JASC 7200
Service difficulty reports · 14,730
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 YADA2021062101Engine · failedINTERNAL ENGINE FAILURE OF RIGHT ENGINE WHILE ON DECENT FOR LANDING - ENGINE REPLACED - O/H FACILITY DID NOT DETERMINE ORIGINAL FAILURESDR YENA2021012900079Engine · fireFLT 1710, PAP-FLL. RETUNRED TO FIELD. EMERGENCY DECLARED. ENGINE 2 FIRE, HI EGT TEMP, BOTH FIRE BOTTLES USED. ENGINE 2 WAS SHUTDOWN AND QRH S-4 WAS ACCOMPLISHED. SUPPLEMENTAL INFORMATION TO FOLLOW.SDR ANCF20210127008Engine · failedN422AV FLIGHT 9331 CLO-BOG. DURING ENGINE NR 2 START APPEARS SPARKS OBSERVED Y GROUND PERSONNEL. CORRECTIVE ACTION: IN ACCORDANCE WITH AMM 80-11-10 PB 401, THE PNEUMATIC STARTER WAS REPLACED, AND AMM 80-11-20 PB 401 THE STARTER SHUTOFF VALVE WAS REPLACED. ESDR JJBA20210123024Engine · failedENGINE 2 FAILED AND SHUT DOWN ON CLIMB OUT. INSTALLED REPLACEMENT NR 2 ENGINE. OPERATIONS AND LEAK CHECK SATISFACTORY.SDR ASMF202104001Engine · making metalDURING OVERNIGHT CHECK AT MEX STATION, IT WAS DETECTED THE MESSAGE IN EICAS AND STATUS OF ENG OIL DMS L. MAINTENANCE PERSONNEL PERFORMED A REVISION, CONFIRMING THE MESSAGE IN EICAS AND STATUS OF ENG OIL DMS; SO THE DEBRIS MONITORING SYSTEM SENSOR DETAILED INSPSDR CALA2021012200073Engine · vibrationNUMBER 2 ENGINE VIB 3.8 AFTER TALKING TO THE FLIGHT CREW CREW REPORTS NUMBER TWO ENGINE VIBRATION WAS BETWEEN 3.4 AND 3.8 AT CRUISE ALTITUDE. DURING DESCENT AT LOWER ALTITUDES NUMBER TWO ENGINE VIBRATION DROPPED TO 2.4 TO 2.8 AFTER LANDING WITH NUMBER TWO ENGSDR P5CA2021012200020Engine · damagedOIL FOUND IN RT EXHAUST CONE AND SPINNER DAMAGED. RT ENGINE CHANGE COMPLETE, IAW WORK CARD A-71-999-09-02. ENGINE RUNS ARE GOOD AT THIS TIME.SDR FDEA202101190153Attach Bracket · gougedNR 2 ENGINE STARTER DUCT SUPPORT LINK ATTACH BRACKET ON THE ENGINE SIDE IS GOUGED AT THE 3 O'CLOCK POS (OUTBOARD SIDE). REMOVED AND REPLACED NR 2 ENGINE LINK ATTACH BRACKET ON THE ENGINE SIDE AT THE 3 O'CLOCK POSITION, IAW B757 SRM 51-40-02 AND AMM 70-50-00, SDR I5VA202101190001Engine · shutdownAT FL410 IN CRUISE FLIGHT, CREW EXPERIENCED A LOUD "BANG" FROM THE NR 2 RIGHT ENGINE FOLLOWED BY INCREASING ITT AND VIBRATION. CREW ADVISED ATC OF THE SITUATION AND REQUESTED A LOWER ALTITUDE. DURING THE DECENT THERE WAS A SMELL OF JET FUEL. AT THAT POINT TSDR I5PA2021011568804Chip Detector · damagedRT ENGINE MASTER MAGNETIC CHIP DETECTOR HOUSING DAMAGED. CORRECTIVE ACTION: REMOVED AND REPLACED RT ENGINE MCD HOUSING, IAW AMM 79-21-10. LEAK CHECK OK.SDR 2021FA0000057Engine · vibratesCLIMBING THROUGH FLIGHT LEVEL 350 WE NOTICED A VIBRATION FOLLOWED BY A RISE IN ITT AND AN “ENGINE VIB” EICAS MESSAGE. PER