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 DALA2024110510672Engine · vibrationAIRCRAFT 3761, ON DESCENT INTO ANC @ FL340 NOTED BOTH POWER LEVERS MATCHED, LEFT ENGINE @ 90% N1, LEFT @ 60 % N1, AND ROLLED BACK. ACCOMPANYING AUDIBLE VIBRATION PERFORMED QRH, VIB WENT AWAY WITH THRUST LEVER CLOSED, VIB GAUGE NORMAL THE ENTIRE TIME. FA REPORTSDR U2RA2024110400063Seal · damaged"DURING A-CHECK INSPECTION, IT WAS DISCOVERED THAT THE AFT SEAL, LOCATED ON THE OUTBOARD ENGINE CORE COWL OF ENGINE 1 HAD A MISSING PORTION NEAR THE LOWER CORNER. A REPAIR WAS EMBODIED AND CLASSIFIED AS ""MAJOR"" VIA FVCI EO 24193-1. REF NAL M-8A 63130-12."SDR HNAA2024103001038O-Ring · failedON TAKEOFF ROLL BLD 2 LEAK MSG DISPLAYED ON EICAS. MEL 30OCT24 13:17 AVL C30409 36-1-4 BOTH ENG BLEEDS FACT 31OCT24 01:50 AVL R+R'S BLEED 2 COUPLING O-RINGS UNDER PANEL 272AF IAW AMM 36-11-10. OPS AND LEAK CHECK GOOD. REACTIVATED E1+E2 BLEED VLVS IAW SDR SWAA2024110154509Engine · fire warningAFTER LANDING ON TAXI IN NR 1 FIRE INDICATIONS ILLUMINATED. CHECKLIST ACCOMPLISHED INCLUDING DISCHARGING 1 FIRE BOTTLE. INDICATIONS WENT OUT BUT RETURNED AFTER ABOUT 5 MINS. SECOND FIRE BOTTLE. ENGINE REMOVED AND REPLACED ON TTG8Q00UPQV0 ALL WORK ACCOMPLISHEDSDR DALA2024103010507Engine · making metalSHIP 3305 -ATO- DISCONTINUED TAKEOFF AT 25 KNOTS DUE TO RIGHT ENGINE FAILURE ALONG WITH FIRE INDICATION WARNING IN THE FLIGHT DECK. RIGHT ENGINE FIRE BOTTLES DISCHARGED. CORRECTIVE ACTION: FOUND METAL IN THE 2.5 AND 2.9 BLEED PORTS, ENGINE CHANGE REQUIRED. MAISDR HNAA2024102901034Engine · making metalENGINE 2 SHUTDOWN IN FLIGHT, WITH NO N2 ROTATION DFRL 28OCT24 21:14 PHL MX FOUND FOD IN CORE AND EXHAUST. RAR #2 ENGINE IAW WC 710000 AND OPS CHECKED IAW WC 727000SDR DALA2024102810444Engine · failedSHIP 3818 -ATB/IFSD- RETURNED TO SMF DUE TO LEFT ENGINE FAILURE. CORRECTIVE ACTION: LEFT ENGINE REPLACED IAW AMDS WORKCARD 7100-4423-LH. ALL OPS GOOD, REF LOG PAGE 0631249.SDR SWIA202410280027Engine · smokeAFTER ENGINE SHUTDOWN AT GATE EXCESSIVE AMOUNT OF SMOKE COMING FROM ENGINE 2 (FLIGHT 6490 - FILED OPEN)PLEASE REFERENCE AML 1460063. REMOVED AND REPLACED RH FMU IN REFERENCE TO ERJ AMM 73-21-03 AND CF34-8E LMM 73-00-00 SPECIAL PROCEDURES 003. LEAK CHECK GOOD ASDR VNAA2024121711101Engine · fumesON DESCENT, THE FLIGHT CREW REPORTED FUMES IN COCKPIT IN FLIGHT, SMELLING OF TIRES AND OCCASIONAL BURNING. THE LOCATION OF THE FUMES WAS IN THE COCKPIT AND FORWARD JUMP SEAT AREA. THE CAPTAIN WAS EVALUATED BY PARAMEDICS DUE TO THE HEADACHE THAT FORMED FROM THESDR 3EJA2024102600010Engine · power lossDURING DESCENT THE LEFT ENGINE ROLLED BACK OR FLAMED OUT. PER THE CHECKLIST GUIDANCE WE WAITED UNTIL 18000 TO PERFORM A STARTER ASSIST RESTART WHICH WAS