Manufacturer Maintenance Manual

found in the footer on the left hand side of each page. Manufacturer Maintenance Manual AutoGyro MTOsport MMM-MT-A_16-02-08 Part A – Introduction and Declarations Page 4 of 12 INTENTIONALLY LEFT BLANK Manufacturer Maintenance Manual AutoGyro MTOsport MMM-MT-A_16-02-08 Part A – Introduction and Declarations Page 5 of 12 Contents 0 – PREFACE ...........................................................................................................................................2 1 – INTRODUCTION ................................................................................................................................3 Revision Service ...................................................................................................................................3 Record of Revisions .............................................................................................................................3 Maintenance Concept and Eligibility ....................................................................................................7 Warnings, Caution and Notes ..............................................................................................................7 Organization and Handling of the Manual ............................................................................................8 ATA100 Numbering System .................................................................................................................8 ATA100 – Chapter Code ..................................................................................................................8 Nomenclature and Structure of Maintenance Tasks (Job Cards) ....................................................9 Page Block Code ..............................................................................................................................9 Effectivities......................................................................................................................................10 Parts List Codes – PC / PIT............................................................................................................10 Abbreviations and Acronyms ..............................................................................................................11 Service Bulletin (SB) and Airworthiness Directives (AD) ...................................................................12 Manufacturer Maintenance Manual AutoGyro MTOsport MMM-MT-A_16-02-08 Part A – Introduction and Declarations Page 6 of 12 INTENTIONALLY LEFT BLANK Manufacturer Maintenance Manual AutoGyro MTOsport MMM-MT-A_16-02-08 Part A – Introduction and Declarations Page 7 of 12 Maintenance Concept and Eligibility The maintenance concept of the MTOsport gyroplane is structured into 4 qualification levels:  Basic operational (OPR) Maintenance / Pilot Checks and Servicing  Line (LNE) Maintenance (inspection of Critical Parts (CP) included)  Heavy (HVY) Maintenance (Flight Safety Sensitive Maintenance Tasks, handling of CPs)  Specialized (SPC) Level Tasks (Major Modification, Repair & Overhaul, Special Topics) The respective maintenance level for each maintenance task is printed in right hand position in the header line on each Job Card as three-letter code for quick reference (see red circle in example below) and repeated under ‘GENERAL, REFERENCES AND REQUIREMENTS’. Maintenance tasks may be carried out solely by persons or organizations fulfilling the requirements for personal qualification, infrastructure and required equipment, and only in strict compliance with the documentation and manuals listed in below table. Examples are provided for better illustration: Level Qualification Documentation Example OPR Licensed Pilot or trained/briefed person Pilot’s Operating Handbook and Job Cards marked ‘OPR’ Check and replenish engine coolant. LNE AutoGyro maint. course (and organization approval) ‘Line’ Manufacturer Maint. Manual (MMM) Job Cards ‘LNE’ All tasks to perform a 100 hrs inspection HVY AutoGyro maint. course and organization approval ‘Heavy’ Manufacturer Maint. Manual (MMM) Job Cards ‘HVY’ Adj. / replace rotor head, flight controls SPC AutoGyro special courses and org. approval ‘Specialized’ MMM Job Cards ‘SPC’ and manufacturer instructions Main frame overhaul, major mod., repair Warnings, Caution and Notes This manual uses WARNINGs, CAUTIONs and NOTEs in bold italic letters to indicate especially critical and important instructions. The call-outs appear at the top of the Maintenance Job Card if of general nature or applicable for the complete task, or will directly precede the individual Work Step. The meaning of each call-out is defined below: WARNING: A warning means that the neglect of the appropriate procedure or condition could result in personal injury or fatal accidents. CAUTION: A caution means that the neglect of the appropriate procedure or condition could result in damage to or destruction of equipment. NOTE: A note stresses the attention for a special circumstance, which is essential to emphasize. Manufacturer Maintenance Manual AutoGyro MTOsport MMM-MT-A_16-02-08 Part A – Introduction and Declarations Page 8 of 12 Organization and Handling of the Manual This manual is structured according to ATA100 numbering system. The numbering system will be explained later in more detail. On document level, the manual is subdivided into 6 parts, named A to F. The designation and content of each part is listed below: Part Designation / Content A Introduction and Declarations This section. Explains the basic concept, handling of this manual, its structure according to the ATA100 numbering system, abbreviations and acronyms. B Master Servicing Manual (ATA Chapters 00 to 20) General description of the aircraft, basic definitions and standard procedures, tools, spares, airworthiness limitations, time limits, inspections and checks. Briefly, part B describes ‘what is to be done, and when’. C System Description Section (ATA Chapters 21 to 90) Part C describes all aircraft systems, following the ATA100 numbering system. D Diagrams and Charts Part D contains diagrams and charts, if necessary in special sizes or as fold-outs. E Maintenance Job Cards [Maintenance] Job Cards are collected in Part E. Note that the footer of Part E does not spell out to the part’s designation, but just shows part and the job index of the referred maintenance task according to the ATA100 numbering system. Briefly, Part E describes ‘how something has to be done’. (F) Protocols and Forms Protocols and forms, such as maintenance check lists, are available for download. ATA100 Numbering System ATA100 – Chapter Code The Air Transport Association (ATA) Standard 100 numbering system is a widely accepted standard that provides a 6 digit numbering system to identify aircraft systems, subsystems and individual components in a structured, hierarchical approach. The first or leftmost pair of digits defines the Chapter, respectively system. The next pair of digits refers to the subsystem. The third pair of digits specifies a unit. Only complex systems use unit numbers. In case of simple systems, all information is contained in the main chapter and there is no subsystem or unit breakdown. The ATA100 numbering system and the corresponding system designations were adopted where ever possible and rational. In some cases the wording and nomenclature was adapted to match the design specifics of a gyroplane in best possible way. Due to its high degree of system integration, some systems cannot clearly be assigned to a single function. In this case the system or component was categorized by its main function. Example: the pneumatic trim cylinder also acts as brake in its secondary function. Chapter 02 has been modified to contain “TOOLS, SPARES AND CONSUMABLE MATERIALS”. Manufacturer Maintenance Manual AutoGyro MTOsport MMM-MT-A_16-02-08 Part A – Introduction and Declarations Page 9 of 12 Nomenclature and Structure of Maintenance Tasks (Job Cards) Part E of this manual describes maintenance tasks to be performed by a qualified person in order to check, inspect, replenish, adjust, replace, repair, clean, or to identify malfunctions. Each Task is outlined in detail in a [Maintenance] Job Card. Each [Maintenance] Job Card (sometimes referred to as Task Card) consists of  Task Description (header, descriptive text) with task level in most right position  a section referring to GENERAL, REFERENCES AND REQUIREMENTS  a section listing SPECIAL TOOLS AND CONSUMABLE MATERIALS  a section pointing out PRECAUTIONS AND SAFETY MEASURES  a section called PROCEDURES, which lists all Work Steps to be performed subsequently  a PARTS LIST listing part numbers and associated information, and  explanatory GRAPHICS, such as explosion drawings or photographs For ease of navigation each page in Part E shows a unique job index in the page footer consisting of 3 elements:  Chapter Code (acc. to ATA100, see explanation below)  Page Block Code (distinct index/number per type of maintenance action, see explanation below)  Sub-Index Page Block Code The pages within a chapter are structured and numbered according to the page block numbering system as specified below: Subject Code Introduction / Description and Operation 0 Fault Isolation / Trouble Shooting 1 Maintenance Procedures 2 Servicing 3 Removal / Installation / Disassembly / Assembly 4 Adjustment / Test 5 Inspection 6 Cleaning / Painting 7 Repair / Replacement / Retrofit / Modification 8 Storage 9 Manufacturer Maintenance Manual AutoGyro MTOsport MMM-MT-A_16-02-08 Part A – Introduction and Declarations Page 10 of 12 Effectivities A job card may contain information relating to different versions of the referred aircraft. This may be stipulated by optional equipment installed, by different design states (Serial Number driven), or modification (MI, AD). The keyword EFFECTIVITY, followed by a term describing its applicability, marks the start of instructions that apply exclusively to a specified version. Examples: EFFECTIVITY: Variable Pitch Propeller The following instructions must be performed and are applicable only if a Variable Pitch Propeller is installed EFFECTIVITY: up to S/N 0123 The following instructions apply to serial numbers 0123 and before EFFECTIVITY: S/N 0124 to S/N 0248 The following instructions refer only to serial numbers 0124 up to, and including, 0248 EFFECTIVITY: S/N 0124 and subsequent The following instructions must be performed for serial numbers starting 0124 and subsequent EFFECTIVITY: before MI 2011-99 Instructions refer to modification state before/without the referenced MI implemented EFFECTIVITY: MI 2011-99 accomplished Instructions apply only to those versions where the referenced MI has been accomplished The end of the range of validity is marked by the term EFFECTIVITY – END In case the effectivity solely comprises of the subsequent work step, or another effectivity statement is introduced, the term EFFECTIVITY – END will be omitted. Instructions outside of EFFECTIVITY statements apply to the standard model, respectively to all versions. Parts List Codes – PC / PIT Parts Lists specify PC (Procurement Code) and PIT (procure item through) for each item (see example). The procurement code may show L0, L1, L2 or L3 as explained below. L0 Part/Assembly available for purchase for a registered pilot/operator (OPR) L1 Part/Assembly orderable for individuals/organizations qualified to perform Line Maint. L2 Part/Assembly orderable for organizations qualified to perform Heavy Maintenance L3 Part/Assembly orderable for organizations qualified to perform Specialized Level tasks ‘PIT’ lists the order number of the part, bundle, set, or smallest assembly in which the referred part is contained. Manufacturer Maintenance Manual AutoGyro MTOsport MMM-MT-A_16-02-08 Part A – Introduction and Declarations Page 11 of 12 Abbreviations and Acronyms In this manual, a minimum number of abbreviations are used. Where possible the abbreviations and acronyms used correspond with regulations and common standards. AD Airworthiness Directive ATA Air Transport Association CHT Cylinder Head Temperature CP Critical Part CRP Carbon Reinforced Plastic DOM Date of Manufacture ELT Emergency Locator Transmitter FOD Foreign Object Damage (Debris) GRP Glass Reinforced Plastic hrs hours i.f.d. in flight direction JNP Jahresnachprüfung (annual inspection, annual airworthiness review) LED Light Emitting Diode LH left hand LR Limited reusability (Parts or components that can be used only once or a limited number of times, such as self-locking nuts, split pins, …) LTA Lufttüchtigkeitsanweisung (AD, issued by the Airworthiness Authority) MAP Manifold Absolute Pressure MI Manufacturer Information [Letter] (dt. Herstellerinformation) MLL Manufacturer Life Limit MMM Manufacturer Maintenance Manual N/A not applicable NPI non procurable item OAT Outside Air Temperature PC Procurement Code PIT procure item through POH Pilot’s Operating Handbook Qty. Quantity RBT Rotor Bearing Temperature rcv receive rec. recommended RH right hand RPM Revolutions Per Minute SB Service Bulletin SoC Statement of Compliance sqm square metre(s) STP Stückprüfung (C of A, i.e. conformity of airworthiness) TADS Type Approval Data Sheet (dt.: Geräte-Kennblatt) TBO Time Between Overhaul VPP Variable Pitch Propeller VSI Vertical Speed Indicator xmt transmit yr year(s) Manufacturer Maintenance Manual AutoGyro MTOsport MMM-MT-A_16-02-08 Part A – Introduction and Declarations Page 12 of 12 Service Bulletin (SB) and Airworthiness Directives (AD) Service Bulletin (SB), old designation Manufacturer Information [Letters] (MI) (Herstellerinformationen) or Airworthiness Directives (AD) will be incorporated into the Maintenance Manual with the next revision Manufacturer Maintenance Manual AutoGyro MTOsport MMM-MT-B_14-11-19 Part B – Master Servicing Manual (Ch. 00 – 20) Page 1 of 24 Contents CHAPTER 00 - INTRODUCTION / AIRCRAFT GENERAL .....................................................................3 General .................................................................................................................................................3 CHAPTER 01 - GENERAL .......................................................................................................................4 01-11-00 Definitions, Terms and Standard Procedures ..................................................................4 01-12-00 Standard Bolt Torques ......................................................................................................6 01-21-00 Standard Commercial Tools .............................................................................................6 01-91-00 Conversion Tables ............................................................................................................7 CHAPTER 02 - TOOLS, SPARES AND CONSUMABLE MATERIALS ...................................................9 02-51-00 Consumable Materials ......................................................................................................9 CHAPTER 03 - MINIMUM EQUIPMENT REQUIREMENT ....................................................................10 CHAPTER 04 – MANUFACTURER LIFE LIMITATIONS .......................................................................11 CHAPTER 05 - TIME LIMITS, INSPECTIONS & CHECKS ...................................................................12 05-10-00 Time Limits .....................................................................................................................12 05-20-00 Scheduled Inspections & Checks ...................................................................................13 Daily / Pre-Flight Check ..................................................................................................................13 Complementary / Servicing Tasks ..................................................................................................13 25 hrs Inspection (one-time / non-recurrent) ..................................................................................13 100 hrs / Annual Inspection ............................................................................................................13 05-21-00 Temporary Scheduled Inspections & Checks ................................................................13 05-30-00 Unscheduled Inspections ...............................................................................................14 05-50-00 Conditional Inspections ..................................................................................................14 05-51-00 Inspections - Special Operational Conditions .................................................................14 