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:

CESSNA 510

REVISION NO. 1

DATE: 04/04/2013

PAGE NO.

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) Procedures

VII                

1

04/04/2013

--    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:

CESSNA 510

REVISION NO. 1

DATE: 04/04/2013

PAGE NO.

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:

CESSNA 510

REVISION NO. 1

DATE: 04/04/2013

PAGE NO.

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:

CESSNA 510

REVISION NO. 1

DATE: 04/04/2013

PAGE NO.

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:

CESSNA 510

REVISION NO. 1

DATE: 04/04/2013

PAGE NO.

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 Two

Added relief for CAS messages.

 

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

AIRCRAFT:

CESSNA 510

REVISION NO. 1

DATE: 04/04/2013

PAGE NO.

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:

CESSNA 510

REVISION NO. 1

DATE: 04/04/2013

PAGE NO.

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:

CESSNA 510

REVISION NO. 1

DATE: 04/04/2013

PAGE NO.

VIII

 

 

 

 

 

 

 

 

 

 

SECTION ONE

 

LRU ORIENTED MMEL RELIEF

 

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

 

AIRCRAFT:

CESSNA 510

REVISION NO. 1

DATE:  04/04/2013

PAGE NO.

21-1

 

 

SYSTEM,

SEQUENCE NUMBERS & ITEM

1. REPAIR CATEGORY

 

 

2. NUMBER INSTALLED

 

 

 

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:

a)          Cockpit fan is operative, and

b)          CABIN FAN remains OFF.

I

I

I

 

-21-03

 

Cockpit Fan

C

1

0

May be inoperative provided:

a)          Cabin fan is operative,

b)          Cabin and cockpit temperature control system is operative,

c)          All glareshield fans are operative, and

d)          COCKPIT FAN remains OFF.

I
I
I
I
I
I
I

 

-21-04

 

Glareshield Fan

C

3

1

May be inoperative provided:

a)          Cockpit fan is operative and selected ON, and

b)          Air conditioning system is operative and selected ON.

I
I

 

-30-01

Cabin Pressurization System

(Unpressurized)

C

1

0

(O) May be inoperative provided:

a)          PRESS CTRL is selected to STANDBY,

b)          CABIN DUMP is selected ON,

c)          Aircraft is operated at 14,100 feet cabin altitude or below, and

d)          Flight crew oxygen system is operative and used as required by 14 CFR.

I

I
I
I
I
I
I
I
I

 

 

 

 

 

 

NOTE: PRESS CTRL amber message will appear. CABIN ALTITUDE red message may appear at 9,800 +/- 200 feet cabin altitude.

I
I
I
I

 

-31-01

 

Pressurization Controller Auto Schedule Mode (NORM)

(Unpressurized)

C

1

0

May be inoperative provided cabin pressurization system is considered inoperative.

I
I
I

I

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

 

AIRCRAFT:

CESSNA 510

REVISION NO. 1

DATE:  04/04/2013

PAGE NO.

21-2

 

 

SYSTEM,

SEQUENCE NUMBERS & ITEM

1. REPAIR CATEGORY

 

 

2. NUMBER INSTALLED

 

 

 

3. NUMBER REQUIRED FOR DISPATCH

 

 

 

 

4. REMARKS AND EXCEPTIONS

 

21

AIR CONDITIONING

 

 

 

 

 


-32-01

 

Cabin Differential Pressure (EICAS Indication)

 

 

 

 

 

 

-01

(Unpressurized)

C

1

0

May be inoperative provided cabin pressurization system is considered inoperative.

I
I
I

 

-02

(Pressurized)

C

1

0

(O) May be inoperative provided:

a)          Cabin altitude and rate (EICAS Indication) are operative,

b)          Pressurization controller auto schedule mode is operative, and

c)          A chart is provided and used to convert cabin and aircraft altitude to differential pressure.

 

 

I

I

I

 

I

 

 

-32-02

 

Cabin Altitude (EICAS Indication)

 

 

 

 

 

 

-01

(Unpressurized)

C

1

0

May be inoperative provided cabin pressurization system is considered inoperative.

I

I

I

 

-02

(Pressurized)

C

1

0

(O) May be inoperative provided:

a)          Cabin differential pressure (EICAS Indication) is operative,

b)          Pressurization controller auto schedule mode is operative, and

c)          A chart is provided and used to convert aircraft altitude and differential pressure to cabin altitude.

I

I

I

I

I

I

I

I

I

 

-33-01

 

Cabin Outflow Valve

(Unpressurized)

C

2

0

(M) May be inoperative provided:

a)          Affected cabin outflow valve is removed, and

b)          Cabin pressurization system is considered inoperative.

 

I

I

I

I

 

-33-02

 

Flow Control Valve

C

2

1

(O) One may be inoperative provided:

a)          Pressurization controller auto schedule mode is operative,

b)          Cabin pressurization air source is selected to operative source, and

c)          Aircraft is operated at FL 250 or below.

 

I

I

I

I

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

 

AIRCRAFT:

CESSNA 510

REVISION NO. 1

DATE:  04/04/2013

PAGE NO.

21-3

 

 

SYSTEM,

SEQUENCE NUMBERS & ITEM

1. REPAIR CATEGORY

 

 

2. NUMBER INSTALLED

 

 

 

3. NUMBER REQUIRED FOR DISPATCH

 

 

 

 

4. REMARKS AND EXCEPTIONS

 

21

AIR CONDITIONING

 

 

 

 

 

-33-03

 

Pressure Regulating Shutoff Valve

(Failed Closed)

C

2

1

(O) One may be inoperative provided:

a)          Affected pressure regulated shutoff valve is verified closed,

b)          Pressurization controller auto schedule mode is operative,

c)          Cabin pressurization air source is selected to operative source, and

d)          Aircraft is operated at FL 250 or below.

 

 

I

I

I

I

I

 

-33-04

Cabin Dump Function

(Unpressurized)

C

1

0

(M) May be inoperative provided:

a)          One cabin outflow valve is removed, and

b)          Cabin pressurization system is considered inoperative.

I

I

I

I

I

 

-50-01

Air Conditioning System

C

1

0

(M) May be inoperative provided:

a)          Air conditioning system is deactivated,

b)          Cabin and cockpit temperature control system is operative,

c)          All glareshield fans are operative, and

d)          Aircraft is restricted to temperature limitation in accordance with AFM.

 

I

 

 

I

I

I

I

II

 

-60-01

 

Cabin and Cockpit Temperature Control System

C

2

1

May be inoperative provided:

a)          Crew determines that cockpit and cabin temperature are satisfactory, and

b)          DUCT O’HEAT amber message is monitored.

I

 

 

 

I

I

 

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

 

AIRCRAFT:

CESSNA 510

REVISION NO.  01

DATE:  04/04/2013

PAGE NO.

22-1

 

 

SYSTEM,

SEQUENCE NUMBERS & ITEM

1. REPAIR CATEGORY

 

 

2. NUMBER INSTALLED

 

 

 

3. NUMBER REQUIRED FOR DISPATCH

 

 

 

 

4. REMARKS AND EXCEPTIONS

 

22

AUTO FLIGHT

 

 

 

 

 

-00-01

 

Autopilot

B

1

0

(M) May be inoperative provided:

a)          Autopilot is deactivated,

b)          Aircraft is not operated single pilot,

c)          Enroute operations do not require its use,

d)          Approach minimums do not require its use, and

e)          Aircraft is not operated RVSM.

