Master Minimum Equipment List (MMEL) Cessna 525

1) Cargo handling equipment (unloaded, empty or with ballast); 2) Fly away kits (excluding e.g. cans of hydraulic fluid, cleaning solvents, batteries, capacitors, chemical generators, etc.); Note: If serviceable tyres are included, they should only be inflated to a minimum pressure that preserves their serviceability; and 3) Inflight service material (return catering — only closed catering trolleys/boxes, no newspapers, no alcohol or duty free goods). 7. ‘Commencement of flight’ is the point when an aircraft begins to move under its own power for the purpose of preparing for take-off. 8. ‘Considered Inoperative’ as used in the dispatch conditions, means that item must be treated for dispatch, taxiing and flight purposes as though it were inoperative. The item shall not be EUROPEAN AVIATION SAFETY AGENCY MASTER MINIMUM EQUIPMENT LIST AIRCRAFT: CESSNA 525 REVISION NO. 01 DATE: 08/19/2014 PAGE NO. IV 525MMELEU-01 DEFINITIONS used or operated until the original deferred item is repaired. Additional actions include: documenting the item on the dispatch release (if applicable), placarding, and complying with all remarks, exceptions, and related MMEL provisions, including any (M) and (O) procedures and observing the rectification interval. 9. ‘Daylight’ means the period between the beginning of morning civil twilight and the end of evening civil twilight relevant to the local aeronautical airspace; or such other period, as may be prescribed by the appropriate authority. 10. ‘Day of discovery’ means the calendar day that a malfunction was recorded in the aircraft maintenance record/log book. 11. ‘Flight’ for the purposes of this MMEL, means the period of time between the moment when an aircraft begins to move under its own power, for the purpose of preparing for take-off, until the moment the aircraft comes to a complete stop on its parking area, after the first landing. 12. ‘Flight Day’, a 24-hour period from midnight to midnight based on either UTC or local time, as selected by the operator, during which at least one flight is initiated for the affected aircraft. ‘ETOPS’ or ‘ER operations’ refers to extended range operations of a two engine airplane as defined by Part-SPA. 13. ‘Icing Conditions’ means an atmospheric environment that may cause ice to form on the aircraft or in the engine(s) as defined in the AFM/RFM. 14. ‘If installed’ means that the item is either optional or is not required to be installed on all aircraft covered by the MMEL. 15. ‘Inoperative’ means that the item does not accomplish its intended purpose or is not consistently functioning within its approved operating limits or tolerances. 16. ‘Is not used’ in the provisions, remarks or exceptions for an MMEL item may specify that another item relieved in the MMEL ‘is not used’. In such cases, crew members should not activate, actuate, or otherwise utilise that item under normal operations. It is not necessary for the operators to accomplish the (M) procedures associated with the item. However, operations-related provisions, (O) procedures must be complied with. An additional placard must be affixed, to the extent practical, adjacent to the control or indicator for the item that is not used to inform crew members that an item is not to be used under normal operations. 17. ‘Intended flight route’ corresponds to any point on the route including diversions to reach alternate aerodromes required to be selected by the operational rules. 18. ‘Item’ means component, instrument, equipment, system or function. 19. ‘(M)’ indicates a requirement for a specific maintenance procedure which must be EUROPEAN AVIATION SAFETY AGENCY MASTER MINIMUM EQUIPMENT LIST AIRCRAFT: CESSNA 525 REVISION NO. 01 DATE: 08/19/2014 PAGE NO. V 525MMELEU-01 DEFINITIONS accomplished prior to operation with the listed item inoperative. Normally these procedures are accomplished by maintenance personnel, however, other personnel may be qualified and authorised to perform certain functions. The satisfactory accomplishment of all maintenance procedures, regardless of who performs them, is the responsibility of the operator. Appropriate procedures are required to be published as part of the Operator’s Manual or MEL. 20. ‘Master Minimum Equipment List’ means a document approved by the Agency that establishes the aircraft equipment allowed to be inoperative under conditions specified therein for a specific type of aircraft. 21. ‘Maximum distance from an adequate aerodrome for two-engine aeroplanes’ as defined in SPA.ETOPS and CAT.OP.AH.140. 22. ‘Minimum Equipment List’ means a document established as specified under 8.a.3. of Annex IV to Regulation (EC) No 216/2008 and approved by the competent authority, in accordance with ORO.MLR.105, that authorises an operator to dispatch an aircraft with aircraft equipment inoperative as per CAT.IDE.A/H.105 or NCC.IDE.A/H.105 under the conditions specified therein. 23. ‘Night” means the period between the end of evening civil twilight and the beginning of morning civil twilight relevant to the local aeronautical airspace; or such other period, as may be prescribed by the appropriate authority. Opposite of ‘Daylight’. 24. ‘Notes’ provide additional information for flight crew or maintenance consideration. Notes are used to identify applicable material which is intended to assist with compliance, but do not relieve the operator of the responsibility for compliance with all applicable requirements. Notes are not a part of the dispatch conditions. 25. ‘Number Installed’ is the number (quantity) of items normally installed in the aircraft. This number represents the aircraft configuration considered in developing this MMEL. Should the number be a variable (e.g. passenger cabin items), or not applicable, a number is not required; a ‘-’ is then inserted. Note: Where the MMEL shows a variable number installed, the MEL should reflect the actual number installed, as far as practical. 