TRANSPORT CANADA MMEL SUPPLEMENT REVISION 04 EMB-120 BRASILIA MASTER MINIMUM EQUIPMENT LIST

Transcription

1 MMEL SUPPLEMENT REVISION 04 TO MASTER MINIMUM EQUIPMENT LIST W. R. Jupp Chief Aircraft Certification Flight Test for Minister of Transport Jan. 06, 2004 Revision: 04

2 MMEL SUPPLEMENT REVISION 04 TO MASTER MINIMUM EQUIPMENT LIST Original signed by: W. R. Jupp Chief Aircraft Certification Flight Test for Minister of Transport Jan. 06, 2004 Revision: 04

3 PAGE: I REVISION: 04 JAN. 06, 2004 List of Effective Pages Title Page List of Effective Pages I Revision 04 Jan. 06, 2004 II Revision 04 Jan. 06, 2004 Log of Revisions III Revision 04 Jan. 06, 2004 Reasons for Changes IV Revision 04 Jan. 06, 2004 V Revision 04 Jan. 06, 2004 VI Revision 04 Jan. 06, 2004 VII Revision 04 Jan. 06, 2004 Introduction VIII Revision 04 Jan. 06, 2004 Pages 21-1 Revision 04 Jan. 06, Revision 04 Jan. 06, Revision 04 Jan. 06, Revision 04 Jan. 06, Revision 04 Jan. 06, Revision 04 Jan. 06, Revision 04 Jan. 06, Revision 04 Jan. 06, Revision 04 Jan. 06, Revision 04 Jan. 06, Revision 04 Jan. 06, Revision 04 Jan. 06, Revision 04 Jan. 06, Revision 04 Jan. 06, Revision 04 Jan. 06, Revision 04 Jan. 06, Revision 04 Jan. 06, Revision 04 Jan. 06, 2004 List of Effective Pages (cont d)

4 PAGE: II REVISION: 04 JAN. 06, 2004 Pages 31-1 Revision 04 Jan. 06, Revision 04 Jan. 06, Revision 04 Jan. 06, Revision 04 Jan. 06, Revision 04 Jan. 06, Revision 04 Jan. 06, Revision 04 Jan. 06, Revision 04 Jan. 06, Revision 04 Jan. 06, Revision 04 Jan. 06, Revision 04 Jan. 06, Revision 04 Jan. 06, Revision 04 Jan. 06, Revision 04 Jan. 06, Revision 04 Jan. 06, Revision 04 Jan. 06, Revision 04 Jan. 06, Revision 04 Jan. 06, 2004

5 PAGE: III REVISION: 04 JAN. 06, 2004 Log of Revisions Revision No. Date Page Number Initials Original Jan. 5, 1990 All 01 May 17, 1991 All 02 Feb. 20, 1992 i, ii, L-1 L-2, L-3, L-4, L-5, L-6, 23-1, 27-1, 33-3, 34-1, 34-3, 77-1, 77-2, AMI-1,2 03 Sept. 06, 1996 All 04 Jan. 06, 2004 All

6 PAGE: IV REVISION: 04 JAN. 06, 2004 Reasons for Changes General Review of CTA Approved MMEL:Rev. 19 Jul. 31, Pressurization Triple Indicator new item with relief and repair category per Guidance Book (GB) items 21.2, 21.4 and Cockpit Door Blow Out Shear Plate made mandatory based on CAR Air Conditioning Packs new item with repair category per GB item Electrical Trim System new item with relief and repair category per GB item Autopilot/Flight Director System new item with relief and repair category per GB item Autopilot Disconnect Switches new item with relief and repair category per GB item Yaw Damper System new item with relief and repair category per GB item Autopilot Disconnected Warning System new item with relief and repair category per GB item VHF Communications Transmitters/Receivers new item with relief per GB item Selective Call System (SELCAL) new item with relief per GB item ARINC Communications Addressing and Reporting System (ACARS) new item wirth relief per GB item Passenger Address System revised item with format changes only Pre Recorded Announcement (Passenger Briefing System) new item with relief per GB item Boom Sets (Microphones and Headsets) revised item with relief per GB item Flight Deck Speakers revised item with new provisos per GB item Service Interphone System Cockpit to Cabin and Cabin to Cockpit revised item with relief per GB item Integrated Audio System item deleted in Rev. 04. CTA MMEL is now applicable.

