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 IXXA0500175SShroud · wornDURING ROUTINE C-CHECK FOUND NUMBER 1 ENGINE FAN ABRADABLE SHROUD WORN BEYOND LIMITS AT 12:00, AND 1:00 POSITIONS. REMOVED ACCOUSTICAL PANELS, POTTED REPAIR AREAS, APPLIED FIBERGLASS OVERLAYS, CLEANED AND SEALED AREAS. REINSTALLED ACCOUSTICAL PANELS IAW CFM SDR AALA20050044Engine · damagedEN ROUTE PHL-DFW, COMPRESSOR STALL ON RIGHT ENGINE AFTER TAKEOFF. POWER WAS REDUCED AND STALLS CLEARED. ALL ENGINE INDICATIONS REMAINED IN NORMAL RANGE. RIGHT ENGINE KEPT RUNNING FOR APPROACH. LANDED PHL WITHOUT INCIDENT. REPLACED NUMBER 2 ENGINE DUE TO FSDR CA050131009Engine · shutdown(CAN) THE ENGINE EXPERIENCED AN UNCOMMANDED POWER ROLL-BACK IN CRUISE (ZERO TORQUE INDICATED).THE PILOT DECLARED AN EMERGENCY AND SHUT THE ENGINE DOWN IN FLIGHT. MFG WILL MONITOR INVESTIGATION OF THE EVENT AND WILL SUPPLEMENT THIS REPORT TO PROVIDE ROOT CAUSESDR DXTA200500550Engine · stoppedON COMPLETION OF THE SPOILER TEST THE LT ENGINE QUITS. OPERATED SPEED BRAKES THRU SEVERAL CYCLES, VERIFIED 85 PERCENT SWITCHES RETRACT THE SPEED BRAKES, PERFORMED SEVERAL SLAM CHECKS OF LEFT AND RIGHT ENGINES. NO DEFECTS NOTED, SPEED BRAKES AND ENGINE THROTTSDR 2005F00049Engine · malfunctionedDURING TAKEOFF, WITH POWER ABOVE 80 PERCENT TORQUE AIRCRAFT BEGINS VIBRATIONS INCREASING TO SEVERE WITH OSCILLATION BETWEEN 20-30 PERCENT ON TORQUE GAUGE. MAINTENANCE REMOVED AND REPLACED ENGINE ASSY WITH SERVICABLE SERIAL NUMBER CAE-890158. WORK DONE IAW BESDR CA050127005Seal · leaking(CAN) CAUSE OF SMOKE ODOR IN CABIN DUE TO OIL CONTAM OF GAS PATH AIRFLOW DUE TO A LARGE NR OF AIR/OIL SEALS HAD EXCESSIVE CLEARANCES, ALLOWING OIL TO ENTER SECONDARY AIR SYS. ENG DID HAVE A SIGNIFICANT AMOUNT OF FRETTING DAMAGE ON COMBUSION COMPONENTS, WHICH SDR CA050126010Engine · fod(CAN) WHILE DOING THE DAILY INSPECTION, TECHNICIAN NOTICED SUBSTANTIAL FOREIGN OBJECT DAMAGE TO THE BYPASS FAN AND THE FIRST STAGE COMPRESSOR BLADES OF THE ENGINE INSTALLED IN POSITION NR 1. AIRCRAFT HAD JUST COMPLETED 9.6 HOURS OF FLYING WITHOUT ANY INDICATISDR CA050131006Engine · failed(CAN) ENGINE FAILED IN FLIGHT, AIRCRAFT HAD JUST EXITED ICING CONDITIONS, CONTINUOUS IGNITION WAS TURNED OFF A FEW MINUTES PRIOR TO ENGINE FAILURE. AIRCRAFT RETURNED TO BASE AND ENGINE WAS INSPECTED FOR ANY CAUSE OF THE FAILURE, NOTHING WAS FOUND. GROUND/POWESDR CA050126007Engine · fluctuates(CAN) THE ENGINE EXPERIENCED TORQUE FLUCTUATIONS IN CRUISE FOLLOWED BY AN UNCOMMANDED REDUCTION IN