JASC 7200
Service difficulty reports · 14,726
Reports filed under 7200 · Engine (Turbine/Turboprop), 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 = '7200' 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 = '7200' 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 SWAA2026083151036Engine · fireUPON POST FLIGHT WALK AROUND, 5 MINUTES AFTER SHUTDOWN, FLAMES WERE OBSERVED INSIDE ENG#2 EXHAUST NOZZLE. EVENTUALLY, FLAMES WENT OUT BY THEMSELVES._ 02 - INSPECTED PER [AMM 71-00-00-800-803-F00-NG (INSPECTION AFTER AN ENGINE FIRE USE OF FIRE EXTINGUISHING AGESDR AALA202608277604Engine · vibrationAIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED AND THE AIRCRAFT DIVERTED TO AUS DUE TO THE FLIGHT CREW REPORTING THAT POSITION 1 ENGINE HAD VIBRATIONS AND STALLED AFTER LEVELING AT CRUISE -THE FLIGHT CREW REPORTED THAT THE ENGINE WAS STUCK AROUND 50% N1 AND SDR TAMF20260826059Engine · vibrationAIRCRAFT N334QT, WHILE IN CRUISE ON THE BOG-SAP ROUTE, EXPERIENCED A HIGH ENGINE NO. 1 VIBRATION INDICATION. AS A PRECAUTIONARY MEASURE, THE FLIGHT CREW DECIDED TO DIVERT AND LAND AT SAL, EL SALVADOR. PERFORMED RELUBRICATION OF THE ENGINE LP COMPRESSOR BLADESSDR DALA2026082504818Engine · making metalDIVERTED TO YYT DUE TO MULTIPLE LEFT ENGINE STALLS. FOUND METAL IN THE TAILPIPE. REPLACED NR 1 ENGINE. OK FOR SERVICE. (8817440) AIRCRAFT WAS GROUNDED.SDR GCXA2026082600187Engine · overtempDURING TAKE-OFF (TOGA) BOTH ENGINES OVERHEATED UNTIL THRUST REDUCTION ENG 1 REACH 973DEG C, ENG 2 REACH 965DEG C.SDR 2026F00182Engine · vibrationATB - AFTER TAKEOFF, ENGINE 1 EXPERIENCED INCREASES IN EGT, WF, ICT, AND LPR; DECREASES IN N2, CET, AND TER; INCREASED N2 VIBRATION LEVELS; AND DECREASED EGTM. INITIAL BORESCOPE INSPECTION FOUND MATERIAL LOSS AND DAMAGE IN THE HPT AND COMBUSTION CHAMBER; TROUBSDR 2026FA0000663Engine · vibrationATB - AFTER TAKEOFF, ENGINE 1 EXPERIENCED INCREASES IN EGT, WF, ICT, AND LPR; DECREASES IN N2, CET, AND TER; INCREASED N2 VIBRATION LEVELS; AND DECREASED EGTM. INITIAL BORESCOPE INSPECTION FOUND MATERIAL LOSS AND DAMAGE IN THE HPT AND COMBUSTION CHAMBER; TROUBSDR DALA2026082404801Engine · failedIFSD/ATB/DE - DUE TO RIGHT ENGINE FAILURE SHORTLY AFTER TAKEOFF. FOUND METAL IN THE TAILPIPE, REPLACED ENGINE. (9587390) AIRCRAFT WAS GROUNDEDSDR DXTA2026082409378Engine · unknownAT ABOUT 200-300 FT AGL ON TAKEOFF, TOWER INFORMED SAW SMOKE COMING FROM ONE ENG. DEPARTED RUNWAY 12 AT KTUS WHICH PUT RT ENG ON TOWER SIDE, BUT TOWER COULD NOT TELL WHICH ENG SMOKE COMING FROM. THEY ALSO DID NOT DESCRIBE THE SMOKE IN ANY MANNER. RETURNED TSDR JTAA20260821001Engine · making metalNR 2 ENGINE FAILED IN FLIGHT. ON INSPECTION FOUND METAL PARTICLES