Cessna Citation 500 Eagle: Checklist V 0.4
Cessna Citation V · Checklist
Overview
This document is a checklist for the Cessna Citation 500 Eagle, providing essential procedures and performance data for pilots operating this aircraft. It includes pre-flight checks, normal operations, emergency procedures, and abnormal situations. The checklist is designed to ensure safety and efficiency during flight operations, covering critical aspects such as engine start, takeoff, landing, and emergency situations. Pilots should refer to this document to verify procedures and performance specifications to enhance operational safety and compliance with aviation regulations.
- V1 speed ranges from 100 KIAS at 12,500 lbs to 93 KIAS at 11,000 lbs.
- Normal climb rates vary depending on altitude and weight, with specific speeds provided for each condition.
- Emergency procedures include detailed steps for engine failure, electrical fires, and rapid decompression scenarios.
- Engine thrust limits are specified for various temperatures and altitudes, crucial for safe operation.
- Pre-flight checks include verifying cockpit instruments, fuel quantity, and passenger safety briefings.
Document
Source
Originally published by b.org.za. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.
Document details
- Type
- Checklist
- Year
- 2003
- Pages
- 21
- File size
- 79 KB
- Publisher
- b.org.za
Common. Rarer than 1% of the aircraft models we track.
Most owners only have the POH. Here's the essential set for the Cessna Citation V.
- Pilot's Operating Handbook / AFM
- Checklist
- Maintenance Manual
- Parts Catalog (IPC)
- Systems & Wiring
- Service Bulletins
- Type Certificate (TCDS)
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In this document
Normal Checklist
The Normal Checklist outlines the procedures to follow before starting engines, during engine start, and throughout various phases of flight including taxi, takeoff, and landing. Key items include cockpit and exterior inspections, engine settings, and passenger briefings. Specific checks for instruments, fuel quantity, and safety systems are emphasized to ensure readiness for flight.
Performance Data
This section provides crucial performance data for the Cessna Citation 500 Eagle, including takeoff and landing speeds based on weight and altitude. For instance, V1 varies from 100 KIAS at 12,500 lbs to 93 KIAS at 11,000 lbs. The document also details climb performance and thrust limits under various conditions, ensuring pilots can make informed decisions regarding weight and environmental factors.
Emergency Procedures
The Emergency Procedures section details actions to take in various emergency situations, such as engine failure during takeoff, electrical fires, and rapid decompression. Each scenario includes step-by-step instructions to manage the situation effectively, emphasizing the importance of maintaining control and ensuring passenger safety.
Abnormal Checklist
The Abnormal Checklist addresses specific issues that may arise during flight, such as low oil pressure, landing gear malfunctions, and hydraulic failures. It provides clear guidance on how to respond to these situations, including necessary checks and actions to mitigate risks.
Engine Thrust Limits
This section outlines the thrust limits for takeoff and maximum continuous operation under varying temperatures and altitudes. For example, at sea level and -20°C, the takeoff thrust is 90.4% N2 with anti-ice off. This information is critical for pilots to ensure they operate within safe performance parameters.
Safety notes
- Always refer to the PFM for authoritative procedures.
- Monitor engine instruments closely during all phases of flight.
- Ensure all safety systems are operational before takeoff.