26. ‘Number required for dispatch’ is the minimum number (quantity) of items required for operation provided the conditions specified are met. Should the number be a variable (e.g. passenger cabin items) or not applicable, a number is not required; a ‘-’ is then inserted. Note: Where the MMEL shows a variable number required for dispatch, the MEL should reflect the actual number required for dispatch, as far as practical, or an alternate means of configuration control approved by the competent authority. 27. ‘-’ in the Number Installed Column (respectively Number Required for Dispatch Column) indicates a variable number (quantity) of the item installed (respectively item required) or not EUROPEAN AVIATION SAFETY AGENCY MASTER MINIMUM EQUIPMENT LIST AIRCRAFT: CESSNA 525 REVISION NO. 01 DATE: 08/19/2014 PAGE NO. VI 525MMELEU-01 DEFINITIONS applicable. Note: Where the MMEL shows a variable number installed, the MEL should reflect the actual number installed, as far as practical. 28. ‘(O)’ indicates a requirement for a specific operational procedure which must be accomplished in planning for and/or operating with the listed item inoperative. Normally these procedures are accomplished by the flight crew; however, other personnel may be qualified and authorised to perform certain functions. The satisfactory accomplishment of all procedures, regardless of who performs them, is the responsibility of the operator. Appropriate procedures are required to be published as a part of the operator’s manual or MEL. Note: The (M) and (O) symbols are required in the operator’s MEL. 29. ‘Operating minima’ means the set of requirements associated to operations requiring a specific approval (refer to Part-SPA). 30. ‘Placarding’ Each inoperative item must be placarded, as applicable, to inform and remind the crew members and maintenance personnel of the item’s condition. Note: To the extent practical, placards should be located adjacent to the control or indicator for the item affected; however, unless otherwise specified, placard wording and location will be determined by the operator. 31. ‘Rectification intervals’ Inoperative items or components, deferred in accordance with the MEL, must be rectified at or prior to the rectification intervals established by the following letter designators: Category A No standard interval is specified. However, items in this category shall be rectified in accordance with the conditions stated in the MMEL. (i) Where a time period is specified in calendar days or flight days, the interval excludes the day of discovery. (ii) Where a time period is specified other than in calendar days or flight days, it shall start at the point when the defect is deferred in accordance with the operator’s approved MEL. Category B Items in this category shall be rectified within three (3) calendar days, excluding the day of discovery. Category C Items in this category shall be rectified within ten (10) calendar days, excluding the day of discovery. EUROPEAN AVIATION SAFETY AGENCY MASTER MINIMUM EQUIPMENT LIST AIRCRAFT: CESSNA 525 REVISION NO. 01 DATE: 08/19/2014 PAGE NO. VII 525MMELEU-01 DEFINITIONS Category D Items in this category shall be rectified within one hundred and twenty (120) calendar days, excluding the day of discovery. 32. ‘Remarks or Exceptions’ include statements either prohibiting or allowing operation with a specific number of items inoperative, provisos (conditions and limitations), notes, (M) and/or (O) symbols, as appropriate for such operation. 33. ‘Required Cabin Crew Seat’ is a seat in the aircraft cabin which meets the following conditions: 1) Where the certification of the cabin requires this seat to be occupied by a qualified cabin crew member as specified in the Operations Manual; 2) This seat is a part of the station to which a qualified cabin crew member is assigned for the flight; and 3) The qualified cabin crew member assigned to the station is a member of the minimum cabin crew designated for the flight. 34. ‘Visible Moisture’ means an atmospheric environment containing water in any form that can be seen in natural or artificial light; for example, clouds, fog, mist, rain, sleet, hail, or snow. EUROPEAN AVIATION SAFETY AGENCY MASTER MINIMUM EQUIPMENT LIST AIRCRAFT: CESSNA 525 REVISION NO. 01 DATE: 08/19/2014 PAGE NO. VIII 525MMELEU-01 PREAMBLE Introduction The following is applicable for operators under European air operations regulations (Regulation Air Operations). Paragraph 1.c.2 of Annex I to Article 5 (essential requirements for airworthiness) of Regulation (EC) No 216/2008 (the ‘Basic Regulation’) requires that all equipment installed on an aircraft required for type certification or by operating rules shall be operative. However, paragraph 2.a.3 of Annex IV to Article 8 (essential requirements for air operations) of the Basic Regulation also allows the use of a Minimum Equipment List (MEL) where compliance with certain equipment requirements is not necessary in the interests of safety under all operating conditions. Experience has shown that with the various levels of redundancy designed into aircraft, operation of every system or installed items may not be necessary when the remaining operative equipment can provide an acceptable level of safety. Purpose and limitations This Master Minimum Equipment List (MMEL) is developed by the applicant and holders of (Supplemental) Type Certificate and approved by the European Aviation Safety Agency to improve aircraft use and thereby providing more convenient and economic air transportation for the public. This MMEL includes those items related to airworthiness, air operations, airspace requirements and other items the Agency finds may be inoperative and yet maintain an acceptable level of safety by appropriate conditions and limitations; it does not contain obviously required items such as wings, flaps, and rudders. In order to maintain an acceptable level of safety, the MMEL establishes limitations on the duration of and conditions for operation with inoperative items. Unless specifically allowed by this MMEL, an inoperative item may not be removed from the aircraft. Utilisation The MMEL is the basis for the development of individual operator’s MEL which take into consideration the operator’s