# Service difficulty reports: Schweizer 269C

A list on [Schweizer 269C](https://openairdocs.org/model/schweizer-269c.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 3 · 118 reports

- [SDR 2026F00166](https://openairdocs.org/sdr/2026F00166.md): Support Frame · cracked · Jul 28, 2026 · N776LH · Hughes 269C · Fuselage Main, Structure
  > LEFT AFT AIRFRAME CLUSTER FITTING THAT ATTACHES TO REAR CROSSMEMBER, LANDING GEAR, AND TAIL-BOOM SUPPORT STRUT WAS FOUND CRACKED DURING A VISUAL PREFLIGHT INSPECTION. AIRCRAFT IS GROUNDED AND HAS NOT BEEN RETURNED TO SERVICE. FRAME REPLACEMENT IS REQUIRED. AIR
- [SDR BY8S2014092600566](https://openairdocs.org/sdr/BY8S2014092600566.md): Magneto · failed · Sep 13, 2014 · N645KA · Hughes 269C · Magneto/Distributor
  > COMPLETE RT MAGNETO IGNITION FAILURE/NO OUTPUT. MAGNETO FAILED PRIOR TO SCHEDULED HOUR INSPECTION.
- [SDR 2014FA0000546](https://openairdocs.org/sdr/2014FA0000546.md): Magneto · failed · Sep 13, 2014 · N645KA · Hughes 269C · Magneto/Distributor
  > COMPLETE RT MAGNETO IGNITION FAILURE WITH NO OUTPUT. MAGNETO FAILED PRIOR TO SCHEDULED INSPECTION.
- [SDR FAA20140910000001](https://openairdocs.org/sdr/FAA20140910000001.md): Sensor · detached · Aug 23, 2014 · N34LB · Hughes 269C · Turbine Engine Oil System
  > THE ENGINE STOPPED DUE TO LACK OF OIL. THE OIL TEMPERATURE SENSOR, AND CRUSH WASHER WERE FOUND HANGING BY ITS ELECTRICAL CONNECTOR INSIDE THE ENGINE COMPARTMENT. A REMOTE FILTER SYSTEM WAS INSTALLED ON THE ACFT 1298 HOURS PRIOR TO THE INCIDENT.
- [SDR 2011FA0000183](https://openairdocs.org/sdr/2011FA0000183.md): Tail Rotor · damaged · Mar 18, 2011 · N958CP · Hughes 269C · Tail Rotor Drive System
  > ODOR OF BURNING LUBRICANT, EXCESSIVE VIBRATION, FORCED A SUCCESSFUL OFF AIRPORT LANDING. FOUND AFT "H" FRAME BEARING, PN 269A5050-56, SEIZED, OVERHEATED, DRIVESHAFT JAMMED FWD AGAINST BEARING, AFT BEARING SUPPORT BROKEN OFF FRAME, PN 269A5573-13, AND MISSING.
- [SDR 2011FA0000027](https://openairdocs.org/sdr/2011FA0000027.md): Thrust Bearing · mismanufactured · Jan 14, 2011 · N811TT · Hughes 269C · Main Rotor Drive System
  > (OG5S) DURING 800 HR, 12 AND 24 MONTH INSP, THE MAIN ROTOR DRIVE SHAFT WAS FOUND TO BE WORN JUST ABOVE THE MAIN ROTOR THRUST BEARING. UPON FUTHER INSP, THE WEAR WAS DETERMINED TO BE CAUSED BY THE M/R THRUST BEARING TUBE NOT BEING CHAMFERED IN THE CONTACT AREA
- [SDR 2010FA0001006](https://openairdocs.org/sdr/2010FA0001006.md): Pin · worn · Sep 17, 2010 · N8363C · Hughes 269C · Fuel Storage
  > DURING 200 HR INSP WEAR MARKS WERE FOUND ON THE BOTTOM OF BOTH FUEL TANKS, CAUSED BY ATTACH PIN PN MS20392-2C47 USED ON STRAP ASSY. PN 269A8329-23. DETAILED INSP FOUND WEAR TO BE CAUSED BY INSUFFICIENT PAD MATERIAL INSTALLED ON STRAP ALLOWING CONTACT BETWEEN T
