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 AALA20130630003Engine · malfunctionedSMOKE IN THE MID GALLEY & FORWARD, MID LAVATORY SMOKE ALARMS WENT OFF. EMERGENCY DECLARED FLIGHT RETURNED LAX LANDED WITHOUT INCIDENT. ACFT FERRIED TO TUL FOR FURTHER MX. REPLACED RT ENGINE AT TUL. SYSTEM GROUND CHECKED NORMAL.SDR UALA2013070204606Liner · damagedAPPROX FOUR INCHES OF THE ACCOUSTIC MATERIAL IS MISSING AT THE 11 O'CLOCK POS, NR 1 ENGINE. NR 1, FAN CASE ATTRITION LINER AT 1 O`CLOCK DAMAGE 4.5" X 2.5", WITHIN LIMITS OF AMM MT72-017 . REPAIRED ATTRITION LINER IAW AMM MT 72-017.SDR CA130701016Engine · unknown(CAN) FOLLOWING REPORTED MECHANICAL ISSUES, POSSIBLY ENGINE RELATED, THE CREW ATTEMPTED A FORCED LANDING DURING WHICH THE ACFT EXITED THE LANDING STRIP BEFORE HITTING 2 TRENCHES AND A PERIMETER FENCE. THE STRIP WAS APPARENTLY UNDER CONSTRUCTION. NO ONE ON BOSDR CA130701015Engine · warning light(CAN) DURING T/O ROLL, A LOUD NOISE WAS HEARD FOLLOWED BY A MASTER WARNING FOR ENGINE VIBRATIONS. THE T/O WAS ABORTED AND THE A/C EXITED THE RUNWAY SAFELY. POST EVENT INSPECTION FOUND THAT THE FAN COULD NOT BE ROTATED.SDR ASAA2013062695346Unknown · unknownABORTED NR 1 ENGINE START, DUE TO 0 FUEL FLOW. SECOND START ATTEMPT ABORTED, DUE TO FF BUT NO LIGHT OFF. THIRD START ATTEMPT SUCCESSFUL WITH BOTH SELECTED ON IGN. FIRST TWO START ATTEMPTS WERE MADE ON RT IGN. ACFT GROUNDED. ACCOMPLISHED BITE & OPS CHECK, SDR CA130709005Engine · failed(CAN) PRECAUTIONARY SHUTDOWN OF THE RT ENGINE DUE TO LOUD BANG, AIRFRAME VIBRATION, SMELL OF BURNED ENGINE OIL, AND HIGH ITT. REMOVED RT ENGINE AND SENT FOR REPAIR. WILL UPDATE SDR FOR THE ENGINE SHUTDOWN CAUSE ONCE A TEARDOWN REPORT HAS BEEN PROVIDED.SDR CA130701011Engine · power loss(CAN) DURING FLIGHT, THE ENGINE POWER ROLLED BACK BY 6 PERCENT UNCOMMANDED. THE ACFT LANDED SAFELY, TROUBLESHOOTING IS ON-GOING.SDR CA130701013Engine · power loss(CAN) DURING T/O, THE ENGINE LOST POWER. THE FLIGHT RETURNED TO THE POINT OF DEPARTURE WHERE AN UNEVENTFUL SINGLE ENGINE LANDING WAS PERFORMED. NO OTHER DETAILS ARE AVAILABLE AT THIS TIME. THE AUTHORITIES ARE INVESTIGATING.SDR CA130625001Engine · unknown(CAN) ENGINE WAS SENT FOR INVESTIGATION AND REPAIR AFTER THE OPERATOR REPORTED POOR PERFORMANCE. THE OPERATOR REPORTED THAT THE ENGINE STARTED HOTTER THAN NORMAL AND WAS SURGING.SDR UALA2013062404385Engine · surgesRT ENGINE SURGED, RETURNED TO FIELD.SDR CA130701010Engine · making metal(CAN) DURING CRUISE, THE