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U.S. Department of Transportation Federal Aviation Administration Washington, D.C.
Master Minimum Equipment List (MMEL)
Revision: 1 Date: 04/04/2013
Cessna-510
For PART 91 and PART 135 ONLY
Thomas M. Kieffaber Chair, Flight Operations Evaluation Board
Federal Aviation Administration Kansas City Aircraft Evaluation Group 901 Locust Street, Department of Transportation Building Kansas City, MO 64106
Telephone: (816) 329-3233 FAX: (816) 329-3241 This Page Intentionally Left Blank U.S. DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST FEDERAL AVIATION ADMINISTRATION AIRCRAFT: REVISION NO. 1 PAGE NO. CESSNA 510 DATE: 04/04/2013 I TABLE OF CONTENTS / CONTROL PAGE SYSTEM PAGES REVISION DATE
-- Cover Page - 1 04/04/2013 -- Table of Contents / Control Page I 1 04/04/2013 -- Highlights of Change II, III, IV, V 1 04/04/2013 -- Definitions and Preamble VI 1 04/04/2013 -- Guidelines for (M) & (O) VII 1 04/04/2013 Procedures -- Section One VIII 1 04/04/2013 21 Air Conditioning 21-1 thru 21-3 1 04/04/2013 22 Auto Flight 22-1 1 04/04/2013 23 Communications 23-1 thru 23-4 1 04/04/2013 24 Electrical 24-1 1 04/04/2013 25 Equipment/Furnishings 25-1 thru 25-5 1 04/04/2013 26 Fire Protection 26-1 1 04/04/2013 27 Flight Controls 27-1 1 04/04/2013 28 Fuel 28-1 1 04/04/2013 30 Ice & Rain Protection 30-1 thru 30-2 1 04/04/2013 31 Indicating/Recording Systems 31-1 thru 31-2 1 04/04/2013 32 Landing Gear 32-1 1 04/04/2013 33 Lights 33-1 thru 33-3 1 04/04/2013 34 Navigation 34-1 thru 34-7 1 04/04/2013 35 Oxygen 35-1 1 04/04/2013 38 Water/Waste 38-1 1 04/04/2013 45 Central Maintenance System 45-1 1 04/04/2013 46 Information Systems 46-1 1 04/04/2013 52 Doors 52-1 thru 52-3 1 04/04/2013 73 Engine Fuel and Control 73-1 1 04/04/2013 76 Engine Controls 76-1 1 04/04/2013 -- Section Two INT-1 thru INT-3 1 04/04/2013 -- CAS Relief 2-1 thru 2-5 1 04/04/2013 U.S. DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST FEDERAL AVIATION ADMINISTRATION AIRCRAFT: REVISION NO. 1 PAGE NO. CESSNA 510 DATE: 04/04/2013 II HIGHLIGHTS OF CHANGE
NOTE: This revision incorporates a revised numbering format. Definitions and preamble replaced with a requirement to include definitions and preamble in operators MEL. ATA 21 Moved Cabin Altitude Warning System relief to Chapter 31. -20-01 Added relief for Cockpit Air Outlet. -20-02 Added relief for Cabin Air Outlet. -21-01 Revised remarks and exceptions. -21-02 Revised remarks and exceptions. -21-03 Revised remarks and exceptions. -21-04 Revised title, number required for dispatch, and remarks and exceptions. -30-01 Added relief for Cabin Pressurization System. -31-01 Revised title and remarks and exceptions. -32-01 Revised title and remarks and exceptions. -32-02 Revised title and remarks and exceptions. -33-01 Revised title and remarks and exceptions. -33-02 Revised remarks and exceptions. -33-03 Revised title and remarks and exceptions. -33-04 Added relief for Cabin Dump Function. -50-01 Revised title and remarks and exceptions. -60-01 Revised title and remarks and exceptions. ATA 22 Moved Electric Elevator Trim relief to Chapter 27. -00-01 Revised remarks and exceptions. -10-01 Revised remarks and exceptions. -10-02 Added relief for Go-Around Button. -10-03 Revised title and remarks and exceptions. -10-04 Added relief for Autopilot/Flight Director Sync (CWS Button). ATA 23 Moved Emergency Locator Transmitter (ELT) relief to Chapter 25. -00-01 Added relief for Flight Phone System. -10-01 Added relief for High Frequency (HF) Communications System. -12-01 Revised remarks and exceptions. -20-01 Moved Datalink relief from Chapter 34. -30-01 Added relief for Auxiliary Audio Input System. -30-02 Added relief for XM Radio Wireless Remote System. -40-01 Added relief for Passenger Address (PA) System -50-01 Standardized relief for Flight Deck Headsets Earphone/Headphones and Boom Microphones with PL-58. -50-02 Added relief for Hand Microphone. -50-03 Added relief for Hand Microphone Jack. -50-04 Added relief for Hand Microphone Holder. -50-05 Revised title and remarks and exceptions. Added relief for individual buttons. -50-06 Added relief for Cockpit Speaker. -60-01 Separated Static Wick relief into zones. -70-01 Added relief for Cockpit Voice Recorder ATA 24 Removed relief for Standby Instrument Battery. -31-01 Added relief for Battery Temperature Indication. -40-01 Added relief for External Power System. -60-01 Added relief for Cockpit 12V Outlet. U.S. DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST FEDERAL AVIATION ADMINISTRATION AIRCRAFT: REVISION NO. 1 PAGE NO. CESSNA 510 DATE: 04/04/2013 III HIGHLIGHTS OF CHANGE -60-02 Added relief for Interior Disconnect. ATA 25 Removed relief for Passenger Convenience expired on 31 Dec 2007. -00-01 Added relief for Document Holder. -10-01 Added relief for Flight Crew Seat -10-02 Revised title and remarks and exceptions. -10-03 Added relief for Cockpit Assist Handle. -10-04 Deleted remarks and exceptions. -10-05 Added relief for Emergency Gear Handle Cover. -20-01 Revised remarks and exceptions. Added relief for individual items. -20-02 Added relief for Folding Cabin Seat. -20-03 Added relief for Cabin Curtain. -20-04 Added relief for Non-Essential Equipment & Furnishings (NEF) -30-01 Added relief for Cabin Storage Compartment. -30-02 Added relief for Storage Compartment Key Lock. -40-01 Added relief for Ashtray. -60-01 Separated Emergency Medical Equipment by type. -61-01 Added relief for Life Preserver. -62-01 Moved Emergency Located Transmitter (ELT) relief from Chapter 23. -64-01 Added relief for Life Raft. ATA 26 -22-01 Revised number required for dispatch and remarks and exceptions. ATA 27 -31-01 Moved Electric Elevator Trim relief from Chapter 22. -60-01 Revised remarks and exceptions. -60-02 Added relief for Speed Brake Position. -60-03 Added relief for Speed Brake Switch. -70-01 Added relief for Aileron/Elevator Control Lock. -70-02 Added relief for Rudder Lock. ATA 28 -10-01 Added relief for Over-wing Refueling Cap Lock. -41-01 Added relief for Fuel Low Level Indicating System. ATA 30 -10-01 Revised title and remarks and exceptions. -10-02 Revised title and remarks and exceptions. -20-01 Revised title and remarks and exceptions. -30-01 Revised title, number installed, number required for dispatch and remarks and exceptions. -30-02 Revised title, number installed, number required for dispatch, and remarks and exceptions. -30-03 Added relief for Stall Warning Vane Heater. -40-01 Revised title and remarks and exceptions. -40-02 Added relief for Windshield Rain Repellant. -70-01 Added relief for Air Conditioner FWD Evaporator Drain Heater. ATA 31 -20-01 Revised remarks and exceptions. -30-01 Added relief for Flight Data Recorder (FDR) System. -30-02 Added relief for Quick Access Recorder. U.S. DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST FEDERAL AVIATION ADMINISTRATION AIRCRAFT: REVISION NO. 1 PAGE NO. CESSNA 510 DATE: 04/04/2013 IV HIGHLIGHTS OF CHANGE -40-01 Added relief for Electronic Checklist. -40-02 Added relief for Fuel Totalizer -50-01 Separated relief for Master Caution/Warning to annunciator and function. -50-02 Added relief for Cabin Altitude Warning System ATA 32 -41-01 Revised remarks and exceptions. Added note. -41-02 Added relief for Tire Spin Down System. ATA 33 -10-01 Revised title and remarks and exceptions. -10-02 Revised remarks and exceptions. -10-03 Revised remarks and exceptions. -10-04 Added relief for Cockpit Map Light. -10-05 Added relief for G1000 Display Dimmer. -20-01 Revised title, repair category, number installed, number required for dispatch and remarks and exceptions. -20-02 Revised title, repair category, number installed, number required for dispatch and remarks and exceptions. -30-01 Revised title. Added relief for Door Proximity Switch. -30-02 Added relief for Door Proximity Switch. -40-01 Revised title, repair category and remarks and exceptions. -40-02 Revised title and remarks and exceptions. -40-03 Revised title and remarks and exceptions. -40-04 Revised title and remarks and exceptions. -40-05 Revised title. -50-01 Added relief for Cockpit Flashlight and Holder Assembly. ATA 34 Moved Datalink relief to Chapter 23. -23-01 Revised remarks and exceptions. -25-01 Added relief for MFD Remote Mounted Control Panel. -25-02 Added relief for Mode Control Panel. -25-03 Added relief for Synthetic Vision. -25-04 Added relief for Moving Map Display. -25-05 Added relief for certain Primary Flight Display (PFD) buttons/functions. -31-01 Separated from Navigation Equipment. Revised remarks and exceptions. -31-02 Separated from Navigation Equipment. Revised remarks and exceptions. -32-01 Added relief for Glideslope. -34-01 Revised number required for dispatch and remarks and exceptions. -42-01 Revised number required for dispatch and remarks and exceptions. -43-01 Revised remarks and exceptions. -44-01 Added relief for Radar Altimeter System. -44-02 Separated into individual functions. -45-01 Added relief for Traffic Alert and Collision Avoidance System (TCAS). -45-02 Added relief for Traffic Information System (TIS). -45-03 Added relief for Traffic Collision Avoidance Device (TCAD). -51-01 Revised remarks and exceptions. -52-01 Revised remarks and exceptions. Added -04 per PL-076, Revision 05. -52-02 Added relief for ADS-B per PL-105, Revision 01. -55-01 Revised remarks and exceptions. U.S. DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST FEDERAL AVIATION ADMINISTRATION AIRCRAFT: REVISION NO. 1 PAGE NO. CESSNA 510 DATE: 04/04/2013 V HIGHLIGHTS OF CHANGE -57-01 Revised title and remarks and exceptions. -60-01 Revised title, repair category, and remarks and exceptions. -60-02 Added relief for Data Loader (SD Card Slot). ATA 35 -00-01 Added relief for Oxygen Tank Fill Port. -00-02 Added relief for Plastic Blowout Disc/Green Label. -20-01 Revised remarks and exceptions. Separated relief for Cabin Mask and Drop Out Panel. -30-01 Added relief for Protective Breathing Equipment. -30-02 Added relief for Portable Oxygen Bottles. ATA 38 -30-01 Revised remarks and exceptions. ATA 45 -00-01 Added relief for Citation Diagnostics and Maintenance System (CDMS). ATA 46 -00-01 Added relief for Electronic Flight Bag (EFB) System. ATA 52 -10-01 Grouped items under Cabin Door. Revised remarks and exceptions. Added relief for Gust Lock, Pull Chain, Step Assembly and Step Support Cable. -20-01 Added relief for Escape Hatch Pin. -30-01 Grouped items under Baggage Doors. Revised remarks and exceptions. Added relief for Nose Door Gas Spring, Aft Door Gas Spring and Aft Door Seal. -70-01 Grouped items under Cabin Door Monitoring System. Revised remarks and exceptions. ATA 73 Moved Engine Synchronizer System relief to Chapter 76. -31-01 Revised remarks and exceptions. ATA 76 -01-01 Moved Engine Synchronizer System relief from Chapter 73. Section Added relief for CAS messages. Two U.S. DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST FEDERAL AVIATION ADMINISTRATION AIRCRAFT: REVISION NO. 1 PAGE NO. CESSNA 510 DATE: 04/04/2013 VI DEFINITIONS AND PREAMBLE
DEFINITIONS
The required definitions listed are listed in Appendix B of MMEL Policy Letter 25. Additional definitions may be included in an operators MEL as desired. Revision of PL-025 does not require revision to the operator’s MEL.
