# Service difficulty reports: Eci O360A1A

A list on [Eci O360A1A](https://openairdocs.org/engine/eci-o360a1a.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 3 · 103 reports

- [SDR 2023FA0000625](https://openairdocs.org/sdr/2023FA0000625.md): Cylinder · separated · Jun 19, 2023 · N2838L · Cessna 172H · Reciprocating Engine Cylinder Section
  > CYL €¢3 DEVELOPED/, CRACK IN THE CYLINDER HEAD BETWEEN COOLING FINS IIPPROXIMATEL Y 1 625 INCHED ABOVE LOWEST FINE AT HE/ID/ 81\RREL ATTACHMENT. IOCIITED IN LOWER CORNEER EDGE OF CLINDER HEAD ON INTAKE VALVE SIDE. PILOT NOFLCED CYL HEAD !HIP RISINC, TO APPR
- [SDR 2018FA0000176](https://openairdocs.org/sdr/2018FA0000176.md): Exhaust Stack · blocked · Jun 13, 2018 · N5832P · Piper PA24180 · Engine Collector/Tailpipe/Nozzle
  > A COMPLETE EXHAUST SYSTEM REPAIR AND OVERHAUL. REINSTALLED ON AIRCRAFT. PERFORMED A RUN-UP OF ENGINE AND EXPERIENCED INCREASED VIBRATION LEVELS AND LOW EGT READINGS ON THE NR 3 CYLINDER. AN AUDIBLE, METALLIC-SOUNDING PING COULD BE HEARD IN THE CABIN AND FROM
- [SDR 2018FA0000122](https://openairdocs.org/sdr/2018FA0000122.md): Turnbuckle · separated · Mar 31, 2018 · N5910R · Cessna 172G · Aileron Control System
  > AIRCRAFT LOST AILERON CONTROL IN FLIGHT, DECLARED EMERGENCY AND LANDED. AFTER SHUTDOWN THE SEPARATED CABLE FOR LEFT AILERON FROM TURNBUCKLE SWEDGED FITTING UNDER RIGHT SIDE OF COCKPIT PANEL WAS DISCOVERED. AIRCRAFT GROUNDED.
- [SDR 2017FA0000047](https://openairdocs.org/sdr/2017FA0000047.md): Spark Plug · departed · Feb 7, 2017 · N6260Z · Piper PA25 · Spark Plug/Igniter
  > DURING CRUISE, THE NR 3 CYLINDER, LOWER SPARK PLUG, DEPARTED THE ENGINE, CAUSING A SUBSTANTIAL LOSS OF POWER. THE SUSPECT SPARK PLUG WAS RECOVERED, AND WAS FOUND TO HAVE THE HELICOIL FROM THE CYLINDER STILL FIRMLY ATTACHED.
- [SDR 2015FA0000305](https://openairdocs.org/sdr/2015FA0000305.md): B-Nut · loose · Jun 30, 2015 · N6194J · Piper PA28181 · Engine Fuel Distribution
  > ENGINE FIRE DURING START UP. FIRE EXTINGUISHED ON GROUND. INSPECTED ENGINE COMPARTMENT AFTER FIRE AND FOUND THAT FLEXIBLE FUEL LINE FROM FUEL PUMP TO CARBURETOR HAD COME LOOSE AT THE B-NUT ON ENGINE DRIVEN FUEL PUMP AND WAS LEAKING FUEL.
