DEPARTMENT OF TRANSPORTATION Revision: 6 a Date: 12/18/95 FEDERAL AVIATION ADMINISTRATION WASHINGTON, D.C. M A S T E R M I N I M U M E Q U I P M E N T L I S T DORNIER 228-100/101/200/201/202/212 AIRCRAFT EVALUATION GROUP, MKC-AEG Department of Transportation Federal Aviation Administration 1201 WALNUT SUITE 900 Kansas City, Missouri 64106 Telephone: (816) 426-3946 FAX: (816)426-3084 FEDERAL AVIATION ADMINISTRATION Page: I Revision: 6 a MASTER MINIMUM EQUIPMENT LIST Date: 12/18/95 DORNIER 228-100/101/200/201/202/212 Table of Contents SYSTEM NO. SYSTEM PAGE -- Table of Contents I -- Log of Revisions II -- Control Page III, IV -- Highlights of Change V -- Definitions VI, VII, VIII, IX -- Definitions X, XI, XII, XIII -- Preamble XIV, XV -- Guidelines for (O) & (M) Procedures XVI, XVII, XVIII 21 Air Conditioning 21-1, 2 22 Auto Flight 22-1 23 Communications 23-1, 2, 3 24 Electrical Power 24-1 25 Equipment/Furnishings 25-1, 2, 3 26 Fire Protection 26-1 27 Flight Controls 27-1, 2 28 Fuel 28-1, 2 30 Ice and Rain Protection 30-1, 2 31 Indicating/Recording Systems 31-1 32 Landing Gear 32-1 33 Lights 33-1, 2, 3 34 Navigation 34-1, 2, 3, 4, 5 34 Navigation 34-6, 7, 8 35 Oxygen 35-1 52 Doors 52-1 56 Windows 56-1 61 Propellers 61-1 73 Engine Fuel & Control 73-1 74 Ignition 74-1 77 Engine Indicating 77-1 FEDERAL AVIATION ADMINISTRATION Page: II Revision: 6 a MASTER MINIMUM EQUIPMENT LIST Date: 12/18/95 DORNIER 228-100/101/200/201/202/212 Log of Revisions ---------------------------------------------------------------------- | REV.NO. | DATE | PAGE NUMBERS | INITIALS | ---------------------------------------------------------------------- | ORIGINAL | 07/13/83 | ALL | | | 1 | 01/06/86 | ALL | | | 2 | 11/18/87 | PAGE 52-1 | | | 3 | 02/05/88 | ALL PAGES | | | 4 | 03/10/89 | ALL PAGES | | | 5 | 06/19/89 | HIGHLIGHTS OF REV.,DEFINITIONS | | | 5 | 06/19/89 | PREAMBLE | | | 5a | 04/17/91 | HIGHLIGHTS OF REV.,DEFINITIONS | | | 5a | 04/17/91 | 23-2 | | | 6 | 08/03/93 | HIGHLIGHTS OF REV.,DEFINITIONS | | | 6 | 08/03/93 | GUIDELINES | | | 6 | 08/03/93 | 21-1,21-2,22-1,23-1,23-2 | | | 6 | 08/03/93 | 23-3,24-1,25-1,25-2,25-3 | | | 6 | 08/03/93 | 26-1,27-1,27-2,28-1,28-2 | | | 6 | 08/03/93 | 30-1,30-2,31-1,32-1,33-1 | | | 6 | 08/03/93 | 33-2,33-3,34-1,34-2,34-3 | | | 6 | 08/03/93 | 34-4,34-5,35-1,52-1,56-1 | | | 6 | 08/03/93 | 61-1,73-1,74-1,77-1 | | | 6a | 12/18/95 | HIGHLIGHTS OF REV.,DEFINITIONS | | | 6a | 12/18/95 | GUIDELINES | | | 6a | 12/18/95 | 23-1,23-2,23-3,25-3,26-1 | | | 6a | 12/18/95 | 33-1,33-2,33-3,34-1,34-2 | | | 6a | 12/18/95 | 34-3,34-4,34-5,34-6,34-7 | | | 6a | 12/18/95 | 34-8 | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | ---------------------------------------------------------------------- FEDERAL AVIATION ADMINISTRATION Page: III Revision: 6 a MASTER MINIMUM EQUIPMENT LIST Date: 12/18/95 DORNIER 228-100/101/200/201/202/212 Control Page SYSTEM PAGE REV NO. CURRENT DATE Cover Page - 6 a 12/18/95 Table of Contents I 6 a 12/18/95 Log of Revisions II 6 a 12/18/95 Control Page III 6 a 12/18/95 IV 6 a 12/18/95 Highlights of Change V 6 a 12/18/95 Definitions VI 6 01/31/95 VII 6 01/31/95 VIII 6 01/31/95 IX 6 01/31/95 X 6 01/31/95 XI 6 01/31/95 XII 6 01/31/95 XIII 6 01/31/95 Preamble XIV 2 06/14/89 XV 2 06/14/89 Guidelines for (O) & (M) Procedures XVI 6 a 12/18/95 XVII 6 a 12/18/95 XVIII 6 a 12/18/95 21 21-1 6 08/03/93 21-2 6 08/03/93 22 22-1 6 08/03/93 23 23-1 6 a 12/18/95 23-2 6 a 12/18/95 23-3 6 a 12/18/95 24 24-1 6 08/03/93 25 25-1 6 08/03/93 25-2 6 08/03/93 25-3 6 a 12/18/95 26 26-1 6 a 12/18/95 27 27-1 6 08/03/93 27-2 6 08/03/93 28 28-1 6 a 12/18/95 28-2 6 a 12/18/95 30 30-1 6 08/03/93 30-2 6 08/03/93 31 31-1 6 08/03/93 32 32-1 6 08/03/93 33 33-1 6 a 12/18/95 33-2 6 a 12/18/95 FEDERAL AVIATION ADMINISTRATION Page: IV Revision: 6 a MASTER MINIMUM EQUIPMENT LIST Date: 12/18/95 DORNIER 228-100/101/200/201/202/212 Control Page SYSTEM PAGE REV NO. CURRENT DATE 33-3 6 a 12/18/95 34 34-1 6 a 12/18/95 34-2 6 a 12/18/95 34-3 6 a 12/18/95 34-4 6 a 12/18/95 34-5 6 a 12/18/95 34-6 6 a 12/18/95 34-7 6 a 12/18/95 34-8 6 a 12/18/95 35 35-1 6 08/03/93 52 52-1 6 08/03/93 56 56-1 6 08/03/93 61 61-1 6 08/03/93 73 73-1 6 08/03/93 74 74-1 6 08/03/93 77 77-1 6 08/03/93 FEDERAL AVIATION ADMINISTRATION Page: V Revision: 6 a MASTER MINIMUM EQUIPMENT LIST Date: 12/18/95 DORNIER 228-100/101/200/201/202/212 Highlights of Change Passenger Address System relief revised in accordance with Policy Letter(PL) 9, designated as Global Change(GC) 13. Relief for Boom Microphones revised in accordance with Policy Letter 58, designated as Global Change 14. Relief for First Aid Kits added in accordance with PL-73, designated as GC-17. Relief for Portable Fire Extinguishers revised in accordance with PL-75, designated as GC-19. Relief for Flight Compartment and Instrument Lighting Systems revised in accordance with PL-77, designated as GC-21. Relief for ATC Transponders and Automatic Altitude Reporting Systems revised in accordance with PL-76, designated as GC-20. Relief for TCAS II revised in accordance with PL-32, designated as GC-2. Relief for TCAS I in acordance with PL-9, designated as GC-62. Relief for Ground Proximity Warning System revised in accordance with PL-54, designated as GC-10. Relief for Flight Profile Advisory System(FPAS) added in accordance with PL-74, GC-18. FEDERAL AVIATION ADMINISTRATION Page: VI Revision: 6 MASTER MINIMUM EQUIPMENT LIST Date: 01/31/95 DORNIER 228-100/101/200/201/202/212 Definitions 1. System Definitions. System numbers are based on the Air Transport Association (ATA) Specification Number 100 and items are numbered sequentially. a. "Item" (Column 1) means the equipment, system, component, or function listed in the "Item" column. b. "Number Installed" (Column 2) is the number (quantity) of items normally installed in the aircraft. This number represents the aircraft configuration considered in developing this MMEL. Should the number be a variable (e.g., passenger cabin items) a number is not required. | c. "Number Required for Dispatch" (Column 3) is the minimum number (quantity) of items required for operation provided the conditions specified in Column 4 are met. NOTE: Where the MMEL 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. d. "Remarks or Exceptions" (Column 4) 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. e. A vertical bar (change bar) in the margin indicates a change, addition or deletion in the adjacent text for the current revision of that page only. The change bar is dropped at the next revision of that page. 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 FEDERAL AVIATION ADMINISTRATION Page: VII Revision: 6 MASTER MINIMUM EQUIPMENT LIST Date: 01/31/95 DORNIER 228-100/101/200/201/202/212 Definitions Certificate Data Sheet. 3. "As required by FAR" means that the listed item is subject to certain provisions (restrictive or permissive) expressed in the Federal Aviation Regulations operating rules. The number of items required by the FAR must be operative. When the listed item is not required by FAR it may be inoperative for time specified by repair category. 4. Each inoperative item must be placarded to inform and remind the crewmembers and maintenance personnel of the equipment condition. NOTE: To the extent practical, placards should be located adjacent to the control or indicator for the item affected; however, unless otherwise specified, placard wording and location will be determined by the operator. 5. "-" symbol in Column 2 and/or Column 3 indicates a variable number (quantity) of the item installed. | 6. "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. 7. "ER" 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. | 8. "Federal Aviation Regulations" (FAR) means the applicable portions of the Federal Aviation Act and Federal Aviation Regulations. 9. "Flight Day" means a 24 hour period (from midnight to midnight) either Universal Coordinated Time (UCT) or local time, as established by the operator, during which at least one flight is initiated for the affected aircraft. 10. "Icing Conditions" means an atmospheric environment that may cause ice to form on the aircraft or in the engine(s). 11. Alphabetical symbol in Column 4 indicates a proviso (condition or limitation) that must be complied with for FEDERAL AVIATION ADMINISTRATION Page: VIII Revision: 6 MASTER MINIMUM EQUIPMENT LIST Date: 01/31/95 DORNIER 228-100/101/200/201/202/212 Definitions operation with the listed item inoperative. 12. "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). 13. "Notes:" in Column 4 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. 14. 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). 15. "(M)" symbol 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. 16. "(O)" symbol 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 FEDERAL AVIATION ADMINISTRATION Page: IX Revision: 6 MASTER MINIMUM EQUIPMENT LIST Date: 01/31/95 DORNIER 228-100/101/200/201/202/212 Definitions 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. 17. "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. 18. "Visual Flight Rules" (VFR) is as defined in FAR Part 91. This precludes a pilot from filing an Instrument Flight Rules (IFR) flight plan. 19. "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. 20. "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. 21. "Passenger Convenience Items" means those items related to passenger convenience, comfort or entertainment such as, but not limited to, galley equipment, movie equipment, ash trays, stereo equipment, overhead reading lamps, etc. 22. Repair Intervals: All users of an MEL approved under FAR 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 column of the operator's approved MEL. 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 FEDERAL AVIATION ADMINISTRATION Page: X Revision: 6 MASTER MINIMUM EQUIPMENT LIST Date: 01/31/95 DORNIER 228-100/101/200/201/202/212 Definitions 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. 23. 