# Service difficulty reports: Piper PA-32RT-300

A list on [Piper PA-32RT-300](https://openairdocs.org/model/piper-pa-32rt-300.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 2 · 53 reports

- [SDR 2026FA0000637](https://openairdocs.org/sdr/2026FA0000637.md): Servo · faulted · Aug 13, 2026 · N3041B · Piper PA32RT300 · Engine Fuel Distribution
  > PILOT REPORTED THE FUEL PRESSURE PEGGED MAX PRESSURE CAUSING THE GAUGE TO BECOME INOP. IT WAS REPLACED AND AGAIN THE GAUGE WENT TO MAX & BECAME INOP, THE FUEL FLOW AT FULL THROTTLE NOW EXCEEDS 30GPH INDICATED WHERE IT USED TO BE 28GPH & ALL THE CYLINDER HEAD T
- [SDR 17GR20191108901](https://openairdocs.org/sdr/17GR20191108901.md): Valve · bent · Nov 8, 2019 · N39551 · Piper PA32RT300 · Reciprocating Engine Cylinder Section
  > DURING 50 HOUR INSPECTION NO COMPRESSION ON CYLINDER 4. INSPECTION REVEALED STUCK EXHAUST VALVE AND BENT PUSH ROD.
- [SDR 2017FA0000594](https://openairdocs.org/sdr/2017FA0000594.md): Squat Switch · out of adjust · Nov 14, 2017 · N356DP · Piper PA32RT300 · Landing Gear Position and Warning
  > SQUAT SWITCH FOUND OUT OF ADJUSTMENT, NOSE LANDING GEAR POSITION LIGHT DID NOT ILLUMINATE WHEN GEAR HANDLE WAS LOWERED.
- [SDR 17GR2016051600001](https://openairdocs.org/sdr/17GR2016051600001.md): Rib · cracked · May 13, 2016 · N89VG · Piper PA32RT300 · Wing, Rib/Bulkhead
  > PERFORMING INSPECTION AS PART OF SB 1161, DISCOVERED CRACKS IN BOTH WHEEL WELLS. CRACKS WERE VISIBLE WITHOUT NDT INSPECTION. THE WERE RADIATING FROM THE LOWER CORNER UP.
- [SDR 17GR2015FA0000253](https://openairdocs.org/sdr/17GR2015FA0000253.md): Trunnion · cracked · May 29, 2015 · N39551 · Piper PA32RT300 · Wing, Landing Gear Attach Fittings
  > PERFORMING SB 1161, DISCOVERED CRACKS IN RADIUS OF LT AND RT WHEEL WELL AT SIDE STRUT ATTACH POINT.
- [SDR MGOR201405210001](https://openairdocs.org/sdr/MGOR201405210001.md): Trunnion · cracked · May 20, 2014 · N39478 · Piper PA32RT300 · Wing, Landing Gear Attach Fittings
  > OPERATOR REPORTED THEIR RT STRUT WAS FLAT. VISUALLY INSPECTED STRUT AND NO OBVIOUS LEAKS NOTED. SERVICED STRUT WITH NITROGEN TO RAISE ACFT FOR JACK INSTALLATION. NOTICED FINE MIST EMANATING FROM CRACK ON THE AFT SIDE OF THE UPPER TRUNNION. NOTE: PAINT CHIP
- [SDR 2012FA0000783](https://openairdocs.org/sdr/2012FA0000783.md): Turnbuckle · broken · Nov 29, 2012 · N41EK · Piper PA32RT300 · Elevator Control System
  > AFT FUSELAGE ELEVATOR CABLE TURNBUCKLE END, CRACKED AND BROKE OFF AT THE BARREL SIDE IN THE SHANK PART,.6250" BACK FROM THE THREADED PORTION OF THE TURNBUCKLE END, JUST AT THE THICKER PART WHERE THE SAFETY WIRE HOLE IS, OPPOSITE THE SWEDGED END. THERE WAS E
- [SDR 2010FA0000002](https://openairdocs.org/sdr/2010FA0000002.md): Vernatherm · distorted · Jan 7, 2010 · N82EB · Piper PA32RT300 · Engine Oil Cooler