IN OIL FILTER BOWL.SDR CALA2026082318809Engine · odorDIRTY SOCK ODOR COMING FROM PACKS WHEN ON ENGINE. CAN SMELL IN FLIGHT DECK AND CABIN. REF AMM 05-51-26-800-801-C1 SMOKE/ODOR IN FLIGHT DECK (EC0500-01013H). ODOR ONLY OCCURS WHEN ENGINES SUPPLYING PNEUMATICS TO SYSTEM, WHEN SWITCHED TO THE APU THE ODOR DISSIPSDR CALA2026083119059Engine · failedLEFT ENGINE FAILED DURING CLIMB, ENG1 SN. (TSI= , CSI= CYC). CREW REPORTED THAT ENG1 WAS SHUTDOWN DUE TO THICK SMOKE IN THE CABIN (L/P 3038084). OIL PRESS IN RED WHILE IN IDLE. EGT 715, FLIGHT ATTENDANTS REPORTED THAT LEFT ENG WAS SHAKING VIOLENTLY ON THE WINSDR GCXA202608260188Engine · overtempDURING TAKE-OFF BOTH ENGINES 1 & 2 OVERHEATED JUST AFTER ROTATION AND REMAINED OVERHEATED UNTIL THRUST REDUCTION. ENGINE 1 REACHED A MAXIMUM TEMPERATURE OF 965 & ENGINE 2 REACHED A MAXIMUM TEMP OF 955. OVERTEMPTS LASTED APPROXIMATELY 30SEC.SDR 2026FA0000654Engine · faultedON AUGUST 17, 2026, OF AN IFSD EVENT INVOLVING ENGINE 729827, WHICH OCCURRED ON AUGUST 11, 2026. THE CUSTOMER STRONGLY SUSPECTS A BEARING-RELATED ISSUE. A CSC CASE IS CURRENTLY ONGOING FOR THE ANALYSIS OF THE DFDR DATA. THE LAST SV OF THIS ENGINE WAS PERFORMSDR SCNA20260916400Engine · vibrationNUMBER 1 ENGINE VIBRATION AT 3.9 IN CLIMB AND 3.3 DURING CRUISE. PERFORMED VIBRATION SURVEY TEST 7 IAW AMM 71-00-00-00-700-814-F00, HIGH VIBRATION OF 3.1, PERFORMED TEST 14B AVM FAN BALANCE TRIM, REPEAT VIBRATION SURVEY TEST 7, HIGH VIBRATION OF .5 AT T/O POWSDR SWAA2026082066279Engine · failedNR 1 ENG, LOUD BANG DURING CLIMB OUT. REMOVED AND REPLACED NR 1 ENGINE IAW MT 771-00-01 ON TTG8Q006VJKP.SDR 2026FA0000659Engine · bird ingestionAFTER TAKEOFF DURING INITIAL CLIMB BIRD STRIKE TO ENG 2 WITH ENG FAILURE. PERFORM JIC-32S-71-01022 COMPONENT (JOB INSTRUCTION CARD) R MANDATORY: PERFORM JIC-32S-71-01022 COMPONENT (JOB INSTRUCTION CARD) REV. 00. POWER PLANT REMOVAL AND INSTALLATION.SDR JJBA20260819014Engine · failedE1 OUT IN FLIGHT AT FLIGHT LEVEL 300. OCCURRED AT 30000, IT WAS SMOOTH AND THEN SEEMED LIKE TURBULENCE AND #1 ENGINE SHUTDOWN WITH EICAS MESSAGE. ATTEMPTED #1 ENGINE START WITH NO N2 AND NO FUEL FLOW. OIL AT 11 QTS, NORMAL ENGINE VIBRATION AND OIL TEMPS IN THESDR SIMA20260816001Engine · bird ingestionBIRD STRIKE ON TAKEOFF NR 1 ENG FROM KHPN. HIGH VIBRATION ON CLIMB AS WELL AS APPROACH BACK INTO KHPN. EMERGENCY DECLARED. PERFORMED BIRD STRIKE W/C INSPECTION PER ENVOY W/C EA05-50-200-801A. ON ENG NR 1 FOUND BLADE DEFORMATION TO BE OUT OF LIMIT SEE LOG PG 1SDR SWAA2026081981735Plate · cracked#1 ENG #7 DEFLECTOR PLATE HAS A RADIAL CRACK IN AREA A WITH LENGTH MEASUREMENT OF 0.517 FROM CENTER TO EDGE WITH 0.060 REMAINING TO EDGE #1 ENG #7 DEFLECTOR PLATE HAS A RADIAL CRACK IN AREA A WITH LENGTH MEASUREMENT OF 0.517 FROM CENTER TO EDGE WITH 0.060 REMASDR SWAA2026081991721Plate · crackedNR 1 ENGINE, NR 17 DEFLECTOR PLATE HAS A RADIAL CRACK IN AREA, LENGTH MEASUREMENT OF 0.426, & REMAINING EDGE MEASUREMENT OF 0.062 NR 1 ENG, NR 17 DEFLECTOR PLATE HAS A RADIAL CRACK IN AREA A WITH LENGTH MEASUREMENT OF 0.426 AND REMAINING EDGE MEASUREMENT OF SDR SWAA2026081973499Engine · no discrepancyOTS, NR 1 ENGINE SLOW TO SPOOL ON TAKE OFF ROLL, ABORTED AT 40 KTS. ACCOMPLISHED FDR DOWNLOAD AND UPLOADED FOR POWERPLANT ENGINEERING. IAW MM 31-31-00. ACCOMPLISHED ACCELLERATION TEST 8 PER MM 71-00-00, WITHIN ALLOWABLE LIMITS. ACCOMPLISHED POWER ASSURANCE SDR SWAA2026081812205Engine · stalled#2 ENGINE STALL/STAG ON T/O AT APPROXIMATELY 600. ENGINE RECOVERED ABOVE IDLE THRUST. STALL/STAG AGAIN AT ABOUT 60% N1. RECOVERED WHEN RETARDED AND REMAINED THERE FOR REMAINDER OF FLIGHT. #2 ENGINE STALL/STAG ON T/O AT APPROXIMATELY 600. ENGINE RECOVERED ABOVESDR 2026FA0000640Engine · bird ingestionMASTER WARNING FOLLOWED BY LOSS OF OIL PRESSURE. ENGINE SHUT DOWN AND RETURNED TO KCCO. DISCOVERED BIRD STRIKE AND BENT FAN BLADES AFTER LANDINGSDR DALA2026090204961Engine · contaminatedATB / DE - DUE TO REPORT OF BURNING RUBBER/SMOKE ODOR IN THE AFT CABIN AND COCKPIT AFTER LIFTOFF. NO TROUBLE FOUND. PERFORMED LEVEL A DECONTAMINATION. POSSIBLE RESIDUE DUE TO ENGINE FOAM WASH DURING PREVIOUS RON MAINTENANCE VISIT.SDR DXTA2026081709313Engine · malfunctionedON OUR DESCENT OUT OF FL390 WHILE DECREASING POWER, GOT A VIBRATION OUT OF RT ENG, FOLLOWED BY RT ENG ROLLING BACK. SHORTLY AFTER, RECEIVED AN ENG SHUTDOWN R CYAN MESSAGE. AFTER ABOUT 5 - 10 SECS, RT ENGINE STARTED RELIGHTING ITSELF, & STABILIZED TO NORMAL SSDR CALA2026081718690Engine · faultedBLEED TRIP OFF LIGHT CAME ON DURING CLIMB, NO RESET WITH QRH. FOUND FITTING TO BLANKING CAP LOOSE ON BAR WITH MINOR LEAKAGE. SECURED, NO FURTHER LEAKS. DUE TO SHOP HISTORY, SUSPECT HIGH STAGE REGULATOR BAD. REPLACED HIGH STAGE REGULATOR AS PRECAUTION IAW SDR UIEA2026081200747Engine · faultedENGINE 2 OIL TEMP INFLIGHT. ENG 2 IFS. PERFORMED WINDMILLING INSPECTION & NO TROUBLE FOUND IAW AMM 72-00-00/601. PERFORMED ENG MAG CHIP INSPECTION & NO TROUBLE FOUND IAW AMM 79-00-00/601. R & R NR 2 ENG'S EEC & OPS CHECKED OK IAW AMM 73-21-15/401, AMM 79-34-0SDR G1IA20260810115Warning Message · multiple indHIGH ITT INDICATIONS WITH SUBSEQUENT EIS IND, INCLUDING CAUTION, WARNING & FLASHING ITT TEMP. ITT TEMP INDNS FLUCTUATE BTWN 920 & 960, REGARDLESS OF TORQUE SETTING. NO SECONDARY INDNS IN COCKPIT TO INCLUDE OIL TEMP NORMAL AS WELL AS ALL OTHER ENG INSTS. NO NOTSDR