Operation in sand or dust ...............................................................................................................14 Winter operation .............................................................................................................................14 05-55-00 Inspections - Special Operational Incident .....................................................................15 Suspected hard landing ..................................................................................................................15 Rotor contact with obstacle ............................................................................................................15 Propeller contact with obstacle or external impact .........................................................................15 Birdstrike .........................................................................................................................................15 Lightning strike ...............................................................................................................................16 05-60-00 Ground Test Run ............................................................................................................16 05-70-00 Functional Test Flight .....................................................................................................16 05-90-00 Maintenance Records & Aircraft Logs ............................................................................16 CHAPTER 06 - DIMENSIONS & AREAS ...............................................................................................17 CHAPTER 07 - LIFTING / JACKING / SHORING ..................................................................................18 CHAPTER 08 - LEVELING & WEIGHING .............................................................................................18 CHAPTER 09 - TOWING & TAXIING ....................................................................................................18 CHAPTER 10 - PARKING, STORAGE & RETURN TO SERVICE ........................................................18 CHAPTER 11 - PLACARDS & MARKINGS ...........................................................................................19 CHAPTER 12 - SERVICING ..................................................................................................................21 12-10-00 Cleaning ..........................................................................................................................21 12-20-00 Lubrication ......................................................................................................................21 Lubrication: Teeter hinge ................................................................................................................21 Lubrication: Pre-rotator drive coupling sleeve ................................................................................21 Lubrication: Pre-rotator belt and pulleys .........................................................................................21 12-30-10 Servicing: Engine Air Filter .............................................................................................21 12-30-20 Servicing: Tire Pressure .................................................................................................22 12-30-30 Servicing: Battery............................................................................................................22 12-30-40 Servicing: Engine Coolant ..............................................................................................22 12-40-00 Replenishing/Replacement of Fluids ..............................................................................22 Manufacturer Maintenance Manual AutoGyro MTOsport MMM-MT-B_14-11-19 Part B – Master Servicing Manual (Ch. 00 – 20) Page 2 of 24 CHAPTER 13-17 – UNASSIGNED / N/A ...............................................................................................22 CHAPTER 18 – VIBRATION & NOISE ANALYSIS ...............................................................................23 CHAPTER 19–20 – UNASSIGNED / N/A ..............................................................................................24 Manufacturer Maintenance Manual AutoGyro MTOsport MMM-MT-B_14-11-19 Part B – Master Servicing Manual (Ch. 00 – 20) Page 3 of 24 CHAPTER 00 - INTRODUCTION / AIRCRAFT GENERAL General The MTOsport is a ‘new generation’ gyroplane with 3-bladed push propeller and a 2-blade aluminium main rotor system with swivelling rotor head. It features an open-cockpit fuselage with two seats in tandem configuration. The load carrying frame consists of inert-gas welded stainless steel square tubing. Fuselage and stabilizer with rudder are made from glass fibre reinforced (GRP) plastic. The tricycle gear with GRP (glass fibre reinforced plastic) suspension bow features a steerable nose gear. Rotor flight control consists of conventional linkage using push-rods while the rudder is controlled by cables. Manufacturer Maintenance Manual AutoGyro MTOsport MMM-MT-B_14-11-19 Part B – Master Servicing Manual (Ch. 00 – 20) Page 4 of 24 CHAPTER 01 - GENERAL 01-11-00 Definitions, Terms and Standard Procedures The following definitions, procedures and words with special meanings are used in this manual: adjust To put in specified position or condition, usually using tools or devices Example: Adjust the clearance to 1 mm Check (noun) A set of check items to be performed. Example: pre-flight check check (verb) To make sure that the item is present and/or a given requirement is fulfilled. No tools are required. Example: Warning Lights…Check NONE Critical Part (CP) “Critical Parts” are those parts whose failure during ground or flight operation could have a disastrous effect on the gyroplane. dent Depression in a surface having area and depth with no sharp edges (see also ‘nick’) discard Put away in order to exclude inadvertent or intentional re-use of the item. Comply with FOD procedures. dispose of Discard item or substance while employing strict procedures, such as environmental or legal requirements. hand-tighten Use the bare hand without any tools, gloves or extra efforts inspect / examine To look carefully at an item and compare with its standard or specification. Tools or devices may be needed. The condition may be explicitly specified (example: no corrosion). Generally, or if not otherwise stated, inspect/examine means: Make sure that the item - is complete - is correctly attached - has no loose parts - shows no signs of leaks - is not cracked or damaged - is not worn Make sure that - the surface protection is not damaged - all locking devices are installed correctly Make sure that items such as pipes, hoses and cables - look serviceable - do not rub against other items For log books and other technical records: - find pending faults - make sure they are up-to-date and correctly maintained Inspection Maintenance procedure to be performed as described in this manual. Example: 100 hrs / Annual Inspection maintenance Any one or combination of overhaul, repair, inspection, replacement, modification or defect rectification of an aircraft or component, with the exception of pre-flight inspection Manufacturer Maintenance Manual AutoGyro MTOsport MMM-MT-B_14-11-19 Part B – Master Servicing Manual (Ch. 00 – 20) Page 5 of 24 measure To find out dimensions, capacity or quantity of something. Except for counting of smaller numbers, calibrated measurement devices are needed. monitor To watch a parameter or item over a certain period of time in order to read an exact value, derive a trend or identify a change caused by an event. Example: monitor rotor speed indication, monitor RPM drop, … nick A dent with sharp edges (see also ‘dent) re-torque Refer to procedure ‘torque-tighten’. In contrary to procedure ‘torque check’ attachment hardware may rotate during re-torquing. Record (noun) Technical name for a documentation that shows the accomplishment of maintenance tasks or other activities, usually stating the responsible person’s name and date of compliance. record (verb) To make an (official) entry in a maintenance record. remove securing hardware Cut open and remove split pins, lock wire, and such. Wear eye protection. Hold securing hardware with other hand to prevent