# Service difficulty reports: Pratt & Whitney R1340 series

A list on [Pratt & Whitney R1340 series](https://openairdocs.org/engine/pratt-whitney-r1340-series.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 2 · 54 reports

- [SDR 2018FA0000331](https://openairdocs.org/sdr/2018FA0000331.md): Throttle Arm · worn · Aug 2, 2018 · N5553X · Ayres S2R · Fuel Control/Reciprocating Engines
  > THE PILOT WAS UNABLE TO DECREASE ENGINE RPM, INITIATED A GO AROUND. ON THE SECOND APPROACH THE PILOT NEEDED TO INCREASE RPM AND FOUND THAT ALL THROTTLE CONTROL INPUTS WERE UNRESPONSIVE. THE AIRCRAFT LANDED IN A CORN FIELD 260 YARDS SHORT OF THE RUNWAY. INSPEC
- [SDR CA150526005](https://openairdocs.org/sdr/CA150526005.md): Cam · worn · May 19, 2015 · Dhav DHC3 · Reciprocating Engine Power Section
  > (CAN) AT SPRING RUN UP, ENG SOUNDS LIKE TWIN ENG ACFT WITH PROPS OUT OF SYNC. CAM RING EXHAUST TRACK WEAR SUSPECTED AS IS A KNOWN PROBLEM WITH THIS INDICATION. CAM INSPECTED & WEAR FOUND ON 3 OF 4 CAM LOBES OF EXHAUST TRACK. CAM PN 11768 & 9 EXTRACK ROLLERS
- [SDR RZIG2014092400553](https://openairdocs.org/sdr/RZIG2014092400553.md): Cylinder · fractured · Aug 24, 2014 · N91968 · Airtrc AT401 · Reciprocating Engine Cylinder Section
  > AFTER TAKEOFF NR 2 CYLINDER EXHAUST VALVE STUCK IN OPEN POSITION LETTING PISTON CONTACT VALVE, BREAKING EXHAUST ROCKER HOUSING FROM CYLINDER. ACFT LOST POWER FORCING LANDING. ACFT CAUGHT FIRE.
- [SDR FQWG2014082200494](https://openairdocs.org/sdr/FQWG2014082200494.md): Engine · power loss · Jul 28, 2014 · N8593S · Airtrc AT301 · Engine (Reciprocating)
  > DURING PESTICIDE APPLICATION, THE ENGINE STARTED LOOSING POWER AND RUNNING ROUGH. UNABLE TO MAINTAIN FLIGHT.
- [SDR 2014FA0000023](https://openairdocs.org/sdr/2014FA0000023.md): Bearing · failed · Apr 24, 2013 · N23416 · Airtrc AT301 · Reciprocating Engine Supercharger
  > SUPERCHARGER BLOWER AFT BEARING FAILURE DURING TAKEOFF.
- [SDR CA120509001](https://openairdocs.org/sdr/CA120509001.md): Strut · cracked · May 2, 2012 · Dhav DHC3 · Wheel/Ski/Float
  > (CAN) FOUND 4" CRACK IN CENTER OF BOTTOM WEB OF LEFT STRUT. DIAGRAM SHOWN ON PAPER VERSION SDR FORM.
- [SDR 2011FA0000539](https://openairdocs.org/sdr/2011FA0000539.md): Engine · failed · Aug 22, 2011 · N1735S · Ayres S2R · Engine (Reciprocating)
  > ENGINE FAILED JUST AFTER TAKEOFF, FOR UNKNOWN REASONS RESULTING IN AN ACCIDENT. PILOT REPORTED HEARING A LOUD "BANG" COME FROM THE ENGINE WITH A SUDDEN LOSS OF POWER, FOLLOWED BY TOTAL ENGINE FAILURE.
- [SDR 2011FA0000567](https://openairdocs.org/sdr/2011FA0000567.md): Engine · power loss · Aug 4, 2011 · N4345S · Airtrc AT301 · Engine (Reciprocating)
  > TOTAL LOSS OF POWER ON TAKEOFF. 500 HOURS SINCE O/H.
- [SDR CA110809006](https://openairdocs.org/sdr/CA110809006.md): Cylinder Head · cracked · Jul 29, 2011 · Dhav DHC3 · Reciprocating Engine Cylinder Section
  > VIBRATIONS PRIOR TO TAKEOFF - PRECAUTIONARY LANDING - VISUAL INSPECTION REVEALED A SEPARATION (CRACK) OF THE CYLINDER HEAD H1.
