# Service difficulty reports: Schweizer 269C-1

A list on [Schweizer 269C-1](https://openairdocs.org/model/schweizer-269c-1.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 2 · 83 reports

- [SDR 2016FA0000558](https://openairdocs.org/sdr/2016FA0000558.md): Mast · corroded · Nov 9, 2016 · Hughes 269C1 · Main Rotor Mast/Swashplate
  > MAIN ROTOR ASSEMBLY, CORROSION AROUND MAIN ROTOR THRUST BEARING RETAINER, AND SCISSOR MOUNTING LUG.
- [SDR CA141023007](https://openairdocs.org/sdr/CA141023007.md): Bearing · making metal · Oct 6, 2014 · Hughes 269C1 · Tail Rotor Head
  > (CAN) THE ROTOR SYS WAS FOUND TO BE INCREASING IN VIBRATION. CHECKED THROUGH THE SYSTEM AND FOUND THE BEARINGS WHEN PURGED OF GREASE WERE SHOWING FINE METAL PARTICLES. CARRIED OUT A WEIGHTED ROTATIONAL TEST ON PITCH HOUSINGS AND FOUND THE BEARINGS TO BE A BI
- [SDR 2012FA0000070](https://openairdocs.org/sdr/2012FA0000070.md): Piston · failed · Jan 14, 2012 · N1868S · Hughes 269C1 · Reciprocating Engine Power Section
  > NORMAL TAKEOFF, HOVER, AND STEADY LEVEL FLIGHT. 30 MINUTES ENROUTE, SUDDEN VIBRATIONS FOLLOWED BY LOW RPM WARNING LIGHT & HORN. VERIFIED DROPPING NEEDLES AND LOWERED COLLECTIVE FOR AUTOROTATION. CHECKING AIRSPEED GAUGE AT 40KTS, ADJUSTED FORWARD CYCLIC FOR
- [SDR CA110315004](https://openairdocs.org/sdr/CA110315004.md): Blade · cracked · Mar 11, 2011 · Hughes 269C1 · Tail Rotor Blades
  > (CAN) DURING THE INSPECTION 600 HOURS/ANNUAL, WE PERFORMED VISUAL INSPECTION OF THE TAIL ROTOR BLADES AND OBSERVED A SPANWISE CRACKS AT THE TRAILING EDGE SKINS. ACCORDING TO THE MANUFACTURER SCHWEIZER, NO CRACKS ARE ALLOWED AT THE TAIL ROTOR.
- [SDR 2010FA0001059](https://openairdocs.org/sdr/2010FA0001059.md): Engine · failed · Sep 15, 2010 · N302HG · Hughes 269C1 · Engine (Reciprocating)
  > THE OIL TEMP SPIKED ABOVE RED LINE AS THE HELICOPTER TURNED FINAL. AN IMMEDIATE LANDING WAS MADE. AS THE HELICOPTER TOUCHED DOWN, A LOUD NOISE WAS HEARD FOLLOWED BY SMOKE AND FIRE. THE FIRE WAS QUICKLY EXTINGUISHED. PARTS OF THE ENGINE CRANKCASE, ROD BEARING A
- [SDR CA091206005](https://openairdocs.org/sdr/CA091206005.md): Bearing · cracked · Dec 6, 2009 · Hughes 269C1 · Main Rotor Head
  > (CAN) INNER RACE OF FLAPPING HINGE BEARING FOUND CRACKED HALF WAY THROUGH DURING ANNUAL INSP.
- [SDR CA091206004](https://openairdocs.org/sdr/CA091206004.md): Bearing · cracked · Nov 23, 2009 · Hughes 269C1 · Main Rotor Head
  > (CAN) INNER RACE OF FLAPPING HINGE BRG FOUND CRACKED HALF WAY THROUGH ON ANNUAL INSP.
