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 2013FA0000251Duct · crackedDISCOVERED EXHAUST CASE FLANGE CRACKED (APPROX 2" LONG) AT THE RADIUS OF THE FLANGE TO THE EXHAUST CASE PROPER. THIS CRACK WAS NOTED DURING MX FOLLOWING AN EXHAUST STACK/DUCT PIPE FRACTURE.SDR UALA2013042502898Tail Cone · crackedNR 1 ENGINE EXHAUST TAILCONE CRACKED. TOTAL LENGTH OF CRACK EST 9 INCHES. REPLACED TAILCONE.SDR CA130419001Exhaust Pipe · burned(CAN) DURING ROUTINE MAINTENANCE, PROP BALANCING, THE AME NOTICED THAT THE UPPER EXHAUST TAIL PIPE ON THE RT ENGINE HAD A LARGE HOLE BURNED THRU. PIPE WAS REMOVED AND FOUND TO HAVE ERRODED FROM THE INSIDE AND HAD SEVERAL CRACKS. UPPER AND LOWER TAIL PIPE, PN SDR UALA2013041902701Exhaust Duct · damagedNR 2 ENGINE EXHAUST LEFT INBOARD SIDE OF THE FAN AIR DUCT (C-DUCT) HAS SOME LOOSE MESH MATERIAL. AREA OF DELAMINATION IS NEAR OF TRAILING EDGE OF THE C-DUCT. SQUARE INCG AREA OF DELAM IS APPROX 24 SQUARE INCH PER MT 78-010. LOOSE MATERIAL HAS BEEN REMOVED,SDR UALA2013041502546Exhaust Duct · crackedCRACK FOUND ON NR 2 EXHAUST CONE AT 2 O`CLOCK POSITION 3-4 INCHES FROM END OF CONE. CRACK IS 1 INCH AND EXTENDS 1-4 INCHES INTO ZONE 3 IAW AMM. CONE REPLACED IAW ECRA 7811-01189.SDR V0XR2013041200002Shroud · crackedCRACK ON CENTER EXHAUST SHROUD ON THE FORWARD WELDED TROUGH. STOP DRILLED ENDS OF CRACK AND WELDED SHUT THE CRACK DAMAGE WITH AMS4951 FILLER ROD SHIELDING BOTH SIDES WITH ARGON GAS, AND PART MARKING IAW BOMBARDIER REPAIR DRAWING 8-78-351.SDR V0XR2013041200001Shroud · chafedLEFT EXHAUST CENTER SHROUD BOTTOM SECTION CHAFED THROUGH AT INBOARD CENTER. CUT OUT DAMAGED AREA, INSPECTED FOR CRACK INDICATIONS, FABRICATED AND WELDED INTO POSITION A REPAIR SKIN OF 0.020 TITANIUM, MIL-T-9046 CP-3 USING AMS4951 FILLER ROD WITH ARGON GAS SHISDR 2013FA0000222Exhaust Duct · crackedTHE LT EXHAUST SYS DEVELOPED CRACKS DURING A RECENT INSPECTION AT 825 HRS TT. THE NEW STYLE EXHAUST KIT WAS INSTALLED.SDR P5CA2013031800006Nozzle · crackedDURING WALKAROUND MAINTENANCE FOUND A CRACK ON THE EXHAUST NOZZLE OUTER SLEEVE, CRACK IS LOCATED AT THE 11 O'CLOCK POSITION ON THE NR 2 ENGINE. THE CRACK IS APPROXIMATELY 10" LONG. AS PER SRM 54-41-30 THE LENGTH OF THE CRACK IS OUT OF LIMITS. DISPOSITION ISSDR UALA2013030701353Exhaust Duct · crackedNR 1 ENGINE HAS A CRACK IN EXHAUST CONE, . STOP DRILLED. DID NOT JUMP STOP DRILL. REMOVED DIRT DEBRIS, ALL CHECKED GOOD..SDR UIEA2013030500114Exhaust Stack · crackedDURING MX WALK AROUND, FOUND A CRACK ON ENGINE NR 3 PRIMARY EXHAUST NOZZLE LOCATED AT 9 O'CLOCK