AMM in french pdf
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1. 10 50 HOUR INSPECTION Fuel Injected Normally Aspirated Engines 5 9 Visite des 100 heures 2 Hr eee 6 12 6 1 1 Entretien courant graissage seen 6 12 6 1 2 Conditionnement eos 6 12 6 1 3 Circuit l ctrique nen ai diia 6 12 6 1 4 Circuit carburant 2 22 genen ae ne ee na 6 12 6 1 5 Syst me de freinage cosine eoon eee OEE seeded RNA Re nes 6 12 6 1 6 Instruments tisse es ee hse Rte ce RP ER LE nt SR ee Nes 6 13 6 1 7 Commandes de VU erra ee o E E A RE RP Se SE se ot 6 13 6 1 8 FH NICS EE E nn nn sktl 6 13 6 1 9 MOIEUL EE Pe MR Res da 6 13 6 1 10 100 HOUR INSPECTION Fuel Injected Normally Aspirated Engines sornvrrnorrvvrrvrrrnrvenre 6 13 Mat riels prep ii an ate nm en nn AGE s 7 17 ANNEXES nn ce dese ne a tente mines 8 18 C WINDOWS Profiles cyril Mes Documents Panda Programme d_entretien doc MANUEL D ENTRETIEN DU POTTIER P230S PANDA 2 Prolegomenes 2 1 Avertissement Cette publication contient des informations n cessaires pour r aliser la maintenance et les visites 50 et 100 heures du Pottier P230S PANDA quip d un moteur IO240B Ce document est dit titre informatif et n est en aucun cas un document officiel et ne peut suffire lui seul pour maintenir l aptitude de navigabilit de l a ronef 2 2 Evolutions Ce document est appel s enrichir jour apr s jour d l ments nouveaux il est donc publi ici en temps que projet C WINDOWS Profiles cy2. Reference TCM Service Bulletin SB94 8 or latest revision for magneto to engine timing C WINDOWS Profiles cyril Mes Documents Panda Programme d_entretien doc MANUEL D ENTRETIEN DU POTTIER P230S PANDA specifications If not prior to adjusting magneto timing inspect the breaker points for condition and signs of arcing Replace breaker points and condenser if arcing signatures are noted Note Magnetos using riveted type impulse coupling require repetitive 100 inspection Refer to TCM Service Bulletin MSB645 or latest revision for specific instructions 8 Clean inspect gap and test all spark plugs Rotate plugs as directed in the applicable Maintenance or Overhaul Manual to achieve maximum service life WARNING SPARK PLUGS THAT ARE EXCESSIVELY WORN AND CONTINUED IN SERVICE MAY CAUSE INTERNAL ARCING IN THE MAGNETOS 9 Check all fasteners for indications of improper assembly loss of torque and obvious defects ___ 10 Check all engine controls control cables control rod ends and levers for security wear improper assembly routing and freedom of movement throughout the entire range of travel Refer to TCM Service Bulletin SB95 2 or latest revision for detailed instructions on control linkage inspection and lubrication Note Engine control rod ends should be fastened securely to the control lever The rod end should move freely through the entire range of travel Do not attempt to achieve freedom of movement or travel by
3. any discrepancies noted during this inspection prior to returning the engine to service OBSERVATIONS C WINDOWS Profiles cyril Mes Documents Panda Programme d_entretien doc MANUEL D ENTRETIEN DU POTTIER P230S PANDA 5 Visite des 50 heures 5 1 1 Entretien courant graissage Les charni res d aileron et de volets doivent tre lubrifi avec une huile fine poss dant une propri t anticorrosion Les coulisse de commande de volet sont graiss es l aide de graisse blonde 5 1 2 Conditionnement d air V rifier le fonctionnement des commandes de clapet au besoin lubrifier les axes des clapets V rifier la fixation des gaines souples au niveau des raccordements 5 1 3 Circuit lectrique V rification du c blage lectrique l avant de la cloison pare feu pour frottements et usure anormale V rifier le serrage des cosses lectriques V rifier la charge de la batterie recharger ventuellement V rifier le fonctionnement du phare d atterrissage des feux de navigation des feux clat de l avertisseur de d crochage 5 1 4 Circuit carburant Nettoyage du pot d canteur noter l tat remontage la molette de serrage du pot doit tre arr t e au fil freiner V rifier les tuyaux pour frottements rayon de courbure et usure anormale 5 1 5 Syst me de freinage V rifier le circuit pour fuite et dommage V rifier le niveau du liquide de frein Compl ter ventu