7 PAGE: V REVISION: 04 JAN. 06, 2004 Reasons for Changes (cont d) Crew Member Shoulder Harness (Flight Deck and Cabin) reinstated item with mandatory requirement for clarification purposes Crew Member Seat Adjustment Mechanism new item with relief per GB item 25.10Passenger Seats (includes seat backexterior Lavatory Door Ashtray Flight Crew Power Seat Adjustment System new item with relief per GB item Cabin Attendant s Seat new item made mandatory per GB item Overhead Storage Bin(s)/ Cabin And Galley Storage Compartment/Closets new item with relief per GB item Passenger Seats (includes seat back) revised item adding relief for underseat baggage restraint bar Exterior Lavatory Door Ashtray new item with relief per GB item Lavatory NO SMOKING Placard new item with relief per GB item Fasten Seat Belt While Seated Signs or Placard new item with relief pe GB item Emergency Locator Transmitter revised item with repair category per CAR Passenger Convenience Items new item with added NOTES per GB item Observer Seat (including associated equipment) revised item with revised relief per GB item Flight Attendant Flashlights/Flashlight Holders new item with relief per GB Item Megaphone new item with relief per GB item First Aid Kit new item with relief per GB item Lavatory Smoke Detection System revised item with relief per GB item Lavatory Fire Extinguisher System revised item with relief per GB item Portable Fire Extinguishers reinstated item to provide repair category per GB item Rudder Pedal Adjustment new item with relief per GB item Pitch Trim Takeoff Aural Warning reinstated item for clarification.

8 PAGE: VI REVISION: 04 JAN. 06, 2004 Reasons for Changes (cont d) Flap Warning Indicating Lights (ASYMMETRY, CONTROL FAULT, DISAGREEMENT) revised item with mandatory proviso for clarification Flap Annunciator Light Bars revised item with mandatory proviso for clarification Pitot Static Tubes INOP Lights new item with relief per GB item AOA Sensor Heating Systems revised item with mandatory proviso for clarification Ice Detection System deleted item replaced by item in CTA MMEL Clocks new item with relief per GB item Flight Data Recorder item reinstated with relief for paramenters per GB item Flight Compartment and Instrument Lighting System revised item with relief per GB item Passenger Notice System (No Smoking/Fasten Seat Belt/Return to Cabin Signs) revised item with relief per GB item Altitude Alert System revised item with repair category per GB item Air Data Sensor deleted item in Rev. 04. CTA MMEL is now applicable Attitude and Heading Reference Systems (AHRS) reinstated item to provide relief for compass magnetic and free gyro modes per GB item EADI/ADI revised item with mandatory proviso for clarification EHSI/HSI revised item with mandatory proviso for clarification Standby Attitude Indicator reinstated item with proviso per GB item Standby Magnetic Compass revised item with relief for TSO d GPS per GB item Ground Proximity Warning System revised item with relief and repair category per GB item Radio Altimeters new item with repair category per GB item ADF new item with cross reference NOTE added VOR/ILS Systems new item with cross reference NOTE added Marker Beacon System new item with relief per GB item Long Range Navigation Systems new item with relief for Data Base per GB item 34.6.

9 PAGE: VII REVISION: 04 JAN. 06, 2004 Reasons for Changes (cont d) Crew Oxygen System new item for relief of Observer Seat oxygen Lavatory Oxygen new item with relief per GB item Attendants Portable Oxygen Cylinder (and mask) new item with relief per GB item Protective Breathing Equipment new item with relief per GB item Pneumatic Deicing Bleed Shutoff Valves revised item with title change Pneumatic Deicing CLOSED DEICE Lights item deleted in Rev. 04. CTA MMEL is now applicable Lavatory Waste Systems new item with relief per GB item Potable Water Systems new item with relief per GB item Door Warning Indication Lights revised item with mandatory proviso for clarification NP Indicators revised item typo correction NH Indicators revised item with editorial only T6 Indicators revised item with editorial only. AMI-1 Page deleted in Rev. 04.

10 PAGE: VIII REVISION: 04 JAN. 06, 2004 Introduction This Transport Canada MMEL constitutes a mandatory change to the CTA Approved MMEL for the EMB-120 Brasilia. This MMEL must be used in conjunction with the CTA Approved MMEL, Revision No. 19, July 31, 2002 or later applicable revision. The information contained herein supersedes the existing CTA MMEL only for those items listed herein. For items not contained in this supplement, consult the CTA approved MMEL. Operating and/or maintenance procedures referred to in this supplement are the same as those supporting the CTA MMEL unless otherwise indicated. Procedures required by the Transport Canada MMEL and not indicated in the CTA Approved MMEL must be provided by the operator. The CTA MMEL has entries where the Remarks and/or Exceptions column states as required by local regulations. Unless such an entry is superseded by an item in this, all references should be made to the applicable Canadian regulation. This MMEL uses the standard four column format as referenced in the Transport Canada MMEL/MEL Policy and Procedures Manual (TP 9155E). The same definitions and symbols as the FAA MMEL are also used. Items which have no MMEL relief (i.e. relief withdrawn) are not categorized. Comments and inquiries should be directed to: Transport Canada Director of Aircraft Certification Place de Ville, Tower C 330 Sparks Street 3rd Floor Ottawa, Ontario K1A 0N8