particular aircraft equipment configuration and operational conditions. An operator’s MEL may differ in format from the MMEL, but shall not be less restrictive than the MMEL. The individual operator’s MEL, when approved, allows operation of the aircraft with inoperative items of equipment for a certain period of time until rectification can be accomplished. The MEL cannot deviate from Airworthiness Directives, or any other additional mandatory requirements. It is important to remember that all items related to the airworthiness and the operational regulations of the aircraft not listed on the MMEL shall be operative. Suitable conditions and limitations in the form of placards, maintenance procedures, crew operating procedures and other restrictions as prescribed in this MMEL shall be specified in the MEL to ensure that an acceptable level of safety is maintained. It is important that rectifications be accomplished at the earliest opportunity. When an item is discovered to be inoperative, it is reported by making an entry in the continuing EUROPEAN AVIATION SAFETY AGENCY MASTER MINIMUM EQUIPMENT LIST AIRCRAFT: CESSNA 525 REVISION NO. 01 DATE: 08/19/2014 PAGE NO. IX 525MMELEU-01 PREAMBLE airworthiness record system or the operator’s technical log, as applicable. Following sufficient fault identification, the item is then either rectified or deferred following the MEL or other approved means of compliance acceptable to the competent authority and the Agency prior to further operation. MEL conditions and limitations do not relieve the operator from determining that the aircraft is in a condition for safe operation with items inoperative. Prior to operation with any item inoperative acceptance by the crew is required in accordance with the continuing airworthiness management procedures. Operators shall establish a controlled and sound rectification programme including the parts, personnel, facilities, procedures and schedules to ensure timely rectification. Operators should include guidance in the MEL to deal with any failures which occur between the commencement of the flight and the start of the take-off. When developing the MEL, compliance with the stated intent of the preamble, definitions and the conditions and limitations specified in this MMEL is required. Multiple inoperative items Operators are responsible for exercising the necessary operational control to ensure that an acceptable level of safety is maintained. The exposure to additional failures during continued operation with inoperative items shall also be considered. Wherever possible, account has been taken in this MMEL of multiple inoperative items. However, it is unlikely that all possible combinations of this nature have been accounted for. Therefore, when operating with multiple inoperative items, the inter-relationships between those items and the effect on aircraft operation and crew workload shall be considered. Rectification interval extension The operator may be permitted, by its competent authority, to extend the rectification intervals of the MEL. This MMEL has been evaluated taking into account a one-time extension of the rectification intervals of category B, C and D. EUROPEAN AVIATION SAFETY AGENCY MASTER MINIMUM EQUIPMENT LIST AIRCRAFT: CESSNA 525 REVISION NO. 01 DATE: 08/19/2014 PAGE NO. X 525MMELEU-01 GUIDELINES FOR (M) & (O) PROCEDURES The OEB 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 525 Master Minimum Equipment List (P/N 525COMPEU-01-00, or later revision). Operator’s MEL procedures should be based on the Cessna procedures. EUROPEAN AVIATION SAFETY AGENCY MASTER MINIMUM EQUIPMENT LIST AIRCRAFT: CESSNA 525 REVISION NO. 01 DATE: 08/19/2014 PAGE NO. 21-1 SYSTEM, SEQUENCE NUMBERS & ITEM 1. REPAIR CATEGORY 2. NUMBER INSTALLED 3. NUMBER REQUIRED FOR DISPATCH 4. REMARKS AND EXCEPTIONS 21 ENVIRONMENTAL CONTROL 525MMELEU-01 -20-01 Cabin Overhead Air Outlet C - 0 -20-02 Cockpit Overhead Air Outlet C 2 0 -21-06 Glareshield Fan (Units -0001 thru -0359 excluding G1000-equipped aircraft) C - 1 -21-06 Glareshield Fan (Units -0001 thru -0359 G1000-equipped aircraft) C 2 1 One may be inoperative provided aircraft is operated in accordance with G1000 AFM supplement temperature limitations. -21-06 Glareshield Fan (Units -0360 thru -0701) C 2 1 One may be inoperative. -21-07 Instrument Panel Cooling Fan (CNI-5000 communications rack) (Units -0001 thru -0359 excluding G1000-equipped aircraft and Units -0360 thru -0558) B 2 0 NOTE: Radio service life may be extended by selecting unused radios OFF. -01 FAN 1 Amber Light C 1 0 (M) May be inoperative provided both cooling fans are verified operative. EUROPEAN AVIATION SAFETY AGENCY MASTER MINIMUM EQUIPMENT LIST AIRCRAFT: CESSNA 525 REVISION NO. 01 DATE: 08/19/2014 PAGE NO. 21-2 SYSTEM, SEQUENCE NUMBERS & ITEM 1. REPAIR CATEGORY 2. NUMBER INSTALLED 3. NUMBER REQUIRED FOR DISPATCH 4. REMARKS AND EXCEPTIONS 21 ENVIRONMENTAL CONTROL 525MMELEU-01 -21-08 Nose Avionics Cooling Fan -01 Radome Bulkhead (RH FS 43) (Units -0001 thru -0359 excluding G1000-equipped aircraft) C 1 0 May be inoperative provided aircraft is operated in accordance with AFM NOSE AVIONICS COOLING FAN abnormal procedure. -01 Radome Bulkhead (RH FS 43) (Units -0001 thru -0359 G1000-equipped aircraft) C 1 0 May be inoperative provided aircraft is operated in accordance with G1000 AFM supplement temperature limitations. -01 Radome Bulkhead (LH FS 43) (Units -0360 and on) C 1 0 May be inoperative provided ground operations with avionics ON are limited to 30 minutes. -02 Vaneaxial Snorkel (MN001) (Units -0001 thru -0359) C 1 0 -21-10 Ported Cooling Fan -01 Radio (KA 33 Panel Fan) (Units -0001 thru -0359 G1000-equipped aircraft) C 1 0 May be inoperative provided aircraft is operated in accordance with G1000 AFM supplement temperature limitations. -02 Integrated Avionics Unit (GIA FAN 1/2) (Units -0001 thru -0359 G1000-equipped aircraft) C 2 1 May be inoperative provided aircraft is operated in accordance with G1000 AFM supplement temperature limitations. -21-11 Display Fan (Units -0001 thru -0359 G1000-equipped aircraft) C 3 0 May be inoperative