particles from darting around. Collect all splinters and particles of securing hardware and discard. replace To remove an unserviceable item and install a serviceable in the same location servicing Simple tasks such as lubrication and cleaning, checking and adjusting of air tire pressure, replenishing of fluids set To change (or verify) status of equipment to a given parameter, condition or mode. Example: set altimeter sub-scale to 1013 hPa torque-check Refer to procedure ‘torque-tighten’. Check with the (minimum) torque value supplied. Attachment hardware must NOT turn! If rotation of attachment hardware was noticeable the torque check FAILED. Refer to procedure described in Job Card. torque-tighten Use a calibrated tool with the correct range and handle properly and carefully. Set tool to minimum torque (if min. and max. torque values are provided). Use stretched fingers at the long end of the tool and counterhold directly at the pivot point. Click-Type: Stop upon the first clicking. If multiple clicking is heard or further rotation is suspected, open/unscrew and repeat. Replace attachment hardware if appropriate. In order to align attachment hardware (for example in case of a split pin) adjust tool to the maximum allowed torque and tighten carefully until hardware aligns. NO clicking must be heard! If clicking was heard, redo the complete procedure while trying different attachment hardware and/or in different installation position. verify Check that a certain dimension or condition, or set of these, is in-line with given specifications. In order to do so, a special (measurement) procedure will be required and the reference to comply with will be specified. If not otherwise stated the following standards are based on aeronautical regulations and recommendations (AC43.13-1B), industry and safety standards, and general practices, and shall be applicable throughout this manual. Examples are:  Torquing  Securing (handling of lockwire and other securing hardware)  Removal of securing hardware  FOD (foreign object damage) protection  Discard and disposal procedures  Handling of hazardous material  Workplace safety Manufacturer Maintenance Manual AutoGyro MTOsport MMM-MT-B_14-11-19 Part B – Master Servicing Manual (Ch. 00 – 20) Page 6 of 24 01-12-00 Standard Bolt Torques Standard torques are M4 2-3 Nm, M5 5-6 Nm, M6 11 +/-1 Nm, M8 25 +/-3Nm, M10 35 +/-4Nm. Always assess the joint to be tightened and use engineering judgement – do not overtighten plastic or unsupported tube joints! 01-21-00 Standard Commercial Tools Most maintenance tasks on the MTOsport can be conducted using standard, commercially available metric tools. In addition, the following standard commercial tools are required:  Inclinometer (digital) / Digital spirit level with angle gauge  Spring balance / Dynamometer  Tensiometer (to measure cable tension)  1m aluminium ruler  Fuel hose clamp  Torque wrench (in required torque ranges)  Multimeter  3 m-tape measure  Torch light  Tyre pressure gauge / tyre filling device Manufacturer Maintenance Manual AutoGyro MTOsport MMM-MT-B_14-11-19 Part B – Master Servicing Manual (Ch. 00 – 20) Page 7 of 24 01-91-00 Conversion Tables LENGTH / DISTANCE Multiply by to obtain / Multiply by to obtain m (metre) 3.28 ft (feet) 0.305 m mm (millimetre) 0.039 in (inch) 25.4 mm km (kilometre) 0.54 nm (nautical mile) 1.852 km SPEED Multiply by to obtain / Multiply by to obtain m/s (metre per second) 196.85 ft/min (feet per minute) 0.0051 m/s km/h (kilometre per hour) 0.54 kts (knots) 1.852 km/h km/h (kilometre per hour) 0.62 mph (miles per hour) 1.61 km/h PRESSURE Multiply by to obtain / Multiply by to obtain hPa (hectopascal) 1.0 mbar (millibar) 0.0001 bar bar (Bar) 14.50 psi (lb per square inch) 0.0689 bar bar (Bar) 0.0295 inHg (inch mercury) 33.864 bar FORCE / WEIGHT Multiply by to obtain / Multiply by to obtain N (Newton) 2.205 lbf (pound force) 0.4536 N N (Newton) 0.1019 (respective force of 1 kg) 9.81 N MASS (WEIGHT) Multiply by to obtain / Multiply by to obtain kg (kilogram) 2.2046 lb (pound) 0.4536 kg VOLUME Multiply by to obtain / Multiply by to obtain l [or ltr] (Litre) 0.2642 US gal (US gallons) 3.7854 l/ltr l [or ltr] (Litre) 1.057 US qts (US quarts) 0.946 l/ltr l [or ltr] (Litre) 0.0164 in3 (cubic inch) 0.946 l/ltr TORQUE Multiply by to obtain / Multiply by to obtain Nm (Newton metre) 0.738 lbf.ft. (pound-foot) 1.3558 Nm Nm (Newton metre) 0.113 lbf.in. (pound-inch) 8.851 Nm kgmm 0.0098 Nm 101.94 kgmm Manufacturer Maintenance Manual AutoGyro MTOsport MMM-MT-B_14-11-19 Part B – Master Servicing Manual (Ch. 00 – 20) Page 8 of 24 Celsius-Fahrenheit Conversion Chart -150 -100 -50 0 50 100 150 200 250 300 350 400 450 500 -100 -75 -50 -25 0 25 50 75 100 125 150 175 200 225 250 Fahrenheit - °F Celsius - °C Manufacturer Maintenance Manual AutoGyro MTOsport MMM-MT-B_14-11-19 Part B – Master Servicing Manual (Ch. 00 – 20) Page 9 of 24 CHAPTER 02 - TOOLS, SPARES AND CONSUMABLE MATERIALS 02-51-00 Consumable Materials Consumable Material (CM) referenced throughout this Maintenance Manual is coded AG-XXX-NN where NN is a consecutive number and XXX represents the material code according to the classification listed below: Class Description Class Description BAS BONDING, ADHESIVES AND SEALANTS LUB LUBRICANTS CCM CHEMICAL CONVERSION MAT. MSC MISCELLANEOUS CLA CLEANING AGENTS OIL OILS CPA CORROSION PREVENTIVE AGENTS PNT PAINT AND LACQUERS FUE FUELS PRM PRIMER, PREPARATION FOR PAINTING GRS GREASES PRS (STORAGE) PRESERVATION HYF HYDRAULIC FLUIDS The following consumable materials are referenced in the Maintenance Manual: CM-Item Material / Description AutoGyro Order Codes AG-BAS-01 Loctite 221 red 88-00-00-S-30487 AG-BAS-02 Loctite 243 blue 88-00-00-S-30483 AG-BAS-03 Loctite 542 red 88-00-00-S-30488 AG-BAS-04 Loctite 638 green 88-00-00-S-30485 AG-CPS-01 ‘Hohlraumspray’ 88-00-00-S-34197 AG-GRS-01 Silicon grease Lagermeister 2002 88-00-00-S-30477 AG-LUB-01 Ballistol Öil Universal 88-00-00-S-31816 (5L can 88-00-00-S-31846 (2ml injection syringe) 88-00-00-S-31847 (5ml injection syringe) AG-LUB-02 Aluminium Anti-Seize Spray 88-00-00-S-31590 AG-LUB-03 HHS 2000 88-00-00-S-30476 AG-LUB-04 Silicon Spray 88-00-00-S-30490 AG-OIL-01 Öl Shell Advance AX7 10W- 40 API SG 1-L 88-00-00-S-31665 Manufacturer Maintenance Manual AutoGyro MTOsport MMM-MT-B_14-11-19 Part B – Master Servicing Manual (Ch. 00 – 20) Page 10 of 24 CHAPTER 03 - MINIMUM EQUIPMENT REQUIREMENT In accordance with the Pilot’s Operating Handbook (POH) Section 2.11 the following equipment must be operative for flight Air speed indicator Altimeter Compass Rotor RPM indicator Engine instruments (oil pressure, oil temperature, RPM, CHT) HOBBS meter Pre-rotator Depending on the equipment state or relevant condition a limited or restricted operation may be granted to facilitate maintenance efforts and operability. Equipment / System Condition Limitation/Restriction Compass Defective Local flights within the traffic pattern and with ground reference. Rotor RPM indicator Defective Flight to a maintenance facility. Pre-rotator Defective / No function R-RPM indicator working Flight to a maintenance facility under the following conditions:  Experienced pilot as sole occupant  Concrete/asphalt runway with a minimum of 5 times the normal required take-off roll distance available  Second briefed person ‘handpropping’ the rotor while engine/propeller is off  Steady, laminar headwind Pre-rotator Malfunction, R-RPM > 120 R-RPM indicator working Flight to a maintenance facility under the following conditions:  Experienced pilot  Concrete/asphalt runway with a minimum of 3 times the normal required take-off roll distance available  Steady, laminar headwind Manufacturer Maintenance Manual AutoGyro MTOsport MMM-MT-B_14-11-19 Part B – Master Servicing Manual (Ch. 00 – 20) Page 11 of 24 CHAPTER 04 – MANUFACTURER LIFE LIMITATIONS For the safe operation over the specified lifecycle of the aircraft and liability reasons the following manufacturer limitations shall apply. In case the component has an operating hours and calendric time limit the first limit shall apply. Note that at expiration of the specified manufacturer life limit (MLL) the component shall be replaced for your own safety, independent of its condition. ATA Equipment / System MLL 24-30-00 Battery See manufacturer 25-10-00 Seat belts 10 yrs 25-60-00 ELT Battery See manufacturer 