11 Date: Jan. 06, of 2 21 AIR CONDITIONING Pressurization Triple Indicator 1) Cabin Differential Pressure Indicator C 1 0 (M)(O) May be inoperative provided: a) Cabin altitude indicator operates normally, and b) A chart is provided to convert cabin altitude to differential pressure. D 1 0 (O) May be inoperative provided flight is conducted in an unpressurized configuration. 2) Cabin Altitude Indicator C 1 0 (M)(O) May be inoperative provided: a) Cabin differential pressure indicator operates normally, and b) A chart is provided to convert cabin differential pressure to cabin altitude. D 1 0 (O) May be inoperative provided flight is conducted in an unpressurized configuration. 3) Cabin Rate of Change Indicator C 1 0 (M) May be inoperative provided all other instruments and functions of the pressurization system operate normally. D 1 0 (O) May be inoperative provided flight is conducted in an unpressurized configuration.

12 Date: Jan. 06, of 2 21 AIR CONDITIONING Cockpit Door Blow Out Shear Plate 2 2 Must be operative Air Conditioning Packs C 2 1 No change from CTA MMEL D 2 0 No change from CTA MMEL

13 Date: Jan. 06, of 2 22 AUTO FLIGHT Electrical Trim System 1) Autopilot Computer Trim Channel C 2 1 (O) One may be inoperastive proc=vided: a) Associated autopilot is not used, and b) Manual pitch trim operates normally. B 2 0 (O) Both may be inoperative provided: a) Associated autopilot is not used, and b) Manual pitch trim operates normally. 2) Pitch Trim Switches C 2 0 (O) May be inoperative provided Manual pitch trim operates normally Autopilot/Flight Director System C 2 1 One may be inoperative provided approach minimums do not require its use. B 2 0 Both may be inoperative provided approach minimums do not require its use Autopilot Disconnect Switches C 2 1 One may be inoperative provided: a) The autopilot is not utilized at less than the initial approach altitude, and b) The pilot flying has the operative disconnect. B 2 0 Both may be inoperative provided the autopilot is not used.

14 Date: Jan. 06, of 2 22 AUTO FLIGHT Yaw Damper System C 2 1 One may be inoperative provided: a) Inoperative yaw damper remains disengaged, and b) Autopilot associated with operative yaw damper operates normally. B 2 0 Both may be inoperative provided: a) Yaw damper remains disengaged, and b) Approach minimums do not require their use.. NOTE Autopilot will not engage with inoperative yaw dampers Autopilot Disconnected Warning System B 1 0 May be inoperative provided autopilot is not used.

15 Date: Jan. 06, of 4 23 COMMUNICATIONS VHF Communications Transmitters/Receivers 1) VHF COM Control Panel (CTL-22) D - 2 Any in excess of those required by regulation and not powered by a standby or emergency bus and not required for emergency procedures may be inoperative. VHF No. 2 may be inoperative provided HF is installed and operative. No change from CTA MMEL Selective Call System (SELCAL) C 1 0 (O) May be inoperative provided alternate procedures are established and used. D 1 0 May be inoperative provided routine procedures do not require its use ARINC Communications *** Addressing and Reporting System (ACARS) C - 0 NOTE: Any station that operates normally may be used. D - 0 May be inoperative provided routine procedures do not require its use.

16 Date: Jan. 06, of 4 23 COMMUNICATIONS Passenger Address System B 1 0 (O) May be inoperative provided: a) Alternate procedures are established and used; b) Flight deck/cabin interphone, (two way) with associated calls (e.g. chimes) is operative, and c) Megaphone(s) is/are readily available and operative. A 1 0 (O) May be inoperative for non-passenger carrying operations for one flight day provided: a) Ccrew members are the only occupants of the aircraft, and b) Alternate procedures are established and used. 1) All Ccargo Operations D 1 0 May e inoperative provided all crew members are on the flight deck Pre Recorded *** Announcement (Passenger Briefing System) 1) Passenger Configuration C 1 0 (O) May be inoperative provided alternate procedures are established and used. 2) Cargo Configuration D 1 0 May be inoperative provided all crew members are on the flight deck.