- [SDR CA090304017](https://openairdocs.org/sdr/CA090304017.md): Support Bracket · damaged · Mar 2, 2009 · Hughes 269C1 · Main Landing Gear
  > (CAN) GROUND HANDLING WHEEL HANDLE DISENGAGED FROM LANDING GEAR STEP SUPPORTS INFLIGHT AND FELL TO THE GROUND. FWD SUPPORT IS A CRADLE-TYPE BRACKET THAT IS DRILLED AT BOTH ENDS AND THROUGH THE STEP THAT IT IS ATTACHED TO. HANDLE IS ALSO DRILLED AT ONE END SO T
- [SDR 2008FA0000751](https://openairdocs.org/sdr/2008FA0000751.md): Booster · exploded · Oct 24, 2008 · N2014T · Hughes 269C1 · Magneto/Distributor
  > START MAGNETO, START BOOSTER BOX PN SS1001 BLEW THE TOP PORTION APART. IT CAUGHT ON FIRE AND SMOKE WENT EVERYWHERE. INSPECTED HELICOPTER WHEN SMOKE CLEARED AND COULD NOT FIND THE PROBLEM. TURNED OFF THE FUEL AND BUMPED THE STARTER AND FOUND THE PROBLEM TO BE T
- [SDR CA090609008](https://openairdocs.org/sdr/CA090609008.md): Drive Belt · delaminated · Sep 24, 2008 · Hughes 269C1 · Engine/Transmission Coupling
  > (CAN) DRIVE BELTS DELAMINATING. FOUND ON 100 HR INSP. DRIVE BELTS REPLACED UNDER WARRANTY.
- [SDR CA090609007](https://openairdocs.org/sdr/CA090609007.md): Exhaust Valve · stuck · Nov 19, 2007 · Hughes 269C1 · Reciprocating Engine Cylinder Section
  > (CAN) EXHAUST VALVE ON NR 2 CYL STUCK CAUSING LOSS OF ENG PWR. ACFT DESCENDED INTO A FIELD. THE HELICOPTER WAS TAKEN BY TRUCK TO MX FACILITY TO DETERMINE PROBLEM. ENGINE MFG WARRANTIED REPAIR OF CYLINDER AND VALVE ASSY.
- [SDR CA070909001](https://openairdocs.org/sdr/CA070909001.md): Bracket · broken · Sep 8, 2007 · Hughes 269C1 · AC Generator-Alternator
  > (CAN) ALTERNATOR BRACKET FOUND WITH BROKEN ATTACHMENT LUG. ALTERNATOR BELT TENSION LOSS AND SUBSEQUENT SYSTEM UNSERVICEABILITY. CAUSE OF FAILURE UNDER INVESTIGATION. (TC NR 20070909001)
- [SDR 2007FA0000667](https://openairdocs.org/sdr/2007FA0000667.md): Cylinder Head · separated · Jul 26, 2007 · N2021G · Hughes 269C1 · Reciprocating Engine Cylinder Section
  > NR 2 CYLINDER HEAD SEPARATED FROM CYLINDER BARREL IN FLIGHT.
- [SDR 2007FA0000677](https://openairdocs.org/sdr/2007FA0000677.md): Cylinder Head · separated · Jul 15, 2007 · N2021G · Hughes 269C1 · Reciprocating Engine Cylinder Section
  > 2 NR CYLINDER HEAD ASSEMBLY APPEARS TO HAVE FAILED DURING FLIGHT RESULTING IN A SEVERE ENGINE VIBRATION AND A FORCED LANDING. EXAMINATION OF UPPER HALF OF FAILED CYLINDER ASSEMBLY REVEALS THAT A CRACK OCCURRED AND PROPAGATED SYMMETRICALLY AROUND THE CYLINDER A
- [SDR CA070705012](https://openairdocs.org/sdr/CA070705012.md): Alternator · failed · Jul 5, 2007 · Hughes 269C1 · DC Generator-Alternator
  > (CAN) ALTERNATOR FAILED ON STARTUP. FOUND ROTOR JAMMING AND PULLEY HAD OVERHEATED. LOOSE PARTS HEARD INSIDE ALTERNATOR. NO PREVIOUS INDICATIONS OF IMPENDING FAILURE. (TC NR 20070705012)
- [SDR CA070705013](https://openairdocs.org/sdr/CA070705013.md): Gasket · cracked · Jul 2, 2007 · Hughes 269C1 · Engine Collector/Tailpipe/Nozzle
  > (CAN) DURING ROUTINE INSP, IT WAS NOTICED THAT NEARLY ALL OF THE GASKET BETWEEN THE FWD FLANGE AND THE EXHAUST MUFF HAD CRACKED AND FALLEN AWAY, LEAVING THE POSSIBILITY OF A CABIN EXHAUST LEAK. (TC NR 20070705013)