PREAMBLE
The applicable preamble must be inserted in the operator’s MEL from current FAA Policy Letter PL-34 or Policy Letter PL-36. U.S. DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST FEDERAL AVIATION ADMINISTRATION AIRCRAFT: REVISION NO. 1 PAGE NO. CESSNA 510 DATE: 04/04/2013 VII GUIDELINES FOR (M) & (O) PROCEDURES
The FOEB has identified a need for certain procedures to provide an adequate level of safety while providing relief for some items. These procedures must be established by the operator and may be based on the aircraft manufacturer’s recommended procedures, Supplemental Type Certificate modifier’s recommended procedures, or equivalent operator procedures. When recommended procedures are published the operator should comply with these procedures. If recommended procedures are not published, the following guidelines delineate the aspects to be considered by the operator in the development of required procedures.
Cessna has developed recommended (M) maintenance and (O) operational procedures for the Cessna 510 Master Minimum Equipment List (P/N 510COMP-01-00, or later revision). Operator’s MEL procedures should be based on the Cessna procedures. U.S. DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST FEDERAL AVIATION ADMINISTRATION AIRCRAFT: REVISION NO. 1 PAGE NO. CESSNA 510 DATE: 04/04/2013 VIII
SECTION ONE
LRU ORIENTED MMEL RELIEF U.S. DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST FEDERAL AVIATION ADMINISTRATION AIRCRAFT: REVISION NO. 1 PAGE NO. CESSNA 510 DATE: 04/04/2013 21-1 1. REPAIR CATEGORY SYSTEM, 2. NUMBER INSTALLED SEQUENCE NUMBERS & ITEM 3. NUMBER REQUIRED FOR DISPATCH 4. REMARKS AND EXCEPTIONS 21 AIR CONDITIONING -20-01 Cockpit Air Outlet C 2 0 I -20-02 Cabin Air Outlet C - 1 I -21-01 Fresh Air Fan C 1 0 May be inoperative provided pressurization system is operative. I -21-02 Cabin Fan C 1 0 May be inoperative provided: I a) Cockpit fan is operative, and I b) CABIN FAN remains OFF. I -21-03 Cockpit Fan C 1 0 May be inoperative provided: I a) Cabin fan is operative, I b) Cabin and cockpit temperature I control system is operative, I c) All glareshield fans are operative, I and I d) COCKPIT FAN remains OFF. I -21-04 Glareshield Fan C 3 1 May be inoperative provided: I a) Cockpit fan is operative and I selected ON, and b) Air conditioning system is operative and selected ON. -30-01 Cabin Pressurization C 1 0 (O) May be inoperative provided: I System a) PRESS CTRL is selected to I (Unpressurized) STANDBY, I b) CABIN DUMP is selected ON, I c) Aircraft is operated at 14,100 feet I cabin altitude or below, and I d) Flight crew oxygen system is I operative and used as required by I 14 CFR. I NOTE: PRESS CTRL amber message I will appear. CABIN ALTITUDE I red message may appear at I 9,800 +/- 200 feet cabin altitude. I -31-01 Pressurization Controller C 1 0 May be inoperative provided cabin I Auto Schedule Mode pressurization system is considered I (NORM) inoperative. I (Unpressurized) I -32-01 Cabin Differential Pressure (EICAS Indication) -01 (Unpressurized) C 1 0 May be inoperative provided cabin I pressurization system is considered I inoperative. I U.S. DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST FEDERAL AVIATION ADMINISTRATION AIRCRAFT: REVISION NO. 1 PAGE NO. CESSNA 510 DATE: 04/04/2013 21-2 1. REPAIR CATEGORY SYSTEM, 2. NUMBER INSTALLED SEQUENCE NUMBERS & ITEM 3. NUMBER REQUIRED FOR DISPATCH 4. REMARKS AND EXCEPTIONS 21 AIR CONDITIONING -02 (Pressurized) C 1 0 (O) May be inoperative provided: a) Cabin altitude and rate (EICAS Indication) are operative, I b) Pressurization controller auto I schedule mode is operative, and I c) A chart is provided and used to convert cabin and aircraft altitude I to differential pressure. -32-02 Cabin Altitude (EICAS Indication) -01 (Unpressurized) C 1 0 May be inoperative provided cabin I pressurization system is considered I inoperative. I -02 (Pressurized) C 1 0 (O) May be inoperative provided: I a) Cabin differential pressure (EICAS I Indication) is operative, I b) Pressurization controller auto I schedule mode is operative, and I c) A chart is provided and used to I convert aircraft altitude and I differential pressure to cabin I altitude. I -33-01 Cabin Outflow Valve C 2 0 (M) May be inoperative provided: (Unpressurized) a) Affected cabin outflow valve is I removed, and I b) Cabin pressurization system is I considered inoperative. I -33-02 Flow Control Valve C 2 1 (O) One may be inoperative provided: a) Pressurization controller auto I schedule mode is operative, I b) Cabin pressurization air source is I selected to operative source, and I c) Aircraft is operated at FL 250 or below. U.S. DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST FEDERAL AVIATION ADMINISTRATION AIRCRAFT: REVISION NO. 1 PAGE NO. CESSNA 510 DATE: 04/04/2013 21-3 1. REPAIR CATEGORY SYSTEM, 2. NUMBER INSTALLED SEQUENCE NUMBERS & ITEM 3. NUMBER REQUIRED FOR DISPATCH 4. REMARKS AND EXCEPTIONS 21 AIR CONDITIONING -33-03 Pressure Regulating Shutoff C 2 1 (O) One may be inoperative provided: Valve a) Affected pressure regulated (Failed Closed) shutoff valve is verified closed, I b) Pressurization controller auto I schedule mode is operative, I c) Cabin pressurization air source is I selected to operative source, and I d) Aircraft is operated at FL 250 or below. -33-04 Cabin Dump Function C 1 0 (M) May be inoperative provided: I (Unpressurized) a) One cabin outflow valve is I removed, and I b) Cabin pressurization system is I considered inoperative. I -50-01 Air Conditioning System C 1 0 (M) May be inoperative provided: a) Air conditioning system is I deactivated, b) Cabin and cockpit temperature control system is operative, I c) All glareshield fans are operative, I and I d) Aircraft is restricted to I temperature limitation in II accordance with AFM. -60-01 Cabin and Cockpit C 2 1 May be inoperative provided: I Temperature Control a) Crew determines that cockpit and System cabin temperature are satisfactory, and b) DUCT O’HEAT amber message is I monitored. I U.S. DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST FEDERAL AVIATION ADMINISTRATION AIRCRAFT: REVISION NO. 01 PAGE NO. CESSNA 510 DATE: 04/04/2013 22-1 1. REPAIR CATEGORY SYSTEM, 2. NUMBER INSTALLED SEQUENCE NUMBERS & ITEM 3. NUMBER REQUIRED FOR DISPATCH 4. REMARKS AND EXCEPTIONS 22 AUTO FLIGHT -00-01 Autopilot B 1 0 (M) May be inoperative provided: I a) Autopilot is deactivated, I b) Aircraft is not operated single I pilot, I c) Enroute operations do not require II its use, I d) Approach minimums do not I require its use, and I e) Aircraft is not operated RVSM. -10-01 Yaw Damper C 1 0 (M) May be inoperative provided: I a) Yaw damper is deactivated, I b) Autopilot is considered I inoperative, and I c) Aircraft is operated at FL 300 or I below. I -10-02 Go-Around Button -01 C 2 1 I -02 C 2 0 May be inoperative provided: I a) Flight director is not used for I takeoff or during go-around, and I b) Autopilot is disconnected for go- I around. I NOTE: FMS missed approach procedure I must be activated manually. I -10-03 Autopilot/Trim Disconnect (Red Yoke AP TRIM DISC Button) (Fails to disconnect) I -01 C 2 1 Right side may be inoperative for single I pilot operations. I -02 C 2 0 May be inoperative provided electric I elevator trim is considered inoperative. I -10-04 Autopilot/Flight Director C 2 0 I Sync I (CWS Button) I U.S. DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST FEDERAL AVIATION ADMINISTRATION AIRCRAFT: REVISION NO. 1 PAGE NO. CESSNA 510 DATE: 04/04/2013 23-1 1. REPAIR CATEGORY SYSTEM, 2. NUMBER INSTALLED SEQUENCE NUMBERS & ITEM 3. NUMBER REQUIRED FOR DISPATCH 4. REMARKS AND EXCEPTIONS 23 COMMUNICATIONS -00-01 Flight Phone System D - 0 I *** I -01 Handset D - 0 May be inoperative provided procedures I do not require its use. I -02 Antenna system D - 0 May be inoperative provided procedures I do not require its use. I -10-01 High Frequency (HF) D - - Any in excess of those required by 14 I *** Communications System CFR may be inoperative. I -01 Wire Antenna C - 0 (M) May be inoperative provided: I a) Horizontal and vertical stabilizers I are inspected for damage, I b) Any remaining portion of wire I antenna is removed, and I c) High Frequency (HF) I communication system is I considered inoperative. I -12-01 Communication Systems C - - May be inoperative provided: I (VHF) a) Affected system is not on I emergency bus, I b) System is not required by 14 CFR, I and I c) Procedures do not require its use. I -20-01 Datalink (Including Satellite I Radio and Weather) I -01 D - 0 May be inoperative provided procedures I do not require its use. I NOTE: Any function(s) that operate I normally may be used. I -02 C - 0 (O) May be inoperative provided alternate I procedures are established and used. I -30-01 Auxiliary Audio Input C 1 0 I *** System I -30-02 XM Radio Wireless Remote C 1 0 I *** System I -40-01 Passenger Address (PA) *** System (Aircraft with cabin headset jacks only) -01 B - 0 (O) May be inoperative provided alternate I normal, abnormal, and emergency I procedures, and/or operating restrictions I are established and used. I U.S. DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST FEDERAL AVIATION ADMINISTRATION AIRCRAFT: REVISION NO. 1 PAGE NO. CESSNA 510 DATE: 04/04/2013 23-2 1. REPAIR CATEGORY SYSTEM, 2. NUMBER INSTALLED SEQUENCE NUMBERS & ITEM 3. NUMBER REQUIRED FOR DISPATCH 4. REMARKS AND EXCEPTIONS 23 COMMUNICATIONS -02 D - 0 May be inoperative provided system is I not required by 14 CFR. I -50-01 Flight Deck Headset I Earphone/Headphone and I Boom Microphone I -01 Headset Boom Microphone -10 A - 0 May be inoperative provided: I a) Hand microphone is installed and I operates normally, I b) Repairs are made within three I flight days, and I c) Aircraft is not operated single I pilot. I -20 D - - Any in excess of those required by 14 I CFR may be inoperative. I -02 Headset Earphones/Headphone -10 C - 1 May be inoperative provided associated I cockpit speaker operates normally. I -20 D - - Any in excess of those required by 14 I CFR may be inoperative. I -03 Active Noise D - 0 May be inoperative provided normal I *** Canceling/Reduction audio function of headset is operative. I Function I -04 Headset Audio System C - - May be inoperative provided associated I cockpit speaker is operative and used. I -50-02 Hand Microphone C 1 0 May be inoperative provided an operative I headset boom microphone(s) is available. I -50-03 Hand Microphone Jack C 1 0 May be inoperative provided an operative I headset boom microphone(s) is available. I -50-04 Hand Microphone Holder C 1 0 (O) May be inoperative provided hand I Microphone is secured by alternate I means. I -50-05 Audio Control Panel
