BGA AIRWORTHINESS AND MAINTENANCE PROCEDURES PART 2, LEAFLET 2-1 CONTENTS PILOT OWNER MAINTENANCE INTRODUCTION .................................................................................................................................1 BASIC PRINCIPALS ............................................................................................................................1 (a) Competence and responsibility.....................................................................................................1 (b) Tasks.............................................................................................................................................2 (c) Performance of the maintenance Pilot-owner tasks and records..................................................2 (d) Additional information.................................................................................................................2 SCOPE OF PERMITTED WORK ........................................................................................................3 Table A PILOT OWNER MAINTENANCE TASKS for EASA POWERED AIRCRAFT (TUGs)3 Table B PILOT OWNER MAINTENANCE TASKS for EASA SAILPLANES AND POWERED SAILPLANES INCLUDING BGA ANNEX II GLIDERS ..............................................................5 Table C PILOT OWNER MAINTENANCE TASKS for CAA ANNEX II AIRCRAFT AND POWERED SAILPLANES ...............................................................................................................8 SOURCES OF INFORMATION ..........................................................................................................9 CERTIFICATION .................................................................................................................................9 APPLICABILITY OF PERSONS TO CARRY OUT MAINTENANCE OF CLUB AIRCRAFT......9 MONITORING PILOT/OWNER MAINTENANCE ...........................................................................9 ANNEX A............................................................................................................................................10 Example ...............................................................................................................................................11 INTRODUCTION 1. Where an aircraft is used for private flying, the Air Navigation Order and EU regulation 1056/2008 allows certain work to be carried out and certified personally by the holder of a Private Pilots' Licence or glider equivalent who is the owner or operator of the aircraft concerned. Such aircraft must not exceed 2730 kg maximum total weight authorised and must not be used for commercial air transport. The nature of the work allowed to be carried out is specified in the Air Navigation Order and EU regulation as amended and form part of the approved maintenance programme. The aim of this Leaflet is to explain these requirements, identify permitted tasks and show how pilot owner maintenance should be certified in the aircraft Log Book. BASIC PRINCIPALS 2. Explanation of the basic principals taken from Part M (1056/2008) Appendix viii. (a) Competence and responsibility 1. The Pilot-owner is always responsible for any maintenance that he performs. 2. Before carrying out any Pilot-owner maintenance tasks, the Pilot-owner must satisfy himself that he is competent to do the task. It is the responsibility of Pilot-owners to familiarize themselves with the standard maintenance practices for their aircraft and with the aircraft maintenance programme. If the Pilot-owner does not consider him/herself confident they should not carry out the maintenance and seek advice from a BGA inspector. A pilot-owner cannot carry out and certify maintenance on an aircraft that he is not the owner or operator. AMP 2-1/ Nov 08 BGA AMP Part 2, Leaflet 2-1, Page 1 3. The Pilot-owner or his CAMO is responsible for identifying the Pilot-owner tasks according to these basic principles and combining them into maintenance programme. For aircraft operating within the BGA airworthiness system the BGA has done this and will manage the approval and updates and this leaflet forms part of the maintenance programme. (b) Tasks The Pilot-owner may carry out simple visual inspections or operations to check for general condition and obvious damage and normal operation of