# Service difficulty reports: Lycoming IO-360-M1A

A list on [Lycoming IO-360-M1A](https://openairdocs.org/engine/lycoming-io-360-m1a.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 3 · 128 reports

- [SDR 2026FA0000625](https://openairdocs.org/sdr/2026FA0000625.md): Exhaust Riser · severed · Aug 6, 2026 · N985DS · Engine Collector/Tailpipe/Nozzle
  > N985DS WAS SHOOTING APPROACHES INTO KWRI WHEN A LOUD NOISE WAS HEARD AND EXHAUST WAS SMELLED IN THE CABIN. AN IN-FLIGHT EMERGENCY WAS DECLARED AND THE AIRCRAFT LANDED. UPON EVALUATION BY MAINTENANCE IT WAS DISCOVERED THE #3 EXHAUST RISER HAD SEVERED ADJACENT
- [SDR 2025FA0000411](https://openairdocs.org/sdr/2025FA0000411.md): Attach Bolt · broken · Jun 19, 2025 · N656BC · Diamon DA40 · Main Landing Gear Attach Section
  > THE BOTTOM MOST BOLT, WASHER, AND NUT, WAS FOUND MISSING ON THE MLG AXLE WHERE THE AXLE ATTACHES TO THE LANDING GEAR LEG. BOLT P/N: LN9037-M6042, WASHER P/N: DIN125A-M6-A2, NUT P/N: DIN985-M6-A2.
- [SDR 2025FA0000279](https://openairdocs.org/sdr/2025FA0000279.md): Rocker · worn · Apr 17, 2025 · Diamon DA40 · Reciprocating Engine Cylinder Section
  > FOUND BRONZE COLORED PARTICLES IN OIL FILTER. OPENED ENGINE FOR INSPECTION AND DETERMINED THE PARTICULATES WERE FROM THE ROCKER ARM BUSHINGS. INSPECTED ALL BUSHINGS, DETERMINED INBOARD 1/3 TO 1/2 OF THE ROCKER ARM BUSHING CIRCUMFERENCE WAS WORN AND DAMAGED. BU
- [SDR 2024FA0000596](https://openairdocs.org/sdr/2024FA0000596.md): Spring · pulled · Aug 7, 2024 · Diamon DA40 · Rudder Control System
  > PILOT'S SIDE RUDDER PEDAL LATCH FRAME ASSEMBLY LEFT HAND "U" SHAPED PIN WHICH HOLDS LOWER END OF RUDDER PEDAL RETURN SPRING PULLED OUT OF LATCH FRAME. RUDDER PEDAL REMAINED EFFECTIVE BUT WOULD NOT SPRING BACK INTO NEUTRAL POSITION. FOUND DURING PREFLIGHT, FLIG
- [SDR 2024FA0000254](https://openairdocs.org/sdr/2024FA0000254.md): Starter · inoperative · Mar 22, 2024 · N787EC · Diamon DA40 · Engine Starter
  > STARTER NOT ENGAGING WITH FLYWHEEL RING GEAR.
- [SDR 2024FA0000241](https://openairdocs.org/sdr/2024FA0000241.md): Bulkhead · worn · Mar 21, 2024 · N415KG · Diamon DA40 · Propeller Hub Section
  > SIX-INCH CRACK EMANATING FROM OUTSIDE EDGE AND RIVETS SHEARED ON REINFORCEMENT PLATE.
- [SDR 2024FA0000244](https://openairdocs.org/sdr/2024FA0000244.md): Ignition Switch · worn · Mar 21, 2024 · N655DS · Diamon DA40 · Ignition System
  > DIFFICULTY TURNING KEY BETWEEN POSITIONS AND DIFFICULTY REMOVING KEY FROM SWITCH.