- [SDR 2011FA0000637](https://openairdocs.org/sdr/2011FA0000637.md): Exhaust Valve · stuck · Jul 29, 2011 · N45332 · Airtrc AT401 · Reciprocating Engine Cylinder Section
  > ACFT DEVELOPED HEAVY VIBRATION DUE TO A STUCK EXHAUST VALVE IN THE CYLINDER ASSY.
- [SDR 2010FA0001228](https://openairdocs.org/sdr/2010FA0001228.md): Hinge · damaged · Nov 3, 2010 · N5485V · Namer SNJ6 · Ailerons
  > RT WING TIP, AILERON, BRACKET AND HINGE DAMAGED. APPEARS TO BE CONTACT WITH PAVEMENT.
- [SDR 2010FA0000957](https://openairdocs.org/sdr/2010FA0000957.md): Cylinder Head · cracked · Jul 21, 2010 · Reciprocating Engine Cylinder Section
  > CYLINDER NR2 CRACKED IN AREA OF FRONT SPARK PLUG TO REAR SPARK PLUG. THIS DEFECT IS CALLED OUT IN: AD 99-11-02 AND SB 1787.
- [SDR CA100806012](https://openairdocs.org/sdr/CA100806012.md): Cylinder Head · failed · Jul 12, 2010 · Reciprocating Engine Cylinder Section
  > (CAN) 3 CYLINDERS HAVE FAILED WITHIN THE LAST 33 HOURS ENGINE TIME. NR 6 & 8 CYLINDERS SPLIT HORIZONTALLY BELOW THE SPARK PLUG HOLE AT THE HEAD TO BARREL JUNCTION AT TAKEOFF POWER ON 2 SEPARATE OCCASIONS. A CRACK HAS BEEN DISCOVERED IN THE SAME LOCATION ON C
- [SDR CA100608011](https://openairdocs.org/sdr/CA100608011.md): Fitting · worn · Jun 7, 2010 · Namer HARVARD* · Horizontal Stabilizer, Attach Fittings
  > DURING MX IN THE AREA, MOVEMENT WAS FOUND BETWEEN THE HORIZ STABILIZER REAR SPAR CONNECTOR FITTING, PN 77-121021(LWR) AND THE REAR SPAR. FURTHER MOVEMENT WAS ALSO FOUND AT PN 52-31107 (FITTING -FUSELAGE HORIZ STABILIZER REAR ATTACHING LT) WHERE IT MOUNTS TO P
- [SDR 2010FA0000341](https://openairdocs.org/sdr/2010FA0000341.md): Isolator · split · Apr 14, 2010 · N3370 · Airtrc AT301 · Engine Mount Section
  > ENGINE ISOLATOR MOUNTS PN 22387 WERE REPLACED WHEN ACFT RESTORED. FIRST ANNUAL AFTER INSTALLATION WITH APPROX 60 HRS TIS MOUNTS SHOWED EXCESSIVE CRACKING AND DETERIORATION REQUIRING REPLACEMENT. LOWER MOUNTS SHOWED THE MOST AMOUNT OF WEAR WITH THE AREA AROUND
- [SDR 2008FA0000652](https://openairdocs.org/sdr/2008FA0000652.md): Engine · stopped · Aug 22, 2008 · N2391Z · Airtrc AT301 · Engine (Reciprocating)
  > ENGINE QUIT IN MID-AIR. ENGINE HAD 1195.0 HOURS SINCE MAJOR OVERHAUL. (K)
- [SDR CA080812005](https://openairdocs.org/sdr/CA080812005.md): Exhaust Valve · broken · Aug 3, 2008 · Dhav DHC3 · Reciprocating Engine Cylinder Section
  > (CAN) EXHAUST VALVE BROKE IN CRUISE FLIGHT 15 MIN AFTER DEPARTURE. PARTIAL POWER LOSS - ENGINE VIBRATION. PRECAUTIONARY LANDING EXECUTED. SERVICEABLE CYL COMPLETE INSTALLED AFTER LOCATING THE DEFECT/FAILURE. ACFT RETURNED TO SERVICE.
