JASC 7810
Service difficulty reports · 1,900
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 2015FA0000560Exhaust Riser · blew outPILOT REPORTED LOSS OF MANIFOLD PRESSURE AND SLOW LOSS OF AIRSPEED. MADE A PRECAUTIONARY LANDING. INVESTIGATION REVEALED THAT THE EXHAUST MANIFOLD HAD BREACHED JUST BELOW THE NR 4 CYLINDER ALLOWING EXHAUST TO MELT THROUGH THE LT TURBO AIR INLET FILTER BOX ANDSDR A6WA201543203Stiffener · crackedLEFT JET PIPE FAIRING, CRACKED AT FWD INNER SUPPORT RING. REPAIRED LT EXHAUST NOZZLE FAIRING FWD STIFFENER IAW CMM 78-11-00-300-810-A01 REPAIR SRS 042.SDR 7C7A20151028092Duct · gougedGOUGE DAMAGE IN CTR SHROUD ASSEMBLY EXHAUST SYS.SDR 2015FA0000517Exhaust Stack · separatedEXHAUST STACK SEPARATED AT THE WELD OF THE ENGINE EXHAUST MANIFOLD MOUNT, NR 1 CYLINDER.SDR IPXA2015092994077Sleeve · damagedINSPECTION TYPE:C, DURING MAJOR MAINTENANCE VISIT 6764, FOUND DAMAGE - NR 1 EXHAUST SLEEVE OUTER SKIN DAMAGE 6 TO 7 O'CLOCK POSITION NAC BS 321TO 339REF EGAT NRC DGU05028 EVALUATED DAMAGE IAW SRM 54-42-30-1A-1, REV 63.00 INFORMATION SUBMITTED FOR ADM DAMAGE WSDR 2015FA0000470Exhaust Pipe · detachedOVERBOARD EXHAUST ELBOW, BETWEEN THE WASTEGATE AND THE TAILPIPE DISENGAGED BY THE SLIP-JOINT FROM WASTEGATE FLANGE, PN 1250992-4. NO CLAMP FAILURE WAS EVIDENT.SDR A6WA201543069Stiffener · crackedRIGHT EXHAUST NOZZLE FAIRING 446 AL HAS A CRACKED STIFFENER NEXT TO THE UPPER INBD MOUNT ASSEMBLY.SDR BQ8S2015FA0000423Exhaust Duct · failedTHE EXHAUST SYSTEM WAS INSPECTED IAW FAA AD 2015-02-09, AND REV ON 7/28/05 AT 200.59 ENGINE HOURS. THE INSPECTION WAS CARRIED OUT USING HIGH POWERED LIGHTING AND 10 POWER MAGNIGFICATION. NO VISUAL DEFECTS WERE DETECTED DURING THIS INSPECTION. ON 8/8/15 AT ASDR 2015FA0000376Exhaust Pipe · damagedTHE EXHAUST TUBE FROM THE TURBO CHARGER TO THE MUFFLER FAILED AT THE WELD WITH A SUBSEQUENT FIRE.SDR CA150911008Clamp · failed(CAN) IN FLIGHT, THE NUMBER 1 ENGINE ZONE 1 FIRE WARNING LIGHT ILLUMINATED. THE FLIGHT CREW OPTED TO REDUCE THE POWER LEVER SETTING ON THE NR 1 ENGINE AND THE FIRE WARNING LIGHT EXTINGUISHED. THE FLIGHT CREW CONTINUED ON TO ITS FINAL DESTINATION. THE MAINTENANSDR FQAR20150731084Exhaust Riser · fracturedDURING A PREFLIGHT RUN, WHEN THE RT ENG CARB HEAT WAS SELECTED ON, THE ENG RPM DROPPED OVER 600 RPM & THE ENG RAN ROUGH. INSPECTION REVEALED THE NR 4 CYLINDER EXHAUST RISER HAD FRACTURED ABOUT THE FLANGE & HAD FALLEN OPEN, ALLOWING EXHAUST GASSES TO BE EMITTESDR REXA2015071200684Tab · brokenTASK CARD 900-78-430-100R RT ENG EXHAUST NOZZLE CHAFE PAD ALIGNMENT TAB BROKEN. R & R RT ENG EXHAUST NOZZLE ALIGNMENT TAB IAW SRM 54-13-00.SDR REXA2015071200683Nozzle · chafedTASK CARD 900-78-430-100R RT ENG EXHAUST NOZZLE CHAFED AT PYLON SEAL MATING SURFACE. REPAIRED RT ENG EXHAUST NOZZLE IAW SRM 54-13-00.SDR 2015FA0000354Manifold · crackedTHE ACFT WAS INVOLVED IN AN INFLIGHT EMERGENCY AND WAS VECTORED TO LAND WITH NO FURTHER INCIDENT. SHORTLY AFTER THE PILOT DECLARED THE EMERGENCY FOR AN ELECTRICAL SYSTEM FAILURE, SMOKE ENTERED THE COCKPIT. THE SMOKE MOST LIKELY ENTERED THROUGH THE FLOOR VENTSDR CA150612003Exhaust Duct · damaged(CAN) ENGINE WAS SENT FOR OVERHAUL FOR INVESTIGATION & REPAIR AFTER THE OPERATOR REPORTED LIBERATED MATERIAL IN THE INNER CONE SECTION OF THE EXHAUST DUCT. SEE ATTACHED EIR REPORT PT6A 2015-043.SDR 2015FA0000264Exhaust Stack · crackedDURING AN OIL CHANGE THE TECH WAS DOING A VISUAL INSPECTION OF THE ENGINE AND NOTICED SOME EXHAUST SOOT/STAINING ON THE HEAT SHIELD FOR THE J BOX. DISCOVERED THE SOURCE TO BE THE CRACKED EXHAUST ELBOW.SDR ASAA2015051111697Flange · crackedLT ENGINE TURBINE EXHAUST FLANGE ASSY HAS CRACKS AT BOLT LOCATIONS. ACFT GROUNDED. REMOVED NR 1 ENGINE TURBINE EXHAUST FLANGE IAW 72-56-00-000-802. INSTALLED TURBINE EXHAUST FLANGE IAW 72-56-00-400-801, STEP F. 2, A-G + 3 A- C, INSTALLED PRIMARY PLUG IAW 78-SDR CA150513002Clamp · failed(CAN) IN FLIGHT THE ACFT NR 2 ENG ZONE 1 FIRE WARNING LIGHT ILLUMINATED. THE FLIGHT CREW ACCOMPLISHED THE ENG FIRE DRILL & CHECKLIST PROCEDURES WHICH RESULTED IN A SHUTDOWN OF THE ENG. UPON SHUTDOWN, THE FIRE WARNING LIGHT EXTINGUISHED. THE FLIGHT CREW RETUSDR A6WA201542706Stiffener · crackedTHE 2ND STIFFENER FROM LE IS CRACKED ON RT ENG EXHAUST NOZZLE FAIRING AT APPROX. 9 O'CLOCK POSITION.SDR ZESA20150504001Exhaust Mixer · crackedDURING A PREFLIGHT, THE EXHAUST NOZZLE, MIXER, WAS NOTICED TO HAVE CRACKS THROUGHOUT. THE ACFT WAS GNDED & PUT INTO MX. THROUGH FURTHER INSPECTION WE HAD TO PERFORM A BORESCOPE INSPECTION & A VIBRATION SURVEY TO THE ENG & IT WAS OUT OF LIMITS. THE BORESCOPESDR A6WA201542687Stiffener · crackedRIGHT ENG EXHAUST NOZZLE FAIRING SECOND STIFFENER FROM LE IS CRACKED.SDR A6WA201542686Heat Shield · crackedRIGHT ENG EXHAUST FAIRING INNER HEAT SHIELD HAS TWO EACH CRACKS NEAR DOUBLER.SDR CA150428010Exhaust Stack · loose(CAN) RETENTION CABLE FOUND BROKEN ON EXHAUST STACK. FLIGHT WITH BROKEN RETENTION CABLE NOT PERMITTED IAW EASA AD 2012-0022. INVESTIGATION FOUND STACK NOT MFG TO MFG SPECIFICATIONS PLACING STRAP UNDER TENSION. STRAP RETAINING RIVETS SHOULD HAVE A SPACING OSDR A6WA201542654Stiffener · crackedRT ENG EXHAUST FAIRING 2ND STIFFENER CRACKED.SDR CA150417011Clamp · loose(CAN) SHORTLY AFTER TAKEOFF, DURING CLIMB, ALL THE FIRE DETECT WARNINGS, BOTH VISUAL AND AURAL