JASC 7200
Service difficulty reports · 14,727
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 2024F00154Bearing · failedAIRCRAFT WAS CLIMBING THROUGH 4000' #2 ENGINE ROLLED BACK AND SHUT DOWN. NO EICAS INDICATION OF PROBLEMS. DECLARED EMERGENCY AND LANDED AT KSVH WITH NO FURTHER INCIDENT. MAINTENANCE REVIEWED CENTRAL MAINTENANCE COMPUTER DATA AND FOUND SINGLE INDICATION OF OILSDR DALA2024062106277Plug · missingSHIP 3273 DISC: DIV - RECEIVED ENG 1 FIRE INDICATION INFLIGHT, RAN QRH & ECAM WHEN THRUST LEVER PLACED AT IDLE WARNING WENT AWAY. LEFT ENGINE AT IDLE AND DIVERTED TO PIB. C/A: FOUND BOROSCOPE PLUG AT 6 O'CLOCK POSITION OFF. REINSTALLED PLUG PER A320 AMM 72-51.SDR ABXA20240617114Engine · unknownWHILE STARTING #2 ENGINE DURING TAXI ,START TEMP RAPIDLY INCREASED AND EXCEEDED EGT START LIMITS(551 MAX) AC RETURNED TO GATE AND MAINTENANCE GROUNDED AC MAINTENANCE PERFORMED FIM 71-08 FAULT TREE 816 CHART AREA F. PERFORMED SECOND ENG START, ENG START WAS SSDR DALA2024061706144Engine · making metalSHIP 3741 -IFSD/ATB- DUE TO RIGHT ENGINE FAILURE DURING CLIMB. FOUND METAL IN TAILPIPE AND EXTENSIVE LPT BLADE DAMAGE. REPLACED THE RIGHT ENGINE.SDR NACA2024061500006Bracket · damagedDURING ENGINE INSPECTION FOUND A SMALL PIECE MISSING FROM INTERMEDIATE CASE SEGMENT AT 5 OCLOCK POSITION. DEFERRED PER DMI 72-34 IS APPROVED FOR ONE FLIGHT CYCLE. REMOVED AND REPLACE INTERMEDIATE FAN CASE SERVICE BRACKET @ #1 ENG 5 OCLOCK POSITION IAW AMM 72-3SDR NACA2024061500005Case · gougedDURING ENGINE INSPECTION FOUND GOUGE ON OUTER FAN CASE AT 4 OCLOCK AND 8 OCLOCK POSITION. PERFORMED BLEND OUT IAW PW TASK 72-33-01-300-02SDR AALA202406190489Engine · overtempAIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO DEN DUE TO ON TAKE OFF AFTER ROTATION THE #1 ENGINE AND THE #2 ENGINE HAD OVERTEMP ECAM WARNINGS. THE FLIGHT CREW REPORTED THAT AFTER THRUST REDUCTION THE #2 ENGINE OVERTEMP CLEARED SDR AALA202406190166Engine · overtempAIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO DEN DUE TO ON TAKE OFF AFTER ROTATION THE #1 ENGINE AND THE #2 ENGINE HAD OVERTEMP ECAM WARNINGS. THE FLIGHT CREW REPORTED THAT AFTER THRUST REDUCTION THE #2 ENGINE OVERTEMP CLEARED SDR WX0A2024061732073Engine · power loss(AIRCRAFT NOT GROUNDED) (EMERGENCY DECLARED) (MX REPOSITION FLIGHT) ENGINE #1 ROLLED BACK AND FAILED AFTER TAKEOFF AT APPROXIMATELY 7000 FEET. NO DAMAGE SUSPECTED SAW PUDDLE UNDER THE ENGINE. / REMOVED AND REPLACED #1 ENG. FUEL NOZZLE FILTER SUPPLY TUBE GASKETSDR AALA202406180075Seal · damagedAIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO LAS DUE THE THE FLIGHT CREW REPORTING THAT ON DEPARTURE RECIEVING AN ECAM MESSAGE FOR ENGINE #2 EGT OVER LIMIT. FLIGHT CREW FOLLOWED THE ECAM PROCEDURES AND SHUT DOWN THE #2 ENGINE. SDR AALA202406140075Engine · overtempAIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO LAS DUE THE THE FLIGHT CREW REPORTING THAT ON DEPARTURE RECIEVING AN ECAM MESSAGE FOR ENGINE #2 EGT OVER LIMIT. FLIGHT CREW FOLLOWED THE ECAM PROCEDURES AND SHUT DOWN THE #2 ENGINE. SDR QMLA2024062520067Seal Ring · crackedDURING FIRST GROUND RUN FOLLOWING TURBINE ASSEMBLY REPLACEMENT, OIL WAS FOUND LEAKING FROM THE GAS PRODUCER TURBINE PRESSURE OIL NOZZLE. THIS IS NOT SOMETHING WE HAD TOUCHED. UPON INSPECTION IT WAS FOUND THAT THE SEALING RING UNDER THE NOZZLE HAD BEEN CRACKED,SDR CALA2024061701812Engine · vibrationVIBRATION INDICATION (ENGINE) HIGH (BLACK NUMBERS ON WHITE BOX) FIM TASK REF : 31-90-F8-03A-421B-A CMC MSG# 7711602 FLIGHT STATUS: A INTERMITTENCE CODE: M PH: CRUISE NARRATIVE: ENGINE MONITOR UNIT (RIGHT ENGINE) REVIEW CHRONIC HIST (CHAPTER 77). (CLOSED FUSDR DALA2024061306053Engine · overtempATB/IFSD- RETURNED TO TUS DUE TO FLIGHT CREW SHUTDOWN #2 ENGINE DUE TO EGT EXCEEDANCE. CORRECTIVE ACTION: FOUND EGT REACHED 976 DEGREES, REQUIRES ENGINE CHANGE DUE TO AREA C EGT EXCEEDANCE. PERFORMED BORESCOPE WITH NO FINDINGS, AMM ALLOWS 1 CYCLE NON-REVENUE FSDR 3EJA841JS061124Engine · damagedHIGH SPEED TAKE OFF ABORT DUE TO A LOUD BANG AND AIRCRAFT YAW. BELIEVED TO BE A COMPRESSOR STALL. CLEARED THE RUNWAY, FOD FROM THE ENGINE FOUND IN THE AFTERMATH. NO INJURIES OR ADDITIONAL DAMAGE TO THE AIRCRAFT.SDR 2024FA0000440Engine · unknownDETECTED BASED ON A CUSTOMER REQUEST REGARDING TEST DATA, THAT MTU-H INCORRECTLY DETERMINED THE N1 MODIFIER LEVEL IN CERTAIN CASES FOR BOEING FADEC ENGINES. FOR POST-SB 73-0288 ECU SOFTWARE THE ESM 72-00-00 TESTING 007 EFFECT C SUBTASK 72-00-00-760-379 REQUISDR DXTA2024061112018Engine · bird ingestionINGESTED A SEAGULL AT ROTATION INTO THE LEFT ENGINE. THERE IS AT LEAST ONE VISIBLY DAMAGED FAN BLADE. COMPLIED WITH BORESCOPE INSPECTION AND FOUND EVIDENCE OF BIRD INGESTION THROUGH THE CORE OF THE ENGINE; SIX DAMAGED FAN BLADES REMOVED LT ENGINE. INSTALLED RSDR QMLA2024061020062Engine · warning light#1 ENG CHIP LIGHT ILLUMINATED ENROUTE BACK TO HOME BASE. EMERGENCY PROCEDURES WERE PERFORMED IAW WITH THE RFM. LANDING AT HOME BASE WAS ACCOMPLISHED WITHOUT INCIDENT. APPROPRIATE LOGBOOK ENTRIES AND NOTIFICATIONS WERE MADE.SDR NACA2024060900002Engine · failedLEFT ENGINE CHANGE IS REQUIRED DUE TO BORESCOPE INSPECTION AS UNSERVICEABLE CONDITION ENGINE SN 724732. REMOVED AND INSTALLED LEFT ENGINE IAW AMM 71-00-02, LEAK CHECK AND ENGINE RUN GOOD.SDR NACA2024060700004Engine · faultedL ENG EEC C1. L ENG EEC C1 STATUS MESSAGE ASSOCIATED WITH L ENG AO VALVE , REMOVED AND REPLACED #1 ENGINESDR QMLA2024060620060Engine · overtempFLOAT PILOT OVER TEMP THE MGT IN FLIGHT. MGT EXCEEDANCE OF 741 FOR 3 SECONDS. PERFORMED SPECIAL INSPECTION OF TURBINE