INTENTIONALLY LEFT BLANK · 2016-07-04 · JULY 05, 2016 List of Effective Pages Title Page List of Effective Pages I Revision 02 July 05, 2016 II ... Lasertrack installed. 34-34

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TRANSPORT CANADA Master Minimum Equipment List

Supplement

DASSAULT FALCON 50

PAGE: I REVISION: 02 JULY 05, 2016

List of Effective Pages

Title Page

List of Effective Pages I Revision 02 July 05, 2016

II Revision 02 July 05, 2016

Log of Revisions III Revision 02 July 05, 2016

Reasons for Changes IV Revision 02 July 05, 2016

V Revision 02 July 05, 2016

VI Revision 02 July 05, 2016

VII Revision 02 July 05, 2016

Introduction VIII Revision 02 July 05, 2016

Pages 21-1 Revision 02 July 05, 2016

22-1 Revision 02 July 05, 2016




















Supplement

DASSAULT FALCON 50

PAGE: II REVISION: 02 JULY 05, 2016

List of Effective Pages (cont’d)

Pages 31-1 Revision 02 July 05, 2016













34-10 Revision 02 July 05, 2016

34-11 Revision 02 July 05, 2016

34-12 Revision 02 July 05, 2016

34-13 Revision 02 July 05, 2016

34-14 Revision 02 July 05, 2016









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DASSAULT FALCON 50

PAGE: III REVISION: 02 JULY 05, 2016

Log of Revisions

Revision No. Date Page Number Initials

Original Mar. 14, 2002 All

01 Jan. 21, 2004 All

02 July 05, 2016 All


Supplement

DASSAULT FALCON 50

PAGE: IV REVISION: 02 JULY 05, 2016

Reasons for Changes

General This revision incorporates the following documents:

EASA MMEL Revision 6;

TC Guidance Book Revision 7;

TC Global Change 7

Due to the extent of changes in this TC MMEL Supplement, revision bars are not used.

Item No.

21-4 Revised to align with EASA MMEL and GB items 21-30-3, 21-30-5, and 21-30-6.

21-9 New item as per EASA MMEL except for Repair Interval Category of second relief of sub-item (2) that is aligned with GB item 21-50-1 (cat D for the unpressurized case).

22-1 Revised as per GB item 22-10-1.

22-2 New item as per EASA MMEL with Repair Interval Category aligned with item 22-1 (cat B as Autopilot is not used).

22-5 New item to indicate appropriate Repair Interval Category for sub-item (1): cat B is aligned with item 22-1 relief (Autopilot not used).

22-6 Renumbered as per EASA MMEL (previously item 22-2) and revised as per GB item 22-10-2.


22-8 New item as per EASA MMEL with Repair Interval Category of second relief aligned with item 22-1 (cat B as Autopilot is not used).

22-9 New item as per EASA MMEL with Repair Interval Category of first relief aligned with item 22-1 (cat B as Autopilot is not used).



23-3 New item as per GB item 23-10-1.





23-9 Deleted (previously item 23-7). Refer to EASA MMEL.


23-13 Renumbered as per EASA MMEL (previously item 23-12).

23-20 New item to address relief for STC SA13-72.


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DASSAULT FALCON 50

PAGE: V REVISION: 02 JULY 05, 2016

Reasons for Changes (cont’d)

Item No.

25-1 Revised as per EASA MMEL as well as GB item 25-10-2. Relief for sub-items (1) and (3) requires a (M) to secure seat in an acceptable position.

25-3 Deleted. Refer to EASA MMEL.




25-7 Revised as per Global Change 7.

25-11 Deleted.

25-12 Deleted.




26-2 Revised to indicate appropriate Repair Interval Category for sub-items (2) and (3):


26-5 Deleted.

26-6 Deleted.

26-7 Deleted.

26-8 Deleted.

26-9 Deleted.

27-5 Revised to align sub-item numbering with EASA MMEL. Aural Warning, sub-item (2) (b), must be operative for dispatch.

27-9 Revised to align sub-item numbering with EASA MMEL


27-12 Deleted.


28-8 Revised to align proviso a) with FAA MMEL Rev 6 and proviso b) with EASA MMEL.






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DASSAULT FALCON 50

PAGE: VI REVISION: 02 JULY 05, 2016


Item No.




33-1 Revised to align with EASA MMEL and GB item 33-10-1.




33-10 Updated reference in Remarks or Exceptions column to replace “JAA” with “EASA”.

33-11 Editorial change in first relief.

33-15 New item to indicate appropriate Repair Interval Category as per GB item 33-40-4.

33-16 New item to correct Number Required of first relief that should indicate “1” (one light out of two may be inoperative) as well as to add proviso b) to second relief as per current TC Flight Test policy on Ice Detection Light relief.

33-17 New item to address current TC Flight Test policy on Ice Detection Light relief. Use of a portable light is not acceptable.

