MINIMUM EQUIPMENT LIST

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MINIMUM EQUIPMENT LIST

Reference to FAA MMEL Rev.8d

HAWKER

HS - 125

Doc. No: LBZ-MEL HS 125 Issued 2 Revision 0

18 May 2020

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1 APPROVAL PAGE

2 APPROVAL REVISION STATUS 3 LIST OF EFFECTIVE PAGES 4 TABLE OF CONTENT

5 RECORD OF REVISION 6 DISTRIBUTION LIST 7 DEFINITION

8 PREAMBLE

9 MEL REVISION MANAGEMENT ATA 21 Air Conditioning

1 Engine Main Air Valves 21 – 1

2 Engine Main Air Valve Position Indicators 21 – 1

3 Air Cycle Machine / Cold Air Unit 21 – 3

4 Foot Warmer and Windscreen Demister Valve 21 – 3

5 Cabin Flood Valve 21 – 3

6 Ram Air Shut Off Valve 21 – 3

7 Overhead Air Flow Distribution Vents 21 – 4

8 Cabin Floor Valves 21 – 4

9 Cabin Flood Valve Indicator 21 – 4

10 Cabin Floor Valve Indicator 21 – 5

11 HP Air Valve 21 – 5

12 Pressure Regulating Shutoff Valve (PRSOV) 21 - 6

13 Cabin Recirculating Fan 21 – 6

14 Flight Deck Heat Valve/Auxiliary Heating Valve 21 – 6

15 Flight Deck Recirculating Fan (s) 21 – 6

16 Mixing Valves 21 – 6

17 Cabin Altitude Warning Light / Annunciator 21 - 6

18 Cabin Altitude Aural Warning 21 - 7

19 Automatic Cabin Pressure Controller / DCPS AUTO Mode 21 - 7

20 Fan Operated Venturi 21 - 8

21 Outflow / Safety Valves 21 - 8

22 Cabin Pressure Instruments 21 – 8

23 Absolute Pressure Regulators 21 - 10

24 Air Jet Pump 21 - 10

25 Temperature Control System 21 - 11

26 Cabin Temperature Indicator 21 – 11

27 Cabin Duct Temperature Indicator 21 – 11

28 Low Limit Temp Control Valve 21 - 11

29 Cabin / VIP Temperature Control Switch 21 - 11

30 Cabin Temperature Control Valve 21 - 11

ATA 22 Auto Flight

1 Autopilot System(s) 22 – 1

2 Autopilot Control Yoke Disengage Switches 22 – 1

3 Yaw Damper / Autopilot Disconnect Switch on Autopilot Controller Panel 22 – 1

4 Go Around (GA) Switches 22 – 2

5 Control Yoke Pitch / Roll 22 – 2

6 Yaw Damper System 22 – 2

7 Autopilot Trim Annunciators 22 – 2

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8 Guidance Controller 22 – 2

9 Mode Select Panel 22 – 3

ATA 23 Communication

1 Radio management Units 23 – 1

2 Communications System 23 – 1

3 Audio Control panels 23 – 1

4 High Frequency (HF) Communication System 23 – 1

5 Selective Call System 23 – 1

6 Passenger Address System 23 – 2

7 Prerecording Passenger Announcement System 23 - 2

8 Flight Deck Speakers 23 - 2

9 Emergency locator transmitter (ELT) 23 - 2

10 Crewmember Interphone System 23 – 3

11 Headsets 23 – 3

12 Handheld Microphone 23 – 3

13 Boom Microphones 23 – 3

14 Glare shield Microphone Key Button(s) 23 – 3

15 Flight Deck Pilot-to-Pilot Interphone System 23 – 3

16 Cockpit Voice Recorder (Aircraft without FDR) 23 - 4

ATA 24 Electrical Power

1 AC Main Inverters 24 – 1

2 Standby Inverter 24 – 1

3 Inverter Fail Lights / Annunciators 24 – 1

4 Standby Inverter “ON” Light / Annunciator 24 – 1

5 AC Voltmeter 24 – 1

6 AC Alternators(s) 24 – 2

7 AC Alternator Fail Warning Light / Annunciator(s) 24 – 2

8 115 VAC / 60 HZ System 24 – 2

9 APU Generator 24 – 2

10 DC Generator Fail Lights / Annunciators 24 – 2

11 EXT POWER 24 – 2

12 DC Bus Tie Light / Annunciator 24 – 2

13 Battery Contactor Annunciators 24 - 3

14 APU Generator Fail Light / Annunciator 24 - 3

15 APU Generator Overheat Light / Annunciator 24 - 3

16 External Power System 24 - 3

17 AC Bus Fail Lights / Annunciators 24 - 3

18 26 VAC Bus Fail Annunciators 24 - 3

ATA 25 Equipment and Furnishing

1 Non-Essential Equipment & Furnishing (NEF) 25 – 1

2 Medical Transport System 25 – 1

3 Pilot (s) Seat Adjustment System 25 – 1

4 Cockpit Sun Visors 25 – 1

5 Observer Seat 25 – 2

6 Passenger Seat 25 – 2

7 Flight Inspection Panel 25 – 3

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8 Waste Receptacle Access Door / Cover 25 – 3

9 Emergency Medical Equipment 25 – 3

10 Overwater Equipment 25 - 4

ATA 26 Fire Protection

1 Engine Fire Warning Lights/ Annunciators 26 – 1

2 HP Cock Fire Warning Lights 26 – 1

3 APU Fire Detection System 26 – 1

4 APU Fire Detection Test System 26 – 1

5 APU Fire Extinguisher System 26 – 1

6 Engine Fire Extinguisher Relief Discharge Indicator 26 – 1

7 Portable Fire Extinguishers 26 - 2

8 Forward / Aft baggage Smoke Detection Systems 26 – 2

9 Lavatory Smoke Detection System 26 – 2

10 Rear Baggage Pannier Smoke Detection System 26 – 2

ATA 27 Flight Control

1 Aileron Trim Position Indicator 27 - 1

2 Rudder trim Position Indicator 27 - 1

3 Rudder Pedal Adjustment Systems 27 - 1

4 Electrical Elevator Trim 27 - 1

5 Stick Shaker Motors 27 - 2

6 Mach Trim System 27 - 2

7 Flap Position Indicator 27 - 2

8 Flap Handle Select Position Indicator 27 - 2

9 Flap Position Switches 27 - 3

10 Air Brake Position Indicator(s) 27 - 4

11 Control Column Lock System 27 - 4

ATA 28 Fuel

1 Fuel Booster Pumps 28 – 1

2 Fuel Transfer/Cross feed Indicator 28 – 1

3 Ventral Tank Fuel Transfer Valve 28 – 2

4 Ventral Tank Transfer Light/Annunciator 28 – 2

5 Pressure Fueling System 28 - 2

6 Pressure Refuel Blanking Cap 28 – 3

7 Wing Tank Fuel Content Indicators 28 - 3

8 Ventral Tank “EMPTY/FULL” Indicator 28 - 3

9 Low Vmo Audible Warning System 28 - 3

10 Fuel Temperature Indicator 28 - 4

ATA 29 Hydraulic

1 HYD LO PRESS 1 or 2 Annunciators 29 – 1

2 Combined BRAKES and SUPPLY Pressure Gauge 29 – 1

3 AUX HYD LO LEVEL Annunciator 29 – 1

4 Accumulator Pressure Indicators 29 – 1

5 Thrust Reverser Accumulator Pressure Indicator 29 - 2

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ATA 30 Ice and Rain Protection