17 Date: Jan. 06, of 4 23 COMMUNICATIONS Boom Sets (Microphones and Headsets) 1) Headset Function C - - Headset function may be inoperative on any boom set provided alternate headset is installed, operative and used. If CVR required to record boom microphone 2) Mike Function A - - May be inoperative for three flight days provided:. a) FDR is operative, and b) Hand mike is installed, operative and used. If CVR not required to record boom microphone 3) Mike Function D - 0 May be inoperative provided hand mike is installed, operative and used Flight Deck Speakers C 2 0 May be inoperative provided: a) Procedures are not dependent on their use, b) Headsets are installed and used by each person on flight deck duty, c) All aural alerts, messages and other communication which are normally routed through the flight deck speakers must be audible through the headsets, and d) A spare headset must be readily available for crew use.

18 Date: Jan. 06, of 4 23 COMMUNICATIONS Service Interphone System Cockpit to Cabin and Cabin to Cockpit B - 1 (O) May be inoperative provided: a) An operative flight deck/cabin interphone (two way) is at an operative flight attendant seat, and b) Alternate communications procedures between the affected flight attendant station(s) are established and used. A 1 0 (O) May be inoperative for non-passenger carrying operations for one flight day provided: a) Crew members are the only occupants of the aircraft, and b) Alternate procedures are established and used. 1) All Cargo Operations D 1 0 May be inoperative provided all crew members are on the flight deck. 2) Cockpit to Ground C 1 0 (O) May be inoperative provided alternate procedures are established and used. D 1 0 May be inoperative provided procedures are not dependent on its use Integrated Audio System Deleted in Rev. 04. Refer to CTA MMEL.

19 Date: Jan. 06, of 7 25 EQUIPMENT/ FURNISHINGS Crew Member Shoulder Harness (Flight Deck and Cabin) - - Must be operative for each crew member on duty Crew Member Seat Adjustment Mechanism C - - (M) Vertical and fore/aft adjustment may be inoperative provided the seat is secured in a position to meet individual pilot requirements Flight Crew Power Seat *** Adjustment System D - 0 May be inoperative provided the system is deactivated Cabin Attendant s Seat 1 1 Must be operative Overhead Storage Bin(s)/ Cabin And Galley Storage Compartment/Closets C - - (M) May be inoperative provided: a) Procedures are established to secure compartment CLOSED, or remove the lid/door, b) Compartment is not used for storage of emergency equipment, and c) Affected compartment is not used for storage of any item(s) except for those permanently affixed.

20 Date: Jan. 06, of 7 25 EQUIPMENT/ FURNISHINGS Overhead Storage Bin(s)/ Cabin And Galley Storage Compartment/Closets (cont d) NOTES: 1. If no partitions are installed, the entire overhead stowage compartment is considered one bin. 2. An inoperative lid/door latch renders the door inoperative Passenger Seats (includes seat back) D - - (M) May be inoperative provided: a) It does not block or restrict access to an emergency exit; b) It does not restrict any passenger from access to the main aisle; and, c) The affected seat(s) is not used and is blocked and placarded DO NOT OCCUPY. NOTES: 1. A seat with an inoperative seat belt is considered inoperative. 2. The affected seat(s) may include the seat behind and the adjacent outboard seats. 1) Recline Mechanism D - - (M) May be inoperative provided the seat is secured in the upright position.

21 Date: Jan. 06, of 7 25 EQUIPMENT/ FURNISHINGS Passenger Seats (includes seat back) (cont d) 2) Underseat Baggage Restraining Bars (for seats that are not designated as crew baggage storage areas) C - - (O) May be inoperative or missing provided: a) Baggage is not stowed under associated seat or seat assembly, b) Associated seat or seat assembly is placarded DO NOT STOW BAGGAGE UNDER THIS SEAT, and c) Procedures are established to alert crew members of inoperative or missing restraining bar Exterior Lavatory Door Ashtray B 1 0 May be missing Lavatory NO SMOKING Placard 1 1 Must be operative. NOTE: A temporary placard may be used to dispatch an aircraft to a station where normal placards are available.

22 Date: Jan. 06, of 7 25 EQUIPMENT/ FURNISHINGS Fasten Seat Belt While Seated Signs or Placard C - - One or more signs or placards may be illegible or missing provided a legible sign or placard is readable from each occupied passenger seat Emergency Locator Transmitter A 1 0 As required by regulation Passenger Convenience Items - 0 No change from CTA MMEL NOTE: 1. Exterior lavatory door ash trays are not considered convenience items. 2. Galley equipment restraining devices such as latches, etc. must be serviceable or the compartment must not be used for storage and placarded INOPERATIVE - DO NOT USE. 3. Movie equipment individual screens, if applicable, must be capable of being stowed. 4. Audio or audio-visual entertainment equipment which is used as the sole means of providing safety briefings and demonstrations is not considered a passenger convenience item.