- [SDR 2010FA0000443](https://openairdocs.org/sdr/2010FA0000443.md): Strut · broken · Apr 30, 2010 · N75105 · Hughes 269C · Rotorcraft Tail Boom
  > (OG5S) DURING UNSCHEDULED MX THE LOWER DRIVE SUPPORT STRUT WAS FOUND TO BE CRACKED 90 PERCENT THROUGH THE TUBE WHERE THE UPPER ATTACH LUG IS WELDED. UPON REMOVAL THE LUG COMPLETELY SEPARATED FROM THE TUBE. IF TUBE HAD SEPARATED DURING FLIGHT LOSS OF MAIN ROTO
- [SDR 2009FA0000920](https://openairdocs.org/sdr/2009FA0000920.md): Gearbox · leaking · Sep 29, 2009 · N656RB · Hughes 269C · Tail Rotor System
  > PILOT NOTE THE TAIL ROTOR GEARBOX WAS LEAKING. GEARBOX WAS CLEANED WITH SOLVENT AND AIR DRIED AND THEN GROUND RAN FOR 2-3 MIN. LEAKAGE AND CRACK WERE NOTED IN AREA DEPICTED IN DIAGRAM BELOW. LOGBOOK RESEARCH NOTED NO EVIDENCE OF DAMAGE HISTORY OR TAIL ROTOR
- [SDR CA090126006](https://openairdocs.org/sdr/CA090126006.md): Bolt · broken · Jan 26, 2009 · Hughes 269C · Tail Rotor Head
  > OPERATING A SCHWEIZER 269 C MODEL SERIAL NUMBER S1575 TSN 6449.5 THE CONICAL BRGS WERE REPLACE WITH NEW AT 6338.8 AND A NEW BOLT WAS INSTALLED AT THIS TIME P/N 269A6092-3 WHICH WAS PURCHASE NEW FROM SCHWEIZER ON. THE RETORQUE WAS CARRIED OUT AT 6416.1 TSN NO
- [SDR GLQ2008F00000](https://openairdocs.org/sdr/GLQ2008F00000.md): Nut · damaged · Sep 11, 2008 · N6143K · Hughes 269C · Flight Control System
  > ROUTINE INSPECTION OF TRANSIENT ACFT REVEALED BOTH UPPER PULLEY FWD BEARING RETAINER CAP ATTACH BOLT NUTS LOOSE-APPROX Q.5 THREADS ONLY ENGAGED. THESE WERE SERVICEABLE USED NUTS. THREAD MARKINGS NOTED IN LOCK AREA. NUTS STILL EXHIBIT LOCKING CAPABILITY. FRAME
- [SDR 2008FA0000271](https://openairdocs.org/sdr/2008FA0000271.md): Line · leaking · Apr 3, 2008 · N111AB · Hughes 269C · Aircraft Fuel Distribution System
  > FUEL LEAKING FROM GASCOLATOR INLET LINE, APPROX 5.0 HRS SINCE NEW. (K)
- [SDR CA080212005](https://openairdocs.org/sdr/CA080212005.md): Link · disconnected · Feb 8, 2008 · Hughes 269C · Fuel Controlling System
  > (CAN) THE COTTER PIN SECURING THE IDLE MIXTURE LINK BLOCK TO THE MIXTURE CONTROL ARM BECAME DISLODGED. THIS ALLOWED THE MIXTURE LINK BLOCK TO BECOME DISCONNECTED FROM THE MIXTURE CONTROL ARM. RESULTING A LOSS OF CONTROL OVER FUEL FLOW TO THE ENGINE AND THE ENG
- [SDR 2007FA0000697](https://openairdocs.org/sdr/2007FA0000697.md): Condenser · disconnected · Jul 11, 2007 · N7508H · Hughes 269C · Magneto/Distributor
  > SPRING CLIP ON TERMINAL WIRE CAME OFF ALLOWING WIRE TO DISCONNECT. (K)
- [SDR 2007FA0000688](https://openairdocs.org/sdr/2007FA0000688.md): Bracket · loose · Jul 10, 2007 · N9988F · Hughes 269C · Electrical Power System