1 TKS Airframe De-icing System 30 – 1

2 WING/TAIL ANTI-ICE Control Switches 30 – 1

3 T.K.S. Quantity Indication System 30 – 1

4 ANTI-ICE LO PRESS Annunciator 30 – 1

5 ANTI-ICE LO QTY Annunciator 30 – 2

6 Engine Inlet Anti-icing Systems 30 - 2

7 Engine Inlet Anti-Ice Indicators/Annunciators 30 - 3

8 MWS “ICE PROT SELECTED” White Annunciator 30 – 3

9 Pitot Probe/Pitot Mast Heaters 30 - 3

10 Pitot Ammeter & Selector 30 - 3

11 Pitot/Mast Heater FAIL Light(s)/Annunciator(s) 30 – 4

12 Static Plate Heaters 30 - 4

13 Stall Vane Heaters 30 - 4

14 L or R VANE HTR FAIL Annunciators 30 - 4

15 Windscreen Heating System 30 – 5

16 Windscreen Overheat Lights/Annunciators 30 – 5

17 Ice Detection System 30 - 5

ATA 31 Indicating Recording System

1 Clocks 31 – 1

2 Flight Data Recorder (FDR) System 31 – 1

3 Dual Filament Annunciator (s) 31 – 1

4 Transfer/Reversion Switch Lights (Collins Proline 21) 31 – 1 ATA 32 Landing Gear

1 MLG Door Latch Springs 32 – 1

2 Gear Down and Locked 32 - 1

ATA 33 Lights

1 Cockpit / Flight Deck / Flight Compartment and Instrument Lighting

Systems 33 – 1

2 Master Warning Light Systems 31 – 1

3 Cabin Interior Light System 31 – 1

4 Passenger Notice System 31 – 1

5 EMERG LTS NOT SEL/EMER LTS NOT SLCT Annunciator 33 – 2

6 Wheel Well Lighting System 31 – 1

7 Rear Equipment Bay Lighting 31 – 1

8 Pannier Lighting System 31 – 2

9 Anti-Collision Beacons 31 – 2

10 Landing Lights 31 – 2

11 Taxi Lights 31 – 2

12 Position Lights (Navigation) 31 - 3

13 Wing Ice Light(s) 31 - 3

14 Logo Lights 31 - 3

15 Pulselite System 31 - 3

16 Wing Tip Taxi Lighting System 31 – 4

17 Cabin Emergency Lighting System 31 – 4

18 Floor Proximity Lighting System 31 – 4

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ATA 34 Navigation

1 Mach Indications 34 – 1

2 SAT/ TAT Indicating System 34 – 1

3 TAS/ Indicating System 34 – 1

4 Non-Stabilized Magnetic Compass (Standby) 34 – 1

5 VMO/ MMO Aural Warnings 34 – 2

6 Altitude Alerting System 34 – 2

7 Altimeter Vibrators 34 – 3

8 Outside Air Temperature (OAT) Indicator 34 – 3

9 Air Data Computer Changeover/ Reversion Switches 34 – 3

10 Vertical Speed Indicator 34 – 3

11 Flight Director System(s) 34 – 3

12 Turn and Bank Indication 34 – 4

13 Magnetic Direction Indicator (Standby compass) 34 – 4

14 Compass and Attitude/AHRS Changeover/Reversion Switches 34 – 4

15 Symbol Generator Reversion Switches 34 – 5

16 Instrument Comparator 34 – 5

17 Standby Flight Instruments /Displays 34 – 5

18 Marker Beacons 34 – 6

19 Radio Compass (ADF) System 34 – 6

20 NAV/ COM Preselect Tuning Functions 34 – 6

21 NAV/ COM/ ADF/ TDR Memory Channels 34 – 6

22 NAV/ COM/ ADF/ TDR Digital Frequency Selector/ LCD/ LED 34 - 6

23 Radio Altimeter System 34 - 6

24 Weather Radar System 34 – 7

25 Terrain Awareness Warning System (TAWS) (Class B) 34 - 7 26 Flight Management System (FMS) / Control Display Units (CDU) 34 - 9

27 Distance Measuring Equipment (DME) Systems 34 - 9

28 ATC Transponders and Automatic Altitude Reporting Systems 34 - 9

29 VHF Navigation (VOR/ILS) System 34 - 9

30 Global Positioning System (GPS) 34 - 9

31 Traffic Collision and Avoidance System 34 – 10

32 Electronic Flight Displays (EFD’s) 34 – 10

33 EFIS Symbol Generator Units (SG, MSG, DPU, and/or MPU) 34 - 10

34 EADI Annunciator/Displays 34 – 11

35 Electronic Checklist System and Controls 34 - 11

ATA 35 Oxygen 35 – 1

1 Oxygen Content Indicator(s) 35 – 1

2 Oxygen Cylinders 35 – 3

3 Barometric Valve Automatic Function 35 – 3

4 Protective Breathing Equipment (PBE) 35 – 3

5 Passenger Oxygen Masks and Stowages 35 - 3

6 Portable Oxygen Dispensing Unit 35 - 4

ATA 38 Water and Waste

1 Portable Water System 38 – 1

2 Oxygen Cylinders 38 – 1

3 Lavatory Waste System (Blue Water) 38 – 2

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ATA 45 Central Maintenance Computer