33-20 Deleted.

34-2 Added aircraft applicability under item title as per EASA MMEL.



34-6 Renumbered as per EASA MMEL (previously item 34-10). Revised Number Installed from “1” to “-”.

34-7 Renumbered as per EASA MMEL (previously item 34-9). Revised Number Installed from “1” to “-”.




34-13 Renumbered as per EASA MMEL (previously item 34-21-1) and revised as per GB item 34-50-1.




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DASSAULT FALCON 50

PAGE: VII REVISION: 02 JULY 05, 2016


Item No.


34-17 Renumbered as per EASA MMEL (previously item 34-21-7).

34-18 Renumbered as per EASA MMEL (previously item 34-21-8).




34-24 New item to indicate that sub-item (1) (a), Heading Information, is required for dispatch (2 Installed/2 Required).

34-26 New item to indicate appropriate Repair Interval Category.


34-29 Renumbered as per EASA MMEL (previously item 34-21-9). Added relief with/without Lasertrack installed.

34-34 Renumbered as per EASA MMEL (previously item 34B-5 on page 34B-1). Added appropriate Repair Interval Category to sub-items (1) and (5).


34-42 New item. The second relief in the EASA MMEL is not acceptable and therefore is not applicable to Canadian-registered aircraft.

35-1 Editorial changes.

35-2 Renumbered as per EASA MMEL (previously item 35-1-2) as well as added relief for Passenger Masks.

35-3 New item to indicate system required for dispatch.






73-3 New item to indicate appropriate Repair Interval Category that is aligned with EASA MMEL item 73-2.


Supplement

DASSAULT FALCON 50

PAGE: VIII REVISION: 02 JULY 05, 2016

Introduction

This Transport Canada MMEL Supplement constitutes a mandatory change to the EASA Recommended MMEL for the Dassault Falcon 50 aircraft. This MMEL Supplement must be used in conjunction with the EASA Recommended MMEL (Revision No. 6, November 02, 2011, or later applicable revision). The information contained herein supersedes the existing EASA MMEL only for those items listed herein. For items not contained in this Supplement, consult the EASA Recommended MMEL. Operating and/or maintenance procedures referred to in this Supplement are the same as those supporting the EASA MMEL unless otherwise indicated. Procedures required by the Transport Canada MMEL Supplement, and not indicated in the EASA Recommended MMEL must be provided by the operator. The EASA MMEL has entries where the “Remarks or Exceptions” column states “As required by Regulations”. Unless such an entry is superseded by an item in this Supplement, all references should be made to the applicable Canadian regulation. This MMEL Supplement uses the standard four-column format as referenced in the Transport Canada MMEL/MEL Policy and Procedures Manual (TP9155E). The same definitions and symbols as the EASA MMEL are also used. Items that have no MMEL relief (i.e. relief withdrawn) are not categorized. Comments and inquiries should be directed to: Transport Canada Chief, Flight Test - AARDC National Aircraft Certification


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Aircraft:

DASSAULT FALCON 50

Revision No. 02 Page:

Date: July 05, 2016 21-1

System & 1. 2. Number Installed

Sequence 3. Number Required for Dispatch

Numbers 4. Remarks or Exceptions

21 AIR CONDITIONING

4. Triple Cabin Indicator

(1) Cabin Altitude

Indication C 1 0 No change from EASA MMEL

D 1 0 No change from EASA MMEL

(2) Cabin Differential Pressure Indication

C 1 0 No change from EASA MMEL


(3) Cabin Vertical Speed Indication



9. CABIN and CREW Air Conditioning Systems: Valves (13H1, 13H2) and Controls (12H1, 12H2)

(1) AUTO Mode C 2 0 No change from EASA MMEL

(2) MANUAL Mode C 2 1 No change from EASA MMEL



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DASSAULT FALCON 50


Date: July 05, 2016 22-1




22 AUTOFLIGHT

1. AP Function B 1 0 No change from EASA MMEL

B 1 0 No change from EASA MMEL

2. FD Function B 2 1 No change from EASA MMEL


5. Autopilot Disengaged Warning Light

(1) AP Caution Light

(Aircraft without modification M1924)


(2) AP Warning Light

(Aircraft with modification M1924)


6. Control Wheel Disengage Pushbutton

C 2 1 One may be inoperative provided: a) The autopilot is not used below

1,500 ft. AGL, b) Approach minimuns do not require

the use of the autopilot, and c) The pilot flying has the operative

disengage switch.

B 2 0 Both may be inoperative provided autopilot is not used.