- [SDR 2023FA0000852](https://openairdocs.org/sdr/2023FA0000852.md): Pump · inoperative · Dec 27, 2023 · N304AF · Diamon DA40 · Engine Fuel Pump
  > 5100-00-9CJ (NEW) FAILED AFTER 12 HOURS (TACH TIME). THE AUX FUEL PUMP IS REQUIRED DURING ENGINE START, TAKE-OFF, AND LANDING ONLY. THIS FAILURE OCCURRED DURING ENGINE START, WITH BATTERY ON AND FUEL PUMP SWITCH ACTIVATED; THE 5-AMP C/B POPS AFTER APPROX. 5 SE
- [SDR 2022FA0000628](https://openairdocs.org/sdr/2022FA0000628.md): Damper · unserviceable · Mar 30, 2022 · N285DS · Diamon DA40 · Nose/Tail Landing Gear
  > WHILE DISASSEMBLING NLG ELASTOMER PACK FOUND NLG DAMPER ROD TO BE EXTREMELY WORN. MEASURED WARE TO BE ~2MM OF MISSING MATERIAL. PER SB40-082 THIS IS OUT OF LIMITS. IF WEAR CONTINUED, NLG STRUT COULD BECOME DISATTACHED FROM CENTER ENGINE MOUNT ATTAC POINT, AT T
- [SDR 2021FA0000220](https://openairdocs.org/sdr/2021FA0000220.md): Probe · leaking · Aug 5, 2021 · N79US · Diamon DA40 · Engine Oil Temperature
  > OIL TEMP PROBE LEAKING OIL THROUGH WIRE CONNECTION PINS
- [SDR 2021FA0000055](https://openairdocs.org/sdr/2021FA0000055.md): Truss · cracked · Feb 23, 2021 · N636AT · Diamon DA40 · Engine Mount Section
  > DURING POWER PLANT INSPECTION. ENGINE TRUSS WAS NOTED TO BE CRACKED AT THE LOWER LEFT ENGINE SHOCK MOUNT ATTACH POINT IN THE WELDED AREA (GUSSET TUBE).
- [SDR 2021FA0000058](https://openairdocs.org/sdr/2021FA0000058.md): Cylinder Head · separated · Feb 22, 2021 · N59LU · Diamon DA42 · Reciprocating Engine Cylinder Section
  > LEFT ENGINE NR 2 CYLINDER HEAD SEPARATION ORIGINATING FROM BOTTOM SPARK PLUG HOLE. ENGINE OVERHAUL WITH FACTORY NEW CYLINDERS PERFORMED BY POPLAR GROVE CRS YYBR664L WO 6165 4/15/2014.
- [SDR 2020FA0000132](https://openairdocs.org/sdr/2020FA0000132.md): Exhaust Pipe · cracked · Feb 6, 2020 · N979DS · Amtr V100 · Engine Exhaust System
  > #2 CYLINDER EXHAUST PIPE RISER CRACKED
- [SDR 2019FA0000246](https://openairdocs.org/sdr/2019FA0000246.md): Bracket · damaged · Aug 7, 2019 · N569DS · Diamon DA40 · DC Generator-Alternator
  > ALTERNATOR ATTACHMENT BRACKET MOUNTING HOLES ELONGATED CAUSING THE ALTERNATOR FAN/FLYWHEEL TO GRIND AGAINST THE ALTERNATOR ATTACHMENT BRACKET LEADING TO ALTERNATOR FAILURE. THIS ENGINE WAS RECENTLY OVERHAULED AND HAD ONLY 80 HOURS SINCE OVERHAUL. THE FRONT BUS
- [SDR 2019FA0000137](https://openairdocs.org/sdr/2019FA0000137.md): Fuel Sys · low pressure · May 3, 2019 · N127KC · Diamon DA40 · Fuel Controlling System
