AIRPLANE MAINTENANCE MANUAL - AME Academy
AIRPLANE MAINTENANCE MANUALFor theCIRRUS DESIGN SR22SRCIRRUS DESIGN INCORPORATED4515 Taylor CircleDuluth, MN 55811FAA APPROVAL HAS BEEN OBTAINED ON THE TECHNICAL DATA IN THIS PUBLICATION THAT AFFECTS AIRPLANE TYPE DESIGN.COPYRIGHT 1999 CIRRUS DESIGN CORPORATION DULUTH, MINNESOTA, USAP/N 13773-001ISSUED Nov 2000REVISION 1 July 2001
Log of RevisionsRevisionNumber13773-00130 Nov ssueDateDateInsertedInsertedByAMM-RevLogPage 1
Log of Temporary RevisionsTRNumber13773-00130 Nov 2000Issue DateDate InsertedInserted ByDateRemovedRemoved ByAMM-TmpRevLogPage 1
INTRODUCTION1. COVERAGEThis Cirrus Design SR22 Airplane Maintenance Manual was prepared by Cirrus Design Technical Publications. This manual contains information necessary to enable a trained mechanic to inspect, service, clean,trouble shoot, functionally test, and repair systems and equipment in the Cirrus Design SR22. It alsoincludes information necessary for the mechanic to perform maintenance or make minor repair to units inthe airplane normally requiring such action on the flight line or in the maintenance hangar. This manualcovers the as delivered airplane configuration.The Cirrus Design SR22 Airplane maintenance manual was prepared using GAMA Specification #2 (Specification for Manufacturers Maintenance data), Revised September 1982 as a content model and formatguide. However, as the specification is written to cover a whole class of aircraft rather than a particularmodel, some deviations from the specification were made for clarity.This Maintenance Manual does not reflect part numbers and cannot be used for ordering replacementparts. Spares and replacement parts should be ordered using the current Cirrus Design SR22 IllustratedParts Catalog.Wiring schematics within the description and operation sections of this manual are for general informationpurposes only. Troubleshooting shall be performed using the Wiring Manual, and the optional avionics andelectrical wiring diagrams provided at delivery.2. USING THE MAINTENANCE MANUALThis Maintenance Manual is divided into four major sections, each of which is separated into chapters.Each chapter contains its own list of effective pages and table of contents.A. Page Numbering SystemPage numbers used in this Maintenance Manual consist of two-element numbers separated bydashes, under which the page number and date are printed.Whenever the chapter/system element number is followed by zeros in the section/subsystem (32-00)the information presented on the page is applicable to the entire system.The section/subsystem number is used to identify information applicable to section or subsystemswithin a chapter or system respectively. The subject/unit element number progresses from the number‘10’ in accordance with GAMA Specification No. 2 and the number of section/subsystem units covered.All system/subsystem data is page numbered separately.3. WARNINGS, CAUTIONS, AND NOTESWarnings, Cautions, and Notes are used to highlight or emphasize important points.Warnings call attention to use of materials, processes, methods, procedures, or limits which must be followed precisely to avoid bodily injury.Cautions call attention to methods and procedures which must be followed to avoid damage to equipment.Notes call attention to methods which make the procedure easier.13773-00130 Nov 2000AMM-IntroPage 1
4. LIST OF PUBLICATIONSThe following publications should be used in conjunction with this manual:Manual No.Manual Title - EngineManufactureX30568AModel IO-550 Overhaul ManualTeleydyne Continental MotorsX30634AModel IO-550 Maintenance ManualTeleydyne Continental MotorsX30569AModel IO-550 Parts CatalogTeleydyne Continental MotorsX30565Maintenance and Operator’s ManualTeleydyne Continental MotorsX30592Starter Service InstructionsTeleydyne Continental MotorsX30593AFuel Injection Systems Overhaul andParts CatalogTeleydyne Continental MotorsX40000TCM Ignition Systems Master ServiceManualTeleydyne Continental MotorsManual No.Manual Title - PropellerManufacture115NPropeller Owner’s Manual and Log Book Hartzell202AStandard Practices ManualAW-9511-2The Smooth Propeller: How to Perform