- [SDR 2012FA0000698](https://openairdocs.org/sdr/2012FA0000698.md): Exhaust Stack · eroded · Sep 23, 2012 · N7059P · Piper PA24 · Engine Collector/Tailpipe/Nozzle
  > THE PILOT MADE AN INTENTIONAL GEAR-UP LDG AFTER SEVERAL UNSUCCESSFUL ATTEMPTS TO FULLY EXTEND THE LANDING GEAR. FOLLOW-UP INSPECTION OF THE ACFT REVEALED THAT A SECTION OF THE LEFT-FRONT EXHAUST STACK ASSY HAD FAILED AND SEPARATED FROM THE ENGINE EXHAUST SYS,
- [SDR CA120711007](https://openairdocs.org/sdr/CA120711007.md): Crankshaft · failed · Jun 22, 2012 · Reciprocating Engine Power Section
  > (CAN) CUSTOMER BROUGHT ENGINE TO US AFTER 40HRS SINCE MAJOR O/H. THE CUSTOMER WAS SOLD A CRANKSHAFT AND CONNECTING RODS, FROM AN ENGINE SHOP. THE ENGINE WAS DECLARED TO BE AN O/H AND INSTALLED HIS ENGINE. AT 38.1 HRS SINCE O/H THE CUSTOMERS ENGINE STOPPED DU
- [SDR CA120104011](https://openairdocs.org/sdr/CA120104011.md): Step · cracked · Dec 30, 2011 · Amtr RV6A · Fuselage Main, Structure
  > (CAN) RIGHT PASSENGER STEP CRACKED BETWEEN ARM AND PLATE ON THE LOWER SURFACE ADJACENT TO THE WELD. CRACK LENGTH APPROXIMATELY 1 INCH. TOTAL TIME ON PART 202 HOURS.
- [SDR CA110919002](https://openairdocs.org/sdr/CA110919002.md): Cable · shorted · Sep 6, 2011 · Piper PA28151 · Equipment/Furnishings Wiring
  > (CAN) THE CABLE THAT RUNS FROM THE ELT REMOTE SWITCH TO THE ELT HAD A SHORT IN IT. THIS WAS CAUSING THE ELT TO ACTIVATE IN FLIGHT AND OR ON THE GROUND.
- [SDR 2010FA0000386](https://openairdocs.org/sdr/2010FA0000386.md): Carburetor · defective · Apr 16, 2010 · N68RS · Amtr RV7A · Fuel Control/Reciprocating Engines
  > PARTIAL LOSS OF POWER ON DEPARTURE AT 1,000` AGL. AFTER RETURNING TO LAND, ENGINE ROUGHNESS INCREASED. DURING TAXI IN, MAX ATTAINABLE RPM WAS 900. MECHANIC TROUBLESHOT AND DETERMINED THE PROBLEM TO BE FUEL STARVATION. FUEL SUPLY TO THE CARBURETOR WAS NORM
- [SDR CA090706007](https://openairdocs.org/sdr/CA090706007.md): B-Nut · loose · Jul 5, 2009 · Cessna 172M · Reciprocating Engine Oil System
  > (CAN) IN FLIGHT, PILOT NOTICED THE OIL PRESSURE GAUGE FLUCTUATING. PILOT TURNED AROUND AND RETURNED TO DEPARTURE. WHILE RETURNING, OIL PRESSURE DROPPED TO 0 AND OIL TEMP CLIMBED TO RED LINE. PILOT SHUTDOWN ENG AND GLIDED BACK TO AIRPORT. ON TROUBLESHOOTING,
- [SDR 2008FA0000535](https://openairdocs.org/sdr/2008FA0000535.md): Downlock · worn · Jul 30, 2008 · N74542 · Mooney M20B · Landing Gear Selector
  > LANDING GEAR LEVER BECAME DISENGAGED FROM THE DOWN LOCK LATCHING ASSY ON THE PILOT`S LOWER CENTER INSTRUMENT PANEL. AC WAS ON THE GROUND DURING LANDING ROLLOUT. THIS ALLOWED GEAR TO COLLAPSE. SB M20-88B, 5/10/94. (K)
- [SDR 2008FA0000547](https://openairdocs.org/sdr/2008FA0000547.md): Downlock · worn · Jun 28, 2008 · N74542 · Mooney M20B · Landing Gear Position and Warning