- [SDR CA070612004](https://openairdocs.org/sdr/CA070612004.md): Drive Belt · split · Jun 12, 2007 · Hughes 269C1 · Engine/Transmission Coupling
  > (CAN) DRIVE BELT AXIAL SPLIT OVER 50 PERCENT OF BELT CIRCUMFERENCE; SPLIT OCCURS UNDER OUTER LAYER OF BELT. NOTE: PLEASE ADVISE IF PHYSICAL VERIFICATION IS REQUIRED AS MUST RETURN BELTS TO MFR FOR WARRANTY CONSIDERATION. (TC NR 20070612004)
- [SDR CA070614001](https://openairdocs.org/sdr/CA070614001.md): Drive Belt · split · Jun 8, 2007 · Hughes 269C1 · Engine/Transmission Coupling
  > (CAN) DRIVE BELT AXIAL SPLIT OVER 50 PERCENT OF BELT CIRCUMFERENCE; SPLIT OCCURS UNDER OUTER LAYER OF BELT. DEFECT HAS BEEN FOUND ON (2) OTHER AIRCRAFT OF THE SAME TYPE. NOTE: PLEASE ADVISE IF PHYSICAL INSPECTION IS REQUIRED AS MUST RETURN BELTS TO MANUFACTU
- [SDR CA070515006](https://openairdocs.org/sdr/CA070515006.md): Bracket · broken · May 1, 2007 · Hughes 269C1 · DC Generator-Alternator
  > (CAN) ALTERNATOR BRACKET BROKEN. REPLACED BRACKET WITH NEW PART PN LW10382. (TC NR 20070515006)
- [SDR 2006FA0001041](https://openairdocs.org/sdr/2006FA0001041.md): Drive Belt · stretched · Oct 6, 2006 · N17535 · Hughes 269C1 · Main Rotor System
  > NEW DRIVE BELTS WERE INSTALLED, STRETCHED FOR 24 HOURS, AND RE-ADJUSTED IAW MM. THE AIRCRAFT WAS RETURNED TO SERVICE AND.5 HOUR INTO THE FIRST FLIGHT THE PILOT NOTICED THE MAIN ROTOR RPM DECAYING AND ENGINE RPM INCREASING. A STEEP DESCENT WITH POWER WAS PER
- [SDR CA060224006](https://openairdocs.org/sdr/CA060224006.md): Adapter · broken · Feb 15, 2006 · Hughes 269C1 · Magneto/Distributor
  > DURING 25 HOUR INSPECTION, OIL WAS DRAINED FROM ENGINE AND FOUND BEARING CAGE BALL RETAINER MADE OF PLASTIC (KIND OF) ON ENGINE OIL SCREEN. REMOVED BOTH MAGNETO DRIVE ADAPTER ASSEMBLY AND FOUND THE PROBLEM ON THE RT ADAPTER (BALL RETAINERS MISSING). REPLACED
- [SDR CA060306013](https://openairdocs.org/sdr/CA060306013.md): Starter · failed · Jan 13, 2006 · Hughes 269C1 · Engine Starter
  > (CAN) STARTER NOT OPERATING. REPLACED STARTER. (TC NR 20060306013)
- [SDR CA060306007](https://openairdocs.org/sdr/CA060306007.md): Magneto · failed · Jan 10, 2006 · Hughes 269C1 · Magneto/Distributor
  > (CAN) AIRCRAFT HARD TO START AND 125 DROOP. REPLACED LT MAGNETO. (TC NR 20060306007)
- [SDR CA060213005](https://openairdocs.org/sdr/CA060213005.md): Bearing · broken · Dec 20, 2005 · Hughes 269C1 · Magneto/Distributor
  > (CAN) SMALL METAL FRAGMENT DISCOVERED WHILE CHANGING ENGINE OIL. FOUND TO BE PART OF A BEARING KEEPER IN RT MAGNETO ADAPTER BEARINGS. THIS IS THE SECOND TIME THIS PROBLEM HAS OCCURRED ON THIS AIRCRAFT. (TC NR 20060213005)
- [SDR CA060306012](https://openairdocs.org/sdr/CA060306012.md): Bracket · cracked · Nov 18, 2005 · Hughes 269C1 · Fuselage Miscellaneous Structure
  > (CAN) BRACKET CRACKED. REPLACED BRACKET. (TC NR 20060306012)
- [SDR CA051206006](https://openairdocs.org/sdr/CA051206006.md): Crankshaft · cracked · Nov 1, 2005 · Hughes 269C1 · Reciprocating Engine Power Section
  > ENGINE WAS IN FOR OVERHAUL. CRACK FOUND IN CRANKSHAFT WITH MPI. NO RECORD OF BLADE STRIKE.