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. | | a. BOEING (B-757/767, B-747-400, B-777) | | Boeing airplanes equipped with Engine Indicating and Crew | Alerting Systems (EICAS), provide different priority levels of | system messages (WARNING, CAUTION, ADVISORY, STATUS and | MAINTENANCE). Any messages that affects airplane dispatch | status will be displayed at a STATUS message level or higher. | The absence of an EICAS STATUS or higher level (WARNING, | CAUTION, ADVISORY) indicates that the system/component is | operating within its approved operating limits or tolerances. | | System conditions that result only in a maintenance level | message, i.e. no correlation with a higher level EICAS message, | FEDERAL AVIATION ADMINISTRATION Page: XI Revision: 6 MASTER MINIMUM EQUIPMENT LIST Date: 01/31/95 DORNIER 228-100/101/200/201/202/212 Definitions do not affect dispatch and do not require action other than as | addressed within an operators standard maintenance program. | | b. DOUGLAS (MD-11) | | Some Douglas aircraft are equipped with an alerting function | which is a subsystem within the Electronic Instrument System | (EIS). The alerting function provides various levels of system | condition alerts (WARNING, CAUTION, ADVISORY, MAINTENANCE and | STATUS). | | Alerts that affect aircraft dispatch will include WARNING, | CAUTION, STATUS or MAINTENANCE level. MAINTENANCE alerts are | displayed on the status page of the EIS display panel under the | maintenance heading. | | A MAINTENANCE alert on the EIS indicates the presence of a | system fault which can be identified by the Central Fault | Display System (CFDS) interrogation. The systems are designed | to be fault tolerant, however, for any MAINTENANCE alert, the | MEL must be verified for dispatch purposes. | | c. AIRBUS (A-300-600, A-310, A-320/319/321, A-330, A-340 | | Airbus aircraft equipped with Electronic Centralized Aircraft | Monitoring (ECAM) provide different levels of system condition | messages (WARNING, CAUTION, STATUS, and ADVISORY). A-320/319/ | 321, A-330, and A-340 also provide MAINTENANCE status messages. | | Any message that effects airplane dispatchability will normally | be at the WARNING, CAUTION or STATUS level. MAINTENANCE | messages (A-320/319/321, A-330, and A-340 only) are also | indicated on ECAM Status Page below the white Maintenance label.| | A MAINTENANCE status (Class II) message on ECAM indicates the | presence of a system fault which can be identified by CFDS | (A-320/319/321) or CMS (A-330/A-340) interrogation. The systems | are designed to be fault tolerant, however for any MAINTENANCE | status (Class II) message, the A-320/319/321 MEL must be | verified for dispatch capability. For the A-330 and A-340, | MAINTENANCE status messages do not affect dispatch. | d. FOKKER (FK-100) | FEDERAL AVIATION ADMINISTRATION Page: XII Revision: 6 MASTER MINIMUM EQUIPMENT LIST Date: 01/31/95 DORNIER 228-100/101/200/201/202/212 Definitions | Fokker aircraft are equipped with Multi Function Display System | (MFDS) which provides electronic message referring to the | different priority levels of system information (WARNING (red), | CAUTION (amber), AWARENESS (cyan) AND STATUS (white). Any | messages that affects aircraft dispatch will be at the WARNING, | CAUTION or AWARENESS level. In these cases the MEL must be | verified for dispatch capability and maintenance may be | required. | | System conditions that only require maintenance are not | presented on the flight deck. These maintenance | indications/messages may be presented on the Maintenance & Test | Panel (MAP) or the Centralized Fault Display Unit (CFDU) and by | dedicated Built In Test Evaluation (BITE) of systems. | 24. "Administrative control item" means an item listed by the operator in the MEL for tracking and informational purposes. It may be added to an operator's MEL by approval of the Principal Operations Inspector provided no relief is granted, or provided conditions and limitations are contained in an approved document (i.e. Structural Repair Manual, airworthiness directive, etc.). If relief other than that granted by an approved document is sought for an administrative control item, a request must be submitted to the Administrator. If the request results in review and approval by the FOEB, the item becomes an MMEL item rather than an administrative control item. 25. "***" 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. 26. "Excess Items" means those items that have been installed that are redundant to the requirements of the FARs. 27. "Day of Discovery" is the calendar day an equipment/instrument malfunction was recorded in the aircraft FEDERAL AVIATION ADMINISTRATION Page: XIII Revision: 6 MASTER MINIMUM EQUIPMENT LIST Date: 01/31/95 DORNIER 228-100/101/200/201/202/212 Definitions 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." FEDERAL AVIATION ADMINISTRATION Page: XIV Revision: 2 MASTER MINIMUM EQUIPMENT LIST Date: 06/14/89 DORNIER 228-100/101/200/201/202/212 Preamble (Effective 6/14/89) The following is applicable for authorized certificate holders operating under Federal Aviation Regulations (FAR) Parts 121, 125, 129, 135: The FAR 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 requirements is not necessary in the interests of safety under all operating conditions. Experience has shown that with the various levels of redundancy designed into aircraft, operation of every system or installed component may not be necessary when the remaining operative equipment can provide an acceptable level of safety. A Master Minimum Equipment List (MMEL) is developed by the FAA, with participation by the aviation industry, to improve aircraft utilization and thereby provide more convenient and economic air transportation for the public. The FAA approved MMEL includes those items of equipment related to airworthiness and operating regulations and other items of equipment which the Administrator finds may be inoperative and yet maintain an acceptable level of safety by appropriate conditions and limitations; it does not contain obviously required items such as wings, flaps, and rudders. 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 not contained in the MMEL; however, relief for administrative control items must be approved by the Administrator. 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 FAR 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. FEDERAL AVIATION ADMINISTRATION Page: XV Revision: 2 MASTER MINIMUM EQUIPMENT LIST Date: 06/14/89 DORNIER 228-100/101/200/201/202/212 Preamble (Effective 6/14/89) 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 FAR. The item is then either repaired or may be deferred per the MEL or other approved means acceptable to the Administrator 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, an Airworthiness Release, Aircraft Maintenance Record/Logbook entry, or other approved documentation is issued as prescribed by FAR. Such documentation is required prior to operation with any item of equipment inoperative. 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 PREAMBLE, DEFINITIONS, AND THE CONDITIONS AND LIMITATIONS SPECIFIED IN THE MEL IS REQUIRED. FEDERAL AVIATION ADMINISTRATION Page XVI Revision: 6 a MASTER MINIMUM EQUIPMENT LIST Date: 12/18/95 DORNIER 228-100/101/200/201/202/212 Guidelines for (O) & (M) Procedures The FOEB has identified a need for certain procedures, to provide an adequate level of safety, while providing relief for the following items. These procedures must be established by the operator. The following are to help establish these required procedures: 21-1 (M) A maintenance procedure to assure the ram air system is operative and the pressure reducing/shutoff valve is in the closed position. 21-4 (M) A maintenance procedure to assure the ram air system is operative and the pressure reducing/shutoff valve is in the closed position. 21-8 (M) Procedure to secure butterfly valve in the cockpit distributor duct in the open position. 21-12 (M) A procedure to assure the bleed air shutoff valve is in the closed position. 22-1 (M) Procedure to determine that servos do not cause binding of the control cables. 22-2 (M) Procedure to determine that servos do not cause binding of the control cables. 23-2 (O) Procedure must be established to provide normal and emergency operations for the inoperative intercom. 23-3 (O) To specify how passengers will be briefed and to operate within MMEL restrictions. 23-4 (O) Procedure must be established to provide normal and emergency operations for the inoperative intercom. 23-10 (O) Procedure to brief passengers via the Passenger Address System or other alternate means. 25-1 (M) Procedure to assure the locking pins are engaged. 27-4 (O) A procedure to ensure flight is conducted in accordance with no flap performance restrictions. FEDERAL AVIATION ADMINISTRATION Page XVII Revision: 6 a MASTER MINIMUM EQUIPMENT LIST Date: 12/18/95 DORNIER 228-100/101/200/201/202/212 Guidelines for (O) & (M) Procedures 28-1 (O) Reliable means to determine accurate fuel quantity(i.e. sticking the tank or emptying the tank and refueling, using the fuel onloaded as the known quantity). 28-5 (M) Procedure to secure valve is secured in the closed position. 30-7 (M) A maintenance procedure to determine the engine inlet anti-ice valves are in the closed position and the aircraft limitations are adhered to. 31-2 (O) Operational procedure to record elapsed flight time. 31-3 (O) Procedure to record elapsed engine operation time. 32-1 (O)(M) Procedure to assure nose wheel is in the free castor mode and the AFM procedures for operation in the free castor mode are adhered to. 33-12 (O) Procedures to comply with MMEL restrictions. 34-17 & CARGO OPERATIONS-SINGLE PILOT 34-4 (O) Procedure for flight crew to reset Directional Indicator to correct for precession. 34-18.1 (M) Procedure to deactivate and secure the system. 34-18.2 (O) Procedure to ensure TA and RA display is visible to the non-flying pilot and audio functions are operative on flying pilot side. 34-18.3 (O) Procedure to ensure non-flying pilot monitors pilot's display. 34-18.3 (O) Procedure to ensure TA ONLY mode is selected and all TA functions/elements are operative. 34-18.4 (O) Procedure to ensure all RA display/functions are operative. 34-20.1,4,5 (O) Procedure to ensure crew awareness of altitude and aircraft performance. 34-21.1,2,3,4,6 (O) Procedure to ensure crew awareness of altitude and aircraft performance. 