POSITION AFT EDGE. THE CRACK DIMENSION RUNS 4.7500" LONG CIRCUMFERENTIAL AND LOCATED .7500" FROM THE NOZZLE AFT END. THE CRACK IS DETERMINED TO BE OUTSIDE ALLOWASDR PAI5201302261142Exhaust Stack · brokenPILOT NOTED RT ENGINE EGT INDICATOR INOPERATIVE IN CRUISE FLIGHT. MX FOUND EXHAUST STACK BROKEN IN 2 JUST FORWARD OF EGT PROBE. NO DAMAGE TO COWLING NOTED.SDR UALA2013022001040Cone · crackedCRACKS ON TOP OF NR 2 ENGINE TAIL CONE NEXT TO REPAIR WELDS. REPLACED ENGINE EXHAUST CONE.SDR UALA2013021500898Fastener · missingRIVET MISSING IN EXHAUST AREA OF NR 1 ENGINE RT C-DUCT LOWER BIFI HAS ONE MISSING FASTENER ON VERTICAL WALL APPROXIMATELY THREE INCHES FROM TRAILING EDGE. REPLACED LOCK FASTENER PER CMM 78-30-00 FIG 31 SHEET 10 ITEM 150.SDR HNAA2013021500076Retainer · crackedLT NACELLE EXHAUST SHROUD SEAL RETAINER IS CRACKED. REPAIRED SEAL RETAINER IAW DWG 85411375.SDR A6WA201303054817Skin · crackedRIGHT ENGINE TAIL PIPE INNER SKIN IS CRACKED NEAR THE 11 O`CLOCK ACCESS PANEL. INSTALLED REPAIR DOUBLER IAW CRJ 200 CMM 78-11.SDR A6WA201303054816Skin · crackedRIGHT ENGINE TAILPIPE INNER SKIN IS CRACKED NEAR THE 8 O`CLOCK POSITION. INSTALLED REPAIR DOUBLE IAW CRJ 200 SMM 78-11-00-300-801.SDR CA130130007Attach Fitting · cracked(CAN) DURING A POST FLIGHT ENGINEERS FOUND RT EXHAUST NOZZLE ATTACHMENT CRACKED.SDR CA130130006Support · broken(CAN) DURING POST FLIGHT INSPECTION, THE ENGINEERS NOTICED THAT THE LT ATTACHMENT SUPPORT ON THE RT EXHAUST NOZZLE HAS BROKEN OFF. DURING FURTHER INSP WE NOTICED THAT THE STRINGER ON THE EXHAUST SUPPORT ASSY HAS CRACKED. LT FORWARD EXHAUST ATTACHMENT BRACKETSDR R61A201301140057Panel · crackedWHILE AIRCRAFT WAS IN HEAVY CHECK MAINTENANCE WORKED DMI 337987103 NUMBER TWO ENGINE AFT PYLON FAIRING INBOARD EXHAUST GRILL IS CRACKED. MAINTENANCE REMOVED AND REPLACED NUMBER TWO ENGINE AFT PYLON FAIRING INBOARD EXHAUST GRILL IAW EMB ETD 2012-190-011599B , SDR R61A201301140056Panel · crackedWHILE AIRCRAFT WAS IN HEAVY CHECK MAINTENANCE WORKED DMI 337987/02 NUMBER ONE ENGINE INBOARD AFT EXHAUST PANEL GRILL IS CRACKED. MAINTENACE REPLACED GRILL HEAT SHIELD NUMBER ONE ENGINE AFT PYLON FAIRING INBOARD POSITION IAW EMB ETD 2012-190-011599-B REV B. TSDR UALA2013011600257Fastener · missingENGINE 2 EXHAUST NOZZLE LOWER FIXED STRUT HAS ONE MISSING RIVET AFT MOST HOLE INBOARD SIDE. LOWER STRUT FAIRING AT 6:00 INBOARD IS MISSING ONE FASTENER. PER MT78-001 ITEM N (2) REPLACED MISSING FASTENER.SDR DALA1301040666Rivet · missingRIVET AFT FAIRING EXHAUST OF LT ENGINE MISSING. REPLACED MISSING RIVET IAW SRM 