PILOT INITIATED AN ENGINE SHUTDOWN FOLLOWING A LOW OIL PRESSURE WARNING. THE FLIGHT RETURNED TO THE POINT OF ORIGIN WHERE AN UNEVENTFUL SINGLE ENGINE LANDING WAS ACCOMPLISHED. POST FLIGHT INSPECTION FOUND METAL DEBRIS ON THE TURBOMACSDR UALA2013062104315Unknown · vibrationLEFT ENGINE RUMBLING NOISE AT LOW POWER FELT AND HEARD. SEEMS TO SMOOTH OUT AT HIGHER POWER SETTINGS. N1 VIB IND 1.1. FOLLOWS THROTTLE MOVEMENT. ACOMPLISHED BORESCOPE INSP IAW MM 72-00-00. CHECKED ALL CHIP DETECTORS, NO DEFECT FOUND. RAN THE ENGINE IAW JRH SDR ASOA201306200050Engine · smokeCREW REPORTED LAV SMOKE INDICATION ON EICAS DURING CLIMBOUT. VISUAL INDICATION OF SMOKE IN CABIN, CREW PERFORMED AN AIR RETURN, DECLARING AN EMERGENCY. MX INSPECTED AND R & R THE RT ENGINE ASSYSDR CA130701007Engine · power loss(CAN) AFTER 40 MINUTES FLIGHT, THE ENGINE NR 2 HAD A POWER ROLLBACK AND TORQUE LOSS DUE TO WATER INGESTION DURING MODERATE RAIN. INVESTIGATION ONGOING.SDR SWAA2013061917352Engine · leakingAIR TURNBACK ON INITIAL CLIMB OUT. F/A REPORT VERY STRONG ODOR IN CABIN AGAIN. FOUND INTEGRAL OIL LEAK AT NR 2 ENGINE. R & R NR 2 ENGINE IAW MT.SDR 2013FA0000357Engine · overtempDURING CRUISE FLIGHT, NR 2 ENGINE TEMPERATURE STARTED TO APPROACH UPPER LIMITS. EMERGENCY PROCEDURES WERE COMPLETED IAW THE EMERGENCY CHECKLIST. THE ACFT DIVERTED TO THE NEAREST AIRFIELD AND AN UNEVENTFUL LANDING WAS PERFORMED.SDR UALA2013061704182Unknown · leakingNR 2 ENG HAS EXCESSIVE OIL DRIPPING FROM FAN COWL. PERFORMED AMM 71-71-00 INSP FOR LEAKS FOUND ACCUMULATION JUST AFT OF TOWER SHAFT. SUSPECT BREATHER AIR BUILD-UP, NO LEAKS FOUND.SDR MASA2013061852487Engine · fodFOD EVENT DURING GROUND OPERATIONS, ENGINE WAS INSPECTED AND ACFT FERRIED TO MX BASE FOR ENGINE REPLACEMENT.SDR ASOA20130614331Engine · overspeedACFT WAS ON TAXI WHEN CREW ABORTED TAKEOFF DUE TO E1 EXCEEDENCE. MX AND INSPECTION FOUND DAMAGE TO ENGINE THRU A BOROSCOPE INSPECTION. THE NR 1 ENGINE WAS R & R IAW TASKCARD 6271001. ECN CONTROL NR JW 111150061313. ALL WORK ACCOMPLISHED WITH LEAK CHECKS ASDR CA140120001Engine · stalled(CAN) DURING A TEST FLIGHT FOLLOWING PROPELLER GOVERNOR REPLACEMENT, AS THE ACFT WAS ON SHORT FINAL, THE PILOT REPORTED IT STALLED BEFORE CRASHING TO THE GROUND SOME 100 FT SHORT OF INTENDED LANDING STRIP. NO OTHER DETAILS ARE AVAILABLE ON THE CIRCUMSTANCESSDR 27MA2013061800356Bearing · failedACFT DEPARTED AND ENROUTE, NR 3 ENGINE HAD SEVERE VIBRATION AT FLIGHT LEVEL FL300. ENGINE INSTRUMENTS INDICATED