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.

SDR HALA2010041900178Shroud · crackedETOPS SIGNIFICANT SYS - CRACK FOUND ON NR1 ENG EXHAUST SHROUD INBD SIDE. NOTE: CRACK IS 10-12" LONG. REPLACED NR 1 ENG TURBINE EXHAUST SLEEVE IAW AMM 78-11-01.Apr 19, 2010 · N596HA · Boeing 767332SDR QXEA2010042000275Bracket · crackedMODIFICATION - NR 2 EXHAUST OTBD STRUT BRACKET IS CRACKED AT ATTACH POINT. R & R BRACKET USING SOLID RIVETS. REF SRM 51-42-06.Apr 18, 2010 · N428QX · Bombdr DHC8402SDR UIEA201000191Nozzle · dentedDURING MX WALKAROUND, FOUND A DENT ON THE EXHAUST NOZZLE OUTER SLEEVE AT APPROX THE 6:00 POSITION ON THE NR1 ENGINE. THE DENT IS APPROX 2" LONG AND 0.05 INCHES WIDE AND IS APPROX 42 INCHES FROM THE T/E OF THE NOZZLE. IAW SRM 54-41-30 THE DENT IS OUT OF LIMITS.Mar 23, 2010 · N409MC · Boeing 74747UFSDR 2011FA0000102Exhaust Pipe · crackedTHE RT TAILPIPE WAS SENT FOR REPAIR ON 3/10/10 BECAUSE IT WAS CRACKED.Mar 10, 2010 · N1029N · Maule MXT7180ASDR P5CA2010030101621Nozzle · crackedENGINE 3 EXHAUST NOZZLE HAS A CRACK AT THE 12 O'CLOCK POSITION APPROXIMATELY 24 INCHES LONG RUNNING FROM 10 O'CLOCK TO 1 O'CLOCK POSITION, 13 INCHES FROM EDGE OF NOZZLE. TIME LIMITED REPAIR ACCOMPLISHED IAW EO 4478A121 AND FAA 8110-3 DATED 25 FEB 2010. DVI RFeb 25, 2010 · N452PA · Boeing 74746NFSDR A6WA201040132Frame · crackedRT TAIL PIPE FAIRING 2ND AFT INNNER FRAME CRACKED. REPAIRED RT EXHAUST NOZZLE FAIRING IAW BOMB CMM 78-11-00. REPAIR NR SRS042.Feb 16, 2010 · N430AW · Cndair CL6002B19SDR A6WA201040118Seal · damagedLT JET PIPE UPPER AND LOWER SEALS REQUIRE REPLACEMENT. R & R UNSERVICEABLE SEALS ON LT JET PIPE UPPER AND LOWER IAW CMM 78-11-00.Feb 12, 2010 · N431AW · Cndair CL6002B19SDR CA100212001Strut · broken(CAN) WHILE A 50HR INSP WAS BEING CARRIED OUT ON THE ACFT, IT WAS DISCOVERED THAT THE EXHAUST STRUT WAS BROKEN IN HALF APPX MID SECTION OF THE SHAFT. IT WAS OBSERVED THAT THERE WERE NO SIGNS OF CORROSION, BENDING, OR OBVIOUS DAMAGE TO THE PART TO CAUSE IT TO FFeb 11, 2010 · Moravn Z242LSDR UIEA201000192Nozzle · crackedNR 4 ENG EXHAUST NOZZLE ASSY FOUND 3 LOCATIONS CRACKED AT FWD FLANGE AREA. NR 4 ENG EXHAUST ASSY 3 LOCATIONS CRACK REPAIR CARRIED OUT AS PER EM CF6-50 REPAIR O2 PROCEDURE B (1) AND EO 4778A148.Feb 4, 2010 · N523MC · Boeing 7472D7BSDR UIEA2010020400005Nozzle · crackedDURING AN ENGINE