Electronic Pilot’s Checklist

* 8 Revised 7 AJ * 8.1 Added 7 AK * 9 thru 11 Revised 7 AA 12 thru 14 Revised 5 AA 15 thru 19 Revised 6 AH 15.1 thru 19.1 Added 6 AI 20 Revised 5 AA 21 thru 25 Revised 6 AH 21.1 thru 25.1 Added 6 AI 26 thru 37 Revised 5 AA * 38 Revised 7 AA 39 Revised 5 AA * 40 Revised 7 AA 41 thru 47 Revised 5 AA 48 Revised 6 AF 48.1 Revised 6 AG 49 thru 56 Revised 5 AA 57 thru 58 Revised 6 AA * 59 Revised 7 AJ * 59.1 Added 7 AK * 60 Revised 7 AA iii 510CLNP-07 AA For Training Purposes Only MODEL 510 TEMPORARY CHANGES Trim to 5.75 x 11 inches 510CLNP NOTE: The accompanying (attached) FAA Approved Temporary Change page(s) may or may not be applicable to your serial aircraft. Please refer to the individual FAA Approved Temporary Change page(s) to determine applicability status for your aircraft. For Training Purposes Only TEMPORARY CHANGES MODEL 510 Trim to 5.75 x 11 inches FAA Approved U.S. Pilots’ Abbreviated Checklist Model 510 Citation Mustang Airplanes 510-0001 and On THIS IS A LIST OF ALL CURRENT TEMPORARY CHANGES. The following list of temporary changes should be incorporated into this FAA Approved Pilots’ Abbreviated Checklist until the removal instructions have been complied with. Insert this page opposite the Log of Effective Pages in the front of this FAA Approved Pilots’ Abbreviated Checklist. A bar located in the margin on the left side of the page, adjacent to the list, will extend the full length of any change. No change bars will be used in the footers or elsewhere. The date in the footer(s) reflects only the issue date of the most recent temporary change(s) listed on that page. . TEMPORARY CHANGE NUMBER PAGE NUMBER ISSUE DATE SERVICE BULLETIN (IF APPLICABLE) OR SERIAL EFFECTIVITY 510CLNP TC-R07-01 9 5/29/09 Airplanes 510-0001 and On 510CLNP TC-R07-02 59 or 59.1 5/29/09 Airplanes 510-0001 and On 510CLNP TC-R07-03 40 9/25/09 Airplanes 510-0001 and On 510CLNP TC-R07-04 v/vi 10/28/09 Airplanes 510-0001 and On 510CLNP TC-R07-05 12 4/29/13 Airplanes 510-0001 and On 510CLNP i U.S. 29 April 2013 For Training Purposes Only Configuration INTRODUCTION MODEL 510 CHECKLIST PART NUMBER Each page in this checklist contains the part number of the checklist and the page status of each page. Refer to the following example: CONFIGURATION CODES The following is a list of configuration codes which appear at the bottom of each page of the Pilots’ Abbreviated Checklist and indicate page effectivity by serial number. Pages marked AA apply to all airplanes of this model. This list contains only the configurations which have been incorporated into this checklist. Each page of the checklist is provided with a configuration code. In the event that a page is applicable to only a select number of airplanes, at least two (2) pages will be provided, one with a regular page number (e.g., 15), and one with a point page number (e.g., 15.1). The operator must then check the configuration code list in the front of the checklist to determine which page applies to his/her airplane. In some cases, multiple pages may be provided to allow for all configurations. This system allows for a “custom” checklist for each individual aircraft and therefore eliminates material that does not apply to the operator’s airplane from the checklist. The page(s) that does(do) not apply to the airplane must be discarded. From each grouping, identify and record the configuration code that applies to your airplane, then select and insert the correct pages into this checklist. (Continued Next Page) Basic Checklist 510 CLNP 07 Page Status (Revised) Checklist Normal Procedures Airplane Model (Model 510) CONFIGURATION CODE EFFECTIVITY BY SERIAL NUMBER APPLICABLE CODES AA Airplanes 510-0001 and On. AF Airplanes 510-0041 and On (Airplanes with Multi-Function Change and Cabin Altitude Module Improvement) AG Airplanes 510-0001 thru -0040 (Airplanes without Multi-Function Change and Cabin Altitude Module Improvement) AH Airplanes 510-0001 thru -0065 incorporating SB510-34-02 (Garmin G1000 2008 Q1 Software/Hardware update) and Airplanes 510-0066 and On. AI Airplanes 510-0001 thru -0065 not incorporating SB510-34-02 (Garmin G1000 2008 Q1 Software/Hardware Update) AA 510CLNP-07 iv For Training Purposes Only TEMPORARY PILOTS’ ABBREVIATED CHECKLIST CHANGE Trim to 5.75 x 11 inches In the Normal Procedures checklist, page v/vi, Configuration Codes, change the serial effectivity of configuration codes AJ and AK as follows: Publication Affected: Model 510 Citation Mustang (510-0001 and On) Pilots’ Abbreviated Checklist Normal Procedures, Revision 7, dated 21 November 2008. Airplane Serial Nos. Affected: Airplanes 510-0001 and On. Description of Change: This temporary change is current with 510FM TC-R07-12 and reflects the following change to the AFM, Section I, Introduction, change the serial effectivity for a configuration set. Filing Instructions: Insert this temporary change in the Model 510 (510-0001 and On) Pilots’ Abbreviated Checklist, Normal Procedures, adjacent to page v/vi. Removal Instructions: This temporary change must be removed and discarded when Revision 8 has been collated into the Pilots’ Abbreviated Checklist Normal Procedures. CONFIGURATION CODE EFFECTIVITY BY SERIAL NUMBER APPLICABLE CODES AJ Airplanes 510-0001 thru -0177 incorporating SB510-34-09 and Airplanes 510-0178 and On. AK Airplanes 510-0001 thru -0177 not incorporating SB510-34-09. 510CLNP TC-R07-04For Training Purposes Only Configuration MODEL 510 INTRODUCTION CONFIGURATION CODES (Continued) CONFIGURATION CODE EFFECTIVITY BY SERIAL NUMBER APPLICABLE CODES AJ Airplanes 510-0001 thru -0152 incorporating SB510-34-09 Navigation - Garmin G1000 Software Version 010-00435-13 Upgrade and Airplanes 510-0153 and On. AK Airplanes 510-0001 thru -0152 not incorporating SB510-34-09 Navigation - Garmin G1000 Software Version 010-00435-13 Upgrade. AA v/vi 510CLNP-07 For Training Purposes Only Configuration MODEL 510 NORMAL PROCEDURES NORMAL PROCEDURES TABLE OF CONTENTS PAGE PREFLIGHT INSPECTION Preliminary Exterior Inspection - - - - - - - - - - - - - - - - - - - - - - - - - 3 Cockpit/Cabin Inspection - - - - - - - - - - - - - - - - - - - - - - - - - - - - - 3 Exterior Inspection - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - 4 Cockpit Preparation - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - 7 Delay Before Flight Without GPU - - - - - - - - - - - - - - - - - - - - - - - 8 BEFORE START/START Before Starting Engines - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - 9 Starting Engines - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - 9 TAXI Before Taxi- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - 10 Taxi - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - 12 Takeoff Performance - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - 14 TAKEOFF/CLIMB/CRUISE Before Takeoff - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - 38 Takeoff - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - 39 After Takeoff - Climb - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - 39 CRUISE/DESCENT/LANDING Cruise - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - 39 Descent - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - 39 Approach - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - 40 Before Landing - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - 40 Landing - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - 41 All Engines Go-Around - - - - - - - - - - - - - - - - - - - - - - - - - - - - - 41 Landing Performance - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - 42 AFTER LANDING/SHUTDOWN After Landing - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - 46 Shutdown - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - 46 Quick Turn Around - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - 47 Turbulent Air Penetration - - - - - - - - - - - - - - - - - - - - - - - - - - - 47 MISCELLANEOUS Warning Systems Test- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - 48 Anti-Ice Flow Schematic - - - - - - - - - - - - - - - - - - - - - - - - - - - - 49 Fuel Schematic- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - 50 Air Conditioning Schematic - - - - - - - - - - - - - - - - - - - - - - - - - - 51 Pilot (LH) Circuit Breaker Panel - - - - - - - - - - - - - - - - - - - - - - - 52 Copilot (RH) Circuit Breaker Panel - - - - - - - - - - - - - - - - - - - - - 53 Electric Flow Schematic - - - - - - - - - - - - - - - - - - - - - - - - - - - - 54 Hydraulic Schematic - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - 55 Landing Gear Schematic - - - - - - - - - - - - - - - - - - - - - - - - - - - - 56 Antenna Configuration- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - 57 Quick Reference Checklist- - - - - - - - - - - - - - - - - - - - - - - - - - - 59 1 510CLNP-06 AA For Training Purposes Only Configuration NORMAL PROCEDURES MODEL 510 PILOT NOTES 510CLNP-00 2 AA For Training Purposes Only Configuration MODEL 510 NORMAL PROCEDURES PREFLIGHT INSPECTION PRELIMINARY EXTERIOR INSPECTION 1. Battery - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - CONNECTED 2. Engine Covers (4) - - - - - - - - - - - - - - - - - - - - - - - - - REMOVED 3. Pitot Covers (2) - - - - - - - - - - - - - - - - - - - - - - - - - - - REMOVED 4. Static Wick Covers - - - - - - - - - - - - - - - - - - - - - - - - - REMOVED 5. Ground Power Unit- - - - - - - - - - - - - - - - - - - NOT CONNECTED COCKPIT / CABIN INSPECTION 1. Documents, Manuals, and Charts - - - - - - - - - CHECK ABOARD a. To be displayed in the airplane at all times: (1) Airworthiness and Registration Certificates. (2) Transmitter License(s) (as required). To be carried in the airplane at all times: (1) FAA Approved Airplane Flight Manual. (2) GARMIN G1000 Avionics Cockpit Reference Guide. (3) Other applicable pilot's manuals as required in Section III, Operating Limitations or applicable AFM Supplement. 