-01 INTR COM Button D 2 0 May be inoperative for single pilot I operations. I -02 PLAY Button D 2 0 I U.S. DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST FEDERAL AVIATION ADMINISTRATION AIRCRAFT: REVISION NO. 1 PAGE NO. CESSNA 510 DATE: 04/04/2013 23-3 1. REPAIR CATEGORY SYSTEM, 2. NUMBER INSTALLED SEQUENCE NUMBERS & ITEM 3. NUMBER REQUIRED FOR DISPATCH 4. REMARKS AND EXCEPTIONS 23 COMMUNICATIONS -03 COM1, COM2, COM3 MIC C 6 0 May be inoperative provided crew refers I Annunciator to PFD frequency boxes for active I transmit frequency (shown in green). I -04 MKR/MUTE Button C 2 0 May be inoperative provided: I a) Approach procedures do not I require its use, and I b) System is not required by 14 CFR. I -05 HI SENS Button (Marker C 2 0 May be inoperative provided approach I Beacon Hi Sensitivity) procedures do not require its use. I -06 DME Button C 2 0 May be inoperative provided procedures I do not require its use. I -07 NAV1, NAV2 Button C 4 0 May be inoperative provided procedures I do not require its use. I -50-06 Cockpit Speaker C 2 1 One may be inoperative provided: I a) Affected speaker is not required I for procedures, and I b) A headset is used for associated I inoperative speaker including I during emergency procedures. I -60-01 Static Wick I -01 Aileron C 2 1 One may be damaged or missing I (Each side) provided outermost wick is installed and I not damaged. I -02 Wing Tip Assembly - 1 1 | (Each side) | -03 Elevator C 3 1 Two may be damaged or missing I (Each side) provided outermost wick is installed and | not damaged. | -04 Vertical Stabilizer - 1 1 | -05 Rudder C 2 1 One may be damaged or missing I provided uppermost wick is installed and | not damaged. | -06 Stinger - 1 1 | -70-01 Cockpit Voice Recorder I *** I -01 With Flight Data Recorder A - 0 May be inoperative provided: I Installed a) Flight data recorder operates I normally, and I b) Repairs are made within three I flight days. I U.S. DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST FEDERAL AVIATION ADMINISTRATION AIRCRAFT: REVISION NO. 1 PAGE NO. CESSNA 510 DATE: 04/04/2013 23-4 1. REPAIR CATEGORY SYSTEM, 2. NUMBER INSTALLED SEQUENCE NUMBERS & ITEM 3. NUMBER REQUIRED FOR DISPATCH 4. REMARKS AND EXCEPTIONS 23 COMMUNICATIONS -02 For an Operator other than A - 0 May be inoperative provided repairs are I a Holder of an Air Carrier or made in accordance with 14 CFR. I Commercial Operator I Certificate I -03 Independent Power Source C - 0 I U.S. DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST FEDERAL AVIATION ADMINISTRATION AIRCRAFT: REVISION NO. 1 PAGE NO. CESSNA 510 DATE: 04/04/2013 24-1 1. REPAIR CATEGORY SYSTEM, 2. NUMBER INSTALLED SEQUENCE NUMBERS & ITEM 3. NUMBER REQUIRED FOR DISPATCH 4. REMARKS AND EXCEPTIONS 24 ELECTRICAL POWER -31-01 Battery Temperature C 1 0 I *** Indication (Aircraft equipped I with Lead-Acid Battery) I -37-01 DC Generator Current B 2 1 One may be inoperative provided GEN I Display (AMPS) OFF L-R amber message is monitored. I (EICAS Indication) | -40-01 External Power System C 1 0 I -60-01 Cockpit 12V Outlet -01 C - 0 (O) May be inoperative provided alternate I procedures are established and used. I -02 D - 0 May be inoperative provided procedures I do not require its use. I -60-02 Interior Disconnect -01 C 1 0 (M) (O) May be inoperative provided: I a) Interior power system is I deactivated, I b) Passengers are briefed on I disabled cabin electrical systems, I and I c) Cabin interior lighting, I cockpit/cabin 12V outlets, and I cabin audio are considered I inoperative. -02 C 1 0 (M) May be inoperative provided: I a) Interior power system is I deactivated, I b) Passengers are not carried, and I c) Cabin interior lighting, I cockpit/cabin 12V outlets, and I cabin audio are considered I inoperative. I U.S. DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST FEDERAL AVIATION ADMINISTRATION AIRCRAFT: REVISION NO. 1 PAGE NO. CESSNA 510 DATE: 04/04/2013 25-1 1. REPAIR CATEGORY SYSTEM, 2. NUMBER INSTALLED SEQUENCE NUMBERS & ITEM 3. NUMBER REQUIRED FOR DISPATCH 4. REMARKS AND EXCEPTIONS 25 EQUIPMENT/FURNISHINGS -00-01 Document Holder D 1 0 (O) May be missing or inoperative I (Airworthiness Certificate, provided an alternate means of securing I Registration, Etc.) and displaying required documents is I used. I -10-01 Flight Crew Seat I (per seat) I -01 Armrest -10 C 1 0 May be inoperative provided affected I armrest is stowed in retracted position. I -20 C 1 0 (M) May be inoperative provided affected I armrest is removed. I -02 Lumbar Support C 1 0 I *** I -03 Recline/Tilt Function C 1 0 (O) May be inoperative provided: I a) Affected seat is failed in a position I that permits normal visibility, I b) Full flight control movement is I available, and I c) Crewmember can reach all I necessary controls and equipment I while restrained. I -04 Restraint Buckle Protective C - 0 I *** Padding I -05 Vertical Adjustment C 1 0 (O) May be inoperative provided: I a) Affected seat is failed in a position I that permits normal visibility, I b) Full flight control movement is I available, and I c) Crewmember can reach all I necessary controls and equipment I while restrained. I -06 Copilot Seat Belt/Shoulder C 1 0 May be inoperative provided seat remains I Harness unoccupied. I -10-02 Cockpit Sun Visor System C 2 0 May be missing or inoperative provided I and/or Attachment pilot’s field of vision is not obstructed. I Mechanism I -10-03 Cockpit Assist Handle D 1 0 I -10-04 Yoke Mounted Chart Holder C 2 0 I -10-05 Emergency Gear Handle C 1 0 May be missing or inoperative provided I Cover cover is removed. I U.S. DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST FEDERAL AVIATION ADMINISTRATION AIRCRAFT: REVISION NO. 1 PAGE NO. CESSNA 510 DATE: 04/04/2013 25-2 1. REPAIR CATEGORY SYSTEM, 2. NUMBER INSTALLED SEQUENCE NUMBERS & ITEM 3. NUMBER REQUIRED FOR DISPATCH 4. REMARKS AND EXCEPTIONS 25 EQUIPMENT/FURNISHINGS -20-01 Passenger Seat C - - May be inoperative provided: a) Seat does not block an I emergency exit, b) Seat does not restrict any cabin I occupant access to main aircraft I aisle, c) Affected seat(s) are blocked and placarded “DO NOT OCCUPY”, and d) A seat with an inoperative seat I belt or shoulder harness is I considered inoperative. I NOTE: Affected seat(s) may include seats near inoperative seat(s). -01 Armrest D - - (M) May be inoperative or missing and I seat occupied provided: I a) Armrest does not block an I emergency exit, I b) Armrest does not restrict any I passenger from access to aisle, I and I c) If armrest is missing, reclining I seat is secured in full upright I position. I -02 Headrest -10 C - - May be inoperative and seat occupied I provided headrest is failed in placarded I taxi, takeoff and landing position. I -20 D - - May be missing or inoperative in other I than placarded taxi, takeoff, and landing I position provided affected seat is I considered inoperative. I -03 Recline Mechanism -10 C - - May be inoperative and seat occupied provided seat back is immovable in the I full upright position. -20 D - - (M) May be inoperative and seat I occupied provided seat is secured in full I upright position. I (Continued) U.S. DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST FEDERAL AVIATION ADMINISTRATION AIRCRAFT: REVISION NO. 1 PAGE NO. CESSNA 510 DATE: 04/04/2013 25-3 1. REPAIR CATEGORY SYSTEM, 2. NUMBER INSTALLED SEQUENCE NUMBERS & ITEM 3. NUMBER REQUIRED FOR DISPATCH 4. REMARKS AND EXCEPTIONS 25 EQUIPMENT/FURNISHINGS -20-01 Passenger Seat (Continued) -04 Seat Belt/Shoulder Harness D - - May be inoperative provided affected seat I is blocked and placarded "DO NOT I OCCUPY". I -05 Seat Belt/Shoulder Harness D - - I Keeper I -06 Lumbar Support D - - I -20-02 Folding Cabin Seat C 1 0 May be inoperative provided: I *** a) Seat does not block an I emergency exit, I b) Seat does not restrict any cabin I occupant access to main aircraft I aisle, I c) Affected seat(s) are blocked and I placarded “DO NOT OCCUPY”, I and I d) A seat with an inoperative seat I belt or shoulder harness is I considered inoperative. I NOTE: Affected seat(s) may include I seats near inoperative