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.
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
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 UIEA2021042300981Fairing · crackedNO.3 ENG L/H C-DUCT UPPER AFT FIXED FAIRING FOUND CRACK.(<P>#3 ENG L/H C-DUCT UPPER AFT FIXED FAIRING CRACK AREA REPAIRED AS PER CMM 78-32-02 REPAIR 007.</P>)SDR UIEA2021043001026Duct · damagedNO.3 ENG LH C-DUCT FITTING HOLE FOUND ELONGATED REF CMM 78-32-02 REPAIR 020. THE POD SUPPORT FWD BUSHING HOLE MEASURED 1.08" DIA, WHICH HAS EXCEEDES THE MAXIMUM REPAIREABLE LIMIT 0.875" DIA.(<P>THE POD SUPPORT FTG CAN NOT REPLACED AS HAECO DOES NOT HAVE CAPABISDR PAIR41221339Exhaust Mixer · crackedDURING PILOTS PRE-FLIGHT INSPECTION A PORTION OF THE MIXER CASE ASSEMBLY WAS OBSERVED IN THE FAN AIR BYPASS DUCT OF THE RIGHT HAND ENGINE. FURTHER INVESTIGATION DISCOVERED MULTIPLE CRACKS AND MISSING SECTIONS OF THE ASSEMBLY. THE LEFT HAND ENGINE MIXER CASE ASSDR MK1Y20210221022Skin · dentedPRIMARY EXHAUST NOZZLE OUTER SLEEVE SKIN, NR 1 ENGINE, AT 3 O'CLOCK. DURING CONVERSION AT IAI FACILITIES, MAINTENANCE HAS FOUND TWO (2) DENTS ON THE NR 1 ENGINE EXHAUST'S AFT EDGE AT 3 O'CLOCK. THE DENTS ARE OUT OF TOLERANCE DUE TO THEIR AY/Y RATIO AND ALSO SDR YV3R2021011100419Shield · crackedCUSTOMER REPORTED EXHAUST SHIELD ASSEMBLY P/N: D314-1 WAS CRACKED.SDR 2020FA0000132Exhaust Pipe · cracked#2 CYLINDER EXHAUST PIPE RISER CRACKEDSDR CALA2019100701711Fairing · missingPDA 3 RIGHT ENG INBD T-R HINGE BUMP FAIRING IS COMPLETELY MISSING. REF IPC 78-31-51-19 ITEM 45 MFG P/N 315A2325-2SDR V0XD20180514009Baffle · crackedLEFT LOWER TRANSCOWL BAFFLE IS CRACKED. REMOVED AND REPLACED THE BAFFLE IAW SRM 51-42-06.SDR 7C7A201505240050Mount Bracket · crackedCRACK DAMAGE TO I/B TRACK MOUNT IN 2 PLACES. WELDED REPAIR IAW BOMBARDIER RD 8-78-149.SDR USAA2014121000004Unknown · smokePASSENGER REPORTED SEEING BLUE SMOKE OUT TAIL CONE OF NR 2 ENG ON LANDING. ACCOMPLISHED ENG RUN IAW AMM 71-00-00. OPERATIONS TESTED OK, NO FAULTS NOTED. NO SMOKE COMING FROM TAIL CONE. OK TO RETURN TO SERVICE.SDR CA141024018Shroud · broken(CAN) THE SHROUD WAS INSTALLED NEW, 98 HOURS PREVIOUS. BOTH THE BOTTOM CLAMP TABS HAD BROKEN OFF. EXAMINATION SUGGESTED THAT SHARP, BURRED EDGES AND SMALL DENTS AND DEFORMITIES LEFT BY THE FORMING PROCESSES MAY HAVE CONTRIBUTED TO STRESS CRACKING. THE PART ISDR CA140811010Riser · broken(CAN) NR 3 EXHAUST RISER BROKEN OFF AT WELDED JOINT WHERE FLANGE CONNECTS TO CYLINDER HEAD, CAUSING OIL OVERTEMP CONDITION IN FLIGHT.SDR CA140807011Support Bracket · damaged(CAN) AIRCRAFT WAS IN CRUISE CONFIGURATION RETURNING TO BASE. PILOT REPORTED "POPPING SOUND COMING FROM ENGINE". INVESTIGATION DETERMINED THAT THE FOLLOWING EXHAUST PARTS HAD FAILED: SUPPORT