FSR500 QUICK REFERENCE HANDBOOK FOR SIMULATION USE ONLY

Piper M500 · Emergency Procedures

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Overview

The FSR500 Quick Reference Handbook is designed for simulation use and provides essential emergency procedures for the Piper M500 aircraft. This handbook serves as a quick reference for pilots and aviation enthusiasts, detailing critical actions to take in various emergency scenarios. It includes procedures for engine failure, oil temperature and pressure issues, and emergency descents, among others. The handbook emphasizes the importance of understanding the aircraft systems and following the outlined procedures to ensure safety during flight operations.

Maintain an airspeed of 100 KIAS during an engine failure immediately after take-off.
Set the power lever to idle and condition lever to cut-off/feather in case of engine failure before rotation.
Monitor oil pressure and temperature closely; reduce power if indications are abnormal.
In-flight engine failure requires maintaining an airspeed of 108 KIAS and feathering the propeller.
Emergency descent procedures involve disengaging the autopilot and setting the power lever to desired torque.

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Document details

Type: Emergency Procedures
Year: 2023
Pages: 11
File size: 1000 KB
Publisher: fsr500.fsreborn.com

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In this document

Engine Failure Before Rotation

In the event of an engine failure before rotation, the pilot should set the power lever to idle and apply brakes as required. If there is insufficient runway for a safe stop, the condition lever should be moved to cut-off/feather, the battery switch turned off, and the firewall fuel shutoff valve pulled off.

Engine Failure Immediately After Take-Off

If an engine failure occurs immediately after take-off, maintain an airspeed of 100 KIAS and keep the landing gear down. The power lever should be set to idle, and the condition lever moved to cut-off/feather. If time allows, extend the flaps to 36° and aim for an airspeed of 85 KIAS before shutting off the battery and pulling the firewall fuel shutoff valve.

Engine Failure In Flight

In-flight engine failure requires the pilot to oxygen as needed and select the MIC SEL switch to MSK. Maintain an airspeed of 108 KIAS, set the power lever to idle, and move the condition lever to cut-off/feather. Verify that the propeller is feathered and check remaining fuel.

Oil Temperature and Pressure Procedures

For high oil temperature indications, reduce power and land as soon as possible. If oil pressure is low, reduce power to a maximum of 1100 ft-lb of torque and land as soon as practical. If oil pressure is high, land as soon as possible.

Emergency Descent Procedures

In an emergency descent, the autopilot should be disengaged, and the power lever set to the desired torque. The descent should be conducted while monitoring altimeters and cabin climate controls.

Safety notes

This handbook is for simulation use only; pilots should be familiar with actual aircraft systems as detailed in the aircraft manual.
Realistic failure settings may not accurately reflect the aircraft's behavior in all scenarios.