56-1 (M) Procedure to assure the MMEL restrictions are adhered to. 77-1 (O) Procedures to assure the flight crews recognize the inoperative status of the ITT/torque limiter and manually set the ITT and torque. FEDERAL AVIATION ADMINISTRATION Page XVIII Revision: 6 a MASTER MINIMUM EQUIPMENT LIST Date: 12/18/95 DORNIER 228-100/101/200/201/202/212 Guidelines for (O) & (M) Procedures ------------------------------------------------------------------------------- | U.S. DEPARTMENT OF TRANSPORTATION | | | | MASTER MINIMUM EQUIPMENT LIST | | FEDERAL AVIATION ADMINISTRATION | | --------------------------------------------------------------------------- | | AIRCRAFT: | REVISION NO: 6 | PAGE: | | | | | | DORNIER 228-100/101/200/201/202/212 | DATE: 08/03/93 | 21-1 | | --------------------------------------------------------------------------- | | 1. | 2. NUMBER INSTALLED | | SYSTEM & | -------------------------------------------- | | SEQUENCE ITEM | | 3. NUMBER REQUIRED FOR DISPATCH | | NUMBERS | | --------------------------------------- | | ------------------------- | | | 4. REMARKS OR EXCEPTIONS | | 21 AIR CONDITIONING | | | | | | | | | | | | | | | 1. Heating System C | 1 | 0 | (M)May be inoperative provided: | | | | | | | | | | a) Pressure reducing and shutoff | | | | | valve is in the closed | | | | | position, and | | | | | | | | | | b) Ram air system is operative. | | | | | | | 2. Heater Ventilating C | 1 | 0 | May be inoperative provided ram | | Fan | | | air system is operative. | | | | | | | 3. Electrical C | 4 | 0 | | | Cabin/Cockpit Heaters | | | | | | | | | | 4. Air Conditioning C | 1 | 0 | (M)May be inoperative provided: | | System | | | | | (air cycle) | | | a) Pressure reducing and shutoff | | | | | valve is in the closed | | | | | position, and | | | | | | | | | | b) Ram air system is operative. | | | | | | | 5. Temperature Mode C | 1 | 0 | May be inoperative provided manual | | Control (automatic) | | | mode is operative. | | | | | | | 6. Temperature Mode C | 1 | 0 | May be inoperative provided | | Control (manual) | | | auto mode is operative. | | | | | | | 7. Individual Air C | - | - | | | Vents | | | | | | | | | | 8. Windshield C | 1 | 0 | (M)May be inoperative provided | | Demisting | | | butterfly valve in the cockpit | | | | | distributor duct is secured open. | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | ------------------------------------------------------------------------------- ------------------------------------------------------------------------------- | U.S. DEPARTMENT OF TRANSPORTATION | | | | MASTER MINIMUM EQUIPMENT LIST | | FEDERAL AVIATION ADMINISTRATION | | --------------------------------------------------------------------------- | | AIRCRAFT: | REVISION NO: 6 | PAGE: | | | | | | DORNIER 228-100/101/200/201/202/212 | DATE: 08/03/93 | 21-2 | | --------------------------------------------------------------------------- | | 1. | 2. NUMBER INSTALLED | | SYSTEM & | -------------------------------------------- | | SEQUENCE ITEM | | 3. NUMBER REQUIRED FOR DISPATCH | | NUMBERS | | --------------------------------------- | | ------------------------- | | | 4. REMARKS OR EXCEPTIONS | | 21 AIR CONDITIONING | | | | | | | | | | | | | | | | | | | | 9. Cabin Temp Caution C | 1 | 0 | May be inoperative provided: | | Light | | | | | | | | a) Pressure reducing and shutoff | | | | | valve is in closed position, | | | | | | | | | | b) Ventilating fans are | | | | | operative, and | | | | | | | | | | c) Ram air system is operative. | | | | | | | 10. Avionics Pedestal C | 1 | 0 | | | Fan | | | | | | | | | | 11. Radio Rack Fan C | 1 | 0 | | | | | | | | 12. Bleed Air Shutoff C | 2 | 0 | (M)May be inoperative provided: | | Valves | | | | | | | | a) Inoperative valve is in the | | | | | closed position, | | | | | | | | | | b) Aircraft is not operated in | | | | | known or forecast icing | | | | | conditions,and | | | | | | | | | | c) Ram air system is operative. | | | | | | | 13. Air Conditioner C | 1 | 0 | | | (freon) | | | | | *** | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | ------------------------------------------------------------------------------- ------------------------------------------------------------------------------- | U.S. DEPARTMENT OF TRANSPORTATION | | | | MASTER MINIMUM EQUIPMENT LIST | | FEDERAL AVIATION ADMINISTRATION | | --------------------------------------------------------------------------- | | AIRCRAFT: | REVISION NO: 6 | PAGE: | | | | | | DORNIER 228-100/101/200/201/202/212 | DATE: 08/03/93 | 22-1 | | --------------------------------------------------------------------------- | | 1. | 2. NUMBER INSTALLED | | SYSTEM & | -------------------------------------------- | | SEQUENCE ITEM | | 3. NUMBER REQUIRED FOR DISPATCH | | NUMBERS | | --------------------------------------- | | ------------------------- | | | 4. REMARKS OR EXCEPTIONS | | 22 AUTO FLIGHT | | | | | | | | | | | | | | | 1. Autopilot C | 1 | 0 | (M)As required by FAR. | | | | | | | 2. Yaw Damper C | 1 | 0 | (M)As required by FAR. | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | ------------------------------------------------------------------------------- ------------------------------------------------------------------------------- | U.S. DEPARTMENT OF TRANSPORTATION | | | | MASTER MINIMUM EQUIPMENT LIST | | FEDERAL AVIATION ADMINISTRATION | | --------------------------------------------------------------------------- | | AIRCRAFT: | REVISION NO: 6 a | PAGE: | | | | | | DORNIER 228-100/101/200/201/202/212 | DATE: 12/18/95 | 23-1 | | --------------------------------------------------------------------------- | | 1. | 2. NUMBER INSTALLED | | SYSTEM & | -------------------------------------------- | | SEQUENCE ITEM | | 3. NUMBER REQUIRED FOR DISPATCH | | NUMBERS | | --------------------------------------- | | ------------------------- | | | 4. REMARKS OR EXCEPTIONS | | 23 COMMUNICATIONS | | | | | | | | | | | | | | | 1. Communications C | - | - | As required by FAR. | | Equipment (VHF,HF,UHF) | | | | | | | | | | 2. Audio Amplifier C | 2 | 0 | (O)May be inoperative provided: | | | | | | | | | | a) Two operative headsets are | | | | | available to the flight crew, | | | | | and | | | | | | | | | | b) System 1 must be operative | | | | | for single pilot operation. | | | | | | | 3. Passenger Address | | | | | System | | | | | | | | | | | | 1) Passenger B | 1 | 0 | (O)May be inoperative provided | | | Configuration | | | alternate, normal, and emergency | | | | | | procedures, and/or operating | | | | | | restrictions are established and | | | | | | used. | | | | | | | | 2) Cargo D | 1 | 0 | | | | Configuration | | | | | | | | | | | 4. Audio Selector and C | 2 | 1 | (O)Right side may be inoperative | | Intercom Unit | | | provided: | | | | | | | | | | a) Two operative headsets are | | | | | available to the flight crew, | | | | | and | | | | | | | | | | b) System 1 must be operative | | | | | for single pilot operation. | | | | | | | | | | | | 5. Cockpit Speaker C | 1 | 0 | May be inoperative provided | | | | | two operative headsets are | | | | | available to the flight crew. | | | | | | | | | | | ------------------------------------------------------------------------------- ------------------------------------------------------------------------------- | U.S. DEPARTMENT OF TRANSPORTATION | | | | MASTER MINIMUM EQUIPMENT LIST | | FEDERAL AVIATION ADMINISTRATION | | --------------------------------------------------------------------------- | | AIRCRAFT: | REVISION NO: 6 a | PAGE: | | | | | | DORNIER 228-100/101/200/201/202/212 | DATE: 12/18/95 | 23-2 | | --------------------------------------------------------------------------- | | 1. | 2. NUMBER INSTALLED | | SYSTEM & | -------------------------------------------- | | SEQUENCE ITEM | | 3. NUMBER REQUIRED FOR DISPATCH | | NUMBERS | | --------------------------------------- | | ------------------------- | | | 4. REMARKS OR EXCEPTIONS | | 23 COMMUNICATIONS | | | | | | | | | | | | | | | 6. Avionics Master C | 1 | 0 | May be inoperative provided: | | Switch | | | | | | | | a) Avionics master circuit breaker | | | | | is pulled, and | | | | | | | | | | b) Avionics master switch is | | | | | in the ON position. | | | | | | | 7. Ground Clearance C | 1 | 0 | | | Switch | | | | | | | | | | 8. Cockpit Voice A | 1 | 0 | May be inoperative provided the | | Recorder(CVR) | | | Flight Data Recorder is operative | | System | | | and repairs are made within three | | (Flight Data Recorder | | | flight days. | | Required by FAR's) | | | | | | | | | | | | | OR | | | | | | | Cockpit Voice A | 1 | 0 | May be inoperative provided | | Recorder(CVR) | | | repairs are made within three | | System | | | flight days. | | (Flight Data Recorder | | | | | Not Required By FAR's) | | | | | | | | | | 9. Boom Microphones | | | | | | (If FDR Required by FAR) | | | | | | | | | | | 1) Cockpit Voice A | - | 0 | May be inoperative provided: | | | Recorder Equipped | | | | | to Record Boom | | | a) Flight Data Recorder(FDR) | | | Microphones per | | | operates normally, and | | | FAR 135.151(d). | | | b) Repairs are made within | | | | | | three flight days. | | | | | | | | | 2) Cockpit Voice D | - | 0 | | | | Recorder not | | | | | | Equipped to Record | | | | | | Boom Microphone | | | | | | | | | | ------------------------------------------------------------------------------- ------------------------------------------------------------------------------- | U.S. DEPARTMENT OF TRANSPORTATION | | | | MASTER MINIMUM EQUIPMENT LIST | | FEDERAL AVIATION ADMINISTRATION | | --------------------------------------------------------------------------- | | AIRCRAFT: | REVISION NO: 6 a | PAGE: | | | | | | DORNIER 228-100/101/200/201/202/212 | DATE: 12/18/95 | 23-3 | | --------------------------------------------------------------------------- | | 1. | 2. NUMBER INSTALLED | | SYSTEM & | -------------------------------------------- | | SEQUENCE ITEM | | 3. NUMBER REQUIRED FOR DISPATCH | | NUMBERS | | --------------------------------------- | | ------------------------- | | | 4. REMARKS OR EXCEPTIONS | | 23 COMMUNICATIONS | | | | | | | | | | | | | | | Boom Microphones | | | | | | (If No FDR Required by | | | | | | FAR) | | | | | | | | | | | 1) Cockpit