- [SDR 2008FA0000379](https://openairdocs.org/sdr/2008FA0000379.md): Spar · corroded · May 30, 2008 · N3628D · Scwzer G164B · Rudder, Spar/Rib
  > FOUND EXTERNAL CORROSION ON RUDDER MAIN TUBULAR SPAR APPROXIMATELY (2) INCHES ABOVE RUDDER CONTROL HORN. POST WAS SEVERELY CORRODED WITH HOLES THRU TUBE. AD 78-08-09 ADDRESSES THIS PROBLEM BUT NOT FOR THIS MODEL AIRCRAFT. (K)
- [SDR CA071128012](https://openairdocs.org/sdr/CA071128012.md): Battery · shorted · Nov 23, 2007 · Namer HARVARDMK4 · Battery/Charger System
  > (CAN) AC SUFFERED ALMOST AN ENTIRE ELECTRICAL FAILURE DURING CLIMBOUT. AFTER SUBSEQUENT UNSCHEDULED LANDING, IT WAS DETERMINED THAT THE BATTERY HAD ACQUIRED AN INTERNAL SHORT, WHICH DEPLETED THE GENERATOR OUTPUT AND CAUSED THE AVIONICS TO MALFUNCTION. BATTERY
- [SDR CA070817003](https://openairdocs.org/sdr/CA070817003.md): Pin · sheared · Aug 16, 2007 · Namer HARVARDMK4 · Wheel/Ski/Float
  > (CAN) DURING 50 HOUR INSP, EXCESSIVE ROTATIONAL MOVEMENT WAS NOTED ON THE TAIL WHEEL KNUCKLE (FORK), WITH THE TAIL WHEEL CONTROL LOCK ON. TAIL WHEEL MAST WAS DISMANTLED AND PIN HOLDING THE UPPER AND LOWER EXTENSION PIECES TOGETHER WAS FOUND SHEARED. THIS COULD
- [SDR CA070411005](https://openairdocs.org/sdr/CA070411005.md): Strut · corroded · Apr 10, 2007 · Dhav DHC3 · Fuselage Main, Structure
  > (CAN) DURING REPLACEMENT OF THE LT WINDSCREEN, CORROSION WAS FOUND ON THE STRUT PN C3FS2-49. AFTER REMOVAL OF SEALANT IT WAS NOTED THE STRUT WAS CORRODED COMPLETELY THROUGH ONE OF THE WALLS OF THE STRUT. RT STRUT INSPECTED AND NO FAULT FOUND (TC NR 20070411
- [SDR N6WA1209002](https://openairdocs.org/sdr/N6WA1209002.md): Connector · damaged · Dec 9, 2006 · N156 · Cndair CL6002C10 · Light System Wiring
  > NR 3 BATTERY PACK WILL NOT TURN OFF. FOUND PIN RESET IN CONNECTOR FOR NR 3 BATTERY, RESET PIN, OPS CHECK GOOD.
- [SDR N6WA00612001](https://openairdocs.org/sdr/N6WA00612001.md): Battery Pack · inoperative · Dec 8, 2006 · N156 · Cndair CL6002C10 · Emergency Lighting
  > EMERGENCY LIGHT BATTERY PACK INOP. REPLACED NR 3 BATTERY PACK. OPS CHECK GOOD.
- [SDR 2006FA0001206](https://openairdocs.org/sdr/2006FA0001206.md): Nut · damaged · Dec 6, 2006 · N8960Q · Ayres S2RRESTD · Wing Spar
  > WHILE PERFORMING (SPLICE BLOCK) MAINTENANCE A NEW TUBE NUT HAD ITS THREADS PULLED OUT BEFORE REACHING TORQUE. THE FOLLOW ON PART WAS EXAMINED AND WAS FOUND TO BE LOOSE ON THE BOLT, EVEN THE USED TUBE NUT WAS TIGHTER. SUSPECT PANTS HAVE NO PN OR STAMP, ALSO N
- [SDR 2006FA0000015](https://openairdocs.org/sdr/2006FA0000015.md): Door · bulged · Jan 4, 2006 · N4914X · Ayres S2R · Passenger/Crew Doors
  > CARBON MONOXIDE ENTRANCE INTO CABIN AREA. INCREASED AIRSPEED RESULTING FROM THIS COMBINATION CAUSED THE RT CABIN DOOR TO BULGE SLIGHTLY. PILOT CONCERNS ABOUT CARBON MONOXIDE ENTRANCE INTO THE CABIN WERE CONFIRMED WITH THE USE OF CO DETECTORS. RT CABIN DOOR
- [SDR 2005FA0000992](https://openairdocs.org/sdr/2005FA0000992.md): Attach Angle · corroded · Jul 22, 2005 · N7621Z · Namer AT6D · Wing, Attach Fittings
  > WING ATTACH ANGLE, CORROSION WITH LINEAR INDICATIONS. (K)
- [SDR CA050803007](https://openairdocs.org/sdr/CA050803007.md): Pushrod · broken · Jul 4, 2005 · Dhav DHC3 · Reciprocating Engine Power Section
  > (CAN) NR 2 CYL EXHAUST ALUMINUM PUSH ROD BROKEN NEAR THE TOP FITTING.