AALA202608118246Probe · faultedAIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED INTO BOS DUE TO THE FLIGHT CREW REPORTING THAT ENGINE 2 IS CREATING SIGNIFICANTLY LESS THRUST THAN ENGINE 1 WHICH WAS CREATING A YAWING MOMENT - THE AIRCRAFT LANDED SAFELY WITHOUT FURTHER INCIDENT. MAINTENANCESDR A6WA202608098906Engine · faultedABORTED T/OFF AT 110 KTS, FLAPS 20, DUE TO A POPPING SOUND AND A/C PULLED TO THE RIGHT, DURING ROLL OUT WITH T/R'S DEPLOYED, NOTICED ITT ON RT ENGINE WAS RED. RETURNED TO NORMAL WHEN RESTOWING T/R'S. (BRAKE TEMP'S 8'S ACROSS THE BRD) AIRCRAFT REMOVED FROM SERSDR CALA2026081418628Circuit Card · faultyRIGHT ENG OVHT EICAS, FL410 EGT SHOWED 587 AFTER ENG BLEED & PACK OFF. THRUST REDUCED. OVERHEAT LIGHT WENT OUT AT 1.39 EGT IAW FIM 26-11 FT 802. R & R AFOLTS CARD M10274, AMM 26-10-01/401.SDR SWAA2026081284224Engine · no discrepancyCREW ABORTED TAKE OFF FOR ASYMMETRICAL ENGINES SPOOL UP, NEVER RETURNED TO GATE OR CONTACTED MOC UNTIL LANDING IN THE NEXT CITY. ENGINE ACCELERATION TEST DUE TO PREVIOUS RTO. PERFORMED ACCELERATION CHECK ON BOTH ENGINES AND NO DEFECTS WERE FOUND IAW AMM 71-00SDR SWAA2026081284582Engine · slowCREW ABORTED TAKE OFF FOR ASYMMETRICAL ENGINES SPOOL UP, NEVER RETURNED TO GATE OR CONTACTED MOC UNTIL LANDING IN THE NEXT CITY. OTS, ENGINE ACCELERATION TEST DUE TO PREVIOUS RTO PERFORMED ACCELERATION CHECK ON BOTH ENGINES, NO DEFECTS FOUND IAW AMM 71-00-00SDR SWAA2026081114863Engine · no discrepancyNR 2 ENGINE SLOW TO SPOOL ON TAKEOFF. EGT 60 SPLIT FROM NR 1 ENGINE. TROUBLESHOT IAW FIM 73-05 TASK 814. PERFORMED TEST 8, ACCELERATION CHECK OF NR 2 ENGINE IAW AMM 71-00-00. TEST PASSED WITH ACCELERATION OF 4.5 SECS. NO EEC FAULTS. NO EGT EXCEEDANCES OBSERSDR VNAA2026081022401Relay · unserviceableL ENG DEGRADED CAUTION IN FLIGHT. REPLACED K19, K21 IAW CRJ 900 AMM 24€“06€“07€“000€“801. FAULT DID NOT REOCCUR. OPS CHECK GOODSDR CALA2026080918416Engine · faultedABORTED ENGINE START ON ENG 2. HUNG START. EGT FLASHING. APROX 270EGT N2 29PCT. OIL ODOR NOTD FOUND POOL OF OIL IN TUBINE EXHAUST AREA, INSPECTED ENGINE FOR DEFECTS, NO FAULTS FOUND. CLEANED OIL FROM TURBINE EXHAUST AREA. ACCOMPLISHED ENGINE RUN IAW AMM 7SDR DALA2026080704580Engine · odorAT 1000' AGL INTO JFK FLIGHT ATTENDANTS CALLED TO REPORT ENTIRE CABIN SMELLED LIKE VINEGAR. UPON LANDING AND CHECKING IN F/A SAID ENTIRE CABIN SMELLED LIKE BURNED TOAST. REPLACED NR 1 ENGINE. (LP 9572982 - AIRCRAFT WAS GROUNDED)SDR SWAA2026081002003Engine · failedNR 1 ENGINE FAILED ON TAKEOFF ROLL. REMOVED AND REPLACED THE NR 1 ENG IAW MT 771-00-01. REF TTG8Q008F2S8.SDR CALA2026080518332Engine · faultyAFTER TAKEOFF AROUND 1200 FT LT ENG STARTED BANGING LOUDLY AND EGT READ 