NORMAL PROCEDURES

Cessna Citation Mustang · Normal Procedures

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Overview

This document is a Pilot’s Abbreviated Checklist specifically for the Cessna Citation Mustang (Model 510). It serves as a condensed reference for pilots, providing essential normal procedures for flight operations. The checklist is designed for training purposes and emphasizes that it should not be used in place of the FAA approved Airplane Flight Manual. The document includes various sections covering preflight inspections, cockpit preparation, engine start procedures, and more, ensuring that pilots are familiar with the aircraft's systems and operations before flight. It is crucial for pilots to refer to the full Airplane Flight Manual for detailed notes and system descriptions, as this abbreviated checklist excludes such information.

Model: Cessna Citation Mustang (Model 510)
Engine start requires monitoring N1, ITT, and oil pressure.
Preflight inspection includes checking battery, engine covers, and required documents.
Cockpit preparation involves setting switches and ensuring landing gear handle is down.
Before taxiing, confirm landing gear position lights show three green lights.

Document

Source

Originally published by www.cavok.at. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.

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Document details

Type: Normal Procedures
Year: 2006
Pages: 66
File size: 20 MB
Publisher: www.cavok.at

Documentation completeness

3/7

Most owners only have the POH. Here's the essential set for the Cessna Citation Mustang.

Pilot's Operating Handbook / AFM
Checklist
Maintenance Manual
Parts Catalog (IPC)
Systems & Wiring
Service Bulletins
Type Certificate (TCDS)

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In this document

Preflight Inspection

The preflight inspection includes a preliminary exterior inspection, cockpit/cabin inspection, and exterior inspection. Key checks involve ensuring the battery is connected, engine covers and pitot covers are removed, and that required documents and equipment are onboard. The cockpit preparation section emphasizes the importance of checking circuit breakers, switch positions, and ensuring the landing gear handle is down.

Before Starting Engines

Before starting the engines, pilots must ensure that the preflight inspection is complete, wheel chocks are removed, and the cabin door is closed and latched. A passenger briefing should be conducted, and external lighting switches should be set as required.

Starting Engines

To start the engines, the ENGINE START button must be pressed momentarily, and the throttle should be set to idle. Pilots must monitor engine instruments, ensuring N1 indicates by 40% N2, and check for a steady increase in oil pressure. ITT should rise without exceeding 830°C for more than 5 seconds.

Taxi Procedures

Before taxiing, pilots should ensure that all pre-taxi checks are completed, including verifying that the landing gear position lights show three green lights and no red lights. The taxiing section provides guidance on maintaining situational awareness and following standard taxi procedures.

Takeoff and Climb

The takeoff section outlines the necessary checks and configurations before departure, including verifying takeoff performance and ensuring that all systems are functioning correctly. After takeoff, pilots must follow the climb procedures to ensure a safe ascent.

Safety notes

The abbreviated checklist excludes notes and system descriptions found in the FAA approved Airplane Flight Manual; the flight manual takes precedence in case of conflict.
Ensure that all normal, emergency, and abnormal procedure items are accomplished regardless of which checklist is used.

