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 UIEA2012091800436Sleeve · crackedNR 2 ENGINE EXHAUST NOZZLE OUTER SLEEVE FOUND CRACKED. DISPOSITION IS TO STOP DRILL THE ENDS OF THE CRACK WITH A 0.125" DIAMETER HOLE IAW PART 4 OF EO 4478A235.SDR UIEA2012091700426Exhaust Pipe · crackedTHERE IS A CRACK ON THE EXHAUST NOZZLE OUTER SLEEVE OF NR 2 ENGINE, APPROX 9 O'CLOCK TO 12 O'CLOCK POSITION (LT SIDE). THE CRACK IS APPROX 16" LONG AND IS 13" FROM AFT SIDE OF EXHAUST SLEEVE IAW SRM 54-41-30 THE DISTANCE BETWEEN THE CRACK AND THE EDGE IS OUT SDR UALA2012091305162Rivet · looseLEFT ENGINE HAS LOOSE RIVET IN EXHAUST CONE AT 6 O'CLOCK POSITION ON DATA PLATE.SDR CA120911007Exhaust Duct · cracked(CAN) EXHAUST Y PIPE, CRACKED INTERNALLY AT THE JUNCTION OF LT AND RT HAND EXHAUST BANK. IF MATERIAL BREAKS FREE IT WILL GO DIRECTLY INTO THE INLET OF THE TURBO CHARGER. THIS EXHAUST SYS IS MFG AND INSTALLED UNDER STC SE00215DE AND STC SA00214DE.SDR UIEA2012090200376Sleeve · crackedA CRACK WAS FOUND ON THE EXHAUST NOZZLE OUTER SLEEVE, APPROX AT 1 O'CLOCK POSITION (RT SIDE) ON THE NR 3 ENGINE. THE CRACK IS APPROX 2.5" LONG AND IS 1" FROM AFT SIDE OF EXHAUST SLEEVE JUST IN FRONT OF NAC STA 361.923. IAW SRM 54-41-30 THE DISTANCE BETWEEN TSDR UIEA2012090200375Sleeve · crackedDURING MX, FOUND A CRACK ON THE EXHAUST NOZZLE OUTER SLEEVE, APPROX AT 3 O'CLOCK POSITION (RT SIDE) ON THE NR 2 ENGINE. THE CRACK IS APPROX 3" LONG AND IS 1" FROM AFT SIDE OF EXHAUST SLEEVE JUST IN FRONT OF NAC STA 361.923 . IAW SRM 54-41-30 THE DISTANCE BETSDR CA120822010Clamp · broken(CAN) ON CLIMBOUT, THE CREW HAD A ZONE 1 FIRE INDICATION, THEY THROTTLED BACK AND INDICATION LIGHT WENT OUT. THEY E-HANDLED THE ENGINE, JETTISONED THE LOAD AND RETURNED TO THE AIRPORT. A BROKEN EXHAUST CLAMP WAS FOUND AT THE FWD END OF THE AFT LONG PORTION SDR R61A201208190663Structure · crackedMAINTENANCE WORKING DEFERRED MAINTENANCE ITEM NUMBER 1 ENGINE EXHAUST GRATE IS CRACKED. MAINTENANCE REMOVED AND REPLACED THE NUMER 1 ENGINE GRATE IAE EMB ETD 2012-190-011697A REV A. THE AIRCRAFT IS OUT OF SERVICE IN HEAVY CHECK.SDR R61A201208190662Structure · crackedMAINTENANCE WORKING DEFERRED MAINTENANCE ITEM NUMBER 2 ENGINE EXHAUST GRATE CRACKED. MAINTENANCE REPLACED NUMBER 2 ENGINE EXHAUST GRILL IAW ETD 2012-190-011697A REV A. THE AIRCRAFT IS OUT OF SERVICE IN HEAVY CHECK.SDR R61A201208150423Bracket · crackedWHILE AIRCRAFT WAS IN HEAVY CHECK MAINTENANCE FOUND THE NUMBER 2 ENGINE OUTBOARD EXHAUST COWL HOLD OPEN ROD BRACKET CRACKED. MAINTENANCE REMOVED AND REPLACED THE NUMBER 2 ENGINE OUTBOARD EXHAUST COWL HOLD OPEN ROD BRACKET IAW EMB SRM 175 SRM 51-43-02. THE AISDR UALA2012080604225Tail Cone · crackedNR 1 ENGINE TAILCONE HAS 4 INCH