Supplement

Aircraft:

DASSAULT FALCON 50


Date: July 05, 2016 22-2




22 AUTOFLIGHT

7. Quick Disconnect B 2 0 No change from EASA MMEL

8. Go-Around C 2 1 No change from EASA MMEL


9. Flight Control Panel (FCP) (Aircraft with modification M1924)



13. Pitch or Roll Servomotors B 2 0 No change from EASA MMEL


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DASSAULT FALCON 50


Date: July 05, 2016 23-1




23 COMMUNICATIONS

2. VHF System D - - Any in excess of those required by regulations may be inoperative provided:

a) It is not powered by a standby or emergency bus, and

b) It is not required for emergency purposes.

3. HF System D - - Any in excess of those required by regulations may be inoperative.

C - 1 (O) May be inoperative while conducting

operations that require two Long Range Communication Systems (LRCS) provided:

a) SATCOM Voice or Data Link operates normally,

b) Alternate procedures are established and used,

c) SATCOM coverage is available over the intended route of flight, and

d) If INMARSAT short codes or IRIDIUM direct dial commercial numbers are not available while using SATCOM voice, prior coordination with the appropriate ATS facility is required.

4. UHF System D - - Any in excess of those required by regulations may be inoperative provided:

a) It is not powered by a standby or emergency bus, and

b) It is not required for emergency purposes.


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DASSAULT FALCON 50


Date: July 05, 2016 23-2




23 COMMUNICATIONS

5. Public Address System

(1) Cargo Configuration D 1 0 May be inoperative provided all crew

members are on the flight deck.

(2) Passenger

Configuration C 1 0 (O) May be inoperative provided alternate,

normal and emergency procedures, and/or operating restrictions are established and used.

6. Cockpit Loudspeakers C 2 0 May be inoperative provided:

a) Procedures are not dependent on their use,

b) Headsets are installed and used by each person on flight deck duty,

c) All aural alerts, messages and other communication which are normally routed through the flight deck speakers must be audible through the headsets, and

d) A spare headset must be readily available for crew use.

7. Headsets

Installations with CVR and FDR

A - 0 May be inoperative for three flight days provided the FDR is operative.

Installations with CVR only A - 0 May be inoperative for three flight days.


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Aircraft:

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Date: July 05, 2016 23-3




23 COMMUNICATIONS

9. Audio Control Panel Deleted in Revision 02

11. Cockpit Voice Recorder (CVR)

If CVR and FDR required by regulations

A 1 0 May be inoperative provided:

a) The Flight Data Recorder is operative, and

b) Repairs are made within three flight days.

If only CVR required by regulations

A 1 0 May be inoperative provided repairs are made within three flight days.

13. SELCAL

C - 0 (O) May be inoperative provided alternate procedures are established and used.

D - 0 May be inoperative provided routine procedures do not require its use.


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Aircraft:

DASSAULT FALCON 50


Date: July 05, 2016 23-4




23 COMMUNICATIONS

20. Future Air Navigation System (FANS) (STC SA13-72)

(1) UL-801 Data Link

Management System C 1 0 (O) May be inoperative provided alternate

procedures are established and used.

D 1 0 May be inoperative provided procedures

do not require its use.

(2) UL-801 VHF Communication Radio

C 1 0 (O) May be inoperative provided alternate procedures are established and used.



(3) ATC Annunciators C 2 1 One annunciator may be inoperative provided Aural Unit and both FANS speakers are operative.


do not require their use.

(4) Iridium Data Link Unit C 1 0 (O) May be inoperative provided alternate procedures are established and used.




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Aircraft:

DASSAULT FALCON 50


Date: July 05, 2016 23-5




23 COMMUNICATIONS

20. Future Air Navigation System (FANS) (cont’d) (STC SA13-72)

(5) Aural Annunciation Unit

PRD60 C 1 0 (O) May be inoperative provided alternate




(6) FANS Speakers C 2 1 One may be inoperative provided Aural Unit and both ATC Annunciators are operative.


do not require their use.

(7) Data Link Printer ***

D 1 0


Supplement

Aircraft:

DASSAULT FALCON 50


Date: July 05, 2016 25-1




25 EQUIPMENT / FURNISHINGS

1. Crew Member Seat

(1) Vertical Adjustment C 2 0 (O)(M) One or more may be inoperative on both seats provided:

a) Seat is secured in a position allowing the crew member to adequately perform his duties, and [OPER 25-1.1 on section 2-25]

b) Associated CREW SEATS circuit breaker is pulled and collared. [OPER 24-0 on section 2-24]

(2) Armrests C 4 0 No change from EASA MMEL

(3) Recline Adjustment B 2 0 (M) One or more may be inoperative provided:

a) Seat back is secured in a position acceptable to the affected crew member, and

b) Seat is able to move full Fore and Aft on its track.

(4) Headrests C 2 0 No change from EASA MMEL

3. Inertial Reels Deleted in Revision 02


Supplement

Aircraft:

DASSAULT FALCON 50


Date: July 05, 2016 25-2





4. Passenger Seats D - - (M) May be inoperative provided:

a) Seat does not block an emergency exit,

b) Seat does not restrict any passenger from access to the aircraft aisle, and

c) The affected seat(s) is blocked and placarded “DO NOT OCCUPY”.