the airframe, engines, systems and components. Maintenance tasks shall not be carried out by the Pilot-owner when the task: 1. is critically safety related, whose incorrect performance will drastically affect the airworthiness of the aircraft or is a flight safety sensitive maintenance task and/or; 2. requires the removal of major components or major assembly unless otherwise specified in the flight manual as a pilot task and/or; 3. is carried out in compliance with an Airworthiness Directive or an Airworthiness Limitation Item, unless specifically allowed in the AD or the ALI and/or; 4. requires the use of special tools, calibrated tools (except torque wrench and crimping tool) and/or; 5. requires the use of test equipment or special testing (e.g. NDT, system tests or operational checks for avionic equipment that is considered a maintenance or bench test) and/or; 6. is composed of any unscheduled special inspections (e.g. heavy landing, ground loop or similar check) and/or; 7. is effecting systems essential for the IFR operations and/or; 8. is listed as a Complex Maintenance task i.e. major repair, or is a component maintenance task i.e. instrument repair. The criteria 1 to 8 listed above can not be overridden by less restrictive instructions in the Maintenance Programme. Any task described in the aircraft flight manual as preparing the aircraft for flight (Example: assembling the glider wings or pre-flight), is considered to be a pilot task and is not considered a Pilotowner maintenance task and therefore does not require a Certificate of Release to Service. (c) Performance of the maintenance Pilot-owner tasks and records The maintenance data such as Flight or Maintenance manuals as appropriate must be always available during the conduct of Pilot-owner maintenance and must be complied with. Details of the data referred to in the conduct of Pilot-owner maintenance must be included in the Certificate of Release to Service. The Pilot-owner must inform the approved continuing airworthiness management organisation responsible for the continuing airworthiness of the aircraft (if applicable) not later than 30 days after completion of the Pilot owner maintenance task to remain in the controlled environment. In the uncontrolled environment pilot owner maintenance is advised by way of log book entries at time of annual airworthiness review. (The BGA is operating “uncontrolled”) (d) Additional information AMP 2-1/ Nov 08 BGA AMP Part 2, Leaflet 2-1, Page 2 1 Inspection tasks/checks of any periodicity included in an approved maintenance programme can be carried out providing that the specified tasks are included in the generic lists in tables A to C. All scheduled maintenance checks, other than 50 hour or less, are required to be certified by an appropriately rated BGA inspector or licensed engineer, however certain elements within that check, with the agreement of the certifying inspector, may be certified by a pilot owner in accordance with this scheme. The completion certification is always signed by the BGA inspector. 2 For the purposes of pilot owner maintenance a pilot is the owner or syndicate partner, in the case of leased or club owned aircraft, competent pilots are nominated by the operator or club management. 3 If a pilot/owner wishes to carry out maintenance outside the scope of this leaflet, it must be under the supervision of an appropriately rated BGA inspector or licensed engineer who will, on satisfactory completion of the work, certify the work in accordance with Part M. SCOPE OF PERMITTED WORK IT SHOULD BE NOTED THAT SOME TASKS ARE ONLY APPLICABLE TO CERTAIN CLASSES OF AIRCRAFT AS ANNOTATED: Table A PILOT OWNER MAINTENANCE TASKS for EASA POWERED AIRCRAFT (TUGs) ATA Area Task <1000kg 1000 – 2730 kg 05 General Maintenance checks. Only tasks as defined in Table A are permitted. All other tasks must be certified by an appropriately rated Part 66 licensed Engineer. The 150 FH & Annual maintenance check final sign off can only be certified by a Part 66 licensed engineer Yes Yes 09 Towing Tow release unit and tow cable retraction mechanism – Cleaning, lubrication and tow cable replacement (including weak links). Yes Yes Mirror –Installation and replacement of mirrors. Yes Yes 11 Placards Placards, Markings – Installation and renewal of placards and Yes markings required