CRACK AT 12 O`CLOCK POSITION TOWARDS THE END OF CONE. REPLACED THE TAILCONE.SDR UIEA2012073000335Plug · crackedFOUND .8750" CRACK AT 6 O'CLOCK POSITION ON THE NR 1 ENGINE TAIL PIPE EXHAUST PLUG, ACCOMPLISHED PART I OF EO 6778A012, WHICH CONSISTED OF STOP DRILLING THE CRACK WITH A 0.125" DRILL BIT AND INSPECTING FOR FURTHER DAMAGE.SDR CA120726005Tailpipe · fire(CAN) CREW REPORT FIRE IN TAIL PIPE ON ARRIVAL.SDR KY7A201207260001Exhaust Pipe · brokenPILOT REPORTED ENGINE FAILED ON CLIMBOUT. PILOT SECURED ENGINE AND RETURNED FOR UNEVENTFUL LANDING. MAINTENANCE PERSONNEL FOUND BROKEN FLANGE ON EXHAUST PIPE UPSTREAM OF TURBOCHARGER. ENGINE FAILURE CAUSE WAS LOSS OF EXHAUST SUPPLY TO TURBOCHARGER WHICH STARVESDR A6WA201240716Support Bracket · crackedRT JETPIPE UPPER CORE COWL STANG ROD SUPPORT BRACKET ASSY MISSING RIVET AND STIFFENER AT XN214 CRACKED. R & R STIFFENER IAW CMM 78-11-00, SRS 042.SDR CA120723016Exhaust Duct · collapsed(CAN) EXHAUST DUCT COLLAPSED. EXHAUST NOZZLE FOR NR 1 ENGINE.SDR UALA2012071203777Exhaust Duct · damagedNR 2 ENG EXHAUST TAILCONE AREA. TWO DAMAGED RIVETS AND 1 MISSING RIVET APPROX 7 O'CLOCK POSITION. CARRIED FORWARD IAW MT 78-001 ITEM G. REPLACED RIVETS.SDR UALA2012070603647Fastener · looseLEFT ENGINE EXHAUST STATOR ABOUT 5 O'CLOCK LOOKING FORWARD SCREW IS COMING OUT. LOOSE FASTENER LOCATED ON INBD INTERMEDIATE CASE FAIRING, 2ND FROM BOTTOM.SDR CALA2012070500430Vent · damagedNR 2 ENGINE EXHAUST FWD CENTER BODY HAS A SECTION MISSING. R & R ENGINE NR 2 CENTER VENT TUBE IAW MM 78-11-03 AND R & RT FWD CENTER BODY IAW MM 78-11-02. OPS CHECKED GOOD.SDR UALA2012070503622Exhaust Duct · damagedENGINE 1 UPPER EXHAUST TAILCONE FAIRING HAS 2 MISSING RIVETS ONE INBOARD, ONE OUTBOARD. SUPPLEMENTAL DATA UPDATE, HAVE ONE RIVET ON EACH SIDE OF THE PEN NIB FAIRING MISSING. MEETS THE REQUIREMENT OF MT 78-001 OK TO CONTINUE FOR 50 HRS TO REPAIR. REPLACED RISDR UALA2012070503613Exhaust Duct · damagedENGINE 1 EXHAUST TAILCONE LOWER FIXED FAIRING OUTBOARD SIDE AFT MOST RIVET DAMAGED AND PROTRUDING. OK TO CARRY FORWARD FOR REPAIR IN 50 HRS PER MT78-001. REPLACED RIVET REF MT 87-001.SDR UALA2012070503612Exhaust Duct · damagedENGINE 1 LOWER EXHAUST TAILCONE FAIRING IS ALSO MISSING ONE RIVET OUTBOARD SIDE ONE HOLE FWD. OK TO CARRY FORWARD FOR REPAIR IN 50 HRS PER MT78-001. REPLACED RIVET REF MR87-0 01.SDR UALA2012070503595Exhaust Duct · crackedNR 2 ENGINE EXHAUST CONE HAS A 2-3 INCH CRACK AT THE SIX O'CLOCK POSITION. SUPPLEMENTAL DATA UPDATE, CRACK RUNS ALONG SEAM OF WELD REPAIR AT 6 0'CLOCK POS APPROX 5 INCHES LONG. ACCOMPLISHED REPAIR BY STOP DRILLING PER MM.SDR A6WA201240701Stiffener · crackedLEFT JET PIPE FWD STIFFENER AT 3 O`CLOCK POSITION IS CRACKED BEYOND STOP