NOTES:

1. A seat with an inoperative safety belt is considered inoperative.

2. Affected seat(s) may include the seat behind and/or the adjacent outboard seats.

(1) Headrests C - 0 No change from EASA MMEL

(2) Recline Mechanism D - - (M) May be inoperative and seat occupied provided seat is secured in the full upright position.

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

5. Jump Seat Deleted in Revision 02


Supplement

Aircraft:

DASSAULT FALCON 50


Date: July 05, 2016 25-3





6. Emergency Locator Transmitter (ELT)

(1) Fixed ELTs A - 0 (M) May be inoperative provided:

a) Placard is displayed in the flight deck indicating the date ELT has been removed, and

b) Repair or replacement is made within the time interval prescribed by regulations.

(2) Survival Type ELTs D - - Any in excess of those required by regulations may be inoperative or missing.

7. Lavatory Door Ashtray A 1 0 May be missing or inoperative for 10 days.

11. Lavatory NO SMOKING Placard

Deleted in Revision 02

12. FASTEN SEAT BELT WHILE SEATED Signs or Placards



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Aircraft:

DASSAULT FALCON 50


Date: July 05, 2016 25-4





13. Passenger Convenience/NEF Items

Note 1: Operators are to select either Passenger Convenience Items or NEF (Non-Essential Equipment and Furnishings) in their MELs.

Note 2: For operators with NEF defect rectification and control procedures, refer to sub-item (2) (NEF) only.

(1) Passenger

Convenience Items - 0 Passenger convenience items as

expressed in this MMEL are those related to passenger convenience, comfort or entertainment, such as, but not limited to – galley equipment, movie equipment, ashtrays, stereo equipment, and overhead reading lamps. Items addressed elsewhere in this document shall not be included.

(M) and (O) procedures may be required and included in the MEL.

Note 1: Exterior lavatory door ashtrays are not considered convenience items.

Note 2: Galley equipment restraining devices such as latches, etc. must be serviceable or the compartment must not be used for storage and placarded “INOPERATIVE - DO NOT USE”.

Note 3: Movie equipment individual screens, if applicable, must be capable of being stowed.

Note 4: Audio or audio-visual entertainment equipment which is used as the sole means of providing safety briefings and demonstrations is not considered a passenger convenience item.


Supplement

Aircraft:

DASSAULT FALCON 50


Date: July 05, 2016 25-5





13. Passenger Convenience/NEF Items (cont’d)

(2) Non-Essential Equipment and Furnishings (NEF)

- 0 May be inoperative, damaged or missing provided that the item(s) is deferred in accordance with the operator's defect rectification and control procedures. The NEF policies are outlined in the operator's Maintenance Control 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 ashtrays are not considered NEF items.


Supplement

Aircraft:

DASSAULT FALCON 50


Date: July 05, 2016 25-6





14. First Aid Kit D - - (O) Any kit or items contained in the kit in excess of those required by regulations may be incomplete or missing provided:

a) Required distribution is maintained, and

b) Procedures are established and used to alert crew members of missing or incomplete kits.

(1) First Aid Kit Seal

(Required First Aid Kits) A - - (O) The seal affixed on the exterior of any

required first aid kit may be missing or broken for three flight days provided:

a) The first aid kit is fully equipped or the kit has a maximum of one missing item,

b) The kit includes a list of its contents,

c) An inventory is taken on the content of the kit prior to departure, and

d) Procedures are established and used to alert crew members of:

1) The missing or broken seal, and

2) The need to perform an inventory under proviso c).

15. Emergency Medical Kit ***

D - - (O) Any kit or items contained in the kit in excess of those required by regulations may be incomplete or missing provided procedures are established and used to alert crew members of missing or incomplete kits.


Supplement

Aircraft:

DASSAULT FALCON 50


Date: July 05, 2016 26-1




26 FIRE PROTECTION

2. APU Fire System (Aircraft with modification M0378)

(1) APU Fire Extinguisher Discharge Indicator Disc


(2) APU Fire Extinguisher C 1 0 No change from EASA MMEL

(3) APU Fire Warning System


3. Hand Fire Extinguishers D - - (O)(M) Any in excess of those required by regulations may be inoperative or missing provided:

a) The inoperative fire extinguisher(s) is/are removed from the passenger cabin and flight deck, and its location is placarded “INOPERATIVE”, or it is removed from the installed location, secured out of sight and the fire extinguisher and its installed location are placarded “INOPERATIVE”,

b) Required distribution is maintained in the passenger compartment and flight deck, and

c) Procedures are established and used to alert crew members of missing portable fire extinguishers.