Full document text
Cessna Citation 500 Eagle: Checklist V 0.4 1 See PFM for authoritative procedures! ©2003 Chris R. Burger Cessna Citation 500 Eagle Speeds (KIAS) VMCA — Below stalling speed VMCG 55 VSSE — Not specified 150 (approx.) at 7500 lb VA 184 (approx.) at MTOW VMO 259 Below 30 400’ MMO 0,705 Above 30 400’ 199 15° (TO & Landing) VFE 173 Above 15° VLE/VLO 173 VSB VMO/MMO Other 125 8500 lb Glide 137 10 500 lb 180 Turbulent air 165 Tire Ground Speed Cruise climb 200-220 Sea level 190-210 10 000’ 180-200 20 000’ 170-190 30 000’ 160-180 40 000’ Landing Reference Speeds (full flap) Weight (lbs) VREF (KIAS) Appr. Climb 11 400 102 108 10 500 98 104 9500 93 100 8500 88 95 7500 83 88 Note: Landing climb at VREF Step Climb Max. Weights FL change Max (lb) FL change Max (lb) 310 to 350 11 800 330 to 370 11 400 350 to 390 10 900 370 to 410 10 500 Cessna Citation 500 Eagle: Checklist V 0.4 2 See PFM for authoritative procedures! ©2003 Chris R. Burger Cessna Citation 500 Eagle Performance Simplified performance Conditions: 1. No obstacles 2. Anti-ice off 3. Flap: TO & APPR 4. Field length: 1372 m or longer 5. No tailwind 6. No uphill Parameter Set 1 Set 2 Unit TOW 12 500 11 000 lb Elev. 3000 5000 ft Tmin -2 -2 °C Field Tmax 21 21 °C V1 100 93 KIAS VR 102 95 KIAS V2 105 99 KIAS Speed VMCA 151 142 KIAS Takeoff 93,9 % SE climb 92,4 % N2 ME climb 90,3 % Note: N2 is turbine RPM Climb-limited takeoff mass limits Anti-ice Off Anti-ice On 0° flap 15° flap 0° flap 15° flap SL 43°C 32°C 4°C 2000 32°C 26°C 4°C 4000 26°C 15°C -7°C 6000 15°C 4°C -18°C 8000 4°C -7°C -29°C Not Possible Note: Temperatures above those shown require mass reduction. See PFM pp. 4-9, 4-10. Cessna Citation 500 Eagle: Checklist V 0.4 3 See PFM for authoritative procedures! ©2003 Chris R. Burger Engine thrust limits (N1 = Fan Speed) Takeoff/Go-around Thrust Temp Anti-Ice Off A-I On °C SL 2000’ 4000’ 6000’ All Alt -20 90,4 93,0 95,6 98,5 95,4 -10 92,0 94,8 97,7 94,0 0 93,7 96,6 96,7 92,6 10 95,6 91,2 20 94,5 NA 30 92,8 NA 40 90,8 NA Maximum Continuous Thrust Temp Anti-Ice Off A-I On °C SL 2000’ 4000’ 6000’ All Alt -20 88,6 91,0 93,7 96,6 96,6 -10 90,4 92,8 95,6 96,4 96,4 0 92,0 94,4 95,5 96,6 10 93,9 94,4 96,4 20 93,2 NA 30 91,6 NA 40 89,7 NA Normal Climb/Cruise Thrust Temp Anti-Ice Off A-I On °C SL 5000’ 15 000 20 000 All Alt -20 86,4 92,2 96,2 98,7 94,5 -10 88,0 94,0 98,0 94,0 0 89,6 95,7 97,0 93,2 10 91,5 95,9 92,2 20 93,0 94,6 NA 30 93,0 NA 40 91,2 NA Minimum turnaround times Braking speed Landing weight kts 8000 lb 11 000 lb 60 4 min 7 min 80 8 min 13 min 100 15 min 20 min 120 22 min 26 min If V1 > 110 kts, add 3 min/kt Cessna Citation 500 Eagle: Checklist V 0.4 4 See PFM for authoritative procedures! ©2003 Chris R. Burger Cessna Citation 500 Eagle Normal Checklist Before starting engines Cockpit inspection: Completed Exterior inspection: Completed Speeds and engine settings: Computed and checked Cabin door: Closed and locked Passenger briefing: Complete Oxygen system: Checked Seats, harnesses, pedals: Adjusted and secure Parking brake: Set Control lock: Off Landing gear handle: Down Circuit breakers: Checked LH Gyro Slave: Auto Generators: On (Off for GPU) Boost pumps: Normal Crossfeed: Off All other switches: Off or Norm Windshield bleed air valves: Off Thrust levers: Off External power: Connected if required Battery switch: BATT Voltage: Check Warning systems: Checked and off Engine instruments: No flags Fuel quantity: Checked Anti-collision lights: On Cessna Citation 500 Eagle: Checklist V 0.4 5 See PFM for authoritative procedures! ©2003 Chris R. Burger Start Centre panel lights: As required Engine start