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 ASMF200512004Engine · flamed outAC PERFORMED AN UNSCHEDULED LANDING, FWD AND AFT FUEL PUMP LIGHTS TURNED ON AND RT ENGINE FLAMED OUT ON FLIGHT AND DURING LANDING THE TIRES POSITION 4 AND 8 WAS FLATTED. THE TIRES POSITION 3, 4, 7 AND 8 WERE REPLACED IAW MM 32-45-01 PAGE 401. DURING MAINTENANCSDR ASMF200512003Engine · noneAIRCRAFT RETURNED TO PLATFORM, DURING TAXING THE LT ENGINE WAS SHUTOFF WITH 420 OF EGT. DURING MAINTENANCE REVISION, THE LT ENGINE PARAMETERS WAS VERIFIED FINDING WITHIN LIMITS IAW MM 71-00-00. THE LT ENGINE WAS STARTED AND THE OPERATIONAL TEST WAS PERFORMED ISDR ASOA05915Engine · malfunctionedFLT 4086 - DURING DESCENT INTO ATL FROM AGS, AT APPROX 9,000 FEET THE CREW NOTICED THE RIGHT ENGINE TORQUE AT APPROX 20 PERCENT AND THE NP AT APPROX 35 PERCENT WITH ALL OTHER INDICATIONS SHOWING NORMAL WHICH WAS FOLLOWED BY A LARGE YAW TO THE RIGHT AND VIBRATISDR I5HA058009Engine · shutdownWHILE ENROUTE, THE CREW OBSERVED THE LT OIL QUANTITY GO TO ZERO. THE CREW PERFORMED A PRECAUTIONARY ENGINE SHUTDOWN AND DIVERTED. INSPECTION REVEALED OIL LEAKING FROM THE STRATER O`RING. THE O`RING WAS REMOVED AND REPLACED AND THE AIRCRAFT RETURNED TO SERVISDR CA051130005Engine · failed(CAN) NR1 ENGINE THE AUTO FEATHER SYSTEM WAS ARMED FOR TAKEOFF. SHORTLY AFTER TAKEOFF THE PILOT DISARMED THAT AUTO FEATHER SYSTEM. THE AIRCRAFT CONTINUED TO CLIMB OUT. THE PILOT NOTICED PROPELLER RPM SLOWLY DROPPING OFF (SUCH AS PROPELLERS OUT OF SYNC). THE PSDR 2005UALA01338Engine · bird ingestionMULTIPLE BIRD STRIKES ON CLIMBOUT, LITE SMOKE ODOR THROUGHOUT CABIN. AIRFRAME AND NR 2 ENG DAMAGED. AMBER ALERT DECLARED AND RETURNED TO FIELD. BIRD STRIKE CAUSED THE RTF. DAMAGED FAN BLADES WERE REPLACED AND THE LPC AND HPC WERE BORESCOPE INSPECTED AND FOSDR DHL2005745013Switch · malfunctionedDURING TAKEOFF ENG NR 2 WAS NOT MAKING TAKEOFF THRUST. ENG NR1, NR3 WERE NORMAL AT 80 KTS WITH THRUST LEVERS MATCH, NR2 EPR WAS AT 1.6 NOT INCREASING, N1 WAS ABOVE RED LINE. REJECTED T/O AT 80KTS,170,000 LBS 3860 PRESSURE. ENGINE RUNUP PERFORMED IAW JRH. NSDR CA051129018Engine · flamed outDURING A TRAINING FLIGHT, THE ENGINE FLAMED OUT WHEN THE POWER LEVEL WAS RETARDED TO IDLE POSITION. A SUCCESSFUL IN-FLIGHT RE-LIGHT WAS ACCOMPLISHED. P&WC WILL MONITOR INVESTIGATION OF THE INCIDENT AND WILL ADVISE OF ROOT CAUSE ONCE DETERMINED.SDR ANCF200400062Engine · malfunctionedDURING TAKEOFF AND AFTER TAKEOFF THRUST WAS APPLIED, RT ENGINE ACCELERATION WAS VERY SLOW AND STOPPED AT 1.7 EPR. ACCELERATION TO 2 EPR WAS REACHED MOVING RT POWER LEVER MANUALLY. WHEN RT ENGINE REACHED 2 EPR N1 INDICATION STARTED FLASHING AND INDICATION WAS 1SDR