4. loosening the torque on the attaching hardware This will result in relative movement between the control lever attach point and the attaching hardware and will result in elongation of the attach point in the lever loss of travel and possible failure of the lever WARNING ASSURE THAT THE FUEL SELECTOR IS IN THE OFF POSITION PRIOR TO REMOVING THE CARBURETOR BOWL DRAIN PLUG 11 Remove the fuel metering unit inlet screen and inspect screen for foreign material Clean screen by soaking in lacquer thinner acetone or methyl ethyl ketone MEK After the screen has been cleaned reinstall screen in fuel control unit using a new gasket and safety 12 Inspect fuel nozzles and nozzle lines for proper routing and support Inspect manifold valve for security of installation proper venting and signs of fuel stains Note Comply with TCM SB95 7 if fuel stains are noted at the manifold valve 13 At the first 100 hour inspection on new rebuilt or overhauled engines remove and clean the fuel injection nozzles Fuel nozzles must be cleaned at 300 hour intervals or more frequently if fuel stains are noted 14 Inspect all accessories for condition security of mounting and proper operation Refer to aircraft or component manufacturer s Maintenance Manual for specifics 15 Inspect engine mount legs for cracks Check engine mount biscuits for signs of deterioration proper assembly and security 16 Correct any discrepancies noted C WINDOWS Prof
5. seals and gaskets for condition and deterioration Replace as required any questionable components Inspect C WINDOWS Profiles cyril Mes Documents Panda Programme d entretien doc 4 6 MANUEL D ENTRETIEN DU POTTIER P230S PANDA carburetor heat control valve for proper travel freedom of movement worn bushings and correct rigging 4 Inspect induction air box for security and deterioration With induction air filter installed verify that the induction air filter retainer is properly installed and the attaching hardware is secure Note Failure to properly install the induction air filter retainer will result in unfiltered air being ingested into the engine which will accelerate engine wear and reduce engine service life 5 Correct any discrepancies noted 6 Perform post inspection operational run up Verify that the engine meets all performance criteria as detailed in Step 1 50 hour pre inspection operational run up and record engine parameters on operational check list Visually inspect engine and nacelle for fuel and oil leaks 7 Prior to engine shut down perform hot magneto test Reference TCM Service Bulletin SB653 or latest revision for amplified instructions WARNING FAILURE TO CORRECT AN OPEN IN THE GROUNDING CIRCUIT OF THE MAGNETO S WILL RESULT IN THE MAGNETO S BEING HOT THIS MAY RESULT IN THE ENGINE FIRING INADVERTENTLY AND RESULT IN BODILY INJURY OR DEATH FROM THE PROPELLER STRIKING AN INDIVIDUAL 8 Correct
6. the STC holder Oil First 25 hours of operation Mineral non detergent oil or Corrosion Preventive oil corresponding to MIL C 6529 Type II Note Mineral oil conforming to MIL C 6529 Type II is a straight mineral oil with a corrosion preventive additive This oil must not be operated in excess of 25 hours or 6 months whichever occurs first If oil consumption has not stabilized within the first 25 hours of engine operation drain and replenish the oil Remove and clean the oil pressure screen or replace the filter Approved Oil Grade All Temperatures 15W 50 20W 50 20W 60 Below 40 F Ambient Air Sea Level SAE30 or 10W 30 Above 40 F Ambient Air Sea Level SAE50 Oil Change Interval With integral oil screen 25 hours With small full flow oil filter 50 hours With large full flow oil filter 100 hours Note Oil must be drained and replenished every six 6 months regardless of hours since last oil change Oil Filter Interval Integral oil pressure screen 25 hours Small oil filter approximately 4 80 high 50 hours Large oil filter approxiamtely 5 80 high 50 hours CAUTION USE ONLY OIL CONFORMING TO TCM SPECIFICATIONS AFTER ENGINE BREAK IN REFER TO TCM SERVICE BULLETIN M87 12 REV 1 OR LATEST REVISION FOR APPROVED OILS 3 Remove and inspect induction air filter Clean or replace as recommended by the filter manufacturer Inspect induction system ducts
