Citation Mustang C510 Memory Items and Limitations

• The Engine Indicating System may take up to 10 minutes to become usable after power is applied when cold soaked below -40°C (-40°F). • Maximum Airport Elevation For Ground Battery Start ......................................................10,000 Feet Power Unit Start ...............................................14,000 Feet • Minimum Battery Voltage For Battery Start NiCad .....................................................................22 Volts Lead Acid ................................................................24 Volts ENGINE START LIMITATIONS (AIR) • Minimum Temperature for Windmill Start ................ -10°C RAT FADEC (FULL AUTHORITY DIGITAL ENGINE CONTROL) • Dispatch with an engine FADEC fault (ENG CTRL SYS L or R message displayed) is prohibited. F O R T R A I N I N G P U R P O S E S O N L Y Citation Mustang C510 Memory Items and Limitations ENGINE START LIMITATIONS • Maximum Time to Stabilized Idle (In-Flight/Windmilling) .......................................... 90 Seconds • Minimum Engine Oil Temperature (as indicated on EICAS) ................................................. -40°C • If engine oil temperature is below -40°C (-40°F), the engine must be preheated prior to conduc�ng a start. • If the ba�ery has been cold soaked for 2 hours or longer at an ambient surface temperature of -10°C (14°F) or lower, it must be preheated to above -10°C (14°F) prior to start. Nickel Cadmium Battery ENGINE START LIMITATIONS Lead Acid Battery • Maximum Time to Stabilized Idle (In-Flight/Windmilling) .......................................... 90 Seconds • Minimum Engine Oil Temperature (as indicated on EICAS) ................................................. -40°C • If engine oil temperature is below -40°C (-40°F), the engine must be preheated prior to conduc�ng a start. • If the ba�ery has been cold soaked for 2 hours or longer at an ambient surface temperature of -18°C (0°F) or lower, it must be preheated to above -18°C (0°F) prior to start. ENGINE OPERATING LIMITS • Oil temperature must be above 22°C for at least 5 minutes before takeoff. Once oil temperature is +10°C or warmer, it is acceptable to increase power-up to the CRU detent to decrease the �me required to warm the oil to 22°C. STARTER CYCLE LIMITATIONS • Starter Cycle Limita�on ............................. Three engine starts per 30 minutes. • Three cycles of opera�on with a 60-second rest period between cycles is permi�ed. GROUND POWER UNIT LIMITATIONS FOR STARTING • Minimum/Maximum Current .......................... 800/1100 Amps • Maximum Voltage ...................................................... 29 VDC • Normal starter current draw is approximately 1000 amps peak. Ground power units with variable maximum current shutoff should be set to 1100 amps. Use of ground power source with voltage in excess of 29 VDC or current in excess of 1100 amps may damage the starter. BATTERY LIMITATIONS • Ba�ery Start Limita�on ........................... Three engine starts per hour • Minimum Voltage for Start NiCad ...................................................................... 22 Volts Lead Acid ................................................................ 24 Volts • If the BATTERY O’TEMP message displays during ground opera�ons, dispatch is prohibited un�l a�er the proper main tenance procedures have been accomplished. • Three generator-assisted cross starts are equal to one bat tery start. If a ground power unit is used for start, no ba�ery cycle is counted. BAGGAGE COMPARTMENTS • Nose Baggage Compartment (L-R) .. 320 lbs max(combined) • Tailcone Baggage Compartment ..... 300 lbs max (combined) ELECTRICAL POWER SYSTEM STATUS: LIMIT • On Ground, Idle ...................................................... 150 Amps • On Ground, Above Idle .......................................... 300 Amps • Air ≤ 30,000 Feet .................................................... 300 Amps • Air > 30,000 Feet .................................................... 