Supplement

Aircraft:

DASSAULT FALCON 50


Date: July 05, 2016 26-2




26 FIRE PROTECTION

5. Aft Compartment Fire Detection


6. Baggage Compartment Smoke Detector


7. Lavatory Fire Extinguishing *** System


8. Lavatory Smoke Detection *** System


9. Landing Gear Well Fire Detection



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Date: July 05, 2016 27-1




27 FLIGHT CONTROLS

5. Takeoff Configuration

(1) Aircraft without modification M1924

No change from EASA MMEL

(2) Aircraft with modification M1924

(a) T/O CONFIG Warning Light


(b) Aural Warning 1 1 Must be operative

(c) through (h) No change from EASA MMEL

9. High Angle-of-attack Protection and Indicating System

(1) Automatic Slat Extension System Test Circuit


(2) Stall Warning Horn B 1 0 No change from EASA MMEL

(3) AUTO SLATS Caution Light



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Aircraft:

DASSAULT FALCON 50


Date: July 05, 2016 27-2




27 FLIGHT CONTROLS

11. Rudder Pedal Adjustment C 2 0 (M) May be inoperative provided:

a) The rudder pedals can be secured in a position which meets individual pilot requirements, and

b) Full and unrestricted movement of the rudder and brake pedal deflection is possible at both pilot stations.

12. Control Wheel Trim Switches Deleted in Revision 02


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Aircraft:

DASSAULT FALCON 50


Date: July 05, 2016 28-1




28 FUEL SYSTEM

7. Quantity (QTY) Indications Deleted in Revision 02

8. Fuel Temperature Indication (Aircraft with modification M0941 or M2518)

C 1 0 May be inoperative provided:

a) Boost pumps, transfer systems and engine crossfeed are operative, and

b) Operations are conducted at a TAT at least 3oC above the fuel freezing point.

10. Pressure Fueling System Deleted in Revision 02


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Date: July 05, 2016 30-1




30 ICE AND RAIN PROTECTION

5. Windshield Heating Systems Deleted in Revision 02

7. Side Window Heating Deleted in Revision 02

8. Windshield Wipers Deleted in Revision 02

10. Pitot Probe Heating Systems Deleted in Revision 02


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Aircraft:

DASSAULT FALCON 50


Date: July 05, 2016 31-1




31 INDICATING / RECORDING SYSTEMS

1. Flight Data Recorder (FDR)

(1) If FDR and CVR required by regulations

A 1 0 May be inoperative provided:

a) Cockpit Voice Recorder is operative, and


(2) If only FDR required by regulations

A 1 0 May be inoperative provided repairs are made within three flight days.

(3) If FDR not required by regulations

D 1 0

(4) Digital FDR Recording Parameters required by regulations

A - - Up to three digital recording parameters may be inoperative provided:

a) Cockpit Voice Recorder is operative, and

b) Repairs are made within twenty calendar days.

(5) Digital FDR Recording Parameters not required by regulations

A - - May be inoperative provided repairs are made before the completion of the next heavy maintenance visit.


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Date: July 05, 2016 31-2




31 INDICATING / RECORDING SYSTEMS

2. Clock C - 0 Aircraft clocks may be inoperative provided a reliable and functioning timepiece is readily available to all flight deck crew members.


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Aircraft:

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Date: July 05, 2016 33-1




33 LIGHTS

1. Instrument Panel Lighting

(1) Glare Shield Ramp

(SHIELD) C 1 0 No change from EASA MMEL

D 1 0 May be inoperative for day operations.

(2) Integral Lightings C 2 0 No change from EASA MMEL


2. Overhead Panel Lighting C 1 0 No change from EASA MMEL


4. Cockpit Lighting (DOME) C 2 1 No change from EASA MMEL


7. NO SMOKING and FASTEN SEAT BELT Signs


10. Landing Lights C 2 1 No change from EASA MMEL



Supplement

Aircraft:

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Date: July 05, 2016 33-2




33 LIGHTS

11. Taxi Light C 1 0 May be inoperative for night operations provided both landing lights are operative.


15. Wing-tip Strobe Lights C 2 0 May be inoperative.

16. Wing Ice Detection Lights (Aircraft with modification M0026)


C 2 0 Both may be inoperative provided:

a) Windshield Ice Detection Light is operative, and

b) Ground deicing procedures do not require their use.

17. Windshield Ice Detection Light

C 1 0 May be inoperative provided both Wing Ice Detection Lights (if installed) are operative.

C 1 0 May be inoperative provided aircraft is not operated in known or forecast icing conditions at night.

20. Exterior Emergency Lighting System



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Date: July 05, 2016 34-1




34 NAVIGATION

2. Mach Airspeed Indicators (Aircraft without EFIS 85/86 and without modification M1924)

2 2 Must be operative.

4. Vertical Speed Indicators (Aircraft without modification M1924)

C 2 1 One may be inoperative for day VMC.

