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 CA131104021Engine · fluctuates(CAN) THE PILOT WAS REQUIRED TO USE EMERGENCY PROCEDURE DUE TO A TORQUE FLUCTUATION FROM THE NR 2 ENGINE. INVESTIGATION IS ONGOING.SDR CA131104020Engine · fluctuates(CAN) THE PILOT WAS REQUIRED TO USE EMERGENCY PROCEDURE DUE TO A TORQUE FLUCTUATION FROM THE NR 1 ENGINE. INVESTIGATION IS ONGOING.SDR WI5R2013101800001Rotor · crackedENGINE, SN 211176 WAS REMOVED FOR INVESTIGATION OF THE AN IP ROTOR BLADE ANOMALY. THE INVESTIGATION REVEALED A CRACK ON 1 OF THE 1ST STAGE BLADES AT THE ROOT RADIUS.SDR GTIA201310161005Engine · fireAIR RETURN DUE TO NR 1 ENGINE FIRE. ENGINE SHUTDOWN IN FLIGHT, SMOKE IN COCKPIT. NR 1 ENGINE CHANGED IAW AMM.SDR SIMA20131014005Engine · vibrationDURING CLIMBOUT MID 20K IN ALTITUDE, NR 1 ENGINE HP VIBRATION GAUGE JUMPED INTO THE AMBER, ABOUT .33 -.5 UP. VIBRATION CHANGED WITH REDUCTION INCREASED WITH ADVANCEMENT. SEEMED WORSE BETWEEN FL 250 AND FL 320. R & R NR 1 ENGINE IAW 71-000-00. OPS & LEAK CHSDR CA131104019Engine · overspeed(CAN) THE PILOT ELECTED TO SHUT THE NR 1 ENGINE DOWN DUE TO A PROPELLER OVERSPEED INDICATION. THE EMU DATA DOWNLOAD CONFIRMED THE OVERSPEED WITHIN ACCEPTABLE TOLERANCES FOR THE PROPELLER AND CONTROL SYSTEM. THE INVESTIGATION IS ONGOING TO DETERMINE THE ROOT SDR WX0A201310280039Engine · power lossAT APPROXIMATELY 1000 FT AGL, RT ENGINE LOST POWER, AND INDICATED APPROXIMATE IDLE CONDITIONS, NO OVERWIEGHT LANDING MADE 124,000 LBS.SDR GLBA2013101400339Engine · making metalDURING DESCENT, TORQUE ON NR 2 ENGINE DECREASED TO APPROX 400 LBS AND ITT INCREASED TO ABOVE 800 CELSIUS F/O SAW FLAMES COMING OUT BOTH EXHAUST STACKS ON NR 2 ENGINE. SECURED ENGINE USING APPROPRIATE CHECKLISTS. MAINTENANCE FOUND PROPELLER STIFF. FOUND DAMASDR CALA2013101592055Engine · making metalENG 2 STALL ECAM, FLT DIVERTED. EXAMINE THE INLET & EXHAUST FOR FOREIGN MATERIAL OR INDICATION OF INTERNAL ENG DAMAGE. IAW MM TASK 71-00-00-810-809-A, INSPECTED ENG FOUND METAL PIECES IN TAILPIPE.SDR CA131021016Engine · unknown(CAN) ENGINE HAD AN EVENT DURING FLIGHT, CAUSING THE SHUTDOWN OF THE LT ENGINE. THE PILOT PERFORMED AN UNEVENTFUL SINGLE ENGINE LANDING.SDR CA131021013Engine · unknown(CAN) UPON LANDING, THE ACFT EXITED THE RUNWAY. DURING THE ON GROUND INVESTIGATION, THE ENGINEER AND THE PILOT ON SITE TRIED TO START THE ACFT ENGINES AND THE LT ENGINE ACCELERATED UNCONTROLLABLY CAUSING THE ITT TO FLASH AMBER AND THE TORQUE TO FLASH RED MOMESDR CA131021008Engine · malfunctioned(CAN) ON LANDING, THE ACFT EXITED THE RUNWAY. DURING THE ON GROUND INVESTIGATION, THE ENGINEER AND THE PILOT ON SITE TRIED TO START THE ACFT ENGINES AND THE LT ENGINE ACCELERATED UNCONTROLLABLY CAUSING THE ITT TO FLASH AMBER AND THE TORQUE TO FLASH RED MOMENTSDR ASAA2013101096157Engine · malfunctionedNR 2 ENGINE SLOW TO SPOOL TO 20 ON START. ACFT GROUNDED. DRY MOTORED NR 1 AND NR 2 ENGINES. BOTH ENGINES CRANKED TO 20-N2 IN 14 SECS. STARTED NR 1 AND 2 ENGINES IAW NORMAL START CHECKLIST. BOTH ENGINES STARTED NORMAL.SDR DTHA201310100033Engine · smokeSHORTLY AFTER TAKEOFF LAV SMOKE INDICATION IN EICAS FIELD WITH STRONG OIL SMELL IN CABIN AND COCKPIT. RETURNED TO FIELD. AFTER INSPECTION IT WAS FOUND THAT OIL CONTAMINATION WAS ENTERING THE BLEED SYS FROM THE COMPRESSOR SECTION OF THE ENGINE. IT WILL NOT BSDR ASAA2013100896134Engine · making metalMCD CHECK FOUND LARGE AMOUNT MAGNETIC MATERIAL ON FWD SUMP CHIP DETECTOR NR 1 ENGINE. ACFT GROUNDED. REPLACED NR 1 ENGINE, REF TASK CARDS 78471000, 78471001 UNDER W/O 229458.SDR DXTA2013100705531Engine · odorSMOKE IN CABIN AT FL 430. DURING CLIMBOUT ABOUT 14,000 APU SYS FAIL ANNUNCIATOR CAME ON AND APU SHUTDOWN. APU GEN HAD BEEN OFF, BUT BLEED AIR ON. APPROX 30 MINUTES LATER, LEVEL AT FL 430 ADVISED OF A LITTLE SMOKY IN CABIN. FINE GREY ENVIRONMENTAL SMOKE/HAZE SDR FDEA201310072434Engine · failedDURING CLIMBOUT, NR 1 ENGINE OVERTEMPED. HEARD A LOUD POP WITH A YAW TO THE LEFT. ALL ENG INDICATIONS WERE NORMAL EXCEPT EGT WHICH WAS 700 DEGREES HIGHER THEN NR 2 EGT, NR 1 EGT STAYED BEWTEEN 600 TO 700 DEGREES. DURING RETURN, MAX EGT 1000 FT. REMOVED ANDSDR CALA2013100991913Engine · malfunctionedDUE TO ENG BLEED "OFF" LIGHT ON ENG START & NO DUCT PRESS. PRECAUTIONARY CHANGE PREVIOUS. DUE TO ENG BLEED "OFF" DURING ENG START, REPLACED NR 1 ENG PREVIOUS IAW AMM 36-11-18,401. ACP OPERATIONS CHECKED WITH ENG RUN OK.SDR HALA2013100700124Engine · making metalNR 2 ENGINE OIL CHIP DETECTED, ILLUMINATED AFTER TOUCHDOWN. REMOVED NR 2 ENGINE IAW 7100-9401-02. INSTALLED NR 2 ENGINE IAW TASK CARD 7100-9401-02.SDR CA131021005Engine · unknown(CAN) THE TAKEOFF WAS ABORTED DUE TO NO ENGINE RESPONSE TO POWER LEVER MOVEMENT. A PNEUMATIC LEAK WAS SUSPECTED. THE INVESTIGATION IS ONGOING.SDR DXTA2013100705529Engine · smokeAFTER TAKEOFF, HAD SMOKE IN COCPIT AND CABIN. WENT THROUGH EMERGENCY PROCEDURE DUMPED CABIN AND WENT TO RAM. SMOKE STOPPED AND LANDED IMMEDIATELY. REMOVED AND REPLACED ENGINE. ALL WORK PERFORMED IAW G200 AMM 71-00-00 AND PW306 EMM 