button: Press briefly FUEL BOOST ON: Illuminated Ignition: Active (check green light) 8 to 10% N2: Wait Temperature: Monitor (limits, rise in 10 s) Fan speed: Present when Turbine at 20 to 25% Engine instruments: Checked Turbine RPM: Set 48 to 50% After start GPU: Disconnect if used Generators: On Lights: As required Inverters: Checked and selected Voltmeters/Load: Checked Passenger advisory lights: PASS SAFE Aft facing seat: Full aft, upright Avionics: As required Vacuum: Check Auto temperature select: As desired Pressurisation: Set altitude and rate Taxi Brakes: Check Deice system: Check if required Anti-ice systems: Check and set Gyros: Check Crossfeed: Check for one minute Cessna Citation 500 Eagle: Checklist V 0.4 6 See PFM for authoritative procedures! ©2003 Chris R. Burger Before takeoff Seats, harnesses: Check secure Ignition: On Engine instruments: Check Fuel quantity: Check Flight instruments: Check Altimeter and altitude alert: Set Avionics: Checked and set Thrust reversers: Cycled, checked and stowed Speedbrakes: Cycled, lights out Electric trim: Checked and set Trims: Set Autopilot: Tested (x3) Flight controls: Full, free, correct movement Flaps: Cycled and set Pressurisation source: Both N1, V1, VR, V2, VREF, VYSE settings: Confirm Takeoff briefing: Completed Annunciator panel: Clear Passenger advisory lights: PASS SAFETY Before takeoff (ready to go) Exterior lights: As required Anti-ice: Checked and as required Pitot/Static heat: On Transponder: Set and on Ignition: On During takeoff run Engine instruments: Monitor Pressurisation: Monitor Cessna Citation 500 Eagle: Checklist V 0.4 7 See PFM for authoritative procedures! ©2003 Chris R. Burger After takeoff Landing gear: Up Flaps: Up Ignition: NORM Climb power: Set Pressurisation: Set Passenger advisory light: As required Anti-ice systems: As required Landing lights: Off Engine instruments: Monitor Climb through FL100 Exterior lights: As required Passenger advisory light: As required Pressurisation: Checked Oxygen: As required Quick-don & 100% above FL250 Descent Cockpit/Defog fan: High (15 min prior to descent) Approach briefing: Completed Foot warmers: Close Windshield anti-ice: As required Windshield bleed air: Low Pressurisation: Set cabin altitude, Rate Anti-ice systems: As required Power: As required (maintain ice protection) Altimeters: Set, crosschecked
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Speed brakes: As required Passenger advisory light: As required Descent through FL100 Exterior lights: As required Pressurisation: Checked Passenger advisory light: As required Cessna Citation 500 Eagle: Checklist V 0.4 8 See PFM for authoritative procedures! ©2003 Chris R. Burger Before landing Seats and belts: Secure VREF, V2, N1: Confirm Lights: As required Passenger advisory lights: PASS SAFE Aft facing seat: Full aft, upright Crossfeed: Off Ignition: On Engine synchronisation: Off Landing gear: Down and locked Flaps: Land Airspeed: VREF Autopilot and yaw damper: Off Annunciator panel: Clear Pressurisation: Check zero differential Speed brakes: Retracted above 50’ After landing Flaps: Up Landing and taxi lights: As required Ignition: Normal Speed brakes: Retract Ice protection: Off Pitot heat: Off Trim: Set Transponder and radar: Off Strobes: Off Shutdown Parking brake: Set Exterior lights: Off Inverters: Off Passenger advisory light: Off Avionics: Off Cockpit/Defog fan: Off ITT: Stable for 1 min Thrust levers: Off Battery: Off Control lock: Engage Parking brake: As required External covers and chocks: Install Cessna Citation 500 Eagle: Checklist V 0.4 9 See PFM for authoritative procedures! ©2003 