970 BEFORE SHUTDOWN DEBRIEFED FLIGHT CREW-AFTER TAKE-OFF DEPARTURE TURN ENGINE NR 1 EGT CLIMBED TO 970'C AND STALLED. REVIEWED DFDAU STORED REPORTS AND VERIFIED ENGINE NR 1 EGT AT 970'C ASDR UIEA2026080500680Engine · vibrationAIRCRAFT VIBRATION INCREASED WITH POWER ADVANCED. ENG 1 LOCKED OUT AND 3 ENG FERRY TO ICN. AFTER FERRY FLIGHT, INSPECTED A/C CONDITION, ALL CHECK OK. PERF ENG RUN UP CHECK, NO STS MSG & NO FAULT FOUND IAW AMM 71-00-00. R & R NR 1 ENG PER W/O 162878 TASK CARSDR SIMA20260804002Engine · power lossREJECTED T/O DUE TO ASYMMETRIC THRUST. TAKEOFF THRUST WAS SET AT TOGA TO START ROLL. NR 1 THRUST LEVER WAS SUBSEQUENTLY PUSHED THROUGH THE DETENT INADVERTENTLY. TO1 RSV WAS ACTIVATED. THRUST DIFFERENTIAL OF AROUND 7% N1 OBSERVED. DECISION MADE TO REJECT AS PM SDR DALA2026080404485Engine · vibrationDIVERTED TO ATL DUE TO NBR 2 ENGINE VIBES. NR 2 ENG VIBS 1.25 FOR 38 SEC. MAINTENANCE IN PROGRESS.SDR WX0A2026080332912Engine · bird ingestion(AIRCRAFT GROUNDED) (EMERGENCY DECLARED) BIRD STRIKE # 1 ENG HIGH VIBRATION FELT AND HEARD IN CABIN AND ON FLIGHT DECK. MAX VIB WAS 3.6./ TROUBLESHOOTING IN PROGRESS"SDR 5OKA202609150082Cover · separatedHONDAJET N909BP, 42000099, TAXIED OUT ON SUNDAY, AUGUST 2, AND THE LINE SERVICE PERSONNEL FOUND A 7" X 2" CURVED STAINLESS-STEEL PLATE/PIECE WITH P/N - 4JQT4-13121-Q0A-0100 LAYING ON THE GROUND WHERE THE AIRCRAFT HAD PARKED. A SECUITY VIDEO SHOWED AN OBJECT BESDR CALA2026080518299Engine · bird ingestionON TAKE OFF AT ABOUT 500 WE HEARD AND FELT A LOUD BANG. 1 ENGINE EGT GUAGE SPIKED AND WENT COMPLETELY RED. THEN AFTER A FEW MINUTES SECOUNDS ENGINE STABILIZED AND INDICATIONS REMAINED NORMAL. FOUND SMEAR OF POSSIBLE BIRD DEBRIS ON ENGINE 1 SPINNER, NO OTHER SDR 2026FA0000614Housing · damagedTHE ISSUE WAS IDENTIFIED FOLLOWING THE DETECTION OF A SIMILAR DISCREPANCY ON ENGINE 602978 DURING A CONFIGURATION REVIEW. DISCUSSIONS WERE HELD WITH THE INVOLVED DISASSEMBLY INSPECTOR AND A TARGETED REVIEW OF THE INSPECTOR'S RECENT DELIVERIES WAS PERFORMED. THSDR VNAA2026073121902Engine · vibrationRIGHT ENGINE N1 FAN VIB UPTO 2.2 / PERFORMED STIFFNESS CHECK AND VIBE CHECK PER AMM 72-21-02-200-803-A01-PSA AND PPGRM 71-00-00-720-806-A01. NO DEFECTS NOTED.SDR N6WA2026073001Engine · degradedLEFT ENG DEGRADED CAUTION, ITT SPIKED, THRUST REDUCED ON LEFT ENGINE. REMOVED AND REPLACED LT ENG IAW AMM 71-00-00 ALL LEAK & OPS CHKD GOOD.SDR CALA2026073118130Engine · odorNUMBER 1 ENG SMOKING FROM REAR MORE THAN NORMAL. ON EXT INSP STRONG ODOR OF FUMES DISCUSSED WITH CREW. SMOKE AND FUMES FROM TAIL PIPE IS NORMAL OPS AFTER ENGINE SHUTDOWN. NO DEFECTS AT THIS TIME.
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