CALA0500414Engine · failedTHE NR 1 ENGINE SHUDDERED AND AUTO SHUTDOWN WHILE ON APPROACH TO IAH. THE CREW DECLARED AN EMERGENCY AND LANDED AT IAH WITHOUT INCIDENT. INITIAL EXAMINATION OF THE ENGINE REVEALED THAT THE NR 1 ENGINE INLET AND EXHAUST WERE CLEAN. THE NR 1 ENGINE WAS REMOVESDR EMB05017Control Quadrant · unknownENGINE NR 2 WOULD NOT START. AIRFLOW APPEARS NORMAL FOR START CONFIGURATION, NO N2 OR N1 ROTATION. AIRCRAFT RELEASED ON MEL. 11/23/05 - TROUBLESHOT SYSTEM, REMOVED AND REPLACED THRUST CONTROL QUADRANT W/AUTO. OPERATIONAL CHECK IS GOOD ON GROUND RUN UP.SDR ANCF200400063Engine · unknownDURING CRUISE FLIGHT AT FL 310, LT OIL PRESS LIGHT CAME (ON) ON EOAP. LT OIL PRESS INDICATION FELL TO 0 WITH (35) AND (40) LIGHTS ON. LT OIL QUANTITY WAS NORMAL INDICATING 16 QTS. LT OIL TEMPERATURE REACHED 131. LT ENGINE WAS SHUTDOWN, FOLLOWING THE CHECKLSDR 2005UALA01319Engine · flamed outRIGHT ENGINE FLAMED OUT AFTER STALL. ACCOMPLISHED ENGINE TROUBLESHOOTING PER AMM71-00-02 WITH NO FAULTS FOUND. REPLACED MAIN ENGINE CONTROL (MEC) AND FUEL PUMP AS PRECAUTION. SHOP FINDINGS ON FUEL PUMP AND MEC FUEL PUMP BENCH TEST FOUND NO FAULTS. MEC BENCH TSDR 2005UALA01301Engine · surgesRETURNED TO FIELD AFTER THE NR 1 ENGINE SURGED. ECM SHOWS NO RECORD OF A SURGE/STALL. EEC/FADEC RECORDED NO STALL MESSAGE. FMU WAS REPLACED FOR N1 OVER SPEED AND CHANNEL B FAULT. FMU TEST SHOWS NO FAULT FOUND. CAUSE OF SURGE CAN NOT BE DETERMINED.SDR COMA0560628Engine · vibrationFLIGHT 5004 - DURING TAKEOFF, ROLL RECEIVED A LT ENGINE VIBRATION CAUTION, ABORTED TAKEOFF AND RETURNED TO GATE. PERFORMED AN INSPECTION OF THE MASTER CHIP DETECTOR, PERFORMED GROUND RUNS, DISCREPANCY COULD NOT BE DUPLICATED.SDR TIM2005F00013Engine · failedAIRCRAFT IN FLIGHT AT 13000 FT OIL PRESSURE AND TORQUE STARTS TO FLUCTUATED SLIGHTLY, MOMENTS LATER THE ENGINE FAILED. NO CAUSE FOR FAILURE HAS BEEN FOUND AT THIS TIME. THE ENGINE HAS BEEN TAGGED. THE ENGINE HAS 87.5 HOURS SINCE REPAIRS TO THE ENGINE AT AN SDR AALA20050761Engine · failedINFLIGHT, SHORTLY AFTER LEVEL OFF AT FL320, RIGHT ENGINE FAILED. RIGHT HAND ENGINE OIL QUANTITY AND PRESSURE WERE NORMAL. EXHAUST GAS TEMPERATURE REACHED 800 DEGREES BEFORE SHUTDOWN. NO FIRE INDICATION OCCURRED. LANDED ORD WITHOUT INCIDENT. REPLACED NUMBESDR CA051124007Engine · overheated(CAN) AS THE POWER LEVERS WERE ADVANCED TO 80 PERCENT THE FLIGHT CREW HEARD POPPING NOISES AND THE TAKEOFF WAS REJECTED. THE NR 2 ENGINE OVERHEAT LIGHT WAS ILLUMINATED AND THE ENGINE WAS SHUTDOWN. THIS ENGINE HAS BEEN REMOVED AND RETURNED TO MANUFACTURER FOR ESDR 2005UALA01285Compressor · stalledNR 1 ENGINE COMPRESSOR STALL. POWER LOSS AT FL360 FOR 8-10 SEC. ENGINE RECOVERED AND FLIGHT