  > ALTERNATOR BRACKET LOOSE AT ENGINE BOSS. BOLT CAUSES DAMAGE TO ENGINE CRANKCASE WHEN LOOSE. FRETTING OF ARM AND ENGINE CRANKCASE OCCURS. (K)
- [SDR 2007FA0000510](https://openairdocs.org/sdr/2007FA0000510.md): Lock Nut · backed out · Jun 18, 2007 · N27YS · Hughes 269C · Tail Rotor Gearbox
  > DURING GROUND RUNUP, PILOT NOTICED TAIL ROTOR NOT SPINNING. AIRCRAFT SHUTDOWN AND RETURNED TO HANGER. UPON DISASSEMBLY IT WAS NOTED THAT THE NUT PN 269A6029 THAT ATTACHES THE DRIVE COUPLING TO THE GEARBOX HAD BACKED OUT COMPLETELY AND WORN A HOLE THROUGH THE A
- [SDR 2007FA0000561](https://openairdocs.org/sdr/2007FA0000561.md): Bushing · worn · May 25, 2007 · N1666S · Hughes 269C · Engine Controls
  > ENGINE MOUNTED THROTTLE LINKAGE BUSHINGS WORN. FOUND ON INSPECTION WITH EXCESSIVE PLAY. PROBABLY OCCURRED DUE TO EXCESSIVE VIBRATION OR LACK OF SUBRICATION. RECOMMENDATION TO PREVENT WOULD BE TO LUBRICATE MORE FREQUENTLY OR DIFFERENT DESIGN OF LINKAGE. (K)
- [SDR BS2R2120003](https://openairdocs.org/sdr/BS2R2120003.md): Pulley Bracket · broken · Nov 17, 2006 · N11047 · Hughes 269C · Engine/Transmission Coupling
  > ONE OF THE TWO BELT DRIVE CLUTCH ACTUATOR CABLE PULLEY BRACKETS BROKE CLEAN ACROSS BETWEEN THE FRAME MOUNT HOLE AND THE PULLEY MOUNT HOLE DURING ENGAGEMENT OF THE ROTOR SYSTEM. DURING THE SUBSEQUENT TAKE OFF ATTEMPT THE ROTOR RPM WOULD BLEED OFF RAPIDLY DUE TO
- [SDR 2006FA0001170](https://openairdocs.org/sdr/2006FA0001170.md): Bracket · broken · Nov 17, 2006 · N11047 · Hughes 269C · Fuselage Main, Attach Fittings
  > ONE OF THE BELT DRIVE CLUTCH ACTUATION SYSTEM CABLE PULLEY BRACKETS (1 OF 2 P/N 269A5472) BROKE CLEAN ACROSS BETWEEN THE PULLEY AND ITS FRAME MOUNT HOLES DURING THE PROCESS OF ENGAGING THE ROTOR SYSTEM. DURING THE SUBSEQUENT ATTEMPTED TAKEOFF THE OPERATOR NOTE
- [SDR AU510001955](https://openairdocs.org/sdr/AU510001955.md): Shaft · loose · Dec 9, 2005 · Hughes 269C · Main Rotor Gearbox
  > (AUS) LATERAL CYCLIC CONTROL BELLCRANK LOOSE. DISASSEMBLY AND INVESTIGATION OF THE TRANSMISSION FOUND THAT THE BELLCRANK MOUNTING SHAFT ATTACHED TO THE TRANSMISSION HAD NO SPLIT PIN WHICH ALLOWED THE NUT TO WORK LOOSE AND COME OFF THE SHAFT. THE NUT AND WASHER
- [SDR CA060303016](https://openairdocs.org/sdr/CA060303016.md): Valve · incorrect · Nov 25, 2005 · Hughes 269C · Fuel Quantity Sensor
  > FUEL SYSTEM SENDER INCORRECT VALVE. REPLACED SENDER.
- [SDR CA050825001](https://openairdocs.org/sdr/CA050825001.md): Ring · failed · Aug 17, 2005 · Hughes 269C · Reciprocating Engine Cylinder Section
  > (CAN) HEAVY OIL CONSUMPTION CYLINDER NR 3. OIL RING NOT PERFORMING ITS WORK. REMOVED AND SENT FOR REPAIR. REINSTALLED CYLINDER.