23 Date: Jan. 06, of 7 25 EQUIPMENT/ FURNISHINGS Observer Seat (including associated equipment) B 1 0 May be inoperative provided: a) It is not required to be occupied in an official capacity, and b) The seat is removed, stowed or secured in the retracted position. D 1 0 (M) May be inoperative provided: a). The seat is not required to be occupied in an official capacity for extended periods of time and b) The seat is removed, stowed, or secured in the retracted position Flight Attendant Flashlights/Flashlight Holders 1) Flashlights (O) May be inoperative or missing provided the flight attendant assigned to the associated seat has a flashlight of equivalent characteristics readily available. 2) Holders (M)(O) May be inoperative or missing provided alternate stowage provisions are provided.

24 Date: Jan. 06, of 7 25 EQUIPMENT/ FURNISHINGS Megaphone *** D - - (M)(O) Any in excess of those required by regulations may be inoperative or missing provided: a) The inoperative megaphone is removed from the passenger cabin and its location is placarded INOPERATIVE, or it is removed from the installed location, secured out of sight and the megaphone and its installed location are placarded INOPERATIVE. b) Required distribution is maintained, and c) Procedures are established to alert crew members of inoperative or missing megaphones. 1) All Cargo Operations D -- May be inoperative provided all crew members are on the flight deck.

25 Date: Jan. 06, of 7 25 EQUIPMENT/ FURNISHINGS First Aid Kit (O) Any kit or items contained in the kit in excess of those required by regulations may be incomplete or missing provided: a) Required distribution is maintained, and b) Procedures are established to alert crew members of missing or incomplete kits. 1) FIRST AID KIT SEAL B - - The seal affixed on the exterior of the first aid kit may be missing or broken provided: a) The first aid kit is fully equipped or the kit has a maximum of one missing item, b) The kit includes a list of its contents, c) An inventory is taken on the content of the kit prior to departure, and d) Procedures are established to alert crew members of: 1) The missing or broken seal, and 2) The need to perform an inventory under proviso c).

26 Date: Jan. 06, of 3 26 FIRE PROTECTION Lavatory Smoke Detection System C 1 0 (M)(O) May be inoperative provided: a) Lavatory is not used by passengers for any purpose; b) Lavatory waste receptacle is empty; c) Lavatory door is locked closed and placarded INOPERATIVE DO NOT ENTER,. d) Access to waste receptacle from outside the lavatory must be secured closed and placarded INOPERATIVE - DO NOT USE, and e) Lavatory is used only by crew members, C 1 0 (O) May be inoperative for non passenger carrying operations provided a) Crew members are the only occupants of the aircraft, and b) Occupants have been briefed that the smoke detection system is inoperative. NOTE: The abovementioned provisos are not intended to preclude crew member lavatory inspections which must be detailed in the (O) procedures.

27 Date: Jan. 06, of 3 26 FIRE PROTECTION Lavatory Fire Extinguisher System C 1 0 May be inoperative provided the lavatory smoke detection is operative. C 1 0 May be inoperative provided: a) Lavatory is not used by passengers for any purpose; b) Lavatory waste receptacle is empty; c) Lavatory door is locked closed and placarded INOPERATIVE DO NOT ENTER. d) Access to waste receptacle from outside the lavatory must be secured closed and placarded INOPERATIVE - DO NOT USE, and. e) Lavatory is used only by crew members. C 1 0 May be inoperative for non-passenger carrying operations provided: a) Crew members are the only occupants of the aircraft and b) Occupants have been briefed as to which lavatory fire extinguishing system(s) is/are inoperative. NOTE: The abovementioned provisos are not intended to preclude crew member lavatory inspections which must be detailed in the (O) procedures.

28 Date: Jan. 06, of 3 26 FIRE PROTECTION Portable Fire Extinguishers D - - (M)(O) Any in excess of those required by regulations may be inoperative or missing provided: a) The inoperative fire extinguisher(s) is/are removed from the passenger cabin, flight deck, and/or class E cargo compartment that is accessible to crew members during flight, and its location is placarded INOPERATIVE, or it is removed from the installed location, secured out of sight and the fire extinguisher and its installed location are placarded INOPERATIVE. b) Required distribution is maintained in the passenger compartment on each deck, the flight deck and each class E cargo compartment that is accessible to crew members during flight, as applicable, and c) Procedures are established to alert crew members of missing portable fire extinguishers.