2. Required Equipment- - - - - - - - - - - - ONBOARD and SERVICED 3. Cabin - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - CHECK a. Emergency Exit - - - - - - - - - - - -SECURE/CLEAR/LOCK PIN REMOVED/COVER IN PLACE b. Passenger Seats - - - - - - - - - - - - - - - UPRIGHT/CONDITION c. Exit Placards - - - - - - - - - - - - - - - - - - - - - - - - - - - - SECURE d. Door Entry Lights - - - - - - - - - - - - - - - - - - - - - - - - - - - - OFF 4. Portable Fire Extinguisher - - - - - - - - - - SERVICED and SECURE 5. Gust Lock - - - - - - - - - - - - - - - - - - - - - - - - REMOVE and STOW 6. Circuit Breakers - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - IN 7. LANDING GEAR Handle- - - - - - - - - - - - - - - - - - - - - - - - -DOWN 8. ANTISKID Switch - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - ON 9. All Other Switches - - - - - - - - - - - - - - - - - - - - - - - OFF or NORM 10. Elevator Trim - - - - - - - - - - - - - - - - - - - - - - - - - - - - CHECK/SET (trim indicator within TO trim range) 11. THROTTLES - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - CUTOFF 12. EMERGENCY GEAR RELEASE Handle - - - - - - - STOWED and COVER INSTALLED 13. BATTERY DISCONNECT Switch- - - - - - - - - - - - - DISCONNECT 14. BATT Switch - - - - - - - - - - - - - - - - -BATT (ALL DISPLAYS OFF) 15. BATTERY DISCONNECT Switch- - - - -NORMAL/COVER DOWN (PFD 1/2 and MFD powered) 16. Ground Power Unit (if desired)- - - - - - - - - - - - - - - CONNECTED 17. PARKING BRAKE - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -SET 18. Pitot-Static Switch - - - - - - - - PITOT STATIC (30 seconds); OFF 19. LANDING Light Switch - - - - - - - - - - - - - - - - - - - - - - - - - - - - ON (Check illumination; OFF, if seen from cockpit) 20. Other EXTERNAL LIGHTING Switches - - - - - - - - - - - - - - - - ON (Check illumination; OFF, if seen from cockpit) (Continued Next Page) 3 510CLNP-05 AA PREFLIGHT INSPECTION For Training Purposes Only Configuration NORMAL PROCEDURES MODEL 510 COCKPIT / CABIN INSPECTION (Continued) 21. PAX SAFETY Switch - - - PAX SAFETY (Check illumination); OFF 22. LANDING GEAR Position Lights - - THREE GREEN LIGHTS / NO RED LIGHT 23. Database/Chart Currency - - - - - - - - - - - - - - - - - - - - - - - CHECK 24. Fuel Quantity and Balance - - - - - - - - - - - - - - - - - - - - - - CHECK 25. FLAP Handle - - - AGREES WITH FLAP POSITION INDICATOR 26. AILERON and RUDDER TRIM - - - - - - - - - - - - - - - -CHECK/SET EXTERIOR INSPECTION During inspection, make a general check for security, condition, and cleanliness of the airplane and components. Check particularly for damage; fuel, oil, and hydraulic fluid leakage; security of access panels; and removal of keys from locks. WARNING PITOT TUBES AND STALL WARNING VANE MAY STILL BE HOT. 1. Hot Items/Lights - - - - - - - - - - - - - - - - - - - - - - - - - - - - - CHECK a. Left and Right Static Ports (4) - - - - - - - - CLEAR and WARM b. Left and Right Pitot Tubes (2) - - - - - - - - - - CLEAR and HOT c. Stall Warning Vane - - - - - - - - - - - - - - -CONDITION and HOT d. LANDING Lights - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -ON (if not observed from cockpit) e. BEACON Light - - - - - - - - - - - - - - - - - - ON and FLASHING (if not observed from cockpit) f. Right NAV and ANTI-COLLISION Lights- - - - - - - - - - - - - -ON (if not observed from cockpit) g. Left WING INSP, NAV and ANTI-COLLISION Lights - - - - -ON (if not observed from cockpit) 2. EXTERNAL LIGHTING Switches - - - - - - - - - - - - - - - - - - - - OFF 3. BATT Switch - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - OFF 4. Left Nose - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - CHECK a. Static Ports (2) and Surrounding Fuselage Skin- - - - - CLEAR and NO DAMAGE b. OAT Probe Inlet and Sensors (2) - - - - - - - - - - - - - - - CLEAR and NO DAMAGE c. Accumulator Bleed Valve - - - OPEN; BLEED DOWN; CLOSE d. Hydraulic ACCUMULATOR PRECHARGE Pressure Gauge- - CHECK (per placard) e. HYDRAULIC RESERVOIR - - - - - - - - CHECK FLUID LEVEL f. Baggage Door - - - - - - - - - - - - - - - - -SECURE and LOCKED g. Nose Gear, Doors, Wheel, Tire, and Strut - - - - - - CONDITION h. Overboard Vent Line - - - - - - - - - - - - - - - - - - - - - - - CLEAR (Continued Next Page) 510CLNP-07 4 AA For Training Purposes Only Configuration MODEL 510 NORMAL PROCEDURES EXTERIOR INSPECTION (Continued) 5. Right Nose and Fuselage Right Side - - - - - - - - - - - - - - - CHECK a. AUX BRAKE Pneumatic Pressure Gauge - - - - - - - - - CHECK (per placard) b. AUX GEAR Pneumatic Pressure Gauge - - - - - - - - - - CHECK (per placard) c. Nose Compartment Light- - - - - - - - - - - - - - - - - - - - - - - OFF d. Baggage Door - - - - - - - - - - - - - - - - SECURE and LOCKED e. Oxygen Blowout Disc - - - - - - - - - - - - - - - - - - - - - - - GREEN f. Fresh Air Inlet- - - - - - - - - - - - - - - - - - - - - - - - - - - - - CLEAR g. Overboard Vent and Drain Lines - - - - - - - - - - - - - - - CLEAR h. Stall Warning Vane - - - - - - - - - - - - - - - - ROTATES FREELY i. Static Ports (2) and Surrounding Fuselage Skin - - CLEAN and NO DAMAGE j. Landing Light - - - - - - - - - - - - - - - - - - - - - - - - - -CONDITION k. Top and Bottom Antennas - - - - - - - - - - - - - - - - -CONDITION 6. Right Wing- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - CHECK a. Fuel Quick Drains (4) - - - - - - - - - - DRAIN and CHECK FOR CONTAMINATION b. Main Gear Door, Wheel, Tire, and Strut - - - - - - - -CONDITION c. Emergency Exit - - - - - - - - - - - - - - - - - - - - - - - - - - SECURE d. Wing Deice Boot- - - - - - - - - - - - - - - - - - - - - - - -CONDITION e. Stall Strip - - - - - - - - - - - - - - - - - - - - - - - - - - - - -CONDITION f. Vortex Generators (8 per wing) - - - - - - - - - - - - -CONDITION g. Fuel Filler Cap - - - - - - - - - - - - - - - - - - - - - - - - - - - SECURE h. Fuel Tank Vent - - - - - - - - - - - - - - - - - - - - - - - - - - - - CLEAR i. Static Wicks - - - - - - - - CHECK (3 installed. 1 may be missing. No more than 2 total missing on entire airplane) j. Aileron, Flap, and Speed Brakes - - - - - - - - - - - -CONDITION (Make sure flap position matches indicator.) 7. Right Engine/Nacelle - - - - - - - - - - - - - - - - - - - - - - - - - - CHECK a. Engine Air Inlet- - - - - - - - - - - - - - - - - - - - - - - - - - - - CLEAR b. Engine Fan Duct and Fan - - - - - - - - - - - - - - - - - - - - CHECK (for bent blades, nicks and blockage of fan stators) c. Engine T2 Probe - - - - - - - - - - - - - - - - - - - - - - -CONDITION d. Pylon Precooler Inlet - - - - - - - - - - - - - - - - - - - - - - - - CLEAR e. Generator Cooling Air Inlet - - - - - - - - - - - - - - - - - - - CLEAR f. Engine Anti-Ice Exhaust - - - - - - - - - - - - - - - - - - - - - CLEAR g. Generator Cooling Air Exhaust- - - - - - - - - - - - - - - - - CLEAR h. Engine Fluid Drains - - - - - - - - - - - - - - - - - - - - - - - - CLEAR i. Oil Filter Differential Pressure Indicator - - - - NOT EXTENDED j. Oil Level - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - CHECK k. Filler Cap and Access Door - - - - - - - - - - - - - - - - - - SECURE l. Engine Exhaust and Bypass Duct- - CONDITION and CLEAR m. Pylon Precooler Exhaust - - - - - - - - - - - - - - - - - - - - - CLEAR (Continued Next Page) 5 510CLNP-05 AA For Training Purposes Only Configuration NORMAL PROCEDURES MODEL 510 EXTERIOR INSPECTION (Continued) 8. Empennage/Aft Fuselage - - - - - - - - - - - - - - - - - - - - - - - CHECK a. Ground Power Service Door - - - - - - - - - - - - - - - - - SECURE b. Air Conditioning Inlet and Exhaust - - - - - - - - - - - - - - CLEAR c. Fairing Vent (bottom of aft fuselage on right side) - - - CLEAR d. Overboard Drains/Vents - - - - - - - - - - - - - - - - - - - - - CLEAR e. FADEC STATIC PORTS (L and R) - - - - - - - - - - - - - - CLEAR f. Tail Strakes - - - - - - - - - - - - - - - - - - - - - - - - - - - CONDITION g. Tailcone Air Inlets- - - - - - - - - - - - - - - - - - - - - - - - - - CLEAR h. Right Horizontal Stabilizer Deice Boot - - - - - - - - CONDITION i. Vertical Stabilizer Deice Boot- - - - - - - - - - - - - - - CONDITION j. Right Horizontal Stabilizer, Elevator, and Trim Tab - - - - - - - - - - - - - - - - - - - - - - - - - - CONDITION (Make sure trim tab position matches indicator.) k. Rudder and Trim Tab - - - - - - - - - - - - - - - - - - - - - - SECURE (Make sure trim tab position matches indicator.) l. Static Wicks (Rudder, Both Elevators, and Tailcone)- - CHECK (10 installed. 1 may be missing from either elevator and 1 may be missing from Rudder or Tailcone. No more than 2 total missing on entire airplane) m. Left Horizontal Stabilizer, Elevator, and Trim Tab - - - - - - - - - - - - - - - - - - - - - - - - - - - - - CONDITION (Make sure trim tab position matches indicator.) n. Left Horizontal Stabilizer Deice Boot - - - - - - - - - CONDITION o. Rudder Gust Lock - - - - - - - - - - - - - - - - - - - - - DISENGAGE 9. Left Engine/Nacelle - - - - - - - - - - - - - - - - - - - - - - - - - - - CHECK a. Pylon Precooler Exhaust- - - - - - - - - - - - - - - - - - - - - CLEAR b. Engine Exhaust and Bypass Duct - CONDITION and CLEAR c. Oil Level - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - CHECK d. Filler Cap and Access Door- - - - - - - - - - - - - - - - - - SECURE e. Engine Fluid Drains - - - - - - - - - - - - - - - - - - - - - - - - CLEAR f. Generator Cooling Air Exhaust - - - - - - - - - - - - - - - - CLEAR g. Engine Anti-Ice Exhaust - - - - - - - - - - - - - - - - - - - - - CLEAR h. Generator Cooling Air Inlet - - - - - - - - - - - - - - - - - - - CLEAR i. EngineT2 Probe- - - - - - - - - - - - - - - - - - - - - - - - CONDITION j. Engine Air Inlet - - - - - - - - - - - - - - - - - - - - - - - - - - - CLEAR k. Engine Fan Duct and Fan - - - - - - - - - - - - - - - - - - - - CHECK (for bent blades, nicks and blockage of fan stators) l. Pylon Precooler Inlet - - - - - - - - - - - - - - - - - - - - - - - CLEAR m. Oil Filter Differential Pressure Indicator - - - NOT EXTENDED 10. Aft Compartment - - - - - - - - - - - - - - - - - - - - - - - - - - - - - CHECK a. Fire Bottle Pressure Gauge - - - - - - - - - - -CHECK per placard b. Junction Box Circuit Breakers - - - - - - - - - - - - - - - - - - - - - IN c. Equipment and Junction Box Access Doors - - - - - - SECURE d. Aft Compartment Baggage - - - - - - - - - - - - - - - - - - SECURE e. Aft Compartment Light - - - - - - - - - - - - - - - - - - - - - - - - - OFF f. Aft Compartment Access Door - - - - -SECURE and LOCKED (Continued Next Page) 510CLNP-06 6 AA For Training Purposes Only Configuration MODEL 510 NORMAL PROCEDURES EXTERIOR INSPECTION (Continued) 11. Left Wing- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - CHECK a. Flap, Speed Brakes, Aileron, and Trim Tab - - - - -CONDITION (Make sure flap position and trim tab matches indicators) b. Static Wicks - - - - - - - - CHECK (3 installed. 1 may be missing. No more than 2 total missing on entire airplane) c. Fuel Tank Vent - - - - - - - - - - - - - - - - - - - - - - - - - - - - CLEAR d. Fuel Filler Cap - - - - - - - - - - - - - - - - - - - - - - - - - - - SECURE e. Wing Deice Boot- - - - - - - - - - - - - - - - - - - - - - - -CONDITION f. Vortex Generators (8 per wing) - - - - - - - - - - - - -CONDITION g. Stall Strip - - - - - - - - - - - - - - - - - - - - - - - - - - - - -CONDITION h. Main Gear Door, Wheel, Tire, and Strut - - - - - - - -CONDITION i. Fuel Quick Drains (4) - - - - - - - - - - DRAIN and CHECK FOR CONTAMINATION 12. Fuselage Left Side - - - - - - - - - - - - - - - - - - - - - - - - - - - - CHECK a. Wing Inspection Light - - - - - - - - - - - - - - - - - - - -CONDITION b. Landing Light - - - - - - - - - - - - - - - - - - - - - - - - - -CONDITION c. Cabin Door Seal - - - - - - - - - - - CHECK for RIPS and TEARS COCKPIT PREPARATION 1. BATTERY DISCONNECT Switch- - - - - - - NORM/COVER DOWN 2. INTERIOR DISCONNECT Switch - - - - - - - - - - - - - - - - - - NORM 3. Circuit Breakers - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - IN 4. STBY INST Switch - - - - - - - - - - - - - - - BATT TEST (5 seconds); GREEN LIGHT ON 5. STBY INST Switch - - - - - - - - - - STBY INST; AMBER LIGHT ON 6. If Ground Power Unit is connected (for battery power only, skip to Step 7): a. BATT Switch - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - ON b. AVN PWR Switch - - - - - - - - - - - - - - - - - - - - - - - - - - - - - ON c. BATTERY VOLTAGE - - - - - - - - - - - - - - - - - - - -CHECK 28V d. COCKPIT/CABIN FAN Knobs - - - - - - - - - - - - - AS DESIRED e. AIR COND Switch - - - - - - - - - - - - - - - - - - - - - AS