by AFM and AMM. Yes 12 Servicing Lubrication – Not requiring a disassembly other than non structural items such as cover plates, cowlings and fairings. Yes Yes 20 Standard Practices Safety Wiring – Replacement of defective wiring or cotter keys, # Excluding those in engine, transmission, flight control systems. Simple Non Structural Standard Fasteners – Replacement and adjustment, excluding the replacement of receptacles and anchor nuts requiring riveting. Yes # Yes NO Yes 21 Air Conditioning Replacement of flexible hoses and ducts. Yes Yes 23 Communication. Communication devices – Remove and replace self contained, Yes** Yes** front instrument panel mount communication devices with quick disconnect connectors, excluding IFR operations. 24 Electrical power Batteries – Replacement and servicing, excluding servicing of Yes** Yes** Ni-Cd batteries and IFR operations. Wiring – Repairing broken circuits in landing light and any other wiring for non critical equipment, excluding ignition system, primary generating system and required communication, navigation system and primary flight instruments. Yes Yes Bonding – Replacement of broken bonding cable. Yes Yes Fuses – Replacement with the correct rating. Yes Yes 25 Equipment Safety Belts – Replacement of safety belts and harnesses excluding belts fitted with airbag systems. Yes Yes AMP 2-1/ Nov 08 BGA AMP Part 2, Leaflet 2-1, Page 3 26 Fire Protection 27 Flight controls 28 Fuel System 31 Instruments 32 Landing Gear 33 Lights 34 Navigation 51 Structure AMP 2-1/ Nov 08 Seats – Replacement of seats or seat parts not involving disassembly of any primary structure or control system. Non essential instruments and/or equipment - Replacement of self contained, front instrument panel mount equipment with quick disconnect connectors. Oxygen System – Replacement of oxygen bottle and system in approved mountings ELT – Removal / Re-installation. Fire Warning – Replacement of sensors and indicators. Removal or re-installation of co-pilot control column and rudder pedals where provision for quick disconnect is made by design. Fuel lines – Replacement of prefabricated fuel lines fitted with self sealing couplings. Fuel Filter elements – Cleaning and/or replacement. Instrument Panel– Removal and re-installation provided this it is a design feature with quick disconnect connectors, excluding IFR operations. Pitot Static System – Simple sense and leak check, excluding IFR operations. Drainage – Drainage of water drainage traps or filters within the Pitot static system excluding IFR operations. Flexible tubes - Replacement of damaged tubes excluding IFR operations. Wheels – Removal, replacement and servicing, including replacement of wheel bearings and lubrication. Hydraulic fluid – Replenishment of hydraulic fluid such as brake fluid. Shock Absorber – Replacement of elastic cords or rubber dampers. Shock Struts – Replenishment of oil or air. Skis – Changing between wheel and ski landing gear. Landing skids – Replacement of landing skids and skid shoes. Wheel fairings (spats) – Removal and re-installation. Mechanical brakes – Adjustment of simple cable operated systems. Brake – Replacement of worn brake pads or shoes. #excludes relining brake pads or shoes Lights – Replacement of internal and external bulbs, filaments, reflectors and lenses. Software – Updating self contained, front instrument panel mount navigational software databases, excluding automatic flight control systems and transponders. Navigation devices – Removal and replacement of self contained, front instrument panel mount navigation devices with quick disconnect connectors, excluding automatic flight control systems, transponders, primary flight control system and IFR operations. Self contained data logger – Installation, data restoration. Fabric patches – Simple patches extending over not more than one rib, not requiring rib stitching or removal of structural parts or control surfaces. Protective Coating – Applying preservative material or coatings where no disassembly of any primary structure or operating system is involved. #excludes painting of aircraft Surface finish - Minor restoration where no disassembly of any primary structure or operating system is involved This includes application of signal coatings or thin foils as well as registration markings. # excludes painting