- [SDR 2005FA0000991](https://openairdocs.org/sdr/2005FA0000991.md): Attach Angle · cracked · Jun 30, 2005 · N7678Z · Namer AT6C · Wing, Attach Fittings
  > WING ATTACH ANGLE, CRACKING BETWEEN ROWS OF FASTENERS. (K)
- [SDR 2005FA0000953](https://openairdocs.org/sdr/2005FA0000953.md): Angle · corroded · Jun 27, 2005 · N92778 · Namer AT6G · Wing, Attach Fittings
  > UPON COMPLYING WITH EMERGENCY AD 2005-12-51 IT WAS DISCOVERED THE LT OUTER WING LOWER BOLTING ANGLE P/N 54-14030 WAS HEAVILY DAMAGED BY PITTING, FILIFORM & ESPECIALLY EXFOLIATION TYPE CORROSIONS. THIS DAMAGE WAS ONLY FOUND AFTER STRIPPING PAINT & PRIMER AWAY
- [SDR CA050712004](https://openairdocs.org/sdr/CA050712004.md): Exhaust Valve · broken · Jun 21, 2005 · Dhav DHC3 · Reciprocating Engine Cylinder Section
  > EXHAUST VALVE BROKE ON NR 1 CYLINDER AND FOUND IN EXHAUST STACK.
- [SDR CA050616003](https://openairdocs.org/sdr/CA050616003.md): Window Post · corroded · May 30, 2005 · Dhav DHC3 · Fuselage Main, Structure
  > (CAN) DURING AN UNSCHEDULED WINDSHIELD REPLACEMENT IT WAS NOTICED THE RT POST WAS CORRODED TO THE EXTENT THAT THE POST NO LONGER PROVIDED THE INTENDED SUPPORT.
- [SDR CA050329001](https://openairdocs.org/sdr/CA050329001.md): Universal Joint · worn · Mar 10, 2005 · Amtr 2 · Trailing Edge Flap Control System
  > (CAN) THE 2 UNIVERSAL JOINTS CONNECTING CENTER SECTION FLAP TO RT FLAP WORN. THE WORN JOINTS CAUSED THE 2 SETS OF FLAP ROLLERS BOTH IB AND OB OF THE UNIVERSALS TO ALSO BE AFFECTED. ALL ABOVE ITEMS WERE REPLACED WITH NEW PARTS.
- [SDR CA050329011](https://openairdocs.org/sdr/CA050329011.md): Rod · cracked · Mar 9, 2005 · Amtr 2 · Aileron Control System
  > (CAN) LT AILERON PUSH PULL ROD REMOVED TO CLEAN CORROSION FROM STEEL ENDS, AFTER CLEANING INSPECTION REVEALED A CRACK PROGRESSING FROM THE INNER RIVET. SUSPECT CRACK FROM AGE HARDENING OF COMPONENT, APPROXIMATELY 61 YEARS OF AGE.