28-20-00 Fuel filter 200 hrs / 2 yrs 28-20-00 Fuel pumps 5 yrs (R912) 28-20-00 Primary fuel pump 1000 hrs (R914) 62-00-00 Rotor System I 1500 hrs 62-00-00 Rotor System II 2500 hrs 62-31-00 Rotor main bearing 1500 hrs 62-32-00 Gimbal head bolts 1500 hrs / 5 yrs 71-20-00 Engine mounting bushings 1500 hrs / 5 yrs Status and lifetimes of components, liquids and fluids is listed in the Event and Configuration Log (AG- F-ECL) form. The initial Event and Configuration Log is delivered with the gyroplane by AutoGyro. An empty form is provided for download on the AutoGyro web site. Manufacturer Maintenance Manual AutoGyro MTOsport MMM-MT-B_14-11-19 Part B – Master Servicing Manual (Ch. 00 – 20) Page 12 of 24 CHAPTER 05 - TIME LIMITS, INSPECTIONS & CHECKS For safe operation and continued airworthiness over the specified lifecycle of the aircraft the following inspection schedule shall apply. Note that specified tolerances must NOT be accumulated! Task Interval Recurrence Tolerance Daily / Pre-Flight Check Before flight / daily Each N/A Complementary / Servicing Tasks 5 hrs (rec.) Each N/A 25 hrs Inspection 25 hrs Once +/- 5 hrs 100 hrs / Annual Inspection 100 hrs / 1 yr Each +/- 10 hrs The 25 hrs inspection has to be performed once, within the specified tolerance. The 100 hrs inspection has to be performed every 100 hours, within the specified tolerance, at latest within 12 months, counted from issue of the aircraft’s Statement of Compliance (Stückprüfung) or Annual Inspection (JNP). Note that tolerances do not accumulate! However, a preponed (earlier) inspection outside the tolerance will reduce the next inspection due cycle accordingly. (Total aircraft hours, counted from engine start to engine shut-down, i.e. HOBBS meter) 05-10-00 Time Limits In addition to time limits for inspection items and checks the following time limits for inspection or overhaul of respective components or replacement of liquids and fluids apply. Please refer also to the engine manufacturer’s manual and time limits specified herein, as well as CHAPTER 04 - Airworthiness Limitations! Components ATA/Ref. Equipment / System Time Limit 53-00-00 Welded Steel Mainframe on condition Liquids and Fluids ATA/Ref. Equipment / System Time Limit 75-00-00 Engine coolant (acc. to coolant manufacturer) at latest 5 years 79-00-00 Engine oil (acc. to engine manufacturer) at latest 100 hrs Refer to CHAPTER 12 concerning replenishing/replacement procedures and types of liquids and fluids. Status and lifetimes of components, liquids and fluids is listed in the Event and Configuration Log (AG- F-ECL) form. It is the obligation of the maintenance facility to keep this form current. An empty form is provided for download on the AutoGyro web site. Manufacturer Maintenance Manual AutoGyro MTOsport MMM-MT-B_14-11-19 Part B – Master Servicing Manual (Ch. 00 – 20) Page 13 of 24 05-20-00 Scheduled Inspections & Checks Daily / Pre-Flight Check All daily or pre-flight check list items consist of visual checks and do not replace professional mechanical inspection and maintenance. The Daily / Pre-Flight Checklist for the standard MTOsport gyroplane is provided in the current Pilot’s Operating Handbook. Note that there is no ‘post-flight’ inspection mentioned. It is reasonable, however, to perform parts of the pre-flight inspection after the last flight of the day in order to take maintenance action in advance, if necessary. Complementary / Servicing Tasks The following tasks have to be performed in-between 100hrs inspections and may be performed on an operational level by the pilot or a trained person. Task Interval Tolerance Lubrication: Teeter hinge (see Ch. 12 – Servicing) 5 hrs (rec.) N/A Lubrication: Pre-rotator drive coupling sleeve as req. N/A Lubrication: Pre-rotator belt and pulleys as required N/A Cleaning/replacement: Engine air filter as req. N/A 25 hrs Inspection (one-time / non-recurrent) The inspection items of the 25 hrs inspection are covered within the 100 hrs inspection protocol, which is available for download. 100 hrs / Annual Inspection The maintenance protocol of the 100 hrs / Annual Inspection (AG-F-PCA-MT) is available for download. 05-21-00 Temporary Scheduled Inspections & Checks Temporary Scheduled Inspections and Checks may be introduced by MIs or AD’s (if any). Notice of, and compliance with ADs is mandatory. If necessary, AutoGyro GmbH will point out the existence of such information and will provide detailed procedures to registered service partners and owners. Important Note: Temporary scheduled inspections introduced by the engine/powerplant manufacturer will not be covered by process. As a contribution to fleet safety, AutoGyro may point out the existence of such information, if possible. Manufacturer Maintenance Manual AutoGyro MTOsport MMM-MT-B_14-11-19 Part B – Master Servicing Manual (Ch. 00 – 20) Page 14 of 24 05-30-00 Unscheduled Inspections In case of the following events or occurrences, unscheduled inspections have to be performed. Event / Occurrence / Unusual Condition Action / Reference Rotor vibration see CHAPTER 18 Propeller vibration see CHAPTER 18 If in doubt contact AutoGyro customer support. 05-50-00 Conditional Inspections Depending on the conditions the gyroplane is operated in or special operational incident the following conditional inspection may apply: 05-51-00 Inspections - Special Operational Conditions Condition Action / Reference Operation in sand or dust see below AVGAS see Pilot Operating Handbook and engine manufacturer documentation Winter operation see below Operation in sand or dust  Refer to engine manufacturer documentation  Inspect/change air filter regularly  Reduce 100 hrs inspection interval to 50 hrs  Apply propeller leading edge protection strip  Operation with keel tube fin (recommended) Winter operation The cooling system for the cylinder heads of the engine is filled with a mixture of anti-freeze and water, which gives freezing protection down to -20°C. Check protection temperature of the coolant and add anti-freeze, if necessary. If temperatures are expected to fall below protection temperature, drain the coolant, and if required for service, refill with pure antifreeze. As anti-freeze ages, renew the coolant every five years. Read the engine manual for the manufacturer’s recommendations. During winter operations the necessary operating temperature for oil and cooling agent may not be reached. This can be compensated by taping some portion of the coolers. Monitor all engine temperatures closely after having the coolers taped and modify, if necessary. When using heated clothing be aware of the electrical power demand in regard to the generator performance. Do not exceed the generator output value in order not to drain the battery. A loss of electric power affects avionics and radio communication and can lead to an engine failure in case of ROTAX 914 engine (depending on configuration). Before each flight inspect all control cables for free and easy movement and sufficient lubrication. Manufacturer Maintenance Manual AutoGyro MTOsport MMM-MT-B_14-11-19 Part B – Master Servicing Manual (Ch. 00 – 20) Page 15 of 24 05-55-00 Inspections - Special Operational Incident Event / Occurrence / Unusual Condition Action / Reference Suspected hard landing see below Rotor contact with obstacle see below Propeller contact with obstacle or external impact see below Birdstrike see below Lightning strike see below Suspected hard landing In case of a suspected hard landing perform the following checks:  Inspect nose gear, attachment, fork, linkage and wheel bearing  Inspect main gear axles and attachment  Examine possible rotor / propeller strike  see ‘Rotor / propeller contact with obstacle’  CRITICAL: Inspect main gear suspension bow (body attachment and both axle attachments ok, no cracks)  CRITICAL: Inspect fuselage, frame and attachment point for possible deformation or cracks. Perform levelling procedure (see JobCard 08-20-00 2-1)  CRITICAL: Inspect engine mounting and propeller to frame clearance approx. 