JASC 7810
Service difficulty reports · 1,904
Reports filed under 7810 · Engine Collector/Tailpipe/Nozzle, newest first.
Query with SQL
duckdb -csv -c "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 jasc_code = '7810' ORDER BY difficulty_date DESC"
Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.
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 jasc_code = '7810' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR HEEA968688Duct Assy · crackedRT DUCT ASSY EXCESSIVE CRACKING.SDR 97ZZZX29Mount Tube · broken tabDURING ANNUAL INSPECTION, FOUND RT HAND FORWARD EXHAUST MUFFLER SUPPORT TUBE BROKEN AT LOWER ATTACH TAB. THIS TUBE ASSY IS THE SAME ONE USED ON ROCKET ENGINEERING 305 - ROCKET CONVERSION ON M20K SERIES MOONEY. THIS TUBE IS OF THE NEWER HEAVY DUTY TYPE DESIGNSDR HEEA968659Ejector Assy · crackedLT EJECTOR ASSY IS CRACKED.SDR HEEA968658Ejector Assy · crackedRT EJECTOR ASSY IS CRACKED.SDR HEEA968656Ejector Assy · crackedEJECTOR IS CRACKED.SDR HEEA968630Ejector Assy · crackedEJECTOR IS CRACKED. (ROUND CRACK AND WORKING RIVETS) SENT TO ALPINE AEROTECH LTD. FOR INSPECTION AND REPAIR.SDR 96ZZZX6168Stack · crackedTHE RIGHT ENGINE INBOARD EXHAUST STACK WAS FOUND TO HAVE A CRACK 10 INCHES LONG PARALLEL WITH THE HORIZONTAL WELD ON THE FORWARD SIDE. THIS IS THE SECOND NEW EXHAUST STACK THAT HAS CRACKED AND ONLY AFTER 78.1 HRS OF OPERATION.SDR 96ZZZX6017Pipe · crackedPILOT HEARD NOISE DURING FLIGHT. AIRCRAFT LANDED WITHOUT INCIDENT. FOUND NR 1 CYLINDER EXHAUST PIPE CRACKED AROUND REINFORCEMENT.SDR HEEA968580Clamp · weld failedCLAMPS HAVE BROKEN SPOT WELDS AND ARE CRACKED. REMOVED PART AND INSTALLED SERVICEABLE PARTS.SDR HEEA968578Exhaust Clamp · corrodedT-BOLT HAVE CORROSION PITS, CHAFED T-BOLTS AND CRACKS. REPLACED WITH SERVICEABLE PART.SDR CA961128024Clamp Band · worn(CAN) LEFT HAND ZONE 1 FIRE WARNING ILLUMINATED. ENGINE SECURED AND FIRE BOTTLES DISCHARGED. AIRCRAFT LANDED SAFELY. MAINTENANCE CHECK FOUND LEFT HAND EXHAUST PIPE UNIVERSAL COUPLING HAD SEPARATED ALLOWING EXHAUST GASES TO ENTER ENGINE NACELLE. COUPLING FAILEDSDR HEEA968538Exhaust Stack · crackedEXHAUST DUCT CRACKED.SDR 96ZZZX6173Tailpipe · crackedLT FIRE LIGHT ILLUMINATED AT ALTITUDE. REPLACED CRACKED TAIL PIPE WITH SERVICEABLE UNIT.SDR 96ZZZX5906Muffler · chafedON ANNUAL INSPECTION THE MUFFLER TAILPIPE WAS FOUND CHAFING ON FRAME NR 1 (FIREWALL). THE HEAT EXPANDS THE TAILPIPE WHICH CAUSED IT TO HIT THE BOTTOM OF FRAME NR 1.SDR 96ZZZX5709Elbow · crackedDURING ROUTINE OIL CHANGE, NOTICED EXHAUST RESIDUE AROUND WASTEGATE ASSEMBLY. FOUND