BRACKET P/N D41-7806-20-02, MUFFLER BRACE P/N D41-7806-20-01, #2 RISESDR CA140623002Riser · shearedPILOT REPORT A LOUD NOISE FROM ENGINE. ACFT RETURNED AND A VISUAL INSPECTION WAS CARRIED OUT. THE LT AFT EXHAUST RISER WAS FOUND SHEARED IN HALF. RT AFT RISER WAS FOUND WARPED. THE ENGINE HAS HAD PREVIOUS INDICATIONS OF HIGH CHT.SDR CALA2013121393649Gasket · looseGASKET CAME LOOSE ON ENG 2, INBD SIDE, FLT DIVERTED. NR 2 ENG INBD SIDE SEAL BETWEEN CNA & C DUCT LOOSE. ACCOMPLISHED INTERIM REPAIR IAW ECRA 7811-01208.SDR CALA2013120993557Seal · looseRT ENG HAS LOOSE BULB SEAL PROTRUDING FROM INBD FWD OF CNA. SECURED LOOSE SEAL INTO RETAINER TRACK.SDR CALA2013120993535Seal · unsecureNR 2 ENG HAS A LARGE SECTION OF A SEAL NOT PROPERLY CONNECTED TO AFT INBD SECTION, SECURED SEAL.SDR CALA2013100991879Rivet · looseSEVERAL LOOSE RIVETS ON NR 1 ENGINE CNA. REPLACED LOOSE FASTENERS IAW MT 78-001.SDR CALA2013082690765Sealant · missingENGINE 2 TRIM SEALANT LOOSE & PROTRUDING. ENGINE 2 CNA HAS MISSING SEALANT RIGHT HAND SEALANT PLATE 6 O'CLOCK. IAW IPC 78-11-09-81 ITM #100. ACCOMPLISHED INTERIM REPAIR IAW ECRA 7811-01201.SDR HALA2013071000086Warning Light · illuminatedREV R FAULT "UNLOCK" LGT ILLUMNATED DURING T/O ROLL, ABORTED TAKEOFF . OPENSDR A6WA201305084948Frame · crackedRIGHT EXHAUST FAIRING 2ND FRAME FROM FRONT CHAFED & CRACKED. REMOVED AND REPLACED FRAME P/N 228-50181-849 ON RIGHT EXHAUST FAIRING IAW CMM 20-40-11 & 20-42-06.SDR UIEA2013012300026Ring · crackedNR 4 ENG RT 'C' DUCT AFT CASCADE SUPPORT RING FOUND CRACKED AT R8 CASCADE VANE NUT PLATE. REPAIRED AS PER EO 1978A067.SDR UALA2012122807439Strut · damagedTURBINE EXHAUST STRUT AT 11 O'CLOCK POSITION HAS 1.5 INCH CRACK AT BASE. STRUT REPAIRED PER GMM 72-54-01 PG 801 PROCEDURE 'A' AND 'B' ITEM 1-5, PERFORMED BY WELDER.SDR CA121017004Tape · departed(CAN) THE FOLLOWING WAS REPORTED TO MFG: DURING A FLIGHT THE 3M TAPE DEPARTED FROM THE RT EXHAUST EJECTOR AND WRAPPED ITSELF AROUND THE RT HORIZONTAL STABILIZER IN FLIGHT. THE CUSTOMER APPLIED SEVERAL TIME THIS TAPE IAW ASB 429-11-04 AND IT CONTINUES TO COMESDR 2012F00151Exhaust Pipe · crackedREMOVED RT ENGINE FOR O/H AT REQUEST OF OPERATOR. FOUND EXHAUST OVERBOARD PIPE, CRACKED APPROX 80 PERCENT AROUND THE CIRCUMFERENCE OF THE PIPE. FOUND CORRODED RIVETS IN FIREWALL. A NUMBER OF RIVETS WERE MISSING. THE FIREWALL WAS DARKENED WITH WHITE RESIDUESDR 2012F00099Skin · damagedINSPECTION OF THE LT AND RT THRUST REVERSER ASSEMBLIES FOUND THE RT TORQUE BOX SKIN TO HAVE NUMEROUS CRACKS AND 1 LARGE TRIANGULAR PIECE BROKEN OUT, AND THE LT TORQUE BOX TO HAVE CRACKS IN THE SKIN ALONG THE EDGE OF THE INBD BLOCKER DOOR HOUSING. FURTHER INSPSDR UALA2012031201611Precooler · brokenNR 2 ENG FOUND PRECOOLER LOWER AFT WELD BROKEN. REMOVED