CHANGE AT AN A-CHECK, MX FOUND 3 EA CRACKS ON THE NR 4 ENG FIXED COWL EXHAUST NOZZLE FWD FLANGE COWL SUPPORT ASSY. THE CRACKS CAN BE REPAIRED IAW THE ESM TASK 78-33-05. REPAIR 002. THE REPAIR CALLS FOR A POST WELD HEAT TREATMENT AND THERMAL SPFeb 4, 2010 · N523MC · Boeing 7472D7BSDR UIEA201000003Sleeve · dentedA DENT WAS FOUND ON THE NR 4 ENG LT EXHAUST SLEEVE, AT THE 9 O'CLOCK LOCATION NEAR NAC STA 349-236. MANUFACTURER PROVIDED INSPECTION TIMELINE OF REF/D/AND PERFORM FPI INSPECTION PER BAC 5423 TO ENSURE NO CRACKS ARE PRESENT ON NOTED DENT. REPEAT INSPECTION EVJan 30, 2010 · N408MC · Boeing 74747UFSDR P5CA1001618Nozzle · crackedNUMBER TWO EXHAUST NOZZLE HAS TWO CRACKS. ENGINEERING ORDER 4478A114 ACCOMPLISHED STOP DRILL AS INTERIM REPAIR AND 3 CYCLE REINSPECTION. NOZZLE MUST BE REPLACED BEFORE NEXT A CHECK. THIS EO APPROVED BY FAA 8110-3 DATED 11 JAN 2010.Jan 29, 2010 · N454PA · Boeing 74746NFSDR P5CA1001619Nozzle · crackedNUMBER TWO EXHAUST NOZZLE HAS A CRACK. ENGINEERING ORDER 4478A115 & FAA 8110-3 DATED 19 JAN 2010. ACCOMPLISHED TO STOP DRILL CRACK AS INTERIM REPAIR & DVI EVERY 3 FLIGHT CYCLES. NOZZLE MUST BE REPLACED BEFORE NEXT A-CHECK.Jan 19, 2010 · N452PA · Boeing 74746NFSDR A6WA201040156Bracket · crackedLT JETPIPE UPPER INBD ATTACH POINT NUTPLATE BRACKET CRACKED. REMOVED DAMAGED BRACKET, DUPLICATED SERVICEABLE BRACKET IAW CMM 78-11-00, AND INSTALLED SERVICEABLE BRACKET IAW CMM 20-42-06.Dec 30, 2009 · N432AW · Cndair CL6002B19SDR A6WA201040002Stiffener · crackedRT JETPIPE 2ND RIB CRACKED. REAPRED RT JETPIPE 2ND RIB IAW CMM TASK 78-11-00-300-810-A01. REPAIR SRS 042.Dec 9, 2009 · N433AW · Cndair CL6002B19SDR 2009FA0001013Clamp · brokenDURING ACCIDENT INVESTIGATION, FOUND TOP LT ENGINE COWLING WITH EVIDENCE OF FIRE AND BURNED HOLES, LT EXHAUST MANIFOLD PIPE WAS LAYING LOOSE, AND LT CLAMP TO TURBO COMPRESSOR BROKEN AND LAYING IN BOTTOM OF ENGINE COWL. AIRCAFT WAS DESTROYED IN FIRE WITH ONE FDec 3, 2009 · N17803 · Beech A36SDR YADA111709Exhaust Stack · crackedPILOT REPORTED OCCASIONAL EXHAUST FUMES IN CABIN. CONFIRMED THAT THE CREW SMELLED EXHAUST ON ROLLOUT WITH PROPS IN BETA AND HAD SMELLED IT AT AN ENGINE START (AS IS COMMON WHEN STARTING WITH A TAIL WIND). MX LOCATED A CRACKED HEATED INTAKE LIP STUB PIPE ON TNov 17, 2009 · N111AX · Beech 1900CSDR CA091116001Shock Mount · broken(CAN) EXHAUST