CAME ON IN THE COCKPIT. THE PILOTS IMMEDIATELY LEVELLED OFF AT AROUND 8000 FT AND FOLLOWED THE RELEVANT EMERGENCY PROCEDURE IAW THE MANUAL. POWER LEVER WAS PULLED SDR CA150408029Duct · cracked(CAN) DURING A NON-SCHEDULED HOT SECTION INSPECTION, THE LARGE EXIT DUCT WAS FOUND CRACKED IN MULTIPLE LOCATIONS ALONG THE OUTER SEAM WELD. THE CRACKS TOTALED APPROXIMATELY HALF OF THE CIRCUMFERENCE OF THE LED. THE TSO OF THE LED IS 1887.5 HOURS. THIS OPERATOSDR CA150406004Shroud · chafed(CAN) DURING HEAVY MAINTENANCE INSPECTION, HOLES WERE FOUND IN THE LT AFT EXHAUST SHROUDS. THIS APPEARS TO BE ATTRIBUTED TO BROKEN LOCKWIRE FROM THE ADJACENT HEAT BLANKET. 3RD OCCURANCE, PN 8784010-005, PN 8784010-007.SDR A6WA201542568Stiffener · crackedLT TAIL PIPE FAIRING HAS CRACK IN STIFFENER NEAR THE POSITION.SDR 39LA20150326124Mount · chafedNUMBER 1 ENG EXHAUST DUCT AFT INBD MOUNT FOUND CHAFED ABOVE & BELOW BASE OF MOUNT STUD. REPLACED WITH SERVICEABLE UNIT IAW MM.SDR CA150323006Support Bracket · broken(CAN) EXHAUST STACK SUPPORT BRACKET FOUND BROKEN ON RT SIDE ENGINE.SDR 2015FA0000208Exhaust Stack · damagedINSTALLED MANIFOLD WAS USED AT THIS ANNUAL INSPECTION TO FIND NR 4 CYLINDER EXHAUST STACK AFT END AT SLIP JOINT BULGED AND CRACKED. STAINS IN THAT AREA WERE NOTED, HEATSHIELD DEFLECTED LEAT FROM ANY FURTHER DAMAGE. PART NOT SOLD SEPARATELY, NEW REDESIGN LEFTSDR JIKA2015031701Exhaust Stack · leakingDURING CRUISE FLIGHT, PILOT NOTICED THE RT FIRE PULL, HANDLE ILLUMINATED, THE PILOT FOLLOWED THE CHECKLIST PROCEDURES IN THE FLIGHT MANUAL & PERFORMED AN INFLIGHT SHUT DOWN OF THE RT ENG. THE PILOT DECLARED AN EMER, RETURNED & LANDED WITHOUT INCIDENT. INSPECSDR A6WA201542506Support · crackedLEFT TAIL PIPE FAIRING NR 3 SUPPORT HAS CRACK NEAR 8 POSITION.SDR HX1R2015033100001Exhaust Pipe · damagedDURING ANNUAL INSPECTION, CYLINDER NR 6 EXHAUST TRANSITION PIPE APPEARED TO BE STARTING TO BLISTER ON OUTSIDE, PHOTOS NR 3 & NR 4. TRANSITION PIPE WAS REMOVED TO INSPECT THE INSIDE OF THE PIPE, PHOTOS NR 1 & NR 2, DIRECTLY OPPOSITE OF THE BLISTERING ON THE OSDR 3BOR2015012715001Duct · crackedDURING THE 12 MONTH/300 HOUR ENGINE INSPECTION ON THE LT AND RT ENGINES ON THE ACFT, A VISUAL INSPECTION OF THE LT ENGINE EXHAUST AREA NOTED A PIECE OF THE ENGINE OUTER BYPASS DUCT MISSING. APPROXIMATELY 6" SECTION MISSING, BETWEEN 10 O'CLOCK AND 1 O'CLOCK ASSDR CA150123003Exhaust Duct · cracked(CAN) WHILE PERFORMING NR 1 PHASE INSPECTION, FOUND NR 1 ENGINE AFT TURBINE EXHAUST HOUSING HAS A CRACK AT 1:00 POSITION ALONG SIDE A WELDED REPAIRED AREA.SDR KY7A20150116001Exhaust Duct · crackedAPPROXIMATELY 12 MINUTES AFTER TAKEOFF, THE RT ENG FIRE