DRILL. REPAIRED LT JET PIPE FWD STIFFENER AT 3 O`CLOCK POSITION IAW CMM 78-11-00, SRS 042.SDR EVCA201206270031Collector · crackedON ROUTINE INSPECTION FOUND CRACKS IN THE REPAIR WELDS ON THE ENGINE EXHAUST COLLECTOR ASSEMBLY.SDR CA120618007Exhaust Duct · cracked(CAN) DURING A ROUTINE INSPECTION, A CRACK WAS NOTICED ON THE EXHAUST DUCT, BETWEEN THE B FLANGE & C FLANGE OF THE POWER SECTION. THIS IS A PRELIMINARY REPORT, MORE TO COME ONCE THE POWER SECTION IS RECEIVED. TIMES & CYCLES SINCE NEW ARE APPROX.SDR 2012FA0000367Exhaust Header · blisteredDURING A PRE-BUY INSPECTION, IT WAS FOUND THAT THE LT EXHAUST MANIFOLD ASSY WAS BLISTERED AND CRACKED IN 2 PLACES BETWEEN THE NR 2 AND NR 4 CYLINDERS.SDR A6WA201240673Exhaust Duct · dentedLEFT JET PIPE HAS SMALL SHARP DENT ON THE TOP SIDE. PERFORMED REPAIR ON LIGHT JET PIPE TOP SIDE IAW CMM 78-11-00.SDR CA120612004Exhaust Duct · damaged(CAN) EIR PT6A 2012-053. THIS ENGINE WAS SENT FOR INVESTIGATION AND REPAIR AFTER THE OPERATOR FOUND THE EXHAUST DUCT TO BE DAMAGED.SDR CA120604010Exhaust Stack · cracked(CAN) EXHAUST FOUND CRACKED AT THE FRONT PART OF THE INTERNAL CONE ON AN ENGINE, SOLOY CONVERSION IAW STC SR01647SE. THE CRACK WAS STILL WITHIN REPAIRABLE AREA, BUT COULDN`T BE STOP-DRILLED, SO THE EXHAUST HAS BEEN REPLACED BY A REPAIRED ONE.SDR CA120529012Exhaust Pipe · failed(CAN) WHILE ON LEVEL FLIGHT, THE PILOT OBSERVED A SUDDEN CHANGE IN THE SOUND WITH THE ENGINE`S EXHAUST. IT WAS LOUD, THEN BECAME LOUDER WITHIN A FEW SECONDS. AS A PRECAUTIONARY MEASURE, THE PILOT ELECTED TO CLIMB. THE INDIVIDUAL DETERMINED THAT THE ENGINE WAS SDR HNAA201205210079Shroud · crackedHOLE IN OTBD FWD SIDE OF NR 1 EXHAUST FINGER NAIL. R & R LT EXHAUSTS SHROUD WITH RETAINED FASTENERS.SDR 2012FA0000294Exhaust Duct · crackedLT ENGINE AFTER BODY, LOWER HALF DUCT, 4" CRACK EMMINATING FROM INNER IGNITION PLUG ACCESS PANEL. DOUBLER PATCH INSTALLED IAW SRM 51-00-00.SDR UALA2012051002683Fastener · failedTWO FAILED RIVETS IN LEFT ENGINE EXHAUST NOZZLE 2 O`CLOCK POSITION. REPLACED RIVETS. OPS OK.SDR T8VA20120503001Exhaust Stack · chafedON CLIMB-OUT RIGHT ENGINE FIRE LIGHT CAME ON. PERFORMED PRECAUTIONARY ENGINE SHUT DOWN CHECKLIST, RETURNED TO DEPARTURE AIRPORT AND LANDED. MAINTENANCE FOUND THAT THE LIP HEAT TUBE CAME OFF IN FLIGHT POSSIBLY DUE TO RUBBING ON COWLING. DUCT WAS FITTED TO SDR T8VA20120426001Exhaust Stack · crackedON CLIMBOUT RIGHT ENGINE FIRE LIGHT CAME ON. PERFORMED PRECAUTIONARY ENGINE SHUTDOWN CHECKLIST AND LANDED AIRCRAFT. MAINTENANCE FOUND RIGHT ENGINE INBOARD EXHAUST STACK LIP HEAT TUBE TO BE CRACKED. DAMAGED EXHAUST STACK REPAIRED BY OUTSIDE VENDOR AND INSTALSDR UALA2012042002385Cone · crackedNR 1 EXHAUST TAIL CONE HAS A CRACK AT THE 10 