1 Maintenance Diagnostic Computer (MDC) 45 – 1

ATA 46 Information System

1 Integrated Flight Information System (Pro Line 21 IFIS-5000) 46 – 1 ATA 49 Airborne Auxiliary Power

1 Auxiliary Power Unit 49 - 1

2 APU Air/Load Control Valve 49 - 1

3 APU Instrumentation 49 - 1

ATA 52 Doors

1 Main Entry Door Unlock Indication System 52 – 1

2 Rear Baggage Pannier/External Baggage Compartment Hatch Unlock

Indication 52 – 1

3 Keyed Exterior Door Locks 52 - 1

ATA 56 Windows

1 Windscreens “A” or “B” 56 - 1

ATA 73 Engine Fuel and Control

1 Fuel Flow Indicator 73 - 1

ATA 74 Engine Ignition

1 Ignition System 74 – 1

ATA 77 Engine Indicating

1 Engine Indications 77 – 1

ATA 78 Engine Exhaust

1 Thrust Reversing System 78 – 1

2 Thrust Reverser Indicating Annunciators 78 – 2

ATA 79 Engine Oil

1 Oil Pressure Low Warning Light/Annunciators 79 – 1

ATA 80 Starting

1 Starter Power Available Annunciator 80 – 1

2 Starter Operating Annunciators 80 - 1

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ATA Chapter Page Last Revision Date of Revision Inserted By

MEL Revision

Management - 18 May 2020 Ops Dept

21-80 14 Apr 2016 18 May 2020 Ops Dept

RETAIN THIS RECORD IN THE FRONT PAGE OF THE MANUAL. UPON RECEIPT OF REVISIONS, INSERT THE REVISED PAGES IN THE MANUAL AS PER THE FILING INSTRUCTIONS PROVIDED.

ENTER THE CORRESPONDING REVISION NUMBER AND DATE ON THIS PAGE. WHEN FINISHED, PROVIDE THE DATE INSERTED AND SIGN OR PRINT NAME ACCORDINGLY

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No. Format Assignment Remarks

1 Soft copy Library Master / Controlled

2 Soft copy DGCA Controlled

3 Printed / Soft copy Aircraft Controlled

Minimum Equipment List (MEL) is available in two versions, printed (hard copy) and electronics (soft copy).

The printed / electronic (Soft Copy) controlled copy document is to be distributed to the name listed below and must be ensure that their document is maintain current, unless such time as they are removed from the distribution list.

This manual will be available and distributed throughout the organization incorporated in the on-line version (electronic manual in PDF format) available on File Management System Website http://192.168.180.10/bizjet/filemanagement or http://Operation.lionair.co.id/bizjet/filemanagement for ensuring that any revisions to this manual are incorporated in the on-line version (electronic manual in PDF format) available on File Management System. The MEL will be CONTROLLED and CURRENT ONLY in this website. Any printed form of this guidance is UNCONTROLLED.

This manual is accessible to flight operation personnel through this website.

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1. System Definitions

System numbers are based on the Air Transport Association (ATA) Specification Number 102 and items are numbered sequentially.

a. "Sequence Number and System" (Column 1) means the equipment, system, component, or function listed in the "Sequence Number and System" column.

b. "Repair Category" (Column 2) is repair intervals, means all users of an MEL approved under CASR 121, 125, 129 and 135 must effect repairs of inoperative systems or components, deferred in accordance with the MEL, at or prior to the repair times established by the following letter designators:

Category A. Items in this category shall be repaired within the time interval specified in the remarks or Exceptions column

Category B. Items in this category shall be repaired within three (3) consecutive calendar days (72 hours), excluding the day the malfunction was recorded in the aircraft maintenance record/logbook. For example, if it were recorded at 10 a.m.

on January 26th, the three day interval would begin at midnight the 26th and end at midnight the 29th.

Category C. Items in this category shall be repaired within ten (10) consecutive calendar days (240 hours), excluding the day the malfunction was recorded in the aircraft maintenance record/logbook. For example, if it were recorded at 10 a.m. on January 26th, the 10 day interval would begin at midnight the 26th and end at midnight February 5th.

Category D. Items in this category shall be repaired within one hundred and twenty (120) consecutive calendar days (2880 hours), excluding the day the malfunction was recorded in the aircraft maintenance log and/or record. The letter designators are inserted adjacent to Column 2

c. "Number Installed" (Column 3) is the number (quantity) of items normally installed in the aircraft. This number represents the aircraft configuration considered in developing this MEL.

Should the number be a variable (e.g., passenger cabin items) a number is not required.

d. "Number Required for Dispatch" (Column 4) is the minimum number (quantity) of items required for operation provided the conditions specified in Column 4 are met.

NOTE: Where the MEL shows a variable number required for dispatch, the MEL must reflect the actual number required for dispatch or an alternate means of configuration control approved by the Administrator.

e. "Remarks or Exceptions" (Column 5) in this column includes a statement either prohibiting or permitting operation with a specific number of items inoperative, provisos (conditions and limitations) for such operation, and appropriate notes.

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f. "Maintenance Procedure Required" (M) indicates a requirement for a specific maintenance procedure, which must be accomplished prior to operation with the listed item inoperative.

Normally these procedures are accomplished by maintenance personnel; however, other personnel may be qualified and authorized to perform certain functions. Procedures requiring specialized knowledge or skill, or requiring the use of tools or test equipment should be accomplished by maintenance personnel. 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.

g. "Operation Procedure Required" (O) indicates a requirement for a specific operations 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 authorized 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 unless otherwise authorized by the Administrator.

h. “-" Symbol in Column 3 and/or Column 4 indicates a variable number (quantity) of the item installed.

i. Alphabetical Symbol (M/O) in Column 5 indicates a proviso (condition or limitation) that must be complied with for operation with the listed item inoperative.

2. "Airplane/Rotorcraft Flight Manual" (AFM/RFM) is the document required for type certification and approved by the responsible FAA Aircraft Certification Office. The FAA approved AFM/RFM for the specific aircraft is listed on the applicable Type Certificate Data Sheet.

3. "As required by CASR" means that the listed item is subject to certain provisions (restrictive or permissive) expressed in the Civil Aviation Safety Regulations operating rules. The number of items required by the CASR must be operative. When the listed item is not required by CASR it may be inoperative for time specified by repair category.

4. "Civil Aviation Safety Regulations" (CASR) means the applicable portions of the Indonesian Directorate General of Air Certification Regulations.

5. "Deleted" in the remarks column after a sequence item indicates that the item was previously listed but is now required to be operative if installed in the aircraft.

6. "ER" or “ETOPS” refers to extended range operations of a two-engine airplane, which has a type design approval for ER operations and complies with the provisions of Advisory Circular 120- 42A.

7. "***" symbol in Column 1 indicates an item which is not required by regulation but which may have been installed on some models of aircraft covered by this MMEL. This item may be included on the operator's MEL after the approving office has determined that the item has been installed on one or more of the operator's aircraft. The symbol, however, shall not be carried forward into the operator's MEL. It should be noted that neither this policy nor the use of this symbol provide authority to install or remove an item from an aircraft.

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8. "Flight Day" means a 24 hour period (from midnight to midnight) either Universal Coordinated Time (UTC) or local time, as established by the operator, during which at least one flight is initiated for the affected aircraft.