provided aircraft is operated in accordance with G1000 AFM supplement temperature limitations. EUROPEAN AVIATION SAFETY AGENCY MASTER MINIMUM EQUIPMENT LIST AIRCRAFT: CESSNA 525 REVISION NO. 01 DATE: 08/19/2014 PAGE NO. 21-3 SYSTEM, SEQUENCE NUMBERS & ITEM 1. REPAIR CATEGORY 2. NUMBER INSTALLED 3. NUMBER REQUIRED FOR DISPATCH 4. REMARKS AND EXCEPTIONS 21 ENVIRONMENTAL CONTROL 525MMELEU-01 -30-01 Cabin Dump Function (Unpressurized) C 1 0 (M) May be inoperative provided: a) One outflow valve is removed, and b) Cabin pressurization system is considered inoperative (Refer to item 21-30-02). -30-02 Cabin Pressurization System -00A (Unpressurized with cabin occupants) (Units -0001 thru -0558) C 1 0 (O) May be inoperative provided: a) PRESS SYSTEM SELECT is selected to MANUAL, b) CABIN DUMP is selected ON, c) Aircraft is operated at 10,000 feet cabin altitude or below, and d) Flight crew oxygen system is used as required by operating rule. NOTE: CAB ALT 10,000 FT red annunciator may illuminate at 10,000 feet cabin altitude. -00A (Unpressurized with cabin occupants) (Units -0600 thru -0701) C 1 0 (O) May be inoperative provided: a) PRESS SYSTEM SELECT is selected to MANUAL, b) CABIN DUMP is selected ON, c) Aircraft is operated at 10,000 feet cabin altitude or below, and d) Flight crew oxygen system is used as required by operating rule. NOTE: CABIN ALT red annunciator may illuminate at 10,000 feet cabin altitude. (Continued) EUROPEAN AVIATION SAFETY AGENCY MASTER MINIMUM EQUIPMENT LIST AIRCRAFT: CESSNA 525 REVISION NO. 01 DATE: 08/19/2014 PAGE NO. 21-4 SYSTEM, SEQUENCE NUMBERS & ITEM 1. REPAIR CATEGORY 2. NUMBER INSTALLED 3. NUMBER REQUIRED FOR DISPATCH 4. REMARKS AND EXCEPTIONS 21 ENVIRONMENTAL CONTROL 525MMELEU-01 -30-02 Cabin Pressurization System (Continued) -00A (Unpressurized with cabin occupants) (Units -0800 and on) C 1 0 (O) May be inoperative provided: a) PRESSURIZATION is selected to STBY, b) CABIN DUMP is selected ON, c) Aircraft is operated at 10,000 feet cabin altitude or below, and d) Flight crew oxygen system is used as required by operating rule. NOTE: PRESSURIZATION CTRL amber message may appear. CABIN ALTITUDE red message may appear and CABIN ALTITUDE aural warning may sound at 9,500 feet cabin altitude. -00B (Unpressurized without cabin occupants) (Units -0001 thru -0558) C 1 0 (O) May be inoperative provided: a) PRESS SYSTEM SELECT is selected to MANUAL, b) CABIN DUMP is selected ON, c) OXYGEN CONTROL VALVE is selected to CREW ONLY, d) No cabin occupants are carried, e) Aircraft is operated at FL250 or below, and f) Flight crew oxygen system is used as required by operating rule. NOTE: CAB ALT 10,000 FT red annunciator may illuminate at 10,000 feet cabin altitude. (Continued) EUROPEAN AVIATION SAFETY AGENCY MASTER MINIMUM EQUIPMENT LIST AIRCRAFT: CESSNA 525 REVISION NO. 01 DATE: 08/19/2014 PAGE NO. 21-5 SYSTEM, SEQUENCE NUMBERS & ITEM 1. REPAIR CATEGORY 2. NUMBER INSTALLED 3. NUMBER REQUIRED FOR DISPATCH 4. REMARKS AND EXCEPTIONS 21 ENVIRONMENTAL CONTROL 525MMELEU-01 -30-02 Cabin Pressurization System (Continued) -00B (Unpressurized without cabin occupants) (Units -0600 thru -0701) C 1 0 (O) May be inoperative provided: a) PRESS SYSTEM SELECT is selected to MANUAL, b) CABIN DUMP is selected ON, c) OXYGEN CONTROL VALVE is selected to CREW ONLY, d) No cabin occupants are carried, e) Aircraft is operated at FL250 or below, and f) Flight crew oxygen system is used as required by operating rule. NOTE: CABIN ALT red annunciator may illuminate at 10,000 feet cabin altitude. -00B (Unpressurized without cabin occupants) (Units -0800 and on) C 1 0 (O) May be inoperative provided: a) PRESSURIZATION is selected to STBY, b) CABIN DUMP is selected ON, c) OXYGEN CONTROL VALVE is selected to CREW ONLY, d) No cabin occupants are carried, e) Aircraft is operated at FL250 or below, and f) Flight crew oxygen system is used as required by operating rule. NOTE: PRESSURIZATION CTRL amber message may appear. CABIN ALTITUDE red message may appear and CABIN ALTITUDE aural warning may sound at 9,500 feet cabin altitude. EUROPEAN AVIATION SAFETY AGENCY MASTER MINIMUM EQUIPMENT LIST AIRCRAFT: CESSNA 525 REVISION NO. 01 DATE: 08/19/2014 PAGE NO. 21-6 SYSTEM, SEQUENCE NUMBERS & ITEM 1. REPAIR CATEGORY 2. NUMBER INSTALLED 3. NUMBER REQUIRED FOR DISPATCH 4. REMARKS AND EXCEPTIONS 21 ENVIRONMENTAL CONTROL 525MMELEU-01 -30-03 Emergency Pressurization System (Failed closed) C 1 0 (O) May be inoperative provided: a) Emergency pressurization valve is verified closed, and b) Aircraft is operated at FL250 or below. -31-02 Cabin Pressurization System Mode -01 Automatic Schedule Mode (Units -0001 thru -0701) C 1 0 May be inoperative provided: a) Isobaric mode is operative, b) Cabin differential pressure gauge / indication is operative, c) Cabin altitude gauge / indication is operative, and d) Cabin vertical speed gauge / indication is operative. -01 Automatic Schedule Mode (NORM) (Units -0800 and on) C 1 0 May be inoperative provided cabin pressurization system is considered inoperative (Refer to item 21-30-02). -03 Isobaric Mode (Units -0001 thru -0701) C 1 0 May be inoperative provided automatic schedule mode is operative. -04 Any Mode (Excluding manual) (Units -0001 thru -0701) C 2 0 May be inoperative provided cabin pressurization system is considered inoperative (Refer to item 21-30-02). -04 Any Mode (Excluding manual) (Units -0800 and on) C 1 0 May be inoperative provided cabin pressurization system is considered inoperative (Refer to item 21-30-02). EUROPEAN AVIATION SAFETY AGENCY MASTER MINIMUM EQUIPMENT LIST AIRCRAFT: CESSNA 525 REVISION NO. 01 DATE: 08/19/2014 PAGE NO. 21-7 SYSTEM, SEQUENCE NUMBERS & ITEM 1. REPAIR CATEGORY 2. NUMBER INSTALLED 3. NUMBER REQUIRED FOR DISPATCH 4. REMARKS AND EXCEPTIONS 21 ENVIRONMENTAL CONTROL 525MMELEU-01 -32-01 Cabin Altitude Gauge/Indication -00A (Pressurized) C 1 0 (O) May be inoperative provided: a) Cabin pressurization system automatic schedule mode is operative and used, b) Cabin differential pressure gauge/indication is operative, and c) A chart is provided to convert differential pressure and