seat(s). I -20-03 Cabin Curtain C 2 0 May be missing or inoperative provided I curtain remains secured open. I -20-04 Non-Essential Equipment & - - 0 May be inoperative, damaged or missing I Furnishings (NEF) provided that the item(s) is deferred in I accordance with the NEF deferral I program. The NEF program, procedures I and processes are outlined in the I operator’s (insert name) Manual. (M) and I (O) procedures, if required, must be I available to the flight crew and included in I the operator’s appropriate document. I I NOTE: Exterior lavatory door ash trays I are not NEF items. I -30-01 Cabin Storage Compartment U.S. DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST FEDERAL AVIATION ADMINISTRATION AIRCRAFT: REVISION NO. 1 PAGE NO. CESSNA 510 DATE: 04/04/2013 25-4 1. REPAIR CATEGORY SYSTEM, 2. NUMBER INSTALLED SEQUENCE NUMBERS & ITEM 3. NUMBER REQUIRED FOR DISPATCH 4. REMARKS AND EXCEPTIONS 25 EQUIPMENT/FURNISHINGS -01 C - - (M) May be inoperative provided: I a) Compartment does not contain I any aircraft system protection I devices, I b) Any emergency equipment I located in affected compartment is I considered inoperative, I c) Affected compartment is not used I for storage of any item except for I those permanently affixed, I d) Procedures are established and I used to secure compartment I closed, and I e) Affected compartment is I prominently placarded “DO NOT I USE”. I -02 C - - (M) (O) May be inoperative provided: I a) Affected door is removed, I b) Affected compartment is not used I for storage of any item, except I those permanently affixed, I c) Cabin occupants are briefed that I affected compartment may not be I used, I d) Affected compartment is I prominently placarded “DO NOT I USE”, and I e) Any permanently affixed I emergency equipment located in I affected compartment is available I for use. I -03 Shelving D - - May be inoperative provided any I permanently affixed emergency I equipment located on affected shelving is I relocated and available for use. I -30-02 Storage Compartment D - 0 May be inoperative in unlocked position. I *** Key Lock I -40-01 Ashtray A - 1 May be inoperative or missing provided it I *** is replaced within three calendar days. I 50-01 Cargo Restraint System C - - May be inoperative or missing provided cargo compartment remains empty. U.S. DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST FEDERAL AVIATION ADMINISTRATION AIRCRAFT: REVISION NO. 1 PAGE NO. CESSNA 510 DATE: 04/04/2013 25-5 1. REPAIR CATEGORY SYSTEM, 2. NUMBER INSTALLED SEQUENCE NUMBERS & ITEM 3. NUMBER REQUIRED FOR DISPATCH 4. REMARKS AND EXCEPTIONS 25 EQUIPMENT/FURNISHINGS -60-01 Emergency Medical I *** Equipment I -01 Automatic External D - 0 I Defibrillator and/or I Associated Equipment I -02 Emergency Medical Kit D - 0 I (EMK) and/or Associated Equipment -03 First Aid Kit (FAK) and/or D - - Any in excess of those required by 14 I Associated Equipment CFR may be incomplete, missing, or I inoperative. I -61-01 Life Preservers D - 0 Any in excess of those required by 14 I *** (Crew And Passenger) CFR may be inoperative or missing. I -62-01 Emergency Locator *** Transmitter I (ELT) -01 Survival Type ELT D - - Any in excess of those required by 14 I CFR may be inoperative or missing. I -02 Fixed ELT -10 A - 0 (M) May be inoperative provided: I a) System is deactivated, and I b) Repairs are made within 90 days. I -20 A - 0 May be missing provided repairs are I made within 90 days. I -30 D - - (M) Any in excess of those required by 14 I CFR may be inoperative provided system I is deactivated. I -40 D - - Any in excess of those required by 14 I CFR may be missing. I -64-01 Life Raft D - - Any in excess of those required by 14 I *** CFR may be inoperative or missing. I U.S. DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST FEDERAL AVIATION ADMINISTRATION AIRCRAFT: REVISION NO. 1 PAGE NO. CESSNA 510 DATE: 04/04/2013 26-1 1. REPAIR CATEGORY SYSTEM, 2. NUMBER INSTALLED SEQUENCE NUMBERS & ITEM 3. NUMBER REQUIRED FOR DISPATCH 4. REMARKS AND EXCEPTIONS 26 FIRE PROTECTION -22-01 Portable Fire Extinguisher D - 1 (O) Any in excess of those required by 14 I CFR may be inoperative or missing I provided: a) Inoperative portable fire extinguisher is tagged inoperative, removed from installed location and stored out of sight so it cannot be mistaken for a functional unit, b) Required distribution is maintained, and c) At least one operable portable fire I extinguisher must be located in I cockpit. I U.S. DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST FEDERAL AVIATION ADMINISTRATION AIRCRAFT: REVISION NO. 1 PAGE NO. CESSNA 510 DATE: 04/04/2013 27-1 1. REPAIR CATEGORY SYSTEM, 2. NUMBER INSTALLED SEQUENCE NUMBERS & ITEM 3. NUMBER REQUIRED FOR DISPATCH 4. REMARKS AND EXCEPTIONS 27 FLIGHT CONTROLS 31-01 Electric Elevator Trim C 1 0 (M) May be inoperative provided: a) Electric trim system is deactivated, b) Manual trim is operative and unaffected, and c) Autopilot is considered I inoperative. I -60-01 Speed Brake Actuation B 1 0 (M) (O) May be inoperative provided: I System a) Speed brakes are deactivate, (Failed in retracted position) b) Steep approaches are not performed, and I c) Operations are limited to VMO of 240 KIAS. -60-02 Speed Brake Position B 1 0 May be inoperative provided speed brake I actuation system is considered I inoperative. I -60-03 Speed Brake Switch C 2 1 I -70-01 Aileron/Elevator Control C 1 0 (O) May be inoperative in unlocked I Lock position provided full flight control is I (Failed Unlocked) available. I -70-02 Rudder Lock C 1 0 (O) May be inoperative in unlocked I (Failed Unlocked) position provided full flight control is I available. I U.S. DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST FEDERAL AVIATION ADMINISTRATION AIRCRAFT: REVISION NO. 1 PAGE NO. CESSNA 510 DATE: 04/04/2013 28-1 1. REPAIR CATEGORY SYSTEM, 2. NUMBER INSTALLED SEQUENCE NUMBERS & ITEM 3. NUMBER REQUIRED FOR DISPATCH 4. REMARKS AND EXCEPTIONS 28 FUEL -10-01 Over-wing Refueling Cap D 2 0 May be inoperative in unlocked position. I Lock I -41-01 Fuel Low Level Indicating A 2 1 (O) One may be inoperative provided: I System a) Procedures for monitoring fuel I quantity are established and used, I and I b) Repairs are made within three I flight days. I U.S. DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST FEDERAL AVIATION ADMINISTRATION AIRCRAFT: REVISION NO. 1 PAGE NO. CESSNA 510 DATE: 04/04/2013 30-1 1. REPAIR CATEGORY SYSTEM, 2. NUMBER INSTALLED SEQUENCE NUMBERS & ITEM 3. NUMBER REQUIRED FOR DISPATCH 4. REMARKS AND EXCEPTIONS ICE AND RAIN 30 PROTECTION -10-01 Wing De-Ice Boot System C 1 0 (M) May be inoperative provided: I (Failure to inflate) a) All de-ice boots must be visually I verified to be deflated and held I down when service air system is I active, and I b) Aircraft is not operated in known, I forecast, or AFM-defined icing I conditions. I -10-02 Tail De-Ice Boot System C 1 0 (M) May be inoperative provided: I (Failure to inflate) a) All de-ice boots must be visually I verified to be deflated and held I down when service air system is I active, and I b) Aircraft is not operated in known, I forecast, or AFM-defined icing I conditions. I -20-01 Engine Anti-Ice System I -01 Failed On C 2 1 One may be inoperative provided: I (Flow) a) Both ENGINE ANTI-ICE switches I are selected ON, I b) Takeoff and landing performance I calculations for anti-ice on are I used, and I c) Aircraft are restricted to I temperature limitation in I accordance with AFM. I -02 Failed Off C 2 0 (M) May be inoperative provided: I (No Flow) a) Affected engine anti-Ice is I secured for no flow, and I b) Aircraft is not operated in known, I forecast, or AFM-defined icing I conditions. I -30-01 Copilot Pitot Heater System B 1 0 May be inoperative provided: I a) Aircraft is not operated in I Instrument Meteorological I Conditions (IMC), and I b) Aircraft is not operated in known, I forecast, or AFM-defined icing I conditions. I U.S. DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST FEDERAL AVIATION ADMINISTRATION AIRCRAFT: REVISION NO. 1 PAGE NO. CESSNA 510 DATE: 04/04/2013 30-2 1. REPAIR CATEGORY SYSTEM, 2. NUMBER INSTALLED SEQUENCE NUMBERS & ITEM 3. NUMBER REQUIRED FOR DISPATCH 4. REMARKS AND EXCEPTIONS ICE AND RAIN 30 PROTECTION -30-02 Copilot Static Port Heater B 2 1 One may be inoperative provided: a) Aircraft is not operated in I Instrument Meteorological I Conditions (IMC), I b) Aircraft is not operated in known, I forecast, or AFM-defined icing I conditions, and I c) Aircraft is not operated RVSM. I -30-03 Stall Warning Vane Heater C 1 0 May be inoperative provided aircraft is not I operated in known, forecast, or AFM- I defined icing conditions. I -40-01 Windshield Anti-Ice System C 2 0 (O) May be inoperative provided: I a) Aircraft is not operated in known, I forecast, or AFM-defined icing I conditions, and I b) Crew has a means to clear windshield of moisture. -40-02 Windshield Rain Repellant C 1 0 May be missing provided aircraft is not I operated in precipitation within five I nautical miles of airport used for takeoff I or intended landing. I -70-01 Air Conditioner Forward C 1 0 May be inoperative provided air I Evaporator Drain Heater conditioning system is considered I inoperative. I U.S. DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST FEDERAL AVIATION ADMINISTRATION AIRCRAFT: REVISION NO. 1 PAGE NO. CESSNA 510 DATE: 04/04/2013 