54-51.SDR 2013FA0000024Seal · leakingFRONT CRANKSHAFT OIL SEAL DETERMINED TO BE LEAKING, AND ALLOWING OIL TO DRIP INTO CABIN HEAT EXCHANGER ON MUFFLER, WHICH WAS THE SOURCE OF A SMOKE ODOR. SEAL REPLACED AND ACFT WAS GROUND RUN AND TEST FLOWN WITHOUT DISCREPANCIES.SDR UALA2013010900137Tail Cone · crackedNR 1 ENGINE TAIL CONE IS CRACKED AT 3 AND 7 O`CLOCK POSITIONS. CRACKS APPROXIMATELY 3-5 INCHES LONG. CRACKS AT 3 AND 7 O'CLOCK ARE FROM PREVIOUS WELDED AREAS AND TRUE MEASUREMENTS OF SEVERAL CRACKS RANGE FROM .5 TO 1.5 INCHES. ALL WITHIN ZONE 1 AND OK FOR SSDR CA130114006Exhaust Duct · cracked(CAN) ON JAN 2, FIN 259 WAS FOUND TO HAVE A CRACKED CTR BODY EXHAUST ON NR 2 ENGINE DEFECT L4759417 READS: DURING PDC CHECK FOUND NR 2 ENGINE CENTER BODY EXHAUST CONE CRACKED 17" FROM AFT TIP AT THE WELD, RADIAL CRACK 60 PERCENT AROUND. CENTERBODY REPLACED ISDR 2013FA0000017Outlet · burnedDURING SCHEDULED INSPECTION, MECHANIC NOTED BURNING AROUND THE AREA OF THE EXHAUST OUTLET. IT WAS NOTED THAT THE BURNING, CRACKING AND DEBONDING HAD TAKEN PLACE IN A 12 X 9 AREA. FURTHER INSPECTION REVEALED THE CAUSE COULD BE FROM AN ENGINE BREATHER TUBE THASDR VNFR20121204002Exhaust Duct · crackedFOUND A LARGE CRACK WAS PRESENT IN THE RIGHT TURBO TRANSITION. TECHS PERFORMED AN EXHAUST SYSTEM PRESSURE TEST TO CONFIRM THE PRESENCE OF THE CRACK. REPLACED TRANSITION.SDR 2012FA0000793Exhaust Pipe · crackedDURING A 50 HOUR INSPECTION, A LARGE CRACK WAS FOUND THAT NEARLY CIRCLED THE ENTIRE TRANSITION. LOWER HALF OF TURBO TRANSITION WAS VERY CLOSE TO SEPARATING FROM THE REMAINING EXHAUST.SDR 2012FA0000792Exhaust Pipe · crackedFOUND A LARGE CRACK WAS PRESENT IN THE RT TURBO TRANSITION. PERFORMED AN EXHAUST SYS PRESSURE TEST AND CONFIRMED THE PRESENCE OF THE CRACK.SDR CA121218014Exhaust Duct · cracked(CAN) DURING AN INSPECTION, THE LT AND RT ENGINE EXHAUST TRANSITIONS WERE FOUND CRACKED. BOTH TRANSITIONS REPLACED WITH SERVICEABLE TRANSITIONS.SDR 2012FA0000782Exhaust Header · failedLEFT SIDE EXHAUST STACK ASSY FAILED AT MUFFLER ATTACH FLANGE. MUFFLER COMPLETELY SEPARATED FROM STACK ASSY.SDR UALA2012112606746Screen · damagedNR 2 ENGINE, LEFT C-DUCT INNER WALL SHOWS WIRE MESH SCREEN DAMAGE. ACCOMPLISHED PERMANENT REPAIR REF MT 78-010.SDR UALA2012112606768Rivet · missingNR 2 ENGINE EXHAUST UPPER PEN NIB FAIRING MISSING ONE RIVET INBOARD SIDE. RIVET REPLACED PER MT 78-001.SDR UALA2012110806437Rivet · damagedFOUND BY FRENCH DGAC ENGINE 2 NOZZLE TRAILING EDGE : ONE BROKEN RIVET (9 O'CLOCK POSITION). MISSING RIVET AT NR 2 ENGINE EXHAUST T-E 9 