DIVERTED INTO DEN. COCKPIT CFDS INDICATED STALL. C3 FINDING DURING BORO MAY OR MAY NOT HAVE CONTRIBUTED TO THE STALL.SDR ALG2005F00108Engine · noisyLOUD HOWLING NOISE AT FLIGHT IDLE FROM THE ENGINE TRANSMISSION AREA. REPLACED ENGINE ASSEMBLY. (K)SDR 2005UALA01274Engine · power lossTHRUST LOSS OCCURRED MULTIPLE TIMES WITH NR 2 ENGINE. REMOVED AND ROUTED THE EEC, PERFORMED A DATA DUMP, NO FAULTS OR FAILURES FOUND. THE EEC BEING MADE SERVICEABLY AND RETURNED. REMOVED THE N2 TRANSDUCER ALTENATOR STATOR. CONPONENT PASSED ALL ELECTRICAL TESSDR AALA20050751Manifold · inoperativeLAX - LEFT ENGINE LOOP-A LIGHT FOLLOWED BY LEFT ENGINE FIRE WARNING DURING CLIMBOUT AT APPROXIMATELY 6000 FEET. THROTTLES TO IDLE AND LIGHTS AND WARNING WENT OUT. LEFT EXHAUST GAS TEMPERATURE AT TAKEOFF IN YELLOW ZONE. RIGHT ENGINE EXHAUST GAS TEMPERATURE NSDR AMTA200501070Module · damagedAT FL 330, NR 1 ENGINE HIGH VIB LIGHT CAME ON AND VIB INDICATED 4.5 UNITS ON CHANNEL A/B WHEN NR 1 THROTTLE WAS REDUCED TO IDLE VIB UNITS WERE IND. HIGH VIBRATION WAS INDICATED ON LOW SIDE ONLY. REPLACED FAN ASSEMBLY, THRUST RING, THRUST RING CARRIER AND AIRSDR 05FDEA03797Engine · malfunctionedABOUT 2-3 MIN AFTER BLEED SHUTDOWN, CREW GOT STICK SHAKER, A/S ALT LOSS WITH NR 3 ENG VIBRATION. BROUGHT NR 3 THROTTLE TO IDLE AND VIBRATION REDUCED BUT STILL NOTICEABLE & NR 3 EVM TURB MONITOR WAS CLIMBING THRU 4 TOWARDS 5. ELECTED TO SHUTDOWN NR 3 ENG & VISDR CA051115007Engine · unknown(CAN) RT ENG DID AN UNCOMMANDED INFLIGHT SHUTDOWN. TROUBLESHOOTING IN PROGRESS . WILL UPDATE FURTHER .SDR CA051116009Engine · shutdown(CAN) AFTER APPLYING TO POWER AND STARTING TO ROLL (APPROX 35KTS), NR 1 ENGINE SHUTDOWN WITH RELATED ECAM MESSAGE ENGINE FAIL . AIRCRAFT CAME BACK TO THE GATE. THERE WAS NO OBVIOUS DAMAGE TO THE ENGINE INTAKE AND EXHAUST. THE EEC WAS INTERROGATED AND MCDU AND SDR DXTA200501077Engine · malfunctionedLEFT ENGINE FAILED AFTER APPROXIMATELY 2-3 MINUTES OF GROUND RUN. PERFORMED ENGINE START UP AND GROUND RAN ACFT FOR 10 MIN. REPEATING PROCEDURE 3 TIMES. DURING RUNS SELECTED VARIOUS MODES OF OPS SUCH AS LT & RT BOOST PUMPS ON/OFF LOW & HIGH GRD IDLE. CABINSDR 111105N523CS1Engine · odorAIRCRAFT DEPARTED AND DURING INITIAL CLIMB OUT CREW NOTICED A LOSS OF OIL PRESSURE AND A SLIGHT ODOR FROM RT ENGINE. THE ENGINE WAS SHUT DOWN AND AN EMERGENCY WAS DECLARED. AIRCRAFT WAS REROUTED AND LANDED WITH NO FURTHUR PROBLEMS. THE ENGINE IS BEING REMOVESDR CA051129013Engine · smokeDURING CRUISE, THE ENGINE LOW OIL PRESSURE WARNING ANNUNCIATED ACCOMPANIED BY OIL SMOKE AND ODOR IN THE CABIN AIR. THE ENGINE WAS SHUT DOWN IN FLIGHT AND THE AIRCRAFT DIVERTED FOR AN UNSCHEDULED LANDING. P&WC WILL INVESTIGATE