7. within the specifications published for the engine and aircraft The scheduled maintenance listings in this program are formatted in a convenient check list form that may be printed and used during the performance of the inspections In addition to the items listed for pre flight inspection the following maintenance should be performed 1 After the first 25 hours of operation on new rebuilt or overhauled engines perform a complete 50 hour inspection Drain the oil used for engine break in If engine oil consumption has stabilized service the engine with an aviation grade ashless dispersant oil meeting TCM specifications refer to the Airplane Flight Maual and or TCM Service Bulletin M87 12 Rev 1 or latest revision for approved oils If oil consumption has not stabilized service engine with a mineral oil conforming to MIL L 6082 Additionally notify your FBO and TCM that oil consumption has not stabilized 2 Engines equipped with integral oil screens require a complete oil change and removal inspection and cleaning of the oil screen every 25 hours of operation C WINDOWS Profiles cyril Mes Documents Panda Programme d_entretien doc 45 MANUEL D ENTRETIEN DU POTTIER P230S PANDA Engines equipped with full flow oil filters as original or optional equipment by the engine or aircraft manufacturer may be operated for 50 hours between oil changes Note Oil filtration systems installed via an STC must be serviced as directed by
8. MANUEL D ENTRETIEN DU POTTIER P2305 PANDA MANUEL D ENTRETIEN DU POTTIER P230S PANDA REPERTOIRE DES EVOLUTIONS EDITION DATE Nature de l volution Pages modifi es Date Emission initiale d mission C WINDOWS Profiles cyril Mes Documents Panda Programme d_entretien doc 1 1 MANUEL D ENTRETIEN DU POTTIER P230S PANDA 1 Table des mati res 1 2 3 4 Table des MAS Nim iaa 1 2 Brolesomenes 24 382 en manuur E E een E E A 2 3 2 1 AVES SEMEN A A een SAR 2 3 2 2 EVOL SA A ASA AA SA 2 3 Programme d inspection nsn R N a pen pen 3 4 3 1 Echelonnement des Visites estres ra rara trtne stren eneren Erener EEEE rra 3 4 3 2 Tenu des documents av1on rerernrnrnrnrnrnrnrnrnvnrnrnrnrnrnrnrnrnrnrnvnvnrnvnrnrnvnnnsnsnensnunensnsnensnenensnsnsnsnenensnsnsvsnsnenee 3 4 3 2 1 Fe camet d ON E SAE re 3 4 3 22 RES ee 3 4 3 2 3 Le ivret moten 3 4 Contenu des VISITES Fes ec dte ae 4 5 4 1 Entretien des 23 he res daa 4 5 4 1 1 25 Hour Inspection Fuel Injected Normally Aspirated Engines 4 5 Viste des 50 heures ras atrossne tt Mes ne ns es 5 8 5 1 1 Entretien courant pralsS LO soto ind remettant te en ne tin ar Reste 5 8 5 1 2 Conditionnement d air 5 8 5 1 3 AAN 5 8 5 1 4 SEN es ee RE Te En Et ae 5 8 5 1 5 Syst me de freinage rss ot ntm iin sen 5 8 5 1 6 Instrument esse seen ee eher ENTER ee nn Ne 5 8 5 1 7 Commandesidevol 2 NET 5 8 5 1 8 E 5 8 5 1 9 Moa ei ies 5 9 5 1
9. ce Bulletins are issued to notify owners operators and FBO s of conditions that affect safety of flight and continued airworthiness ___ 1 Perform pre inspection operational check of the following items with the engine at normal operating temperatures Reference the applicable Airplane Flight Manual for operational values C WINDOWS Profiles cyril Mes Documents Panda Programme d_entretien doc 5 9 MANUEL D ENTRETIEN DU POTTIER P230S PANDA ____ A Idle speed ____ B Idle mixture set to achieve 25 to 50 RPM rise ___ C Magneto drop and variation between magnetos Maximum drop 150 RPM maximum variation 50 RPM D Hot magneto test See TCM Service Bulletin SB653 or latest revision for amplified instructions ____ E Propeller