SUCCESSFUL. MAYDAY WAS DECLARED AND WE DIVERTED TO KMCI DUE TO ITS CLOSE PROXIMITY AND SERVICES. FIRE TRUCKSDR DALA2024102810475Engine · failedSHIP 3315 ENGINE FAILED. CORRECTIVE ACTION: REPLACED ENGINE PER A330 AMM 71-01. (0622941)SDR DALA2024102810427Engine · failedSHIP 3315 -ATO- DISCONTINUED TAKEOFF AT 30 KNOTS DUE TO LEFT ENGINE FAILURE AND ASSOCIATED FIRE INDICATION WARNING IN THE FLIGHT DECK. LEFT ENGINE FIRE BOTTLES DISCHARGED. CORRECTIVE ACTION: FOUND METAL IN THE 2.5 AND 2.9 BLEED PORTS. REPLACED ENGINE AND FIRE SDR QMLA2024102820139Engine · making metalENGINE CHIP LIGHT IN-FLIGHT I ACCEPTED A PATIENT FLIGHT REQUEST FOR AN INTERFACILITY TRANSFER FROM PINE RIDGE HOSPITAL TO MONUMENT HEALTH IN RAPID CITY, SD. FLIGHT WAS UNEVENTFUL ENROUTE TO THE HOSPITAL AND THE PATIENT LEG. THE PATIENT
WAS DROPPED OFF AND WE SDR 2024FA0000790Hp Turbine · damagedTHE ENGINE WAS INDUCTED IN SANAD FOR LEVEL 2 CHECK & REPAIR. UPON REMOVAL OF THE HPT ROTOR FROM THE HP SYSTEM, THE FOLLOWING WAS OBSERVED: 1. NGV ASSEMBLY FOUND 7 BOLTS LOOSE, MISSING SPACER AND WASHER. 2. NGV ASSEMBLY NOTED WITH MULTIPLE IMPACT DAMAGE. 3. HPTSDR DALA2024102810424Engine · vibrationSHIP 3220 DISC: DURING DES 370-350, AIRFRAME VIBRATION BEGAN CHECKED ENG VIB N1/ N2 ON BOTH ENGINES AND INDICATION WERE NORMAL/ GREEN. REC ENG EGT ECAM FOR HIGH TEMP AND DECREASED AND ON #2 ENG AND VIB STOPPED. C/A: REPLACED ENG IAW AMDS 7100-9901, REF. LOGE PSDR DALA2024102410347Engine · failedSHIP 3315 -ATO- DISCONTINUED TAKEOFF AT 30 KNOTS DUE TO LEFT ENGINE FAILURE AND ASSOCIATED FIRE INDICATION WARNING IN THE FLIGHT DECK. LEFT ENGINE FIRE BOTTLES DISCHARGED. CORRECTIVE ACTION: FOUND METAL IN THE 2.5 AND 2.9 BLEED PORTS. MAINTENANCE IS IN THE PROSDR HALA20241023295Packing · leakingETOPS - #1 ENG OIL NEAR FAN BLADES (OIL BLADES). REMOVED AND REPLACED #1 ENG FAN SHAFT COVER PACKING IDLE POWER TEST GOOD. LK CK GOOD. OK FOR SERVICE IAW AMM 72-15-00-960-801-ASDR WX0A2024102332205Engine · odor(AIRCRAFT NOT GROUNDED) DURING DESCENT WE GOT A FOUL SMELL ( MUSTY ODOR ). ACCORDING TO THE FAS ITS STARTED RIGHT AFTER WE STARTED THE DESCENT AND IT LASTED TIL WE PARKED. IN THE FLIGHT DECK THE ODOR DISSIPATED AFTER A FEW MINUTES. APPARENTLY THE ODOR CAME ON SDR SWAA2024102451302Oil System · leaking#2 ENGINE OIL QTY WENT TO ZERO. TEMPERATURE AND PRESSURE REMAINED NORMAL.