a Chadwick HelmuthDynamic Propeller Balance13841-R2Chadwick Helmuth Vibrex 2000 UsersGuideManual No.Manual Title - AvionicsHartzellChadwick HelmuthManufacture8747System 55 Autopilot Pilot’s OperatingHandbookS-TEC Corporation190-00149-01GMA 340 Audio Panel Installation andOperation ManualGarmin International190-00140-02GNS 430 - 400 Series Installation Manual Garmin International190-00187-02GTX 327 Transponder Installation andOperation ManualGarmin International572-0555ICDS 2000 Operations HandbookARNAV SystemsManual No.Manual Title - MiscellaneousManufacture13772-001Pilot’s Operating HandbookCirrus Design Corporation13774-001SR22 Illustrated Parts CatalogCirrus Design CorporationPage 2AMM-Intro13773-00130 Nov 2000
Manual No.Manual Title - MiscellaneousManufacture13775-001SR22 Wiring ManualCirrus Design CorporationGSM-590Gill Battery Service ManualTeledyne9/94Model E-01 ELT Installation and Operation ManualACK TechnologiesDocument No. I-194Inspection Intervals for FiltersBrackett Aircraft Technologies5. REVISIONSThis manual has been prepared in loose-leaf form for ease in inserting revisions. Tabbed dividers, throughout the manual, are in standard GAMA format and numbering and allow quick reference to data in eachsection. Logical and convenient Tables of Contents are located at the beginning of each chapter to aid inlocating specific data within that chapter.Numbered revisions will be issued periodically. These revisions are printed on white paper and contain arevision instruction sheet to assist the user in filing the change.Upon receipt of a numbered revision, file it according to the provided instructions as soon as possible.Additionally, a record of filing must be made on the following Log of Revisions page.6. REVISION BARSChanges to data in an existing section will be identified by a revision bar in the outer margin of the page.Change bars are used in figures to indicate changes.7. TEMPORARY REVISIONSTemporary revisions are used to provide time sensitive information and changes as they become available.Temporary revisions provide, with the least possible delay, new information which assists in maintainingsafe and efficient flight/ground operations.Temporary revisions are incorporated at the next regularlyscheduled revision and become a permanent part of the Maintenance Manual.Upon receipt of a Temporary Revision, file the revision in the applicable chapter in accordance with filinginstructions that appear on the Temporary Revision. Additionally, a record of filing the Temporary Revisionmust be made in the Log of Temporary Revisions for that AMM chapter. Typically, the Log Of TemporaryRevisions for a chapter will be replaced by a blank log when a numbered revision for that chapter is issued.Temporary Revisions should be removed from this manual only when removal instructions are noted onthe regular revision summary sheet or by instructions noted on a superseding Temporary Revision.8. REVISION SERVICERevision Service for this manual is available from Cirrus Design Technical Publications at the addressbelow:Cirrus Design4515 Taylor CircleDuluth, MN 55811Phone: 218 727-2737Fax: 218 727-214813773-00131 July 2001AMM-IntroPage 3
CHAPTERAIRWORTHINESSLIMITATIONS
CHAPTER 4 - AIRWORTHINESS LIMITATIONSLIST OF EFFECTIVE PAGESChapter/SectionPageDate4-LOEP131 JULY 20014-TOC131 JULY 20014-00131 JULY 20014-00231 JULY 20014-00331 JULY 200113773-00131 July 20014-LOEPPage 1
CHAPTER 4 - AIRWORTHINESS LIMITATIONSTABLE OF CONTENTSSubjectAIRWORTHINESS nce LimitationsReplacement LimitationsStructural LimitationsDescription1112Maintenance LimitationsReplacement LimitationsStructural Limitations22313773-00131 July 20014-TOCPage 1