5. Altimeters 3 3 Must be operative.

6. Radio Altimeter System A - 0 May be inoperative provided:

a) Approach and landing minima are not predicated on its use, and



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Date: July 05, 2016 34-2




34 NAVIGATION

7. Altitude Alerting System

(1) Aircraft without EFIS

85/86 and without modification M1924

A - 0 (O) Except where enroute operations require its use, may be inoperative provided:

a) Autopilot altitude hold is operative, and


NOTE:


(2) Aircraft with EFIS 85/86

or modification M1924 A - 0 (O) Except where enroute operations require

its use, may be inoperative provided:

a) Autopilot altitude hold is operative, and


NOTE:


8. Air Data Computer (ADC) Deleted in Revision 02

11. Standby Horizon and Power Supply

B 1 0 May be inoperative for day VMC.


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Date: July 05, 2016 34-3




34 NAVIGATION

12. Standby Magnetic Compass B 1 0 May be inoperative provided any combination of three gyro or INS(IRU) stabilized compass systems are operative.

B 1 0 (O) May be inoperative provided:

a) Any combination of two gyro or INS(IRU) stabilized compass systems operate normally; and

b) Aircraft is operated:

1) With dual independent navigation capability, and

2) Under positive radar control by ATC during the en-route flight phase, or one of the navigation systems is a TSO’d GPS which provides track information.

C 1 0 (O) May be inoperative for flights that are entirely within areas of magnetic unreliability provided at least two stabilized directional gyro systems are installed, operative and, if necessary, used in conjunction with approved free gyro navigation techniques.

(1) Compass Lighting C 1 0 No change from EASA MMEL



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Date: July 05, 2016 34-4




34 NAVIGATION

13. VOR / ILS C - - Any in excess of those required by regulations and not powered by an emergency or standby electrical bus may be inoperative.

NOTE:

The operator’s MEL must cross reference the VOR/ILS and ADF items to specify a minimum of two systems, adequate for enroute and approach facilities for the planned itinerary, must be operative for dispatch.

14. Distance Measuring Equipment (DME)

D - - Any in excess of those required by regulations and not powered by an emergency or standby electrical bus may be inoperative.

15. Marker Beacon Receiver (MKR)

(1) Used routinely C - - (O) Except where enroute operations require its use, may be inoperative provided alternate procedures are established and used.

(2) Not used routinely D - - May be inoperative.


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Aircraft:

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Date: July 05, 2016 34-5




34 NAVIGATION

16. Automatic Direction Finder (ADF)

D - - Any in excess of those required by regulations and not powered by an emergency or standby electrical bus may be inoperative.

NOTE:

The operator’s MEL must cross reference the VOR/ILS and ADF items to specify a minimum of two systems, adequate for enroute and approach facilities for the planned itinerary, must be operative for dispatch.

17. Weather Radar (WR) D - - Any in excess of those required by regulations may be inoperative.

18. ATC Transponder (with Altitude Encoder)

(1) Aircraft without

modification M1924 C - - No change from EASA MMEL

(2) Aircraft with

modification M1924 C 2 - No change from EASA MMEL

20. G.P.S. C - - (O) Except where enroute operations require its use, may be inoperative provided alternate procedures are established and used.

NOTE:

No change from EASA MMEL.


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Date: July 05, 2016 34-6




34 NAVIGATION

21. G.P.W.S.

Class A GPWS

(1) GPWS A - 0 (O) May be inoperative provided:

a) Alternate procedures are established and used, and


(a) Modes 1 to 4 A 4 0 (O) May be inoperative provided:



(b) Test Mode A 1 0 May be inoperative provided:

a) The GPWS is considered inoperative, and


(c) Glideslope

Deviation (Mode 5)

C - 1

B - 0 May be inoperative.

(d) Advisory Callouts (Mode 6)

C - 0 (O) May be inoperative provided alternate procedures are established and used.


Supplement

Aircraft:

DASSAULT FALCON 50


Date: July 05, 2016 34-7




34 NAVIGATION

21. G.P.W.S. (cont’d)

Class A GPWS (cont’d)

(1) GPWS (cont’d)

(e) Windshear Mode

(Mode 7) ***

C 1 0 (O) May be inoperative provided:


b) Windshear Detection and Avoidance System operates normally.

B 1 0 (O) May be inoperative provided:


b) Takeoffs and landings are not conducted in known or forecast windshear conditions.

(2) Terrain System - Forward Looking Terrain Avoidance (FLTA) and Premature Descent Alert (PDA) Functions

B 1 0 May be inoperative.

(3) Terrain Displays B - 0 May be inoperative.


Supplement

Aircraft:

DASSAULT FALCON 50


Date: July 05, 2016 34-8




34 NAVIGATION


Class A GPWS (cont’d)

(4) Runway Awareness and

Advisory System (RAAS) ***

C 1 0 May be inoperative.