I

I

I

I

II

I

I

I

 

-10-01

 

Yaw Damper

C

1

0

(M) May be inoperative provided:

a)          Yaw damper is deactivated,

b)          Autopilot is considered inoperative, and

c)          Aircraft is operated at FL 300 or below.

I

I

I

I

I

I

 

-10-02

Go-Around Button

 

 

 

 

 

 

-01

 

C

2

1

 

I

 

-02

 

C

2

0

May be inoperative provided:

a)          Flight director is not used for takeoff or during go-around, and

b)          Autopilot is disconnected for go-around.

I

I

I

I

I

 

 

 

 

 

 

NOTE:  FMS missed approach procedure must be activated manually.

I

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 pilot operations.

I

I

 

-02

 

C

2

0

May be inoperative provided electric elevator trim is considered inoperative.

I

I

 

-10-04

Autopilot/Flight Director Sync

(CWS Button)

C

2

0

 

I

I

I

 

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

 

AIRCRAFT:

CESSNA 510

REVISION NO. 1

DATE:  04/04/2013

PAGE NO.

23-1

 

 

SYSTEM,

SEQUENCE NUMBERS & ITEM

1. REPAIR CATEGORY

 

 

2. NUMBER INSTALLED

 

 

 

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 do not require its use.

I

I

 

-02

Antenna system

D

-

0

May be inoperative provided procedures do not require its use.

I

I

 

-10-01

***

High Frequency (HF) Communications System

D

-

-

Any in excess of those required by 14 CFR may be inoperative.

I

I

 

-01

 

Wire Antenna

C

-

0

(M) May be inoperative provided:

a)          Horizontal and vertical stabilizers are inspected for damage,

b)          Any remaining portion of wire antenna is removed, and

c)          High Frequency (HF) communication system is considered inoperative.

I

I

I

I

I

I

I

I

 

-12-01

 

Communication Systems (VHF)

 

C

-

-

May be inoperative provided:

a)          Affected system is not on emergency bus,

b)          System is not required by 14 CFR, and

c)          Procedures do not require its use.

I

I

I

I

I

I

 

-20-01

 

Datalink (Including Satellite Radio and Weather)

 

 

 

 

I

I

 

-01

 

D

-

0

May be inoperative provided procedures do not require its use.

I

I

 

 

 

 

 

 

NOTE: Any function(s) that operate normally may be used.

I

I

 

-02

 

C

-

0

(O) May be inoperative provided alternate procedures are established and used.

I

I

 

-30-01

***

Auxiliary Audio Input System

C

1

0

 

I

I

 

-30-02

***

XM Radio Wireless Remote System

C

1

0

 

I

I

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

 

AIRCRAFT:

CESSNA 510

REVISION NO. 1

DATE:  04/04/2013

PAGE NO.

23-2

 

 

SYSTEM,

SEQUENCE NUMBERS & ITEM

1. REPAIR CATEGORY

 

 

2. NUMBER INSTALLED

 

 

 

3. NUMBER REQUIRED FOR DISPATCH

 

 

 

 

4. REMARKS AND EXCEPTIONS

 

23

COMMUNICATIONS

 

 

 

 

 

-40-01

***

Passenger Address (PA) System (Aircraft with cabin headset jacks only)

 

 

 

 

 

 

-01

 

B

-

0

(O) May be inoperative provided alternate normal, abnormal, and emergency procedures, and/or operating restrictions are established and used.

I

I

I

I

 

-02

 

D

-

0

May be inoperative provided system is not required by 14 CFR.

I

I

 

-50-01

Flight Deck Headset Earphone/Headphone and Boom Microphone

 

 

 

 

I

I

I

 

-01

Headset

Boom Microphone

 

 

 

 

 

 

-10

 

A

-

0

May be inoperative provided:

a)          Hand microphone is installed and operates normally,

b)          Repairs are made within three flight days, and

c)          Aircraft is not operated single pilot.

I

I

I

I

I

I

I

 

-20

 

D

-

-

Any in excess of those required by 14 CFR may be inoperative.

I

I

 

-02

 

Headset Earphones/Headphone

 

 

 

 

 

 

-10

 

C

-

1

May be inoperative provided associated cockpit speaker operates normally.

I

I

 

-20

 

D

-

-

Any in excess of those required by 14 CFR may be inoperative.

I

I

 

-03

***

Active Noise Canceling/Reduction Function

D

-

0

May be inoperative provided normal audio function of headset is operative.

I

I

I

 

-04

Headset Audio System

C

-

-

May be inoperative provided associated cockpit speaker is operative and used. 

I

I

 

-50-02

Hand Microphone

C

1

0

May be inoperative provided an operative headset boom microphone(s) is available. 

I

I

 

-50-03

Hand Microphone Jack

C

1

0

May be inoperative provided an operative headset boom microphone(s) is available. 

I

I

 

-50-04

Hand Microphone Holder

C

1

0

(O) May be inoperative provided hand Microphone is secured by alternate means.

I

I

I

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

 

AIRCRAFT:

CESSNA 510

REVISION NO. 1

DATE:  04/04/2013

PAGE NO.

23-3

 

 

SYSTEM,

SEQUENCE NUMBERS & ITEM

1. REPAIR CATEGORY

 

 

2. NUMBER INSTALLED

 

 

 

3. NUMBER REQUIRED FOR DISPATCH

 

 

 

 

4. REMARKS AND EXCEPTIONS

 

23

COMMUNICATIONS

 

 

 

 

 

-50-05

 

Audio Control Panel

 

 

 

 

 

 

-01

INTR COM Button

 

D

2

0

May be inoperative for single pilot operations.

I

I

 

-02

PLAY Button

D

2

0

 

I

 

-03

COM1, COM2, COM3 MIC Annunciator

C

6

0

May be inoperative provided crew refers to PFD frequency boxes for active transmit frequency (shown in green).

I

I

I

 

-04

MKR/MUTE Button

C

2

0

May be inoperative provided:

a)          Approach procedures do not require its use, and

b)          System is not required by 14 CFR.

I

I

I

I

 

-05

HI SENS Button (Marker Beacon Hi Sensitivity)

C

2

0

May be inoperative provided approach procedures do not require its use.

I

I

 

-06

DME Button

C

2

0

May be inoperative provided procedures do not require its use.

I

I

 

-07

NAV1, NAV2 Button

C

4

0

May be inoperative provided procedures do not require its use.

I

I

 

-50-06

Cockpit Speaker

 

 

C

2

1

One may be inoperative provided:

a)          Affected speaker is not required for procedures, and

b)          A headset is used for associated inoperative speaker including during emergency procedures.

I

I

I

I

I

I

 

-60-01

Static Wick

 

 

 

 

I

 

-01

Aileron

(Each side)

C

2

1

One may be damaged or missing provided outermost wick is installed and not damaged.

I

I

I

 

-02

Wing Tip Assembly

(Each side)

-

1

1

 

|

|

 

-03

Elevator

(Each side)

C

3

1

Two may be damaged or missing provided outermost wick is installed and not damaged.