O'CLOCK POSITION. CRACK IS LOCATED IN ZONE 1, AND IS APPROX 4 1-8" LONG. STOP DRILLED CRACK WITH 1-4" DIA DRILL BIT PER AMM.SDR NSVA20120406511Clamp · missingCREW REPORTED TAIL PIPE HOT LIGHT ILLUMINATED A FEW TIMES IN FLIGHT AND EXTINGUISHED. REMOVED THE TAIL PIPE AND FOUND ONE OF THE RUBBER CLAMPS MISSING IN RETURN CHAFING THE WIRING HARNESS.SDR UALA2012040602145Tail Cone · crackedNR 1 EXHAUST TAIL CONE HAS A CRACK AT 10 O'CLOCK POSITION APPROX 6 INCHES LONG. FOUND CRACK TO BE 4.5 INCH LONG, STOP DRILLED CRACK.SDR CA120403009Exhaust Duct · cracked(CAN) ON INSTALLATION OF THE NEW EXHAUST SYS, THE AME CONDUCTED A FINAL INSPECTION OF THE COLLECTOR AND FOUND 3 HUGE CRACKS ON THE FLANGE WHERE A WELD HAD BEEN CARRIED OUT. THE MFG WAS CONTACTED AND A REPLACEMENT WAS SENT. THIS EXHAUST SHOULD HAVE NEVER PASSSDR UALA2012032801952Bolt · backed outENG 2 - TAIL CONE HAS 7 (OF 13) ATTACH BOLTS BACKED OUT AS FOLLOWS (CLOCK POSITION, DISTANCE BACKED OUT): 2:45, 3-16": 3:30, 1-8": 4:30, 1-8": 5:30, 3-16": 6:30, 1-8": 7:30, 7-32": 9:15, 5-32". FROM BASE WRITE-UP U5015K. CHECK TURBINE EXH CASE SHANK NUTS ANDSDR CA120329003Duct · dislodged(CAN) DURING FLIGHT, THE CREW REPORTED HIGH ENGINE TEMPERATURE AND THEY ELECTED TO SHUT IT DOWN BEFORE MAKING AN UNEVENTFUL SINGLE ENGINE LANDING. POST FLIGHT INSPECTION REVEALED A DISLODGED AIRFRAME EXHAUST DUCT. TROUBLESHOOTING IS ON-GOING.SDR UALA2012031901785Cone · crackedCAPTAIN REPORTS NR 1 ENG HAS SEVERAL CRACKS ON EXHAUST CONE. REPLACED NR 1 ENG EXHAUST CONE PER MM.SDR VGCA20120313Exhaust Duct · crackedNR 1 ENGINE ZONE 1 FIRE WARNING. FOUND EXHAUST DUCT CRACKED.SDR HNAA2012030900679Shroud · crackedAFT NACELLE FIREWALL JET PIPE SHROUD ABOVE THE JET PIPE IS CRACKED AT THE 10 O'CLOCK AND 11 O'CLOCK POSITION. REMOVED NACELLE ANGLE. LOCATED, DRILLED ANGLE. INSTALLED ANGLE IAW DWG 85410224 AND SRM 61-40-11. PROSEAL AREA WITH PROSEAL 700 ON NR 2 NACELLE.SDR A6WA201240273Panel · missingMISSING PANEL AT O`CLOCK POSITION. INSTALLED EXHAUST NOZZLE FAIRING MOUNT BOLT ACCESS PANEL IAW AMM 78-11-01, REF L/P 249882/3 FOR MEL.SDR UALA2012022000987Rivet · missingLEFT ENG MISSING RIVET AT THE EXHAUST NOZZLE 12 O'CLOCK POSITION. REPAIR WITHIN 50 FLT HOURS. REPLACED MISSING RIVET PER MT 78-001 PG 3 ITEM G.SDR CA120227005Coupling · broken(CAN) TAIL PIPE COUPLING BROKE ON OUTERBAND AT APPROXIMATELY THE 1:30 POSITION CAUSING THE TAIL PIPE TO FALL OUT OF POSITION.SDR UALA2012021300841Cone · crackedCRACK IN NR 2 ENG EXHAUST CONE. REPLACED REF MM.SDR 2012FA0000368Exhaust Header · fracturedDURING ROUTINE MX, IT WAS FOUND THAT THE LT EXHAUST MANIFOLD HAD CRACKED INTO 2 PIECES BETWEEN THE NR 2 AND NR 4 CYLINDERS.
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