- [SDR 2005FA0000418](https://openairdocs.org/sdr/2005FA0000418.md): Shaft · worn · Jan 7, 2005 · N269TJ · Hughes 269C · Tail Rotor Drive Shaft
  > DURING ANNUAL INSPECTION GREASE IN LOWER PULLEY SHAFT HAD A RUSTY (BROWN) COLOR (NOTE: ANDEROL GREASE IS BLACK). UPON INSPECTION PART HAS 414.2 HOURS SINCE NEW, THE SPLINES WERE WORN BEYOND LIMITS. SPECULATION OF MFG AND OUR FACILITY IS THAT THE GREASE WAS C
- [SDR CA041124003](https://openairdocs.org/sdr/CA041124003.md): Rotor Shaft · broken · Nov 22, 2004 · Hughes 269C · Magneto/Distributor
  > (CAN) ON RUN UP MAGNETO CHECK, FOUND LT MAG INOP. LT MAG REMOVED AND INSPECTED, ROTOR GEAR WAS FOUND SEPARATED FROM ROTOR SHAFT. RT MAGNETO WAS INSPECTED IN THE SAME AREA OF LT MAG FAILURE NO DEFECT FOUND. A NEW MAGNETO WAS INSTALLED IN LT POSITION RT MAGNE
- [SDR CA060303015](https://openairdocs.org/sdr/CA060303015.md): Indicator · failed · May 30, 2004 · Hughes 269C · Engine Oil Pressure
  > OIL PRESSURE UNSERVICEABLE. REPLACED CLUSTER ASSEMBLY.
- [SDR AUS20040413](https://openairdocs.org/sdr/AUS20040413.md): Bolt · separated · May 14, 2004 · Hughes 269C · Fasteners
  > (AUS) GOVERNOR LINKAGE BOLT SEPARATED. LOSS OF ENGINE CONTROL RESULTED IN AUTO ROTATION AND HEAVY LANDING WITH SOME MINOR DAMAGE TO THE AIRCRAFT.
- [SDR H592004F00000](https://openairdocs.org/sdr/H592004F00000.md): Spline · slipped · Feb 28, 2004 · N75070 · Hughes 269C · Tail Rotor Drive Shaft
  > LEVEL FLIGHT, THE TAIL ROTOR DRIVESHAFT STARTED SLIPPING. TAIL ROTOR DRIVESHAFT SPLINES STRIPED. ON FRONT HALF OF SHAFT, STUDENT ENTERED AN AUTOROTATION AND AIRCRAFT LANDED HARD AND RECEIVED SUBSTANTIAL DAMAGE.
- [SDR AUS20040136](https://openairdocs.org/sdr/AUS20040136.md): Fuel Control · faulty · Feb 27, 2004 · Hughes 269C · Fuel Control/Reciprocating Engines
  > (AUS) ENGINE FUEL CONTROL UNIT FAULTY. INVESTIGATION FOUND PRESSURE ON THE MIXTURE ARM CHANGED THE FUEL FLOW RATE CAUSING THE ENGINE TO STOP.
- [SDR AUS20040085](https://openairdocs.org/sdr/AUS20040085.md): Seal · worn · Feb 8, 2004 · Hughes 269C · Reciprocating Engine Power Section
  > (AUS) ENGINE CRANKSHAFT SEAL LEAKING. INVESTIGATION FOUND SEAL HAD DISINTEGRATED AROUND THE SEALING LIP. THIS IS A REPLACEMENT SEAL AFTER THE SEAL FAILURE IN MDR 04/0084.
- [SDR AUS20040084](https://openairdocs.org/sdr/AUS20040084.md): Seal · worn · Feb 7, 2004 · Hughes 269C · Reciprocating Engine Power Section
  > (AUS) ENGINE CRANKSHAFT SEAL LEAKING. INVESTIGATION FOUND SEAL HAD DISINTEGRATED AROUND THE SEALING LIP.
- [SDR CA030703013](https://openairdocs.org/sdr/CA030703013.md): Engine · flamed out · Jun 18, 2003 · Hughes 269C · Engine (Reciprocating)
  > (CAN) SUDDEN ENGINE FLAMES AND A CONTINUOUS LOSS OF SUBSTANTIAL POWER. EMERGENCY LANDING CARRIED OUT. THE ENGINE IS UNDER INVESTIGATION BY TSB. ADDITIONAL REPORT TO FOLLOW.
- [SDR AUS20030615](https://openairdocs.org/sdr/AUS20030615.md): Pinion Gear · failed · Jun 9, 2003 · Hughes 269C · Main Rotor Gearbox
  > (AUS) MAIN TRANSMISSION TAIL ROTOR DRIVESHAFT PINION FAILED IN AREA LOCATED JUST IN FRONT OF THE THREADED AREA ALLOWING THE TAIL ROTOR DRIVE TO SEPARATE. AIRCRAFT STRUCK THE GROUND CAUSING EXTENSIVE DAMAGE TO THE LANDING GEAR.