of aircraft. BGA AMP Part 2, Leaflet 2-1, Page 4 Yes Yes Yes Yes Yes Yes Yes Yes Yes** Yes** Yes** Yes** Yes Yes Yes Yes Yes Yes Yes Yes Yes # Yes Yes Yes** Yes Yes Yes # Yes # Yes Yes Yes Yes Yes Yes Yes Yes NO NO Yes** NO Yes Yes Yes NO Yes Yes Yes NO NO Yes Yes Yes** Yes Yes Yes # Yes # 52 Doors 53 Fuselage 56 Windows 61 Propeller 71 Powerplant installation 72 Engine 73 Engine fuel 74 Ignition 75 Cooling 77 Engine Indicating 79 Oil System Fairings – Simple repairs to non structural fairings and cover plates which do not change the contour. Doors - Removal and re-installation. Upholstery, furnishing – Minor repairs which do not require disassembly of primary structure or operating systems, or interfere with control systems. Side Windows - Replacement if it does not require riveting, bonding or any special process. Spinner – Removal and re-installation. Cowling – Removal and re-installation not requiring removal of propeller or disconnection of flight controls. Chip detectors – Removal, checking and re-installation provided the chip detector is a self sealing type and not electrically indicated. Strainer or Filter elements – Cleaning and/or replacement. Fuel - Mixing of required oil into fuel. Spark Plugs – Removal, re-installation and adjustment. Coolant - Replenishment of coolant fluid. Engine Indicating – Removal and replacement of self contained, front instrument panel mount indicators that do not employ direct reading connections. Strainer or filter elements – Cleaning and/or replacement. Oil – Changing or replenishment of engine oil and gearbox fluid. Yes Yes Yes Yes Yes Yes Yes Yes Yes Yes Yes Yes Yes Yes Yes Yes Yes Yes Yes Yes Yes Yes Yes Yes Yes NO Yes Yes Table B PILOT OWNER MAINTENANCE TASKS for EASA SAILPLANES AND POWERED SAILPLANES INCLUDING BGA ANNEX II GLIDERS Abbreviations applicable to this table: N/A not applicable for this category SP sailplane SSPS self sustaining powered sailplane SLPS/TM self launching powered sailplane/touring motor glider ATA Area 05 General 08 Weighing 09 Towing 11 Placards 12 Servicing 20 Standard. Practices AMP 2-1/ Nov 08 Task Maintenance checks. Only tasks as defined in Table B are permitted. All other tasks must be certified by an appropriately rated BGA inspector. The 150 FH & Annual maintenance check final sign off can only be certified by a BGA inspector Recalculation – Small changes of the Trim plan without needing a reweighing. Tow release unit – Cleaning, lubrication and replacement of unit not involving disassembly of any primary structure, control system or additional adjusting. Mirror –Removal and re-installation of mirrors. Placards, Markings – Installation and renewal of placards and markings required by AFM and AMM. Lubrication – Not requiring a disassembly other than non structural items such as cover plates, cowlings and fairings. Safety Wiring – Replacement of defective wiring or cotter keys. #Excluding flight or engine control systems Simple Non Structural Standard Fasteners – Replacement and adjustment, excluding the replacement of receptacles and anchor nuts requiring riveting. Free play – Measurement of the free play in the control system and the wing to fuselage attachment including minor adjustments by simple means SP N/A Yes Yes N/A Yes Yes Yes # Yes Yes BGA AMP Part 2, Leaflet 2-1, Page 5 SSPS Yes Yes Yes N/A Yes Yes Yes # Yes Yes SLPS/TM Yes Yes Yes Yes Yes Yes Yes # Yes Yes provided by the manufacturer. 21 Air Conditioning Replacement of flexible hoses and ducts. Yes 23 Communication Communication devices – Remove and replace self Yes contained, front instrument panel mount communication devices with quick disconnect connectors. 24 Electrical power Batteries and solar panels – Replacement and Yes servicing. Wiring - Installation of simple wiring connections to Yes the existing wiring for additional equipment such as electric variometers, flight computers but excluding communication, navigation systems and engine wiring. Wiring – Repairing broken circuits in landing light Yes and any other wiring for non critical equipment, excluding ignition system, primary generating system and required communication, navigation system and primary flight instruments. Bonding – Replacement of broken bonding cable. Yes Switches – Replacement without soldering. Yes Fuses – Replacement with the correct rating. Yes 