  > LANDING GEAR LEVER BECAME DISENGAGED FROM THE DOWNLOCK LATCHING ASSY ON THE PILOT`S LOWER CENTER INSTRUMENT PANEL. AC WAS ON THE GROUND DURING LANDING ROLLOUT. THIS ALLOWED GEAR TO COLLAPSE, SB M20-88B, 5-10-94. (K)
- [SDR 2008FA0000105](https://openairdocs.org/sdr/2008FA0000105.md): Fitting · broken · Dec 4, 2007 · N723C · Piper PA18 · Main Landing Gear Strut/Axle/Truck
  > PILOT STATED THAT HE PERFORMED AN OFF AIRPORT LANDING ALONG A BEACH WHILE HUNTING. UPON LANDING, THE UPPER RT MLG CABANE FITTING BROKE. THE LANDING GEAR SAFETY CABLES PREVENTED A TOTAL GEAR COLLAPSE. (K)
- [SDR 2007FA0001084](https://openairdocs.org/sdr/2007FA0001084.md): Nose Rib · cracked · Nov 9, 2007 · N9349Y · Beech B95 · Trailing Edge Flaps
  > IN-FLIGHT, PILOT LOWERED FLAPS AND AIRCRAFT STARTED TO ROLL TO THE RT. PILOT NOTICED RT FLAP WAS RETRACTED, HE THEN RETRACTED FLAP HANDLE. AIRCRAFT LANDED SAFELY, WITHOUT INCIDENT. UPON INSPECTION, FOUND RT FLAP ROD ATTACH BRACKET BROKEN AND FLAP NOSE RIB N
- [SDR 2007FA0001010](https://openairdocs.org/sdr/2007FA0001010.md): Pipe · failed · Nov 1, 2007 · N7066B · Piper PA18150 · Engine Collector/Tailpipe/Nozzle
  > LEADING EDGE EXHAUST SYSTEM INSTALLED BY STC SA02200AK FAILED AT THE SAIL PIPE TO MUFFLER WELD. SYSTEM HAS 36 HOURS SINCE NEW. (K)
- [SDR CA070419005](https://openairdocs.org/sdr/CA070419005.md): Bracket · cracked · Apr 12, 2007 · Cessna 172D · Rudder Structure
  > (CAN) DURING THE ANNUAL INSPECTION, BOTH RUDDER HINGE BRACKETS WERE FOUND TO BE CRACKED. RUDDER WAS REMOVED AND REINSTALLED AFTER REPAIRS. PN 0531018-1 AND 0531018-2 WERE REPLACED WITH NEW IAW THE MM. (TC NR 20070419005)
- [SDR CA070110003](https://openairdocs.org/sdr/CA070110003.md): Torque Link · cracked · Dec 20, 2006 · Cessna 172D · Nose/Tail Landing Gear Strut/Axle
  > (CAN) PRIOR TO INSTALLATION ON AIRCRAFT, NOSE GEAR SHOCK STRUT ASSEMBLY WAS THOROUGHLY INSPECTED. SEVERAL CRACKS WERE FOUND ON UPPER TORQUE LINK. NEW MFG PART WAS INSTALLED. (TC NR 20070110003)
- [SDR 2006FA0000260](https://openairdocs.org/sdr/2006FA0000260.md): Oil Cooler · split · Mar 6, 2006 · N5496H · Cessna 172M · Engine Oil Cooler
  > DURING ROUTINE RUN-UP FOLLOWING AN OIL CHANGE, AN IMMEDIATE EXPULSION OF SEVERAL QUARTS OF OIL OCCURRED IN SECONDS. (K)
- [SDR AU510001642](https://openairdocs.org/sdr/AU510001642.md): Piston Ring · delaminated · Dec 12, 2005 · Socata TB10TOBAGO · Reciprocating Engine Power Section
  > (AUS) ENGINE CYLINDERS (4OFF) HAD TOP PISTON RINGS DELAMINATING. PLASMA FACE SECTION COMING AWAY FROM BASE MATERIAL. ALL 4 CYLINDERS ALSO HAD EXCESSIVELY WORN EXHAUST VALVE GUIDES AND 2 EXHAUST VALVES REQUIRED REPLACEMENT. (CASA NR 510001642)
- [SDR AU510001679](https://openairdocs.org/sdr/AU510001679.md): Piston Ring · delaminated · Dec 12, 2005 · Socata TB10TOBAGO · Reciprocating Engine Power Section
  > TOP COMPRESSION RINGS ON ALL PISTONS DELAMINATING.