PROPELLER SPEED TO 12 PERCENT. THE PILOT SHUT THE ENGINE DOWN AND DIVERTED THE FLIGHT. MFG WILL MONITOR THE INVESTIGATION OF THE INCIDENT AND WILL SUPPLIMENT TSDR GTIA050012Engine · failedFLT 1581 - ACY - ENGINE FAILURE AT FL 240, SURGE ON AIRCRAFT, RIGHT ENGINE FAILED AIRCRAFT YAWED RIGHT, NO FIRE WARNING OR INDICATION. EGT, N1 AND N2 DECREASED RAPIDLY, SHUT DOWN ENGINE AND DIVERTED IN ACY. REMOVED AND REPLACED NR 2 ENGINE. (M)SDR MALA050137Engine · malfunctionedRIGHT GEN FAIL LIGHT ILLUMINATED RIGHT ENGINE OIL PRESSURE WARNING LIGHT ILLUMINATED. OIL PRESSURE DROPPED TO ZERO ENGINE SHUT DOWN IN COMPLIANCE WITH QRH. DIVERTED A/C TO RST. MAINTENANCE REPLACED RIGHT ENGINE PER TASK CARD 7100-301, P/N ON CT7-9B, S/N ON SDR UPS05843662Engine · flamed outNR 2 ENGINE FLAMED OUT IN FLIGHT. A/C IS OOS. PERFORMED STEP 4 UP TO FUEL FILTER REPLACEMENT ON FIGURE 139 SHEET 1 OF MM 71 00 00. TS (558010) PERFORMED ENG MAINT RUN PER MM 71-00-00-1, NO DEFECTS NOTED. A/C OK FOR SERVICE.SDR 05FDEA00116Engine · smokeAT 80 KTS A/C STARTED TO SHUDDER CONTINUOUSLY. A/C STARTED VEERING TO THE RIGHT REQUIRING CONTINUOUS LEFT RUDDER INPUT TO KEEP A/C ON RWY CENTERLINE. AIRPLANE BEHIND, WHO HAD TAXIED INTO POSITION & HOLD REPORTED SMOKE COMING OUT OF THE ENGINE AREA. ABORTED SDR ARWA20050104Engine · failedNR 2 ENGINE FAILED ON ROTATION. ENGINE SHUTDOWN IN ACCORDANCE WITH CHECKLIST. AIRCRAFT RETURNED TO MSLP WITHOUT ANY FURTHER INCIDENT. ACCOMPLISHED RED BORDER 019056; REMOVED AND REPLACED NR 2 ENGINE IN ACCORDANCE WITH ARROW AIR DC-10 WORK CARD 142R7101M. PSDR AALA20050034Engine · failedYVR - INFLIGHT T814/15, ENGINE FAILURE ON TAKEOFF AT APPROXIMATELY 1000 FEET. LOUD BANG AND AIRCRAFT SHUDDERED FOLLOWED BY IMMEDIATE YAW TO THE RIGHT. NO FIRE OR AURAL INDICATIONS. RIGHT ENGINE PULLED TO IDLE UNTIL SHUTDOWN APPROXIMATELY 2 MINUTES LATER. ASDR CA050126005Blades · damaged(CAN) ON LANDING ENGINE TEMPERATURE WAS SEEN TO INCREASE, FOLLOWED BY AN UNCOMMANDED REDUCTION IN POWER. SUBSEQUENT INSPECTION REVEALED COMPRESSOR TURBINE AND POWER TURBINE BLADE DAMAGE. MFG WILL MONITOR THE INVESTIGATION OF THE INCIDENT AND WILL SUPPLIMENTSDR AT0500004Seal · looseN1 VIBRATION ON RIGHT ENGINE INCREASED OVER TIME FROM 4.0 TO 7.0 AT 310. ON DESCENT VIBRATION TO 9.0 AND WAS FELT THROUGHOUT AIRCRAFT. ICING IN CLIMB, ENGINE ONLY NO WING OR TAIL. TEMP AT 310 - 40 C. ENGINE ONLY ICE WAS USED. REMOVED AND REPLACED AIR INTASDR CHQA200500008Engine · leakingFLIGHT 6374 CHM-LGA - ON INITIAL CLIMB-OUT OF CMH AT 