71-00-00.SDR SWAA2013100920994Engine · malfunctionedAIR TURN BACK DECLARED EMERGENCY. RT ENGINE COMP STALL ALERT DISPLAYED DURING CLIMB ALONG WITH AUDIBLE SOUNDS & SLIGHT AIRCRAFT YAWING & POWER LOSS. R &R NR 2 ENGINE IAW TC.SDR CALA2013100791800Engine · malfunctionedNR 1 ENG EGT & N1 RED LINED, RTFL. NR 1 ENGINE EGT & N1 RED LINED DURING TAKE-OFF 3,000 TO 4,000 FT THEN RETURNED TO NORMAL OPERATING PARAMETERS WITH SLIGHT ENG VIBRATION. ON FINAL LANDING APPROACH VIBRATIONS & SURGING CONTINUED UNTIL ENG WAS SHUT DOWN AFTER SDR CA131021007Engine · overheated(CAN) AT FL180 DESCENDING, TWO HEAVY NOISES WERE HEARD FROM NR 2 ENGINE. THE ITT RAISED UP TO 900C THEN DROPPED CONSTANTLY AND THE TORQUE WENT DOWN TO ZERO. THE POWER LEVER WAS MOVED WITHOUT ANY EFFECT. THE ENGINE WAS THEN SHUTDOWN IAW CHECK LIST. AN UNEVENTSDR CA131021004Engine · unknown(CAN) THE ACFT HAD AN EMERGENCY LANDING AFTER 1.2 HRS. FLIGHT DUE TO SUDDEN YAW TO THE LT DURING CRUISE AT 130 KTS FOLLOWED BY KNOCKING/BANGING/POPPING SOUND. THE ACFT SYS IS SHOWING TORQUE SPLIT AND TORQUE OSCILLATION BEFORE LANDING. AWAITING RESULTS OF THSDR HALA2013100400128Pmc · malfunctionedDURING SHORT FINAL, EICAS MESSAGE RT EEC AND AUTO THROTTLE DISCONNECT ILLUMINATED. R & R RT ENG PMC. OPS NORMAL IAW AMM73-21-07. R & R RT ENGINE T12 SENSOR, IAW AMM 73-21-10.SDR CALA2013100791816Engine · bird ingestionHI SPEED ABORT AT 110KTS, DUE TO BIRD STRIKE ON LT MOTORSDR CA131007014Engine · malfunctioned(CAN) THE PILOT REPORTED THE ENGINE NR 2 HAD AN UNCOMMANDED POWER CHANGE. EVENT DETAILS ARE NOT AVAILABLE. THE CUSTOMER ENGINEERING OFFERED TROUBLESHOOTING ASSISTANCE TO PORTER.SDR AALA20131003015Compressor · stalledBHM CREW REPORTED ON CLIMB OUT, RT HAND ENG ENCOUNTERED 2 SUCCESSIVE COMPRESSOR STALLS. EMERGENCY DECLARED FLIGHT RETURNED BHM LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE FOR REPAIR. REPLACED RT HAND ENGINE AT BHM ON 10/04/2013. SYSTEM GROUND CHSDR UHLA2013100300478Engine · vibrationDURING CLIMB, NOTICED VIBRATION FROM RT ENGINE, VIBRATION REDUCED WITH POWER REDUCED. RECEIVED ENG 2 T2 HEAT FAIL MESSAGE, RAN QRH. ATC REPORTED AFTER TAKE OFF, TIRE RUBBER ON RUNWAY. DIVERTED, DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. MX R & R ENGINE ASDR CA131007013Engine · malfunctioned(CAN) DURING TAKEOFF ROLL, A STRONG NOISE WAS HEARD FROM ONE ENGINE ACCOMPANIED BY ACFT YAW TO THE LT. THE TAKEOFF WAS ABORTED AT A SPEED OF 60 TO 70 KTS AND THE ACFT RETURNED TO THE RAMP. EXTENSIVE TROUBLESHOOTING IS ON-GOING AND