9. "Icing Conditions" means an atmospheric environment that may cause ice to form on the aircraft or in the engine(s).

10. "Inoperative" means a system and/or component malfunction to the extent that it does not accomplish its intended purpose and/or is not consistently functioning normally within its approved operating limit(s) or tolerance(s).

11. "Notes:" in Column 7 provides additional information for crewmember 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 provisos.

12. Inoperative components of an inoperative system: Inoperative items, which are components of a system, which is inoperative are usually considered components directly associated with and having no other function than to support that system.

(Warning/caution systems associated with the inoperative system must be operative unless relief is specifically authorized per the MMEL).

13. "Deactivated" and "Secured" means that the specified component must be put into an acceptable condition for safe flight. An acceptable method of securing or deactivating will be established by the operator.

14. Visual Flight Rules" (VFR) is as defined in CASR Part 91. This precludes a pilot from filing an Instrument Flight Rules (IFR) flight plan.

15. "Visual Meteorological Conditions" (VMC) means the atmospheric environment is such that would allow a flight to proceed under the visual flight rules applicable to the flight.

This does not preclude operating under Instrument Flight Rules.

16. "Visible Moisture" means an atmospheric environment containing water in any form that can be seen in natural or artificial light; for example, clouds, fog, rain, sleet, hail, or snow.

17. "Passenger Convenience Items" means those items related to passenger convenience, comfort or entertainment such as, but not limited to, galley equipment, movie equipment, ashtrays, stereo equipment, overhead reading lamps, etc.

18. Electronic fault alerting system - General

New generation aircraft display system fault indications to the flight crew by use of computerized display systems. Each aircraft manufacturer has incorporated individual design philosophies in determining the data that would be represented. The following are customized definitions (specific to each manufacturer) to help determine the level of messages affecting the aircraft's dispatch status. When preparing the MEL document, operators are to select the proper Definition No. 23 for their aircraft, if appropriate.

19. "Excess Items" means those items that have been installed that are redundant to the requirements of the CASR.

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20. "Day of Discovery" is the calendar day an equipment/instrument malfunction was recorded in the aircraft maintenance log and or record. This day is excluded from the calendar days or flight days specified in the MMEL for the repair of an inoperative item of equipment. This provision is applicable to all MMEL items, i.e., categories "A, B, C, and D."

21. "Considered Inoperative", as used in the provisos means that item must be treated for dispatch, taxi and flight purposes as though it were inoperative. The item shall not be 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 MEL provisions, including any (M) and (O) procedures and observing the repair category.

22. "Is not used" in the provisos, remarks or exceptions for an MEL item may specify that another item relieved in the MEL “is not used.” In such cases, crewmembers should not activate, actuate, or otherwise utilize that component or system under normal operations. It is not necessary for the operators to accomplish the (M) procedures associated with the item. However, operational requirements must be complied with, and 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 crewmembers that a component or system is not to be used under normal operations.

23. Extended Over Water Operation:

a) A flight over water more than 50 nautical miles from the nearest shore and that airplane is equipped with a life preserver or an approved flotation means for each occupant of the airplane.

b) A flight over water more than 30 minutes flying time or 100 nautical miles from the nearest shore and it has on board the following survival equipment:

1) A life preserver, equipped with an approved survivor locator light, for each occupant of the airplane

2) Enough life rafts (each equipped with an approved survival locator light) of a rated capacity and buoyancy to accommodate the occupants of the airplane.

3) At least one pyrotechnic signaling device for each life raft.

4) One self-buoyant, water resistant, portable emergency radio signaling device that is capable of transmission on the appropriate emergency frequency or frequencies and not dependent upon the airplane power supply.

5) A lifeline stored with provisions as follows:

(a) Allow one life line to be attached to each side of the fuselage; and

(b) Be arranged to allow the life lines to be used to enable the occupants to stay on the wing after ditching.

(c) The required life rafts, life preservers, and signaling devices must be installed in conspicuously marked locations and easily accessible in the event of a ditching without appreciable time for preparatory procedures.

(d) A survival kit, appropriately equipped for the route to be flown, must be attached to each required life raft.

(e) As used in this section, the term shore means that area of the land adjacent to the water which is above the high water mark and excludes land areas which are intermittently under water.

24. “ULD” or Unit Load Device, is any type of container or pallet in which luggage, freight and mail can be transported by air. Each ULD is manifested separately so that its contents can be tracked.

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The following is applicable to PT. ANGKASA SUPER SERVICES as LION BIZJET.

The following is applicable for authorized certificate holders operating under CASR 135; CASR require that all equipment installed on an aircraft in compliance with the Airworthiness Standards and the Operating rules must be operative. However, the rules also permit the publication of a Minimum Equipment List (MEL) where compliance with certain equipment conditions. Experience has shown that with the various levels of redundancy designed into aircraft, operation of every system or installed component may not be necessary when the remaining operative equipment can provide an acceptable level of safety.

The DGAC approved Master Minimum Equipment List (MMEL) for aircraft which Indonesia holds responsibility as state of design, and MMELs accepted which have been approved by a foreign state of design includes, those items of equipment related to airworthiness, operating regulations and other items of equipment which the DGAC finds may be inoperative and yet maintain an acceptable level of safety. The acceptable level of safety may be achieved by appropriate conditions and limitations; it does not contain obviously required items such as wings, flaps, and rudders.

The MMEL is the basis for development of individual operator MELs which take into consideration the operator’s particular aircraft equipment configuration and operational conditions. Operator MELs, for administrative control, may include items must be approved by the DGAC. An operator’s MEL may differ in format from the MMEL, but cannot be less restrictive than the MMEL. The individual operator’s MEL, when approved and authorized, permits operation of the aircraft with inoperative equipment. Equipment not required by the operation being conducted and equipment in excess of CASR requirements are included in the MEL with appropriate conditions and limitations. The MEL must not deviate from the Aircraft Flight Manual Limitations, Emergency Procedures or with Airworthiness Directives. It is important to remember that all equipment related to the airworthiness and the operating regulations of the aircraft not listed on the MMEL must be operative.

Suitable conditions and limitations in the form of placards, maintenance procedures, crew operating procedures and other restrictions as necessary are specified in the MEL to ensure that an acceptable level of safety is maintained.

The MEL is intended to permit operation with inoperative items of equipment for a period of time until repairs can be accomplished. It is important that repairs be accomplished at the earliest opportunity. In order to maintain an acceptable level of safety and reliability the MMEL establishes limitations on the duration of and conditions for operation with inoperative equipment.

The MEL provides for release of the aircraft for flight with inoperative equipment. When an item of equipment is discovered to be inoperative, it is reported by making an entry in the Aircraft Maintenance Record/Logbook as prescribed by CASR. The item is then either repaired or may be deferred per the MEL or other approved means acceptable to the DGAC prior to further operation.