<[01] REMOVED AND REPLACED #2 ENGINE PER TASK 771-00-01. REFERENCE TTG8Q0064PND FOR ALL DETAILS.;[02] INSPECTION C/WSDR CALA2024102400920Engine · overheatedR ENG OVERHEAT ON GND BEFORE T/O SHUT DOWN ENG HAD CFR INSPECT AND TAXIED BACK. REMOVED AND REPLACED #2 ENGINE IAW 71-00-02-400-801-F00,ACCOMPLISHED 5 MINUTE ENGINE IDLE RUN ALL SYSTEMS TEST NORMAL, SERVICED ALL FLUIDS TO NORMAL LEVELPARTS USED: 57-5452-3-0SDR ANCF20241021020Engine · stalledENG 1 STALL DURING FLIGHT AT 34000 FT "ENG 1" STALL FOLLOWED BY "ENG 1" FAILSDR 4DPA2024102000001Carbon Seal · leakingCREW REPORTED AT APPROX 400’ FA CALLED TO REPORT SMOKE IN THE AFT CABIN AND AN EXHAUST SMELL. SMOKE DISSIPATED BY THE TIME WE LANDED. EMERGENCY DECLARED. REPORTED BY FA: SMOKE SUDDENLY FILLED THE AFT CABIN UP TO ABOUT ROW 11. BEGAN RIGHT BEFORE SHE CALLED (400SDR DALA2024102110281Engine · stalledSHIP 3015 -ATB- RETURNED TO SLC DUE TO A #2 ENGINE STALL MESSAGE ACCOMPANIED BY A FADEC FAULT, LOUD POPS AND AIRCRAFT YAW. CORRECTIVE ACTION: PERFORMED BORESCOPE WITH NO DAMAGED NOTED. REPLACED T25 SENSOR AND ECU. PERFORMED HIGH POWER RUN, ALL PARAMETERS NORMASDR DALA2024120911532Duct · temp repairCRACK ON RIGHT ENG BYPASS DUCT NEAR PRECOOLER INLET WAS TEMPORARILY REPAIRED. RE-INSPECTION REQUIRED PER ER/A 620571-14 REV ORIGINAL. REFER TO LOG #0580374 FOR PRIOR INSPECTION. SECTION 4 INSPECTION MUST BE ACCOMPLISHED BETWEEN 220 AND 180 FLIGHT CYCLES PER ERSDR 2024FA0000785Frame · damagedDURING DISASSEMBLY OF THE ENGINE ESN 60A689 IN THE SAFRAN AIRCRAFT ENGINES SQY MAINTENANCE SHOP (NEAR PARIS), THE TURBINE CENTER FRAME ASSEMBLY WAS OBSERVED WITH A PARTIAL RELEASE OF THE ROPE SEAL. (REFER TO ATTACHED PRESENTATION FOR FURTHER DETAILS). AS THISSDR IPXA2024101886334Fan · vibration**ATB**DURING CLIMB LFT ENG FAN VIB IND 4.1 AIRFRAME VIB ALSO NOTED ACCOMPLISHED INSPECTION OF L/H ENG IAW 77.00.00.206.001.H00 NO DAMAGED FOUND. ACCOMPLISHED FIM 71.5 FAULT 856 AND AMM 77.31.00/501. ACCOMPLISHED AVM FAN TRIM BALANE. ACCOMPLISHED HIGH POWER RSDR SWAA2024102149416Engine · stalledENG #2 COMPRESSOR STALL AT FL380 DESCENDING @ 79% N1. DURATION APPROX 5 MIN. AFTER ARRIVAL AT FL 250 ENG OPERATEDNORMALLY FOR DURATION OF FLIGHT<SDR SCNA20241017329Engine · power lossDEFECT 698089: ENGINE #2 N1 LIMITED ON TAKEOFF 81% THEN WE COULD NOT GET MORE THAT 76% N1 AT 6000'. NO OTHER ABNORMAL INDICATION. 10 MINUTES LATER ENGINE FAILED ON ITS OWN (EMERGENCY DECLARED). - - RESOLUTION: PERFORMED HIGH POWER ENGINE RUN IAW AMM 71-00-00SDR SCNA20241018331Engine · vibrationDEFECT 734071: ENGINE #2 VIBE WENT TO 4.0 AT FL 237 PERFORMED QRH INCREASED THRUST SLIGHTLY TO CONTINUE CLUIMB AND VIBE WENT TO 4.2 MC JP 311181 - - RESOLUTION: RR'D AVM SIGNAL CONDITIONER IAW AMM77-31-03.PERFORMED TEST 14A FAN TRIM BALANCE. SOULTION REMOVED SDR A6WA202410158837Engine · faultedIN CLIMB RIGHT ENGINE HAD SPIKE IN ITT AND REDUCTION IN N1 AND N2 AND WAS UNRESPONSIVE FOR 10-20 SECONDS. THEN RETURNED TO NORMAL. ON APPROACH RIGHT ENGINE AGAIN HAD SAME INDICATION AND AIRCRAFT HAD VIBRATIONS. DURING BOTH EVENTS THRUST WAS BEING REDUCED BY PISDR CALA2024101702668Engine · fodSPARK