Voice A | - | 0 | May be inoperative provided repairs | | | Recorder Equipped | | | are made within three flight days. | | | to Record | | | | | | Boom Microphones | | | | | | per FAR 135.151(d) | | | | | | | | | | | 2) Cockpit Voice D | - | 0 | | | | Recorder Not | | | | | | Equipped to Record | | | | | | Boom Microphone | | | | | | | | | | | 10. Recorded Passenger C | - | 0 | (O)May be inoperative provided | | Address System | | | alternate procedures are | | *** | | | established and used. | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | ------------------------------------------------------------------------------- ------------------------------------------------------------------------------- | U.S. DEPARTMENT OF TRANSPORTATION | | | | MASTER MINIMUM EQUIPMENT LIST | | FEDERAL AVIATION ADMINISTRATION | | --------------------------------------------------------------------------- | | AIRCRAFT: | REVISION NO: 6 | PAGE: | | | | | | DORNIER 228-100/101/200/201/202/212 | DATE: 08/03/93 | 24-1 | | --------------------------------------------------------------------------- | | 1. | 2. NUMBER INSTALLED | | SYSTEM & | -------------------------------------------- | | SEQUENCE ITEM | | 3. NUMBER REQUIRED FOR DISPATCH | | NUMBERS | | --------------------------------------- | | ------------------------- | | | 4. REMARKS OR EXCEPTIONS | | 24 ELECTRICAL POWER | | | | | | | | | | | | | | | 1. Inverter B | 2 | 1 | One may be inoperative for | | | | | day VMC. | | | | | | | 2. A.C. Voltmeter B | 2 | 1 | One may be inoperative for day VMC | | | | | provided associated inverter | | | | | caution light is monitored. | | | | | | | 3. D.C. Voltmeter B | 1 | 0 | May be inoperative provided: | | | | | | | | | | a) Both D.C. ammeters and both | | | | | generator caution lights are | | | | | operative, and | | | | | | | | | | b) Aircraft battery engine start | | | | | is not made. | | | | | | | 4. D.C. Ammeter B | 2 | 1 | One may be inoperative provided: | | | | | | | | | | a) D.C. voltmeter and generator | | | | | caution lights are operative | | | | | and monitored, and | | | | | | | | | | b) The first engine start is | | | | | made on the side of the | | | | | operative ammeter to determine | | | | | proper battery condition prior | | | | | to second engine start. | | | | | | | 5. Generator Caution B | 2 | 1 | One may be inoperative provided: | | Lights | | | | | | | | a) Both ammeters are operative | | | | | monitored, and | | | | | | | | | | b) D. C. voltmeter is operative. | | | | | | | 6. Ground Power C | 1 | 0 | (M)May be inoperative provided the | | Receptacle | | | external power socket circuit | | | | | breaker, 2PD, is pulled and | | | | | banded. | | | | | | ------------------------------------------------------------------------------- ------------------------------------------------------------------------------- | U.S. DEPARTMENT OF TRANSPORTATION | | | | MASTER MINIMUM EQUIPMENT LIST | | FEDERAL AVIATION ADMINISTRATION | | --------------------------------------------------------------------------- | | AIRCRAFT: | REVISION NO: 6 | PAGE: | | | | | | DORNIER 228-100/101/200/201/202/212 | DATE: 08/03/93 | 25-1 | | --------------------------------------------------------------------------- | | 1. | 2. NUMBER INSTALLED | | SYSTEM & | -------------------------------------------- | | SEQUENCE ITEM | | 3. NUMBER REQUIRED FOR DISPATCH | | NUMBERS | | --------------------------------------- | | ------------------------- | | | 4. REMARKS OR EXCEPTIONS | | 25 EQUIPMENT/FURNISHINGS | | | | | | | | | | | | | | | 1. Crewmember Seats | | | | | | | | | | A. Seat Pan Height C | 2 | 0 | (M)May be inoperative provided: | | Adjustment Lever | | | | | | | | a) The crewmember can manipulate | | | | | all flight controls through | | | | | their full travel, and | | | | | | | | | | b) All locking pins are visually | | | | | inspected to determine that | | | | | they are fully engaged. | | | | | | | B. Track Lock C | 2 | 0 | (M)May be inoperative provided: | | Control Lever | | | | | | | | a) The crewmember can manipulate | | | | | all flight controls through | | | | | their full travel, and | | | | | | | | | | b) All locking pins are visually | | | | | inspected to determine that | | | | | they are fully engaged. | | | | | | | 2. Cockpit Crewmember B | 2 | 1 | Right seat shoulder harness may be | | Shoulder Harness | | | inoperative for single pilot | | | | | operations . Right side pilot seat | | | | | must be unoccupied. | | | | | | | 3. Passenger Seat C | - | - | (M)All may be inoperative | | | | | provided: | | | | | | | | | | a) Affected seat does not block | | | | | emergency egress to an aisle | | | | | or exit, and | | | | | | | | | | b) Affected seat is blocked and | | | | | placarded "DO NOT OCCUPY". | | | | | | | | | | (Continued) | | | | | | | | | | | ------------------------------------------------------------------------------- ------------------------------------------------------------------------------- | U.S. DEPARTMENT OF TRANSPORTATION | | | | MASTER MINIMUM EQUIPMENT LIST | | FEDERAL AVIATION ADMINISTRATION | | --------------------------------------------------------------------------- | | AIRCRAFT: | REVISION NO: 6 | PAGE: | | | | | | DORNIER 228-100/101/200/201/202/212 | DATE: 08/03/93 | 25-2 | | --------------------------------------------------------------------------- | | 1. | 2. NUMBER INSTALLED | | SYSTEM & | -------------------------------------------- | | SEQUENCE ITEM | | 3. NUMBER REQUIRED FOR DISPATCH | | NUMBERS | | --------------------------------------- | | ------------------------- | | | 4. REMARKS OR EXCEPTIONS | | 25 EQUIPMENT/FURNISHINGS | | | | | | | | | | | | | | | (Cont'd) | | | | | | | | 1. A seat with an inoperative | | | | | seatbelt or shoulder harness is | | | | | considered to be inoperative. | | | | | | | | | | 2. A seat with an inoperative | | | | | recline mechanism is considered | | | | | to be inoperative if the seat | | | | | back cannot be secured in the | | | | | upright position. | | | | | | | 4. Passenger Seat C | - | - | May be inoperative provided they | | Trays | | | are secured in the upright position | | | | | or removed. | | | | | | | 5. Passenger Seat | | | DELETED, REVISION 6. | | Ashtray | | | See passenger convenience items. | | | | | | | 6. Emergency Locator C | 1 | 0 | As required by FAR. | | Beacon | | | | | | | | OR | | | | | | | C | 1 | 0 | May be inoperative for published | | | | | scheduled flights in air | | | | | carrier service. | | | | | | | 7. Cargo Net C | 1 | 0 | May be inoperative provided no | | | | | baggage/cargo is carried in the | | | | | aft baggage compartment or ski | | | | | container. | | | | | | | 8. Approved Flotation C | - | - | As required by FAR. | | Device | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | ------------------------------------------------------------------------------- ------------------------------------------------------------------------------- | U.S. DEPARTMENT OF TRANSPORTATION | | | | MASTER MINIMUM EQUIPMENT LIST | | FEDERAL AVIATION ADMINISTRATION | | --------------------------------------------------------------------------- | | AIRCRAFT: | REVISION NO: 6 a | PAGE: | | | | | | DORNIER 228-100/101/200/201/202/212 | DATE: 12/18/95 | 25-3 | | --------------------------------------------------------------------------- | | 1. | 2. NUMBER INSTALLED | | SYSTEM & | -------------------------------------------- | | SEQUENCE ITEM | | 3. NUMBER REQUIRED FOR DISPATCH | | NUMBERS | | --------------------------------------- | | ------------------------- | | | 4. REMARKS OR EXCEPTIONS | | 25 EQUIPMENT/FURNISHINGS | | | | | | | | | | | | | | | 9. Passenger Convenience | - | - | Passenger convenience items, as | | | Items | | | expressed in the MMEL, are those | | | | | related to passenger convenience, | | | | | comfort or entertainment such as | | | | | but not limited to, galley | | | | | equipment,movie equipment, ash | | | | | trays, stereo equipment, overhead | | | | | | reading lamps, etc. Items | | | | | addressed elsewhere in this | | | | | document shall not be included. | | | | | (M) and (O) procedures may be | | | | | required and included in the air | | | | | carrier's appropriate document. | | | | | | | 10. First Aid Kits D | - | - | Any in excess of those required by | | | | | | FAR may be incomplete or missing | | | | | | provided the required distribution | | | | | | is maintained. | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | ------------------------------------------------------------------------------- ------------------------------------------------------------------------------- | U.S. DEPARTMENT OF TRANSPORTATION | | | | MASTER MINIMUM EQUIPMENT LIST | | FEDERAL AVIATION ADMINISTRATION | | --------------------------------------------------------------------------- | | AIRCRAFT: | REVISION NO: 6 a | PAGE: | | | | | | DORNIER 228-100/101/200/201/202/212 | DATE: 12/18/95 | 26-1 | | --------------------------------------------------------------------------- | | 1. | 2. NUMBER INSTALLED | | SYSTEM & | -------------------------------------------- | | SEQUENCE ITEM | | 3. NUMBER REQUIRED FOR DISPATCH | | NUMBERS | | --------------------------------------- | | ------------------------- | | | 4. REMARKS OR EXCEPTIONS | | 1. Portable Fire D | - | - | Any in excess of those required by | | | Extinguisher | | | FAR may be inoperative or missing | | | | | | provided: | | | | | | | | | | | a) The inoperative fire | | | | | | extinguisher is tagged | | | | | | inoperative, removed from the | | | | | | installed location, and placed | | | | | | out of sight so it can not be | | | | | | mistaken for an functional unit, | | | | | | and | | | | | | | | | | | b) Required distribution is | | | | | | maintained. | | | | | | | | 2. Engine Fire C | 2 | 0 | | | Extinguisher | | | | | (Applies to | | | | | 100/200 only) | | | | | | | | | | 3. Fire Extinguisher C | 2 | 0 | May be missing provided bottle | | Indicator Discs | | | pressure guage is visually | | | | | checked prior to each flight to | | | | | assure bottle pressure is within | | | | | limits. | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | ------------------------------------------------------------------------------- ------------------------------------------------------------------------------- | U.S. DEPARTMENT