JASC 7800

Service difficulty reports · 281

Reports filed under 7800 · Engine Exhaust System, 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 = '7800'
  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 MALA060105Nozzle · chafedDURING 4K BRIDGE CHECK IN BNA FOUND LEFT LOWER EXHAUST NAZZLE IS CHAFED AND HAS BEEN REPAIRED IAW MESABA EOS54133.Feb 24, 2006 · N424XJ · Saab 340BSDR 2006FA0000219Riser · crackedORDERED A NEW EXHAUST RISER FOR THE NR 2 CYLINDER. INSPECTING THE RISER BEFORE INSTALLATION WE FOUND A CRACK AT THE WELD RADIUS OF THE MOUNT FLANGE AND THE EXHAUST PIPE. THIS MAY HAVE ACCURED FROM EXCESS HEAT DURING MANUFACTUR. THIS THE FIRST CRACK SEEN ON Feb 10, 2006 · N164DS · Diamon DA40SDR CA050803003Segment · cracked(CAN) THE PILOT REPORTED AN INTERMITTENT (POPPING) SOUND DURING ALL PHASES OF OPERATION. MAINTENANCE INVESTIGATION REVEALED A CRACK AND BLOWN EXHAUST GASKET ON NR 3 CYLINDER EXHAUST SEGMENT. THE CRACK EXTENDED AROUND MOST OF THE FLANGE, AND WAS CREEPING UP TJul 28, 2005 · Dhav DHC2*SDR EGRR101267Damper · deterioratedDURING AIRCRAFT INSPECTION, FOUND LT ENGINE EXHAUST SADDLE CHAFING ON ENGINE FIRE EXTINGUISHER BOTTLE UPPER ACTIVATION CARTRIDGE ELECTRICAL WIRE CONNECTING POINT. THE RUBBER NIPPLE WAS CHAFED THROUGH AND THE SADDLE WAS SITTING DIRECTLY ON THE STUD. REPLACED 2Jun 9, 2005 · N15MV · Agusta A109ESDR 2688200410001Crossover Tube · crackedDURING ANNUAL INSPECTION, DISCOVERED CRACK APPROXIMATELY 1.5 INCHES IN LENGTH AROUND THE LT CROSSOVER ASSEMBLY (PN 2254008). UPON REMOVAL, ALSO FOUND DETERIORATION IN THE SLIP JOINT CONNECTING THE RT CROSSOVER ASSEMBLY (PN 2254013). REPLACED BOTH PARTS WITH Sep 3, 2004 · N5091T · Cessna TR182SDR 2688200400001Crossover Tube · crackedDURING ANNUAL INSPECTION, DISCOVERED CRACK APPROXIMATELY 1.5 INCHES IN LENGTH AROUND THE LT CROSSOVER ASSEMBLY (PN 2254008). UPON REMOVAL, ALSO FOUND DETERIORATION IN THE SLIP JOINT CONNECTING THE RT CROSSOVER ASSEMBLY (PN 2254013). REPLACED BOTH PARTS WITH Sep 3, 2004 · N5091T · Cessna TR182SDR 04FDEA00849Duct · crackedCOMPLY WITH EA 7-7254-77153 ENGINE - FAN EXHAUST OUTER DUCT NR 6 OIL SUPPLY TUBE EGRESS BOSS WELD REPAIR. COMPLIED WITH EA 7-7254-77153 ENGINE - FAN EXHAUST OUTER DUCT NR 6 OIL SUPPLY TUBE EGRESS BOSS WELD REPAIR AT MAE.Apr 7, 2004 · N279FE · Boeing 727200SDR GTIA030241Liner · crackedFOUND RT ENGINE HAS A SECTION OF ACCOUSTIC LINER MISSING AND CRACKED TAILPIPE 2 O'CLOCK POSITION. REMOVED AND REPLACED THRUST REVERSER SPACER. OPS AND LEAK CHECK GOOD. (M)Mar 31, 2003 · N130NK · Doug