MEL conditions and limitations do not relieve the operator from determining that the aircraft is in condition for safe operation with items of equipment inoperative. When these requirements are met, a Maintenance Release, Aircraft Maintenance Record/Logbook entry, or other approved documentation is issued as prescribed by CASR. Such documentation is required prior to operation with any item of equipment inoperative.

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Operators are responsible for exercising the necessary operational control to ensure that an acceptable level of safety is maintained. When operating with multiple inoperative items, the interrelationships between those items and the effect on aircraft operation and crew workload will be considered. Operators are to establish a controlled and sound repair program including the parts, personnel, facilities, procedures and schedules to ensure timely repair.

WHEN USING THE MEL, COMPLIANCE WITH THE STATED INTENT OF THE PREMABLE, DEFINITIONS, AND THE CONDITIONS AND LIMITATIONS SPECIFIED IN THE MEL IS REQUIRED.

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Maintenance Department is responsible to prepare the Minimum Equipment List (MEL) revision. Each revision has a revision number and date of last revision on each page concerned. A revision bar marked in the right of the end line only in the affected line. This revision marks indicates that something within the entire line/paragraph has changed from the previous MEL revision.

In a first biweekly every month Operation Department (Chief Flight Standard and Training) and Maintenance Department (Chief PTS) must checking FSIMS (Flight Standard Information Management System) Website to see update MMEL.

In order to keep the MEL valid and updated, the MEL subjected to be reviewed and revised. The MEL review will be done immediately after the notification of any condition which require MEL to be revised has been issued.

Conditions that require MEL to be updated are:

1. Updated on Master Minimum Equipment List (MMEL);

2. Update on CASR which affect MEL;

3. MEL revision suggestion from Operation Department and Maintenance Department;

4. Aircraft Configuration change from Batam Aero Technics (BAT) which affect MEL.

One or several condition may affect the MEL. Hence, Operations Department is responsible to review the update notification(s) and compare with the MEL last revision. Hereinafter, the comparison must be validated through MEL review board. The results of the MEL review board are used by Operations Department to update the MEL upon the approval from Quality Assurance.

Updated MEL will be submitted to the DGCA for review and approval prior to implementation.

Reissuing the document (Manual) will be done, when a manual has undergone fundamental changes both in the title, table of contents, a description of the manual, the manual order, so the traceability for the revision of the manual is difficult to identify.

In terms of distribution, the procedure is refer to section 00-6-Distribution List. Mel Management Program is refer to CMM Chapter 5.2 maintenance Deferral Policy and Procedures.

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Number Required for Dispatch

Remarks or Exceptions

Number of Installed Repair Category

Sequence Number and System

10-1. Engine Main Air Valves C

C 2

2 1

0

(M+O) One may be inoperative for pressurized flight provided:

a) Valve is secured closed, and

b) Flight Deck Heat Valve System is operative

(M+O) May be inoperative provided:

a) Both Valves are secured closed,

b) Ram air and Dump/Vent Valves are verified operative before the first flight of the day

c) DUMP VLV / VENT VALVE is selected OPEN

d) Flight is conducted in an unpressurized configuration

e) Aircraft is operated at or below 15,000 feet MSL and

f) Applicable Oxygen requirements are established and complied with.

Maintenance Procedures:

1. Verify affected valve mechanical indicator arm is secured closed.

2. Pull and collar the affected MAIN AIR VLV circuit breaker 3. Disconnect electrical connector from valve, bag and stow Operation Procedures:

With engines running, select AUX HEAT (F/DK VLV) and confirm that airflow is present.

1. Visually confirm valve mechanical indicator arms are in the closed position.

2. Pull and collar the affected MAIN AIR VLV circuit breaker 3. Disconnect electrical connector from valve, bag and stow Operation Procedures:

Reference Table 1 configure aircraft for unpressurized flight.

10-2. Engine Main Air Valve Position

Indicators C

C

C 2

2

2 1

1

0

(O) One May be inoperative provided booth engine main air valves are operative.

(O) One May be inoperative provided indicator associated with the operative Engine main air valve is operative.

(M+O) May be inoperative provided:

UNCONTROLLED IF PRINTED

(26)

a) Both Valves are secured closed,

b) Ram air and Dump/Vent Valves are verified operative before the first flight of the day

f) Applicable Oxygen requirements are established and complied with.

Operation Procedures:

With engines running and APU OFF,

1. Sequentially select L & R main air valves OPEN and CLOSED

2. Confirm that airflow is present with valve OPEN and that flow stops when valve is closed

With engines running and APU OFF,

1. Select operative main air valve OPEN and CLOSED

2. Confirm that airflow is present with valve OPEN, associated indicator illuminates while valve is OPEN, and that flow stops when valve is closed.

1. Visually confirm booth valve mechanical indicator arms are in the closed position.

2. Pull and collar the affected MAIN AIR VLV circuit breaker.

3. Disconnect electrical connectors from both valves, bag and stow

Reference Table 1 configure aircraft for unpressurized flight.

10-3. Air Cycle Machine / Cold Air

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

a) Ram air and Dump/Vent Valves are verified operative before the first flight of the day

b) Both MAIN AIR VALVES are selected CLOSED

f) Applicable Oxygen requirements are

UNCONTROLLED IF PRINTED

(27)

established and complied with.

Reference Table 1 configure aircraft for unpressurized flight.

10-4. Foot warmer and Windscreen

Demister Valve C 1 0 May be inoperative provided windscreen heating system is operative

10-6. Cabin Flood Valve

1) Two-Way Cabin Flood Valve (Aircraft without Cabin Floor Valves)

2) Cabin Flood Valve (Aircraft with Cabin Floor Valves)

C C

C 1 1

1 0 0

0

May be inoperative

(O) May be inoperative provided LH or RH Cabin Floor Valve is verified operative.