  > DURING CRUISE FLIGHT PILOTS GOT THE RED LOW FUEL PRESSURE WARNING AND ENGINE STARTED SPUTTERING THE PILOTS TURNED ON ELECTRIC FUEL PUMP AND PRESSURED WAS RESTORED TO NORMAL AND THE ENGINE STARTED TO RUNNING NORMAL. COULD NOT DUPLICATE ON GROUND RUNS. INSPECTED
- [SDR 2019FA0000138](https://openairdocs.org/sdr/2019FA0000138.md): Fuel Sys · pressure loss · May 3, 2019 · N118GM · Diamon DA40 · Fuel Controlling System
  > DURING CLIMB FLIGHT PILOTS GOT THE RED LOW FUEL PRESSURE WARNING.THE PILOTS TURNED ON ELECTRIC FUEL PUMP AND PRESSURED WAS RESTORED TO NORMAL. COULD NOT DUPLICATE ON GROUND RUNS. INSPECTED FOR CLEAN FUEL SYSTEM NO PROBLEMS WHERE NOTED INSTALLED NEW MECHANICAL
- [SDR 2019FA0000134](https://openairdocs.org/sdr/2019FA0000134.md): Fork · cracked · Mar 29, 2019 · N526DS · Diamon DA40 · Nose/Tail Landing Gear
  > 100 HRS. INSPECTION REVEALED CRACK IN NLG. THIS PART WAS INSTALLED LESS THAN 300 HRS AGO TO REPLACE A BROKEN NLG THAT RESULTED IN A PROP STRIKE. THIS PART IS NOT PART OF THE CURRENT AD (THE PREVIOUS PART WAS).
- [SDR CA190925009](https://openairdocs.org/sdr/CA190925009.md): Pump · low pressure · Jan 27, 2019 · Diamon DA40 · Engine Fuel Pump
  > (CAN) OVER U78 RED MESSAGE SAID LOW FUEL PRESSURE AND ENGINE SPUTTERED 2X ON R TANK. TURNED ON AUX PUMP AND SWITCHED TO L, NO MORE ISSUES. (TC# 20190925009)
- [SDR CA190925011](https://openairdocs.org/sdr/CA190925011.md): Pump · low pressure · Dec 21, 2018 · Diamon DA40 · Engine Fuel Pump
  > (CAN) LOW FUEL PRESSURE WARNING TURNED ELECTRIC PUMP ON, PRESSURE WENT TO 26-28. TURNED ELECTRIC OFF, PRESSURE FELL TO 19. ELECTRIC PUMP REMAINED ON. (TC# 20190925011)
- [SDR CA190424007](https://openairdocs.org/sdr/CA190424007.md): Bellows · malfunctioned · Jun 19, 2018 · Diamon DA40 · Fuel Control/Reciprocating Engines
  > (CAN) CUSTOMER REPORTED THEY HAD AN IO360-M1A SHUTDOWN ON TAXI. THE COMPONENT SHOP SUSPECTED THE BELLOW (P/N: 2576568-1) FROM THE FUEL INJECTOR SYSTEM BEING THE ISSUE. (TC# 20190424007)
- [SDR 2019FA0000135](https://openairdocs.org/sdr/2019FA0000135.md): Fork · broken · Apr 30, 2018 · N526DS · Diamon DA40 · Nose/Tail Landing Gear
  > NLG BROKE WHILE PERFORMING BRAKE CHECK ON RAMP CAUSING PROP STRIKE. THIS PART WAS INSPECTED REGULARLY AS PART OF A CURRENT AD.
- [SDR B4VR201709250001](https://openairdocs.org/sdr/B4VR201709250001.md): Transducer · shorted · Sep 22, 2017 · N4129M · Diamon DA42 · Engine Fuel Indicating System
  > LEFT HAND ENGINE FUEL FLOW TRANSDUCER FAILED ON FIRST FLIGHT. TRANSDUCER WAS TROUBLESHOT AND DETERMINED TO HAVE INTERNALLY SHORTED WHICH CAUSED ALL OF THE LEFT HAND ENGINE INSTRUMENTS TO "RED X" ON THE G1000 DISPLAY IN FLIGHT.