280 Amps GROUND OPERATION • Limit ground opera�on of pitot-sta�c heat to 2 minutes to preclude damage to the pitot tubes and stall warning vane. • than -40°C. Movement of the flaps is prohibited at temperatures colder FUEL LIMITATIONS • The corresponding electric fuel boost pump must be turned ON when the FUEL LO L-R CAS message is displayed or at 170 pounds or less of indicated fuel in either tank. • Maximum approved fuel imbalance is 200 pounds. • Minimum fuel quan�ty for takeoff is 200 pounds per wing. OIL LIMITATIONS • Maximum oil consump�on is one U.S. quart per 13.5-hour period. If oil consump�on exceeds this amount, refer to the Pratt and Whitney PW615F-A Maintenance Manual. • The oil level must be serviced to the MAX indica�on on the sight glass for any flight planned to exceed 5 hours in dura�on. MINIMUM CREW • One pilot, provided: – The pilot holds a CE510(S), single-pilot type ra�ng – The airplane is equipped for single-pilot opera�on as specified in the Kinds of Opera�ons Equipment List – The pilot must occupy the le� pilot’s seat –OR– • One pilot and copilot provided: – The pilot holds a CE510(S), or CE510 (second in command required) pilot type ra�ng ENROUTE OPERATIONAL LIMITS • Maximum Opera�ng Al�tude ................................ 41,000 Feet • Maximum Al�tude for Extension of Flaps ............ 18,000 Feet • Minimum Temperature for Opera�on of Flaps......... -40°C RAT • Yaw Damper must be engaged above FL300. ENROUTE OPERATIONAL LIMITS RVSM Operations • The following equipment must be installed and opera�ng normally upon entering RVSM airspace: – Pilot and copilot primary al�meters – Autopilot – Al�tude Alerter – ATCRBS Transponder CABIN PRESSURIZATION LIMITATIONS • Normal Cabin Pressuriza�on Limita�ons ............................................. 0.0 to 8.5 (+0.1) PSID MANEUVER LIMITATIONS • Acroba�c maneuvers, including spins, are prohibited. • Inten�onal stalls are prohibited above 18,000 feet. SPEED LIMITATIONS • Maximum Opera�ng Limit Speeds VMO(Between Sea Level and 27,120 Feet) .......... 250 KIAS MMO(Above 27,120 Feet) ............... 0.63 Mach (Indicated) • Maximum Flap Extended Speed - V FE TAKEOFF / APPROACH Detent (15°) .................... 185 KIAS LAND Posi�on (30°) .............................................. 150 KIAS • Maximum Landing Gear Extended Speed - V LE .......................................... 250 KIAS Opera�ng Speed - V LO (Extending) ...................... 250 KIAS Opera�ng Speed - V LO (Retrac�ng) ...................... 185 KIAS • Maximum Speed Brake Opera�on Speed - VSB ....... No Limit • Maximum Autopilot Opera�on Speed ..................... 250 KIAS or 0.63 Mach • Maximum Tire Ground Speed ................................ 160 Knots • Minimum Speed For Sustained Flight In Icing Condi�ons (except takeoff, approach and landing) .................... 160 KIAS TAKEOFF AND LANDING OPERATIONAL LIMITS • Maximum Al�tude Limit ........................................ 14,000 Feet • Maximum Tailwind Component ................................. 10 Knots • Maximum Demonstrated Crosswind Component (Not Limi�ng)......................................................... 25 Knots • Minimum Fuel Quan�ty per Wing for Takeoff ...... 200 Pounds • The maximum approved fuel imbalance is 200 pounds; however, controllability for safe return and landing has been demonstrated with an emergency fuel imbalance of 600 pounds. • The autopilot and yaw damper must be disengaged for take- off and landing. • Dispatch with a ENG CTRL SYS L-R message displayed is prohibited. • Takeoff and landings are limited to paved runway surfaces. • Dispatch with an�skid inopera�ve is prohibited if the forecast condi�ons for the des�na�on approach and landing will require the use of STALL WARNING-HIGH (Flap TO/APR) landing data. • adhering anywhere on the outside of the airplane. STALL Use of flaps in the LAND posi�on is prohibited with ice WARNING-HIGH landing performance data in Sec�on IV is predicated on the use of Flaps TO/APR for landing. • Speed brakes must be retracted prior to 50-feet AGL before landing (unless required by AFM procedure). • Cabin must be depressurized for landing. VORTEX GENERATORS AND STATIC WICKS • The following lists the number of vortex generators required for dispatch: – Wing .......................... 