Chris R. Burger Cessna Citation 500 Eagle Abnormal Checklist Low oil pressure If 35 to 65 PSI: Reduce affected engine’s power If below 35 PSI: Thrust lever (affected engine): Off Accomplish engine failure/shutdown checklist Landing gear will not extend Landing gear handle: Check down Airspeed: Below 173 KIAS Gear control circuit breaker: Check in Auxiliary gear control: Pull handle, rotate to lock Rudder: Yaw if necessary to achieve lock Aux gear control: Pull knob to blow down Flap inoperative approach/landing Seats, harnesses: Secure Approach speed: Confirm Flaps 15°: VREF + 10 else VREF + 20 V2: Confirm Flap 15°: See graph 4-18 or 4A-18 Else VREF+10 Airspeed: As required Flap Control and Flap Motor CBs: Check in Passenger advisory lights: PASS SAFETY Aft facing seat: Full aft and upright Crossfeed: Off Ignition: On Landing gear: Down and locked Engine synchroniser: Off Autopilot and yaw damper: Off Annunciator panel: Clear Pressurisation: Check zero differential Speed brakes: Retracted prior to 50’ Cessna Citation 500 Eagle: Checklist V 0.4 10 See PFM for authoritative procedures! ©2003 Chris R. Burger Single-engine approach/landing Seats, harnesses: Secure VREF, V2, N1: Confirm Passenger advisory lights: PASS SAFETY Aft facing seat: Full aft and upright Crossfeed: Off Ignition (operating engine): On Flaps: TO & APPR Landing gear: Down and locked Airspeed: VREF + 10 kts Engine synchroniser: Off Autopilot and yaw damper: Off Annunciator panel: Clear Pressurisation: Check zero differential Speed brakes: Retracted prior to 50’ Single-engine go-around Thrust levers (operating engine): Takeoff power Flaps: TO & APPR Landing gear: Up when positive climb rate established Climb: Normal, at VYSE Door not locked (DOOR NOT LOCKED on) Note: Nose or tailcone doors, door switches, disengagement of lower forward cabin door pin On the ground: Correct condition prior to flight In flight: Cabin altitude: Select 9500’ Airspeed: Reduce Passenger advisory lights: PASS SAFETY Cabin door: Keep clear Altitude: Descend Land: As soon as practical Wheel brake failure Brake pedals: Remove feet Emergency brake handle: Pull as required Note: Limited capacity! Cessna Citation 500 Eagle: Checklist V 0.4 11 See PFM for authoritative procedures! ©2003 Chris R. Burger Windshield bleed air failure Windshield bleed air switch and valves: Off Windshield alcohol anti-ice: As required (<10 min!) Environment: Leave icing conditions Windshield air overheat Momentary illumination: Windshield bleed air valves: Reduce Continuous illumination: Windshield bleed air switch and valves: Off Windshield alcohol anti-ice: As required Environment: Leave icing conditions Engine anti-ice failure (ICE FAIL on) Thrust levers: Increase Engine anti-ice controls: Check switches and CBs Environment: Leave icing conditions Pitot-static failure Anti-ice switches and circuit breakers: Check Inoperative system: Determine Note: Autopilot uses copilot static Environment system air duct overheat (AIR DUCT OVERHEAT on) Circuit breaker: Reset Auto Temp Select: MAN Manual heat/Manual cool switch: MAN COOL until annunciator goes out If light does not go out: Pressurisation source: LH or RH, reduce power After light goes out: Control temperature manually Cessna Citation 500 Eagle: Checklist V 0.4 12 See PFM for authoritative procedures! ©2003 Chris R. Burger Emergency pressurisation on (automatic actuation) Note: Indicates air cycle machine failure or shutdown Temp control: Adjust to warmer setting Pressurisation source selector: EMER Wait: At least 1 minute Pressurisation source selector: LH, RH or BOTH If emergency pressurisation remains