- [SDR 2017FA0000458](https://openairdocs.org/sdr/2017FA0000458.md): Leg Assy · cracked · Aug 18, 2017 · N591CA · Diamon DA40 · Nose/Tail Landing Gear
  > FOUND THE NOSE GEAR LEG WITH A CRACK, FOUND USING DYE PENETRANT INSPECTION.
- [SDR 2017FA0000307](https://openairdocs.org/sdr/2017FA0000307.md): Leg Assy · cracked · Jul 17, 2017 · N591CA · Diamon DA40 · Nose/Tail Landing Gear
  > THE AIRCRAFT WAS FOUND TO HAVE A NOSE GEAR LEG WITH A CRACK FOUND USING DYE PENETRANT INSPECTION METHOD. INSPECTION WAS PERFORMED AS A SAFETY MEASURE TO CHECK FOR CRACKING AS A RESULT OF THE PART FAILING ON ANOTHER AIRCRAFT WHICH RESULTED IN DAMAGE. THIS GEA
- [SDR 2016FA0000627](https://openairdocs.org/sdr/2016FA0000627.md): Transducer · inaccurate · Dec 12, 2016 · N424TS · Diamon DA42 · Engine Indicating System
  > INACCURATE READINGS FROM RIGHT ENGINE FUEL PRESSURE TRANSDUCER. TRANSDUCER HAS ONLY 307.9 HOURS SINCE NEW. NEW TRANSDUCER WAS INSTALLED AND INDICATION ISSUES WENT AWAY.
- [SDR B4VR121216A](https://openairdocs.org/sdr/B4VR121216A.md): Transducer · inaccurate · Dec 10, 2016 · N424TS · Diamon DA42 · Aircraft Fuel Distribution System
  > INACCURATE READINGS FROM RIGHT ENGINE FUEL PRESSURE TRANSDUCER. TRANSDUCER HAS ONLY 307.9 HOURS SINCE NEW. NEW TRANSDUCER WAS INSTALLED AND INDICATION ISSUES WENT AWAY.
- [SDR 2016FA0000416](https://openairdocs.org/sdr/2016FA0000416.md): Spring · failed · Sep 8, 2016 · N4117H · Diamon DA40 · Passenger/Crew Doors
  > GAS COMPRESSION SPRING FAILED TO MAINTAIN THE DOOR LATCH IN A CLOSED POSITION. DURING CRUISE THE DOOR UNLATCHED. AFTER SHORT TIME IN FLIGHT SAFETY CATCH FAILED CAUSING THE DOOR TO OPEN. WHEN THE DOOR OPENED BOTH HINGES FAILED, CAUSING THE DOOR TO FULLY SEPA
- [SDR 2016FA0000300](https://openairdocs.org/sdr/2016FA0000300.md): Blade · loose · Jun 20, 2016 · N449DS · Diamon DA42 · Propeller Blade Section
  > RT PROPELLER BLADE FOUND LOOSE IN HUB DURING INSPECTION. TRAVEL IS.4375" IN DIRECTION OF THRUST AND.5" IN ROTATIONAL DIRECTION. THE SHIM UNDER THE BLADE SNAP RING WAS FOUND ABOVE SNAP RING. PROPELLER SENT FOR REPAIR.
- [SDR 2016FA0000660](https://openairdocs.org/sdr/2016FA0000660.md): Boss · failed · Jun 1, 2016 · N807E4 · Diamon DA40 · Reciprocating Engine Cylinder Section
  > ENGINE BEGAIN TO RUN ROUGH, MADE A PRECAUTIONARY LANDING. FOUND THE BOSS FOR THE ROCKER SHAFT HAD FAILED.