DC941SDR NACA20030078Exhaust Pipe · crackedDISCREPANCY: ZONE #1 FIRE WARNING ON #3 ENGINE DURING TAKE OFF ROLL.CORRECTIVE ACTION: REPLACED #10 TO #12 CYLINDER EXHAUST AND #11 TO #13 EXHAUST DUE TO BURN THROUGH. EXHAUST WAS BLOWING ON FIRE DETECTOR.Feb 28, 2003 · N43872 · Doug DC6SDR DHL2003748002Tail Cone1) #1 ENGINE TAIL CONE HAS APPROXIMATELY 1" X 1" HOLE.2) TRANSFERRED TO LOG PAGE 338263, ITEM 15M.3) REF. N/R 21A: #1 ENGINE TAIL CONE HAS APPROXIMATELY 1" X 1" HOLE.4) REMOVED #1 ENGINE TAIL CONE. ITEM PLACED ON DEFERRAL PER DHL MEL/CDL 78-30-4, CONTROL #Feb 26, 2003 · N748DH · Boeing 727225SDR MEX2002379Exhaust Stack · damagedFLT 6571 - MEX - DURING TRANSIT DETECTED DAMAGES AT THE EXHAUST AREA OF THE LT ENGINE. AIRCRAFT WAS SENT TO THE HANGAR. LT ENGINE WAS REPLACED IAW MM 71-00-02, OPERATIONAL TESTS WERE PERFORMED IAW MM 71-0-01, ALL CORRECT. (M)Dec 25, 2002 · N161PL · Doug MD88SDR 2003F00344Exhaust Stack · looseON A REPOSITIONING FLIGHT FROM PBI-FPR, AFTER TAKEOFF APPROX 500 FT PILOT REPORTED A LEFT ENGINE FIRE INDICATION. WITH POWER REDUCTION THE LIGHT WENT OUT. AIRCRAFT RETURNED TO PBI. LANDED WITHOUT INCIDENT. INVESTIGATION BY MYI MAINTENANCE DETERMINED NR 2 CDec 10, 2002 · N42MY · Gruman G111SDR DLM11021248Switch · failedNR 1 ENGINE THRUST REVERSER UNLOCK LIGHT ILLUMINATED ON CLIMBOUT. REPLACED LOWER OUTBOARD THRUST REVERSER LOCK ACTUATOR SWITCH.Oct 27, 2002 · N814DE · Doug MD11SDR VJ32002F00062Clamp · crackedDURING PROGRESSIVE INSPECTION FOUND CLAMP CRACKED AND ROLL RIVET SHEARED OFF. PROBABLE CAUSE IS ENGINE VIBRATION.Aug 16, 2002 · N861AF · Grob G120ASDR HEEA080284Duct · crackedBLEED AIR DUCT IS CRACKED. REPLACED WITH SERVICEABLE PART.Jun 27, 2002 · N6603X · Bell 206L3SDR HEEA079921Cover · crackedEXHAUST COVER CRACKED. REPLACED WITH SERVICEABLE PART.Jun 25, 2002 · N911MJ · Skrsky S76ASDR HEEA079997Duct · crackedDUCT ASSY CRACKED AT SEAM.Jun 10, 2002 · N724PH · Bell 407SDR RAIAOO206170Stop5529-STL- DURING TAXI LEFT ENGINE OVERHEAT LIGHT ILLUMINATED. MAINTENANCE REMOVED AND REPLACED THE #! ENGINE EXHAUST PIPE STOP PLATES.Jun 2, 2002 · N571HK · Jetair JETSTM4101SDR HEEA078258Tube · wornEXHAUST TUBE BEARINGS WORN.Mar 13, 2002 · Bell 412SDR HEEA078257Tube · wornEXHAUST TUBE BEARINGS WORN.Mar 13, 2002 · Bell 412SDR CA020226002Muffler · cracked(CAN) FOUND DURING AD CF90-03R2 MUFFLER INSPECTION. CRACK FOUND AT BASE OF TAIL PIPE TO MUFFLER CAN CONNECTION. (ALONG WELD BEAD.)MUFFLER REPLACED IN ACCORDANCE ADCF90-03R2. PART 1 SUB PART 5.Feb 26, 2002 · Cessna 172MSDR COMA0260074Thrust ReverserFLIGHT 