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 CA020503003Coupling · cracked(CAN) DURING TOUBLESHOOTING OF HIGHER THAN NORMAL E.G.T. INDICATION, (CAUSED BY MAGNETO), THE RT EXHAUST PIPE COUPLING AT THE TRANSITION WAS FOUND LOOSE. COUPLING P/N MVT69183-200 WAS REMOVED FOR DETAILED INSPECTION, A CRACK APPROXIMATELY 1.5 INCHES LONG WAS DSDR ERAA078447Collector Ring · groovedEXHAUST COLLECTOR RETURNED FROM OVERHAUL AND ISSUED TO AIRCRAFT BUT COULD NOT BE INSTALLED DUE TO GROOVED .100 IN MOUNT AREA.SDR HEEA078345Duct · crackedEXHAUST DUCT CRACKED.SDR CA020408009Strut · broken(CAN) DURING A 100 HOUR INSPECTION THE EXHAUST STAY STRUT WAS FOUND BROKEN AT THE THREADED PART OF THE EYE END. A NEW STRUT AND EYE END ASSEMBLY WAS INSTALLED AND POSITIONED FOR PROPER FIT. THIS EYE END IS SECURED BY THE UPPER RIGHT HAND NUT THAT ALSO SECURES SDR 2003FA0000219Exhaust Pipe · crackedASSEMBLIES ARE CRACKING WITH LESS THAN 100 HOURS IN SERVICE SINCE NEW. THE CRACKS ARE UNDER THE CABIN HEAT SHROUD AND CAN NOT BE SEEN UNLESS THE SHROUD IS REMOVED. NUMEROUS CRACKS HAVE ALSO BEEN FOUND IN OTHER AREAS OF THESE ASSEMBLIES. IT IS SUGGESTED THATSDR AUS20020236Duct · cracked(AUS) EXHAUST DUCT CONTAINED HAIRLINE CRACKS.SDR AUS20020193Slip Joint · unapproved part(AUS) RT ENGINE EXHAUST SYSTEM SLIP JOINT HARDWARE UNAPPROVED PARTS AND NOT INSTALLED IAW RELEVANT DATA. PERSONNEL/MAINTENANCE ERROR. UNAPPROVED PART.SDR AUS20020192Slip Joint · unapproved part(AUS) LT ENGINE EXHAUST SYSTEM SLIP JOINT HARDWARE UNAPPROVED PARTS AND NOT INSTALLED IAW RELEVANT DATA.SDR 200200182Nozzle · crackedNR 4 ENGINE EXHAUST NOZZLE AT THE 2:00 POSITION, 4 INCHES FROM THE TRAILING EDGE HAS A 10 INCH CRACK IN THE OUTER SKIN. FABRICATED AND INSTALLED REPAIR DOUBLER PER 747 SRM 54-30-03.SDR QXEA0200456Clamp · misalignedGEG - DURING TAXI NR 2 ENGINE FIRE WARNING SYSTEM ACTIVATED. STOPPED THE AIRCRAFT, PERFORMED FIRE ON THE GROUND PROCEDURE. FIRE INDICATION CEASED AFTER ACTIVATING THE FORWARD EXTINGUISHER BOTTLE. MAINTENANCE INSPECTED AND FOUND THE TAILPIPE CLAMP ON THE ENGSDR HEEA078213Duct · crackedEXHAUST DUCT IS CRACKED.SDR P5CA0200662Tailpipe · crackedFOUND NR 1 ENGINE TAIL PIPE INNER SLEEVE, CRACK APPROX 1 INCH LONG AT 6 O'CLOCK POSITION AND APPROX 18 INCHES FROM FWD CONE L/E. CRACK IS 6.5 INCH LONG FOUND ON OUTER SKIN OF EXHAUST CONE INNER BARREL.SDR MALA020176Nozzle · defectiveRT INTAKE HEAT FAILED DURING FLIGHT. DIVERTED TO DTW. REMOVED AND REPLACED RT EXHAUST NOZZLE.SDR HEEA078080Exhaust Stack · crackedENGINE EXHAUST STACK IS CRACKED.SDR CA020226001Cover · cracked(CAN) DURING THE DAILY INSPECTOIN, DAMAGE TO THE M/R BLADE WAS NOTICED. INSPECTION OF THE AIRCRAFT REVEALED THAT THE COVER, EXHAUST DIFFUSER, HELD BY A SPEC. BOLT AND TABWASHER ON THE COVER, TURB., REAR WAS MISSING. THE BOLT & TABWASHER WHERE STILL IN PLACSDR MALA020149Nozzle · defectiveDURING CLIMBOUT OF FLIGHT 3102, LT INTAKE CYCLES, COMPLETED QRH. AIR RETURN TO DTW. MAINTENANCE FOUND CHAFED WIRE ON EXHAUST NOZZLE, INSTALLED SERVICEABLE EXHAUST NOZZLE P/N NC24668-274, S/N ON L290958, S/N