- [SDR 2016FA0000375](https://openairdocs.org/sdr/2016FA0000375.md): Cowling · damaged · May 26, 2016 · N617DS · Diamon DA40 · Engine Cowling System
  > ENGINE COWL HEAT DAMAGED BY EXHAUST SYS RADIATION HEAT. DURING ANNUAL INSPECTION, BOTTOM ENGINE COWL WAS REMOVED AND FOUND TO BE HEAT DAMAGED AS A RESULT OF THE FAILURE AND SEPARATION OF THE WATER BASE COATING APPLIED TO THE FIBERGLASS MATERIAL THE COWLING IS
- [SDR DU0S2016FA0000130](https://openairdocs.org/sdr/DU0S2016FA0000130.md): Servo · abnormal · Mar 11, 2016 · N226DS · Diamon DA42 · Fuel Controlling System
  > FUEL INJECTOR REMOVED FOR BEING EXCESSIVE RICH. THIS INJECTOR IS A NEW UNIT WITH 405 TTSN. IAW MFG CHECK LIST, THE ENGINE IS LEANED AT 2200 RPM TO PEAK. AFTER LEANING THE THROTTLE S RETARDED TO 2200 RPM, THE NORMAL RISE IS 40-50 RPM. THIS WAS IN EXCESS OF 2
- [SDR DU0S2016FA0000131](https://openairdocs.org/sdr/DU0S2016FA0000131.md): Servo · abnormal · Mar 11, 2016 · N226DS · Diamon DA42 · Fuel Controlling System
  > FUEL INJECTOR REMOVED FOR EXCESSIVE RICHNESS IAW MFG CHECKLIST, THE MAG CHECK IS DONE AT 2200 RPM. THE MIXTURE IS LEANED TO PEAK RPM THEN ADJUSTED TO 2200 RPM. THE PEAK IS NORMALLY 40-50 RPM. THIS WAS IN EXCESS OF 200 RPM. AT O/H THE REPAIR STATION REPORTE
- [SDR DU0S2016FA0000132](https://openairdocs.org/sdr/DU0S2016FA0000132.md): Servo · abnormal · Mar 11, 2016 · N388DS · Diamon DA42 · Fuel Controlling System
  > FUEL INJECTOR DURING O/H. IAW THE MFG CHECKLIST MAG CHECK IS AT 2200 RPM. MIXTURE IS LEANED TO PEAK, RPM THEN RETARDED TO 2200 RPM. WHEN LEANED, NORMAL RISE IS 40-50 RPM. THIS WAS IN EXCESS OF 200 RPM. THE REPAIR STATION REPORTED RICHNESS. AT 513TT INJECTOR
- [SDR DU0S2016FA0000133](https://openairdocs.org/sdr/DU0S2016FA0000133.md): Servo · abnormal · Mar 11, 2016 · N388DS · Diamon DA42 · Fuel Controlling System
  > FUEL INJECTOR WAS DETERMINED TO BE EXCESSIVELY RICH. IAW MFG CHECKLIST MAG CHECK IS AT 2200 RPM. MIXTURE IS LEANED TO PEAK THEN THROTTLE RETARDED TO 2200 RPM. THIS RISE SHOULD BE 40-50 RPM. THIS WAS AROUND 200 RPM. REPAIR STATION FOUND UNIT RICH AT BOTTOM
- [SDR 2015FA0000466](https://openairdocs.org/sdr/2015FA0000466.md): Seal · broken · Sep 25, 2015 · N584MT · Diamon DA40 · Magneto/Distributor
  > FOLLOWING A SCHEDULED INSPECTION THE AIRCRAFT WAS RUN AND HAD A BAD MAGNETO CHECK. WHEN THE MAGNETO WAS REMOVED FROM THE ENGINE AND TURNED VERTICALLY TO CLEAR THE ENGINE MOUNT OIL POURED OUT OF THE MAGNETO. THE MAGNETO WAS OPENED TO SEE IF THE OIL SEAL WAS THE