29 Date: Jan. 06, of 1 27 FLIGHT CONTROLS Rudder Pedal Adjustment C - - (M) May be inoperative provided: a) The rudder pedals can be secured in a position which meets individual pilot requirements, and b) Full and unrestricted movement of the rudder and brake pedal deflection is possible at both pilot stations Pitch Trim Takeoff Aural Warning 1 1 Must be operative Flap Position Indicator B 1 0 (O) May be inoperative provided the light bars on the annunciator panel operate normally Flap Warning Indicating Lights (ASYMMETRY, CONTROL FAULT, DISAGREEMENT) 3 3 Must be operative Flap Annunciator Light Bars Must be operative

30 Date: Jan. 06, of 1 29 HYDRAULIC POWER MAIN PUMP LOW PRESS Lights B 2 0 One or both may be inoperative provided the associated pressure indicator operates normally and is monitored during flight.

31 Date: Jan. 06, of 1 30 ICE AND RAIN PROTECTION Leading Edge Failure Indicating Lights C 11 7 (M) or (O) The outboard middle wing indicating lights may be inoperative provided the wing leading edge deicing system is confirmed to operate normally prior to departure in known or forecast icing conditions. NOTE: Crew must visually confirm proper wing deice operation on the affected surfaces while in icing conditions for any inoperative light. B 11 0 Any or all may be inoperative provided airplane is not operated in known or forecast icing conditions Engine Air Inlet Deicing System B 2 1 (O) One may be inoperative provided airplane is not operated in known or forecast icing conditions Pitot Static Tubes INOP Lights AOA Sensor Heating Systems B 3 0 Except for ETOPS beyond 120 minutes, may be inoperative provided: a) No change from CTA MMEL b) No change from CTA MMEL 2 2 Must be operative Ice Detection System Item deleted in Rev. 04 replaced by item 80-2 in CTA MMEL

32 Date: Jan. 06, of 1 31 INSTRUMENTS Clocks C - - Aircraft clock(s) may be inoperative provided a reliable and functioning timepiece is readily available to all flight deck crew members Flight Data Recorder A 1 0 (O) May be inoperative provided: a) Cockpit Voice Recorder is verified operative, and b) Repairs are made within three flight days. 1) Digital FDR Recording Parameters required by regulations. A - - May be inoperative provided: a) Cockpit Voice Recorder is operative, and b) Repairs are made within twenty calendar days. 2) Digital FDR Recording Parameters not required by regulations. May be inoperative provided repairs are made before the completion of the next heavy maintenance visit Aural Warning Unit B 1 1 One channel may be inoperative.

33 Date: Jan. 06, of 1 32 LANDING GEAR Nosewheel Steering System B 1 0 (O)(M) May be inoperative provided: a) System is deactivated; b) Anti-skid system operates normally; and, c) Operations including use of the rolling takeoff technique, are conducted in compliance with the AFM.

34 Date: Jan. 06, of 2 33 LIGHTS Flight Compartment and Instrument Lighting System C - - Individual lights may be inoperative provided remaining lights are: a) Sufficient to clearly illuminate all required instruments, controls and other devices for which it is provided, b) Positioned so that direct rays are shielded from flight crew member s eyes, and c) Lighting configuration and intensity is acceptable to the flight crew. D - - May be inoperative for day operations Passenger Notice System (No Smoking/Fasten Seat Belt/Return to Cabin Signs) C - - (M)(O) Passenger seats, flight attendant seats or lavatories from which a light is not readily legible shall not be occupied and must be blocked and placarded DO NOT OCCUPY. C - - (O) The affected seats or lavatories may be occupied provided: a) The crew call/cabin interphone system including associated chimes and PA system are operative, and b) Procedures are established and used to alert flight attendants and notify passengers when seat belts should be fastened and smoking prohibited.

35 Date: Jan. 06, of 2 33 LIGHTS Passenger Notice System (No Smoking/Fasten Seat Belt/Return to Cabin Signs) (cont d) A - - (O) May be inoperative for one flight day for non-passenger carrying operations provided: a) Crew members are the only occupants of the aircraft, and b) Alternate procedures are established and used. 1) Aural Tone Function C - 0 (O) May be inoperative provided alternate procedures are established and used. 2) Automatic Function C - 0 (O) May be inoperative provided: a) Manual control function is operative, and b) Alternate procedures are established and used. 3) All Cargo Operations D - 0 May be inoperative provided all crew members are on the flight deck.