DESIRED 7. Cockpit Switches and Controls - - - - - - - - - - - - - - - - - - - - - -SET a. OXYGEN CONTROL VALVE - - - - - - - - - - - - - - - - -NORMAL b. L/R GEN Switches - - - - - - - - - - - - - - - GEN (for battery start) OFF (for GPU start) c. L/R IGNITION Switches - - - - - - - - - - - - - - - - - - - - - - NORM d. L/R FUEL BOOST Switches - - - - - - - - - - - - - - - - - - - NORM e. FUEL TRANSFER Knob - - - - - - - - - - - - - - - - - - - - - - - OFF f. Pilot MIC Switch - - - - - - - - - - - - - - - - - - - - - - - - - HEADSET g. ICE PROTECTION Switches - - - - - - - - - - - - - - - - - - - - OFF h. LANDING GEAR Handle - - - - - - - - - - - - - - - - - - - - - -DOWN i. ANTISKID Switch - - - - - - - - - - - - - - - - - - - - - - - - - - - - - ON j. PAX SAFETY Switch- - - - - - - - - - - - - - - - - - - - - - - - - - OFF k. EXTERNAL LIGHTING Switches - - - - - - - - - AS REQUIRED l. COCKPIT/CABIN TEMP Knobs - - - - - - - - - - - - AS DESIRED m. AIR SOURCE SELECT Knob- - - - - - - - - - - - - - - - - - - BOTH n. PRESS CONT Switch - - - - - - - - - - - - - - - - - - - - - - - - NORM (Continued Next Page) 7 510CLNP-07 AA For Training Purposes Only Configuration NORMAL PROCEDURES MODEL 510 COCKPIT PREPARATION (Continued) o. CABIN DUMP Switch - - - - - - - - - - - - - - - - - - - - - - - - NORM p. Copilot MIC Switch- - - - - - - - - - - - - - - - - - - - - - - HEADSET q. ELT Switch - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - ARM r. OXYGEN SUPPLY Handle - - - - - - - - - - - - - - - - PUSHED IN s. THROTTLES- - - - - - - - - - - - - - - - - - - - - - - - - - - - CUTOFF t. ENGINE SYNC Switch - - - - - - - - - - - - - - - - - - - - - - - NORM u. EMERGENCY GEAR RELEASE Handle - - - - - - - - STOWED 8. BATT Switch - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - EMER; CHECK POWER TO EMERGENCY BUS ITEMS 9. BATT Switch - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - BATT 10. STBY INST Amber Light- - - - - - - - - - - - - - - - - - - - - - - - - - - OFF 11. PARKING BRAKE - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - SET 12. LANDING GEAR Position Lights - - - - - THREE GREEN LIGHTS/ NO RED LIGHT 13. Cockpit Lighting- - - - - - - - - - - - - - - - - - - - - - - - - AS REQUIRED 14. AVN PWR Switch - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -ON 15. Database/Chart Currency - - - - - - - - - - - - - - - - - - - - - - - CHECK 16. Rotary TEST Switch- - - - - - - - - - -WARNING SYSTEMS CHECK 17. Oxygen System- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - CHECK a. Oxygen Pressure - - - - - - - - - - - - - - - - - - - 1600 to 1800 PSI b. L and R MIC Switches - - - - - - - - - - - - - - - - OXYGEN MASK c. Pilot and Copilot Masks - - - - - - - - - - TEST/100%/AUDIBLE IN SPEAKER/STOWED d. L and R MIC Switches - - - - - - - - - - - - - - - - - - - - HEADSET e. Smoke Goggles (if installed) - - - - - - - - - - - - - - - - - STOWED 18. Fuel Quantity and Balance - - - - - - - - - - - - - - - - - - - - - - CHECK 19. Pilot, Passenger, Cargo and Fuel Weights - - - - - - - ENTER (MFD AUX-WEIGHT PLANNING Page) 20. ATIS/Clearance - - - - - - - - - - - - - - - - - - - - - - - - - AS REQUIRED 21. Avionics Flight Plan (if desired) - - - - - - - - - - - - - - - - - - - ENTER 22. AVN PWR Switch - - - - - - - - - - - - - - - - - - - - -ON (for GPU start) OFF (for battery start) 23. Wing/Stab Deice System (if required)- - - - - - - - - - - - - - - CHECK a. WING/STAB Deice Switch - - - - - - - - - - - HOLD in MANUAL b. Verify WING DE-ICE and TAIL DE-ICE FAIL messages display after 6 seconds. c. WING/STAB Deice Switch - - - - - - - - - - - - - - - - - - - - - - OFF d. Pitot-Static Switch - - - - - - - RESET STALL WARN then OFF DELAY BEFORE FLIGHT WITHOUT GPU 1. STBY INST Switch- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - OFF 2. BATT Switch - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - OFF 510CLNP-07 8 AJ For Training Purposes Only TEMPORARY PILOTS’ ABBREVIATED CHECKLIST CHANGE Trim to 5.75 x 11 inches In the Normal Procedures Checklist, page 9, Starting Engines procedure, add a Caution after Step 4 and change Step 5 as shown below: STARTING ENGINES 4. Engine Instruments. . . . . . . . . . . . . . . . . . CHECK NORMAL (battery current less than 100 Amps) CAUTION CAUTION If the operating generator drops off-line during a cross-generator start (GEN OFF L-R), an ENG CTRL SYS L or R CAS message posts, or ITT indication is lost at any time during the start sequence, abort the start immediately by bringing the throttle to CUTOFF to reduce the possibility of a hot or hung engine start. 5. Operating Engine N2 . . . . INCREASE to 10% above ground idle N2 (for a cross-generator start) Publication Affected: Model 510 Citation Mustang (510-0001 and On) Pilots’ Abbreviated Checklist, Normal Procedures, Revision 7, dated 21 November 2008. Airplane Serial Nos. Affected: Airplanes 510-0001 and On. Description of Change: This temporary change is current with 510FM TC-R07-07 and reflects the following change to the AFM, Section III, Operating Procedures, Normal Procedures, Starting Engines Checklist, add a Caution and change a step. Filing Instructions: Insert this temporary change in the Model 510 (510-0001 and On) Pilots’ Abbreviated Checklist Normal Procedures adjacent to page 9. Removal Instructions: This temporary change must be removed and discarded when Revision 8 has been collated into the Pilots’ Abbreviated Checklist Normal Procedures. 510CLNP TC-R07-01For Training Purposes Only Configuration MODEL 510 NORMAL PROCEDURES BEFORE STARTING ENGINES 1. If delayed before flight without GPU: a. STBY INST Switch - - - - - - - - - - - - - - - - - - - - - - STBY INST b. BATT Switch - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - BATT 2. Preflight Inspection- - - - - - - - - - - - - - - - - - - - - - - - -COMPLETE 3. Wheel Chocks - - - - - - - - - - - - - - - - - - - - - - - - - - - - REMOVED 4. Cabin Door - - - - - CLOSED. Check indicators for proper door pin position, no CABIN DOOR message displayed, and handle latched. 5. Passenger Briefing - - - - - - - - - - - - - - - - - - - - - - - - -COMPLETE (include seat/seat belt adjustment, emergency exits, smoking, and emergency use of oxygen) 6. Seats and Seat Belts - - - - - - - - - - - - - - - ADJUST and SECURE 7. EXTERNAL LIGHTING Switches - - - - - - - - - - - - AS REQUIRED 8. AIR COND Switch - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - OFF 9. COCKPIT/CABIN FAN Knobs - - - - - - - - - - - - - - - - - - - - - - OFF 10. EICAS- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - CHECK 11. BATTERY VOLTAGE - - - - - - - - - - - - - - - - - - - - - - - - - - CHECK STARTING ENGINES 1. ENGINE START Button - - - - - - - - - - - - PRESS MOMENTARILY (verify button illuminates) 2. THROTTLE - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - IDLE 3. Engine Instruments - - - - - - - - - - - - - - - - - - - - - - - - - MONITOR a. N1 - - - - - - - - - - - - - - Abort start if no N1 indication by 40% N 2 b. ITT - - - - - - - - - - - - - - - - - - - - - - - - - - - - CHECK FOR RISE Abort start if ITT rapidly approaches 830°C or shows no rise within 10 seconds. Do not exceed 830°C for more than 5 seconds, limit 862°C. c. Oil Pressure - - - - - - - - - - - - - - - - - - - - STEADY INCREASE d. Engine must reach stabilized idle within 45 seconds. e. N2 display digits will change from WHITE to GREEN when FADEC start sequence is completed 4. Engine Instruments - - - - - - - - - - - - - - - - - - - CHECK NORMAL (Battery Current less than 100 amps) 5. Operating Engine N 2 - - - - - - - - - - - - - - - - - - INCREASE to 55% (for a cross-generator start) 6. Other Engine - - - - - - - - - - - - - START; repeat steps 1 through 4 7. Ground Power Unit- - - - - - - - - - - - - DISCONNECT (if applicable) 8. L/R GEN Switches - - - - - - - - - - GEN (if ground power was used) 9. AVN PWR Switch - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - ON (Continued Next Page) 9 510CLNP-07 AA BEFORE START/ START For Training Purposes Only Configuration NORMAL PROCEDURES MODEL 510 STARTING ENGINES (Continued) 10. DC AMPS/VOLTS - - - - - - - - - - - - - - - - - - - - - - - - - - - - CHECK a. L GEN Switch - - - - - - - - - - - - - - - - - OFF (L AMP decrease, R AMP increase, battery voltage 28 Volts.) b. L GEN Switch - - - - - - - - - - - - - - - - GEN (L AMPS increase, battery voltage 28 Volts.) c. R GEN Switch - - - - - - - - - - - - - - - - - OFF (R AMP decrease, L AMP increase, battery voltage 28 Volts.) d. R GEN Switch - - - - - - - - - - - - - - - - -GEN (Check generators parallel and battery voltage 28 Volts.) e. BATT Switch - - - - - - - - - - - - - - - - - - - - - OFF (Check L AMP and R AMP decrease, battery voltage 0 Volts.) f. BATT Switch - - - - - - - BATT (Check battery voltage 28 Volts.) BEFORE TAXI 1. COCKPIT/CABIN FAN Knobs - - - - - - - - - - - - - - - - AS DESIRED 2. AIR COND Switch - - - - - - - - - - - - - - - - - - - - - - - - AS DESIRED 3. COCKPIT/CABIN TEMP Knobs - - - - - - - - - - - - - - AS DESIRED 4. WINDSHIELD ANTI-ICE Switches- - - - - AS REQUIRED for defog 5. Avionics Glareshield Cooling Fans (3) - - CHECK FOR AIR FLOW 6. Air Source Select System - - - - - - - - - - - - - - - - - - - - - - - CHECK a. AIR SOURCE SELECT Knob - - - - - - - - - - - OFF (No Inflow) b. AIR SOURCE SELECT Knob - - - - - - - - - L (Check for sound of inflow to cockpit) c. AIR SOURCE SELECT Knob - - - - - - - - - R (Check for sound of inflow to cabin and cockpit) d. AIR SOURCE SELECT Knob - - - - - - - - - - - - - - - - - - BOTH 7. Flight Controls- - - - - - - - - - - - - - - - - - - - - FREE and CORRECT 8. Flaps - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - SET 9. Speed Brakes - - - - - - - - - - - - - - - - - - - -CHECK and RETRACT a. Extend Speed Brakes. b. Advance throttles to the CRU Detent; verify speed brakes retract and the SPD BRK EXTEND CAS message extinguishes; throttles IDLE. 10. Electric Elevator Trim - - - - - - - - - - - - - - - - - - - CHECK and SET (both pilot’s and copilot’s) a. Push both sides of trim switch DOWN - - - - verify correct trim wheel and pointer movement; press AP/TRIM DISC Switch - - verify trim wheel stops moving. b. Push both sides of trim switch UP - - - - - - - verify correct trim wheel and pointer movement; press AP/TRIM DISC Switch - - c. verify trim wheel stops moving. Verify pilot’s trim switch command overrides copilot’s trim switch command. d. Set trim as required within TAKEOFF band. 11. Avionics Setup and Charts - - - - - - - - - - - - - - - - - AS REQUIRED (Continued Next Page) 510CLNP-07 10 AA For Training Purposes Only Configuration MODEL 510 NORMAL PROCEDURES BEFORE TAXI (Continued) 12. Altimeters (pilot, standby and copilot) - - - - - -SET and COMPARE Pilot and copilot altimeters must indicate departure field elevation within +/-50 feet and within 75 feet of each other when set to local altimeter setting. 