NORMAL AND NO MASTER WARNING SYS LIGHTS ILLUMINATED. CREW SHUT NR 3 ENGINE DOWN AND FOLLOW ABNORMAL PROCEDURES TO FLY WITH ON ENGINE INOPERATIVE TSDR RAIA201306130001Engine · shutdownDURING CRUISE, FLIGHT CREW RECEIVED A NR 2 ENGINE TEMPERATURE SPIKE. PULLED THROTTLE BACK AND ENGINE AUTO SHUTDOWN. DIVERTED. MX INSPECTED AND R & R NR 2 ENGINE. OPS CHECKED GOOD.SDR YYFA20130613001Engine · malfunctionedNR 2 ENGINE START VALVE OPEN LIGHT ON, NO ENGINE ROTATION.SDR CA130701008Engine · malfunctioned(CAN) WHEN STARTING TAKEOFF ROLL, THE PILOT NOTICED THAT ENGINE TEMPERATURE WAS DROPPING AS TORQUE WAS INCREASING. THE T/O WAS ABORTED AND THE ACFT RETURNED TO THE GATE. TROUBLESHOOTING IS ON ON-GOING AND FOCUSING ON A POSSIBLE ELECTRICAL INTERFERENCE, GROUNSDR CA130701006Engine · surges(CAN) THE PILOT ABORTED TAKEOFF DUE TO ENGINE SURGE. INVESTIGATION ONGOING.SDR CA130613001Engine · making metal(CAN) EIR PW100 2013-047 IN FLIGHT SHUTDOWN AND METAL CONTAMINATION IN THE TM OIL SYSTEM.SDR CA130701001Engine · power loss(CAN) THE PILOT ELECTED TO ABORT THE TAKEOFF DUE TO NP DROPS OFF FROM 1700 TO 1500 RPM.SDR CA130617002Engine · shutdown(CAN) THE PILOT REPORTED AN ELECTRONIC ENGINE CONTROL SHUTDOWN FROM THE LT ENGINE. THE PILOT REQUESTED MORE POWER FROM RT ENGINE TO FLY OVER THE CABLES IN FRONT OF HIM. THE PILOT COMPLETED AN UNEVENTFUL LANDING AND SHUTDOWN THE ENGINES.SDR CA130614006Engine · shutdown(CAN) SHORTLY AFTER DEPARTURE, THE ACFT CRASHED IN A RESIDENTIAL AREA. POST CRASH FIRE OCCURRED, SETTING 2 HOUSES ON FIRE AND DAMAGING A 3RD. NO ONE ON THE GROUND WAS HURT. ON SITE WRECKAGE DID NOT SHOW ANY OBVIOUS CAUSES FOR THE ACCIDENT AND AS SUCH, THE SDR CA130610001Engine · malfunctioned(CAN) EIR PT6A 2013-039, ENGINE WAS SENT FOR INVESTIGATION AFTER THE CUSTOMER REPORTED A LOSS OF OIL PRESSURE FOLLOWED BY AN IN-FLIGHT SHUTDOWN. ACCORDING TO INFORMATION RECEIVED FROM THE CUSTOMER, SOON AFTER TAKEOFF, A SLIGHT VIBRATION WAS FELT FROM THE ENGISDR CA130614005Engine · malfunctioned(CAN) AFTER DROPPING OFF SKYDIVERS, AS THE ACFT WAS RETURNING TO BASE, THE ENGINE LOST POWER. UNABLE TO CLEAR TREES ON APPROACH, THE PILOT ELECTED TO SET THE ACFT DOWN IN A FIELD. THE PILOT, ONLY 1 ONBOARD, WAS SERIOUSLY INJURED. THE ACFT SUFFERED SUBSTANTISDR ASAA2013060895071Brake Assy · failedNR 2 ENGINE VALVE CLOSED LIGHT BRIGHT WITH NR 2 START LEVER IN CUTOFF. ACFT GROUNDED. REPLACED NR 2 ENGINE START BRAKE ASSY. ALL OPS NORMAL. START VALVE. LIGHT OPS NORMAL. REF