OF TRANSPORTATION | | | | MASTER MINIMUM EQUIPMENT LIST | | FEDERAL AVIATION ADMINISTRATION | | --------------------------------------------------------------------------- | | AIRCRAFT: | REVISION NO: 6 | PAGE: | | | | | | DORNIER 228-100/101/200/201/202/212 | DATE: 08/03/93 | 27-1 | | --------------------------------------------------------------------------- | | 1. | 2. NUMBER INSTALLED | | SYSTEM & | -------------------------------------------- | | SEQUENCE ITEM | | 3. NUMBER REQUIRED FOR DISPATCH | | NUMBERS | | --------------------------------------- | | ------------------------- | | | 4. REMARKS OR EXCEPTIONS | | 27 FLIGHT CONTROLS | | | | | | | | | | | | | | | 1. Flap Position C | 1 | 0 | May be inoperative provided: | | Indicator | | | | | | | | a) Flaps are visually checked for | | | | | full travel and flap operation | | | | | is not affected, and | | | | | | | | | | b) Flaps are visually checked to | | | | | confirm flap position agrees | | | | | with selected position. | | | | | | | 2. Trim Tab Position C | 1 | 0 | May be inoperative provided: | | Indicator (Rudder) | | | | | | | | a) Tab is visually checked for | | | | | full range of operation, | | | | | | | | | | b) Tab operation is not impaired, | | | | | and | | | | | | | | | | c) Tab is positioned to neutral | | | | | prior to each departure and | | | | | neutral position is verified | | | | | by visual inspection. | | | | | | | 3. Trim Tab Position C | 1 | 0 | May be inoperative provided: | | Indicator (Aileron) | | | | | | | | a) Trim is visually checked for | | | | | full range of operation. | | | | | | | | | | b) Trim operation is not | | | | | impaired, and | | | | | | | | | | c) Trim is positioned to neutral | | | | | prior to each departure and | | | | | neutral position is verified | | | | | by visual inspection. | | | | | | | | | | | | | | | | | | | | | | | | | | ------------------------------------------------------------------------------- ------------------------------------------------------------------------------- | U.S. DEPARTMENT OF TRANSPORTATION | | | | MASTER MINIMUM EQUIPMENT LIST | | FEDERAL AVIATION ADMINISTRATION | | --------------------------------------------------------------------------- | | AIRCRAFT: | REVISION NO: 6 | PAGE: | | | | | | DORNIER 228-100/101/200/201/202/212 | DATE: 08/03/93 | 27-2 | | --------------------------------------------------------------------------- | | 1. | 2. NUMBER INSTALLED | | SYSTEM & | -------------------------------------------- | | SEQUENCE ITEM | | 3. NUMBER REQUIRED FOR DISPATCH | | NUMBERS | | --------------------------------------- | | ------------------------- | | | 4. REMARKS OR EXCEPTIONS | | 27 FLIGHT CONTROLS | | | | | | | | | | | | | | | | | | | | 4. Flap System C | 1 | 0 | (O)May be inoperative provided: | | | | | | | | | | a) Flaps are in full up | | | | | position. | | | | | | | | | | b) Performance charts in AFM | | | | | for no flap takeoff and | | | | | landing are used. | | | | | | | 5. Stall Warning System | | | | | | | | | | A. Reference Speed C | 1 | 0 | | | Deviation (RSD) | | | | | Indicator | | | | | | | | | | B. Stall Warning C | 1 | 0 | May be inoperative provided stall | | Light | | | warning horn and reference speed | | | | | deviation indicator are operative. | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | ------------------------------------------------------------------------------- ------------------------------------------------------------------------------- | U.S. DEPARTMENT OF TRANSPORTATION | | | | MASTER MINIMUM EQUIPMENT LIST | | FEDERAL AVIATION ADMINISTRATION | | --------------------------------------------------------------------------- | | AIRCRAFT: | REVISION NO: 6 a | PAGE: | | | | | | DORNIER 228-100/101/200/201/202/212 | DATE: 12/18/95 | 28-1 | | --------------------------------------------------------------------------- | | 1. | 2. NUMBER INSTALLED | | SYSTEM & | -------------------------------------------- | | SEQUENCE ITEM | | 3. NUMBER REQUIRED FOR DISPATCH | | NUMBERS | | --------------------------------------- | | ------------------------- | | | 4. REMARKS OR EXCEPTIONS | | 28 FUEL | | | | | | | | | | | | | | | 1. Fuel Quantity B | 2 | 1 | (O)One may be inoperative | | Indicator | | | provided: | | | | | | | | | | a) A reliable means is established | | | | | to determine that fuel quantity | | | | | on board meets the regulatory | | | | | requirements for the intended | | | | | flight, | | | | | | | | | | b) Both fuel flow indicators are | | | | | operative, and | | | | | | | | | | c) Both fuel quantity and fuel | | | | | pressure annunciators are | | | | | operative. | | | | | | | 2. Fuel Quantity C | 2 | 1 | One may be inoperative provided: | | Annunciator | | | | | | | | a) Fuel quantity on board is | | | | | adequate for intended flight, | | | | | and | | | | | | | | | | b) Fuel quantity indicators are | | | | | operative. | | | | | | | 3. Magna Stick System C | 2 | 0 | May be inoperative provided they | | | | | are not required to determine | | | | | fuel quantity. | | | | | | | 4. Pressure Refueling C | 1 | 0 | | | System | | | | | | | | | | 5. Manual Shutoff C | 1 | 0 | (M)May be inoperative provided it | | Valve (single point | | | is secured in the closed | | refueling system | | | position. | | only) | | | | | | | | | | | | | | | | | | | | | | | | ------------------------------------------------------------------------------- ------------------------------------------------------------------------------- | U.S. DEPARTMENT OF TRANSPORTATION | | | | MASTER MINIMUM EQUIPMENT LIST | | FEDERAL AVIATION ADMINISTRATION | | --------------------------------------------------------------------------- | | AIRCRAFT: | REVISION NO: 6 a | PAGE: | | | | | | DORNIER 228-100/101/200/201/202/212 | DATE: 12/18/95 | 28-2 | | --------------------------------------------------------------------------- | | 1. | 2. NUMBER INSTALLED | | SYSTEM & | -------------------------------------------- | | SEQUENCE ITEM | | 3. NUMBER REQUIRED FOR DISPATCH | | NUMBERS | | --------------------------------------- | | ------------------------- | | | 4. REMARKS OR EXCEPTIONS | | 28 FUEL | | | | | | | | | | | | | | | 6. Booster Pumps C | 4 | 2 | One may be inoperative on each | | | | | side provided refueling/defueling | | | | | manual shutoff valve is in the | | | | | closed position. | | | | | | | | | | NOTE: Usable fuel reduced with | | | | | boost pump inoperative. | | | | | (See AFM) | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | ------------------------------------------------------------------------------- ------------------------------------------------------------------------------- | U.S. DEPARTMENT OF TRANSPORTATION | | | | MASTER MINIMUM EQUIPMENT LIST | | FEDERAL AVIATION ADMINISTRATION | | --------------------------------------------------------------------------- | | AIRCRAFT: | REVISION NO: 6 | PAGE: | | | | | | DORNIER 228-100/101/200/201/202/212 | DATE: 08/03/93 | 30-1 | | --------------------------------------------------------------------------- | | 1. | 2. NUMBER INSTALLED | | SYSTEM & | -------------------------------------------- | | SEQUENCE ITEM | | 3. NUMBER REQUIRED FOR DISPATCH | | NUMBERS | | --------------------------------------- | | ------------------------- | | | 4. REMARKS OR EXCEPTIONS | | 30 ICE AND RAIN | | | | | PROTECTION | | | | | | | | | | 1. Surface Deice C | 1 | 0 | May be inoperative provided | | System (wing, | | | aircraft is not operated in known | | horizontal and | | | or forecast icing conditions. | | vertical stabilizer) | | | | | | | | | | 2. Propeller Deicing C | 2 | 0 | May be inoperative provided | | System | | | aircraft is not operated in known | | | | | or forecast icing conditions. | | | | | | | 3. Windshield Deicing C | 2 | 0 | May be inoperative provided | | System | | | aircraft is not operated in known | | | | | or forecast icing conditions. | | | | | | | 4. Pitot Heater B | 2 | 0 | May be inoperative provided: | | | | | | | | | | a) IFR passenger carrying | | | | | operations are not conducted, | | | | | and | | | | | | | | | | b) Aircraft is not operated in | | | | | known or forecast icing | | | | | conditions. | | | | | | | 5. Windshield Wipers C | 2 | 0 | May be inoperative provided | | | | | aircraft is not operated in | | | | | precipitation within 5 nautical | | | | | miles of the airport of takeoff or | | | | | intended landing. | | | | | | | 1) Park Mode C | 1 | 0 | May be inoperative provided | | | | | wipers work in normal mode and | | | | | wipers can be parked by selecting | | | | | ON or OFF until wipers park in a a | | | | | position that does not impair | | | | | vision. | | | | | | | 6. Stall Warning/Lift B | 1 | 0 | May be inoperative provided | | Transducer Heater | | | aircraft is not operated in known | | | | | or forecast icing conditions. | | | | | | ------------------------------------------------------------------------------- ------------------------------------------------------------------------------- | U.S. DEPARTMENT OF TRANSPORTATION | | | | MASTER MINIMUM EQUIPMENT LIST | | FEDERAL AVIATION ADMINISTRATION | | --------------------------------------------------------------------------- | | AIRCRAFT: | REVISION NO: 6 | PAGE: | | | | | | DORNIER 228-100/101/200/201/202/212 | DATE: 08/03/93 | 30-2 | | --------------------------------------------------------------------------- | | 1. | 2. NUMBER INSTALLED | | SYSTEM & | -------------------------------------------- | | SEQUENCE ITEM | | 3. NUMBER REQUIRED FOR DISPATCH | | NUMBERS | | --------------------------------------- | | ------------------------- | | | 4. REMARKS OR EXCEPTIONS | | 30 ICE AND RAIN | | | | | PROTECTION | | | | | | | | | | 7. Engine Inlet C | 2 | 0 | (M)Both may be inoperative | | Anti-ice Valves | | | provided: | | | | | | | | | | a) Valve is in the off/closed | | | | | position, | | | | | | | | | | b) Aircraft is not operated in | | | | | temperatures below 40 | | | | | degrees F, and | | | | | | | | | | c) Aircraft is not operated in | | | | | known or forecast icing | | | | | conditions. | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | ------------------------------------------------------------------------------- ------------------------------------------------------------------------------- | U.S. DEPARTMENT OF TRANSPORTATION | | | | MASTER MINIMUM EQUIPMENT LIST | | FEDERAL AVIATION ADMINISTRATION | | --------------------------------------------------------------------------- | | AIRCRAFT: | REVISION NO: 6 | PAGE: | | | | | | DORNIER 228-100/101/200/201/202/212 | DATE: 08/03/93 | 31-1 | | --------------------------------------------------------------------------- | | 1. | 2. NUMBER INSTALLED | | SYSTEM & | -------------------------------------------- | | SEQUENCE ITEM | | 3. NUMBER REQUIRED FOR DISPATCH | | NUMBERS | | --------------------------------------- | | ------------------------- | | | 4. REMARKS OR EXCEPTIONS | | 31 INDICATING/RECORDING | | | | | SYSTEMS | | | | | | | | | | 1. Clock with sweep C | 2 | 1 | Two required pilots: | | second hand or | | | One may be inoperative. | | electric digital clock | | | | | | | | | | C | 2 | 1 | One required pilot: | | | | | Right side may be inoperative. | | | | | | | 2. Flight Hour C | 1 | 0 | (O) | | Recorder | | | | | | | | | | 3. Engine Hour C | 1 | 0 | (O) | | Recorder | | | | | | | | | | 4. Flight Data A | 1 | 0 | May be inoperative provided | | Recorder | | | Cockpit Voice Recorder is | | (When Required By | | | operative and repairs are made | | FAR's) | | | within three flight days. | | | | | | | Flight Data C | 1 | 0 | | | Recorder | | | | | (When Not Required By | | | | | FAR's) | | | | | *** | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | ------------------------------------------------------------------------------- ------------------------------------------------------------------------------- | U.S. DEPARTMENT OF TRANSPORTATION | | | | MASTER MINIMUM EQUIPMENT LIST | | FEDERAL AVIATION ADMINISTRATION | | --------------------------------------------------------------------------- | | AIRCRAFT: | REVISION NO: 6 | PAGE: | | | | | | DORNIER 228-100/101/200/201/202/212 | DATE: 08/03/93 | 32-1 | | --------------------------------------------------------------------------- | | 1. | 2. NUMBER INSTALLED | | SYSTEM & | -------------------------------------------- | | SEQUENCE ITEM | | 3. NUMBER REQUIRED FOR DISPATCH | | NUMBERS | | --------------------------------------- | | ------------------------- | | | 4. REMARKS OR EXCEPTIONS | | 32 LANDING GEAR | | | | | | | | | | | | | | | 1. Nosewheel Steering C | 1 | 0 | (O)(M) | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | ------------------------------------------------------------------------------- ------------------------------------------------------------------------------- | U.S. DEPARTMENT OF TRANSPORTATION | | | | MASTER MINIMUM EQUIPMENT LIST | | FEDERAL AVIATION ADMINISTRATION | | --------------------------------------------------------------------------- | | AIRCRAFT: | REVISION NO: 6 a | PAGE: | | | | | | DORNIER 228-100/101/200/201/202/212 | DATE: 12/18/95 | 33-1 | | --------------------------------------------------------------------------- | | 1. | 2. NUMBER INSTALLED | | SYSTEM & | -------------------------------------------- | | SEQUENCE ITEM | | 3. NUMBER REQUIRED FOR DISPATCH | | NUMBERS | | --------------------------------------- | | ------------------------- | | | 4. REMARKS OR EXCEPTIONS | | 33 LIGHTS | | | | | | | | | | | | | | | 1. Flight Compartment C | - | - | Individual lights may be | | | and Instrument | | | inoperative provided remaining | | | Lighting System | | | 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 crewmembers | | | | | | eyes, and | | | | | | c) Lighting configuration and | | | | | | intensity is acceptable to the | | | | | | flight crew. | | | 2. Passenger Notice - C | 1 | 0 | May be inoperative provided | | (Fasten Seatbelt) | | | appropriate verbal briefings are | | | | | given to passengers. | | | | | | | Passenger Notice - C | 1 | 0 | May be inoperative provided | | (No Smoking) | | | appropriate verbal briefings are | | | | | given to passengers. | | | | | | | 3. Landing Lights C | 2 | 1 | One may be inoperative for night | | | | | operations. | | | | | | | | | | OR | | | | | | | C | 2 | 0 | Both may be inoperative for day | | | | | operations. | | | | | | | | | | | | | | | | | 4. Taxi Light C | 2 | 0 | May be inoperative for day | | | | | operations. | | | | | | | | | | OR | | | | | | | C | 2 | 0 | May be inoperative for night | | | | | operations provided both landing | | | | | lights are operative. | ------------------------------------------------------------------------------- ------------------------------------------------------------------------------- | U.S. DEPARTMENT OF TRANSPORTATION | | | | MASTER MINIMUM EQUIPMENT LIST | | FEDERAL AVIATION ADMINISTRATION | | --------------------------------------------------------------------------- | | AIRCRAFT: | REVISION NO: 6 a | PAGE: | | | | | | DORNIER 228-100/101/200/201/202/212 | DATE: 12/18/95 | 33-2 | | --------------------------------------------------------------------------- | | 1. | 2. NUMBER INSTALLED | | SYSTEM & | -------------------------------------------- | | SEQUENCE ITEM | | 3. NUMBER REQUIRED FOR DISPATCH | | NUMBERS | | --------------------------------------- | | ------------------------- | | | 4. REMARKS OR EXCEPTIONS | | 33 LIGHTS | | | | | | | | | | | | | | | 5. Anticollision B | 1 | 0 | May be inoperative provided: | | Light System | | | | | | | | a) Airplane is not operated | | | | | at night. | | | | | | | | | | OR | | | | | | | B | 1 | 0 | b) Strobes are installed and | | | | | operate normally. | | | | | | | | | | NOTE 1: The strobe light system | | | | | must be approved and certificated | | | | | as an Anti-Collision Light System | | | | | if used in place of a rotating | | | | | beacon. | | | | | | | 6. Position Lights C | 3 | 0 | May be inoperative for day | | | | | operations. | | | | | | | 7. Wing Illumination C | 1 | 0 | May be inoperative provided a | | Lights (Ice Detect) | | | portable lamp/light of adequate | | | | | capacity for wing and/or control | | | | | surface inspection is available for | | | | | night operations in icing | | | | | conditions. | | | | | | | 8. Strobe Lights C | 3 | 0 | | | | | | | | 9. Logo Lights C | 2 | 0 | | | | | | | | 10. Passenger Cabin C | - | - | May be inoperative provided | | Lighting | | | lighting configuration is | | | | | acceptable to the flight crew. | | | | | | | 11. Hydraulic System C | 1 | 0 | | | Level Check Light | | | | | | | | | | 12. Master Warning C | 2 | 1 | (O)One may be inoperative provided | | Lights | | | the warning horn is operative. | | | | | | ------------------------------------------------------------------------------- ------------------------------------------------------------------------------- | U.S. DEPARTMENT OF TRANSPORTATION | | | | MASTER MINIMUM EQUIPMENT LIST | | FEDERAL AVIATION ADMINISTRATION | | --------------------------------------------------------------------------- | | AIRCRAFT: | REVISION NO: 6 a | PAGE: | | | | | | DORNIER 228-100/101/200/201/202/212 | DATE: 12/18/95 | 33-3 | | --------------------------------------------------------------------------- | | 1. | 2. NUMBER INSTALLED | | SYSTEM & | -------------------------------------------- | | SEQUENCE ITEM | | 3. NUMBER REQUIRED FOR DISPATCH | | NUMBERS | | --------------------------------------- | | ------------------------- | | | 4. REMARKS OR EXCEPTIONS | | 33 LIGHTS | | | | | | | | | | | | | | | 13. Master Caution C | 2 | 1 | One may be inoperative. | | Lights | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | ------------------------------------------------------------------------------- ------------------------------------------------------------------------------- | U.S. DEPARTMENT OF TRANSPORTATION | | | | MASTER MINIMUM EQUIPMENT LIST | | FEDERAL AVIATION ADMINISTRATION | | --------------------------------------------------------------------------- | | AIRCRAFT: | REVISION NO: 6 a | PAGE: | | | | | | DORNIER 228-100/101/200/201/202/212 | DATE: 12/18/95 | 34-1 | | --------------------------------------------------------------------------- | | 1. | 2. NUMBER INSTALLED | | SYSTEM & | -------------------------------------------- | | SEQUENCE ITEM | | 3. NUMBER REQUIRED FOR DISPATCH | | NUMBERS | | --------------------------------------- | | ------------------------- | | | 4. REMARKS OR EXCEPTIONS | | 34 NAVIGATION | | | | | | | | | | | | | | | 1. Gyroscopic Rate of B | 2 | 1 | May be inoperative on right side | | Turn and Slip Skid | | | for day VMC. | | Indicator | | | | | | | | | | 2. Vertical Speed B | 2 | 1 | One may be inoperative for day | | Indicator | | | VMC. | | | | | | | 3. Navigation Equip- C | - | - | As required by FAR. | | ment (VOR/ILS, Loran, | | | | | Omega/VLF, INS, RNAV, | ? | | | | | Doppler, GPS) | | | | | | | | | | 4. ATC Transponders D | - | - | Any in excess of those required by | | | and Automatic | | | FAR may be inoperative. | | | Altitude Reporting | | | | | | Systems | | | | | | | | | | | 5. Marker Beacon C | 2 | 0 | May be inoperative provided | | | | | approach procedure does not | | | | | require its use. | | | | | | | 6. Weather Radar/ C | 1 | 0 | As required by FAR. | | Thunderstorm | | | | | Detection Equipment | | | | | | | | | | 7. Flight Director C | 2 | 0 | | | *** | | | | | | | | | | 8. Encoding Function | | | Combined with ATC Transponders, | | | of Altimeter | | | Revision 6a. | | | | | | | | 9. Speed Preset C | - | - | | | Markers | | | | | | | | | | 10. Altitude Preset C | - | - | | | Marker | | | | | | | | | | 11. DME C | 1 | 0 | As required by FAR. | | | | | | | | | | | ------------------------------------------------------------------------------- ------------------------------------------------------------------------------- | U.S. DEPARTMENT OF TRANSPORTATION | | | | MASTER MINIMUM EQUIPMENT LIST | | FEDERAL AVIATION ADMINISTRATION | | --------------------------------------------------------------------------- | | AIRCRAFT: | REVISION NO: 6 a | PAGE: | | | | | | DORNIER 228-100/101/200/201/202/212 | DATE: 12/18/95 | 34-2 | | --------------------------------------------------------------------------- | | 1. | 2. NUMBER