5 cm  CRITICAL: Perform a rotor alignment check Defective components must be replaced. In case one or more of the items marked ‘CRITICAL’ are found defective or out of tolerance, contact AutoGyro customer support. Rotor contact with obstacle Rotor contact with obstacle include any rotor strike of the standing or turning rotor with an obstacle, including propeller and fuselage structures. In case of rotor contact with obstacle:  Perform a rotor alignment check and adjust, if necessary  Examine damage of aluminium rotor profile:  allowed damage: dent with max. depth of 1 mm  CRITICAL damage: nick(s)  In case the turning rotor hit the stabilizer/rudder, a detailed inspection of the affected components must be performed. In case CRITICAL damage is found, the rotor system must be replaced. Contact AutoGyro customer support. Propeller contact with obstacle or external impact Refer to engine manufacturer documentation. Perform tap test on propeller blades. Birdstrike  Perform detailed inspection of all affected component  If rotor blades are affected, proceed according to ‘Rotor contact with obstacle’  If propeller is affected, proceed according to ‘Propeller contact with obstacle or external impact’ Manufacturer Maintenance Manual AutoGyro MTOsport MMM-MT-B_14-11-19 Part B – Master Servicing Manual (Ch. 00 – 20) Page 16 of 24 Lightning strike A lightning is likely to have caused invisible damage to many components, especially the main rotor bearing. The aircraft must not be flown until satisfactory inspection has been undertaken and any rectification has been completed. 05-60-00 Ground Test Run The maintenance protocol of the Ground Test Run (AG-F-PGR-MT) is available for download. 05-70-00 Functional Test Flight The maintenance protocol of the Functional Test Flight (AG-F-PTF-MT) is available for download. 05-90-00 Maintenance Records & Aircraft Logs An illustrated ‘Parts List’ (AutoGyro Parts List) will be compiled individually and delivered with each gyroplane. Forms are available for download. An ‘Event and Configuration Log’ (ECL) is delivered with the aircraft by AutoGyro and shall be kept current by the maintenance facility. An empty form (AG-F-ECL) is provided for download. Manufacturer Maintenance Manual AutoGyro MTOsport MMM-MT-B_14-11-19 Part B – Master Servicing Manual (Ch. 00 – 20) Page 17 of 24 CHAPTER 06 - DIMENSIONS & AREAS Length 5.08 m Width 1.88 m Height 2.71 m Rotor diameter 8.4 m Rotor disc area 55.4 sqm Propeller diameter 1.72 m Manufacturer Maintenance Manual AutoGyro MTOsport MMM-MT-B_14-11-19 Part B – Master Servicing Manual (Ch. 00 – 20) Page 18 of 24 CHAPTER 07 - LIFTING / JACKING / SHORING See Job Card 07-00-00 2-1 in Part E of this manual. CHAPTER 08 - LEVELING & WEIGHING Weighing shall be performed in a draft-free hangar on level ground, with the aircraft defueled to minimum useable fuel. Make sure each wheel of the gyroplane is located centred on the scales. The weighing report AG-F-WRP-MT is available for download. CHAPTER 09 - TOWING & TAXIING Experience shows that aircraft may be exposed to much higher loads when operated on ground, than when in flight. Such loads caused by rumbling on rough terrain, or bouncing the aircraft over the hangar threshold may easily exceed the design load in peak. Use caution when handling the gyroplane on ground. Care must be taken when pushing at the rudder or at the outer stabilizers. Avoid excessive swing of the rotor blades as repeated bending ultimately leads to fatigue or damage. CHAPTER 10 - PARKING, STORAGE & RETURN TO SERVICE Parking up to 6 months No special measures need to be taken. NOTE Don´t let E10 remain in the fuel system for unnecessary long time or for long-term storage! Parking more than 6 months  Refer to engine manufacturer documentation  Maintain battery charged CAUTION No overwinter survival mode (snowflake) with Ctek charger MXS3.8 for Super B batteries.  Unload wheel gear  Cover aircraft with a light plastic tarpaulin or cloth Long-term Storage Contact AutoGyro Return to Service Perform a 100 hrs Inspection. Manufacturer Maintenance Manual AutoGyro MTOsport MMM-MT-B_14-11-19 Part B – Master Servicing Manual (Ch. 00 – 20) Page 19 of 24 CHAPTER 11 - PLACARDS & MARKINGS In clear view of the pilot: Only VFR day is approved Aerobatic flight prohibited! Low-G manoeuvres prohibited! Flight in icing conditions prohibited! For additional limitations see Flight Manual! In clear view of the pilot: Max. gross weight: ________ Empty weight: ________ Max. useful load: ________ At front seat: Max. weight in seat: 125 kg Min. weight in seat: 60 kg At aft seat: Max. weight in seat: 129 kg Solo from front seat only Occupant warning (front and aft seat): OCCUPANT WARNING This aircraft has not been certified to an international requirement Manufacturer Maintenance Manual AutoGyro MTOsport MMM-MT-B_14-11-19 Part B – Master Servicing Manual (Ch. 00 – 20) Page 20 of 24 At storage compartment in nose section: Max. load: 10 kg W&B must be respected! At fuel filler neck: Min. ROZ 95 AVGAS 100LL At each fuel tank: Capacity 34 litres At fuel shut-off valve (if installed): At oil filler neck: Engine Oil: ___________________ Approved oil types see engine manual! At both static ports (if installed): Static Port Do not obstruct! Manufacturer Maintenance Manual AutoGyro MTOsport MMM-MT-B_14-11-19 Part B – Master Servicing Manual (Ch. 00 – 20) Page 21 of 24 CHAPTER 12 - SERVICING 12-10-00 Cleaning Care and regular cleaning of engine, propeller, rotor system and fuselage is the basic foundation for airworthiness and reliability. Therefore, the gyroplane should be cleaned after every last flight of the day or more often, if environmental conditions dictate. In order to protect the gyroplane against dirt, dust, bird soil, and sunlight, the aircraft should be covered with a light plastic tarpaulin or cloth. Openings of the engine and airspeed indicator should be closed after the flight (insects, birds etc.). Contamination can be cleaned with clean water, possibly with mild cleaning additives. To clean the rotor it is best to soak contamination with a cloth or towel, wipe with soft or micro-fibre cloth, and rinse thoroughly with water. 12-20-00 Lubrication Component Application Reference Lubrication: Teeter hinge 5 hrs (recomm.) see below Lubrication: Pre-rotator drive coupling sleeve as required see below Lubrication: Pre-rotator belt and pulleys as required see below See CHAPTER 05 for respective time limits. Lubrication: Teeter hinge The teeter hinge consists of a steel bolt running in special Teflon coated bushings. In order to provide proper bearing action and to avoid wear and bearing play, which will cause rotor vibration in consequence, regular lubrication is essential. In order to do so, the best practise is to perform work steps 5 to 7 from Job Card 62-11-00 6-1 INSPECTION: ROTOR – TEETERING PARTS. Make sure to apply grease also on the outer (secondary) bearings inside the teeter tower. Lubrication: Pre-rotator drive coupling sleeve Apply a thin layer of lubricant AG-LUB-03 on coupling sleeve when in extended position in regular intervals, at latest when the sliding surface feels dry or after flight through rain. Lubrication: Pre-rotator belt and pulleys Spray clutch belt and pulleys with AG-LUB-04 (Silicone Spray) regularly, at latest when the clutch begins to judder! 12-30-10 Servicing: Engine Air Filter The air intake filters need to be replaced or cleaned according to the manufacturer‘s recommendation. Depending on environmental conditions, such as dust, sand, or pollution the recommended rate of maintenance should be increased as required. Manufacturer Maintenance Manual AutoGyro MTOsport MMM-MT-B_14-11-19 Part B – Master Servicing Manual (Ch. 00 – 20) Page 22 of 24 12-30-20 Servicing: Tire Pressure Main wheels 1.8 – 2.2 bar Nose wheel 1.6 – 2.0 bar NOTE: Green valve caps are used when the tire is filled with nitrogen. 12-30-30 Servicing: Battery The aircraft is fitted with a maintenance-free electrolyte battery. Maintenance is therefore limited to outside soundness, correct attachment, and cleaning. Check integrity of the battery as leaking fluid contains corrosive sulphuric acid which would lead to extensive damage when contacting the framework and attachments. Charge the battery only with a charging device which is suitable for gel electrolyte batteries. CAUTION: The battery must never be deep discharged, as it will be damaged. If so, it might need to be replaced. CAUTION: No overwinter survival mode (snowflake) with Ctek charger MXS3.8 for Super B batteries. 