Full document text

FSR500 QUICK REFERENCE HANDBOOK FOR SIMULATION USE ONLY FSR500 LIMITATIONS FSR500 QUICK REFERENCE HANDBOOK FOR SIMULATION USE ONLY FSR500 by Copyright © 2023, Flight Sim Technologies ltd. www.fsreborn.com All rights reserved. No part of this manual may be reproduced or used in any manner without written permission of the copyright owner. V1.0 published 4 November 2023, updated 10 November 2023 to v1.09 Manual words and graphic design by AlpineBRAVO THIS HANDBOOK IS FOR SIMULATION USE ONLY Quick Reference Handbook V1.09 FSR500 QUICK REFERENCE HANDBOOK FOR SIMULATION USE ONLY FSR500 LIMITATIONS N-2b -ENGINE START - USING EXTERNAL POWER BATTERY Switch ..........................................................Verify OFF External Power Unit ....................................................... CONNECT Voltmeter.................................. CHECK STABLE 24 to 29 VOLTS FUEL PUMPS Switch .............................................................MAN L and R FUEL PUMP ON CAS Messages ............... ILLUMINATED IGNITION Switch ...................................................................MAN IGNITION ON CAS Message .................................. ILLUMINATED Prop Area ............................................................................... CLEAR START MODE Switch .......................................................... AUTO ...................................................(Light in Switch Extinguished) PUSH START Switch........................................ LIFT COVER/PUSH Oil Pressure .......................................................... CHECK RISING CONDITION Lever ..................................................................RUN ITT .............................................. MAX. 1000°C LIMITED TO 5 SEC. If combustion is not initiated within 10 sec. of moving Condition Lever to Run then: a. CONDITION Lever ........................... CUT-OFF/FEATHER b. START MODE Switch ........................ PUSH MAN/STOP c. Allow minimum 30s fuel draining, then refer to DRY MOTORING RUN CHECKLIST N-15 (ON BACK). ITT must ≤150°C before reattempting engine start. Starter @ 56% Ng ...................................Verify START ENGAGED CAS message extinguished (If not – PUSH START MODE MAN/STOP SWITCH) Ng ............................................................ STABLE at or above 63% Np ................................................... VERIFY 1200 RPM MINIMUM FUEL PUMPS Switch ........................................................... AUTO IGNITION Switch .....................................................................OFF Oil Pressure ................................................ CHECK (Min. 60 PSI) BATTERY Switch ......................................................................ON External Power Unit ................................................. DISCONNECT GEN Switch .................... ON/CHECK POSITIVE AMPS/28 VOLTS ALT Switch ...............................................................................ON N-16 FLIGHT INTO KNOWN ICING CHECKLIST PRIOR to entering icing conditions, the following ice protection systems MUST be activated. SURF DE-ICE ............................................................ SELECT ON STALL HEAT ............................................................. SELECT ON PITOT HEAT ............................................................. VERIFY ON PROP HEAT .............................................................. SELECT ON WINDSHLD HT ................................................ SELECT ANTI ICE Wing Inspection Light (ICE LIGHT)...................... AS REQUIRED IGNITION .......................................................................... MAN Windshield Defog (DEFROST)..................................... PULL ON ECS CABIN COMFORT ....................................................... HIGH During Icing Conditions: Wing Leading Edge ................................................... MONITOR ................................................... for continual shedding of ice EIS Indications and CAS Window ............................. MONITOR ........................ for correct function of ice protection systems ..................................................................(no system failures) After departure from icing conditions with remaining residual/airframe ice: SURF DE-ICE ...................................................... MAINTAIN ON STALL HEAT ....................................................... MAINTAIN ON PROP HEAT ........................................................ MAINTAIN ON PITOT HEAT ....................................................... MAINTAIN ON WINDSHLD HT ........................DE-FOG or ANTI ICE as required IGNITION ......................................................................... AUTO Flaps ..........................................DO NOT EXTEND BEYOND 20° After removal of residual ice: SURF DE-ICE ....................................................................... OFF STALL HEAT ........................................................................ OFF PROP HEAT ......................................................................... OFF PITOT HEAT ....................................................... MAINTAIN ON WINDSHLD HT ........................DE-FOG or ANTI ICE as required Additional Normal Checklist Items WARNING THIS QUICK REFERENCE HANDBOOK IS PROVIDED FOR CONVENIENT REFERENCE ONLY. IF USING REALISTIC FAILURE SETTINGS, PILOTS SHOULD BE FAMILIAR WITH THE AIRCRAFT SYSTEMS AS DETAILED IN SECTION 6 OF THE AIRCRAFT MANUAL AND THE ENHANCED PROCEDURES DESCRIBED IN SECTION 9. FSR500 QUICK REFERENCE HANDBOOK FOR SIMULATION USE ONLY Operating Speeds Limitations Maximum Ramp Weight 5134lb (2329kg) Maximum Take-Off Weight 5092lb (2310kg) Maximum Landing Weight 4850lb (2200kg) Ng Max = 101.8% Torque 1313 lb-ft ITT Start: 1000°C for 5s After start: 770°C Propeller (Np) 1200-2000RPM Oil Temperature & Pressure Start Take-off/MCP/Cruise