OBSERVED FROM RAMP WHILE STARTING THE LEFT ENGINE TOOK IN FOD DURING START. ADDING PICTURES BELOW. PER FLIGHT CREW DEBRIEF, ON ENGINE START SPARKS NOTICED BY RAMP ACCOMPLISHED ENGINE #1 ENGINE FOD GVI AS PER AMM TASK ON #1 ENGINE, NO FLUCTUATIONS OF ENGISDR ANCF20241016019Engine · faultedDURING CLIMB THROUGH FL150 ECAM ADVISORY LOW OIL QTY WAS PRESENTED, THE ECAM ADVISORY WAS MONITORED SHOWING A CONTINOUS DECREASE IN OIL QTY, THROUGH FL 280 THE ECAM WARNING "LOW OIL QTY" WAS PRESENTED. WHILE PERFORMING THE ECAM ACTIONS WHICH COMMANDED TO REDUCSDR CALA2024101500837Engine · vibrationENG 2 N1 VIB INDICATION ON MEL TOMC APPROVES MEL 7700G FOR ENG 2 N1 VIB TURNS YELLOW X OCCASIONALY. REPLACED EVMU IAW MM77-32-34/401 , IPC REF 77-32-34-01A NO HELP STATUS MESSAGE NEED FURTHER T/S. ADJUST AND TEST IAW MM UNIT, ENGINE VI OFF 31-7731-9-0001 0564 SDR 9WGA2026032635609Acoustic Liner · corrodedDURING HEAVY MAINTENANCE CHECK CORROSION SIGNS UNDER ACOUSTIC LINER ENGINE #2 POSITION 3 AND 6 O'CLOCK (REPIAR). CORROSION IN ACOUSTIC INNER LINER ENGINE #2 POSITION 3 AND 6 O'CLOCK WAS CLEANED IAW B747-400F AMM 51-00-53. THE AIRCRAFT WAS APPROVED FOR RETURNSDR DALA2024101410040Engine · failedSHIP 3811 ATB/IFSD RETURNED TO SLC DUE TO CREW REPORTED #2 ENGINE FAILURE. CORRECTIVE ACTION: MAINTENANCE REPLACED THE NUMBER 2 ENGINE REF WORK CARD 7100-4423. ALL CHECKS OK.SDR DALA2024101109976Engine · odorFA ADVISED FUMES IN REAR OF AIRCRAFT WHEN CONFIGURING FOR APPROACH. FUMES HAD A CHEMICAL SMELL AND MADE THEM FEEL LIGHT HEADED. T/S PER A220 SMOKE AND FUMES W/C 0550-2001. NO FAULTS IN OMS. FOUND OIL SMELL W/ #1 ENG AS BLEED SOURCE. #1 ENG HAS HISTORY OF HOC. SDR AALA202410100075Engine · fodAIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED DUE TO: ENGINE NUMBER 1 VIBRATION AT CRUISE. SUSTAINED LEVELS GREATER THAN 1.0 ACCOMPANIED BY AUDIBLE OR AIRFRAME VIBRATIONS; AIRCRAFT DIVERTED TO AND LANDED SAFELY AT CLT. REMOVED TOOLING FROM PREVIOUS JOB INSSDR K11A2024100900288Engine · no discrepancyMULTIPLE BIRD STRIKES DEPARTING RWY 27 IN KCVG AT 200 FOOT ALT. SMELL OF BIRDS THROUGH THE PACKS ON RETURN TO KCVG. PERFORMED CONDITIONAL INSPECTION IAW B737-400 AMM 05-51-37. INSPECTION GOOD NO DEFECTS NOTED. PRIOR TO INSPECTION CLEANED THE BIRD REMAINS FROMSDR DXTA2024100800763Engine · overtempWHILE DESCENDING ON OHSEA 2 ARRIVAL INTO KSNA & PASSING APPROX 15000 FT WITH POWER LEVERS NEAR IDLE, A VIBRATION FELT. NO CAS MESSAGE, DISCONNECTED AUTOPILOT TO SEE IF COULD FEEL ANY FEEDBACK IN CONTROLS. ALSO CHANGED POWER SETTINGS TO CHK ENG INDS. NORMAL SDR NACA2024100500001Engine · vibrationHIGH L ENG VIBRATION N1 5.0. ACCOMPLISHED FIM 77-31-FT 813 BLOCKS 1,2, AND 23 FOUND GROUND SHIELD TERMINAL LUG ON CONN D10994 BROKEN, REMOVED