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 JIK2008F00005Exhaust Duct · crackedAFTER DEPARTURE, AT ABOUT 1000 FEET AGL, THE PILOT REPORTED THAT THE LT ENGINE MANIFOLD PRESSURE DROPPED SUDDENLY, THE ENGINE SURGED AND THEN QUIT RUNNING. THE PILOT RETURNED TO DEPARTURE SAFELY. UPON EXAMINATION, IT WAS FOUND THAT THE EXHAUST FLANGE AT THE WSDR 2008FA0000655Muffler · crackedMUFFLER WAS HEAT BLISTERED AND CRACKED AT TAIL PIPE TRANSITION. COLLECTOR WAS BURNED THRU UNDER CLAMP AT NR 1 CYLINDER, ALSO HEAT BLISTERED. (K)SDR 2008FA0000657Cowling · crackedTHE SECONDARY EXHAUST COWLING WAS FOUND TO HAVE A 5.5 INCH LONG CRACK NEXT TO THE CENTER EXHAUST HANGER ROD END BRACKET. (K)SDR QML2008F00011Exhaust Duct · fodKFMN TO KABQ. AFTER ENGINE STARTUP AND ENVIRONMENTAL SYSTEM TURNED ON, THE PILOT GRADUALLY BECAME AWARE OF A BURNING ODOR IN THE COCKPIT & CABIN. UPON TAXI OUT TO RUNWAY 25 IN KFMN, PILOT SAW BURNING EMBERS/SPARKS COMING FROM PROP AREA AND ENGINE EXHAUST ARESDR 2008FA0000622Cowling · crackedTHE SECONDARY EXHAUST COWLING WAS FOUND TO HAVE A 5.5 INCH LONG CRACK NEXT TO THE CENTER EXHAUST HANGER ROD END BRACKET. IT WAS NOTICED THAT ANOTHER CARAVAN IN THE HANGER FOR INSPECTION HAD THE SAME CRACK (LENGTH AND LOCATION) THAT HAD BEEN PREVIOUSLY REPAIREDSDR C2XA08IA165Diffuser · damagedIAH - FLIGHT 2346 DURING PREFLIGHT INSPECTION THE NR 1 ENG WAS FOUND TO BE MISSING PART OF THE EXHAUST DIFFUSER, WITH DAMAGE TO THE NR 1 THRUST REVERSER, EXHAUST CONE, AND CONE SUPPORT. MX REMOVED AND REPLACED ENG 1 EXHAUST CONE, FORCED MIXER CONE FLOWPATH SUSDR UIE2008F00023Skin · crackedCARRY OUT NR 4 PYLON EXHAUST SKIN CRACK CONDITIONAL CHECK REF EO NR 4754A250. REPAIRED CRACK IAW MFG MESSAGE 1-299984882-19. (K)SDR 2008FA0000451Elbow · misinstalledWHILE ACCOMPLISHING SERVICE ADVISORY 08-03 IT WAS DISCOVERED THAT RT SIDE EXHAUST ELBOW WHICH IS INSERTED BETWEEN WASTEGATE OUTLET FITTING AND TAILPIPE WAS ORIGINALLY INSTALLED BACKWARDS A THE FACTORY. THIS INCORRECT INSTALLATION RESULTED IN ELBOW HAVING ONLY SDR P5CA0801562Nozzle · crackedON WALK AROUND AFTER ARRIVAL FOUND A CRACK AT 2 O'CLOCK POSITION ON NR 3 ENGINE EXHAUST NOZZLE. PERFORMED INTERIM REPAIR IAW EO 4478A070 WITH DVI EVERY 3 FLIGHT CYCLES.SDR CA080602005Exhaust Duct · cracked(CAN) DAMAGED EXHAUST DUCT, PRIMARY FAILURE WAS TO THE INNER CONE OF THE EXHAUST DUCT, APPEARED TO CRACK AT NR 3 BEARING END AND EVENTUALLY DAMAGED THE T/E OF THE PT ROTOR BLADES. (TC NR 20080602005)SDR P5CA0801560Nozzle · crackedDURING WALK AROUND A 15" LONG CRACK WAS FOUND ON THE NR 2 ENGINE EXHAUST NOZZLE ON THE UPPER