AND FIRST STAGE TURBINE WHEEL, TURBINE NOZZLE AND SHIELD. NO DEFECTS NOTED. REASSEMBLED TURBINE, OPS CHECK GOOD.SDR P5CA2024060400011Engine · failed(IFSD) ON TAKEOFF, HEARD A LOUD BANG ON THE RIGHT SIDE. RH ENG N1 ROLLED BACK. CONDUCTED RIGHT ENGINE VISUAL INSPECTION AND SEVERE DAMAGE FOUND. SHUTDOWN RIGHT ENGINE AT 0120Z(<P>MX IN WORK WHILE IN AOGM FOR #2 ENG FAILURE. REMOVED AND REPLACED RH ENG IAW EA SDR WX0A2024060332065Valve · faultedENG 2 STALL ECAM AT TOD. ENGINE 2 N1 ROLLED BACK WITH RYTHMIC SURGING. WITH THRUST LEVER AT IDLE, ENGINE RETURNED TO NORMAL. RESUMED NORMAL OPS. / REMOVED AND REPLACED #2 ENG PRV(4001HA) PER WORK ORDER 00504443 STEP 3 AND IAW AMM 36-11-52-400-042-A. LEAK CHECKSDR YENA2024060300809Valve · failedFLT#44, LGW-JFK. (ETOPS)' REF LOG PAGE 3970765, ITEM 1 POWER PLANT ENGINEERING AFTER BSI OF #2 ENG REVIEW ADVISED ENGINE REQUIRES REPLACEMENT; REF DEFECT 3970767, ITEM 1 (REM/INS ENG 2 PER TC A320-71-00-51-400-802-1. TESTS OK. A/C OK FOR SERVICE) FOR REPLACEMSDR QXEA2024053100145Sensor · malfunctioned#2 OIL BYPASS ADVISORY ON CLIMB. WENT AWAY AFTER 5 SEC. REMOVED FROM SERVICE. CMC SHOWED FAULT CODE 79210004UT1, ENG 2 OIL FILTER IMPENDING BYPASS, PROBE/SENSOR. C/W E175 FIM TASK 79-21-00-810-802-A PARA 1 THRU 6G(1)B. REF FIM TASK 79-21-00-810-802-A FOR REMOVSDR SWIA2024060400528Engine · odorSTRONG FUEL ODOR OBSERVED IN CABIN DURING DESCENT AND LANDING. GROUND CABIN OBSERVED WHITE/BLUE SMOKE COMING FROM LEFT ENGINE AS AIRCRAFT APPROACHED THE GATE WITH BOTH ENGINES RUNNING. SMOKE DECREASED IN INTENSITY AFTER ENGINE WAS SHUT DOWN, BUT WHITE SMOKE COSDR SWAA2024060391021Engine · failedENG 2 EGT EXCEEDENCE FOLLOW BY FAILURE OF #2 ENG. INSPECTED ON 771-00-01-ETOPS (REM/INST - POWER PLANT) TTG8Q008RDYE&REFERENCE]. REMOVED AND REPLACED PER [AMM 71-00-02-401-NG (POWER PLANT - REMOVAL/INSTALLATION - PERMANENT)]SDR SWIA2024053000028Engine · smokeSTRONG FUEL ODOR OBSERVED IN CABIN DURING DESCENT AND LANDING. GROUND CABIN OBSERVED WHITE/BLUE SMOKE COMING FROM LEFT ENGINE AS AIRCRAFT APPROACHED THE GATE WITH BOTH ENGINES RUNNING. SMOKE DECREASED IN INTENSITY AFTER ENGINE WAS SHUT DOWN, BUT WHITE SMOKE COSDR F3LA2024052900078Engine · overtempAIRCRAFT WAS GROUNDED DUE TO AN SDR REPORTABLE EVENT FOR ENGINE 2 OVERTEMP, NO VIBRATION, THRUST BACK TO 65-70%N1 TO KEEP IT OUT OF RED. NEEDLE DANCING SIGNIFICANTLY, ENGINE SHUT DOWN PER ECAM /QR#. REF LP 407377 ITEMS 1,2, & 3 FOR CORRECTIVE ACTION OF CJ13SDR 2024FA0000433Engine · power lossON DEPARTURE FROM KBFL, THE LEFT ENGINE LOST POWER SHORTLY AFTER TAKEOFF, THE ENGINE RETAINED PARTIAL POWER AND THE PROPELLER WAS NOT FEATHERED. THE PILOT IMMEDIATELY RETURNED TO KBFL. INSPECTION OF THE ENGINE REVEALED A LARGE HOLE THROUGH THE TOP OF BOTH HALVSDR SWIA20240523Engine · flamed outR