36 Date: Jan. 06, of 6 34 NAVIGATION Altitude Alert System A 1 0 (O) Except where enroute operations require its use, may be inoperative provided: a) Autopilot altitude hold is operative, and b) Repairs are made within three flight days Air Data Sensors Deleted in Rev. 04. Refer to CTA MMEL 21-1 Attitude and Heading Reference Systems (AHRS) 1) Compass Magnetic Modes 2) Compass Free Gyro modes 2 2 Must be operative B 2 1 (O) One may be inoperative for flights within areas of magnetic reliability provided: a) Compass system operates normally in free gyro mode, and b) Free gyro mode is converted to magnetic mode using operative magnetic heading information. B 2 0 (O) One or both may be inoperative for flights that are entirely within areas of magnetic unreliability provided two stabilized directional gyro systems operate normally and are used in conjunction with free gyro navigation techniques. B 2 0 (O) One or both may be inoperative for flights that are entirely within areas of magnetic reliability (areas south of Northern Domestic Airspace).

37 Date: Jan. 06, of 6 34 NAVIGATION EADI/ADI 2 2 Must be operative EHSI/HSI 2 2 Must be operative Standby Attitude Indicator May be inoperative for day VMC provided the instrument face is covered Standby Magnetic Compass B 1 0 May be inoperative provided any combination of three gyro stabilized compass systems are operating normally. B 1 0 May be inoperative provided: a) Any combination of two gyro or INS(IRU) stabilized compass systems operate normally, and b) Aircraft is operated: (1) With dual independent navigation capability, and (2) Under positive radar control by ATC during the en-route flight phase, or one of the navigation systems is a TSO d GPS which provides track information. C 1 0 (O) May be inoperative for flights that are entirely within areas of magnetic unreliability provided at least two stabilized directional gyro systems are installed, operative and used in conjunction with approved free gyro navigation techniques.

38 Date: Jan. 06, of 6 34 NAVIGATION Ground Proximity Warning System A 1 0 (O) May be inoperative provided: a) Alternate procedures are established and used, and b) Repairs are made within three flight days. 1) Modes 1 to 4 A - 0 (O) May be inoperative provided: a) Alternate procedures are established and used, and b) Repairs are made within three flight days. 2) Test Mode A 1 0 May be inoperative provided: 3) Glideslope Deviation (Mode 5) 4) Advisory Callouts *** 5) Windshear Mode *** a) The GPWS is considered inoperative, and b) Repairs are made within three flight days. B 2 0 One or both may be inoperative. C - 0 (O) May be inoperative provided alternate procedures are established and used. C - 0 (O) May be inoperative provided: a) Alternate procedures are established and used, and b) Windshear Detection and Avoidance System operates normally.

39 Date: Jan. 06, of 6 34 NAVIGATION Ground Proximity Warning System (cont d) 5) Windshear Mode (cont d) *** C - 0 (O) May be inoperative provided: 6) TAWS C - 0 May be inoperative. a) Alternate procedures are established and used, and b) Takeoffs and landings are not conducted in known or forecast windshear conditions Weather Radar System C 1 0 May be inoperative provided forecast or reported weather conditions do not require its use. Stabilization Function B 1 0 May be inoperative provided: a) Antenna sweep is parallel to airplane pitch axis, and b) Antenna tilt operates normally Radio Altimeters C - 0 May be inoperative provided approach minimums or operating procedures are not dependent on its use.

40 Date: Jan. 06, of 6 34 NAVIGATION ADF C - - Any in excess of those required by regulations may be inoperative. NOTE: The operator s MEL must cross reference the VOR/ILS and ADF items to specify a minimum of two systems, adequate for enroute and approach facilities for the planned itinerary, must be operative for dispatch.. 1) ADF Control Panel (CTL- 92) o - - No change from CTA MMEL VOR/ILS Systems C - - Any in excess of those required by regulations may be inoperative. NOTE: The operator s MEL must cross reference the VOR/ILS and ADF items to specify a minimum of two systems, adequate for enroute and approach facilities for the planned itinerary, must be operative for dispatch. 1) NAV Control Panel (CTL-32) No change from CTA MMEL Marker Beacon System 1) If used routinely C - - May be inoperative provided alternate procedures are established and used. 2) If not used routinely D - - May be inoperative provided routine procedures do not require its use.