THE QRH, WE SECURED THE ENGINE VIA PRECAUTIONARY SHUT DOWN CHECKLIST. WE LANDED WITH NO FURTHER INCIDENT. THE ENGINE HAS BEEN REMOVED ASDR CALA2021011100037Engine · stalledSTALL DISPLAYED ON UPPER ECAM SCREEN DURING CLIMB OR CRUISE ACCELERATION. ENGINE NOT SHUTDOWN. ENGINE 2 APPROXIMATELY 3000 FT ON DEPT FELT MINOR THRUST REDUCTION FOLLOWED BY ENG 2 STALL ECAM, ECAM CLEARED AND TH REF TO TSM TASK:71-00-00-810-809-A SURGE OR STSDR ASAA2021011033871Fault Code · activated#2 ENGINE LONG TIME FAULT. THE T3 SIGNAL IS OUT OF RANGE. MSG NBR: 75-20832. DEFERRED PER T/C 78273000. GROUNDED - YES. NO RECENT OR IN FLT FAULT HISTORY ON EEC BITE. INPUT MONITORING PAGE SHOWS HALF DEGREE DIFFERENCE BETWEEN CH A & CH B FOR T3 SENSOR. NO HISTSDR AALA202101139012Engine · overtempAIRCRAFT WAS GROUNDED: FLIGHT CREW REPORTED AND #2 ENGINE EGT INDICATION WAS ABOVE THE RED FOR 10 SECONDS. THE AIRCRAFT YAWED MOMENTARILY WITH A BUMP SOUND / POSSIBLE ENGINE STALL OCCURRED.THE CRW DECLARED AN EMERGENCY AND RETURNED TO SJU WHERE IT LANDED SAFELSDR UIEA2021011100028Engine · odorON CLIMBOUT & DESCENT WE OBSERVED A VERY STRONG FUME ODOR (DIRTY SOCK SMELL). CARRIED OUT CHAPTER 5 CONDITIONAL INSPECTION FOR FUMES IN THE CABIN, PER AMM 05-51-56. FUMES SMELL DETERMINED TO BE COMING FROM RT ENGINE. REMOVED AND REPLACED NR 2 ENGINE ASSEMBLSDR SWIA202155051Engine · fluctuatesLARGE N1 FLUCTUATIONS AT HIGH POWER SETTINGS AFTER TAKEOFF. ERRATIC FUEL FLOW, POWER FLUCTUATIONS COULD BE FELT. RETURNED TO FIELD. MEL 76-11-1 CAT: C DUE: 14JAN2021. LARGE N1 FLUCTUATIONS AT HIGH POWER SETTINGS AFTER TAKEOFF. ERRATIC FUEL FLOW, POWER FLUSDR HNAA2021010500006Engine · shutdownENGINE NR 2 SHUTDOWN IN FLIGHT (NO ABNORMAL INDICATIONS PRIOR TO SHUTDOWN). ENGINE IS BEING R&R'D CURRENTLY IN BDL.SDR ASMF202101018Engine · damagedCAPTAIN REPORTED THAT DURING TAKEOFF ROLL TO V1 AT 100 KTS BY FAILURE OF LEFT ENGINE, DERIVED FROM THE ABOVE ABORTED TAKEOFF. MAINTENANCE PERSONNEL PERFORMED A HIGH ENERGY STOP CONDITIONAL INSPECTION, IAW AMM B787 05-51-14-01A-280A. A BIRD STRIKE CONDITIONALSDR AMCR20210108Bearing · destroyedSHORTLY AFTER OUR INITIAL DESCENT FROM CRUISE ALTITUDE, DESCENDING THROUGH ABOUT 37,000 FEET, WE EXPERIENCED A LOUD, HIGH FREQUENCY VIBRATION. WHILE ADJUSTING THRUST IN ORDER TO DETERMINE THE CAUSE OF THE VIBRATION, WE NOTICED INCREASING ITT ON THE RIGHT ENGISDR IPXA2020123063953Engine · flamed outINSPECTION TYPE: N/A DURING TAXI, NR 2 ENGINE FLAMED OUT, ALL ENGINE PARAMETER ROLLED BACK. NO FCC FAULTS ON ECU 2A ON 2B FAULTS, PER FON MTS NORMAL START, PER MD11 AMM 71-00-00. OPERATIONS TEST GOOD AT THIS TIME.SDR DALA2020122804309Engine · failedTHE FLIGHT