- [SDR 2005FA0000192](https://openairdocs.org/sdr/2005FA0000192.md): Crankshaft · fractured · Feb 7, 2005 · Scwzer G164A · Reciprocating Engine Power Section
  > THE CRANKSHAFT REAR HALF FRACTURED IN TWO, JUST AFT OF THE MASTER ROD BEARING JOURNAL. (K)
- [SDR 2004FA0000764](https://openairdocs.org/sdr/2004FA0000764.md): Bushing · obstructed · Jul 2, 2004 · N915X · Scwzer G164A · Reciprocating Engine Rear Section
  > ENGINE LOST POWER ON TAKE-OFF. PILOT LANDED IN BOG AND FLIPPED OVER. PRELIMINARY INSPECTION SHOWED DAMAGE TO INDUCTION IMPELLER. TEARDOWN REVEALED IMPELLER SHAFT SUPPORTED BY TWO BRONZE BUSHINGS WHICH ARE LUBRICATED BY AN.1250 INCH HOLE ON BOTH BUSHINGS AN
- [SDR 2004FA0000668](https://openairdocs.org/sdr/2004FA0000668.md): Bolt · cracked · Jun 17, 2004 · Reciprocating Engine Power Section
  > THE CRANKSHAFT THRU BOLT APPEARS TO HAVE FRACTURED IN THE AREA JUST BELOW THE THREADS IN THE NECKED DOWN AREA. THE HEAD OF THE COTTER PIN THAT SAFETY LOCKS THE BOLT WAS FOUND IN THE OIL SUMP. THE ENGINE WAS THEN REMOVED AND DISASSEMBLED. UNKNOWN PROBABLE CA
- [SDR HJB2004F00000](https://openairdocs.org/sdr/HJB2004F00000.md): Screw · defective · Jan 23, 2004 · N336AK · Dhav DHC3 · Fasteners
  > BAD LOCKING SCREW.
- [SDR 2002FA0001375](https://openairdocs.org/sdr/2002FA0001375.md): Nut · cracked · Dec 6, 2002 · N1008Q · Airtrc AT401 · Propeller Hub Section
  > A NEWLY OVERHAULED "0" TIME PROPELLER WAS INSTALLED 05/31/01. DURING MAINTENANCE JULY 5, 2002 THE PROPELLER HAD TO BE REMOVED TO FACILITATE OTHER WORK. DURING THE REMOVAL IT WAS DISCOVERED THAT THE PROPELLER RETAINING NUT WAS CRACKED THE FULL HEIGHT OF THE N
- [SDR 2002FA0001376](https://openairdocs.org/sdr/2002FA0001376.md): Nut · cracked · Dec 6, 2002 · N1008Q · Airtrc AT401 · Propeller Hub Section
  > A NEWLY OVERHAULED "0" TIME PROPELLER WAS INSTALLED 05/31/01. DURING MAINTENANCE JULY 5, 2002 THE PROPELLER HAD TO BE REMOVED TO FACILITATE OTHER WORK. DURING THE REMOVAL IT WAS DISCOVERED THAT THE PROPELLER RETAINING NUT WAS CRACKED THE FULL HEIGHT OF THE N
- [SDR 2002FA0001343](https://openairdocs.org/sdr/2002FA0001343.md): Control Cable · broken · Nov 19, 2002 · N7197C · Namer T6G · Landing Gear Steering System
  > AFTER NORMAL LANDING AND ROLLOUT AIRCRAFT SUDDENLY VERIED RT. PILOT BRAKED BUT AIRCRAFT NOSED OVER AND CAME TO REST UPSIDE DOWN. DURING INVESTIGATION FOUND BROKEN STEERING CONTROL CABLE (LEFT).
- [SDR 2002FA0001350](https://openairdocs.org/sdr/2002FA0001350.md): Wire · failed · Nov 18, 2002 · N7502A · Scwzer G164B · Landing Gear Retraction/Extension System
  > LANDING WIRE SEPARATED IN FLIGHT ON RT WING. AIRCRAFT RETURNED FOR LANDING. RT WING SETTLED TO RUNWAY AS AIRCRAFT SLOWED. WIRE APPEARS TO HAVE SMALL ELECTRICAL ARC AT FAILURE POINT THAT COULD HAVE CREATED AS STRESS RISER OCCURRENCE ON 8/28/2002.