- [SDR 2015FA0000457](https://openairdocs.org/sdr/2015FA0000457.md): Magneto · separated · Sep 18, 2015 · N583MT · Diamon DA40 · Magneto/Distributor
  > WHILE TAKING OFF, A RPM LOSS OF ABOUT 100 RPMS WAS NOTICED. THE ACFT RETURNED AND LANDED. WHILE TAXING BACK IN THE RPMS WOULD VARY WITHOUT ADJUSTING THE THROTTLE. THE POWER LOSS WAS REPORTED TO MAINTENANCE. WHILE RUNNING THE ACFT TO TROUBLESHOOT THE PROBLEM
- [SDR 2015FA0000436](https://openairdocs.org/sdr/2015FA0000436.md): Magneto · inoperative · Aug 27, 2015 · N583MT · Diamon DA40 · Magneto/Distributor
  > AFTER A NORMAL RUNUP, PRIOR TO TAKEOFF THE ACFT ENGINE FAILED TO PROVIDE FULL POWER AND STARTED TO MISS ON TAKEOFF ROLL. THE TAKEOFF WAS ABORTED AND THE ACFT RETURNED TO THE RAMP. A TIMING CHECK WAS DONE AND MAGNETO, PN 4370, SN 14061319, WAS FOUND TO HAVE
- [SDR 2015FA0000399](https://openairdocs.org/sdr/2015FA0000399.md): Wire · shorted · Aug 21, 2015 · N566DS · Diamon DA40 · Electrical Power System Wiring
  > ALTERNATOR OUTPUT WIRE, SHORTED BETWEEN THE INNER CABLE AND OUTER SHIELDING, CAUSING FAILURE OF THE TIE BUSS CIRCUIT BREAKERS AND DAMAGE TO ASSOCIATED WIRES IN HARNESS. DAMAGE TO HARNESS CAUSED SHORT TO ENGINE DATA UNIT AND COMPLETE FAILURE OF THE ENGINE INSTR
- [SDR 2015FA0000357](https://openairdocs.org/sdr/2015FA0000357.md): Pump · leaking · Jul 28, 2015 · N289DS · Diamon DA40 · Fuel Boost Pump
  > ENGINE DRIVEN FUEL PUMP FAILED AFTER 80.9 HOURS, TOTAL TIME AND 6 WEEKS. THE PILOT NOTED THAT THE ENGINE RAN ROUGH DURING TAXI FOR DEPARTURE BUT CLEARED UP PRIOR TO RUN-UP. AFTER THE FLIGHT THE PUMP WAS TESTED BY PRESSURIZING THE SYSTEM WITH THE BOOST PUMP
- [SDR GM8S201505290246](https://openairdocs.org/sdr/GM8S201505290246.md): Distributor Gear · loose · May 12, 2015 · N58LU · Diamon DA42 · Magneto/Distributor
  > DURING FLIGHT, ACFT HAD AN ENGINE POWER LOSS. DISCOVERED THE MAGNETO TO HAVE A LOOSE DISTRIBUTOR ARM, WHICH CAUSED THE MAGNETO TO FAIL.
- [SDR GM8S2015052900248](https://openairdocs.org/sdr/GM8S2015052900248.md): Distributor Gear · loose · May 12, 2015 · N58LU · Diamon DA42 · Magneto/Distributor
  > DURING FLIGHT, ACFT HAD AN ENGINE POWER LOSS. DISCOVERED THE MAGNETO TO HAVE A LOOSE DISTRIBUTOR ARM, WHICH CAUSED THE MAGNETO TO FAIL.