- [SDR AU510001711](https://openairdocs.org/sdr/AU510001711.md): Piston Ring · deteriorated · Dec 12, 2005 · Socata TB10TOBAGO · Reciprocating Engine Power Section
  > NR 2 CYLINDER PISTON TOP COMPRESSION RING PLASMA COATING DELAMINATING. TOP RINGS ON ALL OTHER PISTONS SHOWING SIGNS OF DELAMINATION BEGINNING TO OCCUR.
- [SDR AU510001823](https://openairdocs.org/sdr/AU510001823.md): Hinge · corroded · Dec 12, 2005 · Socata TB10TOBAGO · Rudder Structure
  > FOUND TOP RUDDER HINGE CORRODED.
- [SDR AU510001824](https://openairdocs.org/sdr/AU510001824.md): Mount · cracked · Dec 12, 2005 · Socata TB10TOBAGO · Engine Mount Section
  > ENGINE MOUNT CRACKED. FOUND DURING INSPECTION IAW AD/TB10/8 AND TBSB NO 16/1.
- [SDR AU510001825](https://openairdocs.org/sdr/AU510001825.md): Hinge · corroded · Dec 12, 2005 · Socata TB10TOBAGO · Elevator Structure
  > RT STABILATOR HINGE CORRODED, AD/SB DESC: CASA SCHEDULE 5.
- [SDR 2005FA0001597](https://openairdocs.org/sdr/2005FA0001597.md): Engine · malfunctioned · Dec 10, 2005 · N20EA · Amtr RV8 · Engine (Reciprocating)
  > FORCED LANDING, DUE TO ENG FAIL DURING TAKEOFF. DAMAGE TO AC INCLUDED LT MLG WAS BROKEN, LT WING TIP SKIN DENTED, LWR ENG COWLING DAMAGED. DAMAGE TO AC WAS CONSIDERED TO BE MINOR. INSP OF AC REVEALED LT FUEL TANK WAS FULL OF FUEL; FUEL QTY IN RT FUEL TANK C
- [SDR CA050121005](https://openairdocs.org/sdr/CA050121005.md): Fitting · cracked · Nov 25, 2004 · Conaer LA4 · Horizontal Stabilizer Structure
  > (CAN) DURING ANNUAL INSP, IT WAS NOTICED THAT AC DID NOT COMPLY WITH REQUIREMENTS OF AD98-10-12 WITH REF TO SB78 HORIZONTAL STABILIZER INSP AND REWORK. AD98-10-12 WAS SIGNED OUT IN THE TECH RECORDS ON SEPT 1,1998 AT 1683.22 TT. REMOVAL OF FITTINGS REVEALED P/N
- [SDR 2004FA0000782](https://openairdocs.org/sdr/2004FA0000782.md): Cap · clogged · Sep 23, 2004 · N8214Y · Piper PA28181 · Fuel Storage
  > PILOT EXPERIENCED FUEL INTERRUPTION TO ENGINE WHILE ENROUTE. SWITCHED FUEL TANKS AND ENGINE QUIT. MADE EMERGENCY LANDING. REMOVED AC FROM FIELD TO LOCAL AIRPORT (N75). DRAINED ALL FUEL FROM WING TANKS. FOUND WHILE DRAINING FUEL WITH FUEL CAPS ON THAT DRAINING
- [SDR 2004FA0000783](https://openairdocs.org/sdr/2004FA0000783.md): Cap · clogged · Sep 23, 2004 · N8214Y · Cessna 172 · Fuel Storage