TAILPIPE SHOCK MOUNT BORKEN BETWEEN FIREWALL AND TAILPIPE.Nov 13, 2009 · Cessna 172RGSDR DL777091735Plug · missingFOUND DURING WALK AROUND ON ARRIVAL - NR 1 ENGINE AFT EXHAUST PLUG MISSING. SCREWS STILL ATTACHED TO FWD PLUG SECTION. NO DAMAGE FOUND TO AIRCRAFT. REPLACING FWD AND AFT EXHAUST PLUGS. FOUND INSULATION BLANKET ENG COVER DAMAGED. REMOVED AND REPLACED INSULNov 6, 2009 · N860DA · Boeing 777232SDR A6WA200940739Fitting · crackedLEFT TAILPIPE FAIRING VENT FITTING ASSY CRACKED. LT TAIL PIPE FAIRING VENT FITTING ASSY REPLACED IAW SRM 51-42-06. (K)Oct 23, 2009 · N411ZW · Cndair CL6002B19SDR ECQ2009F00001Riser · crackedMECHANIC HEARD ACFT TAXI INTO PARKING. INSP REVEALED FWD MUFFLER ON RT ENGINE LOOSE. FURTHER INSP REVEALED THAT: INBD MUFFLER FLANGE BROKEN. OTBD EXHAUST RISER BROKEN OFF CYLINDER ATTACH FLANGE. MUFFLER WAS LAYING ON LWR COWLING. INBD LWR COWLING HAD A BUOct 5, 2009 · N882FT · Piper PA44180SDR A6WA200940606Stiffener · gougedRT ENGINE TAIL PIPE EXHAUST FAIRING, STIFFENER GOUGED ADJACENT TO ACCESS PANEL AT 6 O`CLOCK POSITION ACCESS PANEL STIFFENER IAW CMM 78-11-00-300-818-A01, REPAIR SRS 084. (K)Sep 24, 2009 · N425AW · Cndair CL6002B19SDR EE4Y09276Angle · corrodedNR 1 ENGINE EXHAUST NOZZLE UPPER SECTION, ANGLE CRACKED.Sep 21, 2009 · N946MD · Doug DC983SDR KS12009F00000Exhaust Stack · crackedINSTALLED EXHAUST STACK ON 9/18/2008. ACFT TT 9927.8. DURING ANNUAL INSPECTION FOUND A CRACK AND HAD A WELD REPAIR DONE. 9/2/2009 ACFT TT 10302.9. DURING A 100 HR INSPECTION, FOUND ANOTHER CRACK. REPLACED EXHAUST STACK FROM SERVICE. (K)Sep 8, 2009 · N26TC · Hughes 369ESDR 2009FA0000773Exhaust Stack · crackedEXHAUST STACK ASSY FOUND TO BE CRACKED AT RELIEF POINTS AROUND BASE IN 2 PLACES. 1ST STACK LASTED 411.1 HOURS, THEN INSTALLED REPAIRED STACK, THIS LASTED APPROX 200 HOURS WITH CRACKS IN SAME PLACE AS WELL AS AT TIP OF CONE. THE 3RD STACK CRACKED UPON INSTALLSep 3, 2009 · N5793P · Snias AS350BASDR A6WA200940569Bracket · crackedLT ENGINE TAILPIPE FAIRING OTBD ATTACHMENT, NUT PLATE BRACKET ASSY IS CRACKED. REPLACED IAW SRM 51-42-06. (K)Sep 2, 2009 · N467AW · Cndair CL6002B19SDR VNAA2009090800003Nozzle · damagedCREW REPORTED A LIGHTNING STRIKE INSPECTION IN MOB. MAINTENANCE INSPECTED AIRCRAFT PER THE AIRCRAFT MAINTENANCE MANUAL. MAINTENANCE REMOVED AND REPLACED NOZZLE ASSY EXHAUST, TAILPIPE