25 Equipments Safety Belts – Replacement of safety belt and Yes harnesses. Seats – Replacement of seats or seat parts not Yes involving disassembly of any primary structure or control system. Non essential instruments and/or equipments - Yes Replacement of self contained, front instrument panel mount equipment with quick disconnect connectors. Removal and installation of non required Yes instruments and/or equipment. Wing Wiper, Cleaner – Servicing, removal and re- Yes installation not involving disassembly or modification of any primary structure, control Static Probes – Removal or re-installation of Yes variometer static and total energy compensation probes. Oxygen System – Replacement of Oxygen Bottle Yes and System. Air Brake Chute – Installation and servicing Yes ELT – Removal / Re-installation. Yes 26 Fire Protection Fire Warning – Replacement of sensors and N/A indicators. 27 Flight Control Gap Seals – Installation and servicing if it does not Yes require complete flight control removal. Control System – Measurement of the control Yes system travel without removing the control surfaces. Control Cables – Simple optical Inspection for Yes Condition. Gas Dampener – Replacement of Gas Dampener in Yes the Control or Air Brake System. Co-pilot stick and pedals - Removal or re-installation Yes where provision for quick disconnect is made by design. 28 Fuel System Fuel lines – Replacement of prefabricated fuel lines N/A fitted with self sealing couplings. Fuel Filter – Cleaning and/or replacement. N/A 31 Instruments Instrument Panel– Removal and re-installation Yes provided this is a design feature with quick disconnect, excluding IFR operations. Pitot Static System – Simple sense and leak check. Yes Instrument Panel vibration damper / shock Yes absorbers- Replacement. Drainage – Drainage of water drainage traps or Yes AMP 2-1/ Nov 08 BGA AMP Part 2, Leaflet 2-1, Page 6 Yes Yes Yes Yes Yes Yes Yes Yes Yes Yes Yes Yes Yes Yes Yes Yes Yes Yes Yes Yes Yes Yes Yes Yes Yes Yes Yes Yes Yes Yes Yes Yes Yes Yes Yes Yes Yes Yes Yes Yes Yes Yes Yes Yes Yes Yes Yes Yes Yes Yes Yes Yes Yes Yes Yes Yes Yes Yes 32 Landing Gear 33 Lights 34 Navigation 51 Structure 52 Doors 53 Fuselage 56 Windows 57 Wings AMP 2-1/ Nov 08 filters within the Pitot static system. Flexible tubes - Replacement of damaged tubes. Wheels – Removal, replacement and servicing, including replacement of wheel bearings and lubrication. Hydraulic fluid – Replenishment of hydraulic fluid such as brake fluid. Shock Absorber – Replacement or servicing of elastic cords or rubber dampers. Shock Struts – Replenishment of oil or air. Landing gear doors - Removal or re-installation and repair including operating straps. Skis – Changing between wheel and ski landing gear. Skids – Removal or re-installation and servicing of main, wing and tail skids. Wheels fairing (spats) – Removal and re-installation. Mechanical brakes – Adjustment of simple cable operated systems. Brake – Replacement of worn brake pads. Springs – Replacement of worn or aged springs. Gear Warning –Removal or re-installation of simple gear warning systems. Lights – Replacement of internal and external bulbs, filaments, reflectors and lenses. Software – Updating self contained, front instrument panel mount navigational software databases, excluding automatic flight control systems and transponders and including update of non required instruments / equipments. Navigation devices – Removal and replacement of self contained, front instrument panel mount navigation devices with quick disconnect connectors, excluding automatic flight control systems, transponders, primary flight control system. Self contained data logger – Installation, data restoration Fabric patches – Simple patches extending over not more than one rib, not requiring rib stitching or removal of structural parts or control surfaces. Protective Coating – Applying preservative material or coatings where no disassembly of any primary structure or operating system is involved. # Excludes painting of aircraft Surface finish - Minor restoration where no disassembly of any primary structure or operating system is involved This includes application of signal coatings or thin foils as well as Registration markings. # Excluded painting of aircraft Fairings – Simple repairs to non structural fairings and