THE INCIDENT AND ADVISE OF ROOT SDR CA051129012Engine · flamed outDURING TAKEOFF, THE ENGINE FLAMED OUT. THE AIRCRAFT DIVERTED TO POINT OF DEPARTURE. P&WC WILL INVESTIGATE THE INCIDENT AND WILL ADVISE OF ROOT CAUSE ONCE DETERMINED.SDR DXTA200501072Engine · shutdownLEFT ENGINE SHUTS DOWN WHEN THROTTLE MOVED FROM CRUISE TO IDLE SETTING. ITEM IS UNDER INVESTIGATION.SDR MASA200500866Engine · flamed outASH 6183 PHX, NR 2 ENGINE FLAMED OUT ON TAXI OUT PREVIOUSLY DSM. ALL INSPECTIONS CHECKED GOOD PER FIM AND GE.SDR CED2006F00013Hose · leakingWHILE PASSING THROUGH FL320 ON CLIMB TO FL350, THE NR1 ENGINE ROLLED BACK TO 25 PERCENT. THE CREW REGAINED POWER AND CLIMBED TO FL350 AND LANDED WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED THE ENGINE TO INCLUDE BORESCOPE, AND REPLACED T2 HOSE. ENGINE FLSDR QXEA200501513Engine · malfunctionedMSO FLIGHT NR 2348 - DURING ENGINE START, FOLLOWING BRINGING PROPS OUT OF FEATHER, NR 1 ENGINE RETURNED TO FEATHER MODE WITH POWERPLANT MESSAGE AND NR 1 PEC CAUTION ILLUMINATED. MAINTENANCE INTERROGATED CDS. FOUND FAULT CODE 130. CLEARED FAULT CODE IAW Q400SDR CA051129017Engine · power lossDURING CRUISE, THE ENGINE EXPERIENCED AN UNCOMMANDED AND UNRECOVERABLE REDUCTION IN POWER ACCOMPANIED BY A REDUCTION IN FUEL FLOW AND COMPRESSOR SPEED. THE FLIGHT DIVERTED. P&WC WILL MONITOR THE INVESTIGATION OF THE EVENT AND WILL ADVISE OF ROOT CAUSE ONCE ESDR CA051129011Engine · malfunctionedDURING CLIMB, THE ENGINE EMITTED A LOUD NOISE AND SHUT DOWN UNCOMMANDED. SUBSEQUENT INSPECTION REVEALED DAMAGE TO THE TURBOMACHINE. P&WC WILL INVESTIGATE THE INCIDENT AND ADVISE OF ROOT CAUSE ONCE DETERMINED.SDR CA051129010Engine · failedON CLIMB, THE ENGINE WAS REPORTED TO HAVE EMITTED A NOISE ACCOMPANIED BY A LOSS OF POWER. THE AIRCRAFT DIVERTED TO DEPARTURE AND SUBSEQUENTLY CRASHED. MFG WILL INVESTIGATE THE INCIDENT AND WILL ADVISE OF ROOT CAUSE ONCE ESTABLISHED.SDR CA051129009Towershaft · fracturedTHE ENGINE FLAMED OUT DURING CLIMB. AN EMERGENCY WAS DECLARED AND THE FLIGHT DIVERTED. SUBSEQUENT INVESTIGATION REVEALED A FRACTURED TOWERSHAFT. P&WC WILL INVESTIGATE THE INCIDENT AND ADVISE OF ROOT CAUSE ONCE ESTABLISHED.SDR LNX2005F00001Engine · unknownAIRCRAFT WAS ON TAKEOFF ROLL FOR DEPARTURE. THE CREW WAS UNABLE TO ACHIEVE TARGET TORQUE ON THE RT ENGINE AND ABORTED THE ROLL. CAUSE OF LOW TORQUE COULD NOT BE ISOLATED TO AN EXTERNAL CAUSE AND THE ENGINE WAS REMOVED AND SENT TO THE VENDOR FOR EVALUATION. SDR ALG2005F00120Engine · failedON PRELANDING CHECK, ENGINE OIL PRESSURE DECREASED AND OIL TEMPERATURE INCREASED ABOVE THE RED LINE. ON LONG FINAL TO THE BASE, SHUTDOWN NR 1 ENGINE. AFTER LANDING, NOTIFIED MAINTENANCE. (K)SDR