INSTALLED | | SYSTEM & | -------------------------------------------- | | SEQUENCE ITEM | | 3. NUMBER REQUIRED FOR DISPATCH | | NUMBERS | | --------------------------------------- | | ------------------------- | | | 4. REMARKS OR EXCEPTIONS | | 34 NAVIGATION | | | | | | | | | | | | | | | 12. Radar Altimeter C | 1 | 0 | | | | | | | | 13. Altitude Alerter B | 1 | 0 | | | | | | | | 14. ADF C | - | 0 | As required by FAR. | | | | | | | | | | Note: The ADF may be operated with | | | | | inoperative timing functions | | | | | (i.e. Elapsed Time, Flight Time, | | | | | Stop Watch, etc.) that do not | | | | | affect ADF navigation. | | | | | | | 15. RMI C | - | 0 | | | | | | | | 16. Nonstabilized B | 1 | 0 | May be inoperative provided any | | Magnetic Compass | | | combination of three gyro or INS | | | | | (IRU) stabilized compass systems | | | | | are operative. | | | | | | | | | | OR | | | | | | | B | 1 | 0 | May be inoperative provided: | | | | | | | | | | a) combination of two gyro or | | | | | INS stabilized compass systems | | | | | are operative, and | | | | | | | | | | b) Aircraft is operated with dual | | | | | independent navigation | | | | | capability and under positive | | | | | radar control by ATC on the | | | | | enroute portion of the flight. | | | | | | | | | | OR | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | ------------------------------------------------------------------------------- ------------------------------------------------------------------------------- | U.S. DEPARTMENT OF TRANSPORTATION | | | | MASTER MINIMUM EQUIPMENT LIST | | FEDERAL AVIATION ADMINISTRATION | | --------------------------------------------------------------------------- | | AIRCRAFT: | REVISION NO: 6 a | PAGE: | | | | | | DORNIER 228-100/101/200/201/202/212 | DATE: 12/18/95 | 34-3 | | --------------------------------------------------------------------------- | | 1. | 2. NUMBER INSTALLED | | SYSTEM & | -------------------------------------------- | | SEQUENCE ITEM | | 3. NUMBER REQUIRED FOR DISPATCH | | NUMBERS | | --------------------------------------- | | ------------------------- | | | 4. REMARKS OR EXCEPTIONS | | 34 NAVIGATION | | | | | | | | | | | | | | | 16. Nonstabilized B | 1 | 0 | May be inoperative for flights | | Magnetic Compass | | | that are entirely within areas of | | (continued) | | | magnetic unreliability provided at | | | | | least two stabilized directional | | | | | gyro systems are installed, | | | | | operative, and used in conjunction | | | | | with approved free gyro navigation | | | | | techniques. | | | | | | | 17. Gyroscopic B | 2 | 1 | (O) Either may be inoperative | | Directional Indicator | | | provided: | | Slaving System | | | | | | | | a) Slaving can be disconnected, | | | | | | | | | | b) Crew can manually set | | | | | heading, and | | | | | | | | | | c) Magnetic compass is | | | | | operative. | | | | | | | 18. Traffic Alert | | | | | | Collision Avoidance | | | | | | System (TCAS) II | | | | | | | | | | | | 1) TCAS System C | - | 0 | (M)May be inoperative provided the | | | | | | system is deactivated and secured. | | | | | | | | | 2) Combined TA C | 2 | 1 | (O)May be inoperative on the non- | | | and RA Dual | | | flying pilot side provided: | | | Displays | | | | | | *** | | | a) TA and RA elements and audio | | | | | | functions are operative on | | | | | | flying pilot side, and | | | | | | | | | | | | b) TA and RA display indications | | | | | | are visible to the non-flying | | | | | | pilot. | | | | | | | | | | | | | | | | | ------------------------------------------------------------------------------- ------------------------------------------------------------------------------- | U.S. DEPARTMENT OF TRANSPORTATION | | | | MASTER MINIMUM EQUIPMENT LIST | | FEDERAL AVIATION ADMINISTRATION | | --------------------------------------------------------------------------- | | AIRCRAFT: | REVISION NO: 6 a | PAGE: | | | | | | DORNIER 228-100/101/200/201/202/212 | DATE: 12/18/95 | 34-4 | | --------------------------------------------------------------------------- | | 1. | 2. NUMBER INSTALLED | | SYSTEM & | -------------------------------------------- | | SEQUENCE ITEM | | 3. NUMBER REQUIRED FOR DISPATCH | | NUMBERS | | --------------------------------------- | | ------------------------- | | | 4. REMARKS OR EXCEPTIONS | | 34 NAVIGATION | | | | | | | | | | | | | | | 3) Resolution C | 2 | 1 | (O)One may be inoperative on non- | | | Advisory (RA) | | | flying pilot side. | | | Display System(s) | | | | | | | | | | | C | - | 0 | (O)May be inoperative provided: | | | | | | | | | | | a) All Traffic Alert (TA) | | | | | display elements and voice | | | | | command audio functions are | | | | | operative, and | | | | | | | | | | b) TA only mode is selected by | | | | | the flight crew. | | | | | | | 4) TA Display C | - | 0 | (O)May be inoperative provided all | | | System(s) | | | installed RA display and audio | | | | | functions are operative. | | | | | | | 19. TCAS I D | 1 | 0 | May be inoperative until required | | | | | | by FAR. | | | | | | | | | | | | | 20. Ground Proximity | | | | | | *** Warning System | | | | | | | | | | | | 1) Modes 1-4 A | - | 0 | (O)May be inoperative provided: | | | | | | a) Alternate procedures are | | | | | | established, used and | | | | | | b) Repairs are made within | | | | | | two flight days. | | | | | | | | | 2) Test Mode A | 1 | 0 | May be inoperative provided: | | | | | | a) The GPWS is considered | | | | | | inoperative and | | | | | | b) Repairs are made within | | | | | | two flight days. | | | | | | | | | 3) Glideslope B | 2 | 0 | | | | Deviation | | | | | | (Mode 5) | | | | | ------------------------------------------------------------------------------- ------------------------------------------------------------------------------- | U.S. DEPARTMENT OF TRANSPORTATION | | | | MASTER MINIMUM EQUIPMENT LIST | | FEDERAL AVIATION ADMINISTRATION | | --------------------------------------------------------------------------- | | AIRCRAFT: | REVISION NO: 6 a | PAGE: | | | | | | DORNIER 228-100/101/200/201/202/212 | DATE: 12/18/95 | 34-5 | | --------------------------------------------------------------------------- | | 1. | 2. NUMBER INSTALLED | | SYSTEM & | -------------------------------------------- | | SEQUENCE ITEM | | 3. NUMBER REQUIRED FOR DISPATCH | | NUMBERS | | --------------------------------------- | | ------------------------- | | | 4. REMARKS OR EXCEPTIONS | | 34 NAVIGATION | | | | | | | | | | | | | | | 4) Advisory C | - | 0 | (O)May be inoperative provided | | | *** Callouts | | | alternate procedures are | | | | | | established and used. | | | | | | | | | 5) Windshear Mode C | - | 0 | (O)May be inoperative provided | | | | | | alternate procedures are | | | | | | established and used. | | | | | | | | 21. Flight Profile | | | | | | Advisory System(FPAS) | | | | | | | | | | | 1) Gear Mode A | 1 | 0 | (O)May be inoperative provided: | | | | | | | | | | | a) Alternate procedures are | | | | | | established and used, and | | | | | | b) Repairs are made within | | | | | | two flight days. | | | | | | | | | | | | | | | | | | | | | | | 2) Minimums Mode A | 1 | 0 | (O)May be inoperative provided: | | | | | | | | | | | a) Alternate procedures are | | | | | | established and used, and | | | | | | b) Repairs are made within | | | | | | two flight days. | | | | | | | | 3) Radio Altitude A | 1 | 0 | (O)May be inoperative provided: | | | Mode | | | | | | | | a) Alternate procedures are | | | | | | established and used, and | | | | | | b) Repairs are made within | | | | | | two flight days. | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | ------------------------------------------------------------------------------- ------------------------------------------------------------------------------- | U.S. DEPARTMENT OF TRANSPORTATION | | | | MASTER MINIMUM EQUIPMENT LIST | | FEDERAL AVIATION ADMINISTRATION | | --------------------------------------------------------------------------- | | AIRCRAFT: | REVISION NO: 6 a | PAGE: | | | | | | DORNIER 228-100/101/200/201/202/212 | DATE: 12/18/95 | 34-6 | | --------------------------------------------------------------------------- | | 1. | 2. NUMBER INSTALLED | | SYSTEM & | -------------------------------------------- | | SEQUENCE ITEM | | 3. NUMBER REQUIRED FOR DISPATCH | | NUMBERS | | --------------------------------------- | | ------------------------- | | | 4. REMARKS OR EXCEPTIONS | | 34 NAVIGATION | | | | | | | | | | | | | | | 4) Test Mode A | 1 | 0 | (O)May be inoperative provided: | | | | | | | | | | | a) Alternate procedures are | | | | | | established and used, and | | | | | | b) Repairs are made within | | | | | | two flight days. | | | | | | | | 5) Glideslope B | 1 | 0 | | | | Deviation Mode | | | | | | | | | | | 6) Advisory C | - | 0 | (O)May be inoperative provided | | | Callouts | | | alternate procedures are | | | | | | established and used. | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | ------------------------------------------------------------------------------- ------------------------------------------------------------------------------- | U.S. DEPARTMENT OF TRANSPORTATION | | | | MASTER MINIMUM EQUIPMENT LIST | | FEDERAL AVIATION ADMINISTRATION | | --------------------------------------------------------------------------- | | AIRCRAFT: | REVISION NO: 6 a | PAGE: | | | | | | DORNIER 228-100/101/200/201/202/212 | DATE: 12/18/95 | 34-7 | | --------------------------------------------------------------------------- | | 1. | 2. NUMBER INSTALLED | | SYSTEM & | -------------------------------------------- | | SEQUENCE ITEM | | 3. NUMBER REQUIRED FOR DISPATCH | | NUMBERS | | --------------------------------------- | | ------------------------- | | | 4. REMARKS OR EXCEPTIONS | | 34 NAVIGATION | | | | | | | | | | | | | | | CARGO ONLY-SINGLE | | | | | PILOT ONLY | | | | | | | | | | 1. Airspeed Indicator B | 2 | 1 | May be inoperative on right side | | | | | provided: | | | | | | | | | | a) Copilot's pitot system is | | | | | functioning normally,and | | | | | | | | | | b) A functioning pneumatic | | | | | indicator is installed and | | | | | available to the pilot. | | | | | | | 2. Gyroscopic Bank B | 2 | 1 | May be