for proper operation ___ F Full power performance R P M Manifold Pressure and Fuel Flow G Cylinder head and oil temperature within limits H Oil pressure Minimum 10 psi idle 30 to 60 psi full power at normal oil temperature 175 to 200 degrees Fahrenheit 2 Drain engine oil If using oil analysis take oil sample in accordance with the analysis company s instructions 3 Remove oil filter or integral oil pressure screen Inspect filter element or screen for foreign material Install new oil filter or clean and reinstall integral oil pressure screen with new gasket and safety Service engine with proper grade of oil in accordance with the Airplane Flight Manual or latest revisi
10. coulisse de commande de volet sont graiss es l aide de graisse blonde 6 1 2 Conditionnement d air V rifier le fonctionnement des commandes de clapet au besoin lubrifier les axes des clapets V rifier la fixation des gaines au raccordement 6 1 3 Circuit lectrique V rification du c blage lectrique l avant de la cloison pare feu pour frottements et usure anormale V rifier le serrage des cosses lectriques V rifier la charge de la batterie recharger ventuellement V rifier le fonctionnement du phare d atterrissage des feux de navigation des feux clat de l avertisseur de d crochage 6 1 4 Circuit carburant Nettoyage du pot d canteur noter l tat remontage la molette de serrage du pot doit tre arr t e au fil freiner voir figure V rifier les tuyaux souples pour p remption frottements rayon de courbure et usure anormale V rification des filtres essence p remption 6 1 5 Syst me de freinage V rifier le circuit pour fuite et dommage V rifier le niveau du liquide de frein Compl ter ventuellement avec du liquide de frein automobile DOT4 uniquement C WINDOWS Profiles cyril Mes Documents Panda Programme d_entretien doc 6 12 MANUEL D ENTRETIEN DU POTTIER P230S PANDA 6 1 6 Instruments Etat du circuit d air d prim p remption des filtres Pour localisation voir figure 6 1 7 Commandes de vol D monter les trappes de visite une sous chaque ai
11. ded Verify that the recorded parameters meet the published performance specifications for the engine as provided in the aircraft and or engine manufacturers Service Operator s and Overhaul Manuals At the completion of any maintenance event the engine must be given a complete and thorough operational run up In some cases where adjustments have been made to the engine fuel system and or turbocharger system a test flight will be required reference FAR 91 407 Record all engine parameters on the operational test form and if a test flight was performed on a test flight log and verify that recorded parameters are within the specifications published for the engine and aircraft The scheduled maintenance listings in this program are formatted in a convenient check list form that may be printed and used during the performance of the inspections Note The Maintenance Schedule checklists contained in this program are intended to complement the Aircraft Manufacturer published recommendations In addition to the items listed for pre flight 25 and 50 hour inspections the following inspections and maintenance must be performed Note During the 100 hour inspection research all Service Bulletins and AD s TCM requires that all Category I Mandatory and Category II Critical Service Bulletins be complied with in accordance with the COMPLIANCE section of the Service Bulletin Category I and Category II Service Bulletins are issued to notify owners o