I

|

|

 

-04

Vertical Stabilizer

-

1

1

 

|

 

-05

Rudder

C

2

1

One may be damaged or missing provided uppermost wick is installed and not damaged.

I

|

|

 

-06

Stinger

-

1

1

 

|

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

 

AIRCRAFT:

CESSNA 510

REVISION NO. 1

DATE:  04/04/2013

PAGE NO.

23-4

 

 

SYSTEM,

SEQUENCE NUMBERS & ITEM

1. REPAIR CATEGORY

 

 

2. NUMBER INSTALLED

 

 

 

3. NUMBER REQUIRED FOR DISPATCH

 

 

 

 

4. REMARKS AND EXCEPTIONS

 

23

COMMUNICATIONS

 

 

 

 

 

-70-01

***

Cockpit Voice Recorder

 

 

 

 

I

I

 

-01

With Flight Data Recorder Installed

A

-

0

May be inoperative provided:

a)          Flight data recorder operates normally, and

b)          Repairs are made within three flight days.

I

I

I

I

I

 

-02

For an Operator other than a Holder of an Air Carrier or Commercial Operator Certificate

A

-

0

May be inoperative provided repairs are made in accordance with 14 CFR.

I

I

I

I

 

-03

Independent Power Source

C

-

0

 

I

 

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

 

AIRCRAFT:

CESSNA 510

REVISION NO. 1

DATE:  04/04/2013

PAGE NO.

24-1

 

 

SYSTEM,

SEQUENCE NUMBERS & ITEM

1. REPAIR CATEGORY

 

 

2. NUMBER INSTALLED

 

 

 

3. NUMBER REQUIRED FOR DISPATCH

 

 

 

 

4. REMARKS AND EXCEPTIONS

 

24

ELECTRICAL POWER

 

 

 

 

 

-31-01

***

Battery Temperature Indication (Aircraft equipped with Lead-Acid Battery)

C

1

0

 

I

I

I

 

-37-01

 

DC Generator Current Display (AMPS)

(EICAS Indication)

B

2

1

One may be inoperative provided GEN OFF L-R amber message is monitored.

I

I

|

 

-40-01

External Power System

C

1

0

 

I

 

-60-01

Cockpit 12V Outlet

 

 

 

 

 

 

-01

 

C

-

0

(O) May be inoperative provided alternate procedures are established and used.

I

I

 

-02

 

D

-

0

May be inoperative provided procedures do not require its use.

I

I

 

-60-02

Interior Disconnect

 

 

 

 

 

 

-01

 

C

1

0

(M) (O) May be inoperative provided:

a)          Interior power system is deactivated,

b)          Passengers are briefed on disabled cabin electrical systems, and

c)          Cabin interior lighting, cockpit/cabin 12V outlets, and cabin audio are considered inoperative.

I

I

I

I

I

I

I

I

I

 

-02

 

 

C

1

0

(M) May be inoperative provided:

a)          Interior power system is deactivated,

b)          Passengers are not carried, and

c)          Cabin interior lighting, cockpit/cabin 12V outlets, and cabin audio are considered inoperative.

I

I

I

I

I

I

I

I

 

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

 

AIRCRAFT:

CESSNA 510

REVISION NO. 1

DATE:  04/04/2013

PAGE NO.

25-1

 

 

SYSTEM,

SEQUENCE NUMBERS & ITEM

1. REPAIR CATEGORY

 

 

2. NUMBER INSTALLED

 

 

 

3. NUMBER REQUIRED FOR DISPATCH

 

 

 

 

4. REMARKS AND EXCEPTIONS

 

25

EQUIPMENT/FURNISHINGS

 

 

 

 

 

-00-01

Document Holder

(Airworthiness Certificate, Registration, Etc.)

D

1

0

(O) May be missing or inoperative provided an alternate means of securing and displaying required documents is used.

I

I

I

I

 

-10-01

Flight Crew Seat

(per seat)

 

 

 

 

I

I

 

-01

Armrest

 

 

 

 

 

 

-10

 

C

1

0

May be inoperative provided affected armrest is stowed in retracted position.

I

I

 

-20

 

 

C

1

0

(M) May be inoperative provided affected armrest is removed.

I

I

 

-02

***

Lumbar Support

C

1

0

 

I

I

 

-03

Recline/Tilt Function

C

1

0

(O) May be inoperative provided :

a)          Affected seat is failed in a position that permits normal visibility,

b)          Full flight control movement is available, and

c)          Crewmember can reach all necessary controls and equipment while restrained.

I

I

I

I

I

I

I

I

 

-04

***

Restraint Buckle Protective Padding

C

-

0

 

I

I

 

-05

Vertical Adjustment

C

1

0

(O) May be inoperative provided:

a)          Affected seat is failed in a position that permits normal visibility,

b)          Full flight control movement is available, and

c)          Crewmember can reach all necessary controls and equipment while restrained.

I

I

I

I

I

I

I

I

 

-06

 

Copilot Seat Belt/Shoulder Harness

C

1

0

May be inoperative provided seat remains unoccupied.

I

I

 

-10-02

 

Cockpit Sun Visor System and/or Attachment Mechanism

C

2

0

May be missing or inoperative provided pilot’s field of vision is not obstructed.

 

I

I

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 Cover

C

1

0

May be missing or inoperative provided cover is removed.

I

I

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

 

AIRCRAFT:

CESSNA 510

REVISION NO. 1

DATE:  04/04/2013

PAGE NO.

25-2

 

 

SYSTEM,

SEQUENCE NUMBERS & ITEM

1. REPAIR CATEGORY

 

 

2. NUMBER INSTALLED

 

 

 

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 emergency exit,

b)          Seat does not restrict any cabin occupant access to main aircraft aisle,

c)          Affected seat(s) are blocked and placarded “DO NOT OCCUPY”, and

d)          A seat with an inoperative seat belt or shoulder harness is considered inoperative.

 

I

 

I

I

 

 

 

 

I

I

I

 

 

 

 

 

 

NOTE: Affected seat(s) may include seats near inoperative seat(s).

 

 

-01

Armrest

D

-

-

(M) May be inoperative or missing and seat occupied provided:

a)          Armrest does not block an emergency exit,

b)          Armrest does not restrict any passenger from access to aisle, and

c)          If armrest is missing, reclining seat is secured in full upright position.

I

I

I

I

I

I

I

I

I

I

 

-02

Headrest

 

 

 

 

 

 

-10

 

C

-

-

May be inoperative and seat occupied provided headrest is failed in placarded taxi, takeoff and landing position.

I

I

I

 

-20

 

D

-

-

May be missing or inoperative in other than placarded taxi, takeoff, and landing position provided affected seat is considered inoperative.

I

I

I

I

 

-03

Recline Mechanism

 

 

 

 

 

 

-10

 

C

-

-

May be inoperative and seat occupied provided seat back is immovable in the full upright position.

 

I

 

 

-20

 

D

-

-

(M) May be inoperative and seat occupied provided seat is secured in full upright position.

I

I

I

 

 

 

 

 

 

(Continued)

 

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

 

AIRCRAFT:

CESSNA 510

REVISION NO. 1

DATE:  04/04/2013

PAGE NO.