31-1 1. REPAIR CATEGORY SYSTEM, 2. NUMBER INSTALLED SEQUENCE NUMBERS & ITEM 3. NUMBER REQUIRED FOR DISPATCH 4. REMARKS AND EXCEPTIONS INDICATING/RECORDING 31 SYSTEMS -20-01 Flight Hour Meter C 1 0 (O) May be inoperative provided flight I time is tracked by alternate means. I -30-01 Flight Data Recorder (FDR) *** System -01 (For a Holder of an Air A - 0 May be inoperative provided: I Carrier or Commercial a) Cockpit Voice Recorder (CVR) I Operator Certificate) operates normally, I b) Airplane is not dispatched from a I designated airport as listed in I operator’s MEL unless: I 1. FDR failure occurs after I dispatch but prior to I takeoff, or I 2. FDR repair was attempted I but was not successful. I c) In those cases where repair is I attempted but not successful, I aircraft may be dispatched on a I flight or series of flights until next I designated airport where repair I must be accomplished prior to I dispatch, and I d) Repairs are made within three I flight days. -10 FDR Recording Parameters A - - Up to three (3) recording parameters may I Required by 14 CFR be inoperative provided: I I a) Cockpit Voice Recorder (CVR) I operates normally, and I b) Repairs are made within 20 I calendar days. -20 FDR Recording Parameters A - - May be inoperative provided repairs are I Not Required by 14 CFR made prior to completion of next I scheduled inspection/check of system. I -02 (For an Operator other than A - 0 May be inoperative provided repairs are I a Holder of an Air Carrier or made in accordance with applicable 14 I Commercial Operator CFR. I Certificate) I -30-02 Quick Access Recorder C 1 0 I *** I -40-01 Electronic Checklist D 1 0 May be inoperative provided equivalent I *** checklist is used. I U.S. DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST FEDERAL AVIATION ADMINISTRATION AIRCRAFT: REVISION NO. 1 PAGE NO. CESSNA 510 DATE: 04/04/2013 31-2 1. REPAIR CATEGORY SYSTEM, 2. NUMBER INSTALLED SEQUENCE NUMBERS & ITEM 3. NUMBER REQUIRED FOR DISPATCH 4. REMARKS AND EXCEPTIONS INDICATING/RECORDING 31 SYSTEMS -40-02 Fuel Totalizer C 1 0 May be inoperative provided: I a) Fuel quantity indicating system is I operative, and I b) MFD map range rings and weight I planning functions are considered I inoperative. I -50-01 Master Warning System I -01 Master Warning Reset B 2 1 Pilot side must be operative for single I Annunciator pilot operations. I -02 Master Warning C 2 1 Pilot side must be operative for single I Cancel/Reset Function pilot operations. I -03 Master Caution Reset C 2 1 Pilot side must be operative for single I Annunciator pilot operations. I -04 Master Caution C 2 1 Pilot side must be operative for single I Cancel/Reset Function pilot operations. I -50-02 Cabin Altitude Warning C 1 0 May be inoperative provided: I System a) Cabin altitude warning is not I displayed, and I b) Aircraft is operated at 9,500 feet I MSL or below. I U.S. DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST FEDERAL AVIATION ADMINISTRATION AIRCRAFT: REVISION NO. 1 PAGE NO. CESSNA 510 DATE: 04/04/2013 32-1 1. REPAIR CATEGORY SYSTEM, 2. NUMBER INSTALLED SEQUENCE NUMBERS & ITEM 3. NUMBER REQUIRED FOR DISPATCH 4. REMARKS AND EXCEPTIONS 32 LANDING GEAR -41-01 Antiskid System C 1 0 (O) May be inoperative provided: I a) Aircraft is operated in accordance I with AFM DISPATCH WITH I ANTISKID SYSTEM I INOPERATIVE abnormal I procedure, and I b) Steep approaches are not I conducted. I NOTE: ANTISKID FAIL amber message I will appear. I -41-02 Tire Spin Down System C 1 0 (O) May be inoperative provided aircraft I is operated in accordance with AFM NO I TIRE SPINDOWN white CAS message I procedure is followed. I U.S. DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST FEDERAL AVIATION ADMINISTRATION AIRCRAFT: REVISION NO. 1 PAGE NO. CESSNA 510 DATE: 04/04/2013 33-1 1. REPAIR CATEGORY SYSTEM, 2. NUMBER INSTALLED SEQUENCE NUMBERS & ITEM 3. NUMBER REQUIRED FOR DISPATCH 4. REMARKS AND EXCEPTIONS 33 LIGHTS -10-01 Cockpit and Instrument C - - Individual lights may be inoperative I Lighting System provided remaining lights are: I (Excluding Internally Lighted a) Sufficient to clearly illuminate all I Annunciators and Buttons, required instruments, controls, I Standby Flight Instrument and other devices for which it is I Lighting, and STDBY provided, I ALT/AS Placard Lighting) b) Positioned so that direct rays are I shielded from crew members eyes, c) Lighting configuration and intensity is acceptable to crew, and d) Cockpit flood light is operative. I -10-02 Cockpit Flood Light C 1 0 May be inoperative provided aircraft is not I operated at night. I -10-03 Windshield Ice Detection Light -01 C 2 0 May be inoperative provided aircraft is not I operated at night. I -02 C 2 1 Right side may be inoperative for single I pilot operations. I -03 C 2 1 (O) One may be inoperative for two pilot I operations provided alternate procedures I are established and used. I -10-04 Cockpit Map Light -01 C 2 1 One may be inoperative provided cockpit I flood light is operative. I -02 C 2 0 May be inoperative provided cockpit flood I light is operative and a flashlight is I available to crew. I -10-05 G1000 Display Dimmer C 1 0 (O) May be inoperative providing display I (DISPLAYS knob) brightness is adjusted through G1000 I menu in manual mode. I -20-01 Lighted Passenger Information Sign (Excluding Cabin Exit Signs) U.S. DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST FEDERAL AVIATION ADMINISTRATION AIRCRAFT: REVISION NO. 1 PAGE NO. CESSNA 510 DATE: 04/04/2013 33-2 1. REPAIR CATEGORY SYSTEM, 2. NUMBER INSTALLED SEQUENCE NUMBERS & ITEM 3. NUMBER REQUIRED FOR DISPATCH 4. REMARKS AND EXCEPTIONS 33 LIGHTS -01 C - 0 (O) May be inoperative provided: I a) Alternate procedures are I established and used to alert I cabin occupants when PAX I SAFETY/SEAT BELT is selected, I and I b) Scheduled operations are not I conducted. I -02 C - 0 May be inoperative provided no cabin I occupants are carried. I -20-02 Cabin Interior Lighting C - - (O) Individual lights may be inoperative I System (Excluding provided cabin emergency lighting is I Emergency Lighting) verified operative. I -30-01 Aft Baggage Light C 1 0 I
-01 Door Proximity Switch C 1 0 (O) May be inoperative providing crew I makes sure light is selected OFF using I toggle switch. I -30-02 Nose Baggage C 1 0 Compartment Light -01 Door Proximity Switch -10 C 2 0 (O) May be inoperative providing crew I makes sure light is selected OFF using I rocker switch on light. I -20 C 2 1 I -40-01 Anti-Collision Light System A 1 0 May be inoperative provided: I (Wing Strobes) (ANTI a) All position (NAV) lights are I COLL) operative, I b) Ground recognition (BEACON) light is operative, and c) Repairs are made within three flight days. -40-02 Position Light System C 1 0 May be inoperative provided system is I (NAV) not required by 14 CFR. I -40-03 Wing Inspection Light C 1 0 May be inoperative provided: I (WING INSP) a) Aircraft is not operated at night, I and I b) Ground deicing procedures do not I require its use. I U.S. DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST FEDERAL AVIATION ADMINISTRATION AIRCRAFT: REVISION NO. 1 PAGE NO. CESSNA 510 DATE: 04/04/2013 33-3 1. REPAIR CATEGORY SYSTEM, 2. NUMBER INSTALLED SEQUENCE NUMBERS & ITEM 3. NUMBER REQUIRED FOR DISPATCH 4. REMARKS AND EXCEPTIONS 33 LIGHTS -40-04 Landing/Taxi/Recognition C 2 0 Any in excess of those required by 14 I Light (LANDING - RECOG CFR may be inoperative. I TAXI) I -40-05 Ground Recognition Light C 1 0 May be inoperative provided anti-collision (BEACON) light system is operative. I -50-01 Cockpit Flashlight and I *** Holder Assembly I -01 Flashlight D - - Any in excess of those required by 14 I CFR may be inoperative or missing. I -02 Holder Assembly C - - May be inoperative provided associated I flashlight is stowed by alternate means. I U.S. DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST FEDERAL AVIATION ADMINISTRATION AIRCRAFT: REVISION NO. 1 PAGE NO. CESSNA 510 DATE: 04/04/2013 34-1 1. REPAIR CATEGORY SYSTEM, 2. NUMBER INSTALLED SEQUENCE NUMBERS & ITEM 3. NUMBER REQUIRED FOR DISPATCH 4. REMARKS AND EXCEPTIONS 34 NAVIGATION -23-01 Non-Stabilized Magnetic Compass -01 B 1 0 (O) May be inoperative provided: a) Both AHRS heading information sources are operative, b) Aircraft is operated with dual independent navigation capability, c) Flight is conducted under positive radar control by ATC during en route portion of flight, and d) MFD nav range ring is selected ON and reference to magnetic north. -02 B 1 0 May be inoperative provided: a) Both AHRS heading information sources are operative, and b) Aircraft is not operated at night or I in IFR conditions. I -25-01 MFD Remote Mounted B 1 0 (O) May be inoperative provided: Control Panel a) Weather radar is considered inoperative, b) Datalink is considered inoperative, c) Electronic chart is considered inoperative, d) Procedures do not require use of MFD, e) Aircraft is operated in Visual Meteorological Conditions (VMC), f) Aircraft is not operated at night, g) PFD Inset maps are used, and h) Alternate procedures are established and used. NOTE: MFD navigation is disabled. -01 Individual buttons C - 0 NOTE: Corresponding buttons/knobs I (CRSR, ,D>, MENU, FPL, on PFD must be operative for I PROC, BACK, SPC, CLR, relief, if applicable. I SEL, <, >, A-Z, 1-0, +/-, and I period) I (Except ENT, Range/PUSH I PAN, and FMS I Knobs/PUSH CRSR) I 25-02 Mode