12. e s tablis pas dans les 30 secondes coupez le moteur et effectuer les v rifications n cessaires Attention Attendre que la temp rature d huile atteigne 75 F et que le CHT atteigne 200 F pour tourner plus de 1800 tr mn Faire tourner le moteur 2100 tr mn Pression carburant PSI Chute RPM magn to gauche tr mn Max 150 tr mn Chute RPM magn to droite tr mn Max 150 tr mn Diff rence magn to G D Tr mn Max 50 tr mn Mettre plein gaz Pression d admission InchHg Pression injection carburant PSI 11 2 0 3 E 2400 tr mn Pression d huile PSI 30 60 PSI 100 max Temp rature d huile F lt 240 F CHT F lt 460 F RPM Tr mn lt 2400 R duire les gaz au ralenti Vitesse de rotation ralenti Tr mn 850 50 tr mn Pression d injection PSI 3 5 4 PSI Pression d huile PSI 10 PSI min Temp rature d huile F Ne pas arr ter le moteur avant que la temp rature de cylindre CHT ne soit au dessous de 300 F Placer la richesse sur la position de test du r gime de ralenti Augmentation du nbre de tr mn Tr mn 25 50 tr mn Coupure franche de l alimentation Magn to sur Off contact g n ral sur Off robinet de s lection r servoir sur Off C WINDOWS Profiles cyril Mes Documents Panda Programme d_entretien doc
13. ellement Avec du liquide de frein automobile DOT4 uniquement 5 1 6 Instrument Rien 5 1 7 Commandes de vol D monter les trappes de visite une sous chaque aile deux sous le fuselage v rifier l tat des guignols des rotules jeux d formations 5 1 8 Helice V rification visuelle des pales pour clat C WINDOWS Profiles cyril Mes Documents Panda Programme d_entretien doc 5 8 MANUEL D ENTRETIEN DU POTTIER P230S PANDA V rification du serrage de l h lice D montage du c ne Serrage des boulons de 44 au couple de 9 10 foots Ibs Serrage des boulons de 1 2 au couple de Remontage du c ne 5 1 9 Moteur Se conformer au 10240 series Maintenance Manual r f TCM X30621A Ou aux recommandations ci dessous 5 1 10 50 HOUR INSPECTION Fuel Injected Normally Aspirated Engines SERVICING SCHEDULED MAINTENANCE Maximum efficiency and engine service life is predicated on compliance with the aircraft and engine manufacturer s required published inspection and maintenance schedule Non compliance may result in a loss of engine performance an increase in unscheduled maintenance and a reduction in engine service life The owner or operator is primarily responsible for maintaining the engine in an airworthy condition including compliance with applicable Airworthiness Prior to any scheduled inspection the engine must be clean and a pre inspection operational run up performed Record the engine operatin
14. eur Le livret se g re de la m me fa on que le pr c dent mais le compte des heures ne concerne que les heures du moteur en cours C WINDOWS Profiles cyril Mes Documents Panda Programme d_entretien doc 3 4 MANUEL D ENTRETIEN DU POTTIER P230S PANDA 4 Contenu des visites 4 1 Entretien des 25 heures Le moteur 10240B du Panda est quip d un filtre tamis oil screen une vidange est n cessaire tous les 25 heures Se conformer au chapitre 19 3 du 10240 series Maintenance Manual r f TCM X30621A ou aux recommandations ci dessous 4 1 1 25 Hour Inspection Fuel Injected Normally Aspirated Engines SERVICING SCHEDULED MAINTENANCE Prior to any scheduled inspection the engine must be clean and a pre inspection operational run up performed Record the engine operating parameters on the operational test form provided Verify that the recorded parameters meet the published performance specifications for the engine as provided in the aircraft and or engine manufacturers Service Operator s and Overhaul Manuals At the completion of any maintenance event the engine must be given a complete and thorough operational run up In some cases where adjustments have been made to the engine fuel system and or turbocharger system a test flight will be required reference FAR 91 407 Record all engine parameters on the operational test form and if a test flight was performed on a test flight log and verify that recorded parameters are