13. Takeoff Data (V1 , VR, V2 , VENR, Takeoff Field Length, and Weight Limits for appropriate takeoff flap setting) - - - - - SET and VERIFY 14. Destination Field Elevation - - - - - - - - - - - - - - - - - - - - - - - - -SET 15. Radar - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - STANDBY 16. CAS/PFD Messages- - - - - - - - - - - - - - - - - - - - - - - - - - - CHECK *** CLEARED / READY FOR TAXI *** 17. PAX SAFETY Switch - - - - - - - - - - - - - - - - - - - - - - - SEAT BELT 18. EXTERNAL LIGHT Switches- - - - - - - - - - - - - - - AS REQUIRED 19. Brakes - - - - - - - - - - - - - - - - - - - - - - - - - - - - APPLY and HOLD 20. PARKING BRAKE - - - - - - - - - - - - - - - - - - - - - - - - - - RELEASE 11 510CLNP-07 AA For Training Purposes Only Configuration NORMAL PROCEDURES MODEL 510 TAXI 1. Brakes - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - CHECK CAUTION CAUTION IF DURING TAXI, A NO BRAKING CONDITION IS ENCOUNTERED, OPERATE THE EMERGENCY BRAKE SYSTEM. MAINTENANCE IS REQUIRED BEFORE FLIGHT. 2. Nosewheel Steering- - - - - - - - - - - - - - - - - - - - - - - - - - - CHECK 3. Flight Instruments (including standby instruments) - - - - - CHECK CROSSWIND COMPONENT TEMPERATURE CONVERSION CHART 510CLNP-05 12 AA For Training Purposes Only TEMPORARY PILOTS’ ABBREVIATED CHECKLIST CHANGE Trim to 5.75 x 11 inches In the Normal Procedures checklist, Tab TAXI, page 12, after step 3, add a warning: TAXI 3. Flight Instruments (including standby instruments) - - - - - -CHECK WARNING Takeoff with a noticeably drifting heading indicator is prohibited. Publication Affected: Model 510 Citation Mustang (510-0001 and On) Pilots’ Abbreviated Checklist, Revision 7, dated 21 November 2008. Airplane Serial Nos. Affected: Airplanes 510-0001 and On. Description of Change: This temporary change is current with 510FM TC-R07-28 and reflects the following change to the AFM, Section III, Operating Procedures, Normal Procedures, TAXI, add a warning. Filing Instructions: Insert this temporary change in the Model 510 (510-0001 and On) Pilots’ Abbreviated Checklist adjacent to page 12. Removal Instructions: This temporary change must be removed and discarded when Revision 8 has been collated into the Pilots’ Abbreviated Checklist. 510CLNP TC-R07-05For Training Purposes Only Configuration MODEL 510 NORMAL PROCEDURES PILOT NOTES 13 510CLNP-05 AA TAXI For Training Purposes Only Configuration NORMAL PROCEDURES MODEL 510 STANDARD PERFORMANCE CONDITIONS All takeoff and landing performance in this checklist is based on a paved, dry runway. TAKEOFF PERFORMANCE SIMPLIFIED CRITERIA A simplified criteria is provided which is intended to cover the majority of situations where runway length is appreciably longer than required for this airplane. The other tabulated data gives more exact performance criteria through a range of conditions which include all but the most extreme cases. The majority of takeoff situations result in field length margins that permit using a single set of values for speeds and power settings for takeoff. If the following conditions are met, the simplified procedures may be used. 1. No obstacle in flight path. 2. Throttles - - -TAKEOFF detent (Thrust mode indicator - green TO). 3. Takeoff and approach flaps (15°). 4. Anti-Ice OFF or ON. 5. Takeoff field length available = 5,000 feet or longer. 6. No tail wind. 7. Runway Gradient-Takeoff = Zero to -2.0% (downhill). 8. Dry paved runway The values to be used are as follows: When conditions are other than those specified in the simplified criteria, the appropriate tabulated data must be referred to. 510CLNP-05 14 AA For Training Purposes Only Configuration MODEL 510 NORMAL PROCEDURES With a runway gradient, the zero runway gradient takeoff field length and V 1 must be adjusted using the table below 15 510CLNP-06 AH For Training Purposes Only Configuration NORMAL PROCEDURES MODEL 510 510CLNP-06 16 AH For Training Purposes Only Configuration MODEL 510 NORMAL PROCEDURES 17 510CLNP-06 AH For Training Purposes Only Configuration NORMAL PROCEDURES MODEL 510 510CLNP-06 18 AH For Training Purposes Only Configuration MODEL 510 NORMAL PROCEDURES 19 510CLNP-06 AH For Training Purposes Only Configuration NORMAL PROCEDURES MODEL 510 PILOT NOTES 510CLNP-05 20 AA For Training Purposes Only Configuration MODEL 510 NORMAL PROCEDURES With a runway gradient, the zero runway gradient takeoff field length and V 1 must be adjusted using the table below 21 510CLNP-06 AH For Training Purposes Only Configuration NORMAL PROCEDURES MODEL 510 510CLNP-06 22 AH For Training Purposes Only Configuration MODEL 510 NORMAL PROCEDURES 23 510CLNP-06 AH For Training Purposes Only Configuration NORMAL PROCEDURES MODEL 510 510CLNP-06 24 AH For Training Purposes Only Configuration MODEL 510 NORMAL PROCEDURES 25 510CLNP-06 AH For Training Purposes Only Configuration NORMAL PROCEDURES MODEL 510 PILOT NOTES 510CLNP-05 26 AA For Training Purposes Only Configuration MODEL 510 NORMAL PROCEDURES With a runway gradient, the zero runway gradient takeoff field length and V 1 must be adjusted using the table below. 27 510CLNP-05 AA For Training Purposes Only Configuration NORMAL PROCEDURES MODEL 510 510CLNP-05 28 AA For Training Purposes Only Configuration MODEL 510 NORMAL PROCEDURES 29 510CLNP-05 AA For Training Purposes Only Configuration NORMAL PROCEDURES MODEL 510 510CLNP-05 30 AA For Training Purposes Only Configuration MODEL 510 NORMAL PROCEDURES 31 510CLNP-05 AA For Training Purposes Only Configuration NORMAL PROCEDURES MODEL 510 PILOT NOTES 510CLNP-05 32 AA For Training Purposes Only Configuration MODEL 510 NORMAL PROCEDURES With a runway gradient, the zero runway gradient takeoff field length and V 1 must be adjusted using the table below. 33 510CLNP-05 AA For Training Purposes Only Configuration NORMAL PROCEDURES MODEL 510 510CLNP-05 34 AA For Training Purposes Only Configuration MODEL 510 NORMAL PROCEDURES 35 510CLNP-05 AA For Training Purposes Only Configuration NORMAL PROCEDURES MODEL 510 510CLNP-05 36 AA For Training Purposes Only Configuration MODEL 510 NORMAL PROCEDURES 37 510CLNP-05 AA For Training Purposes Only Configuration NORMAL PROCEDURES MODEL 510 BEFORE TAKEOFF 1. Anti-Ice/Deice systems (if required) - - - - - - - - - - - - - - - - CHECK a. Engine Speed at or above 70% N 2 . b. L/R ENGINE ANTI-ICE Switches - - - - - - - - - - - - - - - - - - -ON c. L/R ENG A/I COLD CAS message - - - - - - - - - DISPLAY, then EXTINGUISH (within one minute or less) d. L/R ENGINE ANTI-ICE Switches - - - - - - - - - - - - - - - - - - OFF e. WING/STAB Deice Switch - - - - - - - - - - - - - - - - - - - - AUTO (check white SURFACE DE-ICE CAS message sequences properly) f. Verify WING DE-ICE FAIL and TAIL DE-ICE FAIL messages are not displayed. g. WING/STAB Deice Switch - - - - - - - - - - - - - - - - - - - - - - OFF h. Throttles - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - IDLE i. Pitot-Static Switch - - - - - - - RESET STALL WARN then OFF CAUTION CAUTION DO NOT OPERATE DEICE BOOTS WHEN AMBIENT AIR TEMPERATURE IS BELOW -30 °C (-22 °F). 2. STBY INST Switch- - - - BATT TEST; GREEN LIGHT; STBY INST (If not completed previously) 3. Passenger Seats - - - - - - - - - - - - - - - - - - - - - - - FULL UPRIGHT 4. Flaps - - - - - - - - - - - - - - - - - - - - - - - - - - - - SET FOR TAKEOFF 5. Trims (3) - - - - - - - - - - - - - - - - - - - - - - - - - - SET FOR TAKEOFF 6. Speed Brakes - - - - - - - - - - - - - - - - - - - - - - - - - - - RETRACTED 7. Transponder - - - - - - - - - GND (will auto transition to ALT at liftoff) 8. Displays/Avionics/Navigation Systems- - - - - - - - - - - - - - -SETUP 9. Crew Briefing - - - - - - - - - - - - - - - - - - - - - - - - - - - - COMPLETE *** CLEARED / READY FOR TAKEOFF *** 10. Pitot-Static Switch - - - - - - - - - - - - - - - - - - - - - - - PITOT-STATIC CAUTION CAUTION LIMIT GROUND OPERATION OF PITOT-STATIC HEAT TO TWO MINUTES TO PRECLUDE DAMAGE TO THE PITOT- STATIC AND STALL WARNING HEATERS. 11. ENGINE ANTI-ICE Switches- - - - - - - - - - - - - - - - AS REQUIRED 12. WINDSHIELD ANTI-ICE Switches- - - - - - - - - - - - AS REQUIRED 13. PAX SAFETY Switch - - - - - - - - - - - - - - - - - - - - - - PAX SAFETY 14. LANDING Light Switch - - - - - - - - - - - - - - - - - - - - - AS DESIRED 15. ANTI-COLL Light Switch - - - - - - - - - - - - - - - - - - - - - - - - - - -ON 16. Radar - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - AS REQUIRED 17. EICAS - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - CHECKED 510CLNP-07 38 AA For Training Purposes Only Configuration MODEL 510 NORMAL PROCEDURES TAKEOFF 1. THROTTLES - - - - TO Detent (Thrust Mode Indicator - green T/O) 2. Engine Instruments - - - - - - - - - - - - - - - - - - - CHECK NORMAL (N1 matches command bug) 3. Brakes - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - RELEASE 4. Elevator Control - - - - - - ROTATE at V R to +10° initial pitch attitude (use flight director TO mode) AFTER TAKEOFF - CLIMB 1. LANDING GEAR Handle- - - - - - - - - - - - - - - - - - - - - - - - - - - UP 2. FLAP Handle - - - - - - - - - - - UP (V2 + 12 and clear of obstacles) 3. THROTTLES - - - - - - - - - - - - - - - - - - - - - - - - - - - - - CLB Detent 4. Yaw Damper - - - - - - - - - - - - - AS DESIRED (ON Above FL300) 5. Anti-Ice/Deice Systems- - - - - - - - - - - - - - - - - - - AS REQUIRED 6. PAX SAFETY Switch - - - - - - - - - - - - - - - - - - - - AS REQUIRED 7. LANDING Light Switch - - - - - - - - - - - - - - - - - - - AS REQUIRED 8. Pressurization - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - CHECK 9. Altimeters (transition altitude) - - - SET STD and CROSSCHECK CRUISE 1. THROTTLES - - - - - - - - - - - - - - - - - CRU Detent or AS DESIRED 2. Anti-Ice/Deice Systems- - - - - - - - - - - - - - - - - - - AS REQUIRED CAUTION CAUTION DO NOT OPERATE DEICE BOOTS WHEN INDICATED RAT IS BELOW -30°C. 3. Pressurization - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - CHECK 4. In RVSM Airspace: a. Autopilot - - - - - - - - - - - - - - - - - - - -ALT Mode unless severe turbulence is encountered. b. Altimeters - - - - - - - - - - - - - CROSSCHECK pilot and copilot altimeters at 1 hour intervals or less. Maximum allowed difference is 200 feet. DESCENT 1. Pressurization - - - - - - - - - VERIFY destination field elevation set. 2. Anti-Ice/Deice Systems- - - - - - - - - - - - - - - - - - - AS REQUIRED 3. THROTTLES - - - - - - - -AS REQUIRED for anti-ice/deice systems 4. Altimeters (transition altitude) - - - - - - - SET and CROSSCHECK 5. Landing Data (VAPP, VREF, Landing Distance, Weight, and Factors) - - - - - - - - - - - - - - - - - - - SET and VERIFY 6. LANDING Light Switch - - - - - - - - - - - - - - - - - - - AS REQUIRED TAKEOFF/CLIMB/ CRUISE/DESCENT 39 510CLNP-05 AA For Training Purposes Only Configuration NORMAL PROCEDURES MODEL 510 APPROACH 1. Landing Data - - - - - - - - - - - - - - - - - - - - - - - - - - - - - CONFIRM 2. Seats and Seat Belts - - - - - - - - - - - - - - - ADJUST and SECURE 3. Avionics and Flight Instruments- - - - - - - - - - - - - - - - - - - CHECK 4. Minimums - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - SET 5. PAX SAFETY Switch - - - - - - - - - - - - - - - - - - - - - - PAX SAFETY 6. Passenger Seats - - - - - - - - - - - - - - - - - CHECK FULL UPRIGHT 7. FUEL TRANSFER Knob- - - - - - - - - - - - - - - - - - - - - - - - - - - OFF 8. Anti-Ice/Deice Systems - - - - - - - - - - - - - - - - - - - AS REQUIRED 9. LANDING Light Switch - - - - - - - - - - - - - - - - - - - - - - - - - - - - -ON 10. FLAP Handle - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - TO/APR 11. CAS Messages - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - CHECK 12. Crew Briefing - - - - - - - - - - - - - - - - - - - - - - - - - - - - COMPLETE BEFORE LANDING 1. Landing Gear - - - - - - - - - - - - - - - - - - - - - DOWN and LOCKED 2. Speed Brakes - - - - - - - - - - - - - - - - - - - - - - - - - - - RETRACTED 3. FLAP Handle - - - - - - - LAND (STALL WARNING-NORMAL only) 4. Pressurization - - - - - - - - - - - - - - CHECK ZERO DIFFERENTIAL 5. Autopilot and Yaw Damper - - - - - - - - - - - - - - - - - - - - - - - - - OFF 6. Airspeed - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - VREF 510CLNP-07 40 AA For Training Purposes Only TEMPORARY PILOTS’ ABBREVIATED CHECKLIST CHANGE Trim to 5.75 x 11 inches In the Normal Procedures checklist, Tab APPROACH/LANDING, BEFORE LANDING, pg 40, add a new step 7: BEFORE LANDING 7. WINDSHIELD ANTI-ICE Switches - - - - - - - - - - - AS REQUIRED Publication Affected: Model 510 Citation Mustang (510-0001 and On) Pilots’ Abbreviated Checklist, Revision 7, dated 21 November 2008. Airplane Serial Nos. Affected: Airplanes 510-0001 and On. Description of Change: This temporary change is current with 510FM TC-R07-11 and reflects the following change to the AFM, Section III, Operating Procedures, BEFORE LANDING, add a new step 7. Filing Instructions: Insert this temporary change in the Model 510 (510-0001 and On) Pilots’ Abbreviated Checklist adjacent to page 40. Removal Instructions: This temporary change must be removed and discarded when Revision 8 has been collated into the Pilots’ Abbreviated Checklist. 