  > AFTER REMOVING THE LT OIL COOLER SUPPLY HOSE AT THE CASE FOR ACCESS TO MAGNETO, IT WAS NOTICED THAT THE NUT OFF THE END OF THE VERNATHERM WAS STUCK IN THE FITTING STICKING OUT OF THE CASE. VERNATHERM WAS REMOVED AND REMAINING PARTS LOCATED. INSPECTED SEAT AR
- [SDR FFKA140](https://openairdocs.org/sdr/FFKA140.md): Ring · broken · Jul 20, 2009 · N169BW · Piper PA32RT300 · Reciprocating Engine Power Section
  > SHORTLY AFTER TAKEOFF, WHILE CLIMBING THROUGH ABOUT 3000 FT, ENGINE LOST ABOUT 200 - 300 RPM MOMENTARILY AND THEN RECOVERED. IT DID THIS 2 TIMES AND THEN WENT BACK TO NORMAL. NOT LONG AFTER THIS NOTICED THAT THE OIL PRESSURE HAD DIPPED INTO THE YELLOW. MX C
- [SDR FFK2008F00001](https://openairdocs.org/sdr/FFK2008F00001.md): Magneto · broken · Jul 23, 2008 · N169BW · Piper PA32RT300 · Magneto/Distributor
  > PILOT REPORTED OIL LEAKING FROM THE ENGINE COWLING AFTER THE LAST FLIGHT OF THE DAY. MAINT TROUBLESHOT PROBLEM TO BE COMING FROM THE DUEL MAGNETO, PN BL-68256013, SN- G07GA121R, TSO 373. THE BOTTOM MOUNTING FLANGE HAD BROKEN OFF OF THE MAGNETO HSG CAUSING TH
- [SDR 2008F00009](https://openairdocs.org/sdr/2008F00009.md): Landing Gear · collapsed · Mar 19, 2008 · N360SB · Piper PA32RT300 · Landing Gear Retraction/Extension System
  > NOSE LANDING GEAR COLLAPSED AFTER LANDING BUT WHILE STILL MOVING UNDER ITS OWN POWER.
- [SDR 2006FA0001179](https://openairdocs.org/sdr/2006FA0001179.md): Connecting Rod · failed · Dec 5, 2006 · N2148N · Piper PA32RT300 · Reciprocating Engine Cylinder Section
  > INTERNAL ENGINE FAILURE, CYLINDERS 2 AND 4 CONNECTING RODS FAILED. ENGINE WAS ORIGINAL TO THE AIRCRAFT (1979).
- [SDR 2006FA0000604](https://openairdocs.org/sdr/2006FA0000604.md): Control Cable · separated · Jun 14, 2006 · N31709 · Piper PA32RT300 · Elevator Control System
  > CABLE TURNBUCKLE MALE END SEPARATED AT FITTING DURING ROLLOUT AFTER LANDING. FITTING SEEMS TO HAVE CORRODED FROM THE SHANK CORE AND PROGRESSED OUTWARD TO THE SURFACE OVER TIME. (K)
- [SDR 2006FA0000611](https://openairdocs.org/sdr/2006FA0000611.md): Control Cable · separated · Jun 12, 2006 · N31709 · Piper PA32RT300 · Elevator Control System
  > UP ELEVATOR CABLE SEPARATED DURING LANDING FLARE.
- [SDR 2006FA0000610](https://openairdocs.org/sdr/2006FA0000610.md): Control Cable · separated · Jun 12, 2006 · N31709 · Piper PA32RT300 · Elevator Control System
  > UP ELEVATOR CABLE SEPARATED DURING LANDING FLARE.
- [SDR 2006FA0000609](https://openairdocs.org/sdr/2006FA0000609.md): Control Cable · separated · Jun 12, 2006 · N31709 · Piper PA32RT300 · Elevator Control System
  > UP ELEVATOR CABLE SEPARATED DURING LANDING FLARE.
- [SDR 2006FA0000608](https://openairdocs.org/sdr/2006FA0000608.md): Control Cable · separated · Jun 12, 2006 · N31709 · Piper PA32RT300 · Elevator Control System
  > UP ELEVATOR CABLE SEPARATED IN LANDING FLARE.