15. g parameters on the operational test form provided Verify that the recorded parameters meet the published performance specifications for the engine as provided in the aircraft and or engine s manufacturers Service Operator s and Overhaul Manuals At the completion of any maintenance event the engine must be given a complete and thorough operational run up In some cases where adjustments have been made to the engine fuel system and or turbocharger system a test flight will be required Record all engine parameters on the operational test form and if a test flight was performed on a test flight log and verify that recorded parameters are within the specifications published for the engine and aircraft The scheduled maintenance listings in this program are formatted in a convenient check list form that may be printed and used during the performance of the inspections Note The Maintenance Schedule checklists contained in this program are intended to complement the Aircraft Manufacturer s published recommendations In addition to the items included in the pre flight and 25 hour inspection the following inspections and maintenance should be performed Note It would be considered prudent to research the Service Bulletins and AD s at this time TCM requires that all Category I Mandatory and Category II Critical Service Bulletins be complied with in accordance with the COMPLIANCE section of the Service Bulletin Category I and Category II Servi
16. iles cyril Mes Documents Panda Programme d_entretien doc MANUEL D ENTRETIEN DU POTTIER P230S PANDA ____17 Perform post inspection operational run up Verify that engine meets all performance criteria as detailed in Step 1 50 hour pre inspection operational run up and record engine parameters on operational check list Visually inspect engine and nacelle for fuel and oil leaks 18 Correct any discrepancies noted during this inspection prior to returning engine to service OBSERVATIONS C WINDOWS Profiles cyril Mes Documents Panda Programme d_entretien doc MANUEL D ENTRETIEN DU POTTIER P230S PANDA 7 Mat riels a p remption La p remption peut venir d une dur e de r elle de fonctionnement ou d une dur e de vie calendaire Les mat riels doivent tre chang s d s la premi re occurrence d une de ces deux dur es Tuyaux souples 10 ans Filtre air moteur 1000 h Filtre essence 200 h Filtre de r gulateur d air d prim 200 h Filtre d air d prim 500 h C WINDOWS Profiles cyril Mes Documents Panda Programme d_entretien doc MANUEL D ENTRETIEN DU POTTIER P230S PANDA S Annexes ESSAIS MOTEUR AU SOL C WINDOWS Profiles cyril Mes Documents Panda Programme d_entretien doc MANUEL D ENTRETIEN DU POTTIER P230S PANDA ESSAIS MOTEUR AU SOL Date Heure Effectu par Lieu D marrer le moteur conform ment au manuel de vol Pression d huile si la pression n
17. le deux sous le fuselage v rifier l tat des guignols des rotules jeux d formations D montage des habillage de cabine v rification du pied de manche des rotules et fixation graissage jeux Passage de c ble de gouverne de direction jeux usure des guides rotule graissage jeux Rotule de gouverne de direction graissage jeux 6 1 8 H lice V rification visuelle des pales pour clat V rification du serrage de l h lice D montage du c ne Serrage des vis de 4 au couple de 9 10 foots Ibs Serrage des vis de 2 au couple de 45 50 foots Ibs Remontage du c ne 6 1 9 Moteur Se conformer au 10240 series Maintenance Manual r f TCM X30621A ou aux recommandations ci dessous 6 1 10 100 HOUR INSPECTION Fuel Injected Normally Aspirated Engines SERVICING SCHEDULED MAINTENANCE Maximum efficiency and engine service life is predicated on compliance with the aircraft and engine manufacturer s required published inspection and maintenance schedule Non compliance mayresult in a loss of engine performance an increase in unscheduled maintenance and a reduction in engine service life C WINDOWS Profiles cyril Mes Documents Panda Programme d_entretien doc 6 13 MANUEL D ENTRETIEN DU POTTIER P230S PANDA Prior to any scheduled inspection the engine must be clean and a pre inspection operational run up performed Record the engine operating parameters on the operational test form provi