O'CLOCK POSITION CARRIED FORWARD IAW ECRA 7811-011 73. DETAIL VISUAL INSPECTION ACCOMPLISHED, NO FINDINGS. FOUND FASTENER SDR 2012FA0000747Exhaust Pipe · burnedEXHAUST PIPE BURNED THROUGH AT 2 LOCATIONS ADJACENT TO THE CENTERLINE SEAM WELD. THIS IS THE SECOND OCCURANCE ON THE SAME PN WITH VERY LOW HOURS.SDR UALA2012110506353Tail Cone · crackedNR 1 ENGINE TAIL CONE CRACKED. EXISTING 4 INCH CRACK IN ZONE ONE OF NR 1 ENGINE TAIL CONE WAS STOP DRILLED CRACK HAS NOW MIGRATED A .5 OF AN INCH FORWARD. STOP DRILLED CRACK WITH 1-4" DRILL PER MM. TOTAL CRACK LENGTH IS NOW 5 INCHES.SDR UALA2012102206019Structure · crackedCRACK NOTED ON RIGHT SIDE EXHAUST AREA ON LEFT ENGINE. MEASURED LENGTH OF CRACK DETERMINED TO BE 1.75 INCHES. REF SRM 54-31-01 THIS IS WITHIN SERVICEABLE LIMITS. WILL COVER AREA WITH SPEED TAPE TO PROTECT FORM MOISTURE.SDR CA121016005Flange · broken(CAN) EXHAUST FLANGE BROKEN IN HALF.SDR CA130819018Clamp · separated(CAN) THE EXHAUST CLAMP ON THE LT OF THE EXHAUST HAS A PIN WHICH LOCATES THE CLAMP ON BOTH THE MUFFLER AND THE PIPE IT ATTACHES TO. THE PIN HAD ERODED TO THE POINT WHERE IT ALLOWED THE PIPE TO SEPARATE FROM THE MUFFLER CAUSING SMOKE AND HEAT TO ESCAPE. THIS CSDR UALA2012101105787Exhaust Duct · crackedTWO INCH CRACK IN SHEETMETAL IN ENG NR 2 AT 12.30 POSITION IN EXHAUST END. STOPPED DRILLED PER MT78-00. CRACK BEYOND ALLOWABLE MM LIMITS. REPLACED CNA MM 78-11-11.SDR 2012FA0000690Exhaust Pipe · crackedFOUND THAT THE RT TAIL PIPE HAD CRACKED COMPLETELY IN HALF ALONG THE FORWARD EDGE OF THE CABIN HEAT EXCHANGER WELDMENT.SDR 2012FA0000688Manifold · crackedTHIS AIRCRAFT HAS A TURBO NORMALIZING SYS INSTALLED UNDER STCS SA10588SC & SE10589SC. THE FAILURE OCCURRED IN ONE OF THE COMPONENTS INSTALLED WITH THE STC. DURING A 500 HR IN SERVICE INSPECTION IAW SI11-01, IT WAS DISCOVERED THAT THE LT EXHAUST MANIFOLD WAS SDR UALA2012092505440Cone · crackedNR 1 ENGINE EXHAUST CONE CRACKED 1.5 INCHES IN LENGTH ZONE-3 AT 9 O'CLOCK POSITION. REPLACED EXHAUST CONE.SDR 2012FA0000698Exhaust Stack · erodedTHE PILOT MADE AN INTENTIONAL GEAR-UP LDG AFTER SEVERAL UNSUCCESSFUL ATTEMPTS TO FULLY EXTEND THE LANDING GEAR. FOLLOW-UP INSPECTION OF THE ACFT REVEALED THAT A SECTION OF THE LEFT-FRONT EXHAUST STACK ASSY HAD FAILED AND SEPARATED FROM THE ENGINE EXHAUST SYS,SDR A6WA20120921036Nozzle · crackedRIGHT JET PIPE FAIRING HAS HOT SPOT WITH CRACKS. REPAIRED RIGHT EXHAUST NOZZLE FAIRING INNER FIRESHIELD IAW BOMBARDIER CMM 78-11-00 REPAIR #SRS027.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.
Back to JASC 7810