RIGHT QUADRANT. AN INTERIM REPAIR WAS ACCOMPLISHED PER EO 4478A069 AND 8110-3 DATED 27 APRIL 2008 ISSUED.SDR 20080420001Bracket · crackedON TAKE-OFF, 50 FEET, PARTIAL POWER LOSS (2,500+ RPM TO 1,100 RPM) AND ENGINE ROUGHNESS. ABORTED TAKE-OFF. WHEN CARBURATOR TAKEN OFF PLANE, FOUND 1 INCH X .5 INCH PIECE OF METAL LOOSE IN AIR/FUEL MIXING CHAMBER UPSTREAM OF VENTURI. PIECE WAS TOO BIG TO GO THSDR CA080326002Exhaust Duct · cracked(CAN) WHEN THE ENG WAS UNDERGOING A PHASE 6 INSP, A CRACK APPROX 3 INCH LONG WAS DISCOVERED IN THE ENGINE EXHAUST DUCT NEAR THE EGT PROBE BOSSES. IT APPEARED TO BE ON A PREVIOUS WELD. REMOVED AND REPLACED THE DUCT. (TC NR 20080326002)SDR CA081030004Exhaust Duct · deformed(CAN) VISUAL INSP (CF90-03R2) FOUND DEFORMATION AND CRACK IN MUFFLER ASSY AT THE BASE OF THE EXHAUST PIPE WITH SUBSEQUENT LEAK OF EXHAUST GASES INTO CABIN HEAT SYS, NO CO WARNING LIGHTS OR PILOT REPORTS POSTED. PART REPLACED AS REQ`D.SDR C2XA08IA025Exhaust Mixer · brokenIAH - DURING MAINTENANCE INSPECTION THE EXHAUST MIXER ON THE NUMBER TWO ENGINE WAS FOUND TO BE MISSING HALF, AND HAD DAMAGED THE THRUST REVERSER HOUSING UPON DEPARTURE. MAINTENANCE REMOVED AND REPLACED THE NUMBER TWO ENGINE, AND THRUST REVERSER, OPERATIONALLYSDR 2008FA0000376Clamp · looseENGINE DID NOT RESPOND WHEN POWER WAS APPLIED ON A LOW FLY BY OF THE RUNWAY AND CAUSED THE PLANE TO LAND NEXT TO THE RUNWAY IN THE SNOW DAMAGING THE AIRCRAFT. THE FOLLOWING PROBLEM WAS FOUND ON POST INCIDENT INSPECTION OF ENGINE AND EITHER ONE CAN CONTRIBUTE SDR 2008FA0000375Clamp · wornENGINE DID NOT RESPOND WHEN POWER WAS APPLIED ON A LOW FLY BY OF THE RUNWAY AND CAUSED THE PLANE TO LAND NEXT TO THE RUNWAY IN THE SNOW DAMAGING THE AIRCRAFT. THE FOLLOWING TWO PROBLEMS WERE FOUND ON POST INCIDENT INSPECTION OF THE ENGINE AND EITHER ONE CAN COSDR 2008FA0000028Clamp · looseENGINE DID NOT RESPOND WHEN POWER APPLIED ON A LOW FLY BY AND CAUSED THE PLANE TO LAND NEXT TO RUNWAY IN SNOW, DAMAGING ACFT. FOLLOWING PROBLEMS WERE FOUND ON POST INCIDENT INSPECTION OF ENGINE AND EITHER ONE CAN CONTRIBUTE TO LOSS OF LITTLE ALONE BOTH TOGETSDR SIMA200733910Nozzle · dirtyWHEN THRUST LEVERS PUSHED FWD, SMOKE FILLED COCKPIT AND WHEN THRUST LEVERS PULLED BACK SMOKE STARTED TO DISSIPATE. AIRCRAFT RETURNED TO SERVICE. CLEANED EXHAUST NOZZLE NR 1. OPERATIONAL CHECK GOOD IAW EMB 145 AMM 36-10-00 AIRCRAFT RETURNED TO SERVICE