  > PILOT EXPERIENCED FUEL INTERRUPTION TO ENGINE WHILE ENROUTE. SWITCHED FUEL TANKS AND ENGINE QUIT. MADE EMERGENCY LANDING. NO INJURIES OR DAMAGE TO AIRCRAFT. REMOVED AC FROM FIELD TO LOCAL AIRPORT (N75). DRAINED ALL FUEL FROM WING TANKS. FOUND WHILE DRAINING F
- [SDR 2004FA0000744](https://openairdocs.org/sdr/2004FA0000744.md): Cap · clogged · Sep 23, 2004 · N8214X · Cessna 172 · Fuel Storage
  > PILOT EXPERIENCED FUEL INTERUPTION. MADE EMERGENCY LANDING IN SOYBEAN FIELD. NO INJURIES OR DAMAGE TO AC. REMOVED AC FROM FIELD TO LOCAL AIRPORT. DRAINED ALL FUEL FROM WING TANKS. FOUND WHILE DRAINING FUEL WITH FUEL CAPS ON THAT DRAINING FUEL WAS SLOW. REMOV
- [SDR 2004FA0000689](https://openairdocs.org/sdr/2004FA0000689.md): Shaft · failed · Jun 23, 2004 · N9023Z · Hynes B2B · Tail Rotor Gearbox
  > TAIL ROTOR DRIVE FROM 90 GEARBOX TO TAIL ROTOR GEARBOX FAIL AT ATTACHING POINT IN TAIL ROTOR GEARBOX. BY THE DISCOLORATION OF THE BREAK IT APPEARS THAT IT HAD PARTIALLY CRACKED PRIOR TO TOTAL FAILURE. THIS CAUSED LOST OF DIRECTIONAL CONTROL OF AIRCRAFT. THE
- [SDR CA040507001](https://openairdocs.org/sdr/CA040507001.md): Actuator · failed · Mar 29, 2004 · Cndair CL6002B19 · Autopilot Main Servo
  > CAPT REPORTED THE PITCH CONTROL STICKING ( HARD POINT FEELING) AFTER AP DISCONNECTION. CPT HAD TO PULL THE CONTROL COLUMN TO RECOVER THE FLIGHT CONTROL. PITCH SERVO ACTUATOR WAS REPLACED.
- [SDR AUS20040142](https://openairdocs.org/sdr/AUS20040142.md): Bearing · failed · Mar 2, 2004 · Socata TB10TOBAGO · Magneto/Distributor
  > (AUS) MAGNETO DRIVE SHAFT OUTER BEARING COMPLETELY DESTROYED. BEARING HAD BEEN RUNNING DRY FOR SOME TIME. SUSPECT MAGNETO ASSEMBLED WITHOUT GREASE IN THE BEARING. PERSONNEL/MAINTENANCE ERROR.
- [SDR AUS20030967](https://openairdocs.org/sdr/AUS20030967.md): Spar · corroded · Sep 17, 2003 · Socata TB10TOBAGO · Wing Spar
  > (AUS) LT UPPER AFT REAR SPAR WEB CONTAINED LIGHT EXFOLIATION CORROSIONIN AREA ADJACENT TO MAIN LANDING GEAR. FOUND DURING INVESTIGATION FOLLOWING CORROSION IN RT WING SPAR. SEE MDR 03/0900.
- [SDR AUS20030900](https://openairdocs.org/sdr/AUS20030900.md): Spar · corroded · Sep 8, 2003 · Socata TB10TOBAGO · Wing Spar
  > (AUS) RT WING MAIN SPAR AFT LOWER WEB CONTAINED EXFOLIATION CORROSION. CORROSION WAS MAINLY LOCATED IN AREA ADJACENT TO MAIN LANDING GEAR LEG.
