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 ASAA2015121114221Actuator · failedWHILE ACCOMPLISHING T/C 78273000, NR 1 ENGINE HAS FAULT MSG 75-10391, THE VSV POSITION SIGNAL IS OUT OF RANGE. ACFT GROUNDED. R & R NR 1 ENGINE RT VSV ACTUATOR ASSY IAW AMM 75-31-01-00-802-F00 AND 75-31-01-400-800-F00. LEAK AND OPS CK GOOD.SDR ANCF2015121101Engine · failedDURING FLIGHT, ENG 1 FAIL, ENG 1 STALL & ENG 1 SHUTDOWN. REPLACE ENG 1 IN PROGRESS. ENG PN CFM56-5B, SN 577194, TSN 26542 141, CSN 19697. REMAINING TIME IN ORDER TO GO TO THE SHOP, 303 FC.SDR CA151216015Engine · smoke(CAN) DURING TAXI TO THE GATE, THE CONTROL TOWER INFORMED THE CREW THAT SMOKE WAS COMING OUT OF THE NR 1 ENGINE. THE ENGINE HAD BEEN FEATHERED WHEN THE SMOKE CAME OUT. THE CREW RECEIVED A FIRE WARNING AND PULLED THE TEE HANDLE AS A PRECAUTIONARY MEASURE, RESSDR CA151216014Engine · power loss(CAN) DURING CLIMB THE ENGINE LOST POWER WITH NO PRIOR WARNING OR ABNORMAL INDICATIONS. THE ENGINE WAS SECURED AND THE CREW PERFORMED AN UNEVENTFUL SINGLE ENGINE LANDING AT THE DEPARTURE AIRPORT. POST FLIGHT INSPECTION FOUND A SHEARED FUEL PUMP DRIVE SHAFT. THSDR ASAA2015121014226Cover · wornNR 2 ENGINE CENTRAL VENT TUBE SEAL, OIL INLET COVER WEAR. ACFT GROUNDED. R & R NR 2 ENGINE IAW TASK CARDS 78471000, 78471001. ETOPS IPC PN FOR ESN 894886 CORRECTED BY ME-04 ASA-559-0819.SDR CA151216010Vane · failed(CAN) DURING CLIMB, A LOW OIL PRESSURE WARNING OCCURRED. THE CREW ELECTED TO TURN BACK TO THE DEPARTURE AIRPORT WHERE POST FLIGHT INSPECTION FOUND SIGHT GLASS OIL LEVEL ABOVE ADD 1. THE CHIP DETECTOR WAS CLEAN BUT A FUEL ODOR WAS NOTED IN THE OIL. THE FUEL HSDR CA151216009Engine · malfunctioned(CAN) AFTER LANDING, UPON STOWING THE THRUST REVERSERS, THE PILOT NOTICED THE RT ENGINE FAN SPEED WAS LOW, OIL PRESSURE WAS AT ZERO, ENGINE HAD SHUTDOWN WITH ASSOCIATED ENGINE DIAGNOSTIC SYS FAULT MESSAGE. POST FLIGHT INSPECTION FOUND NOTHING WRONG SO A GROUNSDR E07A20151211001Engine · contaminatedON TAKEOFF, CREW NOTED SLIGHT SMOKE IN CABIN & SMELL OF BURNING OIL. RETURNED WITHOUT INCIDENT. THIS WAS FIRST FLIGHT AFTER OVERHAULED ENGS WERE INSTALLED. OPENED BLEED SYS & USED BORESCOPE TO INSPECTED ENG & BLEED SYS UP TO THE PRESS AFT PRESS BULKHEAD. NSDR TSAA20151208006Engine · shutdownON LANDING ROLLOUT, NR 2 ENG SHUTDOWN AUTOMATICALLY. POWER LEVERS WERE INTO SLIGHT REVERSE WHEN NR 2 ENG FAILED. FOLLOWED FAULT ISOLATION MANUAL 71-00-00, VISUALLY INSPECTED NR 2 ENG INLET FOR OBSTRUCTION & IGV RING & ACTUATING LINKAGE ASSEMBLY FOR DAMAGE. SDR CA151216007Engine · power