aircraft altitude to cabin altitude. -00B (Unpressurized) C 1 0 May be inoperative provided cabin pressurization system is considered inoperative (Refer to item 21-30-02). -01 Gauge Lighting (Units -0001 thru -0701) C 1 0 May be inoperative provided flight crew determines adequate natural or artificial lighting exists to read gauge. -32-02 Cabin Differential Pressure Gauge/Indication -00A (Pressurized) C 1 0 (O) May be inoperative provided: a) Cabin pressurization system automatic schedule mode is operative and used, b) Cabin altitude gauge/indication is operative, and c) A chart is provided to convert cabin and aircraft altitude to differential pressure. -00B (Unpressurized) C 1 0 May be inoperative provided cabin pressurization system is considered inoperative (Refer to item 21-30-02). EUROPEAN AVIATION SAFETY AGENCY MASTER MINIMUM EQUIPMENT LIST AIRCRAFT: CESSNA 525 REVISION NO. 01 DATE: 08/19/2014 PAGE NO. 21-8 SYSTEM, SEQUENCE NUMBERS & ITEM 1. REPAIR CATEGORY 2. NUMBER INSTALLED 3. NUMBER REQUIRED FOR DISPATCH 4. REMARKS AND EXCEPTIONS 21 ENVIRONMENTAL CONTROL 525MMELEU-01 -32-03 Cabin Vertical Speed Gauge/Indication -00A (Pressurized) C 1 0 May be inoperative provided: a) Cabin pressurization system automatic schedule mode is operative and used, and b) Cabin altitude gauge/indication is operative. -00B (Unpressurized) C 1 0 May be inoperative provided cabin pressurization system is considered inoperative (Refer to item 21-30-02). -33-01 Cabin Outflow Valve C 2 0 (M) May be inoperative provided: a) One outflow valve is removed, and b) Cabin pressurization system is considered inoperative (Refer to item 21-30-02). -50-02 Vapor-cycle Air Conditioning System C 1 0 (M) May be inoperative provided: a) Air conditioning system is deactivated, b) Cabin and cockpit temperature control systems are operative, c) All glareshield fans are operative, and d) Aircraft is operated in accordance with AFM temperature limitations. -01 *** Compressor Hour Meter C 1 0 (O) May be inoperative provided compressor hours are tracked by alternate means. -02 Compressor Light (COMPRESSOR ON) (Units -0001 thru -0701) C 1 0 EUROPEAN AVIATION SAFETY AGENCY MASTER MINIMUM EQUIPMENT LIST AIRCRAFT: CESSNA 525 REVISION NO. 01 DATE: 08/19/2014 PAGE NO. 21-9 SYSTEM, SEQUENCE NUMBERS & ITEM 1. REPAIR CATEGORY 2. NUMBER INSTALLED 3. NUMBER REQUIRED FOR DISPATCH 4. REMARKS AND EXCEPTIONS 21 ENVIRONMENTAL CONTROL 525MMELEU-01 -50-03 Evaporator Fan -05 Forward (FWD) (Units -0001 thru -0359 excluding G1000-equipped aircraft and Units -0360 and on) C 1 0 (M) May be inoperative provided: a) Aft evaporator fan is operative, b) Forward evaporator fan is deactivated, c) DEFOG FAN is selected OFF, d) Windshield anti-ice system is operative, and e) Crew has a means to clear the windshield of moisture. -05 Forward (FWD) (Units -0001 thru -0359 G1000-equipped aircraft) C 1 0 (M) May be inoperative provided: a) Aft evaporator fan is operative, b) Forward evaporator fan is deactivated, c) DEFOG FAN is selected OFF, d) Windshield anti-ice system is operative, e) Crew has a means to clear the windshield of moisture, and f) Aircraft is operated in accordance with G1000 AFM supplement temperature limitations with air conditioning off. -06 Aft (AFT) C 1 0 (M) May be inoperative provided: a) Forward evaporator fan is operative, b) Aft evaporator fan is deactivated, and c) Cockpit and cabin temperature control system manual mode is operative and used. EUROPEAN AVIATION SAFETY AGENCY MASTER MINIMUM EQUIPMENT LIST AIRCRAFT: CESSNA 525 REVISION NO. 01 DATE: 08/19/2014 PAGE NO. 21-10 SYSTEM, SEQUENCE NUMBERS & ITEM 1. REPAIR CATEGORY 2. NUMBER INSTALLED 3. NUMBER REQUIRED FOR DISPATCH 4. REMARKS AND EXCEPTIONS 21 ENVIRONMENTAL CONTROL 525MMELEU-01 -60-01 Cockpit and Cabin Temperature Control System C 2 0 May be inoperative provided cabin pressurization system is considered inoperative (Refer to item 21-30-02). -01 Automatic Mode C 1 0 May be inoperative provided temperature control system manual mode is operative and used. -02 Manual Mode C 1 0 May be inoperative provided temperature control system automatic mode is operative and used. EUROPEAN AVIATION SAFETY AGENCY MASTER MINIMUM EQUIPMENT LIST AIRCRAFT: CESSNA 525 REVISION NO. 01 DATE: 08/19/2014 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 525MMELEU-01 -10-01 Autopilot Disconnect Button (AP TRIM DISC) (Failed deselected) (Units -0001 thru -0359 excluding G1000-equipped aircraft) -10-01 Autopilot Disconnect Button (AP YD DISC/TRIM INT) (Failed deselected) (Units -0001 thru -0359 G1000-equipped aircraft) -10-01 Autopilot Disconnect Button (AP TRIM DISC) (Failed deselected) (Units -0360 thru -0701) -10-01 Autopilot Disconnect Button (AP DISC) (Failed deselected) (Units -0800 and on) -00A Left Control Wheel B 1 0 May be inoperative provided: a) Right control wheel button is operative, b) Pilot remains seated in right seat with seat belt fastened during all autopilot operations, c) Autopilot system is not used below AFM cruise minimum use height, and d) Approach minimums do not require use of autopilot system. -00B Right Control Wheel C 1 0 May be inoperative for single-pilot operations. (Continued) EUROPEAN AVIATION SAFETY AGENCY MASTER MINIMUM EQUIPMENT LIST AIRCRAFT: CESSNA 525 REVISION NO. 01 DATE: 08/19/2014 PAGE NO. 22-2 SYSTEM, SEQUENCE NUMBERS & ITEM 1. REPAIR CATEGORY 2. NUMBER INSTALLED 3. NUMBER REQUIRED FOR DISPATCH 4. REMARKS AND EXCEPTIONS 22 AUTO FLIGHT 525MMELEU-01 -10-01 Autopilot Disconnect Button (Failed deselected) (Continued) -00C (All buttons failed) B 2 0 May be inoperative provided: a) Autopilot system is considered inoperative (Refer to item 22-10- 03), and b) Electric elevator trim is considered inoperative (Refer to item 27-31- 01). -10-02 Autopilot Interrupt/Flight Director Sync Button (A/P TCS) (Units -0001 thru -0359 excluding G1000-equipped aircraft) C 2 0 -10-02 Autopilot Interrupt/Flight Director Sync Button (A/P CWS) (Units -0001 thru -0359 G1000-equipped aircraft) C 2 0 -10-02 Autopilot Interrupt/Flight Director Sync Button (A/P TCS) (Units -0360 thru -0558) C 2 0 -10-02 Autopilot