25-3

 

 

SYSTEM,

SEQUENCE NUMBERS & ITEM

1. REPAIR CATEGORY

 

 

2. NUMBER INSTALLED

 

 

 

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 is blocked and placarded "DO NOT OCCUPY".

I

I

I

 

-05

Seat Belt/Shoulder Harness Keeper

D

-

-

 

I

I

 

-06

Lumbar Support

D

-

-

 

I

 

-20-02

***

Folding Cabin Seat

C

1

0

May be inoperative provided:

a)          Seat does not block an emergency exit,

b)          Seat does not restrict any cabin occupant access to main aircraft aisle,

c)          Affected seat(s) are blocked and placarded “DO NOT OCCUPY”, and

d)          A seat with an inoperative seat belt or shoulder harness is considered inoperative.

I

I

I

I

I

I

I

I

I

I

I

I

 

 

 

 

 

 

NOTE: Affected seat(s) may include seats near inoperative seat(s).

I

I

 

-20-03

Cabin Curtain

C

2

0

May be missing or inoperative provided curtain remains secured open.

I

I

 

-20-04

Non-Essential Equipment & Furnishings (NEF)

-

-

0

May be inoperative, damaged or missing provided that the item(s) is deferred in accordance with the NEF deferral program. The NEF program, procedures and processes are outlined in the operator’s (insert name) Manual. (M) and (O) procedures, if required, must be available to the flight crew and included in the operator’s appropriate document.

 

NOTE: Exterior lavatory door ash trays are not NEF items.

I

I

I

I

I

I

I

I

I

I

I

I

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

 

AIRCRAFT:

CESSNA 510

REVISION NO. 1

DATE:  04/04/2013

PAGE NO.

25-4

 

 

SYSTEM,

SEQUENCE NUMBERS & ITEM

1. REPAIR CATEGORY

 

 

2. NUMBER INSTALLED

 

 

 

3. NUMBER REQUIRED FOR DISPATCH

 

 

 

 

4. REMARKS AND EXCEPTIONS

 

25

EQUIPMENT/FURNISHINGS

 

 

 

 

 

-30-01

Cabin Storage Compartment

 

 

 

 

 

 

-01

 

C

-

-

(M) May be inoperative provided:

a)          Compartment does not contain any aircraft system protection devices,

b)          Any emergency equipment located in affected compartment is considered inoperative,

c)          Affected compartment is not used for storage of any item except for those permanently affixed,

d)          Procedures are established and used to secure compartment closed, and

e)          Affected compartment is prominently placarded “DO NOT USE”.

I

I

I

I

I

I

I

I

I

I

I

I

I

I

I

I

 

-02

 

C

-

-

(M) (O) May be inoperative provided:

a)          Affected door is removed,

b)          Affected compartment is not used for storage of any item, except those permanently affixed,

c)          Cabin occupants are briefed that affected compartment may not be used,

d)          Affected compartment is prominently placarded “DO NOT USE”, and

e)          Any permanently affixed emergency equipment located in affected compartment is available for use.

I

I

I

I

I

I

I

I

I

I

I

I

I

I

I

 

-03

Shelving

D

-

-

May be inoperative provided any permanently affixed emergency equipment located on affected shelving is relocated and available for use. 

I

I

I

I

 

-30-02

***

Storage Compartment

Key Lock

D

-

0

May be inoperative in unlocked position.

I

I

 

-40-01

***

Ashtray

A

-

1

May be inoperative or missing provided it is replaced within three calendar days.

I

I

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

 

AIRCRAFT:

CESSNA 510

REVISION NO. 1

DATE:  04/04/2013

PAGE NO.

25-5

 

 

SYSTEM,

SEQUENCE NUMBERS & ITEM

1. REPAIR CATEGORY

 

 

2. NUMBER INSTALLED

 

 

 

3. NUMBER REQUIRED FOR DISPATCH

 

 

 

 

4. REMARKS AND EXCEPTIONS

 

25

EQUIPMENT/FURNISHINGS

 

 

 

 

 

50-01

 

Cargo Restraint System

C

-

-

May be inoperative or missing provided cargo compartment remains empty.

 

 

 

-60-01

***

Emergency Medical Equipment

 

 

 

 

I

I

 

-01

 

Automatic External Defibrillator and/or Associated Equipment

D

-

0

 

I

I

I

 

-02

 

Emergency Medical Kit (EMK) and/or Associated Equipment

D

-

0

 

I

 

-03

First Aid Kit (FAK) and/or Associated Equipment

D

-

-

Any in excess of those required by 14 CFR may be incomplete, missing, or inoperative.

I

I

I

 

-61-01

***

Life Preservers

(Crew And Passenger)

D

-

0

Any in excess of those required by 14 CFR may be inoperative or missing.

I

I

 

-62-01

***

 

Emergency Locator Transmitter

(ELT)

 

 

 

 

 

I

 

 

-01

Survival Type ELT

D

-

-

Any in excess of those required by 14 CFR may be inoperative or missing.

I

I

 

-02

Fixed ELT

 

 

 

 

 

 

-10

 

A

-

0

(M) May be inoperative provided:

a)          System is deactivated, and

b)          Repairs are made within 90 days.

I

I

I

 

-20

 

A

-

0

May be missing provided repairs are made within 90 days.

I

I

 

-30

 

D

-

-

(M) Any in excess of those required by 14 CFR may be inoperative provided system is deactivated.

I

I

I

 

-40

 

D

-

-

Any in excess of those required by 14 CFR may be missing.

I

I

 

-64-01

***

Life Raft

D

-

-

Any in excess of those required by 14 CFR may be inoperative or missing.

I

I

 

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

 

AIRCRAFT:

CESSNA 510

REVISION NO. 1

DATE:  04/04/2013

PAGE NO.

26-1

 

 

SYSTEM,

SEQUENCE NUMBERS & ITEM

1. REPAIR CATEGORY

 

 

2. NUMBER INSTALLED

 

 

 

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 CFR may be inoperative or missing 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 extinguisher must be located in cockpit.

I

I

 

 

 

 

 

 

 

 

I

I

I

 

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

 

AIRCRAFT:

CESSNA 510

REVISION NO. 1

DATE:  04/04/2013

PAGE NO.

27-1

 

 

SYSTEM,

SEQUENCE NUMBERS & ITEM

1. REPAIR CATEGORY

 

 

2. NUMBER INSTALLED

 

 

 

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 inoperative.

 

 

 

 

 

I

I

 

-60-01

 

Speed Brake Actuation System

(Failed in retracted position)

B

1

0

(M) (O) May be inoperative provided:

a)          Speed brakes are deactivate,

b)          Steep approaches are not performed, and

c)          Operations are limited to VMO of 240 KIAS.

I

 

 

I

 

-60-02

Speed Brake Position

B

1

0

May be inoperative provided speed brake actuation system is considered inoperative.

I

I

I

 

-60-03

Speed Brake Switch

C

2

1

 

I

 

-70-01

Aileron/Elevator Control Lock

(Failed Unlocked)

C

1

0

(O) May be inoperative in unlocked position provided full flight control is available.