(O) May be inoperative provided:

a) Ram Air and Dump/Vent Valves are verified operative before the first flight of the day, b) DUMP VLV / VENT VALVE is selected OPEN, c) Flight is conducted in an unpressurized

configuration,

d) Aircraft is operated at or below 15,000 feet MSL, and

e) Applicable Oxygen requirements are established and complied with Operation Procedures (1) :

With APU AIR ON or MAV open (Engines Running) 1. Select Cabin Floor Valve OPEN, and 2. Confirm airflow from Cabin Floor Vent Operation Procedures (2) :

Reference Table 1. Configure Aircraft for Unpressurized Flight

10-7. Ram Air Shut-Off Valve B 1 0 (M+O) May be inoperative for pressurized flight provided:

a) Valve is secured fully closed, and b) DUMP/Vent Valve is operative Maintenance Procedures:

1. Locate RAM AIR VALVE circuit breaker on DA-A Panel.

2. Pull and Collar the RAM AIR VLV circuit breaker.

3. Install INOP placard adjacent to shutoff valve lever.

4. Operate Dump valve OPEN and CLOSED Operation Procedures:

Operate Dump Valve OPEN and CLOSED

UNCONTROLLED IF PRINTED

(28)

10-10. Overhead Air Flow Distribution

Vents (Punkah Louvers) D 12 0 May be inoperative 10-11. Cabin Floor Valves C

C

C 2 2

2 1 0

0

One may be inoperative

(O) May be inoperative provided Cabin Flood Valve is verified operative

a) Ram Air and Dump/Vent valves are verified operative before the first flight of the day, b) DUMP VLV / VENT VALVE is selected OPEN, c) Flight is conducted in an unpressurized

configuration,

e) Applicable Oxygen requirements are established and complied with.

With APU AIR ON or MAV open (Engines Running) 1. Select Cabin Floor Valve OPEN, and 2. Confirm airflow from Cabin Floor Vent Operation Procedures:

Reference Table 1. Configure Aircraft for Unpressurized Flight 10-12. Cabin Flood Valve Indicator C

C 1

1 0

0

(O) May be inoperative provide:

a) Cabin Flood Valve is verified operative, and b) Cabin Floor valve Indicator is verified

operative

configuration,

e) Applicable Oxygen requirements are established and complied with Operation Procedures:

1. Confirm Flood Valve control by cycling open and close, check audibly for change in flow 2. Open and close Floor Valves, confirm indicator for position change.

Reference Table 1. Configure Aircraft for Unpressurized Flight

UNCONTROLLED IF PRINTED

(29)

10-13. Cabin Floor Valve Indicator C

C 1

1 0

0

a) Cabin Floor Valve is verified operative, and b) Cabin Flood valve Indicator is verified

operative

a) Ram Air and Dump/Vent Valves are verified operative before the first flight of the day, b) DUMP VLV / VENT VALVE is selected

OPEN,

c) Flight is conducted in an unpressurized configuration,

With either APU or main engine air,

1. Confirm operation of Cabin Floor Valve.

2. Confirm Flood Valve operation and indication by listening for flow change and observing Flood Valve Indicator.

Reference Table 1. Configure Aircraft for Unpressurized Flight 10-15. HP Air Valve

(With TFE-731 Engines Only) C

C 2

2 1

0

(O) One may be inoperative provide:

a) Affected Main Air Valve is verified closed, b) Cockpit auxiliary heating system is

operative, and

c) Aircraft is operated at or below FL250 (O) May be inoperative provided:

a) Both Main Air Valves are verified closed, b) Ram Air and Dump/Vent Valves are verified

operative before the first flight of the day, c) DUMP VLV /VENT VALVE is selected OPEN, d) Flight is conducted in an unpressurized

configuration,

e) Aircraft is operated at or below 15,000 feet MSL, and

f) Applicable Oxygen requirements are established and complied with Operation Procedures:

1. With the engines running and APU off,

Select Main Air Valve on affected side OPEN and CLOSED,

Confirm airflow is present with valve OPEN, associated indicator illuminates while valve is OPEN, and that flow stops when valve is closed.

2. With engines running, select AUX HEAT and confirm that airflow is present.

3. Conduct flight at or below FL 250.

NOTE: Special attention should be given to planning low attitude flights.

UNCONTROLLED IF PRINTED

(30)

Reference Table 1. Configure Aircraft for Unpressurized Flight.

10-16. Pressure Regulating Shutoff

Valve (PRSOV) C 1 0 (O) May be inoperative provided:

a) Ram Air Valve is verified operative prior to each departure,

b) DUMP VLV / VENT VALVE is selected OPEN,

c) RH Main Air Valve remains CLOSED, d) Flight is conducted in an unpressurized

configuration,

e) Aircraft is operated at or below 15,000 feet MSL, and

f) Applicable Oxygen requirements are established and complied with Operation Procedures:

20-1. Cabin Recirculating Fan C 1 0 May be inoperative 20-2. Flight Deck Heat Valve/Auxiliary

Heating Valve C 1 0 (O) May be inoperative closed provided flight is conducted at or below FL 250

Operate at or below FL 250.

NOTE: Special attention should be given to planning low altitude flights 20-3. Flight Deck Recirculating Fan

(s) C 2 0 May be inoperative

20-4. Mixing Valves

(TFE-731 Engine Only) C C

2

2 1

0

One may be inoperative provided affected Main Air Valve is operated LP ON only

a) Ram Air and Dump/Vent Valves are verified operative before the first flight of the day, b) DUMP VLV / VENT VALVE is selected

OPEN,

30-1. Cabin Altitude Warning Light /

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

a) Cabin altimeter is operative, and

b) Cabin altitude aural warning is operative

UNCONTROLLED IF PRINTED

(31)

C 1 0 (O) May be inoperative provided aircraft is Operated at or below 10,000 feet MSL

1. Confirm that cabin altimeter is operative, and

2. Confirm that cabin altitude aural warning is operative.

Operate at or below 10,000 feet MSL

NOTE: Special attention should be given to planning low altitude flights.

30-2. Cabin Altitude Aural Warning C

C 1

1 0

0

a) Cabin altimeter is operative, and

b) Cabin Altitude Warning Annunciator / light is operative

(O) May be inoperative provided aircraft is operated at or below 10,000 feet MSL

1. Confirm that cabin altimeter is operative, and

2. Confirm that cabin altitude warning annunciator light is operative.

Operate at or below 10,000 feet MSL

NOTE: Special attention should be given to planning low altitude flights.

30-3. Automatic Cabin Pressure Controller / DCPS AUTO Mode C

C 1

1 0

0

a) Manual pressure control system / DCPS Manual Mode is operative, and

b) Cabin altitude, Differential Pressure and Cabin Rate of Climb indicators and operative

a) Ram Air and Dump/vent Valves are verified operative before the first flight of the day, b) DUMP VLV / VENT VALVE is selected

OPEN,

1. Confirm manual pressurization control is operative with cabin door closed and either engine or APU air ON:

UNCONTROLLED IF PRINTED

(32)

Select PRESSN OVRD on roof panel.

Select Cabin Alt Control knob fully counter clockwise.

Select Pressurization Control to GROUND TEST position.

Operate Manual Cabin Altitude Control knob to increase and decrease cabin pressure.