RETUNED TO CUN AND AN UNEVENTFUL SINGLE ENGINE LANDING. THE NR 1 ENGINE STALLED AND FAILURE SHORTLY AFTER TAKE-OFF. THE FLIGHT CREW HEARD THE LEFT ENGINE POPPING AND FELT A SHUDDER DURING THE CLIMB OUT. THIS WAS ACCOMPANIED BY ENGINE PARAMETERS RSDR N6WA2020122601Engine · flamed outRT ENGINE FLAME OUT TWICE IN FLIGHT. PERFORMED INSPECTION OF RT ENGINE FOR ITT EXCEEDANCE MESSAGE ON EICAS, IAW CRJ FIM TASK 72-00-00 REFER TO LOG PG 494489 DISCREPANCY FOR WORK DONE. R & R NR 2 ENGINE, IAW CRJ550 AMM 71-00-00SDR SWAA2020122938762Engine · surgesCLIMBING THROUGH 21K SLIGHT SOUND/BUMP ON LEFT SIDE. EGT ON NR 1 WENT TO 900 DEGREES, BUT WAS PULLED BACK BEFORE REF LIMITATION. CRUISED AT 260 WITH EGT APPROXIMATELY 100 DEGREES HIGHER ON NR 1 (COMPARED TO NR 2) WITH THROTTLE ALIGNED. NO OTHER MAJOR INDICASDR ASAA2020122533766Bracket · looseDURING J9 HARNESS CHANGE, FOUND BRACKET THAT HOLDS J9 TO 3 O'CLOCK STRUT LOOSE UNDER RIVETS. GROUNDED-YES. REMOVED AND REPLACED BRACKET AND FASTENERS, BRACKET IS SECURE IN PLACE, REF B737-800 SRM 51-40-02. NO OTHER DEFECTS NOTED.SDR M3XA20201222007Turbine · overtempPILOT PERFORMED A PL WITH A PATIENT ON BOARD FOR AN MGT EXCEEDANCE INDICATION ILLUMINATED DURING FLIGHT. PATIENT WAS TRANSPORTED BY GROUND. INSTRUMENTS DOWNLOADED AND REVEALED A PEAK OF 737 DEG TEMP EXCEEDANCE. ENGINE INSPECTED IAW ENGINE INSPECTION TABLESDR AALA202012229016Engine · stalledAIRCRAFT WAS GROUNDED. "ENG1 STALL" ECAM, FL380 CLEAR AIR LIGHT TURBULENCE. ENGINE RECOVERED BEFORE ECAM COULD BE ACTED ON. OPERATIONS NORMAL FOR REST OF FLIGHT. ACCOMPLISHED TSM TASK 73-00-00-810-866-A, NO DISCREPANCIES NOTED. PERFORMED A SATISFACTORY POSDR SWAA2020122237928Frame · damagedON CLIMB AT MAX POWER NR 1 ENGINE EGT CLIMBED RAPIDLY, 912 DEGREES C MAX NOTED. REDUCED THRUST, EGT DECREASED. NR 1 ENGINE EDT 708-90 DEGREES C HIGHER THAN NR 2 ENGINE. ALL OTHER INDICATIONS NORMAL. COMPLIED WITH MTSI DIS NR/JO 10813 & MTSI DIS NR/JO 10832SDR SWAA2020122238141Bearing · damagedON CLIMB AT MAX POWER NR 1 ENGINE EGT CLIMBED RAPIDLY, 912 DEGREES C MAX NOTED. REDUCED THRUST, EGT DECREASED. NR 1 ENGINE EDT 708-90 DEGREES C HIGHER THAN NR 2 ENGINE. ALL OTHER INDICATIONS NORMAL. COMPLIED WITH MTSI DIS NR/JO 10813 & MTSI DIS NR/JO 10832SDR DALA2020122104181Engine · contaminatedWE EXPERIENCED FUMES SMELL IN THE FLIGHT DECK DURING ENGINE START AFTER DEICING. T/S PER A220 JIC 0550-2001. FOUND SOURCE TO BE DEICING FLUID OF NR 2 ENGINE. ACCOMPLISHED ELIMINATION OF ODOR, IAW A220 EFIM SOLUTION 1-9264. ALL NO GO ODI PROCEDURES C/W. NOSDR SWAA2020122137210Engine · power lossNR 1 ENGINE N1 ROLLED BACK APPROX 15% AT CRUISE AND THEN RECOVERED AFTER 5-7 SECS AND