Control Panel I U.S. DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST FEDERAL AVIATION ADMINISTRATION AIRCRAFT: REVISION NO. 1 PAGE NO. CESSNA 510 DATE: 04/04/2013 34-2 1. REPAIR CATEGORY SYSTEM, 2. NUMBER INSTALLED SEQUENCE NUMBERS & ITEM 3. NUMBER REQUIRED FOR DISPATCH 4. REMARKS AND EXCEPTIONS 34 NAVIGATION -01 Yaw Damper Button C 1 0 NOTE 1: Yaw damper may be engaged I (YD) by engaging autopilot. I NOTE 2: Yaw damper may be I disengaged by pushing AP I TRIM DISC button. I -02 Course Knob Push Direct C 2 0 I Function I (CRS1 or CRS2 PUSH DIR) I -03 Bank Button C 1 0 I (BANK) I -04 HDG Knob PUSH SYNC C 1 0 I Function I -05 Vertical Mode Button I (FLC, ALT, VNV, VS) I -10 C 4 3 I -20 B 4 0 May be inoperative provided: I a) Flight director is considered I inoperative, and I b) Autopilot is considered I inoperative. I -06 Speed Button (SPD) C 1 0 I -07 Lateral Mode Buttons (NAV, B 4 0 May be inoperative provided: I HDG, APR, BC) a) Flight director is considered I inoperative, and I b) Autopilot is considered I inoperative. I -08 Annunciator LEDs and XFR D 13 0 NOTE: PFDs are primary source for I Arrows armed and active mode indications. I -09 XFR Button B 1 0 May be inoperative provided: I a) FD Indicator Arrow is pointing to I LH side if operated single pilot, or I b) Pilot flying must be seated in side I FD Indicator Arrow is pointing to if I operated dual pilot. I -25-03 Synthetic Vision C 1 0 May be inoperative provided procedures I *** do not require its use. I -25-04 Moving Map Display C 3 0 May be inoperative provided procedures I do not require its use. I -25-05 Primary Flight Display (PFD) I -01 Copilot’s BARO Knob and C 1 0 May be inoperative for single pilot I PUSH STD Function operations. I U.S. DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST FEDERAL AVIATION ADMINISTRATION AIRCRAFT: REVISION NO. 1 PAGE NO. CESSNA 510 DATE: 04/04/2013 34-3 1. REPAIR CATEGORY SYSTEM, 2. NUMBER INSTALLED SEQUENCE NUMBERS & ITEM 3. NUMBER REQUIRED FOR DISPATCH 4. REMARKS AND EXCEPTIONS 34 NAVIGATION -02 RANGE/PAN Knob/Joystick C 2 0 May be inoperative provided procedures I do not require its use. I -03 D>, FPL, PROC Button C 6 0 May be inoperative provided I corresponding button(s) on MFD remote I mounted control panel are operative. I -04 Copilot’s Comm Swap C 1 0 May be inoperative for single pilot I Button (Hold for EMERG) operations. I -31-01 Navigation System (VHF) -01 VOR C - - May be inoperative provided: a) Affected system is not on the emergency bus, b) Procedures do not require its use, and c) System is not required by 14 CFR. -02 Localizer C - - May be inoperative provided: a) Affected system is not on the emergency bus, b) Procedures do not require its use, c) System is not required by 14 CFR, and d) Associated glideslope is considered inoperative. -03 Glideslope C - - May be inoperative provided: I a) Affected system is not on the I emergency bus, I b) Approach procedures do not I require its use, and I c) System is not required by 14 CFR. I -34-01 Marker Beacon Receiver C 1 0 May be inoperative provided: System a) Approach procedures do not require its use, and b) System is not required by 14 CFR. I -42-01 Weather Radar System C 1 0 May be inoperative provided system is I not required by 14 CFR. I U.S. DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST FEDERAL AVIATION ADMINISTRATION AIRCRAFT: REVISION NO. 1 PAGE NO. CESSNA 510 DATE: 04/04/2013 34-4 1. REPAIR CATEGORY SYSTEM, 2. NUMBER INSTALLED SEQUENCE NUMBERS & ITEM 3. NUMBER REQUIRED FOR DISPATCH 4. REMARKS AND EXCEPTIONS 34 NAVIGATION -43-01 Altitude Alerting System A 1 0 (O) May be inoperative provided: a) Altitude pre-select function is I operative, I b) Aircraft is not operated RVSM, I c) Aircraft does not depart from a I designated airport (as listed in I operator’s MEL) where repair or I replacement can be made, I d) Autopilot with altitude hold and capture operates normally, and I e) Repairs are made within three flight days. -44-01 Radar Altimeter System A 1 0 May be inoperative provided: I *** a) Approach minimums or operating I procedures do not require its use, I b) TCAS II, if installed, is considered I inoperative, and I c) Repairs are made within two flight I days. I -44-02 Terrain Awareness And I Warning System (TAWS) – I Class B -01 C 1 0 May be inoperative provided system is I not required by 14 CFR. I -02 C 1 0 (O) May be inoperative provided alternate procedures are established and used. NOTE: Any mode that operates normally may be used. -03 Forward Looking Terrain B 1 0 I Avoidance Mode I -04 Premature Descent Alert B 1 0 I Mode I -05 Advisory Callouts I -10 B - 0 (O) May be inoperative provided alternate I procedures are established and used. I -20 C - 0 (O) May be inoperative provided: I a) Advisory callout not required by I 14 CFR, and I b) Alternate procedures are I established and used. I (Continued) U.S. DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST FEDERAL AVIATION ADMINISTRATION AIRCRAFT: REVISION NO. 1 PAGE NO. CESSNA 510 DATE: 04/04/2013 34-5 1. REPAIR CATEGORY SYSTEM, 2. NUMBER INSTALLED SEQUENCE NUMBERS & ITEM 3. NUMBER REQUIRED FOR DISPATCH 4. REMARKS AND EXCEPTIONS 34 NAVIGATION -44-02 Terrain Awareness And Warning System (TAWS) – Class B (Continued) -06 Excessive Descent Rate A 1 0 (O) May be inoperative provided: I Mode a) Alternate procedures are I established and used, and I b) Repairs are made within two flight I days. I -07 Negative Climb Rate or A 1 0 (O) May be inoperative provided: I Altitude Loss After Takeoff c) Alternate procedures are I Mode established and used, and I d) Repairs are made within two flight I days. I -45-01 Traffic Alert and Collision I Avoidance System (TCAS) I -01 TCAS II I *** I -10 Combined Traffic Alert (TA) C - 1 May be inoperative on the pilot not flying I and Resolution Advisory side provided: I (RA) Dual Display System a) TA and RA visual display is I operative on the pilot flying side, I and I b) TA and RA audio function is I operative on pilot flying side. I -20 Audio Function B - 0 May be inoperative provided procedures I do not require use of TCAS II. I -30 Airspace Selection Function C - 0 I -02 Traffic Alert System (TAS) C - 0 May be inoperative provided en route or I *** approach procedures do not require use I of TAS. I -45-02 Traffic Information System C 1 0 I (TIS) I -45-03 Traffic Collision Avoidance C 1 0 I *** Device (TCAD) I -51-01 Distance Measuring D - - Any in excess of those required by 14 I Equipment System (DME) CFR may be inoperative. I -52-01 ATC Transponders and Automatic Altitude Reporting System U.S. DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST FEDERAL AVIATION ADMINISTRATION AIRCRAFT: REVISION NO. 1 PAGE NO. CESSNA 510 DATE: 04/04/2013 34-6 1. REPAIR CATEGORY SYSTEM, 2. NUMBER INSTALLED SEQUENCE NUMBERS & ITEM 3. NUMBER REQUIRED FOR DISPATCH 4. REMARKS AND EXCEPTIONS 34 NAVIGATION -01 D - 1 Any in excess of those required by 14 I CFR may be inoperative. I -02 B 2 0 May be inoperative provided: a) Operations do not require its use, I b) Prior to flight, approval is obtained from ATC facilities having jurisdiction over planned route of flight, c) Aircraft is not operated RVSM, I and I d) Traffic Alert and Collision I Avoidance System (TCAS II) is I considered inoperative. -03 Elementary and Enhanced A 2 0 May be inoperative provided: I Downlink Aircraft Reportable a) Operations do not require its use, I Parameters Not Required and I By 14 CFR b) Repairs are made prior to I completion of next scheduled I inspection/check of system. I -04 ADS-B Squitter A - 0 May be inoperative provided: I *** Transmissions a) Operations do not require its use, I and I b) Repairs are made prior to I completion of next scheduled I inspection/check of system. I -52-02 Automatic Dependent D - 0 May be inoperative provided system is I Surveillance-Broadcast not required by 14 CFR. I (ADS-B) System I NOTE: If ADS-B is installed in lieu of or I as a replacement for 14 CFR I required equipment, repair I category in operator’s MEL will I be the same as that of 14 CFR I required equipment. I -01 Cockpit Display and Traffic D - 0 NOTE: CDTI display of data from other I Information (CDTI) aircraft systems may be used. I (Continued) -52-02 Automatic Dependent Surveillance-Broadcast (ADS-B) System (Continued) U.S. DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST FEDERAL AVIATION ADMINISTRATION AIRCRAFT: REVISION NO. 1 PAGE NO. CESSNA 510 DATE: 04/04/2013 34-7 1. REPAIR CATEGORY SYSTEM, 2. NUMBER INSTALLED SEQUENCE NUMBERS & ITEM 3. NUMBER REQUIRED FOR DISPATCH 4. REMARKS AND EXCEPTIONS 34 NAVIGATION -02 CDTI Control Panel D - 0 May be inoperative provided: I a) Flight ID can be set, and I b) Screen display is acceptable to I flight crew. I -03 Data Link Transmitter D - 0 NOTE: In some aircraft, data link I transmission is an integral part of I the transponder and relief is I provided in that section. I -04 Data Link Receiver D - 0 I -05 ADS-B Application D - 0 I -55-01 Automatic Direction Finding D - - Any in excess of those required by 14 I *** System (ADF) CFR may be inoperative. I -57-01 Navigation Equipment C - - Any in excess of those required by 14 I (GPS, FMS) CFR may be inoperative. I -60-01 Flight Management System A - - May be expired provided aircraft is I (FMS) Navigation Database operated in accordance with applicable I AFM limitations. I -60-02 Data Loader (SD Card Slot) C - - NOTE: Certain card slots are used for I real-time data access. If I inoperative, the associated I features are considered I inoperative. I U.S. DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST FEDERAL AVIATION ADMINISTRATION AIRCRAFT: REVISION NO. 1 PAGE NO. CESSNA 510 DATE: 04/04/2013 35-1 1. REPAIR CATEGORY SYSTEM, 2. NUMBER INSTALLED SEQUENCE NUMBERS & ITEM 3. NUMBER REQUIRED FOR DISPATCH 4. REMARKS AND EXCEPTIONS 35 OXYGEN -00-01 Oxygen Tank Fill Port C 1 0 (M) May be inoperative provided bottle is I filled using alternate means when service I is required. I -00-02 Plastic Blowout Disc/Green C 1 0 (O) May be missing or damaged provided I Label oxygen pressure is verified prior to each I flight. I -20-01 Passenger Oxygen System C 1 0 May be inoperative provided: a) No cabin occupants are carried, I and b) Crew oxygen system is operative. I -01 Cabin Mask C 5 0 Individual oxygen masks or dispensers I may be inoperative or missing provided I associated seats are placarded “DO NOT I OCCUPY”. I -02 Drop Out Panel C 5 0 (M) Individual panels may be out of I normal position provided: I a) Oxygen masks and drop out panel I are removed, and I b) Associated seats are placarded I “DO NOT OCCUPY”. I -30-01 Protective Breathing D - - Any in excess of those required by CFR I *** Equipment (PBE) may be inoperative or removed provided I location placarding is removed or I obscured. I -30-02 Portable Oxygen Bottles C - - Any in excess of those required by 14 I *** CFR may be inoperative provided: I a) Required distribution of I serviceable bottles is maintained I throughout the aircraft, and I b) Bottles not properly serviced are I replaced, serviced or removed at I next available maintenance I facility. I U.S. DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST FEDERAL AVIATION ADMINISTRATION AIRCRAFT: REVISION NO. 1 PAGE NO. CESSNA 510 DATE: 04/04/2013 38-1 1. REPAIR CATEGORY SYSTEM, 2. NUMBER INSTALLED SEQUENCE NUMBERS & ITEM 3. NUMBER REQUIRED FOR DISPATCH 4. REMARKS AND EXCEPTIONS 38 WATER/WASTE -30-01 Lavatory C 1 0 (O) Individual components may be I inoperative provided: I a) Cabin occupants are briefed I prior to each flight that toilet is I inoperative and unusable, and I b) Lavatory is placarded "DO I NOT USE TOILET". I U.S. DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST FEDERAL AVIATION ADMINISTRATION AIRCRAFT: REVISION NO. 1 PAGE NO. CESSNA 510 DATE: 04/04/2013 45-1 1. REPAIR CATEGORY SYSTEM, 2. NUMBER INSTALLED SEQUENCE NUMBERS & ITEM 3. NUMBER REQUIRED FOR DISPATCH 4. REMARKS AND EXCEPTIONS CENTRAL MAINTENANCE 45 SYSTEM (CMS) -00-01 Citation Diagnostics and C 1 0 May be inoperative provided procedures I Maintenance System do not require its use. I (CDMS) I U.S. DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST FEDERAL AVIATION ADMINISTRATION AIRCRAFT: REVISION NO. 1 PAGE NO. CESSNA 510 DATE: 04/04/2013 46-1 1. REPAIR CATEGORY SYSTEM, 2. NUMBER INSTALLED SEQUENCE NUMBERS & ITEM 3. NUMBER REQUIRED FOR DISPATCH 4. REMARKS AND EXCEPTIONS 46 INFORMATION SYSTEMS -00-01 Electronic Flight Bag (EFB) I *** System I -01 Class 3 EFB I -10 D - 0 May be inoperative provided procedures I do not require its use. I -20 C - - (O) May be inoperative provided alternate I procedures are established and used. I NOTE: Any function, program or I document which operates I normally may be used. I -02 Data Connectivity I (Class 2) I -10 D - - May be inoperative provided procedures I do not require its use. I -20 C - - (O) May be inoperative provided alternate I procedures are established and used. I -03 Power Connection I (Class 1 & 2) I -10 D - 0 May be inoperative provided procedures I do not require its use. I -20 C - - (O) May be inoperative provided alternate I procedures are established and used. I -04 Mounting Device (Class 2) -10 D - 0 (M) May be inoperative provided: I a) Associated EFB and hardware is I secured by an alternate means or I removed from aircraft, and I b) Procedures do not require its use. I -20 C - 0 (M) (O) May be inoperative provided: I a) Associated EFB and hardware is I secured by an alternate means or I removed from aircraft, and I b) Alternate procedures are I established and used. I U.S. DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST FEDERAL AVIATION ADMINISTRATION AIRCRAFT: REVISION NO. 1 PAGE NO. CESSNA 510 DATE: 04/04/2013 52-1 1. REPAIR CATEGORY SYSTEM, 2. NUMBER INSTALLED SEQUENCE NUMBERS & ITEM 3. NUMBER REQUIRED FOR DISPATCH 4. REMARKS AND EXCEPTIONS 52 DOORS -10-01 Cabin Door I -01 Seal C 1 0 May be inoperative or unserviceable (Unpressurized) provided: a) Seal does not interfere with door operation, and b) Cabin pressurization system is I considered inoperative. I -02 Key Lock D 1 0 May be inoperative in unlocked position. I -03 Gust Lock B 1 0 (O) May be inoperative provided a I procedure is developed and used to I prevent unrestricted movement of cabin I door. I -04 Pull Chain C 1 0 May be inoperative provided damage or I missing chain does not interfere with door I operation. I -05 Step Assembly C 1 0 (M) (O) May be inoperative provided: I a) Step support cables are removed, I b) Step assembly is removed, and I c) Alternate procedures for I entering/exiting aircraft are I established and used. I -06 Step Support Cable C 2 0 (M) (O) May be inoperative provided: I a) Step support cables are removed, I b) Step assembly is removed, and I c) Alternate procedures for I entering/exiting aircraft are I established and used. I -20-01 Escape Hatch Pin C 1 0 May be missing or inoperative with hatch I in unlocked position. I -30-01 Baggage Door I -01 Aft Door Key Lock C 1 0 May be inoperative in unlocked position I provided door is verified closed and I latched prior to flight. I -02 Nose Door Key Lock -10 C 2 0 May be inoperative in unlocked position I provided door is verified closed and I latched prior to flight. I U.S. DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST FEDERAL AVIATION ADMINISTRATION AIRCRAFT: REVISION NO. 1 PAGE NO. CESSNA 510 DATE: 04/04/2013 52-2 1. REPAIR CATEGORY SYSTEM, 2. NUMBER INSTALLED SEQUENCE NUMBERS & ITEM 3. NUMBER REQUIRED FOR DISPATCH 4. REMARKS AND EXCEPTIONS 52 DOORS -20 C 2 1 (O) One may be inoperative in locked position provided: a) Other side door key lock is not I failed in locked position, I b) Alternate procedures are I established and used to perform I required preflight actions, and I c) All latches are verified secured. I -03 Nose Door Gas Spring C 2 0 (O) May be inoperative or missing I provided precautions are taken when I opening door(s). I -04 Aft Door Gas Spring C 1 0 (O) May be inoperative or missing I provided precautions are taken when I opening door. I -05 Aft Door Seal C 1 0 (O) May be inoperative provided baggage I compartment is verified empty prior to I each flight. I -70-01 Door Monitoring System I -01 Cabin Door C 1 0 (O) May be inoperative provided: a) Door is verified closed and handle latched, b) 8 door pin indicators are visible in sight glass locations, and c) Interior door handle is secure. -02 Aft Door C 1 0 (O) May be inoperative provided door is verified secure and locked. -03 Nose Door C 2 0 (O) May be inoperative provided door is verified secure and locked. U.S. DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST FEDERAL AVIATION ADMINISTRATION AIRCRAFT: REVISION NO. 1 PAGE NO. CESSNA 510 DATE: 04/04/2013 73-1 1. REPAIR CATEGORY SYSTEM, 2. NUMBER INSTALLED SEQUENCE NUMBERS & ITEM 3. NUMBER REQUIRED FOR DISPATCH 4. REMARKS AND EXCEPTIONS ENGINE FUEL AND 73 CONTROL -31-01 Fuel Flow Indicating System B 2 1 (O) One may be inoperative provided a) Both fuel quantity indication systems are operative, and b) Navigation map fuel range rings I and weight planning functions are I considered inoperative. I U.S. DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST FEDERAL AVIATION ADMINISTRATION AIRCRAFT: REVISION NO. 1 PAGE NO. CESSNA 510 DATE: 04/04/2013 76-1 1. REPAIR CATEGORY SYSTEM, 2. NUMBER INSTALLED SEQUENCE NUMBERS & ITEM 3. NUMBER REQUIRED FOR DISPATCH 4. REMARKS AND EXCEPTIONS 76 ENGINE CONTROLS -01-01 Engine Synchronizer C 1 0 System (Failed Off) I U.S. DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST FEDERAL AVIATION ADMINISTRATION AIRCRAFT: REVISION NO. 1 PAGE NO. CESSNA 510 DATE: 04/04/2013 76-1 1. REPAIR CATEGORY SYSTEM, 2. NUMBER INSTALLED SEQUENCE NUMBERS & ITEM 3. NUMBER REQUIRED FOR DISPATCH 4. REMARKS AND EXCEPTIONS 76 ENGINE CONTROLS
SECTION TWO
CAS MESSAGE ORIENTED MMEL RELIEF U.S. DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST FEDERAL AVIATION ADMINISTRATION AIRCRAFT: REVISION NO. 1 PAGE NO. CESSNA 510 DATE: 04/04/2013 76-2 1. REPAIR CATEGORY SYSTEM, 2. NUMBER INSTALLED SEQUENCE NUMBERS & ITEM 3. NUMBER REQUIRED FOR DISPATCH 4. REMARKS AND EXCEPTIONS 76 ENGINE CONTROLS
INTRODUCTION
Two section MMELs are authorized by FAA PL 119. Section Two of two-section MMELs may grant relief for failure indications presented as CAS messages on Engine Indicating and Crew Alerting Systems (EICAS), or Electronic Centralized Aircraft Monitoring (ECAM), rather than the traditional relief (Section One) for failed equipment. New technology self-diagnostic tests eliminate the need for failure isolation procedures by maintenance personnel for many CAS messages. By using (O) procedures, the crew can complete selected system/component deactivation/re- configuration from the cockpit for which the crew has been trained.