cover plates which do not change the contour. Doors - Removal and re-installation. Upholstery, furnishing – Minor repairs which do not require disassembly of primary structure or operating systems, or interfere with control systems. Side Windows - Replacement if it does not require riveting, bonding or any special process. Canopies - Removal and re-fitment. Gas dampener – Replacement of Canopy Gas dampener. Wing Skids – Removal or re-installation and service of lower wing skids or wing roller including spring assembly. Water ballast – Removal or re-installation of flexible Yes Yes Yes Yes Yes Yes Yes Yes Yes Yes Yes Yes Yes N/A Yes Yes Yes Yes Yes # Yes # Yes Yes Yes Yes Yes Yes Yes Yes BGA AMP Part 2, Leaflet 2-1, Page 7 Yes Yes Yes Yes Yes Yes Yes Yes Yes Yes Yes Yes Yes N/A Yes Yes Yes Yes Yes # Yes # Yes Yes Yes Yes Yes Yes Yes Yes Yes Yes Yes Yes Yes Yes Yes Yes Yes Yes Yes Yes Yes Yes Yes Yes Yes Yes Yes # Yes # Yes Yes Yes Yes Yes Yes Yes Yes tanks. Turbulator and sealing tapes – Removal or re- Yes Yes Yes installation of approved sealing tapes and turbulator tapes. 61 Propeller Spinner – Removal and re-installation. N/A Yes Yes 71 Power Plant Removal or installation of power plant unit including N/A Yes # NO engine and propeller. (provided the task is identified in the flight manual as a Pilot task) # Power Plant installation final sign off certified by a BGA inspector only. Cowling - Removal and re-installation not requiring N/A Yes Yes removal of propeller or disconnection of flight controls. 72 Engine Chip detectors – Removal, checking and re- N/A Yes Yes installation provided the chip detector is a self sealing type and not electrically indicated. Rotax CCBCT check N/A Yes No 73 Engine fuel Strainer or Filter elements – Cleaning and/or N/A Yes Yes replacement. Fuel - Mixing of required oil into fuel. N/A Yes Yes 74 Ignition Spark Plugs – Removal, re-installation and N/A Yes Yes adjustment. 75 Cooling Coolant – Replenishment of coolant fluid. N/A Yes Yes 76 Engine Controls Controls – Minor adjustments of non-flight or N/A Yes NO propulsion controls whose operation is not critical for any phase of flight. 77 Engine Indicating Engine Indicating – Removal and replacement of N/A Yes Yes self contained, front instrument panel mount indicators that do not employ direct reading connections. 79 Oil System Strainer or Filter elements – Cleaning and/or N/A Yes Yes replacement Oil – Changing or replenishment of engine oil and N/A Yes Yes gearbox fluid. Table C PILOT OWNER MAINTENANCE TASKS for CAA ANNEX II AIRCRAFT AND POWERED SAILPLANES Abbreviations applicable to this table: >2730 – Aircraft up to 2730 KGS MTOW SLPS/TM self launching powered sailplane/touring motor glider ATA 05 20 23 24 Area General Standard practices Communication Electrical power 25 Equipment 32 Landing gear 51 Structure AMP 2-1/ Nov 08 Task Maintenance Checks up to 50hr/6 months but not including the certification of applicable Airworthiness Directives (AD’s). Replacement of defective safety wiring or split pins excluding those in engine, transmission, flight control and rotor systems; Replacement of VHF communication equipment, being equipment which is not combined with navigation equipment. Replacement of batteries Replacement of generator and fan belts designed for removal where special tools are not required; Repairs to upholstery and decorative furnishing of the cabin or cockpit interior when repair does not require dismantling of any structure or operating system or interfere with an operating system or affect the structure of the aircraft Replacement of safety belts or safety harness; Replacement of seats or seat parts not involving dismantling of any structure or of any operating system Replacement of landing gear tyres, landing skids or skid shoes; Replacement of elastic shock absorber cord units on landing gear where special tools are not required; Patch-repairs to fabric not requiring rib stitching or the removal of structural parts or control surfaces, if the repairs do not cover BGA AMP Part 2, Leaflet 2-1, Page 8 SLPS/MG Yes Yes Yes Yes Yes Yes Yes Yes Yes Yes Yes >2730 Yes Yes Yes Yes Yes Yes Yes Yes Yes Yes Yes 56 Windows 57 Wings 33 Lights 72 Power plant 74 Ignition up structural damage and do not include repairs to rotor blades; Repairs, not requiring welding, to fairings, non-structural