OFF L291489. ALL CHECKS GOOD IAW 71-60-10. ALSO RSDR HP62002F00000Valve · brokenFLAPPER ASSEMBLY, HAS BROKEN AWAY FROM HINGE SHAFT AND WAS EJECTED OUT EXHAUST STACK. CAUSE IS THOUGHT TO BE VIBRATION (METAL FATIGUE).SDR 02FDEA00074Tailpipe · fireAFTER BLOCK IN & ENGINE SHUTDOWN, NR 2 ENGINE TAILPIPE ON FIRE. R&R APU NR 1 FIRE BOTTLE PER MM 26-21-01-4.SDR AUS20020125Exhaust Pipe · leaking(AUS) RH ENGINE FIRE. ENGINE COMPARTMENT DAMAGED. FIRE WAS EXTINGUISHED USING CABIN FIRE EXTINGUISHER. INVESTIGATION FOUND THE FIRE WAS CAUSED BY MISALIGNMENT OF THE EXHAUST SWIVEL JOINT WHICH ALLOWEDEXHAUST GAS TO LEAK INTO THE ENGINE BAY. A LIST OF DAMAGE ISSDR 2003FA0000322Slip Joint · wornTHERE IS AN EXHAUST ELBOW THAT COMES OFF THE WASTEGATE AND RETURNS TO THE TAILPIPE. THIS PIPE HAD WORN NEARLY THROUGH AT THE SLIP JOINT BETWEEN IT AND THE TAIL PIPE. THE TAIL PIPE WAS WORN TO A SHARP EDGE WHERE THE ELBOW ENTERS THE SLIP JOINT. THIS CONDITIOSDR 2002F00290Ejector · crackedEJECTOR ASSEMBLY CRACKED BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT CORRECTED PROBLEM. (M)SDR CA020130004Exhaust Stack · cracked(CAN) CRACKED EXHAUST STACK FROM CYLINDER NR 3 MELTED THE CARB HEAT CABLE INTERIOR LINING CAUSING THE CABLE TO BE VERY STIFF. CABLE. CRACK LOCATED INSIDE THE CARB HEAT SHROUD AT THE MOST FORWARD POINT WHICH IS VERY DIFFICULT TO INSPECT. RECOMMEND REMOVE SHROUSDR 2002FA0000174Exhaust Pipe · crackedPILOT OBSERVED RT FUEL QUANTITY INDICATOR FAILED, THEN RT FUEL TRANSFER LIGHT ON AND RT LANDING LIGHT CIRCUIT BREAKER POPPED. AFTER FLIGHT, VISUAL INSPECTION OF THE RT ENGINE NACELLE IDENTIFIED A BURN THROUGH NACELLE SKIN ADJACENT TO THE RT ENGINE OVERBOARD TSDR P5CA0200625Nozzle · cracked#3 ENGINE EXHAUST NOZZLE OUTER SKIN IS CRACKED ON THE RIGHT SIDE TOP. REMOVED & REPLACED EXHAUST NOZZLE AS PER 78-11-01.SDR J8S2002F00000Crossover Tube · splitCROSSOVER PIPE BETWEEN LEFT AND RIGHT TURBOCHARGERS WAS SPLIT UNDER HEAT SHIELD. ALLOWING HOT EXHAUST TO BLOW ON FORWARD SIDE OF FIREWALL. THE FIREWALL WAS NOT DAMAGED, BUT THE HEAT MELTED THE VINYL TRIM ON THE FORWARD SIDE OF THE NOSE BAGGAGE COMPARTMENT. SDR AUS20011319Exhaust Pipe · cracked(AUS) ENGINE PRIMARY EXHAUST DUCT CRACKED AND HOLED. HOLE WAS APPROXIMATELY228.6MM (9IN) BY 146MM (5.75IN). ESCAPING EXHAUSTGAS DAMAGED OIL COOLER SHROUD RUBBERS AND DISCOLOURED THE PAINT ON THE LOWER RH COWL.SDR 2001F00758Clamp · crackedNEW AEROQUIP EXHAUST CLAMPS ARE CRACKING AROUND OUTER PERIPHERY. APPEAR TO BE MANUFACTURING DEFECTS.SDR 2001F00764Clamp · crackedNEW AEROQUIP EXHAUST CLAMPS ARE CRACKING AROUND OUTER PERIPHERY. APPEAR TO BE MANUFACTURING DEFECTS.SDR AUS20011384Exhaust Stack · cracked(AUS) ENGINE EXHAUST DUCT CRACKED AT AFT FLANGE ATTACHMENT WELD.SDR AC2A077536Exhaust Stack · crackedEXHAUST STACK CRACKED. REPLACED WITH NEW.SDR AC22002F00001Exhaust Header · crackedEXHAUST ASSEMBLY CRACKED. REPLACED WITH NEW EXHAUST DUCT.SDR 2002F00334Thrust Reverser · damagedDURING C-CHECK, THE NR 2 ENGINE THRUST REVERSER LEFT COWL SKIN WAS FOUND DAMAGED ON LEADING EDGE. A DOUBLER WAS INSTALLED