510CLNP TC-R07-03For Training Purposes Only Configuration MODEL 510 NORMAL PROCEDURES LANDING 1. THROTTLES - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - IDLE 2. Brakes - - - - - - - - - - - - - - - APPLY (after nosewheel touchdown) 3. Speed Brakes - - - - - - - - - EXTEND (after nosewheel touchdown) CAUTION CAUTION IF A NO BRAKING CONDITION IS ENCOUNTERED DURING LANDING, OPERATE THE EMERGENCY BRAKE SYSTEM. MAINTENANCE IS REQUIRED BEFORE THE NEXT FLIGHT. ALL ENGINES GO-AROUND 1. THROTTLES - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - TO Detent (Thrust Mode Indicator - green T/O) 2. Airplane Pitch Attitude - - - - - - - - - POSITIVE ROTATION TO +8° (use flight director go-around mode) 3. FLAP Handle - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -TO/APR 4. Climb Speed - - - - - - - - - - - - - - - - - - - - - - - - - - VAPP MINIMUM 5. LANDING GEAR Handle- - - - - - - - - - - - - - - - - - - - - - - - - - - UP (when positive rate-of-climb is established) 6. FLAP Handle - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - UP 7. THROTTLES - - - - - - - - - - - - - - - - - - - - - - - - - - - - - CLB Detent APPROACH/LANDING 41 510CLNP-05 AA For Training Purposes Only Configuration NORMAL PROCEDURES MODEL 510 AA 510CLNP-05 42 For Training Purposes Only Configuration MODEL 510 NORMAL PROCEDURES AA 43 510CLNP-05 For Training Purposes Only Configuration NORMAL PROCEDURES MODEL 510 AA 510CLNP-05 44 For Training Purposes Only Configuration MODEL 510 NORMAL PROCEDURES AA 45 510CLNP-05 For Training Purposes Only Configuration NORMAL PROCEDURES MODEL 510 AFTER LANDING 1. FLAP Handle - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - UP 2. Speed Brakes - - - - - - - - - - - - - - - - - - - - - - - - - - - - - RETRACT 3. WING/STAB Deice Switch - - - - - - - - - - - - - - - - - - - - - - - - - OFF 4. Pitot-Static Switch - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - OFF 5. WINDSHIELD ANTI-ICE Switches- - - - - AS REQUIRED for defog 6. ENGINE ANTI-ICE Switches- - - - - - - - - - - - - - - - AS REQUIRED 7. ANTI COLL Light Switch- - - - - - - - - - - - - - - - - - - AS REQUIRED 8. LANDING Light Switch - - - - - - - - - - - - - - - - - - - - AS REQUIRED 9. Transponder - - - - - - - - - - - - - - - - - - - - - - - - - - - - VERIFY GND 10. Radar - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - OFF or STBY SHUTDOWN 1. PARKING BRAKE - - - - - - - - - - - - - -SET or Wheels - CHOCK 2. ENGINE ANTI-ICE Switches- - - - - - - - - - - - - - - - - - - - - - - - OFF 3. WINDSHIELD ANTI-ICE Switches- - - - - - - - - - - - - - - - - - - - OFF 4. PAX SAFETY Switch - - - - - - - - - - - - - - - - - - - - - - - - - - - - - OFF 5. LANDING Light Switch - - - - - - - - - - - - - - - - - - - - - - - - - - - - OFF 6. AIR COND Switch - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - OFF 7. FLAP Handle - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - TO/APR 8. AVN PWR Switch - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - OFF 9. THROTTLES - - - - - - - - - - - - - - - - - -CUTOFF after allowing ITT to stabilize at minimum value for two minutes 10. EXTERNAL LIGHTING Switches - - - - - - - - - - - - - - - - - - - - OFF 11. COCKPIT/CABIN Fan Knobs - - - - - - - - - - - - - - - - - - - - - - - OFF 12. OXYGEN SUPPLY Handle - - - - - - - - - - - - - - PULL TO CUTOFF 13. BATT Switch - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - OFF 14. STBY INST Switch- - - - VERIFY AMBER LIGHT ON; THEN OFF 15. Gust Lock - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - INSTALL 16. Rudder Gust Lock - - - - - - - LOCK (unless airplane will be towed) CAUTION CAUTION TOWING THE AIRPLANE WITH THE RUDDER GUST LOCK ENGAGED WILL DAMAGE THE NOSEWHEEL STEERING MECHANISM. 17. Engine Oil Level - - - - - - - - - CHECK (10 minutes after shutdown) 510CLNP-05 46 AA For Training Purposes Only Configuration MODEL 510 NORMAL PROCEDURES QUICK TURN AROUND 1. Exterior Inspection - - - - - - - - - - - - - - - - - - - - - - - - -COMPLETE 2. Circuit Breakers - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - IN 3. L/R GEN Switches - - - - - - - - - - - - - - GEN (OFF if ground power is to be used for start) 4. STBY INST Switch - - - - - - - - - - - - - - - BATT TEST (5 seconds) then STBY INST 5. Ground Power Unit (if desired)- - - - - - - - - - - - - - - CONNECTED 6. BATT Switch - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - BATT 7. PARKING BRAKE - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -SET 8. AVN PWR Switch - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - ON 9. ATIS/Clearance - - - - - - - - - - - - - - - - - - - - - - - - AS REQUIRED 10. Rotary TEST Switch - - - - - - - - - - WARNING SYSTEMS CHECK 11. Fuel Quantity and Balance - - - - - - - - - - - - - - - - - - - - - - CHECK 12. Pilot, Passenger, Cargo, and Fuel Weights - - - - - - - - - - - ENTER 13. Avionics Flight Plan (if desired) - - - - - - - - - - - - - - - - - - - ENTER 14. AVN POWER Switch - - - - - - - - - - - - - - - - OFF (if ground power is not connected) 15. Wing/Stab Deice System (if required) - - - - - - - - - - - - - - - CHECK a. Pitot-Static Switch- - - - - - - RESET STALL WARN then OFF 16. LANDING GEAR Handle- - - - - DOWN; THREE GREEN LIGHTS/ NO RED LIGHT 17. OXYGEN SUPPLY Handle - - - - - - - - - - - - - - - - - - - PUSHED IN 18. All other switches - - - - - - - - - - - - - - - - - - - - - - - - OFF or NORM 19. THROTTLES - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - CUTOFF 20. Refer to Normal Procedures, BEFORE STARTING ENGINES. TURBULENT AIR PENETRATION Flight through severe turbulence should be avoided if possible. The following procedures are recommended for flight in severe turbulence. 1. Airspeed - - APPROXIMATELY 160 KIAS (do not chase airspeed) 2. Maintain a constant attitude without chasing the altitude. Avoid sudden large control movements. 3. Operation of autopilot is recommended in basic modes only (ROL and PIT only). 4. PAX SAFETY Switch - - - - - - - - - - - - - - - - - - - - - -PAX SAFETY AFTER LANDING SHUTDOWN 47 510CLNP-05 AA For Training Purposes Only Configuration NORMAL PROCEDURES MODEL 510 WARNING SYSTEMS TEST POSITION INDICATIONS FIRE WARN • Red L ENG FIRE and R ENG FIRE switches illuminate. • Master Warning Lights illuminate. LANDING GEAR • 3 green gear downlock lights illuminate. • Red gear UNLOCK light illuminates. • Gear warning horn sounds. Alternates between pilot and copilot speakers. CABIN ALT • Red CABIN ALT message appears. • Amber CABIN ALT message appears. STALL • Amber STALL WARN FAIL message appears. • Stall warning tone sounds and alternates between pilot and copilot speakers. • Amber STALL WARN HTR message appears. • White STALL WARN HI message appears. FLAPS • The flap indicator on the MFD is replaced with a red “X” for 3 seconds. • Amber FLAPS FAIL message appears. • Amber STALL WARN FAIL message appears for 3 seconds. OVER SPEED • The overspeed warning tone sounds and alternates between pilot and copilot speakers. ANTI SKID • Amber ANTISKID FAIL message appears for 6 seconds. • White NO TIRE SPINDOWN message appears for 6 seconds. ANNU • MASTER CAUTION illuminates and cannot be cancelled. • MASTER WARNING illuminates and cannot be cancelled. • Autopilot Mode Control Panel indicators illuminate. • Audio panel indicators illuminate. • Red “DUMP” illuminates on Cabin Dump switch. • Test audio tone sounds. • Amber Standby Battery Discharge light illuminates (near STBY INST switch). 510CLNP-06 48 AF For Training Purposes Only Configuration MODEL 510 NORMAL PROCEDURES ANTI-ICE FLOW SCHEMATIC AA 49 510CLNP-05 SCHEMATICS For Training Purposes Only Configuration NORMAL PROCEDURES MODEL 510 FUEL SYSTEM SCHEMATIC 510CLNP-05 50 AA For Training Purposes Only Configuration MODEL 510 NORMAL PROCEDURES AIR CONDITIONING SCHEMATIC AA 51 510CLNP-05 For Training Purposes Only Configuration NORMAL PROCEDURES MODEL 510 PILOT (LH) CIRCUIT BREAKER PANEL AA 510CLNP-05 52 For Training Purposes Only Configuration MODEL 510 NORMAL PROCEDURES COPILOT (RH) CIRCUIT BREAKER PANEL AA 53 510CLNP-05 For Training Purposes Only Configuration NORMAL PROCEDURES MODEL 510 ELECTRIC FLOW SCHEMATIC AA 510CLNP-05 54 For Training Purposes Only Configuration MODEL 510 NORMAL PROCEDURES HYDRAULIC SCHEMATIC AA 55 510CLNP-05 For Training Purposes Only Configuration NORMAL PROCEDURES MODEL 510 LANDING GEAR SCHEMATIC AA 510CLNP-05 56 For Training Purposes Only Configuration MODEL 510 NORMAL PROCEDURES ANTENNA CONFIGURATION 57 510CLNP-06 AA For Training Purposes Only Configuration NORMAL PROCEDURES MODEL 510 PILOT NOTES 510CLNP-06 58 AA For Training Purposes Only TEMPORARY PILOTS’ ABBREVIATED CHECKLIST CHANGE Trim to 5.75 x 11 inches In the Normal Procedures Checklist, Quick Reference Checklist, page 59 or 59.1, Starting Engines procedure, change Step 5 as shown below: STARTING ENGINES 5. Operating Engine N2 . . . . INCREASE to 10% above ground idle N2 (for a cross-generator start) Publication Affected: Model 510 Citation Mustang (510-0001 and On) Pilots’ Abbreviated Checklist Normal Procedures, Revision 7, dated 21 November 2008. Airplane Serial Nos. Affected: Airplanes 510-0001 and On. Description of Change: This temporary change is current with 510FM TC-R07-07 and reflects the following change to the AFM, Section III, Operating Procedures, Normal Procedures, Starting Engines Checklist, change a step. Filing Instructions: Insert this temporary change in the Model 510 (510-0001 and On) Pilots’ Abbreviated Checklist Normal Procedures adjacent to page 59 or 59.1. Removal Instructions: This temporary change must be removed and discarded when Revision 8 has been collated into the Pilots’ Abbreviated Checklist Normal Procedures. 