cover plates and cowlings Replacement of side windows where that work does not interfere with the structure or with any operating system; Replacement of wings and tail surfaces and controls, the attachments of which are designed to provide for assembly immediately before each flight and dismantling after each flight; Replacement of bulbs, reflectors, glasses, lenses or lights Replacement of any cowling not requiring removal of the propeller, rotors or disconnection of engine or flight controls Replacement of unserviceable sparking plugs Yes Yes Yes Yes Yes Yes Yes Yes Yes Yes Yes Yes SOURCES OF INFORMATION 3. Further information on the requirements for Pilot Maintenance may be obtained from CAP 520 “Light Aircraft Maintenance” or in CAA approved maintenance programmes – LAMS/A/1999, LAMP/A/2007 or BGA GMS, Manufacturers published information in the form of Maintenance Manuals, Operating Hand Books or Flight manuals should be used as appropriate. Part M regulation 2042/2003 amended by 1056/2008 M.A.803 and Appendix viii. CERTIFICATION 4. An example of how pilot maintenance should be certified in the aircraft Log Book is at Annex A. Note the different certification requirements for Annex II and EASA aircraft. 5. If a mandatory inspection is due as part of the check or replacement then a suitably qualified engineer must sign for at least the mandatory items. APPLICABILITY OF PERSONS TO CARRY OUT MAINTENANCE OF CLUB AIRCRAFT 6. BGA Tug pilots, motor glider pilots or glider pilots who are members of a BGA gliding club, as specified on the aircraft registration document, that operates the aircraft would be deemed “Operators” provided that they were involved with the decision making process regarding pilot maintenance and the club committee designates that person to carry out the maintenance. It is recommended a record of the approval is maintained. In the case of leased aircraft, the lessee is considered the operator/owner and the above rule applies. 7. It strongly recommended that all personnel engaged in maintenance of club aircraft be trained by the licensed engineer, maintenance organisation or BGA inspector that normally maintains the aircraft. Records of this training should be kept to demonstrate that they are competent persons to complete the tasks. Refresher training should be undertaken at regular intervals. MONITORING PILOT/OWNER MAINTENANCE 8. During normal maintenance checks and at other times as circumstances dictate, previously accomplished pilot /owner maintenance standards should be monitored by the licensed engineer, maintenance organisation or BGA inspector to verify standards are maintained. Discrepancies found AMP 2-1/ Nov 08 BGA AMP Part 2, Leaflet 2-1, Page 9 must be reported to the BGA Quality Manager at time of Airworthiness Review and the operating club management to enable retraining or withdrawal of privileges as appropriate. Serious discrepancies must be reported to the BGA Quality Manager within 72 hours of finding the occurrence. ANNEX A AMP 2-1/ Nov 08 BGA AMP Part 2, Leaflet 2-1, Page 10 ANNEX A to AMP Leaflet 2-1 BGA Airworthiness and Maintenance Procedures Manual – Example of Pilot Maintenance Certification Date No. of Flight Time Total Since Engine The work recorded below has been carried out in accordance with the requirements of the Air Navigation Flight Manufacture Cycles Order for the time being in force and in that respect the aircraft / equipment is considered fit for release s to service. 34 Signature Particulars of Maintenance and Other Work Carried Out on the Aircraft Authority 1 Total bf. 20/4/08 21/4/08 2 246 2 3 h mh m 197 50 2 40 200 30 2 25 202 55 5 6 Annex II Aircraft CAA C of A Date 7 25/4/08 1 1 10 204 05 6/5/08 4 4 30 208 35 12/5/08 1 1 30 210 05 50 hour check carried out I.A.W. LAMS/A/1999 issue 2 13/5/08 2 2 25 212 30 J Smith 13/5/08 PPL 12345 Total cf. 50 hour check carried out I.A.W. LAMP/A/2007 issue 1 EASA Aircraft EASA C of A & ARC J Smith 13/5/08 PPL 12345 Example CAP 398 Airframe Log book CAA C of A aircraft Example shows correct format for Private Pilot certified maintenance for aircraft used for private flying. Note: The certification for Annex II is in the main section (box 6). The certification for EASA aircraft is in the CRS section (box 7) AMP 2-1A/ Sep 08 BGA AMP Part 2, Leaflet 2-1, Appendix A