AIRWORTHINESS LIMITATIONS1. GENERALThe Airworthiness Limitations Section is FAA approved and specifies inspection and maintenance requiredunder paragraphs 43.16 and 91.403 of the Federal Aviation Regulations unless an alternative program hasbeen FAA approved.This chapter outlines the maximum replacement intervals and/or maintenance requirements for aircraftcomponents, systems, and structures determined to be life limited and/or require monitoring throughscheduled maintenance.Note:All time limits and requirements listed in this section are also covered in Chapter 5, TimeLimits and Maintenance Checks.The following airworthiness limitations and requirements are separated into groups as described below.A. Maintenance LimitationsComponent and system checks required to be performed during airplane scheduled maintenance.B. Replacement LimitationsListing of time limits for replacement of specific components.C. Structural LimitationsDamage Tolerant Limitations required by Federal Aviation Regulations for certification.13773-00131 July 20014-00Page 1
2. DESCRIPTIONA. Maintenance Limitations(1)The scheduled maintenance requirements listed below are also included in AMM 5-20 (Scheduled Maintenance Checks). The following criteria must be adhered to:(a) Paint FinishTo ensure that the temperature of the composite structure is kept below 150 degreesFahrenheit, the maximum allowable paint on the wing will have an absorptivity not greaterthan 0.4, with an emissivity of at least 0.9. The maximum allowable paint on the fuselagewill have an absorptivity not greater than 0.6, with an emissivity of at least 0.7. (Refer to51-30)(2)Cirrus Airframe Parachute System (CAPS) must be serviced and maintained by Cirrus Designtrained and authorized parachute system technicians only. Airframe and Powerplant license isnot sufficient credentials for performing maintenance on CAPS. Licensed Airframe and Powerplant mechanics may visually inspect the parachute installation and activation handle installationonly as specified in 5-20 (Scheduled Maintenance Checks).B. Replacement LimitationsThe replacement items under this section are also included in AMM 5-10 (Time Limits and Maintenance Checks - Overhaul and Replacement Schedule).(1)Unless otherwise specified, the following components must be replaced with new components,overhauled components, or components which have life remaining, at the intervals specified.ItemPage 2Replacement Limits1.EngineThere are no life limits on the engine or itscomponents. Refer to Chapter 5, Time Limits and Maintenance Checks, for recommended overhaul schedule.2.PropellerThere are no life limits on the propeller or itscomponents. Refer to Chapter 5, Time Limits and Maintenance Checks, for recommended overhaul schedule.3.Cirrus Airframe Parachute System (CAPS)Rocket MotorReplace with new or recharged unit every10 years. Refer to Chapter 95, Special Purpose Equipment.4.Cirrus Airframe Parachute System (CAPS)ParachuteReplace with new or repacked (inspected/repaired/repacked) unit every 10 years.Refer to Chapter 95, Special PurposeEquipment.5.Cirrus Airframe Parachute System (CAPS)Reefing Line CuttersReplace with new line cutters every 3 years.Refer to Chapter 95, Special PurposeEquipment.4-0013773-00131 July 2001
C. Structural LimitationsThe certification requirements of FAR 23.573 require that the composite airframe structure, cabin,wing, empennage their carry thru, and attaching structure whose failure would be catastrophic must bedesigned to damage tolerant criteria. Damage tolerant certification for the selected airframe life of4350 flight hours has been established for all of the affected parts with no special structural limitationsor inspections.13773-00131 July 20014-00Page 3
CHAPTERTIME LIMITS ANDMAINTENANCECHECKS
CHAPTER 5 - TIME LIMITS/MAINTENANCE PRACTICESLIST OF EFFECTIVE PAGESChapter/SectionPageDate5-LOEP131 JULY 20015-TOC131 JULY 20015-TOC231 JULY 20015-00130 NOV 20005-10131 JULY 20015-10231 JULY 20015-20130 NOV 20005-20230 NOV 20005-20331 JULY 20015-20431 JULY 20015-20531 JULY 20015-20631 JULY 20015-20731 JULY 20015-20831 JULY 20015-20931 JULY 20015-201031 JULY 20015-201131 JULY 20015-201231 JULY 20015-201331 JULY 20015-30130 NOV 20005-30230 NOV 20005-30330 NOV 20005-30430 NOV 20005-50130 NOV 20005-50230 NOV 20005-50330 NOV 20005-50430 NOV 200013773-00131 July 20015-LOEPPage 1