IAW REO-G08284. THE AIRCRAFT WAS RETURNED TO REVENUE SERVICE. (M)SDR ARWA20011111Nozzle · crackedDURING C-CHECK INSPECTION, FOUND THE FOLLOWING: NR 4 ENGINE EXHAUST NOZZLE SPLITTER WITH CRACK AT 2 O'CLOCK. REMOVED SPLITTER; FABRICATED NEW SPLITTER IAW DC8 SRM 78-3-2, FIG 8, ITEM C. PRIMED AND INSTALLED IAW DC8 SRM 51-1-8 & 51-1-21.SDR 2001F00713Nozzle · crackedDURING A-CHECK, THE NR 1 ENGINE COMMON NOZZLE ASSY WAS FOUND CRACKED AT BOTH THE INBOARD AND OUTBOARD HOIST ATTACH POINTS. MAINTENANCE REMOVED AND REPLACED THE NOZZLE ASSY. (M)SDR 2001F00712Nozzle · crackedDURING ROUTINE MAINTENANCE AT MDW, THE NR 1 ENGINE COMMON NOZZLE ASSY WAS FOUND TO BE CRACKED AT BOTH INBOARD AND OUTBOARD HOIST ATTACH POINTS. MAINTENANCE REMOVED AND REPLACED THE NOZZLE ASSY. (M)SDR 2001F00711Nozzle · crackedDURING A-CHECK, THE NR 2 ENGINE COMMON NOZZLE ASSY WAS FOUND CRACKED AT THE INBOARD HOIST ATTACH POINT. MAINTENANCE REPAIRED THE ASSY IAW AMTA ERA-757-78R-4616 AND ROLLS-ROYCE TECHNICAL VARIANCE DOCUMENT F37183. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)SDR BUE2001F00000Exhaust Stack · brokenDURING SCHEDULED INSPECTION FOUND LEFT ENGINE EXHAUST STACK INLET HEAT AIR TUBE BROKEN AWAY FROM EXHAUST STACK.(K)SDR 2001F00763Clamp · crackedNEW AEROQUIP EXHAUST CLAMPS ARE CRACKING AROUND OUTER PERIPHERY. APPEAR TO BE MANUFACTURING DEFECTS.SDR 2002F00266Exhaust Pipe · crackedDISCOLORATION OF PAIN ON COWLING, NR 2 ENGINE. FOUND HOLE, APPROX 1 INCH SQUARE, IN TAIL PIPE EXTENSION. HEAT SHIELD OUTER SKIN. (M)SDR CA011105001Flange · cracked(CAN) THE EXHAUST FLANGE WAS FOUND CRACKED AT THE FORWARD RADIUS IN 3 SPOTS. THERE IS A HOLE IN THE FLANGE THAT LINES UP WITH THE THREADS OF A BOLT FROM THE OIL COOLER. THIS HOLE DID NOT LINE UP WITH THE BOLT AND PRODUCED STRESS ON THE FLANGE RESULTING IN THE SDR AC2A077058Exhaust Stack · crackedEXHAUST STACK CRACKED. REPLACED WITH SERVICEABLE.SDR AC2A077057Exhaust Stack · crackedEXHAUST STACK CRACKED. REPLACED WITH NEW .SDR 2002FA0000067Exhaust Stack · crackedENGINE EXHAUST IS CRACKED. INSTALLED SERVICEABLE EXHAUST STACK. (M)SDR HEEA076859Exhaust Stack · crackedEXHAUST STACK CRACKED.SDR AC22001F00006Exhaust Stack · crackedEXHAUST ASSEMBLY, CRACKED. REPLACED WITH NEW EXHAUST STACK.SDR 2001F00448Clamp · crackedNEW AEROQUIP EXHAUST CLAMPS ARE CRACKING AROUND OUTER PERIPHERY. TWO CLAMPS IN LAST 200 HOURS. BOTH APPEAR TO BE MANUFACTURING DEFECTS. NON LIFE LIMITED CLAMPS.SDR 2001F00436Clamp · crackedNEW AEROQUIP EXHAUST CLAMPS ARE CRACKING AROUND OUTER PERIPHERY. FOUR CLAMPS IN 201 HOURS. ALL CLAMPS APPEAR TO BE MANUFACTURING DEFECTS. NON LIFE LIMITED CLAMPS.SDR 2001F00757Clamp · crackedNEW AEROQUIP EXHAUST CLAMPS ARE CRACKING AROUND OUTER PERIPHERY. APPEAR TO BE MANUFACTURING DEFECTS.SDR COMA0160781Bolt · missingDURING REMOVAL OF EXHAUST FAIRING ONE EXHAUST NOZZLE BOLT WAS FOUND MISSING.INSTALLED NEW HARDWARD.SDR COMA0160780Bolt · missingDURING REMOVAL OF EXHAUST FAIRING THREE EXHAUST NOZZLE BOLTS WERE FOUND MISSING.INSTALLED NEW HARDWARE.
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