6013 R/H REVERSER UNLOCK MESSAGE DURING T/O.DEFERRED MAINT. PER M.E.L.Jan 29, 2002 · N940CA · Cndair CL6002B19SDR C1HA200292002Switch#1 ENGINE THRUST REVERSER OPERATING ANNUNCIATOR CAME ON IN CRUISE AND REMAINED ON FOR DURATION OF FLIGHT. ACTION TAKEN: REMOVED AND REPLACED #1 ENGINE THRUST REVERSER SWITCH SYSTEM CHECKS GOOD ON THE GROUND IAW MM 78-30-00.Jan 21, 2002 · N292AS · Boeing 727212SDR HEEA076977Tube · wornWORN BEARINGS. REPLACED WITH SERVICEABLE TUBE ASSY.Oct 31, 2001 · N1202T · Bell 412SDR RAIA00109012Exhaust Pipe5409-STR-FIRE WARNING INDICATION,LEFT HAND ENGINE. MAINTENANCE INSPECTED AND FOUND NO EVIDENCE OF FIRE.IDENTIFIED JET PIPE INSULATION DETERIORATED. REMOVED AND REPLACED LEFT HAND JET PIPE.Sep 23, 2001 · N559HK · Jetair JETSTM4101SDR RRXA11199Skin · puncturedDURING A MAINTENANCE VISIT FOUND PUNCTURE DAMAGE TO #1 ENGINE I/B T/R COWL INNER HEAT SHIELD, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-May 30, 2001 · N606AL · Doug DC873FSDR AALA20011105Fitting · looseDFW - FLT 1953 - EN ROUTE DFW-SHV, RIGHT ENGINE REVERSER ACCUMULATOR LIGHT ILLUMINATED DURING CLIMB-OUT AND RIGHT HYDRAULIC QUANTITY DECREASED. AIR INTERRUPTED AND RETURNED TO DFW. LANDED WITHOUT INCIDENT. TIGHTENED LOOSE FITTING ON ACCUMULATOR LINE. SYSTEMay 19, 2001 · N400AA · Doug DC982SDR SIMA200109802Warning System · activatedORD - FLT 4097 - ENGINE 2 REV DISAGREE CAUTION CAME ON DURING TAKEOFF ROLL, MEL 7802 OPENED. (M)Apr 8, 2001 · N734EK · Emb EMB135LRSDR CA010213028Bolt · sheared(CAN) MAINTENANCE FOUND THE L/H EXHAUST NOZZLE CRACKED DURING A CHECK INSPECTION. DURING REPLACEMENT OF THE EXHAUST NOZZLE, MAINTENANCE FOUND TWO (OUT OF THREE) DELTA BRACKETS ATTACH BOLTS SHEARED, AT 2 AND 10 OCLOCK POSITION.FAULTY PARTS REPLACED PER AMM.Jan 30, 2001 · Cndair CL6002B19SDR AU001234Gasket · misinstalled(AUS) NR 3 CYLINDER EXHAUST GASKET INCORRECTLY FITTED ON ONLY ONE STUD.DURING TIGHTENING OF THE EXHAUST THE FLANGE CRACKED AS WELL ASTHE WELD BETWEEN THE FLANGE AND THE PIPE. LT MUFFLER BAFFLE PIPEALSO ERODED.Dec 29, 2000 · Cessna 150FSDR B3OR20010001Boot Assembly · small cutsThis aircraft has an electronic carbon monoxide detector. In cruise flight, the detector registered a reading of 98 ppm CO. OSHA limits exposure to 50 ppm in normal circustances, avation sources suggest a much more conservative 10 to 20 ppm due to the elevatedDec 6, 2000 · N9403Y · Cessna T210NSDR AALA20001712Nut · leakingDFW - FLT 2468 - EN ROUTE SJC-DFW, UPON ARRIVAL TAXIING TO GATE WITH BOTH ENGINES RUNNING, FLIGHT ATTENDANT REPORTED