PRECOOLER NEEDS CLAMPUP BUSHING. INSTALLED NR 2 ENGINE PRECOOLER WITH NEW CLAMP UP BUSHING. ACP PRECOOLER TEST, OPS CHECKED GOOD.SDR UALA2012030901536Rivet · missingNR 2 ENG EXHAUST, UPPER PEN NIB FAIRING HAS 2 MISSING RIVETS ON LT SIDE LOOKING FWD INTO EXHAUST. ABOUT 11 O'CLOCK POSITION. REPLACED MISSING RIVETS PER MT 78-001.SDR UALA2012030901544Band · brokenLEFT SIDE V-BAND BROKEN ON NR 1 ENGINE, PART # IS IN DISPUTE, NEED BOEING VERIFICATION. INSTALLED LT SIDE V-BAND ROBBED. OPS OK CLOSED AND SECURED COWLINGS.SDR UALA2012022000986Fastener · missingENG 1 HAS MISSING RIVET FROM PEN NIB FAIRING RT SIDE: ONE RIVET MISSING. INSTALLED NEW FASTENER IAW MT 78-001.SDR QXEA2012010601462Attach Bracket · wornINSTALLING RT EXHAUST, FOUND AFT SHROUD RT STRUT ATTACH BRACKET WORN. REMOVED DAMAGED BRACKET IAW SRM 51-42-05-02-01. INSTALLED NEW BRACKET IAW SRM 51-40-07-02-01 AND 51-42-05-02-01.SDR UALA2011121906938Strip · damagedNR 2 ENGINE NR 3 GAP STRIP DAMAGED INBD AFT SIDE. REPLACED GAP STRIP.SDR UALA2011121506902Heat Shield · damagedNR 2 ENGINE NR 2 HEAT SHIELD FWD END DAMAGED. NR 2 HEATSHIELD HUNG IN PLACE. NEEDS BOLTS RE-INSTALLED ONE AT A TIME WITH SEALANT APPLIED PER MM PROCEDURES.SDR UIEA2011073100388Structure · crackedDURING WALK AROUND CHECK, MX FOUND 2EA CRACKS AT 7 O'CLOCK POSITION ON THE AFT CENTER BODY ON THE NR 2 ENGINE. 1EA CRACK MEASURING 1.25 INCHES AND 1EA CRACK MEASURING APPROX 1 INCH REF FIGURE 1. DISPOSITION WAS MADE TO STOP DRILL THE CRACKS USING STANDARD PRSDR CA110106008Clamp · wornFOR STC SR01062LA, IT WAS DISCOVERED DURING INSPECTION THAT THERE THE HEAD OF THE TEE BOLT RESTS IN THE BAND CLAMP HAD WORN THROUGH TO THE POINT THAT THE TEE BOLT COULD BECOME DISENGAGED RESULTING POTENTIALLY IN EXHAUST CLAMP PARTS DEPARTING THE AIRCRAFT INTO SDR CA101001005Manifold · fumesALSO APPLIES TO LT MANIFOLD PN 0319738340 AND PREFERRED INJECTOR PN 0319738350 ALL TSN 51.5 EXHAUST FUMES IN CABIN RESULTING IN COMPLAINTS OF SORE THROAT, ITCHY EYES AND HEADACHE. REPLACED ALL COMPONENTS OF THE INJECTION MANIFOLD AND THE PROBLEM WAS CORRECTESDR NSVA201070Cowling · defectiveRIGHT TAIL PIPE HOT CIRCUIT BREAKER POPPED DURING FLIGHT. REMOVED AND REPLACED EXHAUST COWL.SDR ASMF 20081202Control Valve · leakingDURING TRANSIT CHECK, A HYD LEAK ON THE RT ENG WAS DETECTED. MX TIGHTENED HYDRAULIC LINE AND REPLACED AND TESTED THE RT ENG REVERSE CONTROL VALVE IAW AMM 78-31-04, ALL CORRECT.SDR AALA200801754Clamp · leakingTUL INFLIGHT T9610/02JUL. CREW REPORTED TAIL COMPARTMENT HIGH TEMPERATURE INDICATION JUST AFTER TAKEOFF. RETURNED TO TUL AND LANDED WITHOUT INCIDENT. REPLACED LT AUGMENTATION VALVE CLAMP OUTBOARD SIDE. SYSTEM GROUND CHECKED NORMAL OPERATION. (A)SDR AC2A119533Bolt · brokenBOLT BROKEN.SDR ARWA20080104Tail Cone · damagedON POST FLIGHT, FOUND TAIL CONE COWLING DAMAGE ON NR 1 ENGINE. PERFORMED GENERAL AREA INSPECTION AND CHECK PNEU DUCTING FOR CONDITION, NO DAMAGE FOUND. REMOVED AND REPLACED NR 1 ENGINE O/B AFT CORE COWLING IN ACCORDANCE WITH DC-1030 M/M REF 71-13-01.SDR UIEA200700430Cowling · crackedNR 3 ENGINE RIGHT T/R TRANSLATING COWL LOWER FAIRING HAS A CRACK APPROX 3.0 INCHES AT THE FORWARD SECTION AND RIVETS PULLING THROUGH AT THE AFT SECTION. RIVETS REPLACED IAW SRM 51-40-02. AN INTERIM REPAIR WAS DONE TO THE CRACKED FAIRING BY STOP DRILLING AND SDR BUE2007F00002Bolt · sheared( REF NR: 287N416WM) DURING INSPECTION FOUND THE RT EJECTOR OB BEARING FITTING UPPER BOLT SHEARED, LOWER BOLT BENT/BEGINNING TO SHEAR, IB BEARING FITTING UPPER AND LOWER BOLTS BENT/BEGINNING TO SHEAR, AND THE IB AND OB TRANSLATOR LINKS BENT. REPLACED BOTH TRASDR CA070122002Heat Shield · cracked(CAN) DURING A ROUTINE 100 HR ENGINE/AIRFRAME INSPECTION, IT WAS NOTED THAT THE SUBJECT HEAT SHIELD, THAT IS INSTALLED ON THE ENGINE EXHAUST TAILPIPE, WAS FOUND CRACKED. THE CRACK ORIGINATED IN THE DOUBLER AREA WHERE THE FORWARD CLAMP IS ATTACHED. THE CRACK LOSDR HALA0600897Warning Light · illuminatedBTB - "R REV ISLN VAL" CAME ON AFTER STARTING ENGINES. MTX ADVISED TO RETURN TO GATE. RETURNED TO GATE UNDER TOW. ERASED MESSAGE. CYCLED NR 2 ENG REV FAULT STAYED OUT. REF FIM 78-34-00, FIG 111.SDR CA061018001Exhaust Riser · cracked(CAN) THE (EXHAUST) FLANGE WAS CRACKED THROUGH AND INTO THE UPPER END OF THE (EXHAUST) PIPE ITSELF, WITH THE CRACK TRAVELLING ALMOST HALFWAY AROUND THE PIPE. SUBMITTER REGULARLY FINDS THESE RISERS CRACKED AND SUSPECTS THAT A SHARP/ROUGH EDGE ON THE FLANGE COSDR ASMF200606017Engine · failedAIRCRAFT RETURNED TO PLATFORM, (L ENG REV CONT) AND (L ENG PRI CONT) MESSAGES WERE SHOWN IN EICAS. FIM 78-34-00, FIGURE 112 PROCEDURE WAS PERFORMED AND LT ENGINE EXCEDENCIES PAGE WAS VERIFIED SHOWING P PDIU/EEC S PDIU/ S354-29, S354-4 CODES. MESSAGES WERE ERASSDR ASMF200606006Engine · failedAIRCRAFT RETURNED TO PLATFORM, DURING RT ENGINE STARTING (REVERSE) LIGHT TURNED ON. A REVERSE CYCLE WAS PERFORMED, REVERSE BREAKERS WERE RESEATED AND BITE IN REVERSE UNITS WAS PERFORMED, BUT FAIL CONTINUED. RT REVERSE WAS CANCELLED AND DEFERRED IAW MEL 78-1 CSDR SIMA200614605Control Unit · failedLT REVERSER UNSAFE CAUTION MSG ILLUMINATED DURING TAKEOFF ROLL. REPLACED THRUST REVERSER ICU IAW AMM 78-32-09. OPERATIONAL CHECKS GOOD AIRCRAFT RETURNED TO SERVICE. (M)SDR CA060503009Extractor · crackedDURING INSPECTION THE ENGINEER NOTICED A CRACK IN ONE OF THE EXHAUST GAS EXTRACTORS. FURTHER INVESTIGATION ON THE REMAINING EXHAUST GAS EXTRACTORS REVEALED CRACKS AS WELL. THE PARTS WERE REPAIRED AND REINSTALLED.
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