- [SDR 2005FA0001622](https://openairdocs.org/sdr/2005FA0001622.md): Downlock Switch · broken · Nov 22, 2005 · N39503 · Piper PA32RT300 · Landing Gear Position and Warning
  > UPON ARRIVING AT DESTINATION GEAR WAS SELECTED DOWN. NOSE GEAR GREEN LIGHT DID NOT ILLUMINATE AND IN TRANSIT LIGHT STAYED ON. INSPECTED AND FOUND NOSE GEAR DOWNLOCK SWITCH ACTUATING ARM BROKEN OFF. DETERMINED CAUSE OF BREAKING WAS TIME IN SERVICE AND WORK
- [SDR 2005FA0001503](https://openairdocs.org/sdr/2005FA0001503.md): Window · cracked · Oct 19, 2005 · N39503 · Piper PA32RT300 · Flight Compartment Windows
  > LT FORWARD SIDE WINDOW. CRACKED AND BROKEN 2 PLACES AROUND SIDE VENT WINDOW CAUSING LARGE SECTION TO BECOME LOOSE. (K)
- [SDR AU510001607](https://openairdocs.org/sdr/AU510001607.md): Landing Gear · collapsed · Jan 7, 2005 · Piper PA32RT300 · Main Landing Gear
  > LT MAIN LANDING GEAR COLLAPSED. AIRCRAFT AND LANDING GEAR DAMAGED.
- [SDR 2003FA0000704](https://openairdocs.org/sdr/2003FA0000704.md): Float · worn · Jul 14, 2003 · N31642 · Piper PA32RT300 · Fuel Quantity Indicator
  > FUEL QUANTITY FLOAT P/N 38230-002. COMPOSITE FLOAT HAS BEEN HITTING THE UPPER BODY OF THE ASSY WHEN IN A FULL CONDITION AND HAS WORN.2500 INCH GROOVE ON ONE SIDE OF FLOAT AND.1875 INCH GROOVE ON THE OTHER SIDE. GAUGE STILL OPERATED, BUT PARTICLES OF THE COM
- [SDR AUS20020998](https://openairdocs.org/sdr/AUS20020998.md): Rib · cracked · Sep 6, 2002 · Piper PA32RT300 · Wing, Rib/Bulkhead
  > (AUS) RH WING RIB CRACKED ALONG RIVET LINE IN THREE PLACES.
- [SDR AUS20020997](https://openairdocs.org/sdr/AUS20020997.md): Doubler · cracked · Sep 6, 2002 · Piper PA32RT300 · Wing, Plate/Skin
  > (AUS) WING WALK SKIN CORRUGATED DOUBLER CRACKED IN AREA NEAR RIB AT STN36.9.
- [SDR SO52002F00000](https://openairdocs.org/sdr/SO52002F00000.md): Line · corroded · Aug 5, 2002 · N319SF · Piper PA32RT300 · Fuel Indicating System
  > PILOT REPORTED STRONG SMELL OF FUEL (AVGAS) IN COCKPIT. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND FUEL LINE FROM FUEL PRESSURE GAUGE TO FORWARD BULKHEAD AT STA 53.60 LEAKING. LINE WAS SEVERLY CORRODED IN A 1.5000 IN LONG SECTION APPROX. 3 INCHES
- [SDR AUS20020046](https://openairdocs.org/sdr/AUS20020046.md): Cable · failed · Jan 18, 2002 · Piper PA32RT300 · Elevator Tab Control System
  > (AUS) STABILATOR TRIM CABLE SEPARATED AT ELECTRIC TRIM SERVO ACTUATOR.
- [SDR 2001FA0000220](https://openairdocs.org/sdr/2001FA0000220.md): Muffler · split · Aug 6, 2001 · N3516M · Piper PA32RT300 · Engine Noise Suppressor
  > THE CENTER MUFFLER HOUSING SPLIT OPEN AT THE UPPER WELD SEAM ALLOWING EXHAUST TO DAMAGE THE UPPER ALUMINUM MUFFLER ASSEMBLY SHROUD AND THE ENGINE INDUCTION COVER. SUGGEST THAT A VERY CLOSE INSPECTION BE DONE BY BOTH VISUAL AND PRESSURE CHECK METHODS OF ALL MU
- [SDR 2001FA0000141](https://openairdocs.org/sdr/2001FA0000141.md): Gear · broken · Apr 26, 2001 · N39503 · Piper PA32RT300 · Magneto/Distributor
  > ON TAKE OFF AT APPROXIMATLEY 500 FEET THE ENGINE FAILED. THE AIRCRAFT LANDED IN GRASS AT END OF RUNWAY WITHOUT INCIDENT. INSPECTION SHOWED THAT BOTH DISTRIBUTOR GEARS HAD FAILED, TEETH MISSING.