GROUND RUNS COULD NOT REPRODSDR CA131007012Engine · smoke(CAN) SHORTLY AFTER TAKEOFF, A FIRE INDICATION OCCURRED FOLLOWED BY SMOKE IN THE CABIN. THE PILOT SHUT THE ENGINE DOWN AND THE FIRE INDICATION DISAPPEARED. THE ACFT RETURNED TO THE DEPARTURE AIRPORT WHERE AN UNEVENTFUL SINGLE ENGINE LANDING WAS ACCOMPLISHED. SDR ASAA2013100296222Engine · malfunctionedDURING CLIMB, THROUGH APPROX FL 320, NR 2 ENGINE PARAMETERS BEGAN FLUCTUATING. N1 VARIED /- 3-5 . TURNED AUTO THROTTLES OFF, REDUCED THRUST, FLUCTUATIONS CONTINUED. LEVELED OFF FL 350 FLUCTUATIONS SLOWLY DISSIPATED TO NORMAL WITHIN ABOUT 30 SECONDS. FIRST FSDR Y2PA20131002052Engine · flamed outCREW REPORTED THAT DURING LEVEL OFF AT FL340, RT ENGINE FLAMED OUT. DESCENDED TO FL290, NORMAL RELIGHT, DIVERTED. ACFT LANDED WITHOUT INCIDENT. MX WAS SENT TO ACFT. MX INSPECTED THE RT ENGINE FOR FLAMEOUT IAW SEI-187 MM, CHP 72-00, TABLE 101 TROUBLESHOOTINSDR CA131007024Engine · flamed out(CAN) AT TOP OF DECENT, THE NR 2 ENGINE FLAMED OUT. ENGINE FLAMEOUT CHECKLIST WAS COMPLIED WITH AND THE ENGINE WAS RESTARTED. THE NR 2 ENGINE FUEL FILTER WAS INSPECTED, AND REPLACED. THE FUEL S/O VALVE WAS FUNCTION CHECKED WITH NO FAULTS FOUND. ENGINE RUNS SDR CALA2013093091580Engine · oil consumptionNR 1 ENG HIGH OIL CONSUMPTION EXCEEDS LIMIT. MAY CONTINUE IN SERVICE IN NON ETOPS WITH RED LIMIT IAW SAMC APPROVAL & MM 79-00-95. ACCOMPLISHED CHECK IAW MM79-00-95 PG 2 NO EXTERNAL LEAKAGE NOTED OR FROM DRAIN TUBES.SDR CA131007010Engine · smoke(CAN) AFTER TAKEOFF, WHITE SMOKE STARTED ENTERING THE CABIN. THE CREW ELECTED TO RETURN TO THE DEPARTURE AIRPORT WHERE AN UNEVENTFUL LANDING WAS ACCOMPLISHED. POST FLIGHT TROUBLESHOOTING ISOLATED THE PROBLEM TO THE NR 2 ENGINE. TEST RUNS SHOWED SMOKE INCREASINSDR CA130930005Engine · vibration(CAN) IT WAS REPORTED THAT ACFT HAD TO SHUTDOWN NR 2 ENGINE IN FLIGHT, AFTER A HIGH LEVEL OF VIBRATIONS WAS SENSED AND RT ENGINE VIB AMBER CAS MESSAGE DISPLAYED.SDR AALA20130928008Engine · failedJFK CREW REPORTED LOSS OF LT ENGINE OIL PRESSURE. ASSOCIATED EICAS "OIL PRESSURE" MESSAGE. CREW SHUTDOWN ENGINE. EMERGENCY DECLARED FLIGHT RETURNED JFK LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED LT ENGINE AT JFK ON 09/29/2013. SYSTESDR CALA2013093091564Liner · damagedREPAIRED AREA OF RT ENGINE ACOUSTIC LINER HAS GASPER REPAIR FAILURE. LCL MX REPORTED FAN CASE ATTRITION LINER APPROXIMATELY 9"0 CLK ON ENGINE 2, MISSING MATERIAL APPROXIMATELY 1.5 INCH BY 0.5 INCH, WITHIN CARRY FORWARD LIMITS OF AMM MT72-017. TO