is 250gpm |
| MIN Fuel Temp for Start, Takeoff, Enroute | -31 C |
| MIN Wing Fuel per Tank for Takeoff | 350 lbs. |
| Max Fuel Temp for Start, Takeoff, Enroute | +46 C. |
| Fuel boost pumps or engines must be operating for _____ prior to obtaining initail fuel quantity for takeoff in low fuel configuration. | 3 minutes |
| Fuselage fuel tank unusable fuel. | 3.0 pounds |
| Wing Tank unusable fuel | 30 pounds per wing |
| Preheat engine oil and engine when ambient temperature is _____ | -40 C or less |
| During cold starts, oil pressure up to ____ are allowed for ____. | 55 psig; 3 min |
| Max ITT for Starting | 890 or 910 |
| Engine Sync prohibited during | Takeoff, Landing, and Single-engine operations |
| Engine Fuel Computers | Must be on and operational for takeoff. |
| Fuel Control Manual Governor | Must be verified operational by a satisfactory preflight test. |
| Avoid fan speeds(N1) between ____ RPM and ____ RPM when the engine ice protection systems are on and altitude above _____. | 85%;95% & 25,000 ft. |
| Ground Idle Switch | Must be in HIGH during touch-and-go landings. |
| PACs in high-pressure bleed (PAC HP VLV OPEN) is not approved: | For Takoff and landing or when any bleed air anti-ice is activated. |
| PAC BLD SELECT must be positioned to ____ for flight above ____. | NORM or HP; 45,000 ft. |
| Operation of engine bleed anti-ice system is prohibited above ____ for longer than ____. | +10 C; 10 Seconds |
| Operation of PAC selector switches in the high-flow mode is not approved: | For takeoff and landing, flight greater than 45,000 ft, flights above 25,000 ft with isolation valve open and only one engine suppling air to the PACS, any bleed air anti-icing on. |
| Gear extension above _____ is prohibited. | 20,000 ft. |
| Extension of the speedbrakes and flaps in any position other than ____ is prohibited below ____ AGL | UP; 500 AGL. |
| Crew O2 masks not approved for cabin altitude above _____. | 40,000 ft. |
| Passenger O2 masks not approved for cabin altitude above ____. | 25,000 ft. |
| Auto pilot must be off at ____. | 200 ft AGL. |
| Aileron Boost inoperative or OFF restricts the autopilot to ______. | HDG select and altitude hold. |
Created by:
pilotcarter