HAD ASSOCIATED GRUMBLING NOISE FOR REMAINDER OF FLIGHT. NO EEC LIGHT AND NO HIGH VIBE IND.SDR UIEA2020121502584Engine · damagedNR 1 ENGINE REQUIRES TO REMOVE BLADES FOR FACILITATE REPAIR AND RE-INSTALL AS REQUIRED. REMOVED NR 1 ENGINE BLADES 8EA ,IAW B767 AMM 72-31-02. RE-INSTALLED 8 BLADES, AS PER AMM 72-31-02 ON ENGINE NR 1. PENDING RE-TORQUE POST ENGINE RUN. PERFORMED SPINNER RSDR IPXA2020121463392Engine · failedINSPECTION TYPE: NA ATB-EMERGENCY DECLARED, NO EQUIPMENT USED. A/C WAS TAKEN OUT OF SERVICE. ON DEPARTURE AT 1500' AGL AFTER SELECTING VNAV RT ENGINE N1 ROLLED BACK TO 27% LOUD S RUMBLE IN AIRCRAFT W/POWER LOSS IN RT ENGINE. ENGINE RAN AT IDLE LEFT UNTIL CLSDR YENA2020121700606Engine · vibrationFLT 280, PBI-BOS. RETURNED TO FIELD. ABNORMAL AIRFRAME VIBRATION ON CLIMBOUT THROUGH FL250 UP TO LEVEL OFF AT FL310. ENGINE 2 N1 VIB 1.8, ENGINE 1 N1 BIV .4. FELT MORE LIKE FLT CONTROL FLUTTERING. NO ABNORMAL ECAMS. HYD, FLT CONTROLS READ NORMAL. SUPPLESDR AWKA2020121701Engine · making metalDURING CLIMB OUT FROM OPF, FLIGHT CREW RECEIVED A "CHIP DETECT R" CAS MESSAGE. CREW CONVEYED THEIR SITUATION TO ATC AND REQUESTED REROUTE BACK TO OPF FOR SAFETY AND MAINTENANCE. SOON AFTER, CREW WAS REQUESTED TO DIVERT TO FXE, AND WAS ABLE TO COORDINATE WITHSDR 9WGA2020121234401Compressor · stalledENGINE NR 1 HIGH EGT, COMPRESSOR STALL, VIBRATION. RAN ENGINE LIMIT SURGE/STALL CHECKLIST. SHUTDOWN ENGINE AND RETURNED TO SHV.SDR O9IA20201212530Engine · power lossON TAKE OFF FROM PANC PILOT ROTATED AND AT AN ALTITUDE OF ABOUT 200-300FT, THE LT ENGINE ROLLED BACK ON POWER. ENGINE REMAINED RUNNING AND CREW PULLED POWER BACK AND FEATHERED THE ENGINE. ENGINE REMAINED RUNNING AND ONCE LEVELED OFF AFTER DECLARING A RETURN SDR ASAA2020120933684Actuator · leakingWHILE PERFORMING ETOPS PDC WALK AROUND, FOUND FUEL LEAKING FROM NR 2 ENGINE. GROUNDED-YES. REMOVED AND REPLACED NR 2 ENGINE RT VSV ACTUATOR, IAW B737-800 AMM 75-31-01. OPERATIONS AND LEAK CHECK GOOD.SDR SIMA20201209001Engine · vibrationENGINE 2 LP VIBRATION 4.0 IN FLIGHT. C/A: PERFORMED RT ENGINE FAN BLADES AND PINS-N1 VIB TROUBLESHOOTING, IAW WORK CARD EA72-00-00-012. OPERATIONAL CHECK GOOD.SDR I5EA2020120900003Engine · power lossNR 1 ENGINE, N1 ROLLBACK, UNCOMMANDED IN FLIGHT.SDR HALA2020120800216Engine · failedATB-RT ENGINE COMP STALL RT ENGINE OIL PRESS 0. REMOVED & REPLACED #2 ENG PER W/O 181624 REF TASK CARD E1128-717-72-003-INSTALL OPS/LEAK CHECK OK.SDR FDEA202012053040None · failedCLIMBING THRU 14000 ON DEPARTURE OUT OF KORF #2 ENGINE SLEZED EPR ROLLED BACK TO 0, NI INDICATED 13.5 % N2 WAS 0 ,EGT SPIKED TO 790 DEG, LOW OIL PRESS LIGHT ILLIMINATED. DIVIERTED TO KRIC AFTER