SMOKE IN CABIN. APU WAS IMMEDIATELY SHUT DOWN. SMELL CEASED. CABIN EMERGENCY CHECKLIST FOR SMOKE WAS FOLLOWED. ARRIVED AT GATE WITHOUT FURTOct 15, 2000 · N452AA · Doug DC982SDR 20001012SH026Heat Shield · failedEXHAUST HEAT SHIELD FAILED ITS CLAMP ATTACH TABS. SUBMITTER STATED THIS CONDITION COULD BE CONSIDERED SERIOUS IN THE EVENT A PART FAILS AND BECOMES LOOSE IN THE ENGINE COMPARTMENT. (X)Aug 14, 2000 · N13PR · Rhnflu EA300LSDR DL757001429Engine · damagedA/C 642 HAD A NR 1 ENGINE TAILPIPE FIRE. RAMP DISCOVERED AND REPORTED FIRE AT AROUND 1350M WHILE DOING ROUTINE ARRIVAL WALKAROUND INSPECTION FOR INBOUND DAMAGE TO A/C. MAINTENANCE AND AIRPORT FIRE DEPARTMENT INFORMED. FIRE DEPARTMENT EXTINGUISHED FIRE AFTERJul 29, 2000 · N642DL · Boeing 757232SDR SIMA2093Switch · malfunctionedBOS - FLT 5172 - DURING TAKEOFF ROLL, CREW NOTED NR 2 THRUST REVERSER DISAGREE MESSAGE. ABORTED TAKEOFF AND RETURNED TO GATE. NO FURTHER INCIDENTS REPORTED. THRUST REVERSERS PUT ON MEL. MAINTENANCE REMOVED AND REPLACED NR 2 ENGINE STOW TRANSIT MICROSWITCHEJul 27, 2000 · N712AE · Emb EMB145LRSDR 20001016SH004Heat Shield · looseEXHAUST HEAT SHIELD FAILED ITS CLAMP ATTACH TABS. THIS CONDITION COULD BE CONSIDERED SERIOUS IN THE EVENT A PART FAILS AND BECOMES LOOSE IN THE ENGINE COMPARTMENT. (X)Jul 25, 2000 · N278SJ · Rhnflu EA300LSDR CA000511029Trunnion · failed(CAN) ROCKER TRUNNION FAILED, PART RETURNED FOR INVESTIGATION.Mar 10, 2000 · Dhav DHC3SDR CA000306013Manifold · cracked(CAN) PILOT REPORTED NOISE IN ENGINE AS WELL AS FOUL SMELL AROUND AIRCRAFT WHILE ATTEMPTING GROUND RUN. VISUAL INSPECTION SHOWED EXHAUST STACK (NR 3 CYLINDER) CRACKED/SPLIT AT FLANGE.Feb 28, 2000 · Diamon DA20A1SDR 20000619AP004Ring · damagedBWI - DURING PREFLIGHT, FOUND DAMAGE IN THE COLD STREAM AND TAILPIPE ON THE NR 3 ENGINE. A CRACK WAS ALSO FOUND ON NR 1 ENGINE THRUST REVERSER ACCESS PANEL. A/C WAS FERRIED TO IND FOR MAINTENANCE. REPLACED THE NR 1 T/R PANEL. THE NR 3 EXHAUST FAIRING RING Feb 20, 2000 · N163AT · Lkheed 10113853SDR 20000601SH004Header · failedDURING POST-FLIGHT INSPECTION FOUND EXHAUST HEADER BLOW-OUT OCCURRED AT HEAT EXCHANGER SHROUD INSIDE SHROUD AT CROSSOVER PIPE DIRECTING EXHAUST AT FUEL HOSE AND CONTROL. (X)Feb 4, 2000 · N6913A · Piper PA23250SDR 2000ZZZX406Slip Joint · leakingPILOT REPORTED EXHAUST SMELL IN THE COCKPIT. UPON INVEST, FOUND A SLIP JOINT ABOVE AND FWD OF HEATER MUFF ALLOWING EXHAUST TO ENTER HEAT MUFF. AREA HAD EXCESSIVE EXHAUST STAINS AND SCAT HOSE ON INTAKE SIDE OF THE MUFF WAS BRITTLE AND HEAT DAMAGED. FACTORJan 