SDR AALA20072196Tailpipe · debondedSTL INFLIGHT T531/13NOV - NUMBER ONE ENGINE HAD MULTIPLE COMPRESSOR STALLS DURING CLIMB. RETURNED TO STL AND LANDED WITHOUT INCIDENT. DISCOVERED DISBONDED LINING IN TAIL PIPE. REPLACED NUMBER ONE ENGINE ON 14 NOV 2007 AT STL. REPLACED LEFT ENGINE ISOLATORSSDR CA080122006Collector · damaged(CAN) FOUND WHEN CF90-03R2 WAS DONE. THERE WERE NO VISIBLE SIGNS OF EXHAUST LEAKS. WHEN PRESSURE TESTED WITH AIR AND SOAPY WATER, 4 LEAKS WERE EVIDENT. IT HAS BEEN STANDARD PRACTICE IN THIS AMO TO DO SOAPY WATER TESTS ONLY. OVER THE LAST 8 TO 10 YEARS WE HAVE SDR 2007FA0001010Pipe · failedLEADING EDGE EXHAUST SYSTEM INSTALLED BY STC SA02200AK FAILED AT THE SAIL PIPE TO MUFFLER WELD. SYSTEM HAS 36 HOURS SINCE NEW. (K)SDR CA071212024Exhaust Duct · cracked(CAN) WHILE INSPECTING THE POWER SECTION FOR REASSEMBLY AFTER HSI, CIRCUMFERENTIAL CRACKS WERE DISCOVERED ALONG THE WELDS OF THE EXHAUST DUCT JUST FWD OF THE PT VANE MOUNTING FLANGE. (4) CRACKS RANGED IN LENGTH FROM .75 INCH TO 4.75 INCH. THE POWER SECTION WASSDR CA071128019Tailpipe · burned(CAN) PILOT REPORTED ODOR OF EXHAUST IN CABIN. INSPECTION OF EXHAUST COMPLIED WITH AND FOUND BURNED OUT AREA AT TAILPIPE JUNCTION. CF90-03R2 COMPLIED WITH 72.8 HRS PREVIOUS WITH NO DEFECTS FOUND AT THAT TIME. EXHAUST REPLACED. (TC NR 20071128019)SDR FDKA200709511Mixer Box · brokenFDM 6097 ALB (0001 PHX LCL) - NR 1 ENGINE EXHAUST FORCED AIR MIXER BROKEN. MX REMOVED AND REPLACED MIXER.SDR 2007FA0000850Exhaust Duct · crackedWHILE PERFORMING SCHEDULED MAINTENANCE, REMOVED RT EXHAUST STACKS TO FACILITATE INSPECTING THE EXHAUST DUCT. FOUND A 1 INCH CRACK IN THE SKI SLOPE. SB 3380 WAS COMPLIED WITH 711 HOURS EARLIER. POWER SECTION WAS PULLED AND SENT OFF FOR REPAIR.SDR 2007FA0000853Flange · cracked(2) NEW ENGINES WERE INSTALLED IAW MFG MODIFICATIONS, WITH 938.0 HRS SINCE NEW. AIRCRAFT WAS IN FOR A PHASE INSPECTION AND FOUND 3 OUT OF L1 EXHAUST FLANGES ON THE ENGINE CRACKED. ACCORDING TO THE MFG PARTS MANUAL, EXHAUST STIFFENERS ARE NOT USED ON THIS SN SDR 2007UALA03800Exhaust Duct · crackedNR 1 ENG TAILCONE HAS MANY CRACKS AT THE ATTACH WELD MOUNTS. OVER 12 INCHES TOTAL LENGTH OF CRACKS.SDR MINR2007918AExhaust Pipe · bulgedTHE EXHAUST CROSSOVER EXHAUST PIPE WAS FOUND SEVERELY BULGED IN THE AREA COVERED BY THE HEAT SHROUD. THE DAMAGE WAS TO THE POINT, ISSUES WERE FORMING THAT WOULD HAVE LED TO RUPTURE. IF AN EXHAUST LEAK OCCURS IN THIS AREA, THE HEAT WILL AFFECT THE MAGNETO, FUELSDR UIEA200700349Nozzle · dentedNR 1 ENGINE EXHAUST NOZZLE DENTED AT 0300. NDT CHECKED NIL CRACK DENT AREA WITHIN LIMITS AMM 78-11-01 PAGE 601.SDR UIEA200700350Nozzle · dentedNR 3 ENGINE EXHAUST NOZZLE EXTERIOR SKIN DENTED AT 0900. NDT CHECKED NIL CRACK DENT AREA WITHIN LIMIT AMM 78-11-01 PAGE 601.SDR