on: Press Source Select: EMER Cabin temperature: Control LH thrust lever Vacuum system failure Note: Right AI and EMER DUMP will be inoperative. Cabin pressure will go to max differential Press Source Select: Off before landing Single generator failure (GEN OFF on) Electrical load: Decrease if required (325/400 A) Failed generator: Check switches/CBs, reset as req’d If unable to reset: Failed generator: Off No. 2 AC failure (RAD AC PWR FAIL on) Note: Radar, Bendix radio altimeter will not operate No. 1 AC failure (FD AC PWR FAIL on) AC Power crossover: XOVER Note: Radar, Bendix radio altimeter will not operate Electric trim runaway Autopilot/Trim disengage: Press Manual elevator trim: As required Electric trim inoperative Electric trim circuit breaker: Check CB If still inoperative: Manual elevator trim: As required Cessna Citation 500 Eagle: Checklist V 0.4 13 See PFM for authoritative procedures! ©2003 Chris R. Burger Jammed elevator trim tab Cruise: Trim speed: Maintain as long as possible Takeoff or go-around: Power: Reduce to maintain < 120 KIAS Airspeed: Flaps 0°: VREF + 20 Flaps 15°: VAPP Flaps 40°: VREF Landing gear: Do not retract Land: As soon as practical Note: If flaps not 40°, use flaps inop. procedure Low fuel pressure (FUEL PRESS LO on) Fuel boost: On Circuit breakers: Check in Fuel: Check Crossfeed: If required Low fuel quantity (FUEL LEVEL LO on) Note: Minimum 170 lb remains in either tank Fuel boost: On Land: As soon as practical Low hydraulic pressure (HYD PRESS LO on) Note: Indicates inoperative pump Affects landing gear, speed brakes, reversers Low hydraulic fluid level (HYD LEVEL LO on) Land: As soon as practical Note: Affects landing gear, speed brakes, reversers Cessna Citation 500 Eagle: Checklist V 0.4 14 See PFM for authoritative procedures! ©2003 Chris R. Burger Hydraulic system remains pressurised (HYD PRESS ON) Speed brake control circuit breaker: Pull If system remains pressurised: Reset Gear control circuit breaker: Pull If system remains pressurised: Reset Reverser control circuit breaker: Pull If system remains pressurised: Reset Affected breaker: Leave pulled If system remains pressurised Land: As soon as possible Before landing Circuit breakers: Reset to restore operation Fuel filter bypass (FUEL FILT BYPASS on) Note: Inspect filters after landing False engine start (no ignition) Thrust lever: Off Wait: 15 s Starter disengage: Press Engine fire during ground shutdown (high or sustained ITT) Thrust lever: Check off Start button: Press momentarily Wait: 15 s Starter disengage: Press Supplemental oxygen usage Oxygen masks: NORMAL below 25 000’, 100% above Oxygen supply: Check crew and passengers Cabin altitude: Max 25 000’with pax, else 34 000’ Oxygen: Check endurance (fig. 3.3) Range: Compute (oxygen supply, revised groundspeed) Cessna Citation 500 Eagle: Checklist V 0.4 15 See PFM for authoritative procedures! ©2003 Chris R. Burger Cessna Citation 500 Eagle Emergency Checklist Engine failure/fire during takeoff Speed below V1: Abort takeoff Brakes: As required Throttles: Idle Speed brakes: Extend If engine fire: Accomplish checklist If engine failure: Accomplish checklist Speed above V1: Normally continue takeoff Positive rate of climb: Attain Gear: up Height: Climb 400’ Flaps: Retract at V2 + 10 Airspeed: 140 KIAS If engine fire: Accomplish checklist If engine failure: Accomplish checklist Engine failure/precautionary shutdown Thrust lever (affected engine): Off Electrical load: Reduce as required Crossfeed: As required Generator (affected engine): Off Note: If no fire hazard, leave shutoff open and boost pump on Maximum glide: Emergency landing Airspeed: 125 KIAS @ 8500 lb + 3 KIAS/500 lb Flaps: Up Speed brakes: Retract Landing gear: Up Transponder: Emergency ATC: Advise Passenger advisory switch: PASS SAFE Shoulder harnesses: Secure Before landing: Landing gear: As required Speed brakes: As required Flaps: As required Cessna Citation 500 Eagle: Checklist V 0.4 16 See PFM for authoritative procedures! ©2003 Chris R. Burger Engine failure during coupled approach Power (operating engine): Increase as required Rudder trim: Toward operating engine Airspeed: VREF + 10 kts Flaps: TO & APPR Thrust lever (affected engine): Off If engine fire: Accomplish checklist Passenger advisory lights: PASS SAFE Aft facing seats: Check full aft and upright Ignition (operating engine): On Landing gear: Down and locked Annunciator panel: Check Flaps: LAND (when landing is assured) Emergency restart: One engine Note: Air start envelope in fig 3.1. Without starter assist: Over 200 KIAS. With starter assist: 100 KIAS below 10 000’to 150 KIAS @ 35 000’ Following shutdown, with starter assist: Thrust lever: Off Generator: GEN Firewall shutoff: Check open Ignition: On Start button: Press momentarily Thrust lever: Idle at 8 to 10% turbine RPM Engine instruments: Monitor Ignition: NORM Following shutdown, windmilling, > 200 KIAS Thrust lever: Off Firewall shutoff: Check open Ignition: On Boost pump: On Thrust lever: Idle Engine instruments: Monitor until stable Boost pump: NORM Ignition: NORM Generator: GEN Cessna Citation 500 Eagle: Checklist V 0.4 17 See PFM for authoritative procedures! ©2003 Chris R. Burger Emergency restart: Two engines Note: Air start envelope in fig 3.1. Without starter assist: Over 200 KIAS. With starter assist: 100 KIAS below 10 000’to 150 KIAS @ 35 000’ Ignition: Both on Boost pumps: Both on Thrust levers: Both idle If altitude allows: Increase airspeed to 200 KIAS Firewall shutoff: Check open All anti-ice switches: Off If no start in 10 s: Either start button: Press momentarily Engine fire (ENG FIRE PUSH illuminated) Thrust lever (affected engine): Idle If light remains on: Engine fire switch: Lift cover and push Illuminated BOTTLE ARM switch: Push Ignition: NORM Thrust lever (affected engine): Off Electrical load: Reduce as required 400 A to 35 000’, 325 A above Boost pump: Off If fire warning still on after 30 s: Other BOTTLE ARM switch: Push Land: As soon as possible Light goes out, no secondary indications present: Land: As soon as practical Environmental smoke or odour Oxygen masks: Don and 100% Cabin fan: Off Cockpit/defog fan: Off Pressurisation selector: Isolate LH— RH— EMER Cessna Citation 500 Eagle: Checklist V 0.4 18 See PFM for authoritative procedures! ©2003 Chris R. Burger Smoke removal Note: Action only required if smoke is intense Oxygen masks: Don and 100% Pass Oxy manual valve: On Oxygen priority valve: Check normal Passengers: Assure receiving oxygen Passenger advisory light: PASS SAFE Emergency dump switch: DUMP Refer to use of supplemental oxygen procedure If smoke persists or cannot be verified fire free: Land: As soon as possible Electrical fire or smoke Oxygen masks: Don and 100% selected Known source: Isolate faulty circuit Unknown source: Battery switch: EMER Generators: Off Note: Items inoperative on EMER: Landing gear: Use blow-down system Flaps: Make flap inop landing if required Engine anti-ice will be open: Engine performance OAT gauge unreliable: Caution thrust settings All engine gauges inoperative except N1 > 50% Microphone: EMER COMM Electrical switches: Off Windshield bleed air manual valves: Off All circuit breakers pull except: NAV/RMI2; PN101 compass; COM1; FLOOD; DC