Interrupt/Flight Director Sync Button (A/P SYNC) (Units -0600 thru -0701) C 2 0 -10-02 Autopilot Interrupt/Flight Director Sync Button (CWS) (Units -0800 and on) C 2 0 EUROPEAN AVIATION SAFETY AGENCY MASTER MINIMUM EQUIPMENT LIST AIRCRAFT: CESSNA 525 REVISION NO. 01 DATE: 08/19/2014 PAGE NO. 22-3 SYSTEM, SEQUENCE NUMBERS & ITEM 1. REPAIR CATEGORY 2. NUMBER INSTALLED 3. NUMBER REQUIRED FOR DISPATCH 4. REMARKS AND EXCEPTIONS 22 AUTO FLIGHT 525MMELEU-01 -10-03 Autopilot System B 1 0 (M) May be inoperative provided: a) Autopilot system is deactivated, b) Enroute procedures and approach minimums do not require use of autopilot system, c) Cabin pressurization system is not operated in manual mode, d) Aircraft is not operated RVSM, e) Aircraft is not operated single- pilot, and f) Yaw damper is considered inoperative (Refer to item 22-10- 05). -10-04 Takeoff/Go-Around Button (GA) C 1 0 May be inoperative provided: a) Flight director is not used during takeoff or go-around, b) Autopilot system is disconnected for go-around, and c) Autopilot interrupt/flight director sync button is operative on pilot flying side. NOTE: FMS missed approach procedure must be manually advanced. -10-05 Yaw Damper (Units -0001 thru -0701) B 1 0 (M) May be inoperative provided: a) Yaw damper is deactivated, and b) Autopilot system is considered inoperative (Refer to item 22-10- 03). -10-05 Yaw Damper (Units -0800 and on) B 1 0 (M) May be inoperative provided: a) Yaw damper is deactivated, b) Autopilot system is considered inoperative (Refer to item 22-10- 03), and c) Aircraft is operated at FL280 or below. EUROPEAN AVIATION SAFETY AGENCY MASTER MINIMUM EQUIPMENT LIST AIRCRAFT: CESSNA 525 REVISION NO. 01 DATE: 08/19/2014 PAGE NO. 22-4 SYSTEM, SEQUENCE NUMBERS & ITEM 1. REPAIR CATEGORY 2. NUMBER INSTALLED 3. NUMBER REQUIRED FOR DISPATCH 4. REMARKS AND EXCEPTIONS 22 AUTO FLIGHT 525MMELEU-01 -13-03 Flight Guidance Controller Annunciator (GMC 710) (Failed to illuminate) (Units -0001 thru -0359 G1000-equipped aircraft and Units -0800 and on) -01 Altitude (ALT button) C 1 0 May be inoperative provided appropriate annunciation appears in PFD flight director mode box. -03 Approach (APR button) C 1 0 May be inoperative provided appropriate annunciation appears in PFD flight director mode box. -04 Autopilot (AP button) C 1 0 May be inoperative provided AP annunciation appears in PFD flight director mode box. -05 Back Course (BC button) C 1 0 May be inoperative provided appropriate annunciation appears in PFD flight director mode box. -07 Coupled Side (XFR Button - left or right arrow) C 2 0 May be inoperative provided associated green coupled arrow appears in PFD flight director mode box. -09 Flight Level Change (FLC button) C 1 0 May be inoperative provided appropriate annunciation appears in PFD flight director mode box. -10 Half Bank (BANK button) C 1 0 May be inoperative provided green bank limit arc appears on PFD attitude display. (Continued) EUROPEAN AVIATION SAFETY AGENCY MASTER MINIMUM EQUIPMENT LIST AIRCRAFT: CESSNA 525 REVISION NO. 01 DATE: 08/19/2014 PAGE NO. 22-5 SYSTEM, SEQUENCE NUMBERS & ITEM 1. REPAIR CATEGORY 2. NUMBER INSTALLED 3. NUMBER REQUIRED FOR DISPATCH 4. REMARKS AND EXCEPTIONS 22 AUTO FLIGHT 525MMELEU-01 -13-03 Flight Guidance Controller Annunciator (Continued) -11 Heading (HDG button) C 1 0 May be inoperative provided appropriate annunciation appears in PFD flight director mode box. -12 Navigation (NAV button) C 1 0 May be inoperative provided appropriate annunciation appears in PFD flight director mode box. -13 Vertical Navigation (VNV button) C 1 0 May be inoperative provided appropriate annunciation appears in PFD flight director mode box. -14 Vertical Speed (VS button) C 1 0 May be inoperative provided appropriate annunciation appears in PFD flight director mode box. -15 Yaw Damper (YD button) C 1 0 May be inoperative provided YD annunciation appears in PFD flight director mode box. -13-04 Flight Guidance Controller Function Control (GMC 710) (Units -0001 thru -0359 G1000-equipped aircraft and Units -0800 and on) -02 Approach (APR button) B 1 0 May be inoperative provided procedures do not require its use. -03 Autopilot (AP button) B 1 0 May be inoperative provided autopilot system is considered inoperative (Refer to item 22-10-03). (Continued) EUROPEAN AVIATION SAFETY AGENCY MASTER MINIMUM EQUIPMENT LIST AIRCRAFT: CESSNA 525 REVISION NO. 01 DATE: 08/19/2014 PAGE NO. 22-6 SYSTEM, SEQUENCE NUMBERS & ITEM 1. REPAIR CATEGORY 2. NUMBER INSTALLED 3. NUMBER REQUIRED FOR DISPATCH 4. REMARKS AND EXCEPTIONS 22 AUTO FLIGHT 525MMELEU-01 -13-04 Flight Guidance Controller Function Control (Continued) -04 Back Course (BC button) C 1 0 May be inoperative provided procedures do not require its use. -05 IAS/Mach Change-over (SPD Button) D 1 0 -06 Coupled Side (XFR button) C 1 0 May be inoperative provided arrow points to pilot-flying side. -07 Course (CRS1 or CRS2 knob) B 2 1 One may be inoperative provided procedures do not require its use. -08 Course Direct (CRS1 or CRS2 PUSH DIR) C 2 0 -10 Flight Level Change (FLC button) C 1 0 May be inoperative provided procedures do not require its use. -11 Half Bank (BANK Button) C 1 0 -13 Heading Sync (HDG PUSH SYNC) C 1 0 -14 Navigation (NAV Button) B 1 0 May be inoperative provided procedures do not require its use. -16 Vertical Navigation (VNV button) C 1 0 May be inoperative provided procedures do not require its use. -17 Vertical Speed (VS button) C 1 0 May be inoperative provided procedures do not require its use. (Continued) EUROPEAN AVIATION SAFETY AGENCY MASTER MINIMUM EQUIPMENT LIST AIRCRAFT: CESSNA 525 REVISION NO. 01 DATE: 08/19/2014 PAGE NO. 22-7 SYSTEM, SEQUENCE NUMBERS & ITEM 1. REPAIR CATEGORY 2. NUMBER INSTALLED 3. NUMBER REQUIRED FOR DISPATCH 4. REMARKS AND EXCEPTIONS 22 AUTO FLIGHT 525MMELEU-01 -13-04 Flight Guidance Controller Function Control (Continued) -18 Yaw Damper (YD Button) C 1 0 NOTE 1: Yaw damper may be engaged by engaging autopilot. NOTE 2: Yaw damper may be disengaged by pressing autopilot disconnect button. EUROPEAN AVIATION SAFETY AGENCY MASTER MINIMUM EQUIPMENT LIST AIRCRAFT: CESSNA 