28, 2000 · N32ZA · Zinair CH2000SDR DLL14992515punctured/crackFOUND ON SERVICE CHECK 13, NR 2 ENGINE BLOCKER DOORS AT 1:00 AND 3:00 POSTION DAMAGED. ACTUATING RODS FOR BLOCKER DOORS CAUSED A 3 INCH HOLE IN THE ENGINE EXHAUST NOZZLE AT 1:00 POSITION, AND A 4-5 IN CRACK AT THE 3:00 POSITION. WILL REQUIRE ENGINE CHANGE/EXNov 15, 1999 · N1738D · Lkheed 1011385115SDR CA991007083Nut · disintegrated(CAN) DURING INSPECTION OF EXHAUST DEFLECTOR INSTALLATION, THE NUTS ON THE RETAINER SCREWS WERE FOUND TO BE MISSING. NUTS SUPPLIED ARE NOT CORROSION RESISTANT AND HAD DISINTEGRATED.Sep 29, 1999 · Cessna 208BSDR CA991007079Nut · disintegrated(CAN) DURING INSPECTION OF EXHAUST DEFLECTOR INSTALLATION, THE NUTS ON THE RETAINER SCREWS WERE FOUND TO BE MISSING. NUTS SUPPLIED ARE NOT CORROSION RESISTANT AND HAD DISINTEGRATED.Sep 22, 1999 · Cessna 208BSDR 99ZZZX3178Controller · malfunctionedDURING TAKEOFF ROLL, A LOSS OF MANIFOLD PRESSURE OCCURRED OF APPROXIMTAELY 10 IN HG. TAKEOFF ABORTED WITHOUT INCIDENT. DURING GROUND RUN AND TROUBLESHOOTING, THE PROBLEM WAS DUPLICATED AND DETERMINED TO BE A STICKING WASTEGATE CONTROLLER VALVE. THE CONTROLLJun 22, 1999 · N6491H · Cessna T207ASDR CA990707079Exhaust Pipe · cracked(CAN) THREE CRACKS FOUND ON EXHAUST PIPE, WELD JOINT CRACK MID-FORWARD WHERE MO5 FITS INSIDE. FIRST CRACK ON LEFT SIDE WHERE BOLT THAT HOLDS MO5 HEAT SHIELD ATTACHES.Jun 10, 1999 · Snias AS350BSDR 99ZZZX2234Slip Joint · leakingSLIP JOINT LEAKING ON ENGINE EXHAUST.Apr 28, 1999 · N35ZA · Zinair CH2000SDR 99ZZZX1873Exhaust · loosePILOT NOTICED EXHAUST FUMES IN CABIN. INVESTIGATED AND FOUND NR 1 EXHAUST GASKET BLOWN OUT AND ATTACHING HARDWARE MISSING. NUTS WERE LATER LOCATED IN THE BOTTOM OF ENGINE COWLING. RIGHT HEAT SHROUD HAD SLID DOWN EXHAUST MUFFLER WHICH ALLOWED EXHAUST FUMES TApr 23, 1999 · N182EL · Cessna 182SSDR 99ZZZX1881Clamp · leakingNEW CESSNA WITH 9.0 HOURS. ON ACCEPTANCE INSPECTION, FOUND EXHAUST RISER CLAMPS NOT PROPERLY SEATED AND LEAKING EXHAUST. LOOSENED CLAMPS AND EXHAUST RISER FLANGES AT CYLINDER ENDS. ALIGNED AND TIGHTENED CLAMPS, THEN TORQUED RISER FLANGES. EXHAUST CLAMPS SEApr 19, 1999 · N940SP · Cessna 172SSDR 99ZZZX73Support · failedAIRCRAFT EXHAUST SYSTEM FAILED BY RIGHT UPPER CROSS-OVER SLIP JOINT ATTACH POINT. THE SUPPORT BRACKET HARDWARE FAILED ALLOWING JOINT TO SLIP APART WHICH DIRECTED EXHAUST GAS ONTO AIR CONDITIONING LINES RUPTURING LINES AND IGNITING AIR CONDITIONING OIL WHICH CDec 11, 1998 · N9194F · Piper PA46350P
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