AND REPAIRED TERMINAL WIRING IAW WDM 77-31-11 AND SWPM 20-24-26.SDR CALA2024100700780Valve · faultyL BLEED TRIP OFF LGT CAME ON AT 80KTS. TAKEOFF ABORTED. FOLLOWED FIM 36-10 TASK 809. UNABLE TO PERFORM TS OF PRECOOLER CHK AT LINE. REQUESTING MEL MEL 3603A CANNOT DEFER DUE TO ICING RESTRICTION REF AMM 36-11-00-700-801 ACCOMPLISHED HEALTH CHECK ON HIGH STAGE SDR 2024FA0000754Hose · wrong partATO IN APRIL 27TH, 2024 ON DELTA AIRLINES CFM56-5A 733291 FOLLOWING OIL FILTER CLOGGING INDICATION. TROUBLESHOOTING LEADS TO IDENTIFY INCORRECT CONNECTION OF OIL FILTER DELTA PRESSURE SWITCH FLEXIBLE LINE TO THE LUBE UNIT SUPPLY FILTER PORT INSTEAD OF THE SCAVSDR 2024FA0000753Bolt · looseON MARCH 06TH 2024, THE ENGINE SERIAL NUMBER 59A536 IS OPERATED BY INDIGO WHEN, DURING THE CLIMB PHASE, A COCKPIT ALARM LASTING 3 SECONDS FOR "ENGINE FIRE" IS NOTED BY THE CREW. ON GROUND THE TROUBLESHOOTING REVEALED THAT THE 4 BOLTS (SIN 63520) ATTACHING THSDR I5PA2024100288801Engine · stalledFLT NO: MGE900. ESI - R ENG HAD MULTIPLE IN-FLIGHT COMPRESSOR STALLS DURING CRUISE. R/R RH ENG PER TASK CARD 71-999-00-01.SDR SWAA2024100344795Engine · failedENGINE #2 FAILURE DURING CLIMB OUT. SHUT DOWN PER ENGINE OR ENGINE SEVERE DAMAGE OR SEPARATION QRC. ENGINE FIRE BOTTLE NOT DISCHARGED NO FIRE INDICATION.<SDR ANCF20241002018Tailpipe · fireAFTER BOTH ENGINE SHUTDOWN TAIL PIPE FIRE ON ENG 2 OBSERVED BY RAMP PERSONAL IAW TSM 72-00-00-810-A THE TRF WAS INSPECTED, THE INLET COVER PACKING AND INLET COVER SEAL WERE REMOVED AND REPLACED. NO MORE DAMAGES WERE FOUND. THE MINIMUM IDLE LEAK CHECK TEST WASDR FDEA202410011412Engine · damagedSTARTING CLIMB FROM FL380 TO FL400. WHEN THRUST STARTED TO INCREASE, FELT A MAJOR JOLT FOLLOWED BY MAJOR VIBRATIONS, SMOKE & FUMES IN COCKPIT. LT GEN DRIVE & L ENG OIL PRESSURE LIGHTS ILLUMINATED. DONNED MASKS, DECLARED EMERGENCY & RAN CHECKLISTS. SHUTDOWSDR I5PA2024093088801Engine · overtempFLT NO: MGE301. EVENT - RH ENG OVERTEMP BEFORE V1, ABORTED TAKEOFF EGT 665. PERFORMED PROCEDURES IAW AMM 72-00-00-519-P00 CHART B. NO DEFECTS FOUND. ACFT OK FOR SERVICE.SDR IPXA2024100454655Engine · leakingON DEPARTURE , AT HIGH POWER SETTING, STRONG SMELL OF DIRTY SOCKS? ON FLIGHT DECK. DISSIPATED AFTER POWER REDUCTION T/S PER B767 FIM79-21FAULT TREE 807,PERFROMED BOROSCOPE INSPECTION IAW B767 AMM 72-00-00-211-801. ON THE #1 ENG .FOUND OIL POOLED AT THE 6 O`CLOSDR IPXA2024093054655Engine · leakingON DEPARTURE , AT HIGH POWER SETTING, STRONG SMELL OF DIRTY SOCKS? ON FLIGHT DECK. DISSIPATED AFTER POWER REDUCTION T/S PER B767 FIM79-21FAULT TREE 807,PERFROMED BOROSCOPE INSPECTION IAW B767 AMM 72-00-00-211-801. ON THE #1 ENG .FOUND OIL POOLED AT THE 6 O`CLO
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