2. Confirm normal operation of cabin altitude, differential pressure, and cabin rate of climb indications.

30-4. Fan Operated Venturi

(excludes Digital Cabin Pressurization System)

C 1 0 (O) May be inoperative provided:

a) Dump valve is verified operative, b) DUMP VLV is selected OPEN for all

ground operations, and

c) DUMP VLV is selected OPEN for Takeoff and Landing

WARNING: DO not open the Main Entry Door before the aircraft cabin is depressurized.

Confirm cabin is depressurized before Main Entry Door is opened by either opening Cockpit C-Panel or selecting DUMP VLV fully OPEN.

30-5. Outflow / Safety Valves C 2 0 (O) May be inoperative provided:

configuration,

30-6. Cabin Pressure Instruments (Triple Indicator or Separate Indicators)

1) Cabin Altitude Indicator C

C 1

1 0

0

a) Cabin Differential Pressure Indicator is operative

b) Cabin Rate of Climb Indicator is operative, c) A chart is provided to the flight crew to and

convert cabin differential pressure to cabin altitude

a) Ram Air and Dump/Vent Valves are verified operative before the first flight of the day, b) DUMP VLV /VENT VALVE is selected OPEN, c) Flight is conducted in an unpressurized

configuration,

UNCONTROLLED IF PRINTED

(33)

2) Cabin Differential Pressure Indicator

3) Cabin Rate of Climb Indicator

C

C 1

1

1 0

0

e) Applicable Oxygen requirements are established and complied with

a) Cabin Altitude Indicator is operative, b) Cabin Rate of Climb Indicator is operative, c) A chart is provided to the flight crew to and

convert cabin altitude to cabin differential pressure

configuration,

e) Applicable Oxygen requirements are established and complied with.

(O) May be inoperative provided all other cabin pressure instruments and functions of the pressurization system are operative.

a) Ram air and Dump/Vent Valves are verified operative before the first flight of the day, b) DUMP VLV / VENT VALVE is selected OPEN, c) Flight is conducted in an unpressurized

configuration,

Reference Table 2 Aircraft Altitude Versus Cabin Altitude.

Operation Procedures (1) :

1. Confirm Cabin Differential Pressure Indicator is operative.

2. Confirm Cabin Rate of Climb Indicator is operative, and

UNCONTROLLED IF PRINTED

(34)

3. Use a chart to convert cabin differential pressure to cabin altitude.

Operation Procedures :

Reference Table 1. Configure Aircraft for Unpressurized Flight.

Reference Table 2 Aircraft Altitude Versus Cabin Altitude.

Operation Procedures (2):

1. Confirm Cabin Differential Pressure Indicator is operative.

2. Confirm Cabin Rate of Climb Indicator is operative, and

3. Use a chart to convert cabin altitude to cabin differential pressure.

Operation Procedures (3):

Confirm all remaining functions and instrument of the cabin pressurization system instrument are operative.

30-7. Absolute Pressure Regulators (excludes Digital Cabin Pressurization System)

C 2 0 (O) May be inoperative provided:

a) Ram Air and Dump Valves are verified operative before the first flight of the day, b) DUMP VLV is selected OPEN,

e) Applicable Oxygen requirements are established and complied with Operation Procedures :

30-8. Air Jet Pump C 1 0 (O) May be inoperative provided:

a) Ram Air and Dump/Vent Valves are verified operative before the first flight of the day,

UNCONTROLLED IF PRINTED

(35)

60-1. Temperature Control System 1) Automatic

2) Manual

C

C 1

1 0

0

(O) May be inoperative provided the manual control system is operative

(O) May be inoperative provided the automatic control system is operative.

With engine running, confirm that conditioned air temperature responds to manual temperature control changes.

With engine running, confirm that conditioned air temperature responds to manual temperature control changes.

60-2. Cabin Temperature Indicator C 1 0 May be inoperative 60-3. Cabin Duct Temperature

Indicator C 1 0 May be inoperative

60-4. Low Limit Temp Control Valve C 1 0 (O) May be inoperative provided:

60-5. Cabin / VIP Temperature

Control Switch D 1 0 (O) May be inoperative provided temperature control system is operative from the cockpit Operation Procedures :

With engine running, confirm that conditioned air temperature responds to temperature responds control change.

60-7. Cabin Temperature Control

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

b) DUMP VLV / VENT VALVE is selected

UNCONTROLLED IF PRINTED

(36)

OPEN,

UNCONTROLLED IF PRINTED

(37)

Remarks or Exceptions

Sequence Number and System

10-1. Autopilot System(s) B 1 0 May be inoperative provide en-route operations and/or approach minimums do not require autopilot use.

Note 1: Any operative autopilot mode may be used

Note 2: RVSM is not authorized Operations Procedures:

Plan flight to ensure that:

1. Operations do not require dual autopilot use Operations Procedures:

Plan flight to ensure that:

1. Enroute operations do not require use of autopilot.

2. Approach minimums do not require use of autopilot.

NOTE 1: Any operative autopilot mode may be used

NOTE 2 : RVSM is not authorized 10-2. Autopilot Control Yoke

Disengage Switches C

B 2

2 1

0

(O) One may be inoperative provided:

a) Autopilot is not used below 1,500 feet AGL, and

b) Approach minimums do not require the use of the autopilot

May be inoperative provide:

a) Autopilot is not used, and b) Enroute operations and / or approach minimums do not require autopilot use

NOTE: RVSM is not authorized Operations Procedures:

Disengage autopilot at or above initial approach altitude.

10-4. Yaw Damper / Autopilot Disconnect Switch on Autopilot Controller Panel

C 1 0 May be inoperative provided both Autopilot Control Yoke Disengage Switches are operative

UNCONTROLLED IF PRINTED

(38)

10-6. Go Around (GA) Switches C

C 2

2 1

0

One may be inoperative provided approach minimums do not require its use

a) Autopilot is not used for approach below 500 feet AGL, and

b) Alternate procedures are established and used

Operations Procedures:

1. Disengage autopilot at or above 500 feet AGL

2. Prior to each departure, review missed approach procedures 3. Select 12⁰ pitch when a go-around is required.

10-7. Control Yoke Pitch / Roll (Collins APS-85, Equipped Aircraft Only)

C 2 1 (O) One may be inoperative provided Autopilot Controller is operative

Prior to each flight, confirm normal operation of the autopilot controller.