510CLNP TC-R07-02For Training Purposes Only Configuration MODEL 510 QUICK REFERENCE CHECKLIST COCKPIT PREPARATION 1. BATTERY DISCONNECT Switch - - - NORM/ COVER DOWN 2. INTERIOR DISCONNECT Switch- - - -NORM 3. Circuit Breakers - - - - - - - - - - - - - - - - - - - IN 4. STBY INST Switch BATT TEST (5 seconds); GREEN LIGHT ON 5. STBY INST Switch - - - - - - - - - - STBY INST; AMBER LIGHT ON 6. If Ground Power Unit is connected (for battery power only, skip to Step 7): a. BATT Switch - - - - - - - - - - - - - - - - - ON b. AVN PWR Switch - - - - - - - - - - - - - - ON c. BATTERY VOLTAGE - - - - CHECK 28V d. COCKPIT/CABIN FAN Knobs - - - - - AS DESIRED e. AIR COND Switch - - - - - -AS DESIRED 7. Cockpit Switches and Controls - - - - - - - SET 8. BATT Switch- - - - - - - - - - - - EMER; CHECK POWER TO EMERGENCY BUS ITEMS 9. BATT Switch- - - - - - - - - - - - - - - - - - - BATT 10. STBY INST Amber Light - - - - - - - - - - - OFF 11. PARKING BRAKE- - - - - - - - - - - - - - - - SET 12. LANDING GEAR Position Lights - - - THREE GREEN LIGHTS / NO RED LIGHT 13. Cockpit Lighting - - - - - - - - - AS REQUIRED 14. AVN PWR Switch - - - - - - - - - - - - - - - - - ON 15. Database/Chart Currency - - - - - - - - CHECK 16. Rotary TEST Switch - WARNING SYSTEMS CHECK 17. Oxygen System - - - - - - - - - - - - - - - CHECK 18. Fuel Quantity and Balance- - - - - - - - CHECK 19. Pilot, Passenger, Cargo, and Fuel Weights - - ENTER (MFD AUX-WEIGHT PLANNING Page) 20. ATIS/Clearance - - - - - - - - - AS REQUIRED 21. Avionics Flight Plan (if desired)- - - - - ENTER 22. AVN PWR Switch - - - - - - ON (for GPU start) OFF (for battery start) 23. Wing/Stab Deice System (if required) CHECK DELAY BEFORE FLIGHT WITHOUT GPU 1. STBY INST Switch - - - - - - - - - - - - - - - OFF 2. BATT Switch- - - - - - - - - - - - - - - - - - - - OFF BEFORE STARTING ENGINES 1. If delayed before flight without GPU: a. STBY INST Switch - - - - - - - STBY INST b. BATT Switch - - - - - - - - - - - - - - - BATT 2. Preflight Inspection - - - - - - - - - COMPLETE 3. Wheel Chocks - - - - - - - - - - - - - REMOVED 4. Cabin Door- - - - - - - - - - - - - - - - - - CLOSED 5. Passenger Briefing - - - - - - - - - COMPLETE 6. Seats and Seat Belts ADJUST and SECURE 7. EXTERNAL LIGHTING Switches - - - - - - AS REQUIRED 8. AIR COND Switch- - - - - - - - - - - - - - - - OFF 9. COCKPIT/CABIN FAN Knobs - - - - - - - OFF 10. EICAS - - - - - - - - - - - - - - - - - - - - - - CHECK 11. BATTERY VOLTAGE - - - - - - - - - - - CHECK STARTING ENGINES 1. ENGINE START Button - - - - - - - - - - PRESS MOMENTARILY 2. THROTTLE - - - - - - - - - - - - - - - - - - - - IDLE 3. Engine Instruments - - - - - - - - - - - MONITOR 4. Engine Instruments - - - - - CHECK NORMAL (Battery Current less than 100 Amps) 5. Operating Engine N 2 - - - -INCREASE to 55% (for a cross-generator start) 6. Other Engine - - - - - - - - - - - - - - - - - START; repeat steps 1 through 4 7. Ground Power Unit - - - - - - - - DISCONNECT (if applicable) 8. L/R GEN Switches - - - - - - - - - - - - - - - GEN 9. AVN POWER Switch - - - - - - - - - - - - - - - ON 10. DC AMPS/VOLTS - - - - - - - - - - - - - - CHECK BEFORE TAXI 1. COCKPIT/CABIN FAN Knobs -AS DESIRED 2. AIR COND Switch- - - - - - - - - -AS DESIRED 3. COCK/CABIN TEMP Knobs- - -AS DESIRED 4. WINDSHIELD ANTI-ICE Switches - - - - - AS REQUIRED 5. Avionics Glareshield Cooling Fans (3)- - - - - - CHECK FOR AIR FLOW 6. Air Source Select System - - - - - - - - CHECK 7. Flight Controls - - - - - FREE and CORRECT 8. Flaps - - - - - - - - - - - - - - - - - - - - - - - - - SET 9. Speed Brakes - - - - CHECK and RETRACT 10. Electric Elevator Trim - - - - CHECK and SET 11. Avionics Setup and Charts- - AS REQUIRED 12. Altimeters - - - - - - - - - -SET and COMPARE 13. Takeoff Data- - - - - - - - - - - SET and VERIFY 14. Destination Field Elevation - - - - - - - - - -SET 15. Radar - - - - - - - - - - - - - - - - - - - - STANDBY 16. CAS/PFD Messages- - - - - - - - - - - - CHECK *** CLEARED / READY FOR TAXI *** 17. PAX SAFETY Switch - - - - - - - - SEAT BELT 18. EXTERNAL LIGHT Switches AS REQUIRED 19. Brakes- - - - - - - - - - - - - - APPLY and HOLD 20. PARKING BRAKE - - - - - - - - - - - RELEASE TAKEOFF PERFORMANCE SIMPLIFIED CRITERIA 1. No obstacle in flight path 2. Throttles - TAKEOFF Detent 3. Takeoff and approach flaps (15°) 4. Anti-Ice OFF or ON 5. Takeoff field length available = 5,000 feet or longer 6. No tail wind 7. Runway Gradient - Takeoff = Zero to -2.0% (downhill) 8. Dry paved runway When conditions are other than those specified in the simplified criteria, the appropriate tabulated data must be referred to. TAXI 1. Brakes- - - - - - - - - - - - - - - - - - - - - - CHECK 2. Nosewheel Steering - - - - - - - - - - - - CHECK 3. Flight Instruments (including standby)CHECK BEFORE TAKEOFF 1. Anti-Ice/Deice systems (if required) - CHECK 2. STBY INST Switch - - - BATT TEST; GREEN LIGHT; STBY INST (if not completed previously) 3. Passenger Seats - - - - - - - - FULL UPRIGHT 4. Flaps- - - - - - - - - - - - - - SET FOR TAKEOFF 5. Trims (3) - - - - - - - - - - - SET FOR TAKEOFF 6. Speed Brakes - - - - - - - - - - - -RETRACTED 7. Transponder - - - - - - - - - - - - - - - - - - - GND 8. Displays / Avionics / Navigation Systems - - - - - - - - - - - - - - - - - - - - SETUP 9. Crew Briefing - - - - - - - - - - - - - -COMPLETE *** CLEARED / READY FOR TAKEOFF *** 10. Pitot-Static Switch- - - - - - - - - PITOT STATIC 11. ENGINE ANTI-ICE Switches AS REQUIRED 12. WINDSHIELD ANTI-ICE Switches - - - - - AS REQUIRED 13. PAX SAFETY Switch - - - - - - -PAX SAFETY 14. LANDING Light Switch - - - - - - AS DESIRED 15. ANTI-COLL Light Switch - - - - - - - - - - - - ON 16. Radar - - - - - - - - - - - - - - - - AS REQUIRED 17. EICAS - - - - - - - - - - - - - - - - - - - - - - CHECK TAKEOFF 1. THROTTLES - - - - - - - - - - - - - - - TO Detent 2. Engine Instruments- - - - - CHECK NORMAL 3. Brakes- - - - - - - - - - - - - - - - - - - - RELEASE 4. Elevator Control - - - - - - - - - - - - ROTATE at V R to +10° initial pitch attitude AFTER TAKEOFF / CLIMB 1. LANDING GEAR Handle - - - - - - - - - - - - UP 2. FLAP Handle - - - - - - - - - - - - - - - - - - - - UP (V 2 + 12 and clear of obstacles) 3. THROTTLES - - - - - - - - - - - - - - CLB Detent 4. Yaw Damper - - - - - - - - - - - - - AS DESIRED (ON Above FL300) 5. Anti-Ice/Deice Systems - - - - AS REQUIRED 6. PAX SAFETY Switch - - - - - AS REQUIRED 7. LANDING Light Switch - - - - AS REQUIRED 8. Pressurization - - - - - - - - - - - - - - - - CHECK 9. Altimeters (transition altitude)- -SET STD and CROSSCHECK AJ 59 510CLNP-07 For Training Purposes Only Configuration QUICK REFERENCE CHECKLIST MODEL 510 CRUISE 1. THROTTLES - -CRU Detent or AS DESIRED 2. Anti-Ice / Deice Systems - - - AS REQUIRED 3. Pressurization - - - - - - - - - - - - - - - - CHECK 4. In RVSM Airspace: a. Autopilot - - - - -ALT Mode unless severe turbulence is encountered. b. Altimeters - - - CROSSCHECK pilot and copilot altimeters at 1 hour intervals or less. Maximum allowed difference is 200 feet. DESCENT 1. Pressurization - - - - - - - - - - - - - - - -VERIFY destination field elevation set 2. Anti-Ice/Deice Systems - - - - AS REQUIRED 3. THROTTLES - - - - - - - - - - - AS REQUIRED for anti-ice/deice systems 4. Altimeters (transition altitude) - - - - - SET and CROSSCHECK 5. Landing Data (VAPP, V REF, Landing Distance, Weight, and Factors) - - - - - SET and VERIFY 6. LANDING Light Switch - - - - AS REQUIRED APPROACH 1. Landing Data - - - - - - - - - - - - - - - CONFIRM 2. Seats and Seat Belts ADJUST and SECURE 3. Avionics and Flight Instruments - - - - CHECK 4. Minimums - - - - - - - - - - - - - - - - - - - - - SET 5. PAX SAFETY Switch- - - - - - - PAX SAFETY 6. Passenger Seats - CHECK FULL UPRIGHT 7. FUEL TRANSFER Knob - - - - - - - - - - - OFF 8. Anti-Ice/Deice Systems - - - - AS REQUIRED 9. LANDING Light Switch - - - - - - - - - - - - - ON 10. FLAP Handle - - - - - - - - - - - - - - - - TO/APR 11. CAS Messages- - - - - - - - - - - - - - - - CHECK 12. Crew Briefing - - - - - - - - - - - - - COMPLETE BEFORE LANDING 1. Landing Gear - - - - - - - DOWN and LOCKED 2. Speed Brakes- - - - - - - - - - - - RETRACTED 3. FLAP Handle - - - LAND (STALL WARNING- NORMAL only) 4. Pressurization - - - - - - - - - - - CHECK ZERO DIFFERENTIAL 5. Autopilot and Yaw Damper- - - - - - - - - - OFF 6. Airspeed - - - - - - - - - - - - - - - - - - - - - - V REF LANDING 1. THROTTLES - - - - - - - - - - - - - - - - - - - IDLE 2. Brakes - - - - - - - - - - - - - - - - - - - - - - APPLY (after nosewheel touchdown) 3. Speed Brakes- - - - - - - - - - - - - - - - EXTEND (after nosewheel touchdown) ALL ENGINES GO-AROUND 1. THROTTLES - - - - - TO Detent (Thrust Mode Indicator - green T/O) 2. Airplane Pitch Attitude - - - - - - - - - POSITIVE ROTATION TO +8° 3. FLAP Handle - - - - - - - - - - - - - - - - TO/APR 4. Climb Speed- - - - - - - - - - - - VAPP MINIMUM 5. LANDING GEAR Handle - - - - - - - - - - - - UP (when positive rate is established) 6. FLAP Handle - - - - - - - - - - - - - - - - - - - - UP 7. THROTTLES - - - - - - - - - - - - - - CLB Detent AFTER LANDING 1. FLAP Handle - - - - - - - - - - - - - - - - - - - - UP 2. Speed Brakes- - - - - - - - - - - - - - - RETRACT 3. WING/STAB Deice Switch - - - - - - - - - - OFF 4. Pitot-Static Switch - - - - - - - - - - - - - - - - OFF 5. WINDSHIELD ANTI-ICE Switches - - - - - AS REQUIRED for defog 6. ENGINE ANTI-ICE Systems AS REQUIRED 7. ANTI COLL Light Switch - - - AS REQUIRED 8. LANDING Light Switch - - - - AS REQUIRED 9. Transponder- - - - - - - - - - - - - -VERIFY GND 10. Radar - - - - - - - - - - - - - - - - - -OFF or STBY SHUTDOWN 1. PARKING BRAKE- SET or Wheels - CHOCK 2. ENGINE ANTI-ICE Switches - - - - - - - - OFF 3. WINDSHIELD ANTI-ICE Switches - - - - OFF 4. PAX SAFETY Switch- - - - - - - - - - - - - - OFF 5. LANDING Light Switch - - - - - - - - - - - - OFF 6. AIR COND Switch- - - - - - - - - - - - - - - - OFF 7. FLAP Handle - - - - - - - - - - - - - - - - TO/APR 8. AVN PWR Switch - - - - - - - - - - - - - - - - OFF 9. THROTTLES - - - CUTOFF after allowing ITT to stabilize at minimum value for two minutes 10. EXTERNAL LIGHTING Switches - - - - - OFF 11. COCKPIT/CABIN Fan Knobs - - - - - - - - OFF 12. OXYGEN SUPPLY Handle - - - - - - PULL TO CUTOFF 13. BATT Switch - - - - - - - - - - - - - - - - - - - OFF 14. STBY INST Switch - - - - - - VERIFY AMBER LIGHT ON; THEN OFF 15. Gust Lock - - - - - - - - - - - - - - - - - - INSTALL 16. Rudder Gust Lock- - - - - - - - - - - - - - - LOCK (unless airplane will be towed) 17. Engine Oil Level - - - - - - - - - - - - - - - CHECK (10 minutes after shutdown) QUICK TURN AROUND 1. Exterior Inspection - - - - - - - - - -COMPLETE 2. Circuit Breakers - - - - - - - - - - - - - - - - - - - IN 3. L/R GEN Switches - - - - GEN (OFF if ground power is to be used for start) 4. STBY INST Switch - - - - - - - - - - BATT TEST (5 seconds) then STBY INST 5. Ground Power Unit (if desired) CONNECTED 6. BATT Switch - - - - - - - - - - - - - - - - - - BATT 7. PARKING BRAKE- - - - - - - - - - - - - - - - SET 8. AVN PWR Switch - - - - - - - - - - - - - - - - - ON 9. ATIS/Clearance - - - - - - - - - AS REQUIRED 10. Rotary TEST Switch - WARNING SYSTEMS CHECK 11. Fuel Quantity and Balance- - - - - - - - CHECK 12. Pilot, Passenger, Cargo