- [SDR CA8S2015FA0000137](https://openairdocs.org/sdr/CA8S2015FA0000137.md): Magneto · broken · Mar 13, 2015 · N586MT · Diamon DA40 · Magneto/Distributor
  > WHEN THE PILOT PERFORMED THE RUNUP AND SELECTED THE LT MAGNETO, THE ENGINE QUIT AND COULD NOT BE RESTARTED. THE AIRCRAFT WAS SENT TO MAINTENANCE. MAINTENANCE WAS UNABLE TO START THE ACFT AND IT WAS FOUND THAT THE LT MAGNETO WAS COMPLETELY DEAD. THE LT MAGNET
- [SDR CA141217005](https://openairdocs.org/sdr/CA141217005.md): Blade · cracked · Dec 15, 2014 · Diamon DA40 · Propeller Blade Section
  > (CAN) OWNER REPORTED TO DIAMOND CANADA THAT HE FOUND ONE OF THE THREE PROPELLER BLADES SPLIT OPEN AT ROOT SECTION. SPLIT APPROX. FOUR INCHES IN LENGTH. BLADES HAD BEEN OVERHAULED AT 216.5 HOURS TOTAL TIME, CRACKED DISCOVERED AT 360 HOURS. TIME SINCE OVERHAUL 1
- [SDR U43R2014FA0000509](https://openairdocs.org/sdr/U43R2014FA0000509.md): Bracket · cracked · Aug 27, 2014 · N845RB · Cirrus SR22 · Fuselage Main, Structure
  > PROPELLER CONTROL CABLE BRACKET BROKEN WHICH CHAFES THE CONTROL CABLE.
- [SDR U43R2014FA0000508](https://openairdocs.org/sdr/U43R2014FA0000508.md): Bracket · cracked · Aug 22, 2014 · N845RB · Cirrus SR22 · Fuselage Main, Structure
  > PROPELLER GOVERNOR CONTROL CABLE BRACKET BROKEN AND CHAFED.
- [SDR CA140807011](https://openairdocs.org/sdr/CA140807011.md): Support Bracket · damaged · Jul 26, 2014 · Diamon DA40 · Engine Exhaust System
  > (CAN) AIRCRAFT WAS IN CRUISE CONFIGURATION RETURNING TO BASE. PILOT REPORTED "POPPING SOUND COMING FROM ENGINE". INVESTIGATION DETERMINED THAT THE FOLLOWING EXHAUST PARTS HAD FAILED: SUPPORT BRACKET P/N D41-7806-20-02, MUFFLER BRACE P/N D41-7806-20-01, #2 RISE
- [SDR CA140125001](https://openairdocs.org/sdr/CA140125001.md): Distributor Gear · broken · Jan 24, 2014 · Diamon DA40 · Magneto/Distributor
  > (CAN) FOUND THE ELECTRODE ON THE DISTRIBUTOR GEAR LOOSE AND THE ROTOR GEAR LOOSE ON MAGNETO SHAFT.
- [SDR CA131029006](https://openairdocs.org/sdr/CA131029006.md): Tire · abnormal · Oct 25, 2013 · Diamon DA42 · Tire
  > (CAN) LT TIRE WAS INTERFERRING WITH WING SKIN DURING EXTENSION, PREVENTING GEAR FROM EXTENDING. THE TIRE INSTALLED WAS A RETREAD. THE MAINTAINER INSTALLED A NEW TIRE IAW AND PROBLEM WAS CORRECTED.
- [SDR 2013FA0000422](https://openairdocs.org/sdr/2013FA0000422.md): Starter · failed · Jul 26, 2013 · Cirrus SR20 · Engine Starter
  > AFTER A 1.5 HOURS FLIGHT, CREW SHUTDOWN AIRCRAFT AND NOTICED OIL LEAKING FROM UNDER ENGINE COWLING. DISCOVERED STARTER HAD SEPARATED FROM ADAPTER BUT HAD NOT LEFT THE ENGINE COMPARTMENT. DID NOT HEAR ANY STRANGE SOUNDS DURING THE START OR THROUGH OUT FLIGHT.
- [SDR 2013FA0000417](https://openairdocs.org/sdr/2013FA0000417.md): Exhaust Header · damaged · Jul 18, 2013 · Cirrus SR20 · Engine Collector/Tailpipe/Nozzle
  > NR 1 EXHAUST HEADER SUPPORT BRACKET HOLE ELONGATED. BOLT CHAFED AND REPLACED.

Next page: https://openairdocs.org/engine/lycoming-io-360-m1a/reports.md?page=2

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
WHERE engine_model_key = 'IO360M1A'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/engine/lycoming-io-360-m1a/reports

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