- [SDR CA051007004](https://openairdocs.org/sdr/CA051007004.md): Carburetor · failed · Sep 28, 2005 · Hughes 269C1 · Fuel Control/Reciprocating Engines
  > (CAN) AIRCRAFT HAVE LOW POWER IN FLIGHT. REPLACED CARBURATOR.
- [SDR CA051003015](https://openairdocs.org/sdr/CA051003015.md): Tube · cracked · Sep 22, 2005 · Hughes 269C1 · Main Rotor Mast/Swashplate
  > (CAN) 1) TUBE ASSEMBLY IS CRACKED ON THE MAST SIDE. 2) REPLACED TUBE ASSEMBLY, P/N 269A2172-5.
- [SDR 2005FA0001286](https://openairdocs.org/sdr/2005FA0001286.md): Hinge · broken · Aug 30, 2005 · N1567C · Hughes 269C1 · Fuselage, Landing Gear Attach Fittings
  > THE DOOR PIN PORTION OF THE HINGE, WHICH IS RESPONSIBLE RETAINING THE DOOR, BROKE IN FLIGHT AND THE DOOR WAS UNSECURED AT THE LOWER CONNECTING POINT. THE FLIGHT CREW LANDED, THE DOOR WAS SECURED TEMPORARILY AND THE AIRCRAFT RETURNED TO THE MAINTENANCE FACILIT
- [SDR HA42005F00000](https://openairdocs.org/sdr/HA42005F00000.md): Hinge · broken · Aug 28, 2005 · N1565B · Hughes 269C1 · Passenger/Crew Doors
  > THE DOOR PIN PORTION OF THE HINGE, WHICH IS RESPONSIBLE RETAINING THE DOOR, BROKE. THIS LEAVES THE DOOR CONNECTED AT ONLY 1 POINT AND AN IN-FLIGHT FAILURE COULD POTENTIALLY ALLOW THE DOOR SEPARATE FROM THE AIRCRAFT. (K)
- [SDR 2005FA0001285](https://openairdocs.org/sdr/2005FA0001285.md): Hinge · failed · Aug 27, 2005 · N1542D · Hughes 269C1 · Passenger/Crew Doors
  > THE DOOR PIN PORTION OF THE HINGE, WHICH IS RESPONSIBLE RETAINING THE DOOR, FAILED. THIS LEAVES THE DOOR CONNECTED AT ONLY ONE POINT AND AN IN-FLIGHT FAILURE COULD POTENTIALLY ALLOW THE DOOR SEPARATE FROM THE AIRCRAFT. (K)
- [SDR 2005FA0000889](https://openairdocs.org/sdr/2005FA0000889.md): Cylinder · cracked · Jun 20, 2005 · N2024Z · Hughes 269C1 · Reciprocating Engine Cylinder Section
  > DURING 100HR COMPRESSION CHECK, AIR WAS FOUND TO BE LEAKING AROUND TOP SPARK PLUG AREA. FURTHER INSPECTION NOTED CRACK ALONG TOP COOLING FIN AREA. UPON REMOVING CYLINDER, CRACK WAS FOUND TO RUN FROM AREA AROUND TOP SPARKPLUG HOLE THROUGH EXHAUST SEAT AND THR
- [SDR 2005FA0000888](https://openairdocs.org/sdr/2005FA0000888.md): Cylinder · cracked · Jun 20, 2005 · N2024Z · Hughes 269C1 · Reciprocating Engine Cylinder Section
  > DURING 100HR COMPRESSION CHECK, AIR WAS FOUND TO BE LEAKING AROUND TOP SPARK PLUG AREA. FURTHER INSPECTION NOTED CRACK ALONG TOP COOLING FIN AREA. UPON REMOVING CYLINDER, CRACK WAS FOUND TO RUN FROM AREA AROUND TOP SPARKPLUG HOLE THROUGH EXHAUST SEAT AND THR
- [SDR 2005FA0000475](https://openairdocs.org/sdr/2005FA0000475.md): Spline · stripped · Mar 6, 2005 · N72LP · Hughes 269C1 · Main Rotor Drive System
  > WHILE IN CRUISE FLIGHT, TAIL ROTOR FAILURE AT APPROX 700 FT, PILOT WENT TO FLAT PITCH, PUT HELICOPTER IN A DIVE TO AVOID ROTATION FROM TORQUE, PERFORMED FULL AUTOROTATION TO THE GROUND, NO DAMAGE TO HELICOPTER OR INJURIES TO OCCUPANTS. DRIVE GEAR ON TAIL ROTO