BE REPAIRED SDR CA131007011Engine · surges(CAN) AFTER TAKEOFF PASSING FL17, THE ENGINE SURGED AND THE POWER ROLLED BACK TO 60-70 PERCENT FOR APPROX 3 SEC. BEFORE IT RECOVERED TO 100 PERCENT. ALL PARAMETERS REMAINED NORMAL AFTER THE EVENT. POST FLIGHT TROUBLESHOOTING IS FOCUSING ON A POSSIBLE FAULTY SDR SIMA20130926005Engine · power lossCREW REPORTED DURING DEPARTURE, BETWEEN 80KTS AND V1., ACFT FELT SLIGHT YAW MOVEMENT TO THE SIDES. AT THE SAME TIME THE F/O CALLED FOR AN ABORT DUE TO LT ENGINE POWER LOSS. CREW INITIATED ABORT PROCEDURES. COMPLETED ENGINE SHUTDOWN PROCEDURES. INFORMED OFSDR UIEA2013092700509Engine · vibrationSIGNIFICANT VIBRATION LT ENGINE ALL RANGE OF RPM. REPAIRED IAW SOPM 20-20-01 AND 20-41-02.SDR CA131021001Engine · inoperative(CAN) SHORTLY AFTER TAKEOFF, THE ACFT CRASHED IN A FIELD WITHIN AIRPORT BOUNDARY. THE LT ENGINE WAS PRODUCING NO POWER. THE BEA HAS ASKED FOR ENGINE MFG ASSISTANCE FOR THE INVESTIGATION OF THE ENGINES WHICH WILL TAKE PLACE AT A LATER DATE.SDR CA131007005Engine · power loss(CAN) APPROXIMATELY 30 MIN INTO A FLIGHT, THE POWER STARTED TO GRADUALLY DECREASE. THE PILOT DIVERTED THE FLIGHT AND LANDED SAFELY. POST FLIGHT ENGINE RUN UP RESULTED IN THE ENGINE HANGING AT 38 PERCENT COMPRESSOR SPEED. TROUBLESHOOTING IS ON-GOING.SDR CA131007004Engine · fluctuates(CAN) THE OPERATOR REPORTED A RECENT HISTORY OF POWER FLUCTUATIONS DURING WHICH IN WORST CASES, THE POWER WOULD DROP TO VERY LOW TORQUE AND THE ENGINE WOULD THEN RECOVER TO SET POWER.SDR 2013FA0000650Bearing · failedPILOT HEARD UNUSUAL NOISE DURING START, JUST BEFORE IGNITION, 10-12 PERCENT OF N1. DESCRIBED NOISE AS A "RUMBLING-GEAR TEETH OUT OF MESH" SOUND FROM ENGINE ACCESSORIES GEARBOX. MAGNETIC METAL DETECTORS WERE FUNCTIONING BUT THE CAUTIONARY LIGHT IN THE COCKPISDR MTNA201309250001Engine · malfunctionedDURING TAKEOFF ROLL, THE FLIGHT CREW REPORTED THE LT ENGINE TORQUE DECREASED BY 40 PERCENT. ACFT EXPERIENCED A YAW TO THE LEFT. ABORTED THE TAKEOFF AND RETURNED TO THE RAMP WITHOUT FURTHER INCIDENT.SDR YYFA20130927003Engine · malfunctionedACFT RETURNED, NR 2 ENGINE WILL NOT ACCELERATE PAST IDLE, NR 2 ENGINE FAILED. BOROSCOPE C-7 DAMAGE.SDR CA131007003Engine · failed(CAN) 5 MINUTES AFTER TAKEOFF, THE PILOT NOTICED A VIBRATION AND OBSERVED THE NR 2 ENGINE OIL PRESSURE HAD DROPPED TO ZERO. THE ENGINE THEN SHUTDOWN BY ITSELF. THE ACFT RETURNED TO THE DEPARTURE AIRPORT WHERE A SINGLE ENGINE LANDING WAS SAFELY ACCOMPLISHED.
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