- [SDR 2002FA0000781](https://openairdocs.org/sdr/2002FA0000781.md): Rocker Shaft · departed · Jun 1, 2002 · N48485 · Scwzer G164B · Reciprocating Engine Cylinder Section
  > WHILE FLYING, NR 3 ROCKER SHAFT ON EXHAUST VALVE EXITED THE AIRCRAFT CAUSING THE ENGINE TO LOSE POWER. AIRCRAFT MADE A FORCED LANDING INTO A PLOWED FIELD CAUSING THE AIRCRAFT TO FLIP OVER. THE ENGINE HAD 185 HOURS SINCE OVERHAUL, PART COULD NOT BE FOUND, BUT
- [SDR 2001FA0000195](https://openairdocs.org/sdr/2001FA0000195.md): Cylinder · cracked · Jul 3, 2001 · N3164H · Airtrc AT301 · Reciprocating Engine Cylinder Section
  > THE NR 3 CYLINDER HEAD CRACKED AT THE ROCKER BOSS, ENGINE LOST POWER, AIRCRAFT EMERGENCY LANDED IN A FIELD. 2ND OCCURANCE.
- [SDR CA010628012](https://openairdocs.org/sdr/CA010628012.md): Tube · broken · May 11, 2001 · Dhav DHC3 · Propeller Controlling System
  > (CAN) COULD NOT CYCLE PROPELLER. FOUND OIL TRANSFER TUBE IN NOSE CASE BROKEN AT ATTACH POINT IN CENTRE OF TUBE. ONE TUBE REPLACED AT 274 HOURS SINCE OVERHAUL AND ANOTHER TUBE WAS REPLACED WITH 243 HOURS SINCE REPLACEMENT. THESE ARE 2 SEPARATE OCCURANCES.
- [SDR CA010403011](https://openairdocs.org/sdr/CA010403011.md): Cable · broken · Mar 6, 2001 · Dhav DHC3 · Power Lever
  > (CAN) DURING THE PRE-FLIGHT RUN-UP, THE THROTTLE CONTROL WAS NOT RESPONDING PROPERLY. INVESTIGATION FOUND THAT THE FLEX CABLE WAS BROKEN INSIDE THE TUBING.
- [SDR 99ZZZX2537](https://openairdocs.org/sdr/99ZZZX2537.md): Sun Gear · failed · Jun 15, 1999 · N511BW · Dhav DHC3 · Turbine Engine Reduction Gear
  > UPON TOUCH DOWN RUN, AT TAKEOFF POWER SETTING, ENGINE RUNNING AT FULL POWER FAILED TO POWER PROPELLER. UPON INVESTIGATION, SUN GEAR IN REDUCTION GEARBOX WAS FOUND TO BE IN 3 PIECES. FAILURE DUE TO CRACKED GEAR. REASON FOR CRACKS, UNKNOWN. REPLACED NOSE CAS
- [SDR CA980331001](https://openairdocs.org/sdr/CA980331001.md): Seal · failed · Mar 31, 1998 · Dhav DHC3 · Exhaust Turbocharger
  > (CAN) ENGINE PROBLEM ON DESCENT. SUSPECT BLOWER (SUPERCHARGER) SEAL FAILURE.
- [SDR 98ZZZX184](https://openairdocs.org/sdr/98ZZZX184.md): Roller · spalled · Dec 16, 1997 · Scwzer G164B · Reciprocating Engine Power Section
  > AT THE TIME OF ROUTINE MAINTENANCE, METAL WAS DISCOVERED IN THE OIL SCREEN AND FILTER AND ALSO THE CHIP DETECTOR LIGHT CAME ON. UPON INSPECTION, FOUND THE VALVE TAPPET ROLLERS SPALLING.
- [SDR CA970926010](https://openairdocs.org/sdr/CA970926010.md): Cylinder · separated · Sep 12, 1997 · Dhav DHC3 · Reciprocating Engine Cylinder Section
  > (CAN) THE AIRCRAFT WAS ON DESCENT, FOR SEVERAL MINUTES, WITH REDUCED POWER, THE ENGINE BACKFIRED AND QUIT. POWER OFF LANDING CARRIED OUT ON LAKE. THE ENGINE WAS RESTARTED FOR TAXIING, BUT RAN ROUGH AND WAS SHUTDOWN. INSPECTION FOUND THE NR1 CYLINDER HEAD HAD S
- [SDR CA970822006](https://openairdocs.org/sdr/CA970822006.md): Cylinder · cracked · Aug 2, 1997 · Dhav DHC3 · Reciprocating Engine Cylinder Section
  > (CAN) NR2 CYLINDER FOUND CRACKED ON 100 HOUR INSPECTION.

Next page: https://openairdocs.org/engine/pratt-whitney-r1340-series/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 = 'R1340'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/engine/pratt-whitney-r1340-series/reports

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