- [SDR AUS20030901](https://openairdocs.org/sdr/AUS20030901.md): Spar · corroded · Sep 8, 2003 · Socata TB10TOBAGO · Wing Spar
  > (AUS) LT AND RT WING MAIN SPAR AFT LOWER WEBS CONTAINED EXFOLIATION CORROSION. CORROSION MAINLY LOCATED IN AREA ADJACENT TO MAIN LANDING GEAR.
- [SDR AUS20030844](https://openairdocs.org/sdr/AUS20030844.md): Spar · corroded · Aug 19, 2003 · Socata TB10TOBAGO · Wing Spar
  > (AUS) LT AND RT WING MAIN SPARS CONTAINED SEVERE EXFOLIATION CORROSION.
- [SDR AUS20030835](https://openairdocs.org/sdr/AUS20030835.md): Spar · corroded · Jul 24, 2003 · Socata TB10TOBAGO · Wing Spar
  > (AUS) RT WING MAIN SPAR UPPER CAP CONTAINED CORROSION ON THE AFT FACE. RT WING LEADING EDGE INTERCOSTAL CONTAINED CORROSION ON THE LOWER FLANGE. FOLLOWING REMOVAL OF WINGS FOR REPAIR FURTHER CORROSION WAS FOUND ON THE TOP SURFACE OF THE LT AND RT MAIN SPAR UPP
- [SDR CA030729011](https://openairdocs.org/sdr/CA030729011.md): Screw · loose · Jul 14, 2003 · Piper PA24180 · Fuel Control/Reciprocating Engines
  > (CAN) SCREWS HOLDING FLOAT BOWL TO CARBURETOR HOUSING. ALL SCREWS LOCKED BUT ALL LOOSE IN HOUSING CAUSING CHAFING BETWEEN BOWL, GASKET HOUSING WITH A 1/16 INCHES GAP AND ALL AROUND. DISCOVERED ON ANNUAL INSPECTION.
- [SDR AUS20030833](https://openairdocs.org/sdr/AUS20030833.md): Bracket · corroded · May 25, 2003 · Socata TB10TOBAGO · Rudder Structure
  > (AUS) RUDDER LOWER HINGE SUPPORT BRACKET CONTAINED EXFOLIATION CORROSION. FOUND DURING INSPECTION IAW AD TB10 31.
- [SDR AUS20030832](https://openairdocs.org/sdr/AUS20030832.md): Fitting · corroded · May 23, 2003 · Socata TB10TOBAGO · Flight Compartment Equipment
  > (AUS) REAR SEAT BELT OUTBOARD FITTINGS CONTAINED EXFOLIATION CORROSION.
- [SDR CA031021005](https://openairdocs.org/sdr/CA031021005.md): Spar · broken · May 16, 2003 · Cessna 175 · Horizontal Stabilizer, Spar/Rib
  > (CAN) DISCOVERED A BREAK IN THE STABILIZER SPAR DURING AN ANNUAL INSPECTION.
- [SDR 2003FA0000685](https://openairdocs.org/sdr/2003FA0000685.md): Fork · cracked · May 5, 2003 · Mooney M20C · Propeller Controlling System
  > PITCH CHANGE FORK WAS CRACKED, POSSIBLY DUE TO EXCESSIVE ENGINE VIBRATION. PROPELLER HAD 200 HOURS SINCE LAST OVERHAUL. CUSTOMER WAS ADVISED TO HAVE PROPELLER, DYNAMICALLY BALANCED TO AVOID ANY FURTHER DAMAGE TO PROPELLER ASSEMBLY.