- [SDR CA050208007](https://openairdocs.org/sdr/CA050208007.md): Pump · loose · Feb 8, 2005 · Hughes 269C1 · Engine Fuel Pump
  > (CAN) DURING INSPECTION, FUEL WETNESS WAS DISCOVERED ON THE BOTTOM OF THE FUEL PUMP. UPON FURTHER INSP ALL OF THE DIAPHRAGM RETENTION BOLTS WERE FOUND TO BE LOOSE. A MINIMUM OF THREE QUARTERS TO TWO TURNS WAS OBSERVED ON ALL OF THE BOLTS IN ORDER TO ACHIEVE
- [SDR 2005FA0000420](https://openairdocs.org/sdr/2005FA0000420.md): Shaft · worn · Jan 7, 2005 · N72LP · Hughes 269C1 · Main Rotor Gearbox
  > DURING 600 HOUR INSPECTION GREASE IN LOWER PULLEY SHAFT HAD A RUSTY (BROWN) COLOR (NOTE: ANDEROL GREASE IS BLACK). UPON INSPECTION PART HAS 600.0 HOURS SINCE NEW, THE SPLINES SHOWED IRREGULAR WEAR. SPECULATION OF MFG AND OUR FACILITY IS THAT THE GREASE WAS C
- [SDR 2005FA0000419](https://openairdocs.org/sdr/2005FA0000419.md): Drive Shaft · corroded · Jan 7, 2005 · N72LP · Hughes 269C1 · Tail Rotor Drive Shaft
  > DURING 600 HOUR INSPECTION GREASE IN DRIVE SHAFT HAD A RUSTY (BROWN) COLOR (NOTE: ANDEROL GREASE IS BLACK). UPON INSPECTION PART HAS 600.0 HOURS SINCE NEW. LIFE LIMIT OF 6000 HRS, THE SPLINES WERE WORN TO THE THICKNESS OF A PIECE OF PAPER (APPROX.090 NEW).
- [SDR CA041102002](https://openairdocs.org/sdr/CA041102002.md): Carriage · cracked · Nov 2, 2004 · Hughes 269C1 · Main Rotor Transmission Mount
  > DURING A SCHEDULED 4200 HR O/H THE ABOVE DESCRIBED CARRIER WAS FOUND TO HAVE 3 CRACKS AT 3 SEPARATE LOCATIONS IN THE CARRIER TO COUPLING MOUNTING HOLE LOCATIONS. THESE CRACKS WERE DETECTED DURING FLUORESCENT PENETRANT INSPECTION. FOR THE FUTURE A MIDLIFE INS
- [SDR 2004FA0000842](https://openairdocs.org/sdr/2004FA0000842.md): Bracket · cracked · Oct 21, 2004 · N614TV · Hughes 269C1 · Power Lever
  > A STUDENT NOTICED ON PRE-FLIGHT A CRACK ON THE THROTTLE BELLCRANK SUPPORT BRACKET, (PN 269A8460-1)MOUNTED TO THE CARBURETOR. THE CRACK WAS LOCATED JUST BELOW THE THROTTLE CONTROL BELLCRANK ATTACH LUG AND WAS NOTICEABLE UPON APPLYING LATERAL PRESSURE TO A LINKA
- [SDR 2004FA0000841](https://openairdocs.org/sdr/2004FA0000841.md): Bracket · cracked · Oct 21, 2004 · N614TV · Hughes 269C1 · Power Lever
  > A STUDENT NOTICED ON PRE-FLIGHT, A CRACK ON THE THROTTLE BELLCRANK SUPPORT BRACKET, (PN 269A8460-1) MOUNTED TO THE CARBURETOR. THE CRACK WAS LOCATED JUST BELOW THE THROTTLE CONTROL BELLCRANK ATTACH LUG AND WAS NOTICEABLE UPON APPLYING LATERAL PRESSURE TO A LIN
- [SDR CA041013009](https://openairdocs.org/sdr/CA041013009.md): Switch · malfunctioned · Oct 7, 2004 · Hughes 269C1 · Communications System
  > (CAN)TRIGGER SWITCH MALFUNCTION, NO TRANSMISSION. REPLACED SWITCH P/N M8805/111-04.