12-30-40 Servicing: Engine Coolant The cooling system for the cylinder heads of the engine is filled with a mixture of anti-freeze and water, which gives freezing protection down to -20°C. Check protection temperature of the coolant and add anti-freeze, if necessary. Verify coolant level in the expansion tank, replenish as required up to the top. Verify coolant level in the overflow bottle. Minimum coolant level (cold engine) in the overflow bottle is marked by the cable tie at about the lower third. If temperatures are expected to fall below protection temperature, drain the coolant, and if required for service, refill with pure antifreeze. As anti-freeze ages, renew the coolant every five years. Read the engine manual for the manufacturer’s recommendations. 12-40-00 Replenishing/Replacement of Fluids Liquid / Fluid Max. Filling Qty. Type / Code Engine coolant (50/50 water and EthyleneGlycol antifreeze suitable for aluminium engines) 3.4 ltr (dual radiators) as documented Engine Oil 3.4 ltr as documented See CHAPTER 05 for respective time limits. CHAPTER 13-17 – UNASSIGNED / N/A Manufacturer Maintenance Manual AutoGyro MTOsport MMM-MT-B_14-11-19 Part B – Master Servicing Manual (Ch. 00 – 20) Page 23 of 24 CHAPTER 18 – VIBRATION & NOISE ANALYSIS Vibration may be induced by the rotor system, the propeller or even the engine. Finding out the cause for vibration and its proper cure requires experience and special equipment. This is why vibration analysis and related maintenance can only be performed by specialized service partners (maintenance level ‘S’), or AutoGyro GmbH, Germany directly. The following tests or fault isolation procedures should be performed in order to exclude systematic errors in case of rotor vibration:  rotor system cleanliness  check/verify correct installation position of the shim washers relative to teeter block and teeter tower (one or two dot markings on block, shim washer and teeter tower must align)  check for possible play in teeter bearing in axial or radial direction  check rotor system alignment (see Job Card 62-11-00 5-1)  check for possible play in rotor bearing  adjust (increase) rotor control friction (see Job Card 62-32-00 5-1) In case of unusual vibration, contact AutoGyro or an AutoGyro specialized service partner. If possible, try to describe the type of vibration as precise as possible as this will help to save time to reproduce and troubleshoot, or even allow a first remote assessment. The following table provides a basic classification. Vibration appearance / sensation / parameter Lateral (left-right / back-forth) vibration with approximately 6 per second amplitude Vertical (up-down) vibration with approximately 12 per second amplitude Free-stick movement – carefully release control stick (if possible/safe) and describe path and displacement of control stick head Flight condition (weight, speed) with highest vibration level Rotor RPM Higher frequency vibration (around 50 Hz, like an electric razor), changing with RPM Higher frequency vibration, frequency and amplitude significantly changing with power setting, possibly irregular or erratic RPM or power setting with highest vibration levels Manufacturer Maintenance Manual AutoGyro MTOsport MMM-MT-B_14-11-19 Part B – Master Servicing Manual (Ch. 00 – 20) Page 24 of 24 Noise is mainly created by the propeller. Engine and muffler play a secondary role in noise emission, as long as intact. Any deficiencies could be easily identified by a visual inspection or tap test. A defective muffler can be refilled with insulating material. Repair as necessary. Propeller noise is emitted by the fast turning blade tips and usually increases exponentially with RPM and speed due to interaction of air disturbances with the blade tips. As noise is a subjective perception, only measurement will provide reliable data. However, the following table provides elements and countermeasure to troubleshoot and cure in case of unusual noise emission. Possible causes for noise / countermeasures Check propeller condition (cleanliness, erosion, damaged or splintered blade tips). Clean or repair propeller. Check propeller RPM during take-off (full throttle) or cruise. Adjust/reduce if required. Check/adjust propeller pitch. Check pitch setting of individual blades and adjust. Check leading edge of propeller and leading edge protection strip (if installed). A damaged leading edge protection strip (loose or sticking out end) may change noise signature significantly. Replace as necessary. Check airfilter condition and installation condition. CHAPTER 19–20 – UNASSIGNED / N/A Manufacturer Maintenance Manual AutoGyro MTOsport MMM-MT-C_14-11-19 Part C – System Description Section (Ch. 21 – 90) Page 1 of 22 Contents CHAPTER 21-22 - UNASSIGNED / N/A ..................................................................................................3 CHAPTER 23 - COMMUNICATIONS ......................................................................................................3 23-10-00 Speech Communication / Radio .......................................................................................3 23-40-00 Interphone / Intercom .......................................................................................................3 CHAPTER 24 - ELECTRICAL POWER ...................................................................................................3 24-30-00 DC Generation and Battery ..............................................................................................4 24-60-00 DC Electrical Load Distribution .........................................................................................4 CHAPTER 25 - EQUIPMENT / FURNISHINGS .......................................................................................5 25-10-00 Flight Compartment ..........................................................................................................5 CHAPTER 26 - N/A ..................................................................................................................................5 CHAPTER 27 - FLIGHT CONTROLS ......................................................................................................5 27-00-00 Flight Controls...................................................................................................................5 27-20-00 Flight Controls - Rudder ...................................................................................................5 CHAPTER 28 - FUEL ...............................................................................................................................5 28-10-00 Storage .............................................................................................................................5 28-20-00 Distribution ........................................................................................................................6 28-40-00 Indicating ..........................................................................................................................6 CHAPTER 29-30 - N/A .............................................................................................................................7 CHAPTER 31 – INDICATING SYSTEM ...................................................................................................7 31-10-00 Instruments & Control Panels ...........................................................................................7 31-60-00 Integrated Display Systems ............................................................................................11 CHAPTER 32 - LANDING GEAR ...........................................................................................................12 32-10-00 Main Gear .......................................................................................................................12 32-10-00 Nose Gear ......................................................................................................................12 32-40-00 Wheels and Brakes ........................................................................................................12 CHAPTER 33 - LIGHTS .........................................................................................................................12 33-40-00 Exterior ...........................................................................................................................12 CHAPTER 34 - NAVIGATION ................................................................................................................13 