18. on of M87 12 Rev 1 Note To facilitate installation and removal of the oil filter place a thin film of Dow Corning DC 4 compound on the filter gasket Torque filter to values as directed by filter manufacturer ____4 Inspect ignition leads for chaffing deterioration and proper routing 5 Visually inspect magnetos for condition Inspect repair and adjust as required if magneto drop or split was not within published limits 6 Inspect exhaust system for leakage deterioration loose and missing brackets clamps and hardware 7 Correct all discrepancies noted during pre inspection operational run up 8 Perform post inspection operational run up Verify that engine meets all performance criteria as detailed in Step 1 pre inspection operational run up and record engine parameters on operational check list Visually inspect engine and nacelle for fuel and oil leaks 9 Correct any discrepancies noted during this inspection prior to returning engine to service OBSERVATIONS C WINDOWS Profiles cyril Mes Documents Panda Programme d_entretien doc MANUEL D ENTRETIEN DU POTTIER P230S PANDA C WINDOWS Profiles cyril Mes Documents Panda Programme d_entretien doc MANUEL D ENTRETIEN DU POTTIER P230S PANDA 6 Visite des 100 heures 6 1 1 Entretien courant graissage Les charni res d aileron et de volets doivent tre lubrifi avec une huile fine poss dant une propri t anticorrosion Les
19. perators and FBO s of conditions that affect safety of flight and continued airworthiness l Perform a pre inspection operational ground run up as detailed in the 50 hour inspection 2 Perform a cylinder compression test as detailed in TCM Service Bulletin M84 15 or latest revision Record the cylinder compression readings Any cylinder with compression reading below the low limit established using the Master Orifice Tool requires further inspection to determine the cause and corrective action needed to return the cylinder s to service 3 Inspect the entire engine accessory section and nacelle for indications of fuel oil or hydraulic leaks Inspect all wiring flammable fluid lines and hoses and electrical connections for proper routing support and evidence of deterioration 4 Visually inspect the induction and exhaust system for leaks cracks deterioration broken missing or loose brackets clamps and hardware 5 Visually inspect the cylinder barrels and cylinder heads for cracks and stains that may be associated with fuel or oil leaks Inspect cooling fins for restrictions to cooling air flow 6 Inspect all inner cylinder and peripheral baffling for correct installation proper positioning deterioration and missing or broken sections Note Engine service life will be negatively affected by incorrectly positioned deteriorated or missing baffles 7 Check that magneto to engine timing is with in published specifications
20. ril Mes Documents Panda Programme d_entretien doc 2 3 MANUEL D ENTRETIEN DU POTTIER P230S PANDA 3 Programme d inspection 3 1 Echelonnement des visites L chelonnement des visites est d fini en termes d heure de fonctionnement r elles ou de dates calendaires e Visite 50 h ou 6 mois tol rance 10 h ou 1 mois e Visite 100 h ou 1 ans tol rance 10 h ou 1 mois e Visite 100 h et 2 ans tol rance 10 h ou 3 mois e Visite 100 h et 4 ans Les inspections triennales pour le renouvellement du CNRA viennent en suppl ment des visites Chaque visite fait l objet d un compte rendu succinct dont un mod le est fournis en annexe Ces CR sont archiv s par le propri taire de l a ronef pendant une dur e de cinq ans 3 2 Tenu des documents avion Les documents avion sont e Le carnet de route e Le livret d a ronef e Le livret moteur 3 2 1 Le carnet de route Les pilotes y notent les vols effectu s et leur dur e ainsi que les anomalie de fonctionnement Sur le page droite les visites sont mentionn es succinctement 3 2 2 Le livret d a ronef Les pages de garde doivent tre renseign es avec les organes p remption le moteur et l h lice Dans les pages suivantes ce qui importe c est de conna tre le temps de vol cumul avant une intervention une date pr cis e Il est indispensable de mentionner toutes les visites et les r parations effectu es et les pi ces chang es 3 2 3 Le livret mot
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