I

I

I

 

-70-02

Rudder Lock

(Failed Unlocked)

C

1

0

(O) May be inoperative in unlocked position provided full flight control is available.

I

I

I

 

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

 

AIRCRAFT:

CESSNA 510

REVISION NO. 1

DATE:  04/04/2013

PAGE NO.

28-1

 

 

SYSTEM,

SEQUENCE NUMBERS & ITEM

1. REPAIR CATEGORY

 

 

2. NUMBER INSTALLED

 

 

 

3. NUMBER REQUIRED FOR DISPATCH

 

 

 

 

4. REMARKS AND EXCEPTIONS

 

28

FUEL

 

 

 

 

 

-10-01

Over-wing Refueling Cap Lock

D

2

0

May be inoperative in unlocked position.

I

I

 

-41-01

Fuel Low Level Indicating System

A

2

1

(O) One may be inoperative provided:

a)          Procedures for monitoring fuel quantity are established and used, and

b)          Repairs are made within three flight days.

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U.S. DEPARTMENT OF TRANSPORTATION

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

 

AIRCRAFT:

CESSNA 510

REVISION NO. 1

DATE:  04/04/2013

PAGE NO.

30-1

 

 

SYSTEM,

SEQUENCE NUMBERS & ITEM

1. REPAIR CATEGORY

 

 

2. NUMBER INSTALLED

 

 

 

3. NUMBER REQUIRED FOR DISPATCH

 

 

 

 

4. REMARKS AND EXCEPTIONS

 

30

ICE AND RAIN PROTECTION

 

 

 

 

 

-10-01

 

Wing De-Ice Boot System

(Failure to inflate)

 

C

1

0

(M) May be inoperative provided:

a)          All de-ice boots must be visually verified to be deflated and held down when service air system is active, and

b)          Aircraft is not operated in known, forecast, or AFM-defined icing conditions.

I

I

I

I

I

I

I

I

 

-10-02

 

Tail De-Ice Boot System

(Failure to inflate)

C

1

0

(M) May be inoperative provided:

a)          All de-ice boots must be visually verified to be deflated and held down when service air system is active, and

b)          Aircraft is not operated in known, forecast, or AFM-defined icing conditions.

I

I

I

I

I

I

I

I

 

-20-01

Engine Anti-Ice System

 

 

 

 

I

 

- 01

Failed On

(Flow)

C

2

1

One may be inoperative provided:

a)          Both ENGINE ANTI-ICE switches are selected ON,

b)          Takeoff and landing performance calculations for anti-ice on are used, and

c)          Aircraft are restricted to temperature limitation in accordance with AFM.

I

I

I

I

I

I

I

I

I

 

-02

Failed Off

(No Flow)

C

2

0

(M) May be inoperative provided:

a)          Affected engine anti-Ice is secured for no flow, and

b)          Aircraft is not operated in known, forecast, or AFM-defined icing conditions.

I

I

I

I

I

I

 

-30-01

 

Copilot Pitot Heater System

 

B

1

0

May be inoperative provided:

a)          Aircraft is not operated in Instrument Meteorological Conditions (IMC), and

b)          Aircraft is not operated in known, forecast, or AFM-defined icing conditions.

I

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I

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I

I

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U.S. DEPARTMENT OF TRANSPORTATION

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

 

AIRCRAFT:

CESSNA 510

REVISION NO. 1

DATE:  04/04/2013

PAGE NO.

30-2

 

 

SYSTEM,

SEQUENCE NUMBERS & ITEM

1. REPAIR CATEGORY

 

 

2. NUMBER INSTALLED

 

 

 

3. NUMBER REQUIRED FOR DISPATCH

 

 

 

 

4. REMARKS AND EXCEPTIONS

 

30

ICE AND RAIN PROTECTION

 

 

 

 

 

-30-02

 

Copilot Static Port Heater

 

B

2

1

One may be inoperative provided:

a)          Aircraft is not operated in Instrument Meteorological Conditions (IMC),

b)          Aircraft is not operated in known, forecast, or AFM-defined icing conditions, and

c)          Aircraft is not operated RVSM.

 

I

I

I

I

I

I

I

 

-30-03

Stall Warning Vane Heater

C

1

0

May be inoperative provided aircraft is not operated in known, forecast, or AFM-defined icing conditions.

I

I

I

 

-40-01

 

Windshield Anti-Ice System

 

C

2

0

(O) May be inoperative provided:

a)          Aircraft is not operated in known, forecast, or AFM-defined icing conditions, and

b)          Crew has a means to clear windshield of moisture.

I

I

I

I

 

 

-40-02

 

Windshield Rain Repellant

 

C

1

0

May be missing provided aircraft is not operated in precipitation within five nautical miles of airport used for takeoff or intended landing.

I

I

I

I

 

-70-01

Air Conditioner Forward Evaporator Drain Heater

C

1

0

May be inoperative provided air conditioning system is considered inoperative.

I

I

I

 

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

 

AIRCRAFT:

CESSNA 510

REVISION NO. 1

DATE:  04/04/2013

PAGE NO.

31-1

 

 

SYSTEM,

SEQUENCE NUMBERS & ITEM

1. REPAIR CATEGORY

 

 

2. NUMBER INSTALLED

 

 

 

3. NUMBER REQUIRED FOR DISPATCH

 

 

 

 

4. REMARKS AND EXCEPTIONS

 

31

INDICATING/RECORDING SYSTEMS

 

 

 

 

 

-20-01

 

Flight Hour Meter

C

1

0

(O) May be inoperative provided flight time is tracked by alternate means.

I

I

 

-30-01

***

Flight Data Recorder (FDR) System

 

 

 

 

 

 

-01

(For a Holder of an Air Carrier or Commercial Operator Certificate)

A

-

0

May be inoperative provided:

a)          Cockpit Voice Recorder (CVR) operates normally,

b)          Airplane is not dispatched from a designated airport as listed in operator’s MEL unless:

1.          FDR failure occurs after dispatch but prior to takeoff, or

2.          FDR repair was attempted but was not successful.

c)          In those cases where repair is attempted but not successful, aircraft may be dispatched on a flight or series of flights until next designated airport where repair must be accomplished prior to dispatch, and

d)          Repairs are made within three flight days.

I

I

I

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I

I

I

I

I

I

I

I

I

I

I

I

I

I

I

 

-10

FDR Recording Parameters Required by 14 CFR

A

-

-

Up to three (3) recording parameters may be inoperative provided:

a)          Cockpit Voice Recorder (CVR) operates normally, and

b)          Repairs are made within 20 calendar days.

I

I

I

I

I

I

 

-20

FDR Recording Parameters Not Required by 14 CFR

A

-

-

May be inoperative provided repairs are made prior to completion of next scheduled inspection/check of system.

I

I

I

 

-02

(For an Operator other than a Holder of an Air Carrier or Commercial Operator Certificate)

A

-

0

May be inoperative provided repairs are made in accordance with applicable 14 CFR.

I
I
I
I

 

-30-02

***

Quick Access Recorder

C

1

0

 

I

I

 

-40-01

***

Electronic Checklist

D

1

0

May be inoperative provided equivalent checklist is used.