loss(CAN) DURING TAKEOFF ROLL, THE RT ENGINE TORQUE DID NOT INCREASE AS COMMANDED WHICH PROMPTED THE CREW TO ABORT THE TAKEOFF. TROUBLESHOOTING LED TO THE REPLACEMENT OF THE FUEL CONTROL UNIT.SDR CA151216005Engine · contaminated(CAN) THE ABORTED TAKE-OFF DUE TO THE PRESENCE OF SMOKE IN THE COCKPIT/CABIN. INITIAL INVESTIGATION REVEALED THAT THERE IS A SIGNIFICANT AMOUNT OF OIL CONTAMINATION BEHIND THE BLEED PATH INSPECTION PLATE. THIS IS THE SECOND SUCH EVENT ON THE SAME ACFT IN RECSDR CA151209004Engine · shutdown(CAN) OPERATOR REPORTED AN UN-COMMANDED IN-FLIGHT SHUTDOWN FOLLOWED BY ILLUMINATION OF THE ITT WARNING LIGHTS, ACFT CREW REPORTED UNCOMMANDED INFLIGHT SHUTDOWN ON THE NR 1 ENGINE TURNING FINALS FOR LANDING. CREW REPORTED ONLY SEEING CAUTION LIGHTS ON THE ANNSDR CA151216008Engine · malfunctioned(CAN) JUST AFTER DROPPING SKYDIVERS, THE PILOT FELT A VIBRATION AND SAW THAT THE ENGINE TORQUE READING WAS IN THE RED ARC. HE ELECTED TO PERFORM AN ENGINE SHUT DOWN AND GLIDE BACK TO THE AIRPORT. THE AIRCRAFT HOWEVER LANDED SHORT OF THE INTENDED RUNWAY CAUSINSDR DCGA2015FA0000622Engine · making metalPILOT GOT AN INTERMITTENT ENGINE CHIP LIGHT INDICATION AFTER TAKEOFF AND RETURNED FOR LANDING. MAINTENANCE FOUND LIGHT EXTINGUISHED BUT FOUND METAL ON UPPER AND LOWER ENGINE CHIP PLUGS. ENGINE WAS REMOVED FROM THE ACFT FOR FURTHER INSPECTION.SDR KC8A20151201001Engine · flamed outTHE CREW REPORTED THAT WHILE CLIMBING TO THEIR CLEARED ALTITUDE, THE RT ENGINE FLAMED OUT. THEY DECLARED AN EMERGENCY AND ATC CLEARED THEM TO DESCEND FOR RELIGHT. WITH THE ENGINE RE-STARTED, THEY DIDN’T NOTICE ANY OPERATING ISSUES WITH THE ENGINE AND CLIMBED SDR CA151215009Engine · overtemp(CAN) CLIMBING TO FL400 THE LT ENGINE ITT WENT IN TO THE YELLOW, THE PILOT PULLED THROTTLES BACK AND ITT CAME OUT OF THE YELLOW.SDR CA151215008Engine · power loss(CAN) DURING TAKE-OFF (AFTER V1), THE ENGINE NR 1 POWER RATING NTOP, TORQUE BUG DROP UP TO 30% AND TORQUE INDICATION DROP ABOUT 10%. AFTER THIS, TORQUE BUG BACK TO RATING (CCA 79%) AND TORQUE INDICATION BACK TO SAME LEVEL, NO FURTHER OBSERVATIONS WERE MADE BY SDR YENA20151130614Stator Vane · faultyFLT 1561 RETURNED DUE TO NR 1 ENGINE COMPRESSOR VANE. LEFT EPR 1.370+0.5/ RIGHT EPR 1.370+.003 LEFT EPR RETURNED TO NORMAL INDICATIONS 1.5 HOURS POST EVENT. CONFIRMED POST SB 75-0122 VSV ACTUATOR INSTALLED. PERFORMED TSM TASK IAW 75--30-00-310-352-A. ACCOMPLISDR CA151215012Engine · contaminated(CAN) CUSTOMER REPORTS OIL SMELL/FUMES IN CABIN AND FLIGHT DECK. THE PILOT ELECTED DIVERT THE FLIGHT. THE