16 installed (8 per side) ... 16 required. • T he following lists the number of sta�c wicks that may be missing or broken, but no more than two total: – Right-hand wing�p and aileron .... 3 installed ...... 2 required. – Le�-hand wing�p and aileron ....... 3 installed ...... 2 required. – Rudder and Tailcone ..................... 4 installed ...... 3 required. – Elevators ......................6 installed (3 per side) ..... 5 required. STALL WARNING AND LOW SPEED AWARENESS SYSTEMS • The low speed awareness system can be used as a reference for approach speed (V ) at all airplane weights, CG loca�ons an�-ice/device system se�ngs and flap posi�ons. V REF REF is indicated by a green circle on the pilot and copilot airspeed indicators. • The low speed awareness system may be used as a reference, but does not replace the airspeed display in the Primary Flight Display (PFD) as a primary instrument. PASSENGER COMPARTMENT • For taxi, takeoff, and landing, adjustable passenger seats must be posi�oned with seatbacks upright. Passenger seat belts must be properly fastened. • The maximum passenger sea�ng, not including 2 crew seats, is four. • The use of the lavatory is prohibited for taxi, takeoff, and landing and is limited to one occupant in flight. SUPPLEMENTAL OXYGEN SYSTEM • Service the oxygen system with Aviator’s Breathing Oxygen (MIL-O-27210). The use of medical oxygen is prohibited. • For single-pilot opera�ons, a crew oxygen mask must be available for a passenger occupying the right crew seat. The mask must be checked during preflight and passenger briefed on its use. GARMIN G1000 AVIONICS SYSTEM • Autopilot: a. One pilot must remain seated, with the seatbelt fastened, during all autopilot opera�ons. b. Autopilot opera�on is prohibited if either PFD is in AHRS reversion. c. Autopilot Minimum-Use-Height: (5) Takeoff and Climb ................................ 700 Feet AGL (6) Enroute and Descent ......................... 1000 Feet AGL (7) Approach (GP or GS Mode) ................. 200 Feet AGL (8) Approach (FLC, VS, PIT or ALT Mode) ....... Higher of .............................. 400 Feet AGL or Approach MDA KINDS OF OPERATIONS EQUIPMENT LIST—SINGLE PILOT • The following are required when the airplane is operated with a crew of one pilot; per applicable opera�ng rules: 1. Operable GFC-700 Autopilot. 2. Headset with microphone (must be worn). 3. FAA Approved Pilots’ Abbreviated Normal Procedures Checklist, Cessna PN 510CLNP-07 or later approved revision. 4. FAA Approved Pilots’ Abbreviated Emergency and Abnormal Procedures Checklist, Cessna PN 510CLEAP-07 or later approved revision. 5. Provisions for storage and reten�on of naviga�on • PFD 1—Reversion mode • NAV1 (including marker beacon) • Pilot and copilot audio panel • L and R N 1, N2, and ITT indica�ons • L Oil Temperature • Fuel Temperature • Ba�ery voltage indica�on • Cockpit flood light • Landing gear indicator lights • ELT GPS posi�on interface • Standby instruments (airspeed, al�tude, a�tude • Cabin al�tude and differen�al pressure indica�ons • COM 1 • GPS 1 • ADC 1 • AHRS 1 • L Fuel flow • Magne�c compass light • Cabin dump system • Pilot pitot-sta�c heat • Avionics audio warnings charts, accessible to the pilot from the pilot sta�on. AIRCRAFT GENERAL • V MCA : Flaps 0° VMCA .................................................. 92 KIAS Flaps 15° VMCA ................................................. 81 KIAS • VMCG ........................................................................... 73 KIAS • V X 114 KIAS • V Y .. 150 KIAS Best angle of climb speed (Mul�-engine, flaps 0°) Best rate of climb speed (Mul�-engine, flaps 0°) EMERGENCY BUS ITEMS F O R T R A I N I N G P U R P O S E S O N L Y