- [SDR 2001FA0000154](https://openairdocs.org/sdr/2001FA0000154.md): Gear · broken · Apr 26, 2001 · N39503 · Piper PA32RT300 · Magneto/Distributor
  > AFTER TAKE OFF AT APPROX 500FT AGL, THE ENGINE STOPPED RUNNING. AIRCRAFT MADE EMERGENCY LANDING IN A FIELD WITH NO DAMAGE OR INJURIES. INSPECTION OF MAGNETO REVEALED THAT BOTH DISTRIBUTOR GEARS HAD FAILED. MAGNETO WAS REBUILT BY TCM 04/07/2000 AND INSTALLED
- [SDR 20010416CW006](https://openairdocs.org/sdr/20010416CW006.md): Attach Fitting · cracked · Jan 8, 2001 · N6873C · Piper PA32RT300 · Wing, Attach Fittings
  > INSPECTED AIRFRAME, FOUND THREE SEPARATE CRACKS IN THE LEFT WING FORWARD ATTACH FITTING AREA.
- [SDR 20001019SH007](https://openairdocs.org/sdr/20001019SH007.md): Seal · failed · Sep 1, 2000 · N28WC · Piper PA32RT300 · Reciprocating Engine Oil System
  > SEAL SOFTENED, SWELLED, RUPTURED. NIGHT, PART 135 FLIGHT LOST OIL, ENGINE SEIZED. SEAL MATERIAL NOT OIL PROOF. SUBMITTER SUGGESTED RETURNING TO ORIGINAL MATERIAL. (X)
- [SDR 20000831SH015](https://openairdocs.org/sdr/20000831SH015.md): Engine · failed · Aug 31, 2000 · N165R · Piper PA32RT300 · Engine (Reciprocating)
  > AIRCRAFT WAS IN-FLIGHT WHEN ENGINE LOST ALL OIL PRESSURE, AND HAD A CATASTROPHIC FAILURE. AIRCRAFT WAS ABLE TO MAKE A SAFE OFF-FIELD LANDING WITH NO STRUCTURAL DAMAGE. ENGINE WAS OVERHAULED ENGINE FROM LYCOMING. ENGINE SHOPPED TO LYC FOR INSPECTION. (X)
- [SDR AU000606](https://openairdocs.org/sdr/AU000606.md): Nut · split · Jul 19, 2000 · Piper PA32RT300 · Vertical Stabilizer, Attach Fittings
  > (AUS) ANCHOR NUT FOR RIGHT FORWARD FIN ATTACH BOLT SPLIT.
- [SDR 20000504SH030](https://openairdocs.org/sdr/20000504SH030.md): O-Ring · failed · Mar 22, 2000 · N800TM · Piper PA32RT300 · Landing Gear Actuator
  > AFTER TAKEOFF, THE NOSE GEAR FAILED TO FULLY RETRACT AND WOULD NOT EXTEND TO DOWN AND LOCKED POSITION. THE PILOT PERFORMED VAROIUS MANEUVERS AND GEAR FINALLY EXTENDED DURING A POWER OFF STALL. AFTER LANDING INSPECTION, FOUND THE SHAFT O-RING ON THE NOSE GEAR
- [SDR 99ZZZX2638](https://openairdocs.org/sdr/99ZZZX2638.md): Fitting · corroded · Jul 1, 1999 · N89VG · Piper PA32RT300 · Rudder Structure
  > INSPECTED RUDDER LOWER ATTACH BOLTS AT OWNER'S REQUEST. FOUND LOWER BOLT MISSING AND THE REMAINING BOLT SHOWING SIGNS OF CORROSION AND WEAR. SUBMITTER SUGGESTED DUE POSSIBLY TO STRESS CAUSED BY THE ONE MISSING BOLT.
- [SDR 99ZZZX1938](https://openairdocs.org/sdr/99ZZZX1938.md): Trunnion · failed · Jan 18, 1999 · N39921 · Piper PA32RT300 · Main Landing Gear Attach Section
  > LANDING GEAR TRUNNION FAILED.