PWR LH BUS (3); DC PWR RH BUS (3); LH CB PANEL; RH CB PANEL Note: Headphones required! Battery switch: BATT Generators: GEN If severity of smoke warrants: Initiate smoke removal and/or emergency descent procedures as required If fire or smoke persists or it cannot be verified that the fire is extinguished: Land: As soon as possible If fire or smoke decreases: CBs and switches: Reinstate one at a time Cessna Citation 500 Eagle: Checklist V 0.4 19 See PFM for authoritative procedures! ©2003 Chris R. Burger Electrical fire or smoke Oxygen masks: Don and 100% selected Known source: Isolate faulty circuit Unknown source: Battery switch: EMER Generators: Off Note: Items inoperative on EMER: Landing gear: Use blow-down system Flaps: Make flap inop landing if required Engine anti-ice will be open: Engine performance OAT gauge unreliable: Caution thrust settings All engine gauges inoperative except N1 > 50% Microphone: EMER COMM Electrical switches: Off Windshield bleed air manual valves: Off All circuit breakers pull except: NAV/RMI2; PN101 compass; COM1; FLOOD; DC PWR LH BUS (3); DC PWR RH BUS (3); LH CB PANEL; RH CB PANEL Note: Headphones required! Battery switch: BATT Generators: GEN If severity of smoke warrants: Initiate smoke removal and/or emergency descent procedures as required If fire or smoke persists or it cannot be verified that the fire is extinguished: Land: As soon as possible If fire or smoke decreases: CBs and switches: Reinstate one at a time Cessna Citation 500 Eagle: Checklist V 0.4 20 See PFM for authoritative procedures! ©2003 Chris R. Burger Loss of both generators Generators: RESET then GEN If only one generator comes on: Electrical load: Reduce as required 400 A to 35 000’, 325 A above If neither generator comes on: Battery switch: EMER Note: Only DG2, COM1, NAV2 and floodlight for approx. 30 minutes Note: Items inoperative on EMER: Landing gear: Use blow-down system Flaps: Make flap inop landing if required Engine anti-ice will be open: Engine performance OAT gauge unreliable: Caution thrust settings All engine gauges inoperative except N1 > 50% Microphone selector: emer comm Windshield bleed air manual valves: Off Land: As soon as practical Overpressurisation Cabin altitude selector: Set higher cabin altitude Rate control: INC If still overpressurised: Pressurisation source selector: LH or RH Cabin altitude: Control with thrust lever If unable to control: Oxygen masks: Don and 100% Pass oxy manual valve: On Crew oxy priority valve: Check NORMAL Passengers: Assure receiving oxygen Passenger advisory light: PASS SAFE Emergency dump switch: DUMP Refer to use of suppl. oxygen procedure Cessna Citation 500 Eagle: Checklist V 0.4 21 See PFM for authoritative procedures! ©2003 Chris R. Burger Rapid decompression Oxygen masks: Don and 100% Emergency descent: As required Crew oxy priority: Check NORMAL Passengers: Ensure receiving oxygen Transponder: Emergency If cabin altitude above selected value: Cabin altitude selector: Reduce Rate control: Full INC Pressurisation source select: Check BOTH If selection does not hold pressurisation: Pressurisation source selector: EMER If not arrested by 14 000’ cabin altitude: Emergency descent: Initiate Crew oxy priority valve: Check NORMAL Passengers: Assure receiving oxygen Refer to use of suppl. oxygen procedure Emergency descent Thrust levers: Idle Speed brakes: Extend Bank: Moderate bank angle Passenger advisory lights: PASS SAFE Maximum airspeed: VMO/MMO Note: Reduce speed if structural damage Transponder: Emergency Autopilot hardover Autopilot/Trim disengage: Press Maximum altitude losses: As specified in PFM