1000 FEET, LAV SMOKE MESSAGE APPEARED ON EICAS WITH THE ASSOCIATED TRIPLE CHIME. THE FLIGHT ATTENDANT CALLED WITH THE CABIN EMERGENCY ADDRESS BUTTON AND STATED THE CABIN WAS FULL OF SMOKE. AN EMERGENCY WASSDR CHQA200500007Engine · leakingFLIGHT 6399 CMH-BDL - AFTER TAKEOFF, A LAV SMOKE MESSAGE APPEARED ON EICAS. A HAZE WAS SEEN IN THE COCKPIT AND A LIGHT SMOKE COULD BE SEEN IN THE GALLEY. AFTER THE CHECKLISTS FOR LAV SMOKE WERE COMPLIED WITH, THE MESSAGE EXTINGUISHED. THE AIRCRAFT RETURNED SDR CA050211002Engine · failed(CAN) THE LOW OIL PRESSURE EVENT WAS RESULTS OF A CRACKED MAIN OIL PUMP HOUSING. OIL FILTER & CHIP DETECTOR WERE BOTH FOUND TO BE CLEAN & FREE OF DEBRIS DURING RECEIVING INSPECTION. THIS INDICATED THAT OPERATION OF ENGINE 19212 AT 85 PSIG (5 PSIG BELOW THE MINSDR DL764050030Engine · wornNR 2 ENGINE REPLACED ATL 1/13/05 FOR VANE WEAR.SDR RAIA00501040Engine · failed3643- PIT- RIGHT ENGINE ERRATIC/RIGHT ENGINE OIL PRESSURE RED CAP LIGHT/IN FLIGHT SHUTDOWN PER QRH. MAINTENANCE REMOVED AND REPLACED NR 2 ENGINE.SDR DL76G060039Engine · making metalDURING L/O FOUND METAL IN THE LT ENG MASTER CHIP DETECTOR. REPLACED ENGINE.SDR CA050126001Engine · failed(CAN) DURING A SPRAYING RUN, THE ENGINE EXPERIENCED AN UNCOMMANDED POWER REDUCTION. THE AIRCRAFT CLIPPED TREES AND IMPACTED THE GROUND. MFG WILL PARTICIPATE IN THE INVESTIGATION OF THE INCIDENT AND WILL SUPPLEMENT THIS REPORT TO PROVIDE ROOT CAUSE, ONCE ESTASDR 0500051236Engine · failedWHILE AT CRUISE, THE CREW REPORTED THE NR 3 ENGINE FAILED WITH NO INDICATION OF OIL PRESSURE OR N2 SPEED. THE CREW SECURED THE ENGINE PER COM AND CONTINUED TO AMS LANDING WITHOUT INCIDENT. THE ENGINE WAS REPLACED. OPERATIONAL CHECK GOOD.SDR DL76G050024Engine · wornNR 2 ENG BORO INSP OF HPT STAGE 2 NOZZLES ATL/TMC TMC 5-1087. REPLACED ENGINE DUE TO FAILED BORO.SDR C7WA200400074Engine · damagedNR 3 THROTTLE VIBRATION FELT INFLIGHT ALL OTHER ENGINE INSTRUMENT AND INDICATIONS NORMAL, REF LOGPAGE NR 21307. C1, C2, AND C3 DAMAGE FOUND, NR 3 ENGINE REPLACED, S/N OF INSTALLED ENGINE IS 654920. (M)SDR GTIA050007Engine · malfunctionedTAKEOFF ROLL A/T ENGAGED AT APPROX 40 KNOTS, THROTTLES AT FLEX POWER FELT SOMETHING LIKE A BLOWN TIRE, RT ENGINE SLIGHT YAW, ABORTED TAKEOFF. REMOVED AND REPLACED NR 2 ENGINE. (M)SDR SWAA050068Blade · distortedDURING SCHEDULED HC1 CHECK, FOUND SEVERAL 1ST STAGE LPT BLADES DISTORTED. REMOVED AND REPLACED NR 2 ENGINE PER MM.SDR ASMF200501005Blade · damagedDURING TRANSIT CHECK A BLADE WAS DETECTED