20-1. Yaw Damper System B 1 0 (O) May be inoperative provided:

a) Yaw Damper is not used, b) Autopilot is not used, and

c) Rudder Pedals have normal freedom of movement

NOTE: RVSM is not authorized Operations Procedures:

1. Do not use Yaw Damper or Autopilot 2. Confirm Rudder Pedal movement is free 20-4. Autopilot Trim Annunciators

(Collins APS-85 Equipped Aircraft Only)

B 2 0 (O) May be inoperative provided:

a) Autopilot is not used, and

b) Enroute operations and/or approach minimums do not require autopilot use NOTE: RVSM is not authorized

20-7. Guidance Controller (Honeywell SPZ-8000 and Collins APS-85 and Collins Proline 21 Equipped Aircraft)

B 1 0 (O) May be inoperative provided:

a) Autopilot is considered inoperative, b) Enroute operations and/or approach

minimums do not require

autopilot/guidance controller use, and c) 0.73 IMN is not exceeded unless Mach Trim

is operative

NOTE 1: Autopilot and yaw damper will not be available

UNCONTROLLED IF PRINTED

(39)

NOTE 2: RVSM is not authorized

1. Plan flight to ensure that:

2. 0.73 IMN limitation is not exceeded unless Mach Trim is operative NOTE: Autopilot and yaw damper will not be available.

20-9. Mode Select Panel B 1 0 May be inoperative provided:

a) Autopilot is not used, and

b) Enroute operations and/or approach minimums do not require autopilot use

NOTE: RVSM is not authorized

UNCONTROLLED IF PRINTED

(40)

Remarks or Exceptions

Sequence Number and System 05-1. Radio management Units

(RMU`S) / Radio Tuning Units (RTU`s)

C 2 1 (O) One may be inoperative provided:

a) Inoperative Unit is not powered by an Emergency Bus, or equivalent, and is not required to accomplish Emergency Procedures,

b) Remaining RMU/RTU operates normally, and

c) Alternate procedures are established and used

Operations Procedure:

1. Confirm that inoperative RMU is not powered by PE Bus 2. Confirm Operative RMU/RTU functionality.

3. Crew will established and coordinate using alternative procedures.

10-1. Communications System

(VHF, UHF) D 2 1 Any in excess of those require by CASR may be inoperative provided they are not powered by the Emergency AC Bus (XE), or Emergency DC Bus (PE), and are not required for emergency procedures

10-2. Audio Control panels C 2 2 (O) Any in excess of those required at pilot and copilot`s seat positions may be inoperative provided alternate procedures are established and used

1. Place INOP Placard on r adjacent to affected panel (s).

2. Coordinate with affected user (s) for procedures to be used.

10-4. High Frequency (HF)

Communication System D 1 0 (O) Except for RNP and RVSM Operations may be inoperative provided the route to be flown do not require its use.

1. Requirement for communication systems must be determined by each operator and appropriate procedures established to be used with inoperative items, if required appropriate regulations.

2. For operations that require two long range communications systems with one HF communication system operating ensure SATCOM voice or data link is available over the intended route of flight.

20-1. Selective Call System (SELCAL)

1. Channels

C

D 1

1 0

0

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

May be inoperative provided procedures do not require its use

UNCONTROLLED IF PRINTED

(41)

C

D 2

2 0

0

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

Operation Procedure:

30-1. Passenger Address System 1. Passenger Configuration

2. Cargo Configuration

C

D 1

1 0

0

a) Passenger Address System is not required by CASR, and

b) Alternate normal and emergency

procedures, and/or operating restrictions are established and used

1. Verbally brief passengers and cabin crew in the event that normal or emergency procedures dictate such action.

2. Confirm that Flight Deck/Cabin interphone system is operative (if Installed).

30-3. Prerecording Passenger

Announcement System C

D 1

1 0

0

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

not require its use Operations Procedure:

Verbally brief passengers and cabin crew

30-4. Flight Deck Speakers C 2 0 May be inoperative provided:

a) Procedures do not require their use, and b) Headsets are installed and operative 30-5. Emergency locator transmitter

(ELT)

1. Fixed ELTs A 1 0 May be inoperative or missing provided repairs are made within 90 days

UNCONTROLLED IF PRINTED

(42)

40-1. Crewmember Interphone System

1. Flight Deck to Ground

Function C 1 0 (O) May be inoperative provided alternate procedures are established and used Operations Procedure:

Brief crew members and ground personnel on hand signals to be used.

50-1. Headsets

(Except Microphone) C 3 1 One may be inoperative at either pilot’s station provided speaker system is operative

50-2. Handheld Microphone C 2 1 One may be inoperative at either pilot`s station provided associated headset with boom

microphone is operative

50-3. Boom Microphones

(Including Headset Microphone) A 3 0 May be inoperative provided:

a) Associated Hand Microphone is installed and operative, and

b) Repairs are made within three flight days

50-4. Glare shield Microphone Key

Button(s) C 2 0 (O) May be inoperative provided Handheld Microphone on affected side is operative.

Utilize handled microphones or yoke microphone switches.

50-5. Flight Deck Pilot-to-Pilot

Interphone System A 1 0 (O) May be inoperative provide:

a) Alternate pilot-to-pilot communication procedures are established and used, and b) Repairs are made within three flight days

Use hand signals and/or direct voice communication.

UNCONTROLLED IF PRINTED

(43)

70-1. Cockpit Voice Recorder (Aircraft without FDR)

1. Independent Power Source A

C 1

1 0

0

May be inoperative provided repairs are made within three flight days

UNCONTROLLED IF PRINTED

(44)

Remarks or Exceptions

Sequence Number and System 20-1. AC Main Inverters

(Only Aircraft Equipped with Standby Inverter)

C 2 1 (O) One may be inoperative provided:

a) Standby inverter is verified operative before each departure,

b) For aircraft with 2 AOA Vanes and SSU systems, both Engine Driven AC Alternators are operative, and

c) Flight is not conducted in known or forecast icing conditions.

1. Perform inverter check prior to each departure.

2. For aircraft with two (2) AOA Vanes and SSU systems, verify both engine driven AC alternators are operative.

3. Plan each flight to avoid known or forecast icing conditions along entire route including alternate destination.

20-2. Standby Inverter (Proline 21 Only)

B 1 0 May be inoperative provided both main inverters are operative.

20-3. Inverter Fail Lights /

Annunciators C 2 0 (O) May be inoperative provided:

a) Auto-changeover system is operative, b) Both main inverters are operative, and c) AC voltmeter is installed and operative

1. Confirm both inverters are operative.

2. Confirm AC powered equipment operates with either inverter selected OFF.

3. Confirm AC voltmeter indicates correct voltage.

20-4. Standby Inverter “ON” Light /

Annunciator C 1 0 (O) May be inoperative provided standby inverter is verified operative before each departure.

Prior to each departure:

1. Select STBY INV to ARM.

2. Select INV 1 and INV 2 to STOP.

3. Confirm normal standby inverter voltage on XE Buss.

20-5. AC Voltmeter C 1 0 (O) May be inoperative provided:

a) All Inverters are operative, and

b) All AC System Annunciators are operative Operation Procedures:

1. Prior to each departure, confirm INV and buss FAIL annunciators illuminate with all inverters OFF.