inoperative on right side | | and Pitch Indicator | | | provided two independent power | | System | | | sources are available to drive the | | | | | left side instrument. | | | | | | | 3. Gyroscopic B | 2 | 1 | May be inoperative on right side | | Direction Indicator | | | provided: | | System | | | | | | | | a) Magnetic compass is operative, | | | | | and | | | | | | | | | | b) Two independent power sources | | | | | are available to drive the | | | | | left side system. | | | | | | | 4. Gyroscopic B | 2 | 1 | (O)May be inoperative on either | | Directional Indicator | | | side provided: | | Slaving System | | | | | | | | a) Slaving can be disconnected, | | | | | | | | | | b) Crew can manually set | | | | | heading, and | | | | | | | | | | c) Magnetic compass is | | | | | operative. | | | | | | | | | | | ------------------------------------------------------------------------------- ------------------------------------------------------------------------------- | U.S. DEPARTMENT OF TRANSPORTATION | | | | MASTER MINIMUM EQUIPMENT LIST | | FEDERAL AVIATION ADMINISTRATION | | --------------------------------------------------------------------------- | | AIRCRAFT: | REVISION NO: 6 a | PAGE: | | | | | | DORNIER 228-100/101/200/201/202/212 | DATE: 12/18/95 | 34-8 | | --------------------------------------------------------------------------- | | 1. | 2. NUMBER INSTALLED | | SYSTEM & | -------------------------------------------- | | SEQUENCE ITEM | | 3. NUMBER REQUIRED FOR DISPATCH | | NUMBERS | | --------------------------------------- | | ------------------------- | | | 4. REMARKS OR EXCEPTIONS | | 34 NAVIGATION | | | | | | | | | | | | | | | 5. Altimeter, B | 2 | 1 | May be inoperative on right side | | Barometric Pressure, | | | provided a functioning pneumatic | | Adjustable | | | altimeter, adjustable for | | | | | barometric pressure, is installed | | | | | and available to the pilot. | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | ------------------------------------------------------------------------------- ------------------------------------------------------------------------------- | U.S. DEPARTMENT OF TRANSPORTATION | | | | MASTER MINIMUM EQUIPMENT LIST | | FEDERAL AVIATION ADMINISTRATION | | --------------------------------------------------------------------------- | | AIRCRAFT: | REVISION NO: 6 | PAGE: | | | | | | DORNIER 228-100/101/200/201/202/212 | DATE: 08/03/93 | 35-1 | | --------------------------------------------------------------------------- | | 1. | 2. NUMBER INSTALLED | | SYSTEM & | -------------------------------------------- | | SEQUENCE ITEM | | 3. NUMBER REQUIRED FOR DISPATCH | | NUMBERS | | --------------------------------------- | | ------------------------- | | | 4. REMARKS OR EXCEPTIONS | | 35 OXYGEN | | | | | | | | | | | | | | | 1. Oxygen System C | - | - | As required by FAR. | | (Passenger) | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | ------------------------------------------------------------------------------- ------------------------------------------------------------------------------- | U.S. DEPARTMENT OF TRANSPORTATION | | | | MASTER MINIMUM EQUIPMENT LIST | | FEDERAL AVIATION ADMINISTRATION | | --------------------------------------------------------------------------- | | AIRCRAFT: | REVISION NO: 6 | PAGE: | | | | | | DORNIER 228-100/101/200/201/202/212 | DATE: 08/03/93 | 52-1 | | --------------------------------------------------------------------------- | | 1. | 2. NUMBER INSTALLED | | SYSTEM & | -------------------------------------------- | | SEQUENCE ITEM | | 3. NUMBER REQUIRED FOR DISPATCH | | NUMBERS | | --------------------------------------- | | ------------------------- | | | 4. REMARKS OR EXCEPTIONS | | 52 DOORS | | | | | | | | | | | | | | | 1. Door Warning Light C | 1 | 0 | May be inoperative provided: | | | | | | | | | | a) Flight crew verifies that | | | | | passenger/cargo doors are | | | | | closed properly by an external | | | | | visual inspection prior to | | | | | each departure, | | | | | | | | | | b) Flight crew verifies that | | | | | passenger/cargo doors are | | | | | closed properly and locking | | | | | pins are in place prior to | | | | | each departure, and | | | | | | | | | | c) Flight crew verifies that | | | | | front baggage compartment | | | | | door is properly latched | | | | | and locked. | | | | | | | 2. Pilots' Door C | 2 | 1 | (O)Either may be inoperative | | Handles | | | provided: | | (inside/outside) | | | | | | | | a) The other handle is operative, | | | | | | | | | | b) The door is properly secured | | | | | in the closed position, | | | | | and | | | | | | | | | | c) For cargo only operations | | | | | in which the pilot door is | | | | | required to enter and exit | | | | | the aircraft, both door | | | | | handles must be operable. | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | ------------------------------------------------------------------------------- ------------------------------------------------------------------------------- | U.S. DEPARTMENT OF TRANSPORTATION | | | | MASTER MINIMUM EQUIPMENT LIST | | FEDERAL AVIATION ADMINISTRATION | | --------------------------------------------------------------------------- | | AIRCRAFT: | REVISION NO: 6 | PAGE: | | | | | | DORNIER 228-100/101/200/201/202/212 | DATE: 08/03/93 | 56-1 | | --------------------------------------------------------------------------- | | 1. | 2. NUMBER INSTALLED | | SYSTEM & | -------------------------------------------- | | SEQUENCE ITEM | | 3. NUMBER REQUIRED FOR DISPATCH | | NUMBERS | | --------------------------------------- | | ------------------------- | | | 4. REMARKS OR EXCEPTIONS | | 56 WINDOWS | | | | | | | | | | 1. Copilot's Bad C | 1 | 0 | (M)Copilot's bad weather window | | Weather Window Latch | | | latch may be inoperative | | *** | | | provided: | | | | | | | | | | a) Windshield deicing system is | | | | | operative. | | | | | | | | | | b) Window is secured in the | | | | | closed position, and | | | | | | | | | | c) Copilot's visibility is not | | | | | restricted. | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | ------------------------------------------------------------------------------- ------------------------------------------------------------------------------- | U.S. DEPARTMENT OF TRANSPORTATION | | | | MASTER MINIMUM EQUIPMENT LIST | | FEDERAL AVIATION ADMINISTRATION | | --------------------------------------------------------------------------- | | AIRCRAFT: | REVISION NO: 6 | PAGE: | | | | | | DORNIER 228-100/101/200/201/202/212 | DATE: 08/03/93 | 61-1 | | --------------------------------------------------------------------------- | | 1. | 2. NUMBER INSTALLED | | SYSTEM & | -------------------------------------------- | | SEQUENCE ITEM | | 3. NUMBER REQUIRED FOR DISPATCH | | NUMBERS | | --------------------------------------- | | ------------------------- | | | 4. REMARKS OR EXCEPTIONS | | 61 PROPELLERS | | | | | | | | | | | | | | | 1. Synchrophasing C | 1 | 0 | | | System | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | ------------------------------------------------------------------------------- ------------------------------------------------------------------------------- | U.S. DEPARTMENT OF TRANSPORTATION | | | | MASTER MINIMUM EQUIPMENT LIST | | FEDERAL AVIATION ADMINISTRATION | | --------------------------------------------------------------------------- | | AIRCRAFT: | REVISION NO: 6 | PAGE: | | | | | | DORNIER 228-100/101/200/201/202/212 | DATE: 08/03/93 | 73-1 | | --------------------------------------------------------------------------- | | 1. | 2. NUMBER INSTALLED | | SYSTEM & | -------------------------------------------- | | SEQUENCE ITEM | | 3. NUMBER REQUIRED FOR DISPATCH | | NUMBERS | | --------------------------------------- | | ------------------------- | | | 4. REMARKS OR EXCEPTIONS | | 73 ENGINE FUEL & CONTROL | | | | | | | | | | | | | | | 1. Fuel Totalizer C | 1 | 0 | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | ------------------------------------------------------------------------------- ------------------------------------------------------------------------------- | U.S. DEPARTMENT OF TRANSPORTATION | | | | MASTER MINIMUM EQUIPMENT LIST | | FEDERAL AVIATION ADMINISTRATION | | --------------------------------------------------------------------------- | | AIRCRAFT: | REVISION NO: 6 | PAGE: | | | | | | DORNIER 228-100/101/200/201/202/212 | DATE: 08/03/93 | 74-1 | | --------------------------------------------------------------------------- | | 1. | 2. NUMBER INSTALLED | | SYSTEM & | -------------------------------------------- | | SEQUENCE ITEM | | 3. NUMBER REQUIRED FOR DISPATCH | | NUMBERS | | --------------------------------------- | | ------------------------- | | | 4. REMARKS OR EXCEPTIONS | | 74 IGNITION | | | | | | | | | | | | | | | 1. 10% Speed Switch C | 2 | 0 | May be inoperative provided manual | | | | | start procedures are used. | | | | | | | 2. 55% Speed Switch C | 2 | 0 | May be inoperative provided manual | | | | | start procedures are used. | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | ------------------------------------------------------------------------------- ------------------------------------------------------------------------------- | U.S. DEPARTMENT OF TRANSPORTATION | | | | MASTER MINIMUM EQUIPMENT LIST | | FEDERAL AVIATION ADMINISTRATION | | --------------------------------------------------------------------------- | | AIRCRAFT: | REVISION NO: 6 | PAGE: | | | | | | DORNIER 228-100/101/200/201/202/212 | DATE: 08/03/93 | 77-1 | | --------------------------------------------------------------------------- | | 1. | 2. NUMBER INSTALLED | | SYSTEM & | -------------------------------------------- | | SEQUENCE ITEM | | 3. NUMBER REQUIRED FOR DISPATCH | | NUMBERS | | --------------------------------------- | | ------------------------- | | | 4. REMARKS OR EXCEPTIONS | | 77 ENGINE INDICATING | | | | | | | | | | | | | | | 1. Torque/ITT C | 2 | 0 | (O)May be inoperative provided | | Limiter | | | ITT and torque are set manually. | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | | -------------------------------------------------------------------------------