FAA incident reports · 1
FAA accident and incident reports matched to this aircraft by N69RP and the event date: up to this one’s cancellation.
Service difficulty reports · 15
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR 2007FA0001029Cylinder Head · crackedCRACKED CYLINDER HEAD BEHIND INJECTOR BETWEEN FIN NR 1, NR 3. DEFECTIVE MFG PROCESS. (K)SDR 2007FA0001023Cylinder Head · crackedCRACKED CYLINDER HEAD BEHIND INJECTOR BETWEEN FIN NR 1, NR 3. DEFECTIVE MFG PROCESS. (K)SDR 2007FA0001022Cylinder Head · crackedCRACKED CYLINDER HEAD BEHIND INJECTOR BETWEEN FIN NR 1, NR 3. DEFECTIVE MFG PROCESS. (K)SDR 2007FA0001021Cylinder Head · crackedCRACKED CYLINDER HEAD BEHIND INJECTOR BETWEEN FIN NR 1, NR 3. DEFECTIVE MFG PROCESS. (K)SDR 2007FA0001020Cylinder Head · crackedCRACKED CYLINDER HEAD BEHIND INJECTOR BETWEEN FIN NR 1, NR 3. DEFECTIVE MFG PROCESS. (K)SDR 2007FA0001019Cylinder Head · crackedCRACKED CYL HEAD BEHIND INJECTOR BETWEEN FIN NR 12, NR 3. DEFECTIVE MFG PROCESS. (K)SDR XGN2007F00025Cylinder · crackedNR 6 CYLINDER WAS NEW, REV 3, E SERIES, CRACKED BETWEEN FINS 1-3 BEHIND FUEL INJECTOR. THIS IS 6TH REV 3, E SERIES TO CRACK IN THE SAME LOCATION. (K)SDR XGN2007F00021Cylinder Head · crackedNR 6 CYLINDER WAS NEW ECI, REV 3, E SERIES, CRACKED BETWEEN FINS 1-3 BEHIND FUEL INJECTOR. THIS IS 6TH ECI, REV 3, E SERIES, TO CRACK IN THE SAME LOCATION. (K)SDR 2007FA0000698Cylinder · crackedNR 6 CYLINDER WAS NEW ECI REV 3 E SERIES CRACKED BETWEEN FINS 1-3 BEHIND FUEL INJECTOR. THIS IS 6TH ECI REV 3 E SERIES TO CARCK IN THE SAME LOCATION. (K)SDR XGN2004F00001Camshaft · brokenAIRCRAFT WAS ENROUTE, PIC NOTICED THE AIRCRAFT YAWING WAY TO THE RIGHT. THERE WAS NOT ANY LOSS OF OIL OR FUEL PRESSURE NOR ANY VIBRATION. THE PILOT SHUT THE ENGINE DOWN AND LANDED. THE OIL PAN WAS REMOVED AND FOUND THE CAMSHAFT WAS BROKEN. HAVE NO IDEA WHASDR XGN2002F00000Crankcase · crackedHALF CIRCLE CRACKED AT NR 6 CYLINDER PAD. CRACK RUNS FROM UPPER PART OF CRANKCASE FROM CYLINDER BASE STUD AT 2 OCLOCK POSITION TO CYLINDER BASE STUD AT 10 OCLOCK POSITION. WITH SEVERAL CRACK RADIATING FROM THE HALF CIRCLE CAUSING A SMALL TRIANGULAR PIECE TOSDR 20010411CW007Counterweight · separatedCOUNTERWEIGHT DEPARTED LEFT PROP ON TAKEOFF ROLL. SPINNER AND BACKING PLATE WERE DESTROYED. PROP HUB WAS CRACKED IN TWO PLACES. NO OTHER DAMAGE TO AIRCRAFT OR ENGINE. ROTOR COUNTERWEIGHT WAS NOT FOUND.SDR 95ZZZX6562Flap · failedUPON EXITING THE AIRCRAFT, THE WEIGHT OF THE PILOT STANDING ON THE RT FLAP, TORE THE ACTUATOR ATTACH BRACKET, RIPPED THE SKIN AND PULLED THE RIB ATTACHMENT OUT OF THE FLAP. THIS CONDITION ALLOWED THE FLAP TO GO TO THE EXTENDED POSTION. IN-FLIGHT, AN UNNOTICESDR 95ZZZX2261Oil Pan · crackedDURING FLIGHT, PILOT NOTICED OIL STREAMING FROM RT COWLING. INSPECTION BY MAINTENANCE PERSONNEL REVEALED A 2 INCH CRACK IN THE OIL PAN AT LOWER RADIUS. SUSPECT FATIGUE, POOR STAMPING, DURING MANUFACTURING.SDR 95ZZZX1099Cylinder · crackedDURING A 200-HOUR INSPECTION ALL CYLINDERS OF LT ENGINE PASSED A DIFFERENTIAL COMPRESSION TEST. CLOSER INSPECTION OF CLYLINDER ASSYS REVEALED CRACKS BETWEEN COOLING FINS OF SEVERAL CYLINDERS IN THE EXHAUST PORT AREA. NOTE: CRACKS ORIGINATING IN THIS AREA AR
Other aircraft with N69RP · 1
The FAA can assign a mark to another aircraft once a registration is cancelled. N69RP is registered now to the first aircraft listed.