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Idle Pressure (PSI) Temperature (°C) 0-200 -40 minimum 100-135 0-99 60 minimum -40 to 99 Range 1000nm Operating Ceiling 30,000ft Fuel Temperature -41°C Operating Speeds (V Speeds) KIAS VMO (maximum operating speed – never exceed this speed) 188 VO (maximum manoeuvring speed – no full/abrupt control movements above this speed) 127 VFE (maximum flap extension speed) 10° 20° 30° 168 135 118 VLO (maximum landing gear operation) Extension Retraction 168 129 VR (rotation speed) 85 VX (best angle of climb) 95 VY (best rate of climb) 110 Vglide 108 VSO (stall speed at maximum take-off weight and 0, 30 and 45 bank angle) Clean (no flaps, gear up)* Landing (flaps 36°, gear down)* 0° 30° 45° 78 68 84 74 93 83 VREF (landing speed - full flaps) 85 VREF (landing speed - no flaps) 100 Maximum demonstrated crosswind velocity 16 *Due to MSFS SDK limitations, the FSR500 will stall at lower speeds than indicated in this table. See ‘Stalls’ in Section 9 for further discussion. FSR500 QUICK REFERENCE HANDBOOK FOR SIMULATION USE ONLY FSR500 CAS MESSAGES CAS Messages FSR500 QUICK REFERENCE HANDBOOK FOR SIMULATION USE ONLY FRONT N-1 BEFORE STARTING ENGINE Passengers .................................................................. BOARD Door ........................................................... CLOSE and LATCH All Electrical Switches....................................................... OFF Cabin climate controls ..................................................... OFF Circuit Breakers ...................................................... All Pushed ECS CABIN COMFORT ....................................................... OFF PARKING BRAKE ................................................................ ON Bleed Air Lever ........................................... PULL OFF (closed) Power Lever .....................................................................IDLE Condition Lever ........................................ CUT-OFF/FEATHER EMER Switch ....................................... ON – check PFD – OFF Nav light ............................................................................ ON Battery switch ................................................................... ON Flaps ......................................................................... RETRACT Fuel Gauges ........................ CHECK QUANTITY & IMBALANCE OAT/Fuel/Oil temps ..................................... VERIFY & CHECK FIRE DET/ANN TEST ..................................... PRESS and HOLD, verify ENGINE FIRE CAS, RELEASE CAS .......................................... CONSIDER ANY ILLUMINATED N-2 AUTO ENGINE START – USING BATTERY Battery Voltage .................................................. 24-26 VOLTS Fuel Pumps ............................................................... MANUAL L & R Fuel Pump ON CAS message ................... ILLUMINATED Ignition Switch ......................................................... MANUAL Ignition ON CAS message ................................. ILLUMINATED Prop area...................................................................... CLEAR Start Mode Switch ........ AUTO (Light in Switch Extinguished) PUSH START switch ...................................... Lift Cover. PUSH Oil pressure .........................................................Check Rising Ng (min. 13%).......................................................... Stabilized Condition Lever ............................................................... RUN ITT ................................................. Max 1000°C, limited to 5s If combustion is not initiated within 10s of moving Condition Lever to Run then: a. Condition Lever ............................... CUT-OFF/FEATHER b. Start Mode Switch ....................... PUSH (ILLUMINATED) c. Allow minimum 30s fuel draining, then refer to DRY MOTORING RUN CHECKLIST N-15 (ON BACK). ITT must ≤150°C before reattempting engine start. Starter @ 56% Ng............................ Verify STARTER off (CAS) If not Press MAN/STOP. Maximum starter run time=30s Ng ............................................................... Stable above 63% Np................................................. Verify 1200RPM Minimum GEN Switch .................... ON. Check Positive Amps & 28 Volts ALT Switch ......................................................................... ON Fuel Pumps Switch ........................................................ AUTO Ignition Switch ................................................................. OFF Oil Pressure .................................... CHECK (Minimum 60 PSI) N-3 BEFORE TAXING AVIONICS Switch ............................................................... ON MFD................................................................ ON (Press ENT) CAS Messages ................................ Consider Any illuminated Autopilot ...........................................................Pre-flight test PITOT Switch .........................................ON, Check Operation PITOT Switch .................................................................... OFF TAXI/REC LT Switch ........................................................... ON Cabin Climate Controls ......................................... As required Radios/Avionics ............................................................ CHECK Flaps .........................................................VERIFY RETRACTED Elevator Trim ........................................ SET TAKE-OFF RANGE Rudder Trim ........................ SET 2-3 Right Trim (Green mark) Bleed Air Lever ..................................................PUSH IN (ON) Cabin Pressure DUMP Switch.......................... Verify Position ECS CABIN COMFORT Switch ................................... NORMAL DEST ELV (LFE in TMR/REF window) ................................. SET STALL WARN Test Switch ................................... Press to Test Altimeters.......................................................................... SET Parking Brake ............................................................ RELEASE N-4 TAXIING Taxi area ....................................................................... CLEAR POWER Lever ........................................... ADVANCE SLOWLY Prop RPM ............................................... Minimum 1200RPM Brakes ........................................................................... CHECK Steering ........................................................................ CHECK USE BETA RANGE AS REQUIRED N-5 ENGINE RUN UP Parking Brake .................................................................... SET Power Lever ............................................................ 1900RPM OVERSPEED GOV TEST Switch ........................Push and HOLD Observe approx. Np drop 60RPM. RELEASE Power Lever .................................................................... IDLE REVERSE LOCK OUT Switch ............................. HOLD (min 5s) POWER LEVER ............................................................RETARD Confirm beta & reverse not available REVERSE LOCK OUT Switch ....... RELEASE (light extinguished) GEN Switch ..................... OFF. Confirm Alternator takes load GEN Switch ........................................................................ ON N-6 BEFORE TAKEOFF Seats, Armrests & Belts ........................ ADJUSTED & LOCKED GEN Switch ........................................................................ ON ALT Switch ......................................................................... ON BLEED AIR Lever .................................................................. IN ECS CABIN COMFORT ................................................... NORM Fuel Temperature ............................... CHECK WITHIN LIMITS FUEL PUMPS Switch ....................................................... MAN IGNITION Switch ............................................................. MAN PITOT HEAT ....................................................................... ON Ice Protection ....................................................AS REQUIRED TAXI/REC LT Switch ...........................................AS REQUIRED LANDING LIGHT ................................................................. ON NAV LIGHT ......................................................................... ON STROBE LIGHT Switch ........................................................ ON Flight Instruments ........................................................ CHECK CAS/PFD ................................................................. CONSIDER Engine Instruments ...................................................... CHECK Radios/Avionics/Transponder .................... SET AS REQUIRED Flaps .....................................................................SET (0°-20°) Elevator & Rudder Trim .................................................... SET Flight Controls ............................................. FREE & CORRECT Timer & HDG bug .......................................... START & SYNCH TURN TO BACK FSR500 NORMAL CHECKLISTS FOR SIMULATION USE ONLY BACK N-7 NORMAL TAKEOFF (0° FLAPS) Brakes ...........................................................................APPLY POWER Lever ............................................... SET TO TAKEOFF Brakes ....................................................................... RELEASE Engine Instruments ................................................ MONITOR Indicated airspeed ......... CALL ‘AIRSPEED ALIVE’ & ’60 knots’ Rotation & Liftoff (Vx) .................................................85 KIAS Obstacle Clearance Speed (OCS) ...............................100 KIAS Positive Rate of climb Landing Gear ........................................ UP, confirm no lights. Yaw Damper ...................................................................... ON Autopilot ........................................................... AS REQUIRED N-8 SHORT FIELD / UNPAVED FIELD TAKEOFF SHORT FIELD: FLAPS 20°, Maintain Vx 85 KIAS & Obstacle Clearance Speed = 95KIAS. UNPAVED FIELD: FLAPS 20° & elevator back. Vx 85 KIAS & OCS 95KIAS. Consider rolling take-off if LFL permits. N-9 MAXIMUM CONTINUOUS POWER CLIMB POWER Lever .................................................................. MCP (Torque, ITT & Ng limits as below) FUEL PUMPS.................................................................. AUTO IGNITION ....................................................................... AUTO LANDING LIGHT ................................................................ OFF TAXI/REC LIGHT ................................................. AS REQUIRED Ice Protection .................................................... AS REQUIRED Engine Instruments a. Torque.......................... MONITOR (1313 ft-lbs max) b. ITT ........................................ MONITOR (770°C max) c. Ng ...................................... MONITOR (101.7% max) Climb speed (best rate) .............................................125 KIAS Transponder ................................................. Verify ALT mode For CRUISE CLIMB use 140KIAS to 20,000ft and 125KIAS to 30,000ft. N-10 CRUISE Cruise Power ................... Set as per power tables in Annex A Engine/Fuel indication ........................................... MONITOR Fuel Temperature/OAT .......................................... MONITOR Cabin climate controls ......................................... AS DESIRED N-11 DESCENT WINDSHLD Heat switch .......................... DEFOG (if required) Ice Protection Equipment ................................. AS REQUIRED POWER lever .................................. SET TO DESIRED TORQUE Altimeters .............................................. SET & CROSS CHECK DEST ELV ...................................................................... CHECK Cabin Climate Controls ..................................... AS REQUIRED N-12 BEFORE LANDING Approach Check Autopilot .................................... DISENGAGE below 100 KIAS FUEL PUMPS................................................................... MAN IGNITION ........................................................................ MAN LANDING LIGHT ................................................................. ON Fuel quantity & Balance ............................................... CHECK Seats, Armrests & Belts .........................ADJUSTED & LOCKED Landing Gear .................................... DOWN (below 168KIAS) Flaps ...................................................... SET (10° @ 168 KIAS) Landing Check Gear indication ......................................................... 3 GREEN Brakes ........................................................................... CHECK Flaps .............................................. SET (36° @ 118 KIAS max) Airspeed ...................................................................... 