DAMAGED BECAUSE OF FOD ON RT ENGINE. BLADE WAS BENDED ON UPPER TIP WITH .4375 INCHES OF LENGTH AND .2500 OF DEPTH. DAMAGE WAS WITHIN LIMITS IAW MM 72-00-00 AND WAS REWORKED IAW MM 72-00-00, ALL CORRECT.SDR DXTA200500529Engine · malfunctionedLEFT ENGINE SHUTDOWN WHEN THROTTLES WERE BROUGHT IDLE. PERFORMED LT ENGINE RUN OPERATIONAL CHECK AND NO DEFECTS NOTED. REMOVED LT LOWER COWLING TO INSPECT FUEL CONTROL, STARTER GENERATOR, AND INSPECTED QUADRANT AND NO DEFECTS WERE NOTED. COULD NOT DUPLICATESDR CA050114002Engine · malfunctioned(CAN) ON INITIAL CLIMB, HEARD A SUDDEN AND LOUD NOISE BETWEEN 4000 AND 4500 FT AND THE RT ENGINE SHUTDOWN ITSELF IN FLT. AFTER ASSESSING THE SITUATION AND FOLLOWING QRH AND MEMORY ITEMS, THE CREW NOTIFIED THE FLT ATTENDANT, PAX AND MX OF THE SITUATION. AN EMESDR DXTA200500519Engine · overheatedOVERTEMP NR 2 ENGINE ON TAKEOFF, TEMPERATURE WENT TO 797 DEGREES FOR 2 SECONDS. ABORTED TAKEOFF. ITEM IS UNDER INVESTIGATION.SDR XN0A1220Engine · malfunctionedAFTER ENG START ENG NR 1 REMAINED IN FLT IDLE. TRANSFERRED TO DMI 5011 PER MEL 73-30-02. CATC PLACARDS INSTALLED. (STATUS:ORIG/OPEN)SDR CA050213005Engine · failed(CAN) THE ENGINE EXPERIENCED A FAILURE ON APPROACH AND A SINGLE ENGINE LANDING RESULTED. SUBSEQUENT INSPECTION EVIDENSED PUNCTURE HOLES IN THE GAS GENERATOR CASE. PWC WILL INVESTIGATE THE EVENT AND WILL SUPPLIMENT THIS REPORT TO REFLECT ROOT CAUSE AS AND WHENSDR SIMA200500910Engine · failedNR 2 ENGINE FAILED DURING TAKEOFF ACCOMPANIED BY A NOISE THAT SOUNDED LIKE A COMPRESSOR STALL. MAINTENANCE REMOVED AND REPLACED THE RT ENGINE IAW MM. OPERATIONAL AND LEAK CHECKS WERE SATISFACTORY AND AIRCRAFT WAS RETURNED TO SERVICE. (SW21200502355) (K)SDR DL76P050005Engine · failedINFLIGHT SHUTDOWN OF RIGHT ENGINE. CLIMBING THROUGH FL 260 WITH ALL ENG INDICATIONS NORMAL AND POWER AT CLIMB SETTING, ACFT SHUDDERED VIOLENTLY WITH LOUD BANG. RIGHT ENG HAD FAILED. ACCOMPLISHED ENGINE FAILURE CHECKLIST AND RETURNED TO TPA. PASSENGER REPORSDR HALA0500007Engine · surgesFLT 22 - HNL - PER ACARS REPORT NR 2 ENGINE SURGE OCCURRED, T/O POWER AT 1.40 EPR. ENGINE RECOVERED IN 4 SECS. ENGINE CHANGE IN WORK. (M)SDR RAIA00412040Engine · out of trim5512 - STL - RIGHT ENGINE TORQUE INDICATION HIGH. MAINTENANCE ADJUSTED TRIM FOR BOTH ENGINES AND OPS CK GOOD.SDR CA050110006Engine · inoperative(CAN) THE ENGINE EXPERIENCED AN OIL PRESSURE LOSS IN CRUISE. THE CREW SHUT THE ENGINE DOWN AND DIVERTED FLIGHT. SUBSEQUENT INSPECTION REVEALED METALLIC DEBRIS ON THE