- [SDR 2003FA0000156](https://openairdocs.org/sdr/2003FA0000156.md): Governor · malfunctioned · Feb 17, 2003 · N468JL · Amtr RV8 · Propeller Governor
  > PROPELLER WOULD CYCLE NORMALLY DURING RUN UP. AFTER TAKE OFF THE PROP WOULD BECOME UNCONTROLLABLE. RMP ONLY CONTROLLABLE BY THROTTLE, NOT PROPELLER CONTROL. REMOVAL AND DISASSEMBLY OF PROP GOVERNOR REVEALED THAT ALLEN SCREW HAD BACKED OUT OF REAR OF UNIT AND W
- [SDR 2003FA0000175](https://openairdocs.org/sdr/2003FA0000175.md): Indicator · inoperative · Jan 24, 2003 · N751MB · Amtr RV8A · Altimeter, Barometric/Encoder
  > ALTIMETER PURCHASED NEW. MAY 5, 2001 MANUFACTURE DATE. FAILED TO PASS FRICTION PORTION OF PITOT/STATIC/XPDR. BIANNUAL CHECK. MFG CONTACTED AND IS UNAWARE OF ANY PROBLEMS WITH THIS MODEL BUT TECHNICIAN DOING STATIC TEST NOTES SEVERAL LIKE IT HAVE FAILED SAM
- [SDR AUS20021187](https://openairdocs.org/sdr/AUS20021187.md): Pipe · fractured · Oct 16, 2002 · Socata TB10TOBAGO · Propeller Controlling System
  > (AUS) PROPELLER GOVERNOR EXTERNAL OIL PIPE FAILED AT CONNECTION TO THEGOVERNOR.
- [SDR CA020916005](https://openairdocs.org/sdr/CA020916005.md): Wire Rope · broken · Aug 2, 2002 · Cessna 172D · Wheel/Ski/Float
  > (CAN) ON TAKEOFF RUN, AT APPROXIMATELY 2 FT OFF THE WATER, A/C SETTLED BACK DOWN DUE TO UNSTABLE AIR. A NOISE WAS HEARD AND THE A/C BECAME VERY UNSTABLE. ABORTED TAKEOFF. AS THE A/C SLOWED DOWN & THE LIFT DISSIPATED, THE LT WING SUDDENLY DIPPED DOWN AND C
- [SDR CA020610003](https://openairdocs.org/sdr/CA020610003.md): Line · worn · May 31, 2002 · Cessna 172K · Aircraft Fuel Distribution System
  > (CAN) - FUEL LINE FROM UNION TO FIREWALL (STRAINER) FOUND RUBBING ON CO-PILOT STEERING TORQUE TUBE AND STEERING ARM. FUEL LINE HAD A SMALL PIN HOLE AND A SMALL AMOUNT OF FUEL WAS LEAKING. - NEW LINE WAS MANUFACTURED AND ROUTED AWAY FROM STEERING ARM.
- [SDR AUS20020429](https://openairdocs.org/sdr/AUS20020429.md): Frame · cracked · Apr 26, 2002 · Socata TB10TOBAGO · Fuselage Main, Frame
  > (AUS) FUSELAGE FRAME NR 9 CRACKED AT BOTH TOP CORNERS.
- [SDR CA020205002](https://openairdocs.org/sdr/CA020205002.md): Cylinder · failed · Jan 28, 2002 · Conaer C2 · Main Landing Gear Strut/Axle/Truck
  > (CAN) A/C C-2 SKIMMERS, BOTH UTILIZE COLONIAL STYLE MAIN UNDER CARRIAGE OLEOS. ONE OLEO PER A/C CAME APART.THE MAIN GEAR OLEOS ARE CRACKING AT LOWER END CAP TO CYLINDER (CASING) ATTACH BOLTS. WHEN THIS OCCURS, BEFORE LONG END CAP DISLODGES FROM OLEO CAUSING GE

Next page: https://openairdocs.org/engine/eci-o360a1a/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 = 'O360A1A'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/engine/eci-o360a1a/reports

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.