- [SDR 99ZZZX1648](https://openairdocs.org/sdr/99ZZZX1648.md): Trunnion · failed · Jan 18, 1999 · N39540 · Piper PA32RT300 · Main Landing Gear Attach Section
  > TRUNNION FOUND DAMAGED ON PRE-FLIGHT INSPECTION.
- [SDR 98ZZZX3013](https://openairdocs.org/sdr/98ZZZX3013.md): Alternator · failed · Jul 18, 1998 · N31609 · Piper PA32RT300 · DC Generator-Alternator
  > ALTERNATOR FAILED DUE TO OLD AGE.
- [SDR 97ZZZX4726](https://openairdocs.org/sdr/97ZZZX4726.md): Connecting Rod · failed · Oct 21, 1997 · N2200J · Piper PA32RT300 · Reciprocating Engine Power Section
  > ENGINE HAD A CATASTROPHIC FAILURE 10 MINUTES AFTER TAKEOFF. A SUCCESSFUL EMERGENCY LANDING WAS MADE IN A HAY FIELD. PILOT AND PASSENGER WERE NOT INJURED, AIRCRAFT WAS SUBSTANTIALLY DAMAGED. THE NR 2 CONNECTING ROD CREATED FOUR HOLES IN THE ENGINE CASE AND T
- [SDR 96ZZZX3357](https://openairdocs.org/sdr/96ZZZX3357.md): Trunnion · cracked · May 29, 1996 · N3421W · Piper PA32RT300 · Main Landing Gear Strut/Axle/Truck
  > LEFT MAIN GEAR STRUT FOUND COLLAPSED. FURTHER INSPECTION REVEALED TRUNNION ASSY PN 67926-12 CRACKED AND LEAKING. CRACK EXTENDED 90 PERCENT AROUND TRUNNION. CAUSE IS SUSPECTED TO BE FATIGUE. NOTE AD 94-13-11 ONLY EFFECTS PA34 AND PA44 AIRCRAFT. SUBMITTER S
- [SDR 96ZZZX4146](https://openairdocs.org/sdr/96ZZZX4146.md): P-Lead · shorting · Apr 10, 1996 · N376AA · Piper PA32RT300 · Ignition Harness (Distribution)
  > TROUBLESHOOTING FOR INTERMITTENT INOPERATIVE CONDITION ON RT MAGNETO FOUND P-LEAD SHORTING WHERE IT EXITS THROUGH FIREWALL. REPLACED P-LEADS AND INSTALLED PLASTIC SLEEVING.
- [SDR 96ZZZX1517](https://openairdocs.org/sdr/96ZZZX1517.md): Casting · out of spec · Mar 8, 1996 · N457SC · Piper PA32RT300 · Altimeter, Barometric/Encoder
  > TWO OF THE CRITICAL SHAFTS IN THE MECHANISM WERE UNDER THE MINIMUM END SHAKE CALLED OUT IN THE OVERHAUL MANUAL. THEY MEASURED.0005 INCH AND.0009 INCH (O/H MANUAL CALLS OUT.0020 INCH MINIMUM). SUBMITTER STATED THIS UNDER ENDSHAKE CONDITION COULD CAUSE A PO
- [SDR 95ZZZX6775](https://openairdocs.org/sdr/95ZZZX6775.md): Magneto · worn · Nov 14, 1995 · N3421W · Piper PA32RT300 · Magneto/Distributor
  > MAGNETO FLANGE WEAR. A D6LN-3000 (DUAL MAGNETO) WAS FOUND TO HAVE ITS BASE CLAMPS SECURED. HOWEVER, THE MAGNETO WAS ABLE TO CHAFE BETWEEN THE FLANGE AND THE HOLD-DOWN CLAMP. THIS CAUSED A WEAR PATTERN THE SHAPE OF THE 'MOUSE EAR CLAMP', PN 66M19385, INTO TH
- [SDR 95ZZZX6612](https://openairdocs.org/sdr/95ZZZX6612.md): Magneto · defective · Nov 14, 1995 · N3421W · Piper PA32RT300 · Magneto/Distributor
  > 'ACCESSORY CASE OIL LEAK'. A FACTORY LYCOMING ENGINE HAD A PERSISTENT SLIGHT OIL SEEP AT THE MAGNETO BASE. AFTER REMOVAL, IT WAS FOUND TO HAVE A FLAW IN THE APPARENT CASTING. A LOW SPOT IN THE GASKET AREA ALLOWED OIL TO SEEP BY. PART WAS REPLACED FOR THIS
- [SDR 95ZZZX5645](https://openairdocs.org/sdr/95ZZZX5645.md): Bolt · fractured · Sep 18, 1995 · N3046H · Piper PA32RT300 · Landing Gear Actuator
  > UPON COMPLIANCE WITH PIPER SB 747, NLG ACTUATOR ATTACHMENT BOLT (REAR) WAS FOUND SEVERELY WORN, BENT, AND FRACTURED WITH FORWARD CLEVIS BOLT, PN 400-871 (AN23-19A) FOUND WORN AND BENT ALSO. SUBMITTER SUGGESTS SB 747 SHOULD BE MANDATORY.