ENGINE CHIP DETECTOR AND IN THE ENGINE OIL FILTER. MFG WILL MONITOR THE INVESTIGATION OF THSDR CA050107006Engine · failed(CAN) APPOX 20 MINS INTO FLT, & AT FLT LEVEL 120 ENROUTE TO DIKO FROM DIBK WITH 19 PAX, MASTER CAUTION LIGHT ILLUMINATED ACCOMPANIED WITH NR 2 ENG LOW OIL PRESSURE LIGHT. NR 2 OIL PRESSURE GAUGE CONFIRMED ACTIVE WARNING LIGHT WITH PRESSURE INDICATION OF BELOSDR SIMA200500101Engine · failedDURING CLIMB THE CREW REPORTED HEARING A LOUD BANG FROM ENGINE TWO. THEN ENGINE 2 SHUTDOWN UNCOMMANDED. NO WARNINGS JUST SEEMED TO SPOOL DOWN. MAINTENANCE REMOVED AND REPLACED THE NR 2 ENGINE IAW MM. OPERATIONAL AND LEAK CHECK WAS SATISFACTORY AND AIRCRAFTSDR 2005FA0000006Blade · brokenAIRCRAFT DEPARTED, AT CRUISE, THE LT ENGINE HAD AN EXPLOSIVE NOISE AND THE LEFT ENGINE SEIZED. PRE INSPECTION OF ENGINE INDICATES LOSS OF CT BLADE. (K)SDR CA050110007Engine · inoperative(CAN) THE CREW REPORTED A LOW OIL PRESSURE WARNING FOLLOWING TAKE-OFF. THE CREW SHUT THE ENGINE DOWN IN FLIGHT AND DIVERTED TO POINT OF DEPARTURE. MFG WILL INVESTIGATE THE EVENT AND SUPPLEMENT THIS REPORT TO PROVIDE ROOT CAUSE, ONCE DETERMINED.SDR 04FDEA03481Engine · failedNR 2 ENGINE VIBRATION AT TAKEOFF ROTATION FOLLOWED BY A BANG AT ROTATION. COMPRESSOR STALL REPORTED BY ANOTHER AIRCRAFT. EXCEEDENCE WENT AMBER TO 5.3 ON CLIMB & 4.4 IN CRUISE AT 10K FT, VIBRATION NOTICABLE IN CRUISE WITH ENGINE & WING ANTI-ICE ON & IGNITION SDR CA041223003Engine · malfunctioned(CAN) UNCOMMANDDED ACCELERATION ON THE LT ENGINE ON TAKE OFF AROUND + 7 PERCENT ABOVE RETURN TO NORMAL 40 SECONDS LATER.SDR C8GA20040028Engine · flamed outFLT 725 FROM PHL TO TOL, AFTER LANDING, WHILE ON ROLL-OUT, NR 3 ENGINE FLAME OUT OCCURRED. AIRCRAFT TAXIED TO GATE WITHOUT INCIDENT. PERFORMED VISUAL INSPECTION. ICING CONDITIONS WERE NOTED BUT NO ICE INGESTION WAS EVIDENT. NO DAMAGE WAS NOTED IN ENGINE INSDR XNOA1218Engine · malfunctionedNR 1 ENGINE WOULD NOT LIGHT OFF WHEN STARTING. PULLED AND RESET C/B PER M/M 74-00. OPS CHECK GOOD AT THIS TIME.SDR XNO1218Engine · malfunctionedNR 1 ENGINE WOULD NOT LIGHT OFF WHEN STARTING. PULLED AND RESET C/B PER M/M 74-00. OPS CHECK GOOD AT THIS TIME.SDR 04FDEA03453Engine · malfunctionedAT 1200 FT ON T/O, NR 2 ENGINE SEVERE COMPRESSOR STALLS. TOWER REPORTED FLAME FROM RIGHT ENGINE IN FLIGHT. PERFORMED ENGINE FIRE CHECKLIST NR 2. RETURNED TO LAND, IND WEIGHT 216.0. FIRE HANDLE PULLED, 1ST AGENT DISCHARGED. EPR/EGT EXCEEDENCE MESSAGES ON E
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