Class B GPWS

(1) GPWS A - 0 (O) May be inoperative provided:



(a) Modes 1 and 3 A 2 0 (O) May be inoperative provided:



(b) Test Mode A 1 0 May be inoperative provided:

a) The GPWS is considered inoperative, and



Supplement

Aircraft:

DASSAULT FALCON 50


Date: July 05, 2016 34-9




34 NAVIGATION


Class B GPWS (cont’d)

(1) GPWS (cont’d)

(c) Modes 2, 4 and 5

*** C 3 0 May be inoperative.

(d) Advisory Callouts C - 0 (O) May be inoperative provided alternate


(e) Windshear Mode

*** C 1 0 (O) May be inoperative provided:


b) Takeoffs and landings are not conducted in known or forecast windshear conditions.

(2) Terrain System - Forward Looking Terrain Avoidance (FLTA) and Premature Descent Alert (PDA) Functions

B 1 0 May be inoperative.

(3) Terrain Displays

*** C - 0 May be inoperative.

(4) Runway Awareness and

Advisory System (RAAS) ***

C 1 0 May be inoperative.


Supplement

Aircraft:

DASSAULT FALCON 50


Date: July 05, 2016 34-10




34 NAVIGATION


Class C GPWS

*** C - 0 (O) May be inoperative provided alternate


NOTE:

Any mode that operates normally may be used.

22. T.C.A.S. / ACAS II B - 0 (M) May be inoperative provided the system is deactivated and secured.

(1) Combined Traffic Alert

(TA) and Resolution Advisory (RA) Dual Displays

C 2 1 May be inoperative on the non-flying pilot side provided TA and RA elements and audio functions are operative on flying pilot side.

(2) RA Display System(s) C 2 1 One may be inoperative on non-flying

pilot side.

C - 0 (O) May be inoperative provided:

a) All Traffic Alert display elements and voice command audio functions are operative, and

b) TA only mode is selected by the crew.

(3) TA Display System(s) C - 0 May be inoperative provided all installed

RA display and audio functions are operative.


Supplement

Aircraft:

DASSAULT FALCON 50


Date: July 05, 2016 34-11




34 NAVIGATION

24. Digital Distance and/or Radio Magnetic Indicator (DDRMI / RMI)

(1) Aircraft without EFIS

85/86 and without modification M1924

(a) Heading

Information 2 2 Must be operative.

(b) Bearing

Information C 4 2 No change from EASA MMEL

(2) Aircraft with EFIS 85/86 D 2 1 No change from EASA MMEL

(3) Aircraft with

modifications M2100 and M1924

D - 0 No change from EASA MMEL

26. Flight Director Indicator (ADI) (Aircraft without EFIS 85/86 and without modification M1924)

(1) Glide Slope Pointer C - - No change from EASA MMEL

(2) Localizer Deviation

Pointer C - - No change from EASA MMEL

(3) Turn Indicator C - - No change from EASA MMEL

(4) Slip Indicator C - - No change from EASA MMEL


Supplement

Aircraft:

DASSAULT FALCON 50


Date: July 05, 2016 34-12




34 NAVIGATION

27. Horizontal Situation Indicator (HSI) (Aircraft without EFIS 85/86 and without modification M1924)

(1) Heading Display 2 2 Must be operative

(2) VOR/ILS Mode C 2 - No change from EASA MMEL

(3) Other Modes C - 0 No change from EASA MMEL

29. Flight Management System (FMS)

(1) Aircraft without modification M1924

C - - No change from EASA MMEL

(2) Aircraft with modification M1924

(a) Without Lasertrack Installed

C - 1 No change from EASA MMEL

(b) With Lasertrack Installed

C - 0 (O) Except where enroute/terminal operations require its use, may be inoperative provided IRS is initialized by Lasertrack.


Supplement

Aircraft:

DASSAULT FALCON 50


Date: July 05, 2016 34-13




34 NAVIGATION

34. Attitude and Heading System(s) (INS, AHRS, IRS)

(1) Inertial Navigation System (INS) (Aircraft without EFIS 85/86 and without modification M1924)

D - - Any in excess of two independent attitude and two independent heading reference systems may be inoperative.

Note:

No change from EASA MMEL.

(2) With 3 IRS Installed (Aircraft with EFIS 85/86)

D 3 2 Any in excess of two independent attitude and two independent heading reference systems may be inoperative.

(3) Aircraft with 2 AHS (Aircraft with modification M1924)

2 2 Must be operative.

(4) Aircraft with 3 AHS (Aircraft with modification M1924)

D 3 2 Any in excess of two independent attitude and two independent heading reference systems may be inoperative.