- [SDR 95ZZZX5233](https://openairdocs.org/sdr/95ZZZX5233.md): Fitting · cracked · Aug 30, 1995 · N222PP · Piper PA32RT300 · Nose/Tail Landing Gear Attach Section
  > FITTING INSTALLED TO C/W AD 93-05-10 AND PIPER SB 955 WHICH CALL OUT KIT 766-253. P/N 02867-2 IS PART OF KIT AND IT CRACKED AT FORWARD OUTBOARD CORNER OF WELD. OUTSIDE OF CORNER WELDED ONLY. SUBMITTER STATED INSIDE SHOULD BE WELDED.
- [SDR 95ZZZX4476](https://openairdocs.org/sdr/95ZZZX4476.md): Spar Attach · corroded · Jul 20, 1995 · N2578M · Piper PA32RT300 · Fuselage, Wing Attach Fittings
  > DURING ANNUAL INSPECTION, COMPLIANCE WITH PIPER SB 977, INSPECTION OF REAR SPAR ATTACH FITTINGS IN THE CABIN FOR CORROSION, AND FOUND THIS AREA SEVERELY CORRODED. SB IS APPLICABLE TO ALL PA28, PA32, PA34, AND PA44 SERIES OF AIRCRAFT. ALL INTERIOR AND FIBERGL
- [SDR 95ZZZX2958](https://openairdocs.org/sdr/95ZZZX2958.md): Valve · crimp nut loose · May 31, 1995 · N36590 · Piper PA32RT300 · Engine Oil Temperature Regulator
  > INSPECT OIL COOLER BYPASS VALVE PER LYCOMING SB 518B. FOUND LOOSE NUT. INSTALL NEW VALVE IAW SB.
- [SDR 95ZZZX3141](https://openairdocs.org/sdr/95ZZZX3141.md): Valve · missing · May 17, 1995 · N36398 · Piper PA32RT300 · Engine Oil Temperature Regulator
  > WHEN COMPLYING WTIIH LYCOMING SB 518C (COPY ATTACHED) FOUND CRIMPED NUT HOLDING VALVE TOGETHER WAS MISSING. UPON FURTHER INVESTIGATION, FOUND NUT LODGED IN HOSE ELBOW TO OIL COOLER.
- [SDR 95ZZZX3533](https://openairdocs.org/sdr/95ZZZX3533.md): Grease Seal · wrong part · May 15, 1995 · N222PP · Piper PA32RT300 · Wheel/Ski/Float
  > GREASE SEAL PN 153003 WILL NOT ALLOW AXLE SPACER TO PASS THROUGH ON TO BEARING. ASSEMBLY AS IS CAUSES SHIM TO CUT THROUGH GREASE SEAL AND DOES NOT ALLOW CORRECT PRESSURE ON BEARING. PN 153-004 WOULD BE CORRECT.
- [SDR 95ZZZX2950](https://openairdocs.org/sdr/95ZZZX2950.md): Contact Assy · tip broken · May 3, 1995 · N36590 · Piper PA32RT300 · Magneto/Distributor
  > PILOT NOTED A DEAD MAG IN THE RIGHT POSITION. INVESTIGATION REVEALED THE POINTS NOT OPENING. CONTACT ASSEMBLY HAS TIP BROKEN OFF. PART TOTAL TIME 30 HRS. TCM IGNITION SB 651 COVERS THIS, BUT IS NOT WELL KNOWN. RECOMMEND ALERT BE ISSUED.

Next page: https://openairdocs.org/model/piper-pa-32rt-300/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 = 'PA32RT300'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/piper-pa-32rt-300/reports

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