INLET ELBOW FROM CYLINDERS NR 1, NR 3, AND NR 5 CRACKED. THIS PART IS NOT PART OF AD REQUIRING COMPONENT CHANGE. SUBMITTER RECOMMENDS MAKING REPLACMENT PART OF THICKER MATERSDR P5CA9600866Sleeve · crackedSMALL CRACK NR 4 ENGINE EXHAUST SLEEVE AT 9 O'CLOCK POSITION. STOP DRILLED CRACK AND FABRICATED DOUBLER AND INSTALLED AS PER BOEING SRM 51-40-02 AND REPLACED LOOSE FASTENERS PER BOEING SRM 51-30-02.SDR HEEA968410Collector · crackedTURBINE REMOVED DUE TO OVERHAUL. UPON INSPECTION NOTED THE FOLLOWING: EXCESSIVE CRACKS BEYOND SERVICEABLE LIMITS ON EXHAUST COLLECTOR AS MARKED. REPLACED DISCREPANT PART.SDR 96ZZZX5893Exhaust Duct · crackedAN EXHAUST STAIN WAS OBSERVED ON ENGINE COWLING DURING A PRE-FLIGHT WALK-AROUND. CLOSER INSPECTION BY MAINT PERSONNEL DISCOVERED A LARGE CRACK IN THE UPPER SURFACE OF THE EXHAUST DUCT. PART WAS REMOVED FOR REPAIR AND REPLACED WITH A SERVICEABLE UNIT.SDR ZIAA961138Nozzle · crackedMCN - DURING SCHEDULED CHECK, VISUAL, REFLECTIVE PROBE EDDY CURRENT AND ULTRASONIC INSPECTION TECHNIQUES REVEALED NR 4 NOZZLE CRACKED, 6 O'CLOCK. REPAIRED IAW DWG A74-R11. (X)SDR ZIAA961137Nozzle · out of roundMCN - DURING SCHEDULED CHECK, VISUAL, REFLECTIVE PROBE EDDY CURRENT AND ULTRASONIC INSPECTION TECHNIQUES REVEALED NR 2 NOZZLE OUT OF ROUND, 10-12 O'CLOCK. REPAIRED IAW DWG A74-R01. (X)SDR SRAA961008Tailcone · damagedDURING LANDING NR 1 ENGINE TAILCONE DEPARTED FROM AIRCRAFT. AIRCRAFT LANDED WITHOUT INCIDENT. REPLACED NR 2 ENGINE REAR SCAVENGE PUMP CONE PER MM CH 72.SDR P5CA9600804Exhaust Sleeve · delaminatedDELAMINATED AND CURLED LEADING EDGE SKIN ON NR 4 ENGINE EXHAUST SLEEVE. REPAIRED PER BAC SRM 51-40-02.SDR P5CA9600784Exhaust Strut · crackedCRACK OF MORE THEN 50 PERCENT OF CHORD WIDTH TO NR 1 ENGINE 7 O'CLOCK EXHAUST STRUT. NO CORRECTIVE ACTION, TO BE INSPECTED EVERY 100 HOURS PER BAC MM 72-53-02.SDR HEEA968312Ejector Assy · crackedEJECTOR CRACKED ON INSIDE SKIN BEYOND REPAIR.SDR HEEA968302Ejector Assy · crackedEXCESSIVE CRACKING. SENT TO ALPINE AEROTECH LTD. FOR INSPECTION AND REPAIR.SDR HEEA968281Duct Assy · crackedDUCT ASSY CRACKED.SDR 96ZZZX5765Exhaust · crackedEXHAUST CRACKED AT FLANGE ALONG WELD.SDR HEEA968164Exhaust Duct · crackedEXHAUST DUCT CRACKED ON #1 ENGINE.SDR CA961007006Exhaust Segment · blown open(CAN) #3 ENGINE FIRE WARNING LIGHT ILLUMINATED SHORTLY AFTER LIFTOFF. #3 ENGINE SHUTDOWN AND AIRCRAFT RETURNED TO POINT OF DEPARTURE. POST FLIGHT INSPECTION FOUND THE EXHAUST RING SEGMENT FROM #1 CYLINDER HAD OPENED UP AT THE TOP AREA AND ACTIVATED FIRE WARNINSDR CA961016007Exhaust Stack · cracked(CAN) EXHAUST STACK FOUND CRACKED ALONG THE OUTBOARD WELD SEAM, APPROXIMATELY 5, 1/4" LONG. THIS STACK HAD BEEN REPLACED IN MAY 1995.SDR HEEA967805Ejector Duct · damagedDAMAGE DONE TO EJECTORS. FROM BUMPER PADS THAT ARE MOUNTED TO ENG. COWLING AND AIRFRAME. BUMPER PADS ARE RUBBING HARD ON EXHAUST STACK (EJECTOR) CAUSING WORN AREAS IN FOUR SPOTS. REMOVED DAMAGED AREAS, MANUFACTURER DOUBLERS USING TITANIUM MIL-T9046 TYPE 1 COSDR CA960916001Clamp · sheared(CAN) DURING FLIGHT, ZONE #1 FIRE WARNING ON #1 ENGINE ILLUMINATED, ENGINE SHUT DOWN AND AIRCRAFT LANDED WITHOUT INCIDENT. INVESTIGATION FOUND TAILPIPE CLAMP BROKEN.SDR 96ZZZX5036Stack · crackedTHE NR 2 EXHAUST PORT STACK CRACKED AT MOUNTING FLANGE. THIS PART WAS NEW FROM UNIVAIR. THE EXHAUST STACK ONLY HAD 200 HOURS SINCE NEW. SUBMITTER STATED UNIVAIR STATES THEY HAVE HAD CRACKING PROBLEMS BEFORE. THIS PART IS MANUFACUTRED BY A SUB-CONTRACTOR TOSDR 96ZZZX5342Exhaust Stack · elbow failedAFTER TAKEOFF AT 200 FEET AGL, THE ENGINE QUIT. INVESTIGATION REVEALED THE RT EXHAUST STACK ELBOW HAD PULLED LOOSE FROM STACK ASSY INSIDE ENGINE COWL. INTENSE HEAT FROM EXHAUST BURNED THROUGH ALUMINUM STRUCTURE AFT OF ENGINE AND MELTED MAGNETO WIRES AND OTHESDR 96ZZZX4799Exhaust Tube · flange failedAPPROXIMATELY ONE-HALF OF INTAKE PIPE TO CYLINDER FLANGE BROKE OFF. FOUND ON INSPECTION BY FUEL STAINS AT FLANGE. THIS IS THE 8TH NR 3 INTAKE TUBE ON THIS ENGINE. TT: 1,037.0 HOURS. TUBES WERE CHANGED AT THE FOLLOWING TIMES/HOURS: 30.0, 77.5, 156.0, 197.SDR 96ZZZX4733Exhaust System · crackedNEW EXHAUST SYSTEM WAS INSTALLED AT ENGINE CHANGE. 274 HOURS LATER DURING 100-HOUR INSPECTION, NUMEROUS CRACKS WERE FOUND ON RIGHT SIDE OF EXHAUST, BY TURBO INLET AND FRONT RISER.SDR CA960909022Exhaust Pipe · cracked(CAN) DURING INSPECTION THE LEFT ENGINE INBOARD EXHAUST PIPE WAS FOUND CRACKED AT THE RADIUS ATTACHMENT FLANGE. THE "V" BAND COUPLING HAD TO BE REMOVED TO SEE THE CRACK. THE CRACK WAS APPROXIMATELY 1.5 INCHES LONG.SDR 96ZZZM1381Flex Tube · splitFLT 453 - JAX-TPA - RIGHT ENGINE FIRE WARNING ILLUMINATED IN FLIGHT. REMOVED AND REPLACED EXHAUST FLEX.SDR CA960826077Spring · missing(CAN) THE EXHAUST SPRING WAS MISSING. SUSPECT THE SPRING WAS NOT INSTALLED AT THE FACTORY.SDR AU961149Exhaust Pipe · wrong part(AUS) RH EXHAUST COLLECTOR NO5 RISER PIPE RUBBING ON NO3 INLET MANIFOLD CAUSING WEAR DAMAGE TO BOTH ITEMS - COLLECTOR ASSEMBLY WAS NOT A GENUINE CESSNA PART AND APPEARS TO HAVE BEEN INCORRECTLY MANUFACTURED - A GENUINE CESSNA PART FITTED CORRECTLY -PERSONNEL/MSDR AWXA960376Exhaust Nozzle · damagedLAS - FLT 2993 - ON POST FLIGHT REPORT, DISCOVERED ENGINE NR 1 TAIL CONE FAIRING MISSING (UPPER PART) INSIDE WITH DAMAGE TO THE EXHAUST CONE AND HOLES INSIDE WALLS LEFT SIDE. REPLACED EXHAUST COMMON NOZZLE ASSY PER AMM 78-11-11, PAGE 401-415. (M)SDR 96ZZZX4389Exhaust · brokenEXHAUST FROM NR 1 CYLINDER AND NR 3 CYLINDER BROKE OFF AT FLANGE CAUSING HIGH HEAT INSIDE COWL CAUSING IGNITION TO HEAT UP, OIL TEMPERATURE TO BE EXCESSIVELY HIGH, PLUS LOOSE EXHAUST ASSY JAMMED AILERON CONTROLS. ERRATIC EGT ALSO NOTED.SDR 96ZZZX5302Tailpipe · baffle detachedWHILE TROUBLESHOOTING INTERMITTENT LOSS OF POWER, FOUND BAFFLE INSIDE OF TAILPIPE HAD BROKEN LOOSE AND WEDGED NEAR OUTLET OF TAILPIPE. THIS CAUSED AN INCREASE I N BACK PRESSURE WHICH CAUSED THE ENGINE TO NOT DEVELOP RATED POWER. SUBMITTER SUSPECTS CAUSE, HIGSDR 96ZZZX4424Bolt · failedONE EACH EXHAUST MOUNT BOLT CAME OUT CAUSING EXHAUST TO SLIP OUT OF CLAMP LEAKING HOT EXHAUST GAS ONTO COWL FLAP HYDRAULIC LINE. THE LINE FAILED IGNITING HYDRAULIC FLUID, THE FIRE WARNING SYSTEM OPERATED AS IT WAS SUPPOSED TO. THE COWL FLAP SELECTOR WAS SELESDR 96ZZZX4013Gasket · mismanufacturedNEW EXHAUST GASKET IS MISMANUFACTURED .032 INCH LARGER THAN ORIGINAL. IT WILL FIT OK ON CYLINDERS 1 AND 4, BUT DUE TO CLEARANCE REQUIRED FOR FIT, IT IS TOO LARGE FOR CYLINDERS 2 AND 3.SDR CA961112040Diffuser · cracked(CAN) EXHAUST DIFFUSER RECEIVED FOR INSPECTION, 4" X 1" METAL BREAK-OFF AND 2" CIRCUMFERENTIAL CRACK FOUND ON FORWARD FACE OF THE INNER CONE. CAUSE OF CRACK AND BREAK IS UNKNOWN.SDR 96ZZZX4067Wye Pipe · crackedCRACKED IN FRONT OF ASSY NEAR CENTER SUPPORT BOSS. SUBMITTER STATES VERY HARD TO SEE DUE TO LOCATION AND BLACK COATING OF PART. SUGGEST DIFFERENT COLOR AND REDESIGNED PART MADE OUT OF THICKER MATERIAL.SDR P5CA9600401Exhaust Case · crackedDURING B-CHECK, FOUND NR 3 ENGINE R-RAIL HAS 2 CRACKS AT THE 6:00 AND 7:OO O'CLOCK POSITIONS. WELDED, STRESS RELIEVED, AND SHOT PEENED PER MAINTENANCE MANUAL 72-53-01 AND SRM 51-10-07.SDR P5CA9600400Exhaust Case · crackedDURING B-CHECK, FOUND NR 2 ENGINE R-RAIL HAS 2 CRACKS AT THE 5:30 AND 7:00 O'CLOCK POSITIONS. WELDED, STRESS RELIEVED, AND SHOT PEENED PER MAINTENANCE MANUAL 72-53-01, AND SRM 51-10-07.SDR 96ZZZX3873Stack · separatedEXIT STACK OF MUFFLER SEPARATED FROM THE MUFFLER. APPEARS WELDS MAY NOT HAVE BEEN 'NORMALIZED' CAUSING A BRITTLE AREA AROUND THE WELD. THIS WAS AN FAA/PMA PART. ENGINE SHOWED NO SIGNS OF VIBRATION. EXHAUST EXITED THE MUFFLER INTO COWLING, GASCOLATOR, AND C
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