I

I

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

 

AIRCRAFT:

CESSNA 510

REVISION NO. 1

DATE:  04/04/2013

PAGE NO.

31-2

 

 

SYSTEM,

SEQUENCE NUMBERS & ITEM

1. REPAIR CATEGORY

 

 

2. NUMBER INSTALLED

 

 

 

3. NUMBER REQUIRED FOR DISPATCH

 

 

 

 

4. REMARKS AND EXCEPTIONS

 

31

INDICATING/RECORDING SYSTEMS

 

 

 

 

 

-40-02

Fuel Totalizer

C

1

0

May be inoperative provided:

a)          Fuel quantity indicating system is operative, and

b)          MFD map range rings and weight planning functions are considered inoperative.

I

I

I

I

I

I

 

-50-01

Master Warning System

 

 

 

 

I

 

-01

 

Master Warning Reset Annunciator

B

2

1

Pilot side must be operative for single pilot operations.

I

I

 

-02

Master Warning Cancel/Reset Function

C

2

1

Pilot side must be operative for single pilot operations.

I

I

 

-03

 

Master Caution Reset Annunciator

C

2

1

Pilot side must be operative for single pilot operations.

I

I

 

-04

Master Caution Cancel/Reset Function

C

2

1

Pilot side must be operative for single pilot operations.

I

I

 

-50-02

 

Cabin Altitude Warning System

C

1

0

May be inoperative provided:

a)          Cabin altitude warning is not displayed, and

b)          Aircraft is operated at 9,500 feet MSL or below.

I

I

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I

I

 

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

 

AIRCRAFT:

CESSNA 510

REVISION NO. 1

DATE:  04/04/2013

PAGE NO.

32-1

 

 

SYSTEM,

SEQUENCE NUMBERS & ITEM

1. REPAIR CATEGORY

 

 

2. NUMBER INSTALLED

 

 

 

3. NUMBER REQUIRED FOR DISPATCH

 

 

 

 

4. REMARKS AND EXCEPTIONS

 

32

LANDING GEAR

 

 

 

 

 

-41-01

 

Antiskid System

 

C

1

0

(O) May be inoperative provided:

a)          Aircraft is operated in accordance with AFM DISPATCH WITH ANTISKID SYSTEM INOPERATIVE abnormal procedure, and

b)          Steep approaches are not conducted.

I

I

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I

I

I

I

I

 

 

 

 

 

 

NOTE:  ANTISKID FAIL amber message will appear.

I

I

 

-41-02

Tire Spin Down System

C

1

0

(O) May be inoperative provided aircraft is operated in accordance with AFM NO TIRE SPINDOWN white CAS message procedure is followed. 

I

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I

I

 

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

 

AIRCRAFT:

CESSNA 510

REVISION NO. 1

DATE: 04/04/2013

PAGE NO.

33-1

 

 

SYSTEM,

SEQUENCE NUMBERS & ITEM

1. REPAIR CATEGORY

 

 

2. NUMBER INSTALLED

 

 

 

3. NUMBER REQUIRED FOR DISPATCH

 

 

 

 

4. REMARKS AND EXCEPTIONS

 

33

LIGHTS

 

 

 

 

 

-10-01

 

Cockpit and Instrument Lighting System

(Excluding Internally Lighted Annunciators and Buttons, Standby Flight Instrument Lighting, and STDBY ALT/AS Placard Lighting)

C

-

-

Individual lights may be inoperative provided remaining lights are:

a)          Sufficient to clearly illuminate all required instruments, controls, and other devices for which it is provided,

b)          Positioned so that direct rays are shielded from crew members eyes,

c)          Lighting configuration and intensity is acceptable to crew, and

d)          Cockpit flood light is operative.

I

I

I

I

I

I

I

 

 

 

 

 

I

 

-10-02

 

Cockpit Flood Light

C

1

0

May be inoperative provided aircraft is not operated at night.

I

I

 

-10-03

 

Windshield Ice Detection Light

 

 

 

 

 

 

-01

 

C

2

0

May be inoperative provided aircraft is not operated at night.

I

I

 

-02

 

 

C

2

1

Right side may be inoperative for single pilot operations.

I

I

 

-03

 

C

2

1

(O) One may be inoperative for two pilot operations provided alternate procedures are established and used.

I

I

I

 

-10-04

Cockpit Map Light

 

 

 

 

 

 

-01

 

C

2

1

One may be inoperative provided cockpit flood light is operative.

I

I

 

-02

 

C

2

0

May be inoperative provided cockpit flood light is operative and a flashlight is available to crew.

I

I

I

 

-10-05

G1000 Display Dimmer (DISPLAYS knob)

C

1

0

(O) May be inoperative providing display brightness is adjusted through G1000 menu in manual mode.

I

I

I

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

 

AIRCRAFT:

CESSNA 510

REVISION NO. 1

DATE: 04/04/2013

PAGE NO.

33-2

 

 

SYSTEM,

SEQUENCE NUMBERS & ITEM

1. REPAIR CATEGORY

 

 

2. NUMBER INSTALLED

 

 

 

3. NUMBER REQUIRED FOR DISPATCH

 

 

 

 

4. REMARKS AND EXCEPTIONS

 

33

LIGHTS

 

 

 

 

 

-20-01

 

Lighted Passenger Information Sign

(Excluding Cabin Exit Signs)

 

 

 

 

 

 

-01

 

C

-

0

(O) May be inoperative provided:

a)          Alternate procedures are established and used to alert cabin occupants when PAX SAFETY/SEAT BELT is selected, and

b)          Scheduled operations are not conducted.

I

I

I

I

I

I

I

I

 

-02

 

C

-

0

May be inoperative provided no cabin occupants are carried.

I

I

 

-20-02

 

Cabin Interior Lighting System (Excluding Emergency Lighting)

C

-

-

(O) Individual lights may be inoperative provided cabin emergency lighting is verified operative.

I

I

I

 

-30-01

 

Aft Baggage Light

C

1

0

 

I

 

-01

Door Proximity Switch

C

1

0

(O) May be inoperative providing crew makes sure light is selected OFF using toggle switch.

I

I

I

 

-30-02

 

Nose Baggage Compartment Light

C

1

0

 

 

 

-01

Door Proximity Switch

 

 

 

 

 

 

-10

 

C

2

0

(O) May be inoperative providing crew makes sure light is selected OFF using rocker switch on light.

I

I

I

 

-20

 

C

2

1

 

I

 

-40-01

 

Anti-Collision Light System (Wing Strobes) (ANTI COLL)

A

1

0

May be inoperative provided:

a)          All position (NAV) lights are operative,

b)          Ground recognition (BEACON) light is operative, and

c)          Repairs are made within three flight days.

I

I

I

 

-40-02

 

Position Light System

(NAV)

C

1

0

May be inoperative provided system is not required by 14 CFR.

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I

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

 

AIRCRAFT:

CESSNA 510

REVISION NO. 1

DATE: 04/04/2013

PAGE NO.

33-3

 

 

SYSTEM,

SEQUENCE NUMBERS & ITEM

1. REPAIR CATEGORY

 

 

2. NUMBER INSTALLED

 

 

 

3. NUMBER REQUIRED FOR DISPATCH

 

 

 

 

4. REMARKS AND EXCEPTIONS

 

33

LIGHTS

 

 

 

 

 

-40-03

 

Wing Inspection Light (WING INSP)

C

1

0

May be inoperative provided:

a)          Aircraft is not operated at night, and

b)          Ground deicing procedures do not require its use.