85KIAS Autopilot .......................................................................... OFF Yaw damper ..................................................................... OFF LANDING POWER lever ................................................... IDLE N-13 AFTER LANDING Timer .............................................................................. STOP FUEL PUMPS .................................................................. AUTO IGNITION .......................................................................... OFF PITOT HEAT ...................................................................... OFF Ice Protection Equipment ................................................ OFF Landing/Taxi lights ............................................AS REQUIRED Strobe Light .......................................................AS REQUIRED WX Radar ........................................................................STBY Flaps ......................................................................... RETRACT Transponder ......................................................AS REQUIRED N-14 SHUTDOWN PARK BRAKE ...................................................................... SET ECS CABIN COMFORT ....................................................... OFF POWER lever ................................................................... IDLE Cabin Climate Controls ..................................................... OFF FUEL PUMPS Switch ......................................................... OFF AVIONICS Switch .............................................................. OFF GEN Switch ....................................................................... OFF ALT Switch ........................................................................ OFF ITT.................................................. Stabilize for 2 mins @ idle CONDITION Lever ..................................... CUT-OFF/FEATHER “FEATHER” CASE Message ..................................... CHECK ON BLEED AIR ........................................................................ OUT Exterior lighting switches ................................................. OFF Fuel Remaining .............................................................. NOTE BATTERY Switch ............................................................... OFF Wheel Chocks, tie downs and covers ................AS REQUIRED N-15 ENGINE DRY MOTORING RUN Allow minimum 30s fuel draining period, then: Power Lever .................................................................... IDLE Condition Lever ........................................ CUT-OFF/FEATHER Fuel Pumps Switch ......................................................... MAN Ignition Switch.................................................................. OFF Battery Switch .................................................................. ON Start Mode Switch .......................................................... MAN Push Start Switch .................................PUSH and HOLD (15s) Push start Switch ....................................................... RELEASE Starter should not be engaged for more than 30s maximum in any circumstances. Do not attempt engine restart until ITT ≤150°C FSR500 EMERGENCY PROCEDURES FOR SIMULATION USE ONLY E-1 ENGINE FAILURE BEFORE ROTATION POWER Lever ....................................................................... IDLE Braking .................................................................. AS REQUIRED Stop straight ahead. If insufficient runway remains for a safe stop: CONDITION Lever ......................................... CUT-OFF/FEATHER BATTERY Switch .................................................................... OFF Firewall FUEL SHUTOFF Valve ................. LIFT COVER - PULL OFF E-2 ENGINE FAILURE IMMEDIATELY AFTER TAKE-OFF Airspeed ........................................................................ 100 KIAS Landing Gear .................................................................... DOWN POWER Lever. ...................................................................... IDLE CONDITION Lever. ........................................ CUT-OFF/FEATHER When landing gear is down and time permits: Flaps........................................................................... DOWN 36° Airspeed .......................................................................... 85 KIAS BATTERY Switch .................................................................... OFF Firewall FUEL SHUTOFF Valve ................. LIFT COVER - PULL OFF E-3 ENGINE FAILURE IN FLIGHT Oxygen .................................................................. AS REQUIRED MIC SEL Switch .................................................................... MSK Airspeed ........................................................................ 108 KIAS POWER Lever. ...................................................................... IDLE CONDITION Lever ......................................... CUT-OFF/FEATHER Propeller ...................................................... VERIFY FEATHERED The battery switch must be ON to feather the propeller. Remaining Fuel ................................................................. CHECK Air Start................. Refer to Air Start procedure in this section. E-4 OIL TEMPERATURE Indication: Master Warning, Triple Chime, Flashing Red Oil Temperature Indication POWER Lever. ................................................... REDUCE POWER If temperature remains high, continue flight at reduced power and land as soon as possible. E-5 OIL PRESSURE Indication: Master Warning, Triple Chime, Flashing Red Oil Pressure Indication Engine Torque at or above 1100 ft-lb: Low Oil Pressure, Below 85 PSI POWER Lever. ........................................ REDUCE TO A MAX. OF 1100 FT - LB OF TORQUE Land as soon as practical. High Oil Pressure, Above 200 PSI: Land as soon as practical. Engine Torque below 1100 ft-lb: Low Oil Pressure, Below 60 PSI Power.................... REDUCE TO MINIMUM TORQUE REQUIRED TO COMPLETE FLIGHT Land as soon as possible. High Oil Pressure, Above 200 PSI Land as soon as possible. E-6 AIR START – STARTER ASSIST Oxygen .....................................................................AS REQUIRED MIC SEL Switch ....................................................................... MSK Autopilot .....................................................................DISENGAGE CONDITION Lever ............................................ CUT-OFF/FEATHER Altitude & Airspeed................ WITHIN THE AIR START ENVELOPE POWER Lever. ......................................................................... IDLE GEN Switch ...............................................................................OFF ALT Switch ................................................................................OFF Electrical Load ...................................................................REDUCE ECS CABIN COMFORT Switch ...................................................OFF BLEED AIR Lever. .............................................. PULL OUT (closed) EMERGENCY PRESSURE Circuit Breaker. ................................ PULL (Located on pilot’s aft circuit breaker panel, row B, position 6) FUEL PUMPS Switch .............................................................. MAN IGNITION Switch ................................................................... MAN To obtain an AUTO air start, the START MODE MAN/STOP switch must not be selected. If the switch is selected to MAN (switch light illuminated), the PUSH START switch must be held ON to keep the starter engaged during the start. START MODE Switch ............................................................ AUTO PUSH START Switch ...................................ENGAGE (Verify START ENGAGED message Illuminated) CONDITION Lever (Ng min. 13%) ........................................... RUN ITT and Ng ..................................................................... MONITOR After Engine Relight - Ng ≥ 63%: GEN Switch ................................................................................ON ALT Switch. ................................................................................ON FUEL PUMPS Switch ............................................................. AUTO IGNITION Switch .................................................................. AUTO EMERGENCY PRESSURE Circuit Breaker ............................... RESET (Located on the pilot’s aft circuit breaker panel, row B, position 6) BLEED AIR Lever. .................................................. PUSH IN (open) ECS CABIN COMFORT Switch .............................................. NORM Electrical Equipment. ...............................................AS REQUIRED FSR500 EMERGENCY PROCEDURES FOR SIMULATION USE ONLY E-7 ENGINE FIRE ON GROUND POWER Lever ....................................................................... IDLE CONDITION Lever ......................................... CUT-OFF/FEATHER Brakes ................................................................... AS REQUIRED Firewall FUEL SHUTOFF Valve ................. LIFT COVER - PULL OFF BLEED AIR Lever. ............................................PULL OUT (closed) ECS CABIN COMFORT Switch ................................................ OFF FUEL PUMPS Switch .............................................................. OFF IGNITION Switch ................................................................... OFF Radio .............................................................. EMERGENCY CALL BATTERY Switch .................................................................... OFF Aircraft ....................................................................... EVACUATE Fire .......................................................................... EXTINGUISH E-8 ENGINE FIRE IN FLIGHT Engine Power ................... REDUCE TO MINIMUM ACCEPTABLE ACCORDING TO FLIGHT SITUATION Oxygen ............................ AS REQUIRED (all aircraft occupants) MIC SEL Switch .................................................................... MSK Confirm that fire exists then: CONDITION Lever ......................................... CUT-OFF/FEATHER Firewall FUEL SHUTOFF Valve ................. LIFT COVER - PULL OFF ECS CABIN COMFORT Switch ................................................ OFF BLEED AIR Lever. ............................................PULL OUT (closed) Conduct a Normal Descent, or Emergency Descent (E-9)-as appropriate and Power Off Landing, (E-11) If pressurized, this procedure will result in an immediate loss of pressurization and cabin altitude will rise at an uncontrolled rate. E-9 EMERGENCY DESCENT, MAXIMUM RATE Autopilot ............................................................................... OFF POWER Lever. ...................................................................... IDLE Landing Gear ......................................... Below 168 KIAS, DOWN WINDSHLD HT Switch ...................................................... DEFOG Smooth air Airspeed after Landing Gear is Fully Extended ............. 168 KIAS Rough air Airspeed ....................................................................... 127 KIAS. E-10 CABIN ALTITUDE ABOVE 12,000FT Master Warning, Triple Chime, CABIN ALT 12K, Red cabin altitude indication. Oxygen Mask ............................................................................ ON MIC SEL Switch ....................................................................... MSK ECS CABIN COMFORT Switch ......................Verify NORM or HIGH BLEED AIR Lever. .................................................. Verify IN (open) If cabin altitude exceeds 14,000 feet: Emergency Descent. .................... ACCOMPLISH PER SECTION E-9 Descend as soon as practical. E-11 POWER-OFF LANDING (ENGINE CUT-OFF/FEATHER) Best Gliding Airspeed is 108 KIAS POWER Lever. ...................................................................... IDLE CONDITION Lever ......................................... CUT-OFF/FEATHER Propeller ...................................................... VERIFY FEATHERED FUEL PUMPS Switch .............................................................. OFF IGNITION Switch ................................................................... OFF Firewall FUEL SHUTOFF Valve .................LIFT COVER - PULL OFF Electrical Load ................................................................ REDUCE ECS CABIN COMFORT Switch ................................................ OFF CABIN PRESSURE DUMP Switch ........................................ DUMP Seats and Seat Backs............. UPRIGHT & LOCKED IN POSITION Seat Belts and Harness ..................................... FASTEN / TIGHT CHECK INERTIA REEL Passengers ......................... BRIEF When committed to landing: Landing Gear .................................................... DOWN; 3 GREEN Flaps ...................................................................... AS REQUIRED If landing site is not suitable for gear down landing: Landing Gear ........................................................ MAINTAIN UP Flaps ........................................................................ FULL DOWN Final Approach Speed ..................................................... 85 KIAS After Touchdown: BATTERY Switch .................................................................... OFF After the aircraft has stopped .................................. EVACUATE. E-12 OVER PRESSURIZATION Indication: Master Warning, Triple Chime, Red cabin differential pressure indication. If cabin differential pressure is above 5.8 psi (or 5.6 psi for greater than 30 sec.): Oxygen Mask ......................................................................... ON MIC SEL Switch ..................................................................... MSK ECS CABIN COMFORT Switch ................................................ OFF BLEED AIR Lever. ........................................... PULL OUT (closed) If over pressurization continues: CABIN PRESSURE DUMP Switch ........................................DUMP Emergency Descent. ................. ACCOMPLISH PER SECTION E-9 E-13 HYDRAULIC FAILURE On Ground: Indication: Master Warning , Triple Chime, LANDING GEAR Selector. ...................................... Verify DOWN In Flight: Indication: Master Caution , Double Chime, HYDR PUMP ON HYDRAULIC PUMP POWER Circuit Breaker ........................ PULL (Located on pilot’s forward circuit breaker panel, row C, position 4) Land as soon as practical and investigate the cause. Prior to landing, the HYDRAULIC PUMP POWER circuit breaker must be reset to extend the landing gear. If the pump continues to run after the gear is locked down, pull the HYDRAULIC PUMP POWER circuit breaker. If the gear fails to extend, refer to the Emergency Landing Gear Extension Procedure E-15 HYDR PUMP ON FSR500 EMERGENCY PROCEDURES FOR SIMULATION USE ONLY E-14 LANDING GEAR FAILURE Indication: Master Caution, Double Chime, GEAR SYS HYDRAULIC PUMP POWER Circuit Breaker. ................. Verify IN (Located on pilot’s forward circuit breaker panel, row C, position 4) BATTERY Switch ...........................................................Verify ON GEN Switch ..................................................................Verify ON ALT Switch ...................................................................Verify ON LANDING GEAR Selector .................................................... CYCLE If issue not resolved ...................... Perform Emergency Landing Gear Extension (E-15) E-15 EMERGENCY LANDING GEAR EXTENSION Indication: One or more of the green gear indications not illuminated. Airspeed ........................................................................ 100 KIAS HYDRAULIC PUMP POWER Circuit Breaker (25 amp). .........PULL (Located on pilot’s forward circuit breaker panel, row C, position 4) LANDING GEAR Selector. ................................................. DOWN Emergency Gear Extension Control .....................................PULL If 3 green gear indications are still not present: Yaw the aircraft left and right to lock the main landing gear. Reduce airspeed to minimum safe speed to improve nose gear locking. If 3 green gear indications are present: ............................ Land If not successful, refer to Gear Up Landing (E-16). E-16 GEAR UP LANDING ECS CABIN COMFORT Switch ................................................ OFF Cabin Pressure DUMP Switch. .......................................... DUMP Passengers ......................................................................... BRIEF Flaps.........................................................................FULL DOWN Final Approach Speed ..................................................... 85 KIAS When Runway is Assured POWER Lever ....................................................................... IDLE CONDITION Lever ......................................... CUT-OFF/FEATHER Firewall FUEL SHUTOFF Valve ................ LIFT COVER – PULL OFF After Touchdown BATTERY Switch .................................................................... OFF After the aircraft has stopped ................................... EVACUATE E-17 FUEL QUANTITY Indication: Master Warning, Triple Chime, FUEL QTY Total fuel quantity is less than 100lbs. Land as soon as possible. Reduce power/fuel flow if possible. Indication: Master Caution, Double Chime, FUEL QTY Total fuel quantity is less than 180lbs, Land as soon as practical. Reduce power/fuel flow if possible. E-18 LOW FUEL PRESSURE Indication: Master Warning, Triple Chime, FUEL PRESS LOW Power............................................................................. REDUCE FUEL PUMPS Switch ............................................................ MAN Fuel Quantity and Balance.......................................... MONITOR If fuel pressure annunciator remains illuminated, land as soon as possible. If fuel pressure annunciator remains illuminated, land as soon as possible. Indication: Master Warning, Triple Chime, FUEL IMBALANCE, Red fuel imbalance indication (>125lbs imbalance) FUEL PUMPS Switch ............................................................ MAN If either white “L FUEL PUMP ON” or “R FUEL PUMP ON” message is NOT illuminated, turn the FUEL PUMPS Switch to OFF. In all cases, Land as soon as possible. FUEL IMBALANCE 40 pounds Indication: Master Warning, Triple Chime, FUEL IMBALANCE, Ambar fuel imbalance indication. FUEL PUMPS Switch ................................................ Verify AUTO Fuel Pump ........................... Verify white L or R FUEL PUMP ON (High Fuel Side) message on MFD Fuel Quantity .............................................................. MONITOR E-20 GENERATOR FAILURE Indication: Master Warning, Triple Chime, GENERATOR FAIL Zero generator amps indication. Electrical Load ............................ REDUCE UNTIL TOTAL LOAD IS BELOW 130 AMPS & VOLTS ANNUNCIATOR IS EXTINGUISHED AIR COND Switch .................................................................. OFF GEN Switch ............................................................ OFF then ON If generator fails to reset: GEN Switch ........................................................................... OFF GENERATOR CONTROL Circuit Breaker..............................RESET (Located on the lower left instrument panel.) GEN Switch ............................................................................ ON If circuit breaker opens again or annunciator stays illuminated with zero amps indicated: GEN Switch ........................................................................... OFF GENERATOR CONTROL Circuit Breaker........................... PULL/ DO NOT RESET Land as soon as practical. E-21 ALTERNATOR FAILURE Indication: Master Warning, Triple Chime, ALTERNATOR FAIL Zero alternator amps indication. ALT Switch.............................................................. OFF then ON If alternator fails to reset: ALT Switch............................................................................. OFF ALTERNATOR FIELD Circuit Breaker. ................................. RESET (Located on pilot’s forward circuit breaker panel, row D, position 7) ALT Switch ......................................................................... ON If circuit breaker opens again or annunciator stays illuminated with zero amps indicated: ALT Switch............................................................................. OFF ALTERNATOR FIELD Circuit Breaker. ............................... PULL/ DO NOT RESET If generator has assumed the load, limit load to under 200 amps and continue flight while avoiding icing conditions. Repair alternator as soon as possible. E-19 FUEL IMBALANCE 43e Fuel Imbalance – 125 pounds or greater FSR500 EMERGENCY PROCEDURES FOR SIMULATION USE ONLY E-22 COMPLETE ELECTRICAL FAILURE Indication: PFDs, MFD and all equipment, excluding the Standby Instrument, will be unpowered. Standby Flight Instrument ................... Verify OPERATIONAL Aircraft Control ............................... Use Standby Instrument EMER Switch ..................................................................... ON BATTERY Switch ............................................................... OFF GEN Switch....................................................................... OFF ALT Switch ........................................................................ OFF AVIONICS Switch .............................................................. OFF CABIN PRESSURE DUMP Switch (prior to landing) ...... DUMP Land as soon as possible. The aircraft will now be on emergency bus power only. Please refer to section 5, ‘Emergency Power’ for a description of what systems will be powered. With a complete electrical failure, emergency landing gear extension and landing without flaps will be required. Refer to Emergency Landing Gear Extension () and Landing Without Flaps (). Torque indication will not be available, therefore engine power should be set using throttle lever position, engine sound, airspeed, and the remaining powerplant indications. During operations on the emergency bus, BETA and reverse are not available. E-23 FLAPS SYSTEM MALFUNTION Indication: Master Warning, Triple Chime, FLAP FAIL FLAP WARN Circuit Breaker ............................. PULL AND RESET VERIFY NORMAL FLAP OPERATION (Located on pilot’s side forward panel, row B, position 4) If FLAP FAIL remains indicated: FLAP MOTOR Circuit Breaker ........................... PULL AND RESET VERIFY NORMAL FLAP OPERATION (Located on pilot’s side forward panel, row B, position 3) TO LAND WITHOUT FLAPS, FOLLOW NORMAL PROCEDURES BUT USE Vref = 100KIAS E-24 DUAL FAILURE ON BOTH GENERATOR & ALTERNATOR Indication: Master Warning, Triple Chine ALTERNATOR FAIL And GENERATOR FAIL Zero Amps indicated on both ammeters. Any time total tie bus voltage is below 25 Vdc while Any time total tie bus voltage is below 25 Vdc while illuminate. GEN Switch ................................................................................ OFF ALT Switch ................................................................................. OFF GENERATOR CONTROL Circuit Breaker ............................... RESET (Located on the lower left instrument panel.) ALTERNATOR FIELD Circuit Breaker .................................. RESET (Located on pilot’s forward circuit breaker panel, row D, position 7) GEN Switch (after OFF at least one second)............................. ON ALT Switch (after OFF at least one second) .............................. ON If only the generator resets: ALT Switch ................................................................................. OFF Continue flight while avoiding icing conditions. If only the alternator resets: GEN Switch ................................................................................ OFF Electrical Load ...........................MAINTAIN LESS THAN 130 AMPS Ammeter ........................................................................ MONITOR Land as soon as practical. If neither the generator nor alternator resets: GEN Switch ................................................................................ OFF ALT Switch ................................................................................. OFF EMER Switch .................................................................. Verify OFF BATTERY Switch .............................................................. Verify ON Electrical Load .............................................REDUCE TO MINIMUM Load-shed procedure (for 30-minutes of battery life) E-25 PROPELLOR SPEED Indication: Master Warning, Triple Chime, Flashing Red Propeller Speed Indication For Prop RPM less than 1200: POWER Lever .................................................... INCREASE POWER For Prop RPM greater than or equal to 2040 for more than 2 seconds: POWER Lever .......................................................REDUCE POWER Airspeed .............................................................................REDUCE Land as soon as practical. For Prop RPM greater than or equal to 2080 continuously: POWER Lever ...........................................REDUCE AS NECESSARY Airspeed .................................... REDUCE TO LOWEST PRACTICAL Land as soon as possible. Should heavy vibration or uncontrolled propeller speed occur, be prepared to shut down the engine. CONDITION Lever ............................................ CUT-OFF/FEATHER Conduct a Normal Descent, or Emergency descent (E-9) as appropriate and Power Off Landing (E-11). NOTE

All Piper M500 emergency procedures