525 REVISION NO. 01 DATE: 08/19/2014 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 525MMELEU-01 -00-01 *** Flight Phone / SATCOM System D - 0 May be inoperative provided procedures do not require its use. -01 Cockpit Handset D - 0 May be inoperative provided procedures do not require its use. -02 Cabin Handset D - 0 -10-01 *** High Frequency (HF) Communication System -00A (Dual LRCS not required) D - - Any in excess of those required by operating rule may be inoperative. -00B (Dual LRCS required) C - 1 (O) Any in excess of one may be inoperative while conducting operations which 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 intended route of flight, and d) If SATCOM voice is to be used over intended route of flight, SATCOM voice short codes (INMARSAT) or direct dial commercial numbers (IRIDIUM) must be available, prior coordination with appropriate ATS (FIR) facility is required. NOTE: SATCOM voice is to be used only as a backup to normal HF communications. (Continued) EUROPEAN AVIATION SAFETY AGENCY MASTER MINIMUM EQUIPMENT LIST AIRCRAFT: CESSNA 525 REVISION NO. 01 DATE: 08/19/2014 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 525MMELEU-01 -10-01 High Frequency (HF) Communication System (Continued) -00C A - 1 (O) Any in excess of one may be inoperative provided: a) Alternate communication procedures are established and used, and b) Repairs are made within three calendar days. -01 Wire Antenna C 1 0 (M) May be inoperative, missing, or damaged provided: a) Horizontal and vertical stabilizers are inspected for damage, b) Any remaining portion of wire antenna is removed, and c) HF communication system is considered inoperative (Refer to item 23-10-01). -12-01 Very High Frequency (VHF) Communication System -00A (Operator other than a holder of an air carrier, or commercial operator certificate) D - - Any in excess of those required by operating rule may be inoperative provided: a) Affected system is not on an emergency bus, and b) Procedures do not require its use. (Continued) EUROPEAN AVIATION SAFETY AGENCY MASTER MINIMUM EQUIPMENT LIST AIRCRAFT: CESSNA 525 REVISION NO. 01 DATE: 08/19/2014 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 525MMELEU-01 -12-01 Very High Frequency (VHF) Communication System (Continued) -00B (Holder of an air carrier, or commercial operator certificate) C - 1 (O) May be inoperative provided: a) Affected system is not on an emergency bus, b) Operations are conducted under VFR over routes navigated by reference to visual landmarks, c) Applicable airspace requirements for the intended flight route are complied with, and d) Alternate procedures are established and used, if applicable. -01 *** VHF Datalink (VDL) (Units -0800 and on) D - 0 May be inoperative provided procedures do not require its use. -20-01 *** Satellite Datalink Service -01 Radio D - 0 -02A Weather D - 0 May be inoperative provided procedures do not require its use. NOTE: Any function(s) that operate normally may be used. -02B Weather C - 0 (O) May be inoperative provided alternate procedures are established and used. -03 Internet D - 0 -20-02 Ground Avionics/Diagnostics Wi-Fi System (Units -0800 and on) D 1 0 EUROPEAN AVIATION SAFETY AGENCY MASTER MINIMUM EQUIPMENT LIST AIRCRAFT: CESSNA 525 REVISION NO. 01 DATE: 08/19/2014 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 525MMELEU-01 -20-03 *** Selective Call (SELCAL) (System or individual channel) -00A (SELCAL not required) D - 0 May be inoperative provided procedures do not require its use. -00B (SELCAL required) C - 0 (O) May be inoperative provided alternate procedures are established and used. -20-04 *** SMS Text Message System (Units -0800 and on) D 1 0 -40-01 *** Automatic Cabin Briefer D 1 0 -40-03 Passenger Address (PA) System D 1 0 May be inoperative provided procedures do not require its use. -40-04 Passenger Seat Belt / Safety Chime C 1 0 (O) May be inoperative provided cabin occupants are briefed by alternate means. -50-01 Audio Panel (Units -0001 thru -0701) C 2 1 Right side panel may be inoperative provided aircraft is operated single-pilot. -02 Audio Selector / Volume Control (COM 1, COM 2, COM3, NAV 1, NAV 2, ADF 1, ADF 2, DME, MKR Button) (Per side) (Units -0001 thru -0359 G1000-equipped aircraft) C - - Individual selectors may be inoperative provided associated system is not required by procedures or operating rule. (Continued) EUROPEAN AVIATION SAFETY AGENCY MASTER MINIMUM EQUIPMENT LIST AIRCRAFT: CESSNA 525 REVISION NO. 01 DATE: 08/19/2014 PAGE NO. 23-5 SYSTEM, SEQUENCE NUMBERS & ITEM 1. REPAIR CATEGORY 2. NUMBER INSTALLED 3. NUMBER REQUIRED FOR DISPATCH 4. REMARKS AND EXCEPTIONS 23 COMMUNICATIONS 525MMELEU-01 -50-01 Audio Panel (Continued) -03 Marker Beacon Mute (MKR/MUTE Button) (Per side) (Units -0001 thru -0359 G1000-equipped aircraft) C 1 0 -04 Intercom (INTR COM Button) (Per side) (Units -0001 thru -0359 G1000-equipped aircraft) D 1 0 May be inoperative provided aircraft is operated single-pilot. -05 Cabin Communication (CABIN Button) (Per side) (Units -0001 thru -0359 G1000-equipped aircraft) D 1 0 -06 Clearance Playback (PLAY Button) (Per side) (Units -0001 thru -0359 G1000-equipped aircraft) D 1 0 -07 Marker Beacon High Sensitivity (HI SENS Button) (Per side) (Units -0001 thru -0359 G1000-equipped aircraft) D 1 0 May be inoperative provided approach procedures do not require its use. (Continued) EUROPEAN AVIATION SAFETY AGENCY MASTER MINIMUM EQUIPMENT LIST AIRCRAFT: CESSNA 525 REVISION NO. 01 DATE: 08/19/2014 PAGE NO. 23-6 SYSTEM, SEQUENCE NUMBERS & ITEM 1. REPAIR CATEGORY 2. NUMBER INSTALLED 3. NUMBER REQUIRED FOR DISPATCH 4. REMARKS AND EXCEPTIONS 23 COMMUNICATIONS 525MMELEU-01 -50-01 Audio Panel (Continued) -08 Microphone Selector Annunciator (COM1 MIC, COM2 MIC Annunciator) (Per side) (Units -0001 thru -0359 G1000-equipped aircraft) C 2 0 May be inoperative provided crew refers to PFD frequency box for active transmit frequency (shown in green). -50-05 Cockpit Headset and Boom Microphone D - - Any in excess of one headset (including boom microphone) for each required crew member on flight crew compartment duty