UIEA200700351Nozzle · dentedNR 4 ENGINE EXHAUST NOZZLE EXTERIOR SKIN DENTED AT 0700 TO 0900. NDT CHECKED NIL CRACK DENT AREA WITHIN LIMIT AMM 78-11-01 PAGE 601.SDR 2007FA0000749Exhaust Pipe · crackedDURING COMPLIANCE WITH AD 2000-01-16 THE TAIL PIPE ON THE RT ENGINE WAS FOUND WITH A 6 INCH CRACK. THE LAST INSPECTION WAS 40 HRS PRIOR.SDR 2007FA0001038Gasket · wrong partVISUALLY INSPECTED RT ENG AFTER RECOVERING THE A/C FROM A FIELD. FOUND MELTED WIRING AT NR 6 CYLINDER AND BEHIND IT. THE P-LEAD FOR THE RT MAG WAS MELTED AND WHEN TESTED FOUND TO BE SHORTED OUT. THIS SHUT-OFF RT MAG. THE NR 6 BOTTOM PLUG WIRE WAS HANGING LSDR 2007FA0000861Exhaust Header · crackedNR 5 EXHAUST HEADER HAS CRACKED OFF AT FLANGE, JUNE 6/06 AT 440.6, NOV 18/06 AT 636.1 HOBBS, MAY 18/07 AT 746.7 HOBBS AND AGAIN AUG 20/07 HOBBS NOT AVAILABLE. AFTER INSPECTING HEADER IT WOULD SEEM THAT A HEAVER GAUGE PIPE WOULD RESOLVE THE PROBLEM. THE LAST SDR CA070814007Exhaust Duct · cracked(CAN) DURING ROUTINE MAINTENANCE ON THE ENGINE, AN INSPECTION OF THE POWER TURBINE BLADES INDICATED LARGE CRACKS AND MISSING SECTIONS OF THE EXHAUST DUCT. THIS ENGINE WAS INSTALLED ON APRIL 02, 2007 AFTER OVERHAUL. THE CAUSE OF THE CRACKS ARE UNDER INVESTIGATISDR CA070814005Clamp · broken(CAN) AIRCRAFT WAS ENROUTE TO A FIRE, DURING CRUISE, THE NR 2 ENGINE FIRE WARNING SYSTEM ACTIVATED. THE ENGINE POWER WAS REDUCED AND THE FIRE WARNING WENT OUT. WHEN POWER WAS RE-APPLIED THE FIRE WARNING CAME ON AGAIN. THE RETARDANT LOAD WAS JETTISONED AND THE SDR 2007FA0000854Exhaust Stack · looseDURING AN INSPECTION, FOUND THE EXHAUST STACK AT NR 2 CYLINDER, PULLED DOWN .0625 INCH APPROX. FURTHER INVESTIGATION FOUND THE NR1, NR3, NR5 AND NR 6 ENGINE CYLINDERS EXHAUST STACKS PULLED DOWN, BUT NOT AS MUCH. AFTER RECOMMENDATIONS FROM ENGINE MFG ALSO, THSDR QXEA200701266Valve · contaminatedPDX FLIGHT NR 2265: FA REPORTS EXHAUST ODOR IN REAR OF AC ON APPROACH. PAX REPORTS FEELING SICK FROM ODOR. MAINTENANCE DUPLICATED ODOR USING NR 2 BLEED. C/W FIM 71-00-00-810-817. NO FAULT CODE IN CDS. NO OILY RESIDUE FOUND ON P2.2, P2.7 VALVES, P3.0 DUC ORSDR CA070802007Clamp · worn(CAN) PIN THAT PROTRUDES THROUGH THE MUFFLER AND EXHAUST PIPE WAS WORE ALLOWING THE THEM TO SEPARATE. OTHER AIRCRAFT IN THE FLEET WERE CHECKED AND FOUND OK. (TC NR 20070802007)SDR 07FDEA02379Liner · crackedNR 1 ENGINE HUSH KIT INNER LINER DISBONDED AND CRACKED AT 9 O'CLOCK POS. VERIFIED MATERIAL (INCONEL) REF. 78 -38-41 PREP FOR WELD REF 78-38-41, WELD WITH AMS 5837, A29984 INSPECT REF 78-38-41.SDR CA070704001Exhaust Duct · cracked(CAN) UPON