and Fuel Weights - - - - - - - - - - - - - - - - - ENTER 13. Avionics Flight Plan (if desired) - - - - ENTER 14. AVN POWER Switch - - - - - - - OFF (if ground power is not connected) 15. Wing/Stab Deice System (if required) CHECK a. Pitot-Static Switch - - - - -RESET STALL WARN then OFF 16. LANDING GEAR Handle - - - DOWN; THREE GREEN LIGHTS/NO RED LIGHTS 17. OXYGEN SUPPLY Handle - - - - PUSHED IN 18. All other switches - - - - - - - - - OFF or NORM 19. THROTTLES - - - - - - - - - - - - - - - - CUTOFF 20. Refer to Normal Procedures, BEFORE STARTING ENGINES AA 510CLNP-07 60 For Training Purposes Only COPYRIGHT © 2006 CESSNA AIRCRAFT COMPANY WICHITA, KANSAS, USA 510CLEAP-07 30 AUGUST 2006 THIS CHECKLIST IS CURRENT WITH MODEL 510 CITATION MUSTANG (510-0001 AND ON) FAA APPROVED U.S. AIRPLANE FLIGHT MANUAL REVISION 7 DATED 21 NOVEMBER 2008. (PART NUMBER 510FM-07) the best safety device in any aircraft is a well trained crew .... REVISION 7 21 NOVEMBER 2008 For Training Purposes Only Configuration EMERGENCY/ABNORMAL PROCEDURES MODEL 510 NOTICE THIS PILOTS’ ABBREVIATED CHECKLIST EXCLUDES NOTES AND SYSTEM DESCRIPTIONS FOUND IN THE FAA APPROVED AIRPLANE FLIGHT MANUAL; THEREFORE, IT SHOULD NOT BE USED UNTIL THE FLIGHT CREW HAS BECOME FAMILIAR WITH THE AIRPLANE, ITS SYSTEMS, AND THE FAA APPROVED AIRPLANE FLIGHT MANUAL. SHOULD ANY CONFLICT EXIST BETWEEN THE ABBREVIATED CHECKLIST AND THE CHECKLIST IN THE FAA APPROVED AIRPLANE FLIGHT MANUAL, THE FLIGHT MANUAL SHALL TAKE PRECEDENCE. ALL AIRPLANE FLIGHT MANUAL NORMAL, EMERGENCY AND ABNORMAL PROCEDURE ITEMS MUST BE ACCOMPLISHED REGARDLESS OF WHICH CHECKLIST IS USED. LOG OF EFFECTIVE PAGES Use this page to determine the currency and applicability of your Pilots’ Abbreviated Checklist. Pages affected by the current revision are indicated by an asterisk (*) preceding the pages listed under the Page Number column. Refer to page iv for configuration code definitions, then determine which pages are applicable to your airplane under the configuration code column. Following is a description of the Log of Effective Pages columns: Page Number . . . . . . . Pilots’ Abbreviated Checklist page number. Page Status . . . . . . . . . . Indicates if the page has been added, revised or deleted by the current revision. Revision Number . . . . . . . . . . . . . . Indicates the revision number. Configuration Code . Indicates page effectivity by two letter code. REVISION NUMBER DATE Original 30 August 2006 Revision 1 27 October 2006 Revision 2 20 November 2006 Revision 2A 31 January 2007 Revision 3 7 February 2007 Revision 4 13 April 2007 Revision 5 2 November 2007 Revision 6 29 February 2008 Revision 7 21 November 2008 PAGE NUMBER PAGE STATUS REVISION NUMBER CONFIGURATION CODE * Title Revised 7 AA * ii thru v/vi Revised 7 AA * 1 Revised 7 AJ * 1.1 Added 7 AK * 2 Revised 7 AA * 3 Revised 7 AJ 510CLEAP-07 ii AA For Training Purposes Only Configuration MODEL 510 EMERGENCY/ABNORMAL PROCEDURES PAGE NUMBER PAGE STATUS REVISION NUMBER CONFIGURATION CODE * 3.1 Added 7 AK * 4 thru 5 Revised 7 AA 6 Revised 3 AA 7 Revised 6 AA * 8 Revised 7 AA * 9 Revised 7 AJ * 9.1 Added 7 AK * 10 thru 42 Revised 7 AA * 43 Revised 7 AJ * 43.1 Added 7 AK * 44 thru 45 Revised 7 AA 46 Revised 6 AA * 47 thru 48 Revised 7 AB * 47.1 thru 48.1 Revised 7 AC * 49 thru 71 Revised 7 AA * 72 Revised 7 AJ * 72.1 Added 7 AK * 73 thru 88 Revised 7 AA * 89 thru 90 Added 7 AA iii 510CLEAP-07 AA For Training Purposes Only MODEL 510 TEMPORARY CHANGES Trim to 5.5 x 11 inches 510CLEAP NOTE: The accompanying (attached) Temporary Change page(s) may or may not be applicable to your serial aircraft. Please refer to the individual Temporary Change page(s) to determine applicability status for your aircraft. For Training Purposes Only TEMPORARY CHANGES MODEL 510Trim to 5.5 x 11 inches Pilots’ Abbreviated Checklist Model 510 Airplanes 510-0001 and On THIS IS A LIST OF ALL CURRENT TEMPORARY CHANGES. The following list of temporary changes should be incorporated into this Pilots’ Abbreviated Checklist until the removal instructions have been complied with. Insert this page opposite the Log of Effective Pages in the front of this Pilots’ Abbreviated Checklist. A bar located in the margin on the left side of the page, adjacent to the list, will extend the full length of any change. No change bars will be used in the footers or elsewhere. The date in the footer(s) reflects only the issue date of the most recent temporary change(s) listed on that page. . TEMPORARY CHANGE NUMBER PAGE NUMBER ISSUE DATE SERVICE BULLETIN (IF APPLICABLE) OR SERIAL EFFECTIVITY 510CLEAP TC-R07-01 12 11/19/09 Airplanes 510-0001 and On. 510CLEAP TC-R07-02 iv 10/28/09 Airplanes 510-0001 and On. 510CLEAP TC-R07-03 66 12/23/10 Airplanes 510-0001 and On. 510CLEAP TC-R07-04 61 6/9/10 Airplanes 510-0001 and On. 510CLEAP TC-R07-05 Cancelled Cancelled Replaced by 510CLEAP TC-R07-10. 510CLEAP TC-R07-06 7 6/9/10 Airplanes 510-0001 and On. 510CLEAP TC-R07-07 88 6/23/10 Airplanes 510-0001 and On. 510CLEAP TC-R07-08 21 3/14/12 Airplanes 510-0405 and On and Airplanes 510-0001 thru -0404 incorporating SB510-76-01. 510CLEAP TC-R07-09 58 3/14/12 Airplanes 510-0405 and On and Airplanes 510-0001 thru -0404 incorporating SB510-76-01. 510CLEAP TC-R07-10 28 3/14/12 Airplanes 510-0001 thru -0404 not incorporating SB510-76-01. Replaces 510CLEAP TC-R07-05. 510CLEAP i U.S. 14 March 2012 For Training Purposes Only Configuration EMERGENCY/ABNORMAL PROCEDURES MODEL 510 CHECKLIST PART NUMBER Each page in this checklist contains the part number of the checklist and the page status of each page. Refer to the following example: CONFIGURATION CODES The following is a list of configuration codes which appear at the bottom of each page of the Pilots’ Abbreviated Checklist and indicate page effectivity by serial number. Pages marked AA apply to all airplanes of this model. This list contains only the configurations which have been incorporated into this checklist. Each page of the checklist is provided with a configuration code. In the event that a page is applicable to only a select number of airplanes, at least two (2) pages will be provided, one with a regular page number (e.g., 15), and one with a point page number (e.g., 15.1). The operator must then check the configuration code list in the front of the checklist to determine which page applies to his/her airplane. In some cases, multiple pages may be provided to allow for all configurations. This system allows for a “custom” checklist for each individual aircraft and therefore eliminates material that does not apply to the operator’s airplane from the checklist. The page(s) that does(do) not apply to the airplane must be discarded. From each grouping, identify and record the configuration code that applies to your airplane, then select and insert the correct pages into this checklist. Basic Checklist 510 CLEAP 07 Page Status (Original or Reissue) Checklist Emergency/Abnormal Procedures Airplane Model (Model 510) CONFIGURATION CODE EFFECTIVITY BY SERIAL NUMBER APPLICABLE CODES AA Airplanes 510-0001 and On. AB Airplanes 510-0001 and On with NiCad battery option. AC Airplanes 510-0001 and On without NiCad battery option. AJ Airplanes 510-0001 thru -0152 incorporating SB510-34-09 Navigation - Garmin G1000 Software Version 010-00435-13 Upgrade and Airplanes 510-0153 and On. AK Airplanes 510-0001 thru -0152 not incorporating SB510-34-09 Navigation - Garmin G1000 Software Version 010-00435-13 Upgrade. 510CLEAP-07 iv AA For Training Purposes Only TEMPORARY PILOTS’ ABBREVIATED CHECKLIST CHANGE Trim to 5.5 x 11 inches In the Emergency/Abnormal Procedures checklist, page iv, Configuration Codes, change the serial effectivity of configuration codes AJ and AK as follows: Publication Affected: Model 510 Citation Mustang (510- 0001 and On) Pilots’ Abbreviated Checklist, Emergency/Abnormal Procedures Revision 7, dated 21 November 2008. Airplane Serial Nos. Affected: Airplanes 510-0001 and On. Description of Change: This temporary change is current with 510FM TC-R07-12 and reflects the following change to the AFM, Section I, Introduction, Airplane Configuration Codes, change the serial effectivity for a configuration set. Filing Instructions: Insert this temporary change in the Model 510 (510-0001 and On) Pilots’ Abbreviated Checklist Emergency/ Abnormal Procedures adjacent to page iv. Removal Instructions: This temporary change must be removed and discarded when Revision 8 has been collated into the Pilots’ Abbreviated Checklist Emergency/ Abnormal Procedures. AJ Airplanes 510-0001 thru -0177 incorporating SB510-34-09 and Airplanes 510-0178 and On. AK Airplanes 510-0001 thru -0177 not incorporating SB510-34-09. 510CLEAP TC-R07-02For Training Purposes Only TEMPORARY PILOTS’ ABBREVIATED CHECKLIST CHANGE Trim to 5.5 x 11 inches This Page Intentionally Left Blank 510CLEAP TC-R07-02For Training Purposes Only Configuration MODEL 510 EMERGENCY/ABNORMAL PROCEDURES SYMBOLS USED FOR PROCEDURE DIVISION Symbols are used to mark different parts of procedures. A decision must be made by the pilot to identify the applicable part of the procedure. After the initial choice has been made, a further division of the procedure is possible. In that case, a second choice must be made, etc. When a choice has been made, all remaining actions, consequences, and references are listed. When the procedure is no longer required, this will be indicated by "PROCEDURE COMPLETED". The division symbols are identified as follows:  FIRST DIVISION • SECOND DIVISION  THIRD DIVISION O FOURTH DIVISION AA v/vi 510CLEAP-07 For Training Purposes Only Configuration MODEL 510 EMERGENCY/ABNORMAL PROCEDURES WHITE CAS MESSAGES TABLE OF CONTENTS CABIN ALT - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - A1 ENG A/I COLD L-R - - - - - - - - - - - - - - - - - - - - - - - - - - - - - A2 FUEL BOOST L-R - - - - - - - - - - - - - - - - - - - - - - - - - - - - - A3 FUEL LO INOP L-R- - - - - - - - - - - - - - - - - - - - - - - - - - - - - A4 FUEL TRANSFER - - - - - - - - - - - - - - - - - - - - - - - - - - - - - A5 MFD COLD - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - A6 NO TIRE SPINDOWN - - - - - - - - - - - - - - - - - - - - - - - - - - - A7 PRESS CTRL- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - A8 PRESS OFF- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - A9 SPD BRK EXTEND- - - - - - - - - - - - - - - - - - - - - - - - - - - - A10 STALL WARN HI - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - B1 SURFACE DE-ICE - - - - - - - - - - - - - - - - - - - - - - - - - - - - - B2 W/S A/I FAIL L-R - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - B3 W/S O’HEAT L-R - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - B4 AJ 1 510CLEAP-07 WHITE CAS MESSAGES For Training Purposes Only Configuration EMERGENCY/ABNORMAL PROCEDURES MODEL 510 WHITE CAS MESSAGES White CAS messages are advisory in nature and denote items which are considered normal during operation of the airplane or do not normally require any pilot action. These are intended primarily to provide feedback to the pilot regarding system status. However, some procedures are provided in the event a white message posts at an inappropriate time or when not commanded by the pilot. Garmin G1000 System Messages are displayed in the PFD message window and are accessed by pressing the MSG softkey on either PFD. Additional information on these and other G1000 advisory messages can be found in the Garmin G1000 Cockpit Reference Guide. This message is displayed when the pressurization system is operating in High Altitude Airfield mode and cabin altitude exceeds 10,000 feet for less than 30 minutes. Indicates that the engine inlet temperature is below safe level for satisfactory ice protection. This message will post in white for up to two minutes after engine anti-ice is turned on while the inlet warms up to the normal operating temperature. Indicates that the respective fuel boost pump has been activated normally. Indicates that the fuel quantity signal condition is not able to determine if the fuel level is below 170 lbs. in the respective tank. 1. Refer to Emergency/Abnormal Procedures, FUEL QUANTITY RED “X” OR INCORRECT FUEL QUANTITY INDICATION; Tab D7. PROCEDURE COMPLETED Indicates that the fuel transfer valve is open. In the event that this message remains posted after the fuel transfer knob is turned OFF, refer to Emergency/Abnormal Procedures, FUEL TRANSFER MESSAGE ON WHEN TRANSFER NOT SELECTED; Tab E2. 