may be inoperative or missing. -03 *** Active Noise Reduction (ANR) Function D - 0 May be inoperative provided normal audio function of headset is operative. -04 Powered Headset System (Units -0800 and on) D - 0 May be inoperative provided non- powered headset jack is operative or headset is not used. -50-06 Cockpit Headset Audio System -00A C 2 0 May be inoperative provided: a) Both cockpit overhead communication speakers are operative and used, b) Headset audio system is not required by operating rule or procedures, and c) Aircraft is not operated single- pilot. -00B C 2 1 One may be inoperative provided left side is operative for single-pilot operations. EUROPEAN AVIATION SAFETY AGENCY MASTER MINIMUM EQUIPMENT LIST AIRCRAFT: CESSNA 525 REVISION NO. 01 DATE: 08/19/2014 PAGE NO. 23-7 SYSTEM, SEQUENCE NUMBERS & ITEM 1. REPAIR CATEGORY 2. NUMBER INSTALLED 3. NUMBER REQUIRED FOR DISPATCH 4. REMARKS AND EXCEPTIONS 23 COMMUNICATIONS 525MMELEU-01 -50-07 Push-to-talk (PTT) Switch (Failed deselected) -01 Yoke Switch B 2 1 (O) One may be inoperative provided alternate procedures are established and used for transmitting. -01A Right Yoke Switch B 1 0 May be inoperative provided aircraft is operated single-pilot. -60-01 Static Wick NOTE: May include mounting base provided no damage exists to attaching structure. -01 Aileron (Each side) C 2 1 One may be damaged or missing provided outermost wick is installed and not damaged. -02 Wing Tip Assembly (Each side) (Units -0001 thru -0701) - 1 1 NOTE: Wing tip assembly is entire removable section outboard of fuel closure rib. -05 Elevator (Each side) C 3 1 Two may be damaged or missing provided outermost wick is installed and not damaged. -08 Rudder C 2 1 One may be damaged or missing provided uppermost wick is installed and not damaged. -09 Stinger - 1 1 EUROPEAN AVIATION SAFETY AGENCY MASTER MINIMUM EQUIPMENT LIST AIRCRAFT: CESSNA 525 REVISION NO. 01 DATE: 08/19/2014 PAGE NO. 23-8 SYSTEM, SEQUENCE NUMBERS & ITEM 1. REPAIR CATEGORY 2. NUMBER INSTALLED 3. NUMBER REQUIRED FOR DISPATCH 4. REMARKS AND EXCEPTIONS 23 COMMUNICATIONS 525MMELEU-01 -70-01 Cockpit Voice Recorder (CVR) -00A A 1 0 May be inoperative provided: a) Any Flight Data Recorder (FDR) required to be installed is operative, and b) Repairs are made within 72 hours since CVR was found to be inoperative or eight flights, whichever occurs first. -00C *** C 1 0 May be inoperative provided recorder is not required by operating rule. -01 *** Recorder Independent Power Supply (RIPS) C 1 0 -03A Datalink Recording C 1 0 May be inoperative provided datalink recording is not required by operating rule. -03B Datalink Recording A 1 0 May be inoperative provided repairs are made within three flight days. EUROPEAN AVIATION SAFETY AGENCY MASTER MINIMUM EQUIPMENT LIST AIRCRAFT: CESSNA 525 REVISION NO. 01 DATE: 08/19/2014 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 525MMELEU-01 -22-01 AC Inverter (Units -0001 thru -0099 excluding G1000-equipped aircraft) B 2 1 One may be inoperative provided: a) AC INV is selected to operative inverter, b) Aircraft is not operated at night, and c) Aircraft is not operated IFR. -22-01 AC Inverter (Units -0100 thru -0359 excluding G1000-equipped aircraft) B 2 1 One may be inoperative provided: a) INV is selected to operative inverter, b) Aircraft is not operated at night, and c) Aircraft is not operated IFR. -31-02 *** Battery Temperature Indicator C 1 0 -40-01 External Power System D 1 0 -50-01 *** AC Cockpit Outlet -00A (Outlet not required) D - 0 May be inoperative provided procedures do not require its use. -00B (Outlet required) C - 0 (O) May be inoperative provided alternate procedures are established and used. -60-01 *** DC Cockpit Outlet -00A (Outlet not required) D - 0 May be inoperative provided procedures do not require its use. -00B (Outlet required) C - 0 (O) May be inoperative provided alternate procedures are established and used. -60-02 *** Ground Dispatch Power System C 1 0 EUROPEAN AVIATION SAFETY AGENCY MASTER MINIMUM EQUIPMENT LIST AIRCRAFT: CESSNA 525 REVISION NO. 01 DATE: 08/19/2014 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 525MMELEU-01 -00-01 Required Documents Holder (Airworthiness Certificate, Registration, etc) D 1 0 (O) May be inoperative or missing provided an alternate means of securing and displaying documents is used. -10-01 Cockpit Assist Handle D 1 0 -10-03 Cockpit Sunvisor System (Including attach mechanism) D - 0 May be inoperative or missing provided: a) Crewmember’s field of vision is not obstructed, and b) Oxygen mask quick donning ability is not affected. -10-05 Flight Crew Seat (Per seat) -01A Armrest C 2 0 May be inoperative provided affected armrest is stowed in retracted position. -01B Armrest C 2 0 (M) May be inoperative provided affected armrest is removed. -02 *** Lumbar Support D 1 0 -03 Recline/Tilt Function B 1 0 (M) (O) May be inoperative provided: a) Affected seat is secured 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. -04 *** Restraint Buckle Protective Padding D 1 0 May be damaged or missing. (Continued) EUROPEAN AVIATION SAFETY AGENCY MASTER MINIMUM EQUIPMENT LIST AIRCRAFT: CESSNA 525 REVISION NO. 01 DATE: 08/19/2014 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 525MMELEU-01 -10-05 Flight Crew Seat (Per seat) (Continued) -06 Vertical Adjustment B 1 0 (M) (O) May be inoperative provided: a) Affected seat is secured in a position that permits pilot normal visibility, b) Full flight control movement is available, and c) Crewmember can reach all necessary controls and equipment while restrained. -07 Copilot Seat Belt / Shoulder Harness C 1 0 May be inoperative provided seat remains unoccupied. -08 Copilot Floor Tracking C 1 0 May be inoperative provided seat remains unoccupied. -10-08 Eye Reference Ball C 3 0 (O) May be inoperative or missing provided alternate procedures are established and used for eye position reference. -10-09 *** Yoke-mounted Chart Holder D - 0 -01 *** Light D - 0 -20-01 *** Cabin Ashtray (Excluding lavatory door) A - 1 May be inoperative or missing provided ashtray is replaced within three calendar days.