Section Two will only contain CAS message relief if the crew can act on the item. CAS message relief must ensure safe operation of aircraft. Flight Operations Evaluation Boards (FOEB) will use the normal FOEB processes for determining which CAS messages go into each section.
TWO-SECTION MMEL GUIDANCE:
Modern technology CAS MMELs shall be divided into two sections.
A. Section One. Items which either require maintenance actions (this may include some CAS messages), or caution/advisory information. Section One will continue to use the existing Line Replaceable Units (LRU)-oriented MMEL format and should address the following type of equipment failures:
1. Failures which are not annunciated to crew; and
2. Failures which are annunciated, but the failure indication by itself is not considered sufficient to determine the aircraft airworthiness status.
B. Section Two. Includes only items where flight members may act on CAS messages. MMEL items where CAS messages can be used to determine the aircraft airworthiness should be formatted as follows:
1. It should have only two columns:
a. Column one should list the failure indications (messages) for which relief is given (if desired, the messages may be listed in alphabetical order with no ATA break down).
b. Column two should include the corresponding MMEL limitations and/or procedures. The format of this column should be in line with the format requirements of the “Remarks or U.S. DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST FEDERAL AVIATION ADMINISTRATION AIRCRAFT: REVISION NO. 1 PAGE NO. CESSNA 510 DATE: 04/04/2013 76-3 1. REPAIR CATEGORY SYSTEM, 2. NUMBER INSTALLED SEQUENCE NUMBERS & ITEM 3. NUMBER REQUIRED FOR DISPATCH 4. REMARKS AND EXCEPTIONS 76 ENGINE CONTROLS Exceptions” column of the conventional “LRU oriented” MMEL. Note: In many cases, CAS messages will not require maintenance to perform fault analysis. Relief provisos for these CAS items are expected to be more restrictive in content and repair interval, as compared to Section One relief provisos. U.S. DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST FEDERAL AVIATION ADMINISTRATION AIRCRAFT: REVISION NO. 1 PAGE NO. CESSNA 510 DATE: 04/04/2013 76-4 1. REPAIR CATEGORY SYSTEM, 2. NUMBER INSTALLED SEQUENCE NUMBERS & ITEM 3. NUMBER REQUIRED FOR DISPATCH 4. REMARKS AND EXCEPTIONS 76 ENGINE CONTROLS
2. Section Two CAS message relief items require flight crews to accomplish one or more steps to deactivate/re-configure the affected system prior to flight. The “(O)” indicates the need for these tasks. Tasks include, but are not necessarily limited to the following duties:
a. Procedures accomplished using cockpit (or cabin) system controls.
b. Deactivation of affected systems (by pulling system breaker or use of remote electronic system isolation);
c. Visual confirmation of remote gauge indications, or valve positions as provided by integral external indicators; and
d. Visual inspection behind panels (internal or external).
1) These panels must be accessible without tools via quick-release latches and must clearly indicate their unlocked or unsafe state (red/green safe window; flush fit latches - candidates to be verified at FOEB).
2) The visual inspection of compartments accessed by the panels is within the normal crew duty requirements for which they have been trained; and
3) The crew may use an external ladder for visual inspection behind panels as long as this procedure is within the normal crew duty requirements for which they have been trained. Special equipment such as maintenance stands and hydraulic lifts may not be used by the crew to perform visual inspections.
C. The following statement will be included on page 1 of Section Two in all two-section MMELs:
1. Section Two of the MMEL will list only Crew Alerting system (CAS) messages meeting the following requirements:
a. Equipment failure indications(s) that can be used to determine the airworthiness status of the airplane;
b. Messages that the crew can act upon from the cockpit with simple troubleshooting procedures without the assistance of a mechanic, and for which the crew has been trained.
c. Messages using the new self-diagnostic technology (virtual) actions for which the crew has been trained. U.S. DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST FEDERAL AVIATION ADMINISTRATION AIRCRAFT: REVISION NO. 1 PAGE NO. CESSNA 510 DATE: 04/04/2013 76-5 1. REPAIR CATEGORY SYSTEM, 2. NUMBER INSTALLED SEQUENCE NUMBERS & ITEM 3. NUMBER REQUIRED FOR DISPATCH 4. REMARKS AND EXCEPTIONS 76 ENGINE CONTROLS 2. CAS message relief items not meeting these requirements will be listed in Section One of the MMEL U.S. DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST FEDERAL AVIATION ADMINISTRATION AIRCRAFT: REVISION NO. 1 PAGE NO. CESSNA 510 DATE: 04/04/2013 2-1
PFD Messages / Flags Dispatch Consideration
AFCS flag on PFD Aircraft may be dispatched provided autopilot system is considered inoperative. TAWS FAIL Aircraft may be dispatched provided Terrain Awareness and Warning System (TAWS) is considered inoperative. *** TCAS FAIL Aircraft may be dispatched provided traffic alert (With TCAS II Installed) and collision avoidance system is considered inoperative. U.S. DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST FEDERAL AVIATION ADMINISTRATION AIRCRAFT: REVISION NO. 1 PAGE NO. CESSNA 510 DATE: 04/04/2013 2-2
MFD Messages / Flags Dispatch Consideration
RDR FAIL message on Aircraft may be dispatched provided weather radar page radar system is considered inoperative. RDR FAULT message Aircraft may be dispatched provided weather on radar page radar system is considered inoperative. STAB INOP message on Aircraft may be dispatched provided weather radar page radar system is considered inoperative. U.S. DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST FEDERAL AVIATION ADMINISTRATION AIRCRAFT: REVISION NO. 1 PAGE NO. CESSNA 510 DATE: 04/04/2013 2-3
White PFD Messages Dispatch Consideration
COM2 SERVICE Aircraft may be dispatched provided VHF *** COM3 SERVICE Communication system is considered inoperative. G/S1 FAIL Aircraft may be dispatched provided Glideslope G/S1 SERVICE is considered inoperative. G/S2 FAIL G/S2 SERVICE GCU CONFIG Aircraft may be dispatched provided MFD GCU FAIL remote mounted control panel is considered inoperative. GDL 69 FAIL Aircraft may be dispatched provided datalink is considered inoperative. GPS NAV LOST Aircraft may be dispatched provided GPS is GPS1 FAIL considered inoperative. GPS1 SERVICE GPS2 FAIL GPS2 SERVICE GWX CONFIG Aircraft may be dispatched provided Datalink GWX FAIL satellite weather is considered inoperative. GWX SERVICE NAV2 SERVICE Aircraft may be dispatched provided VHF navigation system is considered inoperative. XPDR1 CONFIG Aircraft may be dispatched provided ATC XPDR1 CTRL FAIL transponder and automatic altitude reporting XPDR1 FAIL system is considered inoperative. XPDR1 SRVC XPDR2 CONFIG XPDR2 CTRL FAIL XPDR2 FAIL XPDR2 SRVC U.S. DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST FEDERAL AVIATION ADMINISTRATION AIRCRAFT: REVISION NO. 1 PAGE NO. CESSNA 510 DATE: 04/04/2013 2-4
Amber CAS Messages Dispatch Consideration
AFT DOOR Aircraft may be dispatched provided aft door monitoring system is considered inoperative. ANTISKID FAIL Aircraft may be dispatched provided antiskid system is considered inoperative. BATT TEMP FAIL Aircraft may be dispatched provided battery temperature indication is considered inoperative. CABIN DOOR Aircraft may be dispatched provided cabin door monitoring system is considered inoperative. CHECK DOORS Aircraft may be dispatched provided cabin door and nose door monitoring systems are considered inoperative. ENG A/I COLD L-R Aircraft may be dispatched provided engine anti-ice system is considered inoperative. NOSE DOOR L-R Aircraft may be dispatched provided nose door monitoring system is considered inoperative. P/S HTR R (in air) Aircraft may be dispatched provided copilot static port or copilot pitot heater system is considered inoperative. PRESS CTRL Aircraft may be dispatched provided pressurization controller auto schedule mode is considered inoperative. STALL WARN HTR Aircraft may be dispatched provided stall warning vane heater is considered inoperative. TAIL DE-ICE FAIL Aircraft may be dispatched provided tail de-ice boot system is considered inoperative. W/S A/I FAIL L-R Aircraft may be dispatched provided windshield anti-ice system is considered inoperative. WING DE-ICE FAIL Aircraft may be dispatched provided wing de-ice boot system is considered inoperative. U.S. DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST FEDERAL AVIATION ADMINISTRATION AIRCRAFT: REVISION NO. 1 PAGE NO. CESSNA 510 DATE: 04/04/2013 2-5
White CAS Messages Dispatch Consideration
*** CVR FAIL Aircraft may be dispatched provided cockpit voice recorder is considered inoperative. *** FDR FAIL Aircraft may be dispatched provided flight data recorder is considered inoperative. FUEL LO INOP L-R Aircraft may be dispatched provided fuel low indicating system is considered inoperative. NO TIRE SPINDOWN Aircraft may be dispatched provided tire spin down system is considered inoperative. P/S HTR R (on ground, Aircraft may be dispatched provided copilot with PITOT STATIC static port or copilot pitot heater system is selected) considered inoperative.