1  CABIN ALT – WHITE 2  ENG A/I COLD L-R – WHITE 3  FUEL BOOST L-R - WHITE (FUEL BOOST PUMP ON) 4  FUEL LO INOP L-R 5  FUEL TRANSFER AA 510CLEAP-07 2 A For Training Purposes Only Configuration MODEL 510 EMERGENCY/ABNORMAL PROCEDURES Indicates that the MFD temperature is below -20°C. Engine start should be delayed until this CAS message clears. The MFD is warmed and operational when the individual display elements such as letters and cursors change without blurring or streaking. Engines may be started when engine instrument numerical values are legible on the MFD. Indicates that the spindown feature of the antiskid system has failed. The following procedures are required for subsequent flights. AFTER TAKEOFF 1. ANTISKID Switch - - - - - - - - - - - - - - - - - - - - - - - - - - -OFF 2. Brakes - - - - - - - - - - - - - - - - - - - - - - - - - - APPLY GENTLY to stop wheel rotation 3. ANTISKID Switch - - - - - - - - - - - - - - - - - - - - - - - - - - - ON 4. LANDING GEAR Handle - - - - - - - - - - - - - - - - - - - - - - -UP PROCEDURE COMPLETED Indicates the loss of communication between the Pressurization Controller and the Garmin system. Pressurization system will continue to function normally using built-in backup sensors; however, it will not be possible to change the Destination Elevation. Indicates that the AIR SOURCE SELECT Knob is in either the OFF or FRESH AIR position. The cabin will not pressurize unless switch positioned in L, BOTH, or R. 1. AIR SOURCE SELECT Knob- - - - - - - - - - L, BOTH, OR R PROCEDURE COMPLETED Indicates that one or both speed brakes are not in the stowed position. 6  MFD COLD 7  NO TIRE SPINDOWN 8  PRESS CTRL – WHITE (PRESSURIZATION CONTROL FAULT) 9  PRESS OFF (PRESSURIZATION OFF) 10  SPD BRK EXTEND 3 510CLEAP-07 A AJ For Training Purposes Only Configuration EMERGENCY/ABNORMAL PROCEDURES MODEL 510 Indicates that the stall warning system is set to the Icing Conditions schedule. • IF STILL IN ICING CONDITIONS OR IT CANNOT BE VISUALLY VERIFIED THAT THE AIRPLANE IS CLEAR OF ICE 1. Landing Performance - - USE STALL WARNING-HIGH LANDING PERFORMANCE CHARTS PROCEDURE COMPLETED • IF IT CAN BE VISUALLY VERIFIED THAT THE AIRPLANE IS CLEAR OF ICE 1. PITOT-STATIC Switch - - - - - - - - RESET STALL WARN AND RELEASE 2. Landing Performance - - - - - - - - - - - - - - - USE STALL WARNING-NORMAL LANDING PERFORMANCE CHARTS PROCEDURE COMPLETED Indicates that a segment of the deice boot system is inflated to a satisfactory pressure. Indicates that the windshield controller has failed for less than 5 seconds or is performing a self-test. This message will normally post for 5 seconds then clear when Windshield Anti-Ice is first turned ON. Indicates that the windshield controller has detected an overheat condition for less than 5 seconds or is performing a self-test. This message will normally post for 5 seconds then clear when Windshield Anti-Ice is first turned ON. 1  STALL WARN HI 2  SURFACE DE-ICE 3  W/S A/I FAIL L-R – WHITE (WINDSHIELD ANTI- ICE FAILURE) 4  W/S O’HEAT L-R – WHITE (WINDSHIELD OVERHEAT) AA 510CLEAP-07 4 B For Training Purposes Only Configuration MODEL 510 EMERGENCY/ABNORMAL PROCEDURES EMERGENCY / ABNORMAL PROCEDURES RED AND AMBER CAS MESSAGES Tab RED CAS MESSAGES BATTERY O’TEMP - - - - - - - - - - - - - - - - - - - - - - - - - - - - - K1 CABIN ALT - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - F2 GEN OFF L-R - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - J2 OIL PRESS LO L-R- - - - - - - - - - - - - - - - - - - - - - - - - - - - - A8 TAIL CONE BLD LK - - - - - - - - - - - - - - - - - - - - - - - - - - - - J1 AMBER CAS MESSAGES AFT DOOR - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - AE2 AFT JBOX CB L-R - - - - - - - - - - - - - - - - - - - - - - - - - - - - - L2 AFT JBOX LIMIT L-R - - - - - - - - - - - - - - - - - - - - - - - - - - - L3 ANTISKID FAIL - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - Z1 BATTERY O’TEMP - - - - - - - - - - - - - - - - - - - - - - - - - - - - - K1 BATT TEMP FAIL - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - L1 CABIN ALT - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - G2 CABIN DOOR - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - AE3 CHECK DOORS- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - AE4 DUCT O’HEAT L-R - - - - - - - - - - - - - - - - - - - - - - - - - - - - - H1 ENG A/I COLD L-R - - - - - - - - - - - - - - - - - - - - - - - - - - - - - P1 ENG CTRL SYS L-R - - - - - - - - - - - - - - - - - - - - - - - - - - - - D5 FLAPS FAIL - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - O2 F/W SHUTOFF L-R- - - - - - - - - - - - - - - - - - - - - - - - - - - - - D6 FUEL BOOST L-R - - - - - - - - - - - - - - - - - - - - - - - - - - - - - D8 FUEL FLTR BP L-R- - - - - - - - - - - - - - - - - - - - - - - - - - - - - D9 FUEL LVL LO L-R - - - - - - - - - - - - - - - - - - - - - - - - - - - - - D10 FUEL PRES LO L-R - - - - - - - - - - - - - - - - - - - - - - - - - - - - E1 GEN OFF L-R - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - L4 HYD PRESS LO - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - AA1 HYD PUMP ON - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - AA2 NOSE DOOR L-R - - - - - - - - - - - - - - - - - - - - - - - - - - - - - AF1 OXYGEN OFF - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - I2 P/S HTR L-R - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - P2 PRESS CTRL- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - I3 STALL WARN FAIL - - - - - - - - - - - - - - - - - - - - - - - - - - - - - V4 STALL WARN HTR - - - - - - - - - - - - - - - - - - - - - - - - - - - - - Q1 T2 HTR FAIL - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - Q2 TAIL DE-ICE FAIL - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - Q4 W/S A/I FAIL L-R - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - Q3 W/S O’HEAT L-R - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - R1 WING DE-ICE FAIL- - - - - - - - - - - - - - - - - - - - - - - - - - - - - R2 WOW MISCOMPARE - - - - - - - - - - - - - - - - - - - - - - - - - - AB1 RED AND AMBER CAS MESSAGES 5 510CLEAP-07 AA For Training Purposes Only Configuration EMERGENCY/ABNORMAL PROCEDURES MODEL 510 PILOT NOTES 510CLEAP-03 6 AA RED AND AMBER CAS MESSAGES For Training Purposes Only TEMPORARY PILOTS’ ABBREVIATED CHECKLIST CHANGE Trim to 6.0 x 11 inches In the Emergency/Abnormal Procedures checklist, Table of Contents, page 7 add the Uncommanded Reduction in Engine Power procedure and delete the Uncommanded Reduction in Engine Power During Icing Conditions procedure: ENGINE/FUEL Uncommanded Reduction in Engine Power - - - - - - - - - - - - - - - - - E3 ICING Uncommanded Reduction in Engine Power During Icing Conditions R3 Publication Affected: Model 510 Citation Mustang (510-0001 and On) Pilots’ Abbreviated Checklist, Emergency/ Abnormal Procedures, Revision 7, dated 21 November 2008. Airplane Serial Nos. Affected: Airplanes 510-0001 and On. Description of Change: This temporary change is current with 510FM TC-R07-21 and reflects the following change to the AFM, Section III, Operating Procedures, Abnormal Procedures, Table of Contents, add and delete a procedure. Filing Instructions: Insert this temporary change in the Model 510 (510-0001 and On) Pilots’ Abbreviated Checklist, Emergency/Abnormal Procedures, adjacent to page 7. Removal Instructions: This temporary change must be removed and discarded when Revision 8 has been collated into the Pilots’ Abbreviated Checklist. 510CLEAP TC-R07-06For Training Purposes Only Configuration MODEL 510 EMERGENCY/ABNORMAL PROCEDURES TABLE OF CONTENTS ENGINE / FUEL Tab Engine Failure or Fire or Master Warning or Any Other Non-Normal Event During Takeoff - - - - - - - - - - - - - - - - - - - - - A1 Engine Failure During Approach (Possible ENGINE FAIL L-R CAS Message - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - A2 ENG FIRE L or R (Engine Fire Warning Light Illuminated) - - - - - - - A3 Emergency Restart - Two Engines - - - - - - - - - - - - - - - - - - - - - - - A4 Airstart Envelope - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - A5 Maximum Glide - Emergency Landing- - - - - - - - - - - - - - - - - - - - - A6 Engine Surges or Unstable Engine Operation - - - - - - - - - - - - - - - A7 OIL PRESS LO L-R (Low Oil Pressure, Red Pointer and Digits)- - - A8 Engine Failure/Precautionary Shutdown - - - - - - - - - - - - - - - - - - - B1 Inflight Restart - One Engine - - - - - - - - - - - - - - - - - - - - - - - - - - - B2 Engine Start Malfunction (Engine Does Not Start)- - - - - - - - - - - - - B3 Dry Motoring - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - B4 Engine Starter Does Not Disengage (Engine Start L or R Switch Light ON After Engine Start) - - - - - - - - - - - - - - - - - - - - C1 Engine Does Not Respond to Throttle Movement - - - - - - - - - - - - - C2 High Sustained ITT During Ground Shutdown - - - - - - - - - - - - - - - C3 Oil Pressure High (>170 PSI Amber Oil Press Indication) - - - - - - - D1 Low Oil Pressure (Amber Pointer and Digits) - - - - - - - - - - - - - - - - D2 Oil Temperature High (>135°C, Amber Oil Temp Indication) - - - - - D3 Engine Indication Failure (Red “X” on Engine Display) - - - - - - - - - D4 ENG CTRL SYS L-R (Engine Control System Fault)- - - - - - - - - - - D5 F/W SHUTOFF L-R (Firewall Shutoff Valves Closed) - - - - - - - - - - D6 Fuel Quantity Red “X” or Incorrect Fuel Quantity Indication - - - - - - D7 FUEL BOOST L-R - Amber (Fuel Boost Pump ON) - - - - - - - - - - - D8 FUEL FLTR BP L-R (Fuel Filter Bypass) - - - - - - - - - - - - - - - - - - - D9 FUEL LVL LO L-R (Fuel Level Low) - - - - - - - - - - - - - - - - - - - - - D10 FUEL PRES LO L-R (Fuel Pressure Low) - - - - - - - - - - - - - - - - - - E1 Fuel Transfer Message ON When Transfer Not Selected - - - - - - - E2 COCKPIT / CABIN / BAGGAGE FIRE Electrical Fire or Smoke- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - E3 Environmental System Smoke or Odor - - - - - - - - - - - - - - - - - - - - E4 Smoke Removal - - - - - - - - - - -