FAIRING ASSEMBLY AND STATIC WICKS. CHECKS WERE COMPLETED PER AIRCRAFT MAINSep 1, 2009 · N244PS · Cndair CL6002B19SDR P5CA2009090101606Sleeve · crackedCRACK FOUND ON NR 2 ENGINE EXHAUST SLEEVE FROM 12 O'CLOCK TO THE 1 O'CLOCK POSITION. NO OTHER DAMAGE FOUND. INTERIM REPAIR ACCOMPLISHED IAW EO 4478A097/FAA 8110-3 DATED 29 AUG09. DETAIL VISUAL INSPECTION DUE EVERY 3 FLIGHT CYCLES AND PERMANENT REPAIR DUE ATAug 29, 2009 · N452PA · Boeing 74746NFSDR P5CA2009082801605Sleeve · crackedCRACK FOUND ON THE NR 2 ENGINE EXHAUST SLEEVE AT THE 12 O'CLOCK POSITION DURING WALK AROUND INSPECTION. INTERIM REPAIR ACCOMPLISHED IAW EO 4478A096 ISSUED PER FAA 8110-3 DATED 27 AUG 09. DETAILED VISUAL INSPECTION DUE EVERY 3 FLIGHT CYCLES UNTIL NEXT A-CHECKAug 27, 2009 · N451PA · Boeing 74746NFSDR CA090824004Exhaust Pipe · crackedWHILE TAXIING TO POSITION ON THE RUNWAY FOR TAKEOFF THE LT FIRE WARNING ILLUMINATED AS POWER WAS ADDED, LIGHT EXTINGUISHED WHEN POWER WAS REDUCED. FOUND 3 CRACKED EXHAUST PIPES, 2 OF WHICH HAD BROKEN OFF OF THE CYLINDERS NR 4 AND 5. FIREWALL WAS INSPECTED SEAug 21, 2009 · Gruman FIRECATSDR A6WA200940457Bracket · crackedLT TAIL PIPE FAIRING FWD BRACKET OF COVER ASSY CRACKED. LT TAIL PIPE FAIRING FWD BRACKET OF COVER ASSY. REPLACED IAW SRM 51-42-06. (K)Aug 4, 2009 · N423AW · Cndair CL6002B19SDR CIEA200900010Exhaust Stack · crackedRIGHT ENGINE OUTBOARD EXHAUST STACK CRACKED. REMOVED RIGHT ENGINE OUTBOARD EXHAUST STACK PART NUMBER 78-00-00-20, SERIAL NUMBER 2203, DUE TO LARGE CRACK RUNNING 80 % AROUND THE CIRCUMFERENCE OF THE EXHAUST STACK AND REPLACED WITH NEW EXHAUST STACK PART NUMBER Jul 28, 2009 · N5ST · Beech 200BEECHSDR A6WA200940380Fairing · dentedLT ENG EXHAUST NOZZLE FAIRING DENTED AT 6 O’CLOCK CLOSE TO DRAINS. LT ENG EXHAUST NOZZLE FAIRING AT 6 O`CLOCK. REPAIRED IAW CMM78-11-00-300-805-401. (K)Jul 9, 2009 · N461AW · Cndair CL6002B19SDR P5CA2009052901597Exhaust Pipe · crackedDURING WALK AROUND CHECK, AN 8 INCH LONG CRACK WAS FOUND AT THE 12 O'CLOCK POSITION 13 INCHES FROM THE TRAILING EDGE OF THE NR 2 ENGINE EXHAUST NOZZLE. "AREA WAS INSPECTED IAW SRM 54-41-30 AND EO 4478A086 WAS ISSUED BY ENGINEERING WITH FAA 8110-3. THE AIRCRAMay 27, 2009 · N450PA · Boeing 74746NFSDR P5CA2009052901596Exhaust Pipe · crackedDURING WALK AROUND CHECK, A 12 INCH LONG CRACK WAS FOUND AT THE 12 O'CLOCK