WARNING & WING OVERHEAT LIGHTS ILLUMINATED. PILOT PERFORMED EMER STOP FEATHER & FIRED THE FIRE EXTINGUISHER; THE WARNINGS EXTINGUISHED IMMEDIATELY. RETURNED & LANDED WITHOUT INCIDENT. POST LANDING INSSDR A6WA201542302Skin · crackedRIGHT EXHAUST FAIRING SKIN CRACKED AT DRAIN FITTING.SDR 2014FA0000714Riser · crackedEXHAUST RISER FROM NR 2 CYLINDER WHERE IT "Y'S" INTO THE CROSSOVER TUBE FROM THE NR 1 CYLINDER CRACKED.SDR SWIA201440443Tab · wornRT ENGINE EXHAUST NOZZLE, INBD. ALIGNMENT TAB WORN. REPAIRED DAMAGE IAW EA.SDR QXEA2014121001022Channel · crackedRIGHT NACELLE EXHAUST CHANNEL CRACKED. REMOVED AND REPLACED THE CHANNEL IAW SRM 51-42-05, SRM 51-42-05, SRM 51-40-15 AND DWG 85414389, REV B.SDR QXEA2014120601004Exhaust Duct · damagedNR 1 ENGINE, FINGERNAIL EXHAUST HAS SEVERAL SUPPORT CLIPS BROKEN. NOTICED BY PASSENGER, VIBRATING DURING CRUISE. REMOVED NR 1 EXHAUST EJECTOR IAW AMM TASK 78-10--26-00-801. INSTALLED NEW SERVICABLE NR 1 AFT EXHAUST OUTLET IAW AMM TASK 78-10-26-400-801. RETSDR CA141205003Exhaust Duct · cracked(CAN) RIGHT HAND EXHAUST COLLECTOR CRACKED AT THE FLANGE FOR THE NR 1 CYLINDER. MUFFLER ALSO HAD SMALL CRACK ON NEAR/THE TOP SIDE OF THE EXIT DUCT.SDR QXEA2014121001020Bracket · crackedAFT LT EXHAUST OUTLET LOWER BRACKET FOUND CRACKED. REMOVED AND REPLACED THE BRACKET IAW SRM 51-42-05, PROCEDURE 4E STEPS 1-3 AND SRM 51-40-15, PARA 6M(1-5) AND DWG 85414389, REV -B.SDR QXEA2014120901008Plate · chafedRIGHT OTBD EXHAUST AFT MOUNT COVER PLATE HAS CHAFE ON MIDDLE OF PLATE. INSTALLATION ACCOMPLISHED ON JOB 5408316, OP 4.SDR QXEA2014112600925Outlet · crackedF/A REPORTED THAT A PIECE OF METAL IS VIBRATING ON TOP OF THE NR 1 ENGINE EXHAUST. FOUND TO BE NR 1 ENGINE EXHAUST OUTLET. REPLACED NR 1 ENGINE EXHAUST OUTLET IAW AMM 78-10-26-00-400-801. ALSO, REPAIRED FOULING CONDITION BETWEEN AFT UPPER COWLING AND THE AFTSDR GQRR2014FA0000673Exhaust Stack · crackedENGINE DEICE HOT AIR OUTLET CRACKED.SDR QXEA2014120100945Seal · deformedRIGHT FWD EXHAUST, FWD SHROUD SEAL DEFORMED AND PINCHED. REMOVED JET PIPE FROM THE FWD EXHAUST ASSEMBLY, REF AMM TASK 78-10-06-000-802. INSTALLED THE JET PIPE TO THE FWD EXHAUST ASSY, REF AMM TASK 78-10-06-400-802. REMOVED SEAL FROM THE FWD EXHAUST ASSY REF SDR GQRR2014FA0000706Heat Shield · chafedHEAT SHIELD CHAFED THROUGH.SDR 2014FA0000713Exhaust Duct · misalignedDURING MAINTENANCE IT WAS NECCESARY TO REMOVE THE EXHAUST SYSTEM. WHEN EXHAUST RISER WAS REMOVED FROM MUFFLER IT WAS NOTED THAT HOLES FOR ALINGMENT PIN/CLAMP WERE NOT IN ALINGMENT WITH EACH OTHER. THIS CONDITION RESULTED IN THE EXHAUST SYSTEM BEING INSTALLED
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