DECLIARING EMERGENCY. #2 ENGINE REPLACEMENT.SDR QXEA2020120400336Shutoff Valve · malfunctionedREJECTED TAKEOFF DUE TO NR 1 BLEED HOT CAUTION LIGHT ON TAKEOFF ROLL. NR 2 BLEED HOT CAUTION SHORTLY AFTER CLEARING RUNWAY, RAN CHECKLIST. CAUTION LIGHTS CLEARED. BLEED FLOW SELECTOR WAS IN "MIN" DUCT & CABIN TEMPS APPEARED TO BE NORMAL. TAKEOFF REJECTED BSDR UIEA2020113002494Seal · deterioratedNR 2 ENGINE DRAIN MAST PROTECTOR SEAL IS DETERIORATED. REPAIRED DETERIORATED FIRE INSULATION AT NR 2 ENGINE DRAIN MAST, IAW B767-3 AMM 78-31-01.SDR FDEA202011282983Engine · failedPASSING THROUGH APPROX 1000 FEET DURING INITIAL CLIMB OUT AIRCRAFT BEGAN TO LURCH ACCOMPANIED BY A LOUD BANGING NOISE. THIS A/C WAS PREVIOUSLY WRITTEN UP AFTER A REJECTED T/O DUE TO THE NR 3 ENGINE COMPRESSOR STALLING. THE CREW INITIATED A SHUTDOWN OF THE NRSDR 2020F00473Egt Indication · illuminatedQRF TO CBB, ENGINE LT ON TAKEOFF EGT REACHES 953°C DURING 30 SECS APPROXIMATELY. CORRECTIVE ACTION: AFTER TURNBACK WAS PERFORMED EGT EXCEEDANCE INSPECTION, IAW AMM TASK 72-00-00-216-0602(B). PERFORMED EGT TRIM BOX THERMOCOUPLE HARNESS AND PROBE SYSTEM TEST. SDR UIEA2020113002474Engine · power lossBELOW 5000 ON ARRIVAL AMBER IDLE DISAGREE MESSAGE DISRUPTED LT ENGINE WAS 28% WHEN RT ENGINE WAS 40%. PERFORMED LT & RT ENGINE PIMU BITE PROCEDURE 71-01-01 FT 810. NO FAULTS ON EITHER PIMU BITE. NO IDLE DISAGREE MESSAGE DISPLAYED NO FAULTS AT THIS TIME.SDR UIEA2020112202436Acoustic Liner · tornNR 1 ENGINE ACOUSTIC PANEL HAS TEAR, REQUIRES REPAIR OR REPLACEMENT LOCATED AT 5 O'CLOCK POSITION. REMOVED AND REPLACED DAMAGED ACOUSTICAL PANEL LINER AT NR 1 ENGINE BY 5 O'CLOCK POSITION, PER B767-300 AMM 72-33-01-009-001-H00, AMM 72-33-01-404-011-H00.SDR MTNA20201120001Engine · failedWHILE CLIMBING THROUGH 16,000 FEET NR 1 ENGINE FAILED WITH A LOSS OF OIL PRESSURE INDICATED ON THE INDICATOR AND LOW OIL PRESSURE WARNING AND UNABLE TO FEATHER ENGINE. THE ENGINE WAS MANUALLY SHUT DOWN AND AN EMERGENCY WAS DECLARED. THE AIRCRAFT RETURNED TO SDR 9JLA2020120824759Engine · inoperativeA FLIGHT WAS CANCELLED DUE TO THE CREW NOT BEING ABLE TO START THE NR 1 ENGINE. THE MAINTENANCE TEAM TROUBLESHOT, BUT WAS UNABLE TO DUPLICATE THE DISCREPANCY. AS A PRECAUTIONARY MEASURE THE STARTER DISENGAGE SWITCH WAS CLEANED. OPERATIONAL CHECKS WERE SATISSDR A6WA202011167424Engine · overheatedCLIMBING THROUGH 7000 RH ENG ITT 888 FLASH RED AT N1 87% AFTER APPROXIMATELY 10 SEC HEARD BANG AND SHUTTER. A/C YAWED AS RH, ENG POWER REDUCED. ACCOMPLISHED ENG SHUTDOWN. ***AIRCRAFT REMOVED FROM SERVICE*** REPLACED R/H ENGINE S/N 872452 OFF WITH S/N 87230
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