POSITION 13 INCHES FROM THE TRAILING EDGE OF THE NR 3 ENGINE EXHAUST NOZZLE. "AREA WAS INSPECTED IAW SRM 54-41-30 AND EO 4478A085 WAS ISSUED BY ENGINEERING WITH FAA 8110-3. THE AIRCRAMay 27, 2009 · N450PA · Boeing 74746NFSDR 2009FA0000346Exhaust Duct · crackedDURING THE SID INSPECTION THE LT ENG EXHAUST EDUCTOR WAS FOUND CRACKED. REMOVED EDUCTOR FOR REPAIR AND REINSTALLED.May 1, 2009 · N256DD · Cessna 441SDR UIEA201000182Nozzle · damagedPUNCTURE ON THE LONG FIXED CORE EXHAUST NOZZLE (LFCEN) ON THE NR 2 ENGINE. THE PUNCTURE IS APPROX 0.25" WIDE, APPROX 5.0 INCHES FROM THE T/E OF THE EXHAUST SLEEVE AT THE 3:00 POS. SMOOTH THE EDGES OUT USING STANDARD PRACTICES AND ELEMENTARY OPERATIONS. REPLACEApr 21, 2009 · N523MC · Boeing 7472D7BSDR 2009FA0000456Exhaust Pipe · crackedWHILE FLYING PART OF THE EXHAUST PIPE ON THE PILOT SIDE SEPARATED FROM THE PLANE. THE BREAK OCCURRED AT THE WELD JOINT WHERE THE LAST HEADER JOINED THE MAIN PIPE. THIS EXHAUST SYS WAS A CUSTOM BUILT EXHAUST WITH NO SLIP JOINTS OR SUPPLEMENTAL SUPPORTS. THE Apr 18, 2009 · N200SX · Amtr PUSHERSDR CA090330002Duct · cracked(CAN) NR 2 PWR OUTPUT SECTION EXHAUST DUCT CRACKED AND DAMAGED, SUBSEQUENT PWR TURBINE BLADE DAMAGE. NO ENG PWR OR PERFORMANCE WAS EFFECTED DURING FLIGHT OPERATIONS. DAMAGE TO POWER OUTPUT SECTION EXHAUST DUCT WAS FOUND DURING ENG EXHAUST OUTLET REPLACEMENT. EMar 22, 2009 · Beech 200BEECHSDR P5CA2009031501588Sleeve · cracked2.5 IN CRACK FOUND ON NR 2 ENG EXHAUST NOZZLE OUTER SLEEVE AT THE TRAILING EDGE AT THE 10 O'CLOCK POSITION. "PER EO 4478A081, STOP DRILLED CRACK AND REPAIR WITHIN 10 FLIGHT CYCLES. FAA 8110-3 ISSUED 15 MAR 09".Mar 15, 2009 · N450PA · Boeing 74746NFSDR CA090211001Cone · crackedVISUAL INSPECTION DURING "A-CHECK" (WITH FLASHLIGHT) REVEALED LARGE CRACK IN CIRCUMFERENCE OF EXHAUST UNIT INNER CONE. CLOSER INSPECTION (CRAWLED UP JET-PIPE) INDICATED APPROX, 2/3 OF INNER CONE CIRCUMFERENCE CRACKED. DAMAGED AREA NORMALLY RESTS WITHIN 1/8 -Jan 30, 2009 · Braero HS7482ASDR UPS09554433Bracket · brokenINSPECTION TYPE:C2 UPPER TURBINE CASE DRAIN TUBE BRACKET BROKEN NR 1 ENGINE. REMOVED, FABRICATED, INSTALLED BRACKET PER M/M 78-11-04-8.Jan 22, 2009 · N463UP · Boeing 75724APFSDR GAJ2009F00000Slip Joint · crackedAD DEALING WITH 3 EXHAUST FLANGES CRACKING AND CAUSING FIRE SO WE REMOVED THAT MFG FLANGES AT TRANSITION