Full document text

NORMAL PROCEDURES This Pilot’s Abbreviated Checklist is applicable to Citation Mustang Airplanes 510-0001 and on. Pilot’s Checklist FOR TRAINING PURPOSES ONLY Configuration INTRODUCTION MODEL 510 NOTICE THE 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 M A N U A L . S H O U L D A N Y C O N F L I C T E X I S T B E T W E E N T H E 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. (Continued Next Page) REVISION NUMBER DATE Original 30 August 2006 Revision 1 27 October 2006 Revision 2 30 November 2006 Revision 2A 31 January 2007 Revision 3 7 February 2007 Revision 4 13 April 2007 Revision 5 02 November 2007 Revision 6 29 February 2008 Revision 7 21 November 2008 Revision 7A 10 December 2018 PAGE NUMBER PAGE STATUS REVISION NUMBER CONFIGURATION CODE Revised 7A AA Revised 7A AA Revised 7A AA Original 0 AA * Title * ii thru vi * 1 2 3 Revised 5 AA 510CLNP-07A ii AA FOR TRAINING PURPOSES ONLY Configuration MODEL 510 INTRODUCTION PAGE NUMBER PAGE STATUS REVISION NUMBER CONFIGURATION CODE 4 Revised 7 AA 5 Revised 5 AA 6 Revised 6 AA 7 Revised 7 AA 8 Revised 7 AJ 8.1 Revised 7 AK Revised 7A AA Revised 5 AA Revised 7A AA Deleted 7A AI Revised 5 AA Revised 7A AA Deleted 7A AI Revised 5 AA Revised 7A AR Added 7A AS Revised 5 AA Revised 7A AA Revised 5 AA Revised 7A AR Added 7A AS Revised 5 AA Revised 6 AF Revised 6 AG Revised 5 AA Revised 6 AA Revised 7A AT Revised 7A AU Added 7A AV Added 7A AW Revised 7A AR * 9 thru 12 13 thru 14 * 15 thru 19 * 15.1 thru 19.1 20 * 21 thru 25 * 21.1 thru 25.1 26 thru 37 * 38 * 38.1 39 * 40 41 thru 45 * 46 * 46.1 47 48 48.1 49 thru 56 57 thru 58 * 59 * 59.1 * 59.2 * 59.3 * 60 * 60.1 Added 7A AS iii 510CLNP-07A AA 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) AA 510CLNP-07A iv FOR TRAINING PURPOSES ONLY AA AF Configuration MODEL 510 INTRODUCTION CONFIGURATION CODES (Continued) INCORPORATION OF TEMPORARY CHANGES (TCs) This checklist incorporates the following Normal Procedures TCs, listed with their associated Flight Manual TCs. CONFIGURATION CODE EFFECTIVITY BY SERIAL NUMBER APPLICABLE CODES AJ Airplanes 510-0001 thru -0177 incorporating SB510-34-09 or SB510-34-11, and Airplanes 510-0178 and On. AK Airplanes 510-0001 thru -0177 not incorporating SB510-34-09 or SB510-34-11. AR Airplanes 510-0475 and On and Airplanes 510-0001 thru -0474 incorporating SB510-34-17. AS Airplanes 510-0001 thru -0474 not incorporating SB510-34-17. AT Airplanes 510-0001 thru -0177 incorporating SB510-34-09 and SB510-34-17, Airplanes 510-0178 thru -0474 incorporating SB510-34-17, and Airplanes 510-0475 and On. AU Airplanes 510-0001 thru -0177 incorporating SB510-34-09 and not incorporating SB510-34-17, and Airplanes 510-0178 thru -0474 not incorporating SB510-34-17. AV Airplanes 510-0001 thru -0177 not incorporating SB510-34-09, and incorporating SB510-34-17. AW