MM 76-11-10, 28-22-00, 73-21-00, 74-00-00, 25-11-01. GROUND VERIFICATION SATISFSDR DALA1315020650Engine · failedEMERGENCY DECLARED DUE TO LEFT ENGINE COMPRESSOR STALL AND IN FLIGHT ENGINE SHUTDOWN. MX FOUND METAL IN TAILPIPE. R & R ENGINE.SDR CA131022008Support · damaged(CAN) ACFT EXPERIENCED A LOW OIL PRESSURE EVENT WHILE IN FLIGHT. TWIN ENGINE, FLIGHT CREW SHUTDOWN THE ENGINE AND LANDED THE ACFT. ENGINE WAS REMOVED AND SENT TO FOR REPAIR. ENGINE WAS DISASSEMBLED AND FOUND TO HAVE SUFFERED OIL STARVATION DUE TO A SHEAREDSDR CA130617001Engine · power loss(CAN) DURING CLIMB OUT AT APPROXIMATELY 3500 FT, THE ENGINE NR 1 LOST TORQUE THE NORMAL ENGINE OUT PROCEDURES WERE APPLIED BUT THE PILOT WAS UNABLE TO FEATHER THE PROPELLER WITH THE CONDITION LEVER AND HAD TO USE THE ALTERNATE FEATHERING PROCEDURE. THE ACFT RSDR UALA2013060703982Structure · erodedNR 1 ENGINE ACCOUSTICAL LINER 4 O`CLOCK POSITION AFT OF FAN SECTION HAS AREAS OF ERROSION ON PREVIOUS REPAIR APPLIED FILLER TO AREA OF DAMAGE, REPAIR UNDER HEAT LAMP. WILL NEED LAMP REMOVED AT END OF CURE, APPROX 1100 5JUN13. REMOVED HEAT LAMP.SDR USAA2013060500004Engine · malfunctionedDURING CRUISE AT FL310, THE NR 1 ENGINE SURGED SEVERAL TIMES THEN FLAMED OUT. CREW DECLARED AN EMERGENCY AND STARTED DESCENT INTO CLT. OIL QUANTITY NR 1 ENGINE LOW. FLEW ON NR 2 ENGINE FOR APPROX 20 MINUTES. FLIGHT LANDED WITHOUT INCIDENT AND TAXIED TO GATE SDR CA130614004Engine · making metal(CAN) DURING FLIGHT, THE PILOT REPORTED VIBRATION ON NR 1 ENGINE WITH A RAISE OF TEMPERATURE. THE POWER WAS REDUCED AND SOON AFTER A NOISE WAS HEARD ACCOMPANIED BY RUMBLING. THE ENGINE WAS SHUTDOWN AND AN UNEVENTFUL SINGLE ENGINE LANDING FOLLOWED. POST FLIGSDR CA130611005Engine · making metal(CAN) ACFT WAS ENROUTE TO DROP THE OWNER OFF FOR VACATION. ENGINE CHIP LIGHT ILLUMINATED. ACFT LANDED, REMOVED THE UPPER AND LOWER CHIP PLUGS AND FOUND CHIPS ON UPPER AND LOWER PLUGS BUT THE UPPER PLUG HAD A 1.93 MM "CHUNK" THAT ILLUMINATED THE LIGHT IAW THESDR CA130617008Engine · multiple fail(CAN) ON TAKEOFF HAD A WINDSHEAR WARNING, PUSHED THRUST LEVERS TO MAX THRUST. RT ITT OVERTEMPED. OUT OF WINDSHEAR, PULLED THRUST LEVERS BACK CLIMBING OUT OF 13,000 FT. RT ENGINE OIL PRESSURE WARNING MESSAGE, RAN QRH PROCEDURE. MONITORED ENGINE GAUGES TO SEE SDR CA130611009Engine · making metal(CAN) SUBJECT HELICOPTER, ROUTINE ANNUAL INSPECTION, WHEN TECHS CHECKED THE ENGINE CHIP PLUGS IAW ASB 407-13-99 AND CEB A-72-6075 AND FOUND