- [SDR AUS20030521](https://openairdocs.org/sdr/AUS20030521.md): Frame · cracked · May 17, 2003 · Hughes 269C · Fuselage Main, Frame
  > (AUS) FUSELAGE FRAME RT CLUSTER CRACKED.
- [SDR AUS20020700](https://openairdocs.org/sdr/AUS20020700.md): Carburetor · faulty · Jul 12, 2002 · Hughes 269C · Fuel Control/Reciprocating Engines
  > (AUS) NEWLY FITTED ENGINE CARBURETTOR WAS UNABLE TO LEAN THE MIXTURE USING THE MIXTURE SCREW.
- [SDR AUS20020649](https://openairdocs.org/sdr/AUS20020649.md): Bearing · failed · Jun 17, 2002 · Hughes 269C · Main Rotor Gearbox
  > (AUS) MAIN ROTOR TRANSMISSION OUTPUT SHAFT BEARING DISINTEGRATED. TAILROTOR DRIVESHAFT TWISTED UP AT TRANSMISSION END.
- [SDR AUS20020610](https://openairdocs.org/sdr/AUS20020610.md): Bolt · broken · Jun 15, 2002 · Hughes 269C · Tail Rotor Head
  > (AUS) TAIL ROTOR FORK BOLT BROKEN IN HALF.
- [SDR AUS20011318](https://openairdocs.org/sdr/AUS20011318.md): Bracket · cracked · Dec 11, 2001 · Hughes 269C · Engine/Transmission Coupling
  > (AUS) LOWER DRIVE PULLEY SUPPORT BRACKET CRACKED. ONE ATTACHMENT LUGSEPARATED.
- [SDR AUS20011251](https://openairdocs.org/sdr/AUS20011251.md): Damper · loose · Nov 19, 2001 · Hughes 269C · Main Landing Gear Strut/Axle/Truck
  > (AUS) LH REAR LANDING GEAR DAMPER UPPER CAP UNSCREWED AND SEPARATED FROM PISTON. SUSPECT CAUSED BY VIBRATION.
- [SDR AUS20011055](https://openairdocs.org/sdr/AUS20011055.md): Frame · cracked · Sep 30, 2001 · Hughes 269C · Fuselage Main, Frame
  > (AUS) FUSELAGE FRAME CRACKED AT LT CLUSTER. FOUND VISUALLY AND CONFIRMED USING DYE PENETRANT INSPECTION. AIRCRAFT HAD OPERATED FOR 192.2 HOURS SINCE AD/HU269/57 AMDT2 WAS CARRIED OUT.AD/HU269/57 AMDT2 IS CARRIED OUT EVERY 200 HOURS.
- [SDR CA010724035](https://openairdocs.org/sdr/CA010724035.md): Blade · damaged · Jul 10, 2001 · Hughes 269C · Tail Rotor Blades
  > (CAN) ON INSPECTION OF OPPOSITE TAIL ROTOR BLADE, THIS TAIL ROTOR BLADE WAS FOUND TO HAVE NO ABRAISON STRIP ON LEADING EDGE OF BLADE. FURTHER INSPECTION REVEALED THAT FILLER WAS USED UNDER PAINT TO BUILD UP EDGE. BOTH BLADES WERE REMOVED AND SENT TO SCHWEIZER
- [SDR CA010724034](https://openairdocs.org/sdr/CA010724034.md): Blade · cracked · Jul 10, 2001 · Hughes 269C · Tail Rotor Blades
  > (CAN) ON DAILY INSPECTION OUTBOARD PART OF BLADE SKIN WAS FOUND TO BE CRACKED. CRACK IS FORMED AROUND TIP BLOCK ON BLADE. THE CRACK IS APPROX. 3 INCHES LONG, STARTING FROM BEHIND ABRASION STRIP TO ABOUT MIDDLE OF BLADE.
- [SDR AUS20010479](https://openairdocs.org/sdr/AUS20010479.md): Retainer · worn · Apr 6, 2001 · Hughes 269C · Engine/Transmission Coupling
  > (AUS) THERMOFIT SLEEVE WORN ON RETAINER.