I

I

I

I
I

 

-40-04

 

Landing/Taxi/Recognition Light (LANDING - RECOG TAXI)

C

2

0

Any in excess of those required by 14 CFR may be inoperative.

I

I

I

 

-40-05

 

Ground Recognition Light (BEACON)

C

1

0

May be inoperative provided anti-collision light system is operative.

 

I

 

-50-01

***

Cockpit Flashlight and Holder Assembly

 

 

 

 

I

I

 

-01

Flashlight

D

-

-

Any in excess of those required by 14 CFR may be inoperative or missing.

I

I

 

-02

Holder Assembly

C

-

-

May be inoperative provided associated flashlight is stowed by alternate means.

I

I

 

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

 

AIRCRAFT:

CESSNA 510

REVISION NO. 1

DATE:  04/04/2013

PAGE NO.

34-1

 

 

SYSTEM,

SEQUENCE NUMBERS & ITEM

1. REPAIR CATEGORY

 

 

2. NUMBER INSTALLED

 

 

 

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 in IFR conditions.

 

 

 

I

I

 

-25-01

MFD Remote Mounted Control Panel

B

1

0

(O) May be inoperative provided:

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

(CRSR, ,D>, MENU, FPL, PROC, BACK, SPC, CLR, SEL, <, >, A-Z, 1-0, +/-, and period)

(Except ENT, Range/PUSH PAN, and FMS Knobs/PUSH CRSR)

C

-

0

NOTE:     Corresponding buttons/knobs on PFD must be operative for relief, if applicable. 

I

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I

I

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

 

AIRCRAFT:

CESSNA 510

REVISION NO. 1

DATE:  04/04/2013

PAGE NO.

34-2

 

 

SYSTEM,

SEQUENCE NUMBERS & ITEM

1. REPAIR CATEGORY

 

 

2. NUMBER INSTALLED

 

 

 

3. NUMBER REQUIRED FOR DISPATCH

 

 

 

 

4. REMARKS AND EXCEPTIONS

 

34

NAVIGATION

 

 

 

 

 

25-02

Mode Control Panel

 

 

 

 

I

 

-01

Yaw Damper Button

(YD)

C

1

0

NOTE 1:  Yaw damper may be engaged by engaging autopilot.

I

I

 

 

 

 

 

 

NOTE 2:  Yaw damper may be disengaged by pushing AP TRIM DISC button.

I

I

I

 

-02

Course Knob Push Direct Function

(CRS1 or CRS2 PUSH DIR)

C

2

0

 

I

I

I

 

-03

Bank Button

(BANK)

C

1

0

 

I

I

 

-04

HDG Knob PUSH SYNC Function

C

1

0

 

I

I

 

-05

Vertical Mode Button

(FLC, ALT, VNV, VS)

 

 

 

 

I

I

 

-10

 

C

4

3

 

I

 

-20

 

B

4

0

May be inoperative provided:

a)          Flight director is considered inoperative, and

b)          Autopilot is considered inoperative.

I

I

I

I

I

 

-06

Speed Button (SPD)

C

1

0

 

I

 

-07

Lateral Mode Buttons (NAV, HDG, APR, BC)

B

4

0

May be inoperative provided:

a)          Flight director is considered inoperative, and

b)          Autopilot is considered inoperative.

I

I

I

I

I

 

-08

Annunciator LEDs and XFR Arrows

D

13

0

NOTE: PFDs are primary source for armed and active mode indications.

I

I

 

-09

XFR Button

B

1

0

May be inoperative provided:

a)          FD Indicator Arrow is pointing to LH side if operated single pilot, or

b)          Pilot flying must be seated in side FD Indicator Arrow is pointing to if operated dual pilot.

I

I

I

I

I

I

 

-25-03

***

Synthetic Vision

C

1

0

May be inoperative provided procedures do not require its use.

I

I

 

-25-04

Moving Map Display

C

3

0

May be inoperative provided procedures do not require its use.

I

I

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

 

AIRCRAFT:

CESSNA 510

REVISION NO. 1

DATE:  04/04/2013

PAGE NO.

34-3

 

 

SYSTEM,

SEQUENCE NUMBERS & ITEM

1. REPAIR CATEGORY

 

 

2. NUMBER INSTALLED

 

 

 

3. NUMBER REQUIRED FOR DISPATCH

 

 

 

 

4. REMARKS AND EXCEPTIONS

 

34

NAVIGATION

 

 

 

 

 

-25-05

Primary Flight Display (PFD)

 

 

 

 

I

 

-01

Copilot’s BARO Knob and PUSH STD Function

C

1

0

May be inoperative for single pilot operations.

I

I

 

-02

RANGE/PAN Knob/Joystick

C

2

0

May be inoperative provided procedures do not require its use.

I

I

 

-03

D>, FPL, PROC Button

C

6

0

May be inoperative provided corresponding button(s) on MFD remote mounted control panel are operative.

I

I

I

 

-04

Copilot’s Comm Swap Button (Hold for EMERG)

C

1

0

May be inoperative for single pilot operations.

I

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:

a)          Affected system is not on the emergency bus,

b)          Approach procedures do not require its use, and

c)          System is not required by 14 CFR.

I

I

I

I

I

I

 

-34-01

 

Marker Beacon Receiver System

C

1

0

May be inoperative provided:

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 not required by 14 CFR.

I

I

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

 

AIRCRAFT:

CESSNA 510

REVISION NO. 1

DATE:  04/04/2013

PAGE NO.

34-4

 

 

SYSTEM,

SEQUENCE NUMBERS & ITEM

1. REPAIR CATEGORY

 

 

2. NUMBER INSTALLED

 

 

 

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 operative,

b)          Aircraft is not operated RVSM,

c)          Aircraft does not depart from a designated airport (as listed in operator’s MEL) where repair or replacement can be made,

d)          Autopilot with altitude hold and capture operates normally, and

e)          Repairs are made within three flight days.

 

I

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I

 

 

-44-01

***

Radar Altimeter System

A

1

0

May be inoperative provided:

a)          Approach minimums or operating procedures do not require its use,

b)          TCAS II, if installed, is considered inoperative, and

c)          Repairs are made within two flight days.

I

I

I

I

I

I

I

 

-44-02

 

Terrain Awareness And Warning System (TAWS) – Class B

 

 

 

 

I

I

 

-01

 

C

1

0

May be inoperative provided system is not required by 14 CFR.

I

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 Avoidance Mode

B

1

0

 

I

I

 

-04

Premature Descent Alert Mode

B

1

0

 

I

I

 

-05

Advisory Callouts

 

 

 

 

I

 

-10

 

B

-

0

(O) May be inoperative provided alternate procedures are established and used.

I

I

 

-20

 

C

-

0

(O) May be inoperative provided:

a)          Advisory callout not required by 14 CFR, and

b)          Alternate procedures are established and used.