34-10-00 Flight Environment Data .................................................................................................13 34-20-00 Attitude and Direction .....................................................................................................13 34-70-00 ATC Transponder ...........................................................................................................13 CHAPTER 35 - N/A ................................................................................................................................13 CHAPTER 36 - PNEUMATIC .................................................................................................................13 36-11-00 Generation / Compressor ...............................................................................................13 36-21-00 Distribution ......................................................................................................................13 CHAPTER 37-50 - UNASSIGNED / N/A ................................................................................................14 CHAPTER 51 - STANDARD PRACTICES - STRUCTURES .................................................................14 51-00-00 Standard Practices - Structures......................................................................................14 CHAPTER 52 - DOORS, COVERS AND COWLINGS ..........................................................................14 52-10-00 Passenger / Crew ...........................................................................................................14 52-40-00 Service Covers and Cowlings .........................................................................................14 CHAPTER 53 – FUSELAGE / MAIN FRAME ........................................................................................14 CHAPTER 54 - N/A ................................................................................................................................14 CHAPTER 55 - STABILIZERS ...............................................................................................................15 55-40-00 Rudder ............................................................................................................................15 CHAPTER 56 - WINDOWS ....................................................................................................................15 56-10-00 Flight Compartment / Windshields ......................................................................................15 CHAPTER 57-60 - UNASSIGNED / N/A ................................................................................................15 CHAPTER 61 - PROPELLER ................................................................................................................16 61-10-00 Propeller assembly .........................................................................................................16 61-20-00 Controlling .......................................................................................................................16 Manufacturer Maintenance Manual AutoGyro MTOsport MMM-MT-C_14-11-19 Part C – System Description Section (Ch. 21 – 90) Page 2 of 22 CHAPTER 62 - ROTOR .........................................................................................................................16 62-11-00 Rotor – Teetering Parts ..................................................................................................16 62-31-00 Rotor Head Bridge, Bearing and Teeter Tower ..............................................................17 62-32-00 Rotor Gimbal Head .........................................................................................................17 62-41-00 Rotor RPM Monitoring ....................................................................................................17 CHAPTER 63 - ROTOR DRIVE .............................................................................................................17 63-11-00 Pre-rotator.......................................................................................................................17 63-11-10 Pre-rotator Lower Engagement ......................................................................................17 63-11-20 Pre-rotator Drive .............................................................................................................18 63-11-30 Pre-rotator Upper Engagement ......................................................................................18 63-51-00 Rotor Brake System .......................................................................................................18 CHAPTER 64-66 - N/A ...........................................................................................................................18 CHAPTER 67 - ROTOR FLIGHT CONTROL.........................................................................................18 67-05-00 Pitch Trim System / Rotor Brake ....................................................................................18 67-06-00 Roll Trim System ............................................................................................................19 CHAPTER 68-70 - UNASSIGNED / N/A ................................................................................................19 CHAPTER 71 - POWER PLANT ............................................................................................................19 71-20-00 Engine Mounts ................................................................................................................19 71-50-00 Engine Electrical Harness ..............................................................................................19 71-60-00 Engine Air Intakes...........................................................................................................19 71-70-00 Engine Drains .................................................................................................................19 CHAPTER 72 TO 74 - ENGINE RELATED ............................................................................................20 CHAPTER 75 - AIR / ENGINE COOLING ..............................................................................................20 CHAPTER 76 - ENGINE CONTROLS ...................................................................................................21 76-10-00 Power Control / Choke ...................................................................................................21 76-20-00 Engine Shutdown / Emergency ......................................................................................21 CHAPTER 77 - ENGINE INDICATING ..................................................................................................21 77-10-00 Power ..............................................................................................................................21 77-20-00 Temperature ...................................................................................................................21 77-40-00 Integrated Engine Instrument Systems ..........................................................................22 CHAPTER 78 - EXHAUST .....................................................................................................................22 78-00-00 Exhaust ...........................................................................................................................22 CHAPTER 79 - OIL SYSTEM.................................................................................................................22 79-11-00 Storage / Oil tank ............................................................................................................22 79-20-00 Distribution and Cooling .................................................................................................22 79-21-00 Oil Hoses and Lines .......................................................................................................22 79-22-00 Oil Cooler ........................................................................................................................22 79-30-00 Indicating ........................................................................................................................22