CA051109007Engine · fluctuates(CAN) INFLIGHT SHUTDOWN FROM TORQUE FLUCTUATIONS INDICATED IN CONJUNCTION WITH OIL PRESSURE FLUCTUATIONS. NO CHIP DETECTER LIGHT, NO OIL PRESSURE LIGHT. ENGINE SECURED BEFORE LOSS OF OIL PRESSURE MAINTENANCE CHECKED CHIP DETECTER, CLEAN. MAINTENANCE CHECKED SDR K2Z2005F00001Gasket · failedPILOT NOTED DROP IN ENGINE OIL PRESSURE IN CRUISE FLIGHT. POSTFLIGHT INSPECTION REVEALED SILICON GASKET (SUCKED) INTO THE ROCKER BOX ALLOWING SUBSTANTIAL OIL LOSS. ENGINE SHUTDOWN, PROP FEATHERED, PRECAUTIONARY LANDING ACCOMPLISHED WITHOUT INCIDENT. (K)SDR 0501599943Engine · smokeAFTER TAKEOFF FLIGHT ATTENDANTS AND PASSENGERS COMPLAINED OF SMOKE IN THE CABIN. FLIGHT CREW RETURNED AIRCRAFT TO DEPARTURE AIRPORT. MAINTENANCE REPLACED ENGINE NR 1.SDR S2YA05074Eec · malfunctionedSHORTLY AFTER TAKEOFF, THE CREW REPORTED A LT FADEC MAJOR CAS MESSAGE. MX REQUESTED THE PERFORMED AN AIR-TURN-BACK, BECAUSE OF PRIOR HISTORY (LISTED BELOW). MX REPLACED TWO RELAYS AND SCHEDULED A TEST FLIGHT. AFTER THE TEST FLIGHT, HAD NO DISCREPANCIES THE SDR 2005FA0001554Plate · crackedDURING MAJOR INSPECTION THE NR 1 COOLING PLATE WAS FOUND TO HAVE CRACKS IN (SURFACE M). THERE ARE 6 EA CRACKS APPROXIMATELY .250 IN LENGTH. THE OVERALL GOOD, AND THERE WAS NO EVIDENCE OF AN OVERTEMPATURE ON ANY PARTS. (K)SDR WRLA2005146Engine · overheatedBRU-DAY DIVERSION TO YYZ BECAUSE OF NR 1 ENGINE HIGH EGT AND HIGH FUEL FLOW. BEGINNING/DURING DESCENT INTO YYZ THE ENGINE FIRE WARNING BEGIN FLICKERING LIGHT AND ENGINE WAS SHUTDOWN PER ENGINE FIRE/FAILURE CHECKLIST. FLICKERING LIGHT WAS IN FIRE HANDLE AND SSDR C2XA05BT078Heat Shield · brokenDURING ROUTINE CHECK MAINTENANCE FOUND THE NR 1 ENGINE REAR TURBINE BEARING SUPPORT HEAT SHIELD BROKEN, DAMAGED TWO REAR TURBINE BEARING SUPPORT STRUTS/PYLONS (P/N 23077731). THE 11 O`CLOCK POSITION STRUT HAD BEEN CUT 0.25 INCHES THROUGH AND THE 1 O`CLOCK POSSDR PCSA11030501Engine · vibrationWHILE IN CRUISE, CREW REPORTED VIBRATION ON THE CENTER CONSOLE, WHEN NR 1 ENGINE THROTTLE WAS PULLED BACK VIBRATION SEEMS TO DIMINISH. AIRCRAFT RETURNED AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED ALL 3 ENGINES, INTAKES, AND EXHAUST, NO DAMAGE FSDR CA051129008Engine · fireDURING AEROBATIC MANEUVERS (RAYTHEON T-6A) SMOKE AND FUMES BECAME EVIDENT IN THE COCKPIT. P&WC WILL MONITOR INVESTIGATION OF THE INCIDENT AND WILL ADVISE OF ROOT CAUSE ONCE ESTABLISHED.SDR ALG2005F00119Engine · failedIN FLIGHT, NR 1 ENGINE T-5 INCREASED IN TEMPERATURE, AFTER LANDING, NOTIFIED MAINTENANCE. A POWER CHECK REVEALED THAT NR 1 ENGINE WAS A -7. REMOVED AND REPLACED ENGINE WITH A SERVICEABLE ASSEMBLY IAW MM. (K)
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