41 Date: Jan. 06, of 6 34 NAVIGATION Long Range Navigation Systems 1) If used routinely C - - May be inoperative provided alternate procedures are established and used. 2) If not used routinely D - - May be inoperative provided routine procedures do not require its use. 3) GPS Data Base C - - May be out of currency for enroute operations only provided: a) Current Aeronautical Charts are used to verify Navigation Fixes prior to dispatch, b) Procedures are established and used to verify status and suitability of Navigation Facilities used to define route of flight, and c) Approach Navigation Radios are manually tuned and identified.

42 Date: Jan. 06, of 3 35 OXYGEN Crew Oxygen System 1) Observer s Seat Oxygen B/D 1 0 May be inoperative provided it is selected OFF and the seat is not occupied. NOTE: This relief must be checked because there may be designs where shutting off the Observer oxygen disables the supply to one of the crew members Lavatory Oxygen C 1 0 (O) May be inoperative provided: a) The lavatory is not used for any purpose, and b) The lavatory door is locked and placarded INOPERATIVE DO NOT ENTER. (O) May be inoperative provided the aircraft is not operated above FL 250.

43 Date: Jan. 06, of 3 35 OXYGEN Attendants Portable Oxygen Cylinder (and mask) D - - (M)(O) Any in excess of those required by regulation may be inoperative or missing provided: a) Required distribution of operative units is maintained throughout the aircraft, b) The inoperative portable oxygen dispensing unit is removed from the passenger cabin and its location is placarded INOPERATIVE, or it is removed from the installed location, secured out of sight and the portable oxygen dispensing unit and its installed location are placarded INOPERATIVE, and c) Procedures are established to alert crew members of inoperative or missing equipment.

44 Date: Jan. 06, of 3 35 OXYGEN Protective Breathing Equipment D - - (M)(O) Any in excess of those required by regulation may be inoperative or missing provided: a) Required distribution of operative units is maintained throughout the aircraft, b) The inoperative protective breathing equipment unit is removed from the passenger cabin and its location is placarded INOPERATIVE, or it is removed from the installed location, secured out of sight and the protective breathing equipment unit and its installed location are placarded INOPERATIVE, and c) Procedures are established and used to alert crew members of inoperative or missing equipment.

45 Date: Jan. 06, of 1 36 PNEUMATIC Pneumatic Deicing Bleed Shutoff Valves C 2 1 (O) One may be inoperative closed provided flight is not conducted in known or forecast icing conditions Pneumatic Deicing CLOSED DEICE Lights Deleted in Rev. 04 Refer to CTA MMEL Engine Bleed DUCT LEAK Lights C 2 1 (M)(O) One may be inoperative provided: a) Crossbleed valve remains closed; b) Associated engine bleed shutoff valve remains closed; and, c) Aircraft is not operated in known or forecast icing conditions.

46 Date: Jan. 06, of 1 38 WATER/WASTE Potable Water Systems C 1 0 (M)(O) System may be inoperative provided: a) Tank is drained and inspected to ensure no leakage, and b) Procedures are established to deactivate applicable system components to prevent its use or servicing. C - 0 (M)(O) Individual components may be inoperative provided: a) Associated components are deactivated or isolated, and b) Associated system components are verified not to have leaks Lavatory Waste Systems C 1 0 (M)(O) May be inoperative provided: a) Waste is drained and system is inspected for leakage, b) Procedures are established to deactivate system components, c) Lavatory door is locked closed and placarded INOPERATIVE - DO NOT ENTER, NOTE: Any portion of system which operates normally may be used.

47 Date: Jan. 06, of 1 52 DOORS Door Warning Indication Lights 4 4 Must be operative.

48 Date: Jan. 06, of 1 73 ENGINE FUEL AND CONTROL Fuel LOW TEMP Lights B 2 0 (O) One or both may be inoperative provided the associated fuel flow indicator, fuel FILTER and fuel LOW PRESS lights operate normally. C 2 0 (O) One or both may be inoperative provided the OAT is -5 deg C or higher during the flight.

49 Date: Sep. 07, of 1 77 ENGINE INDICATING Torque Indicators C 2 2 The digital counter on each engine may be inoperative NP Indicators C 2 2 The digital counter on each engine may be inoperative NH Indicators 1) PW 118 engines C 2 2 The digital counter on each engine may be inoperative. 2) PW 118A engines C 2 2 Both the digital counter and analogue indicator must be operative NL Indicators B 2 1 (O) For PW-118 engines one may be inoperative provided: a) the TQ, Np, NH and T6 indications on the associated engine operate normally; b) the torque of the affected engine is adjusted equal to the other engine; and, T6 Indicators 1) PW-118 Engines C 2 2 The digital counter on each engine may be inoperative. 2) PW-118A Engines C 2 2 Both the digital counter and analogue indicator must be operative.