CESSNA CITATION C750 (CITATION X)

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1 DEPARTAMENTO “SEGURIDAD OPERACIONAL” SUBDEPARTAMENTO “LICENCIAS” SECCIÓN EVALUACIONES “CESSNA CITATION C750 (CITATION X)” “PUNTA BRAVA S.A.” (Rev. 2 - 10 Abril 2012) A.- LIMITATIONS: 1.- Limitations ( KIAS) V (Turbulence - Max) 350 VMO (below 8.000’) 270 VMO (8.000 a 30.650’) 350 MMO (Above 30.650’) 0.92M MMO (Mach Trim OFF) 0.82M VFE ( 5° position) 250 VFE ( 15° position) 210 VFE (Full Position) 180 VLO/VLE 210 VSB max NO LIMIT VSB min VREF + 15 Vslats extended 250 VTIRE (Ground Speed) 182 Kts VS VSO VX VY VXSE VYSE 190 Max Cross Wind (Hyd. Fail) 10 Max Tail Wind 10 Max Cross Wind CAT II 15 Max Tail Wind CAT II 10 2.- Fuel (U.S. GAL & LBS) Type to Utilize JET A – A1 Main Fuel System Auxiliary Fuel System Max Usable Fuel Quantity Max Asymmetric Fuel 400 Emerg Asymmetric Fuel 800 Min Wing Fuel Per tank For T/O 500 3.- Weight (LBS) Maximum TAKE-OFF 36.100 Maximum LANDING 31.800 MAX ZFW 24.400 MAX Baggage Compartment 700 4.- Altitude Limitation Max Alt Ext Flaps & L-Gear 18.000 Max Operating Alt 51.000 Max Alt For T/O & Landing 14.000 5.- Starter Limitations 30 SEC ON 30 SEC OFF 30 SEC ON 30 SEC OFF 30 SEC ON 25 MIN OFF 2 B.- EMERGENCY PROCEDURES: 1. APU FIRE 1. APU FIRE Switch Lift Cover and Push 2. AUTO SLAT FAIL 1. Control Column Push, Pitch Down to Horizon 2. Throttles Set to TO/MC Detent 3. Airspeed Increase 3. BATT 1 or 2 O’TEMP 1. Battery Switch (affected side ) OFF 4. CABIN ALTITUDE 1. Oxygen Masks Don and 100% 2. L and R MIC Switches MIC OXY MASK 3. Emergency Descent As Required 5. EDM – EMERGENCY DESCENT 1. Initiate maximum rate-of-descent to a safe altitude. 6. ENGINE FIRE L or R 1. Throttle (affected engine) IDLE 2. WING XOVER ANTI-ICE Switch (if icing conditions) WING XOVER  If ENG FIRE Light Remains On (15 Seconds) Probable Fire 3. Illuminated ENG FIRE Button Lift Cover and Push 4. Either Illuminated BOTTLE ARMED Light Push 3 7. HYD PUMP FAIL A and B 1. A AUX PUMP Switch ON 8. MINIMUM SPEED 1. Control column Push, Pitch Down to Horizon 2. Throttles Set to TO/MC Detent 9. NO TAKEOFF  Speed Below V1 – Takeoff Rejected 1. Takeoff Abort 10. NO TAKEOFF  Speed Above V1 – Takeoff Continued 1. Climb to a Safe Altitude. 11. RUDDER LIMIT FAIL 1. Rudder Pedals Do Not Apply Large or Abrupt Rudder Input 12. TR AUTOSTOW L and R 1. THRUST REVERSER Stow switches (both) STOW EMER 2. Throttles (both) IDLE, Then Normal Operation 13. ENGINE FAILURE OR OTHER EMERGENCY DURING TAKEOFF  If Speed Below V1 1. Takeoff Abort 4 14. ENGINE FAILURE OR OTHER EMERGENCY DURING TAKEOFF  If Speed at or Above V1 1. Climb to a safe altitude 2. WING XOVER Switch (if bleed air anti-ice systems are on) XOVER 15. ENGINE FAILURE DURING FINAL APPROACH 1. Flaps Select 15° 2. Airspeed Vref (Flaps 15°)+ 10 KIAS Minimum Until landing is assured 16. THRUST REVERSER IN-FLIGHT DEPLOYMENT 1. TRHUST REVERSER Stow Switch (affected thrust reverser) STOW EMER 2. Throttle (affected engine) IDLE 3. Control Wheel/Autopilot Grip/Disengage 4. Airspeed Reduce to 170 KIAS Maximum 17. DUAL ENGINE FLAMEOUT – LOW ALTITUDE 1. Fuel Check (tank/quantity; crossfeed/as required; transfer/as required) 2. FUEL BOOST Switches ON 3. Throttles CUTOFF 18. DUAL ENGINE FLAMEOUT – CRUISE 1. Crew Oxygen Masks (if required) DON 19. ELECTRICAL SYSTEM SMOKE OR FIRE 1. Oxygen Masks Don and EMER 2. Smoke Goggles Don (as required) 5 20. ENVIROMENTAL SMOKE OR ODOR 1. Oxygen Masks Don and EMER 2. Smoke goggles Don (as required) 21. SMOKE REMOVAL 1. Oxygen Masks Don and EMER 2. Smoke goggles Don (as required) 22. HYDRAULIC WHEEL BRAKE FAILURE 1. Brake Pedals Remove Feet 2. EMERGENCY BRAKE Handle Pull and Hold Until Stopped 23. NOSEWHEEL STEERING MALFUNCTION 1. AP/TRIM/NWS Disengage Button Push and hold 24. JAMMED ROLL OR PITCH CONTROL SYSTEM 1. Control Wheel Relax Pressure 2. Pitch/Roll Disconnect Handle Pull Until Latched 3. Operative Flight Control Wheel Identify, Recover Aircraft Attitude 25. PRIMARY PITCH TRIM RUNAWAY 1. AP/TRIM/NWS Disengage Button Push and hold 26. SECONDARY PITCH TRIM RUNAWAY 1. SECONDARY TRIM Switch OFF (close guard cover) 6 27. INADVERTENT STALL (STICK SHAKER, BUFFET, AND/OR ROLL-OFF) 1. Autopilot Disconnect 2. Pitch Attitude Reduce 3. Roll Attitude Level 4. Throttles TO Detent 28. EMERGENCY DESCENT 1. AP/TRIM/NWS Disengage Button Press (to disengage autopilot) 2. Throttles IDLE 3. Speed Brakes Extend 4. Initial Pitch Attitude 15° Down 29. TOTAL LOSS OF (OR UNRELIABLE) AIRSPEED INDICATION (PILOT, COPILOT AND STANDBY) 1. AP/TRIM/NWS Disengage Button Press 2. Flight Director OFF 3. LH/RH PITOT/STATIC Anti-ice Switches Both OFF, then ON 4. Rudder Pedals Do Not Apply Large or Abrupt Rudder Input