I

I

I

I

I

 

 

 

 

 

 

(Continued)

 

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

 

AIRCRAFT:

CESSNA 510

REVISION NO. 1

DATE:  04/04/2013

PAGE NO.

34-5

 

 

SYSTEM,

SEQUENCE NUMBERS & ITEM

1. REPAIR CATEGORY

 

 

2. NUMBER INSTALLED

 

 

 

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 Mode

A

1

0

(O) May be inoperative provided:

a)          Alternate procedures are established and used, and

b)          Repairs are made within two flight days.

I

I

I

I

I

 

-07

Negative Climb Rate or Altitude Loss After Takeoff Mode

A

1

0

(O) May be inoperative provided:

c)          Alternate procedures are established and used, and

d)          Repairs are made within two flight days.

I

I

I

I

I

 

-45-01

Traffic Alert and Collision Avoidance System (TCAS)

 

 

 

 

I

I

 

-01

***

TCAS II

 

 

 

 

I

I

 

-10

Combined Traffic Alert (TA) and Resolution Advisory (RA) Dual Display System

 

C

-

1

May be inoperative on the pilot not flying side provided:

a)          TA and RA visual display is operative on the pilot flying side, and

b)          TA and RA audio function is operative on pilot flying side.

I

I

I

I

I

I

I

 

-20

Audio Function

B

-

0

May be inoperative provided procedures do not require use of TCAS II.

I

I

 

-30

Airspace Selection Function

C

-

0

 

I

 

-02

***

Traffic Alert System (TAS)

C

-

0

 May be inoperative provided en route or approach procedures do not require use of TAS.

I

I

I

 

-45-02

Traffic Information System (TIS)

C

1

0

 

I

I

 

-45-03

***

Traffic Collision Avoidance Device (TCAD)

C

1

0

 

I

I

 

-51-01

 

Distance Measuring Equipment System (DME)

D

-

-

Any in excess of those required by 14 CFR may be inoperative.

I

I

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

 

AIRCRAFT:

CESSNA 510

REVISION NO. 1

DATE:  04/04/2013

PAGE NO.

34-6

 

 

SYSTEM,

SEQUENCE NUMBERS & ITEM

1. REPAIR CATEGORY

 

 

2. NUMBER INSTALLED

 

 

 

3. NUMBER REQUIRED FOR DISPATCH

 

 

 

 

4. REMARKS AND EXCEPTIONS

 

34

NAVIGATION

 

 

 

 

 

-52-01

 

ATC Transponders and Automatic Altitude Reporting System

 

 

 

 

 

 

-01

 

D

-

1

Any in excess of those required by 14 CFR may be inoperative.

I

I

 

-02

 

B

2

0

May be inoperative provided:

a)          Operations do not require its use,

b)          Prior to flight, approval is obtained from ATC facilities having jurisdiction over planned route of flight,

c)          Aircraft is not operated RVSM, and

d)          Traffic Alert and Collision Avoidance System (TCAS II) is considered inoperative.

 

I

 

 

 

 

I

I

I

I

 

-03

Elementary and Enhanced Downlink Aircraft Reportable Parameters Not Required By 14 CFR

A

2

0

May be inoperative provided:

a)          Operations do not require its use, and

b)          Repairs are made prior to completion of next scheduled inspection/check of system.

I

I

I

I

I

I

 

-04

***

ADS-B Squitter Transmissions

A

-

0

May be inoperative provided:

a)          Operations do not require its use, and

b)          Repairs are made prior to completion of next scheduled inspection/check of system.

I

I

I

I

I

I

 

-52-02

Automatic Dependent Surveillance-Broadcast (ADS-B) System

D

-

0

May be inoperative provided system is not required by 14 CFR.

I

I

I

 

 

 

 

 

 

NOTE:  If ADS-B is installed in lieu of or as a replacement for 14 CFR required equipment, repair category in operator’s MEL will be the same as that of 14 CFR required equipment.

I

I

I

I

I

I

 

-01

Cockpit Display and Traffic Information (CDTI)

D

-

0

NOTE: CDTI display of data from other aircraft systems may be used.

I

I

 

 

 

 

 

 

(Continued)

 

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

 

AIRCRAFT:

CESSNA 510

REVISION NO. 1

DATE:  04/04/2013

PAGE NO.

34-7

 

 

SYSTEM,

SEQUENCE NUMBERS & ITEM

1. REPAIR CATEGORY

 

 

2. NUMBER INSTALLED

 

 

 

3. NUMBER REQUIRED FOR DISPATCH

 

 

 

 

4. REMARKS AND EXCEPTIONS

 

34

NAVIGATION

 

 

 

 

 

-52-02

Automatic Dependent Surveillance-Broadcast (ADS-B) System

(Continued)

 

 

 

 

 

 

-02

CDTI Control Panel

D

-

0

May be inoperative provided:

a)          Flight ID can be set, and

b)          Screen display is acceptable to flight crew.

I

I

I

I

 

-03

Data Link Transmitter

D

-

0

NOTE: In some aircraft, data link transmission is an integral part of the transponder and relief is provided in that section.

I

I

I

I

 

-04

Data Link Receiver

D

-

0

 

I

 

-05

ADS-B Application

D

-

0

 

I

 

-55-01

***

Automatic Direction Finding System (ADF)

D

-

-

Any in excess of those required by 14 CFR may be inoperative.

I

I

 

-57-01

 

Navigation Equipment

(GPS, FMS)

C

-

-

Any in excess of those required by 14 CFR may be inoperative.

I

I

 

-60-01

 

Flight Management System

(FMS) Navigation Database

A

-

-

May be expired provided aircraft is operated in accordance with applicable AFM limitations.

I

I

I

 

-60-02

Data Loader (SD Card Slot)

C

-

-

NOTE: Certain card slots are used for real-time data access. If inoperative, the associated features are considered inoperative.

I

I

I

I

I

 

 

 

 

U.S. DEPARTMENT OF TRANSPORTATION

MASTER MINIMUM EQUIPMENT LIST

FEDERAL AVIATION ADMINISTRATION

 

AIRCRAFT:

CESSNA 510

REVISION NO. 1

DATE:  04/04/2013

PAGE NO.

35-1

 

 

SYSTEM,

SEQUENCE NUMBERS & ITEM

1. REPAIR CATEGORY

 

 

2. NUMBER INSTALLED

 

 

 

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 filled using alternate means when service is required.

I

I

I

 

-00-02

Plastic Blowout Disc/Green Label

C

1

0

(O) May be missing or damaged provided oxygen pressure is verified prior to each flight.

I

I

I

 

-20-01

 

Passenger Oxygen System

 

 

C

1

0

May be inoperative provided:

a)          No cabin occupants are carried, and

b)          Crew oxygen system is operative.

 

I

 

I

 

-01

Cabin Mask

C

5

0

Individual oxygen masks or dispensers may be inoperative or missing provided associated seats are placarded “DO NOT OCCUPY”.

I

I

I

I

 

-02

Drop Out Panel

C

5

0

(M) Individual panels may be out of normal position provided:

a)          Oxygen masks and drop out panel are removed, and

b)          Associated seats are placarded “DO NOT OCCUPY”.

I

I

I

I

I

I

 

-30-01

***

Protective Breathing Equipment (PBE)

D

-

-