ENG FLAMEOUT WARNING MESSAGE ON CLIMB AROUND 28,000 FEET. ALL RIGHT ENGINE GAUGES WENT TO NEARLY IDLE. WE RAN THE QRC/QRH, DIVERTED TO KGRR AND PERFORMED A SINGLE ENGINE LANDING. (FLIGHT 4055 FILED CLOSED)THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 2827909SDR HNAA2024052400473Engine · power lossENGINE #2 ROLLED BACK WITH LOUD BANG ON TAKEOFF ROLL. ( CAPTAIN SAID HE REJECTED TAKEOFF AND REQUESTED MAINTENANCE TO TOW THE PLANE BACK, AFTER WHICH HE SHUT DOWN THE PACKS WHEN HE STARTED TO SMELL THE FUMES )SDR AALA202405265198Engine · overtempAIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO CLT. FLIGHT CREW REPORTED THAT ENGINE #2 EGT OVER LIMIT ON TAKE OFF CLIMB WAS 400 DEGREES, APPROXIMATELY 920C. FLIGHT CREW SHUTDOWN THE #2 ENGINE AND REPORTED THAT LATER IT COOLED TOSDR DALA2024052305455Engine · stalledSHIP 3307 ENGINE STALL WITH ABORTED TAKE OFF. CORRECTIVE ACTION: ENGINE REPLACED THIS IS TIED TO LOG PAGE 5394984 AND ODI 2024-00364. JOB COMPLETE.SDR AALA202405235198Engine · overtempAIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO CLT. FLIGHT CREW REPORTED THAT ENGINE #2 EGT OVER LIMIT ON TAKE OFF CLIMB WAS 400 DEGREES, APPROXIMATELY 920C. FLIGHT CREW SHUTDOWN THE #2 ENGINE AND REPORTED THAT LATER IT COOLED TOSDR HALA20240522141Liner · damagedETOPS - ON LANDING, POSSIBLE BIRD STRIKE, RIGHT SIDE OF AIRCRAFT WITH POSSIBLE BIRD INGESTION #2 ENG. PERFORMED VISUAL EXAMINATION OF #2 ENG. PER AMM 72-00-00-210-807-A. FOUND OUTER LINER SEGMENT POSITIONS 6 AND 8 DAMAGED. REMOVED AND REPLACED SEGMENTS IAW AMMSDR SIMA20240520001Engine · power lossLOSS OF THRUST ON ENG 1 DURING REDUCTION TO FLIGHT IDLE. DURING LOSS OF THRUST ITT DROPPED SIGNIFICANTLY. ONCE THRUST WAS APPLIED TOOK APPROX. 10 SECONDS FOR ENG 1 N1 TO MATCH ENG 2 N1. PERFORMED ENGINE RUNS OF #1 AND #2 ENGINE IAW ERJ 175 AMM 71-00-01 AND GE SDR R61A2024052300234Engine · vibrationON CLIMB OUT AROUND 8500-9000 FT WE GOT THE 4.0 VIBE ON ENGINE 2. RAN QRH AND CONTINUED. AROUND 15500 - 16000 FEET IT HAPPENED AGAIN. WE LEVELED OFF AT 17000 AND ENGINE WENT BACK INTO 4.0 AT CONSTANT POWER AROUND 74%. HAD TO GO TO 40-30% N1 TO GET IT BACK BELOSDR BJNA202405180001Engine · overtemp#2 ENGINE EGT WENT INTO THE RED ON TAKE OFF ROLL. TAKE OFF ABORTED RETURNED TO GATE. OBTAINED EXCEEDANCE DATA IAW AMM71-00-00-740-801 AND FOUND TEMP EXCEEDED 725 CELSIUS FOR 10 SEC. AND PEAKED AT 777 CELSIUS. BORESCOPE REQUIRED PER AMM 71-00-00-800-804 STEP ESDR DXTA2024052011801Engine · stalledAFTER TAKEOFF CLIMBING THROUGH 400' AGL THE RED CAS MSG ENG EXEEDANCE R DISPLAYED ALONG WITH ENGINE COMPRESSOR STALLS. AMBER CAS MESSAGES ENG CTRL FAULT R AND ENGINE EGT HIGH R CAME ON AFTER LANDING. VISUAL INSPECTION OF RIGHT ENGINE DOES NOT SHOW ANY DAMAGE. SDR AALA202405171966Engine · power lossAIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO MCO: FLIGHT CREW REPORTED A SUDDEN LOSS OF POWER EXPERIENCED ON NUMBER 2 ENGINE DURING ROTATION. THE AIRCRAFT EXPERIENCED A VIOLENT YAW MOTION TO THE RIGHT. THE FLIGHT CREW REPORTED SDR SWIA20240520015Blade · bentFOUND RH ENGINE BLADE #19 BENT/DEFORMED ON LEADING EDGE, MIDSPAN. (FILED CLOSED)INSPECTED RH FAN ROTOR BLADE #19 IN REFERENCE WITH -8E GE LMM 72-21-00, INSPECTION 003. FOUND DEFORMATION IN LEADING EDGE TO BE OUT OF SERVICEABLE LIMITS, 0.0625" FROM CONTOUR X 3.SDR CALA2024051601483Engine · flamed outENG FAIL L CAUTION THE LEFT ENGINE HAS FLAMED OUT AND RUN DOWN BELOW IDLE SPEED. FIM TASK REF : G73-90-F8-01A-421B-A CMC MSG# 7332901 FLIGHT STATUS: A INTERMITTENCE CODE: M PH: CLIMB NARRATIVE: ELECTRONIC ENGINE CONTROL CHAN-B (LEFT ENG) SDR FLAGGED.SDR DALA2024051405214Engine · vibrationSHIP 5037 -ATB- PERFORMED AN AIR TURN BACK FOR HIGH ENGINE VIBES ON THE NUMBER 2 ENGINE. CORRECTIVE ACTION: INSPECTED INLET, NO DEFECTS NOTED ON FAN BLADES. PERFORMED EEC SOFTWARE UPGRADE, PERFORMED VIBE RUN ALL INDICATIONS NORMAL. (LP 5341912)SDR NACA2024051000001Shutoff Valve · warning messageR ENG HPSOV STATUS MESSAGE. DEFERRED RH HPSOV PER MEL 36-11-02-02 CAT C 5/10/2024 0649ZSDR CALA2024051301450Engine · vibrationHIGH E1 N1 VIB ON TAKEOFF. AFTER THRUST REDUCTION N1 WENT BACK TO WITHIN LIMIT VERIFIED CHIP DETECTOR INSTALLATION IAW GMM 09-10-05. EICS MESSAGE L ENG BB VIBRATION PRESENT. CREW REPORTED N3 ENGINEERING UPDATE: PLEASE ACCOMPLISH BLOCK 3, 7, 8 AND 9 WITHIN REFSDR CALA2024051301451Gasket · failedENG 2 OVERHEAT DURING DEPARTURE. LIGHT EXT AFTER REDUCING POWER OPENED #2 ENGINE COWLING AND INSPECTED BLEED AIR DUCTING. FOUND THE STAGE 9 INLET TUBE [23] TO THE HPTACC VALVE LOOSE AND COMBUSTION CASE FLANG AND SEAL BLOWN OUT. REPLACED SEAL ON STAGE 9 DUCT SDR CALA2024051301448Engine · overheatedNO.2 OVRHEAT LT ILLUM IN FLT. SEE RELATED FIM 26-10 TASK 811. PERFORMED FIM TASK 26-10 TASK 801. NO FAULTS FOUND. PERFORMED FIM TASK 26-10 TASK 811 ( EXCEPT ENG RUN), PERFORMED FIRE DETECTION LOOP RESISTANCE SYS TEST, NO FAULTS. ON MIDS UNCONNECTED FROM HARNSDR QMLA2024050820050Unknown · unknownINITIAL CONDITIONS PRIOR TO TAKE OFF WERE AS FOLLOWS: DEPARTING FROM KHZL WITHIN WEIGHT AND CG LIMITS, 2+30 FUEL ON-BOARD, AVERAGE CREW WEIGHT BETWEEN ALL THREE CREW MEMBERS, AND OBSERVED WINDS OF 230@5. PILOT PERFORMED A HOVER POWER CHECK CENTER SOD PRIOR TOSDR 2024FA0000357Hub · damagedSIGNATURE TECHNICAIR - OMAHA ENGINE SERIAL NUMBER JC0603 WAS SHIPPED TO STANDARDAERO FOR INVESTIGATION AND REPAIR AFTER THE OPERATOR REPORTED METAL CONTAMINATION OF THE OIL SYSTEM. STANDARDAERO DISASSEMBLED AND INVESTIGATED ENGINE SERIAL NUMBER JC0603 FOR THE
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