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Airplanes 510-0001 thru -0177 not incorporating SB510-34-09 or SB510-34-17. CHECKLIST TC FLIGHT MANUAL TC 510CLNP TC-R07-01 510FM TC-R07-07 510CLNP TC-R07-02 510FM TC-R07-07 510CLNP TC-R07-03 510FM TC-R07-11 510CLNP TC-R07-04 510FM TC-R07-12 510CLNP TC-R07-05 510FM TC-R07-28 510CLNP TC-R07-09 510FM TC-R07-41 510CLNP TC-R07-10 510FM TC-R07-42 510CLNP TC-R07-11 510FM TC-R07-41 510CLNP TC-R07-12 510FM TC-R07-42 AA v 510CLNP-07A FOR TRAINING PURPOSES ONLY AJ AR AT NORMAL PROCEDURES MODEL 510 PILOT NOTES vi 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 - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - 10 TAXI Before Taxi- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - 11 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 - 42 Landing Performance - - - - - - - - - - - - - - - - - - - - - - - - - - - - - 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-07A AA FOR TRAINING PURPOSES ONLY NORMAL PROCEDURES MODEL 510 PILOT NOTES 2 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 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 9 510CLNP-07A AA BEFORE START FOR TRAINING PURPOSES ONLY Configuration NORMAL PROCEDURES MODEL 510 STARTING ENGINES 1. ENGINE START Button - - - - - - - - - - - - PRESS MOMENTARILY (verify button illuminates) 2. THROTTLE- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - IDLE 3. Engine Instruments - - - - - - - - - - - - - - - - - - - - - - - - - MONITOR a. N1 - - - - - - - - - - - - - Abort start if no N 1 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) 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 N 2 - - - - - - - INCREASE to 10% above ground idle N2 (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 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.) 510CLNP-07A 10 AA FOR TRAINING PURPOSES ONLY Configuration MODEL 510 NORMAL PROCEDURES 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- -verify trim wheel stops moving c. 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 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-07A AA FOR TRAINING PURPOSES ONLY Configuration NORMAL PROCEDURES MODEL 510 TAXI 1. Brakes - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - CHECK I F D U R I N G TA X I , A N O B R A K I N G C O N D I T I O N I S ENCOUNTERED, OPERATE THE EMERGENCY BRAKE SYSTEM. MAINTENANCE IS REQUIRED BEFORE FLIGHT. 2. Nosewheel Steering- - - - - - - - - - - - - - - - - - - - - - - - - - - CHECK 3. Flight Instruments (including standby instruments) - - - - - CHECK WARNING TAKEOFF WITH A NOTICEABLY DRIFTING HEADING INDICATOR IS PROHIBITED. CROSSWIND COMPONENT TEMPERATURE CONVERSION CHART 510CLNP-07A 12 AA FOR TRAINING PURPOSES ONLY CAUTION MODEL 510 NORMAL PROCEDURES PILOT NOTES 13 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-07A AA FOR TRAINING PURPOSES ONLY Configuration NORMAL PROCEDURES MODEL 510 510CLNP-07A 16 AA FOR TRAINING PURPOSES ONLY Configuration MODEL 510 NORMAL PROCEDURES 17 510CLNP-07A AA FOR TRAINING PURPOSES ONLY Configuration NORMAL PROCEDURES MODEL 510 510CLNP-07A 18 AA FOR TRAINING PURPOSES ONLY Configuration MODEL 510 NORMAL PROCEDURES 19 510CLNP-07A AA FOR TRAINING PURPOSES ONLY NORMAL PROCEDURES MODEL 510 PILOT NOTES 20 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-07A AA FOR TRAINING PURPOSES ONLY Configuration NORMAL PROCEDURES MODEL 510 510CLNP-07A 22 AA FOR TRAINING PURPOSES ONLY Configuration MODEL 510 NORMAL PROCEDURES 23 510CLNP-07A AA FOR TRAINING PURPOSES ONLY Configuration NORMAL PROCEDURES MODEL 510 510CLNP-07A 24 AA FOR TRAINING PURPOSES ONLY Configuration MODEL 510 NORMAL PROCEDURES 25 510CLNP-07A AA FOR TRAINING PURPOSES ONLY NORMAL PROCEDURES MODEL 510 PILOT NOTES 26 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 MODEL 510 NORMAL PROCEDURES PILOT NOTES 32 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 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 - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - white ALT (will auto transition to green ALT at liftoff) 8. Displays/Avionics/Navigation Systems- - - - - - - - - - - - - - -SETUP 9. Crew Briefing - - - - - - - - - - - - - - - - - - - - - - - - - - - - COMPLETE *** CLEARED / READY FOR TAKEOFF *** 10. Pitot-Static Switch - - - - - - - - - - - - - - - - - - - - - - - PITOT-STATIC 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-07A 38 AR FOR TRAINING PURPOSES ONLY CAUTION CAUTION 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 7. WINDSHIELD ANTI-ICE Switches- - - - - - - - - - - - AS REQUIRED 510CLNP-07A 40 AA FOR 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 white ALT 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) 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-07A 46 AR FOR TRAINING PURPOSES ONLY CAUTION 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 NORMAL PROCEDURES MODEL 510 PILOT NOTES 58 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 10% above ground idle (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 - - - - - - - - - - - - - - - white ALT 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 AT 59 510CLNP-07A FOR TRAINING PURPOSES ONLY Configuration QUICK REFERENCE CHECKLIST MODEL 510 510CLNP-07A 60 AR 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 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 7. WINDSHIELD ANTI-ICE Switches - - - - - - - - - - - - - - AS REQUIRED 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 white ALT 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 FOR TRAINING PURPOSES ONLY

All Cessna Citation Mustang normal procedures