SIGNIFICANT AMOUNTS OF METAL FLAKES ON BOTH PLUGS. AT LEAST 1 OF THE CHIPS EXCEEDS THE R & R OPS & MM 72-00-00, PAGE 33SDR AALA20130602003Engine · failedINFLIGHT, CREW REPORTED RT ENGINE OIL FILTER CLOG LIGHT ILLUMINATED. CREW SHUTDOWN RT ENGINE (SINGLE ENGINE TIME 27 MINUTES). EMERGENCY DECLARED FLIGHT DIVERTED RDU LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. ACFT FERRIED FOR MX. REPLACED RT ENGINSDR REXA2013060101067Engine · overheatedLEFT ENGINE REACHED 902C ON TAKEOFF ROLL. ITT GAUGE FLASHED RED BUT NO AUDIBLES. ABORTED AT 85 KNOTS. PERFORMED VISUAL INSP LT ENGINE/ECS DUCTING. NO FAULTS NOTED. PERFORMED POWER ASSURANCE GROUND RUN/ENGINE ACCELERATION CHECK. ALL CHECKED GOOD IAW AMM 71SDR SWIA201333598Engine · failedON DESCENT SMOKE ENTERED CABIN. RAN QRH LANDED WITHOUT FURTHER INCIDENT. REPLACED RT ENGINE IAW AMM.SDR CA130531012Engine · warning message(CAN) WHILE THE ACFT WAS ENROUTE, THE FLIGHT CREW ELECTED TO SHUTDOWN THE NR 1 ENGINE FOR ILLUMINATION OF THE OIL FILTER BYPASS LIGHT. FOLLOWING THE FOM AND REDUCING THRUST DID NOT EXTINGUISH THE LIGHT. THE FLIGHT RETURNED TO POS AND MADE AN UNEVENTFUL LANDISDR SIMA20130530003Engine · bird ingestionTHE PILOT REPORTED HE WAS UNAWARE OF A BIRDSTIKE THAT MUST HAVE OCCURRED. HE SAID THAT HE USED THE CAPTAIN’S FLASHLIGHT AND MISSED IT ON THE POST INSPECTION. WHILE TROUBLESHOOTING, SMOKE IN THE COCKPIT FOUND NR 2 ENGINE SMELLING LIKE A BIRD HAD GONE THROUGH ISDR JJBA20130529021Pcu · failedAT 400 FT, THE NR 1 ENGINE TORQUE WAS AT 116. THEN THERE WAS A STRONG YAW TO THE LEFT. THE PCU WAS CHANGED.SDR ASOA2013053103740Engine · overtempAFTER TAKEOFF, RT ENGINE REACHED APPROX 926, N1 WAS SET AT .91-4. TARGET WAS 91-5 POWER WAS REDUCED & RECREASED INTO NORMAL RANGE. RETURNED TO DEPARTURE, EMERGENCY DECLARED. R & R RT ENGINE ASSY OPS AND LEAK CHECKED GOOD.SDR CA130605006Engine · making metal(CAN) ACFT IS AOG DUE TO ENGINE METAL PARTICLES. FIRST ENGINE CHIP LIGHT REPORTED 16 MAR 2013 AT 94.7 HOURS. SMALL AMOUNT OF VERY FINE PARTICLES AND SEDIMENT FOUND ON THE CHIP PLUGS. PROCEDURES FOLLOWED IAW THE MANUAL AND ACFT RETURNED TO SERVICE. ON 03 APSDR CA130603007Engine · power loss(CAN) REPORTED THAT THE ENGINE EXPERIENCED A POWER REDUCTION AND HIGH ITT DURING FLIGHT. AT FINAL APPROACH THE ENGINE LOST ALL POWER. THE ON GROUND INVESTIGATION REVEALED THAT THE PROPELLER COULD NOT TURN, THE CHIP DETECTOR WAS CLEAN AND THE COMPRESSOR WAS T
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