ROUTINE INSPECTION, THE MAINTENENCE CREW FOUND THE EXHAUST DUCT CRACKED. THE ENGINE WAS REMOVED AND THE EXHAUST DUCT WAS REPLACED WITH A OVERHAULED ONE. NO OTHER PROBLEMS WERE DETECTED AT THIS INSPECTION. (TC NR 20070704001)SDR CA070705013Gasket · cracked(CAN) DURING ROUTINE INSP, IT WAS NOTICED THAT NEARLY ALL OF THE GASKET BETWEEN THE FWD FLANGE AND THE EXHAUST MUFF HAD CRACKED AND FALLEN AWAY, LEAVING THE POSSIBILITY OF A CABIN EXHAUST LEAK. (TC NR 20070705013)SDR CA070614002Exhaust Stack · separated(CAN) PRIOR TO DEPARTURE, ENGINE RUN-UP PILOT REPORTED THAT RT ENGINE RUNNING ROUGH. ENGINE ONLY PRODUCING 30" MP AND MAX 2250 RPM, AT GPH FF. RT MAG DROP WAS EXCESSIVE. MAINT INVESTIGATION FOUND ENGINE RT EXHAUST SEGMENT P/N LW-15849 SEPARATED FROM NR 5 EXHAUSDR C2XA07CL045Exhaust Mixer · failedCLE FLIGHT 2541 UPON ARRIVING IN CLE FROM AUS THE NR 1 ENGINE EXHAUST MIXER ASSEMBLY WAS FOUND TO BE MISSING LARGE PIECES. THE EXHAUST CONE WAS DAMAGED AND THE NR 1 THRUST REVERSR WAS ALSO DAMAGED. THE NR 1 ENGINE WAS REPLACED ALONG WITH THE NR 1 THRUST REVESDR CA070516002Exhaust Duct · cracked(CAN) SECONDARY EXHAUST DUCT CRACKED ALONG THE SEAM ON THE OUTER SIDE FROM ABOUT .2500 THE LENGTH DOWN TO .7500 THE LENGTH, CAUSING SEVERAL SMALLER CRACKS TO FORM ALONG INITIAL CRACK 90 DEGREES FROM THE ORIGINAL BOTH ON THE UPPER AND LOWER SIDES. OTHER OPERATSDR I5HA0758010Exhaust Pipe · looseWHILE EN-ROUTE FROM MIAMI (MIA) TO CANCUN (MUN) THE LEFT HAND ENGINE FIRE WARNING BELL SOUNDED. THE CREW REDUCED POWER ON THE ENGINE AND THE ALARM STOPPED. THE AIRCRAFT RETURNED TO MIA AND LANDED UNEVENTFULLY. THE CREW DID NOT DECLARE AN EMERGENCY. INSPECTSDR CA070502015Exhaust Pipe · broken(CAN) ON CLIMB PILOTS EXPERIENCED TORQUE FLUCTUATIONS ON RT ENGINE. THEY RETURNED TO THE AIRPORT WITH NO FURTHER PROBLEMS. ON TAXI THEY BLEW THE FIRE BOTTLES ON THE RT ENGINE. WHEN MAINTENANCE REMOVED THE COWLS THEY DISCOVERED HEAT DAMAGE TO SOME WIRING. ON FSDR 2007FA0000355Exhaust Duct · crackedCRACKING OCCURRED IN A SHORT TIME SPAN, DURING NORMAL OPERATION. CRACKS WERE OVER AN AREA APPROX 7 INCHES X 7 INCHES. ONE PIECE APPROX 3 INCHES X 3 INCHES SEPARATED FROM THE PART. AFTER CRACKING, DEFORMATION OF LOWER TRAILING EDGE OCCURRED BECAUSE IT WAS NOSDR 2007FA0000419Exhaust Duct · crackedWHILE PREFORMING SCHEDULED MAINTENANCE,REMOVED EXHAUST STACKS TO FACILTATE INSPECTING THE EXHAUST DUCT.A CRACK WAS FOUND IN THE SKI SLOPE.THE EXHAUST DUCT SB 3380 HAD BEEN COMPLIED WITH 365 HOURS PRIOR.POWER SECTION WAS REMOVED FOR REPAIR.
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