CHAPTER 5 - TIME LIMITS/MAINTENANCE PRACTICESTABLE OF CONTENTSSubjectTIME LIMITS AND MAINTENANCE CHECKSChapter/SectionPage5-00General1Annual Inspections1100-Hour Inspections1Unscheduled Maintenance Checks1Special Conditions - Cautionary Notice1OVERHAUL AND REPLACEMENT SCHEDULE5-10DescriptionSCHEDULED MAINTENANCE CHECKS15-20Description1Inspection Groups and Criteria1Visual InspectionMoving PartsComposite PartsMetal PartsFuel, Air, and Hydraulic Oil Lines and HosesElectrical WiringBolts and NutsFilters and ScreensWet Fuel AreasOperational InspectionFunctional InspectionScheduled Inspection Report111222222223Pre-InspectionEngine GroupPropeller GroupCabin GroupRadio GroupFuselage and Empennage GroupWing GroupLanding Gear GroupReturn to ServiceAIRPLANE OPERATIONAL AND FUNCTIONAL CHECK34779101011125-30Description1Operational Inspection Report213773-00131 July 20015-TOCPage 1
CHAPTER 5 - TIME LIMITS/MAINTENANCE PRACTICESTABLE OF CONTENTSSubjectChapter/SectionUNSCHEDULED MAINTENANCE CHECKSPage5-50Description1Hard/Overweight LandingsOverspeedSevere Air Turbulence or Severe ManeuversLightning StrikeHigh Drag/Side Loads Due to Ground HandlingMaintenance Practices111112Hard/Overweight LandingLanding GearWingsOverspeedLanding gearFuselageCowlingStabilizersWingsSevere Turbulence and/or ManeuversStabilizersWingLightning ingsPropellerPowerplantForeign Object DamageLanding gh Drag/Side Loads Due to Ground HandlingLanding GearWings2222222222233333333333333333334Page 25-TOC13773-00131 July 2001
TIME LIMITS AND MAINTENANCE CHECKS1. GENERALThis chapter outlines the recommended intervals for overhaul and replacement of components, scheduledand unscheduled maintenance, and annual inspections. The following Scheduled Maintenance Checktable shows the recommended intervals at which items are to be inspected based on normal usage underaverage environmental conditions.2. ANNUAL INSPECTIONSAs required by Federal Aviation Regulation Part 91.409, all civil airplanes must undergo a completeinspection each 12 calendar months. This inspection must be performed by an authorized maintenanceperson as described in FAR Part 43.3. A signed and dated record must be maintained as each inspectiontask is completed. When the last task of the inspection has been completed, the Inspection Report is to besigned off in the Log Book/Maintenance Record. The inspection items to be covered in the annual inspection are identical to the 100-hour inspection items.The inspection interval to the next annual inspection may not exceed twelve calendar months. For Example: If an inspection were signed off on 15 September 2005, the next annual inspection would be due andmust be accomplished no later than 30 September 2006. All subsequent annual inspection will be due inSeptember unless the schedule is reset by performing an annual inspection early.3. 100-HOUR INSPECTIONSIn addition to the annual inspection, if the airplane is operated commercially (for hire) the airplane mustalso have an inspection every 100 flight hours. The 100-hour interval between inspections should never beexceeded by more than 10 hours, and then only if additional time is required to reach a place where theinspection can be satisfactorily accomplished.Additionally, the time the interval was exceeded must be included as flight hours in the next 100-hour interval. For example: If a 100-hour inspection was due at 650 flight hours and was actually signed-off at 658flight hours, the next 100-hour inspection is due at 750 flight hours, not 758 flight hours. Inspection tolerances cannot be accumulated.4. UNSCHEDULED MAINTENANCE CHECKSAbnormal airplane operations require special maintenance checks. Definitions and inspection proceduresfor hard/overweight landings, overspeed, severe air turbulence, lightning strike, foreign object damage,and high drag/side loads due to ground handling are listed in Chapter 5-50.5. SPECIAL CONDITIONS - CAUTIONARY NOTICEAirplanes operated for Air Taxi operation or other than normal operation and airplanes operated in humidtropics or cold and damp climates, etc., may need more frequent inspections for wear, corrosion, delamination, and/or lack of lubrication. In these areas, periodic inspections should be performed until the operatorcan set his own inspection periods based on experience.Note:The recommended periods do not constitute a guarantee that the item will reach the periodwithout malfunction as in-service factors cannot be controlled by the manufacturer.“On Condition” items are to be repaired, overhauled or replaced when inspection or performance of these items reveal a potentially unserviceable or unsafe condition.The date on the “ORIGINAL STANDARD AIRWORTHINESS CERTIFICATE,” FAA Form No.8100-2, which is issued with a new airplane, is to be used as the basis for all inspected components listed in the following schedules.13773-00130 Nov 20005-00Page 1