- [SDR AU001170](https://openairdocs.org/sdr/AU001170.md): Key · disintegrated · Dec 8, 2000 · Hughes 269C · Reciprocating Engine Cylinder Section
  > (AUS) NO3 CYLINDER EXHAUST VALVE SPRING LOCKING KEYS SHATTERED BUT WERE STILL HOLDING THE SPRINGS IN PLACE. CAP PNO MS13998-3 ALSO HADSEVERAL CHIPS MISSING. THE VALVE SEAT WAS DAMAGED BEYOND LIMITS.FOUND DURING INSPECTION IAW LYCOMING SB 388B. NO EVIDENCE OFME
- [SDR CA000530017](https://openairdocs.org/sdr/CA000530017.md): Boot · torn · May 18, 2000 · Hughes 269C · Engine/Transmission Coupling
  > (CAN)WHILE PERFORMING A POST-FLIGHT INSPECTION, THE PILOT NOTED GREASE ON THE FAN HOUSING (SCROLL ASSY). INSPECTION SHOWED A TEAR ON BOOT 269A-5473 INSTALLED ON ADAPTER 269A5411. DRIVESHAFT GREASE HAS LEAKED RADIALLY FROM BOOT. BOOT STILL CONTAINED SUFFICIE
- [SDR 20000505SH034](https://openairdocs.org/sdr/20000505SH034.md): Swashplate · binding · Mar 29, 2000 · N61447 · Hughes 269C · Tail Rotor Control System
  > INTERMITTENT T/R PEDAL BINDING. (X)
- [SDR CA991004031](https://openairdocs.org/sdr/CA991004031.md): Cylinder · worn · Aug 31, 1999 · Hughes 269C · Reciprocating Engine Cylinder Section
  > (CAN) POWER LOSS EXPERIENCED DUE TO STICKY VALVES.
- [SDR 99ZZZX2210](https://openairdocs.org/sdr/99ZZZX2210.md): Pulley · damaged · May 12, 1999 · N9623F · Hughes 269C · DC Generator-Alternator
  > ALTERNATOR PULLEY COOLING FINS BECAME DETACHED FROM PULLEY CAUSING ALTERNATOR TO VIBRATE OFF ENGINE SHEARING BRACKET BOLTS. INSTALLED NEW BOLTS AND ALTERNATOR. PROBLEM HAS NOT RECURRED. POSSIBLE CAUSE IS FATIGUE OF COOLING FINS. SUBMITTER SUGGESTED INSPECT
- [SDR 99ZZZX2160](https://openairdocs.org/sdr/99ZZZX2160.md): Alternator · damaged · May 1, 1999 · N9623F · Hughes 269C · Alternator-Generator Drive
  > ALTERNATOR PULLEY COOLING FINS BECAME DETACHED FROM PULLEY CAUSING ALTERNATOR TO VIBRATE OFF ENGINE SHEARING BRACKET BOLTS. INSTALLED NEW BOLTS AND ALTERNATOR. PROBLEM HAS NOT RECURRED. POSSIBLE CAUSE IS FATIGUE OF COOLING FINS. SUGGEST INSPECTION OF FINS
- [SDR 99ZZZX239](https://openairdocs.org/sdr/99ZZZX239.md): Bearing · failed · Nov 12, 1998 · N103WP · Hughes 269C · Reciprocating Engine Oil System
  > WHILE IN-FLIGHT, PILOT NOTICED SLIGHT VIBRATION COMING FROM THE ENGINE AND A DROP IN OIL PRESSURE STARTING TO OCCUR. PILOT OPTED FOR A PRECAUTIONARY LANDING. UPON COMPLETION, OIL PRESSURE NOTED TO BE AT 15 PSI WITH A LOUD SQUEAL COMING FROM THE ENGINE. PILO
- [SDR 99ZZZX237](https://openairdocs.org/sdr/99ZZZX237.md): Strut · cracked · Nov 9, 1998 · N2011A · Hughes 269C · Fuselage Miscellaneous Structure
  > ONE INCH CRACK LOCATED AT UPPER PART OF DRIVE PULLEY FRAME STRUT ASSEMBLY. CRACK ORIGINATED AT WELD.

Next page: https://openairdocs.org/model/schweizer-269c/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 aircraft_model_key = '269C'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/schweizer-269c/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.