(5) NO AIR Amber Light (on MSU) (Aircraft with IRS installed)




Supplement

Aircraft:

DASSAULT FALCON 50


Date: July 05, 2016 34-14




34 NAVIGATION

41. Navigation Databases C - - (O) May be out of currency provided:

a) Current Aeronautical Charts are used to verify Navigation Fixes prior to dispatch,

b) Procedures are established and used to verify status and suitability of Navigation Facilities used to define route of flight,

c) Approach Navigation Radios are manually tuned and identified, and

d) Approaches are not conducted using associated system.

42. Navigation Databases Data Loader

C 1 0 May be inoperative provided Navigation Databases are not out of currency.


Supplement

Aircraft:

DASSAULT FALCON 50


Date: July 05, 2016 35-1




35 OXYGEN

1. Passenger Oxygen System

(1) With Passengers B 1 0 (O) May be inoperative provided:

a) Minimum en route altitude does not exceed 13,000 ft above MSL,

b) Pressurization system is operative,

c) Flight remains at or below FL 250,

d) Portable oxygen units are provided for all crew members and 10% of the passengers for half an hour (supplemental oxygen), and

e) Passengers are appropriately briefed.

(2) Without Passengers D 1 0 No change from EASA MMEL


Supplement

Aircraft:

DASSAULT FALCON 50


Date: July 05, 2016 35-2




35 OXYGEN

2. Passenger Oxygen System (Automatic Mode / Masks)

(1) Automatic Mode (drop out of masks)

B 1 0 (O)(M) May be inoperative provided:

a) OVERRIDE and FIRST AID systems are verified operative,

[MAINT 35-1 on section 3-35]

b) If the need arises, the supply of oxygen is controlled by selection of the OVERRIDE (above 18,000 ft flight altitude) and FIRST AID (below 18,000 ft flight altitude) positions,

c) CABIN warning light and the cabin altitude aural warning are verified operative, and

[OPER 21-1.3 on section 2-21]

d) Flight remains at or below FL 300.

(2) Passenger Masks D - 0 No change from EASA MMEL


Supplement

Aircraft:

DASSAULT FALCON 50


Date: July 05, 2016 35-3




35 OXYGEN

3. FIRST AID Oxygen 1 1 Must be operative.

4. Portable Breathing Equipment (PBE)

D - - (O)(M) Any in excess of those required by regulations may be inoperative of missing provided:

a) Required distribution of operative units is maintained throughout the aircraft,

b) The inoperative portable breathing equipment unit is removed from the passenger cabin and its location is placarded INOPERATIVE, or it is removed from the installed location, secured out of sight and the portable breathing equipment unit and its installed location are placarded INOPERATIVE, and

c) Procedures are established and used to alert crew members of inoperative or missing equipment.


Supplement

Aircraft:

DASSAULT FALCON 50


Date: July 05, 2016 38-1




38 WATER/WASTE

1. Potable Water Systems C - 0 (O)(M) System may be inoperative provided:

a) Tank is drained and inspected to ensure no leakage, and

b) Procedures are established to deactivate applicable system components to prevent its use or servicing.

NOTES:

1. The (O) procedure addresses other means for water provision for crew members as well as the need to advise of system status during crew changes.

2. Aviation Occupational Health & Safety (AOH&S) requirements should be addressed.

C - - (M) Individual components may be inoperative provided:

a) Associated components are deactivated or isolated, and

b) Associated system components are verified not to have leaks.

NOTE:

Any portion of the system that operates normally may be used.


Supplement

Aircraft:

DASSAULT FALCON 50


Date: July 05, 2016 38-2




38 WATER/WASTE

2. Lavatory Waste System C 1 0 (M) May be inoperative provided:

a) Waste is drained and system is inspected for leakage,

b) Procedures are established to deactivate system components, and

c) Lavatory door is locked closed and placarded “INOPERATIVE - DO NOT ENTER”.

NOTE:

Aviation Occupational Health & Safety (AOH&S) requirements should be addressed.

C - - (M) Individual components may be inoperative provided:

a) Associated components are deactivated or isolated, and

b) Associated system components are verified not to have leaks.

NOTE:

Any portion of the system that operates normally may be used.


Supplement

Aircraft:

DASSAULT FALCON 50


Date: July 05, 2016 49-1




49 AIRBORNE AUXILIARY POWER

2. N1 Indication (Aircraft with modification M0378)


3. T5 Indication (Aircraft with modification M0378)



Supplement

Aircraft:

DASSAULT FALCON 50


Date: July 05, 2016 73-1




73 ENGINE FUEL AND CONTROLS

3. CMPTR 1, CMPTR 2 or CMPTR 3 Caution Lights

A 3 2 One may be inoperative for three calendar days provided relevant engine computer is considered inoperative in AUTO mode. (Refer to EASA MMEL item 73-2)

Documents

INTENTIONALLY LEFT BLANK · 2016-07-04 · JULY 05, 2016 List of Effective Pages Title Page List of Effective Pages I Revision 02 July 05, 2016 II ... Lasertrack installed. 34-34