OVERHAUL AND REPLACEMENT SCHEDULE1. DESCRIPTIONThe following components must be overhauled or replaced at the specified intervals. To ensure correctobservation of these times, the date of removal, installation, or overhaul of such components as well as theairplanes flight hours must be entered into the Service Time Record filed in the Airplane Maintenance Log.ItemIntervalReplc. O’haulNotes1. EnginePer Manufacturer.(Recommended 2000Hours) Refer to Teledyne Continental Motors ServiceLetter SIL 98-9.2. Propeller GovernorPer Manufacturer.(Recommended 2400Hours) Refer to WoodwardGovernor CompanyService Bulletin 33580F.3. MagnetosPer Manufacturer.(Recommended atEngine Overhaul)4. PropellerPer Manufacturer.(Recommended 2400Hours or 6 Years whichever comes first.) Refer to Hartzell Propeller Service Letter 61.5. Alternator 1Per Manufacturer.(Recommended 500Hours) Refer to Teledyne Continental Motors ManualNo. X30531-3.6. Alternator 2Per Manufacturer.(Recommended 1700Hours) Factory Overhaul.7. Induction Air FilterAt Annual Inspection or 200 Hours.8. Muffler and Heat Exchanger1000 Hours 9. Flexible Fuel Lines5 Years 10. Fuel System Boost Pump10 Years Refer to 28-2011. Gascolator Seals5 Years Refer to 28-2012. Fuel System Drain Valve Seals5 Years Refer to 28-1013. Flexible Oil System Lines5 Years 14. Flexible Brake System Lines5 Years 15. Aileron-Rudder InterconnectShock Cord5 Years 13773-00131 July 2001 Refer to Teledyne Continental Motors IO-550Overhaul Manual.If at any time, the filter isfound to be more than50% covered by foreignmaterial, the filter mustbe replaced.Refer to 78-20Refer to 27-205-10Page 1
Item (Continued)IntervalReplc. O’haulNotes16. Emergency Locator TransmitterBatteriesBatteries at 50 percentof useful life or after 1hour use - whichevercomes first Refer to ACK Technologies Model E-01 Installation and OperationManual.17. Fire Extinguisher20 Years Refer to Chapter 26-20.18. Cirrus Airframe Parachute System 10 Years(CAPS) Rocket Motor Replace with new unit.Refer to Chapter 95Special Purpose Equipment for CAPS maintenance practices.19. Cirrus Airframe Parachute System 10 Years(CAPS) Parachute Replace with new orrepacked unit. Refer toChapter 95, SpecialPurpose Equipment forCAPS maintenancepractices.20. Cirrus Airframe Parachute System 3 Years(CAPS) Reefing Line Cutters Replace with new unit.Refer to Chapter 95,Special Purpose Equipment for CAPS maintenance practices.CAUTION:Page 2Airplane control surface balance is critical to flight safety. Removal and/or addition of anypaint or body filler to a control surface requires that the control surface be re-balanced.(Refer to 55-00)5-1013773-00131 July 2001
SCHEDULED MA
X30592 Starter Service Instructions Teleydyne Continental Motors X30593A Fuel Injection Systems Overhaul and Parts Catalog Teleydyne Continental Motors X40000 TCM Ignition Systems Master Service Manual Teleydyne Continental Motors Manual No. Manual Title - Propeller Manufacture 115N Propeller Owner’s Manual and Log Book Hartzell
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Recording Arts and Sound Design – The focus is on audio and music recording and production, audio content creation and sound design: AME 140 – Intro to Audio and Music Engineering AME 191 – Art and Technology of Recording AME 192 – Critical Listening for Audio Prod AME 193 – Sound Design
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Rod Machado’s Private Pilot Handbook B4. later I’ll show you how to recognize when you’re near a stall). As long as the airplane stays above its stall speed, enough lift is produced to counter the airplane’s weight and the airplane will fly. If the stall speed of Airplane C
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