- [SDR CA041006001](https://openairdocs.org/sdr/CA041006001.md): Trim Switch · sticks · Sep 28, 2004 · Hughes 269C1 · Stabilizer Position Indicating
  > (CAN) TRIM SWITCH STICKS WHEN PULLED FOR REAR ACTIVATION. REPLACED SWITCH.
- [SDR CA040706002](https://openairdocs.org/sdr/CA040706002.md): Carburetor · failed · Jun 1, 2004 · Hughes 269C1 · Fuel Control/Reciprocating Engines
  > HIGH MANIFOLD PRESSURE. REPLACED CARBURETOR.
- [SDR CA040427013](https://openairdocs.org/sdr/CA040427013.md): Shaft · broken · Mar 12, 2004 · Hughes 269C1 · Main Rotor Gearbox
  > (CAN) BEARING SIZE DUE TO LACK OF LUBRICATION. DUE TO INCORRECT INSTALLATION AT REPAIR.
- [SDR CA040127017](https://openairdocs.org/sdr/CA040127017.md): Nut · loose · Jan 5, 2004 · Hughes 269C1 · Engine/Transmission Coupling
  > (CAN) OIL LEAKING FROM FREEWHEEL WAS NOTED AT REFUELING STOP. NUT (WHICH IS ALSO SEAL RUNNER) WAS FOUND LOOSE. NUT WAS RETORQUED AND FLUSH OF FREEWHEEL PRODUCED NO DISCOLORATION OR PARTICLES. LEAK CHECK CARRIED OUT AND RETURNED TO SERVICE. NOTE: THAT OIL ON
- [SDR CA030129003](https://openairdocs.org/sdr/CA030129003.md): Camshaft · damaged · Jan 13, 2003 · Hughes 269C1 · Reciprocating Engine Power Section
  > (CAN) THE ENGINE HAD 6 HOURS TTSO. THE PILOTS NOTICED AN ENGINE VIBRATION, AND STARTING WAS BECOMING EVER MORE DIFFICULT. THE AME THEN PROCEEDED IN REPLACING THE TWO MAGNETOS AND THE CARBURETOR. AFTER A FEW HOURS OF FLIGHT THE PROBLEM PERSISTED. THE AME THEN C
- [SDR CA030103004](https://openairdocs.org/sdr/CA030103004.md): Intake Valve · leaking · Nov 5, 2002 · Hughes 269C1 · Reciprocating Engine Cylinder Section
  > (CAN) BASE LINE DIFFERENTIAL CHECK OF NEW AIRCRAFT REVEALED LEAKING NR 4 CYLINDER INTAKE VALVE. CYLINDER REMOVED AND REPAIRED.
- [SDR CA030103002](https://openairdocs.org/sdr/CA030103002.md): Control Unit · failed · Oct 30, 2002 · Hughes 269C1 · Engine/Transmission Coupling
  > (CAN) PILOT REPORTED DURING HOVER, THE TAXI LOW ROTOR WARNING ACTIVATED BUT ROTOR RPM WAS IN PROPER AREA OF GREEN ARC ON DUAL TACH. DURING SHUTDOWN, SWITCHING BELT DRIVE ENGAGEMENT SWITCH TO DISENGAGE MADE ENGINE QUIT. TROUBLESHOOTING REVEALED CONTROL UNIT DI
- [SDR CA021031016](https://openairdocs.org/sdr/CA021031016.md): Bracket · cracked · Sep 26, 2002 · Hughes 269C1 · DC Generator-Alternator
  > (CAN) ALTERNATOR BRACKET BROKEN. REPLACED BRACKET.
- [SDR CA021031014](https://openairdocs.org/sdr/CA021031014.md): Bearing · worn · Sep 24, 2002 · Hughes 269C1 · Power Lever
  > (CAN) BEARING ON CARBURETOR LOOSE IN THROTTLE. REPLACED BEARING.

Next page: https://openairdocs.org/model/schweizer-269c-1/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 = '269C1'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/schweizer-269c-1/reports

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