AND REPLACED WITH OTHER MFG IF ORIGINAL WERE CRACKED. NOW HAVE OTHER MFG FLANGES AND ORIGINAL MFG SLIP JOINTS AND IT WAS NOTED THAT YOU COULD HAVE THE SLIJan 2, 2009 · N80GV · Piper PA31350SDR 2009FA0000018Collector · damagedEXHAUST COLLECTORS 3 TO 1 TYPE. BULGES AND BLOW OUTS.Dec 23, 2008 · N417PK · Robsin R44RAVENIISDR GAJ2008F00001Exhaust Pipe · crackedFOUND EXHAUST FLANGE UNDER V-CLAMP CRACKED. FIRST SIGN OF PROBLEM WAS EXHAUST STAINS IN AREA. AFTER THE CLAMP WAS REMOVED THE FLANGE WAS FOUND CRACKED APPROXIMATELY 70 PERCENT OF TH4E CIRCUMFERENCE OF THE FLANGE. (K)Dec 15, 2008 · N8006U · Piper PA31350SDR JIK2008F00007Exhaust Pipe · crackedON 11/24/2008 DURING COMPLETION (FCD) 31-78-2008-02. INSP OF EXHAUST SYS, IT WAS NOTED THAT THE FLANGE OF THE EXHAUST PIPE AS IT GOES INTO THE TRANSITION HSG WAS CRACKED APPROX .5 THE WAY AROUND THE CIRCUMFERENCE OF THE FLANGE. THE EXHAUST MANIFOLD WAS REPLACDec 4, 2008 · N59973 · Piper PA31350SDR FFSA200800007Exhaust Pipe · crackedDURING SCHEDULED INSP MECHANIC NOTICED EXHAUST STAINING AROUND THE AFT SIDE OF THE V-BAND CLAMP AT THE OTBD SIDE OF THE TURBOCHARGER TRANSITION OF THE LT ENGINE. REMOVAL OF THE CLAMP REVEALED A 2.25 INCH CRACK IN THE RADIUS OF THE STACK FLANGE ALONG THE AFT SINov 18, 2008 · N137CS · Piper PA31350SDR YAA2008F00000Collector · crackedPILOT REPORTED SMOKE IN COCKPIT AFTER TAKEOFF, HE LANDED ACFT SAFELY AND TAXIED TO MAINT HANGER. MAINT FOUND HOLE AND CRACK IN EXHAUST NEAR HEATER MUFFLER. REMOVED AND REPLACED LT EXHAUST COLLECTOR, RAN UP ENGINE, FOUND OK FOR SERVICE ALL AD`S ON EXHAUST ARNov 5, 2008 · N6470H · Cessna 207ASDR JIK2008F00004Exhaust Duct · crackedON 9/11/08 DURING AN INSP, IT WAS FOUND THAT THE EXHAUST FLANGE WHERE THE MANIFOLD IS CLAMPED TO THE WASTE GATE HOUSING, THERE WAS A CRACK IN THE FLANGE RADIUS THAT RAN APPROXIMATELY .3333 OF THE WAY AROUND THE PIPE. THE MANIFOLD ASSY WAS REPLACED WITH A NEW AOct 17, 2008 · N27426 · Piper PA31350SDR JIK2008F00006Exhaust Duct · crackedDURING INSPECTION ON JUNE 26, 2008 IT WAS NOTED THAT THERE WAS A CRACK THAT WENT AROUND THE CIRCUMFERENCE OF THE NR 7 EXHAUST FLANGE. A NEW MANIFOLD ASSY WAS ORDERED AND INSTALLED. WHILE REMOVING THE CRACKED ONE, IT WAS DISCOVERED THAT THERE HAD BEEN COMPLETOct 16, 2008 · N35805 · Piper PA31350
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