CUSTOMER PERFORMED A BORESCOPE INSPECTION AND REPORTED HAVING OIL CONTAMINATION INTO ENGINE NR 2 COMPRESSOR. THE ENGINE WILL BE REPLACED AND SENT FOR INVESDR CA151215011Engine · damaged(CAN) DURING CLIMBING OUT THE CREW NEEDED TO SHUT THE LT ENGINE DOWN. THE ACFT RETURNED FOR A SAFE LANDING. BORESCOPE INSPECTION REVEALED EXTENDED DAMAGE AT NUMEROUS LOCATION IN THE ENGINE. THE ENGINE WILL BE SENT FOR INVESTIGATION AND REPAIR.SDR CA151215005Engine · cracked(CAN) DURING A CT DISK REPLACEMENT DUE TO LCF NEARING EXPIRY AT 9841 CYCLES, A CRACK WAS FOUND AT THE FLANGE LEADING TO 2 RIVET HOLES. SERVICE INVESTIGATION REQUESTED THE PART FOR FURTHER ANALYSIS.SDR CA151215001Engine · stalled(CAN) DURING DESCENT, WITH THE ENGINE AT IDLE SPEED, THE ENGINE STALLED AND SHUTDOWN BY ITSELF. THE PILOT WAS ABLE TO RESTART THE ENGINE. THE CUSTOMER HAD 2 IN-FLIGHT SHUTDOWNS WITH THE SAME ENGINE DURING DESCENT MODE. THE ACFT LANDED UNEVENTFULLY. TROUBLESSDR CA151202004Engine · overtemp(CAN) ENGINE WAS SENT FOR REPAIR WITH THE OPERATOR REPORTING AN IN FLIGHT-SHUTDOWN IFSD, THE ENGINE TEMPERATURE CLIMBED BEYOND NORMAL OPERATING LEVELS. NO OVERTEMP EVENT WAS RECORDED. THE OPERATOR ALSO REPORTED FOD AND A GRINDING NOISE WHEN ROTATING THE COMPSDR CA151201013Engine · making metal(CAN) ENGINE WAS SENT FOR REPAIR WITH THE OPERATOR REPORTING METAL IN OIL. THE OPERATOR ALSO REPORTED THAT BOTH CHIP DETECTOR LIGHTS WERE ILLUMINATED. THE CUSTOMER PROVIDED A LABORATORY ANALYSIS REPORT OF THE METAL FOUND IN THE MAIN OIL FILTER AND FROM AN OIL SDR CA151204009Shaft · failed(CAN) ON MARCH 26, 2015 AN ENGINE WAS REMOVED FROM SERVICE DUE TO ENGINE SURGE AND HOT SECTION DISTRESS. AFTER INDUCTION INTO THE ENGINE SHOP THE ENGINE WAS DISASSEMBLED AS REQUIRED BY THE WORK SCOPE. THE FAN SHAFT WAS SUBCONTRACTED TO THE MFG FOR REPAIR. ON SDR DJFA20151126001Engine · surgesDURING CLIMB OUT, CREW REPORTED THE LT ENG SURGED & ROLLED BACK MULTIPLE TIMES. ACFT RETURNED TO THE DEPARTURE AIRPORT & LANDED SAFELY. REPLACED THE NR 2 ENG.SDR CA151201008Engine · power loss(CAN) DURING AN OFFSHORE FLIGHT IN A HEAVY RAIN CONDITION PILOT HEARD FEW POPS ON ENGINE NR 2, ABOUT 3-4 SECONDS IN BETWEEN, PILOT BROUGHT THE ENGINE TO IDLE AND ENGINE WAS FINE AND ALL PARAMETERS ARE OK. PILOT TRIED TO INCREASE POWER AGAIN SAME SURGE REPEATEDSDR CA151201007Engine · shutdown(CAN) FLYING LEVEL AT FL 360, PILOT NOTICED A VIBRATION ON THE ACFT, FOLLOWED BY THE MESSAGE RT GENERATOR OFF, GENERATOR RESET PERFORMED AND THE SYS WORKED FOR 3 MINUTES. VIBRATION WAS STILL PRESENT. AFTER 3 MINUTES, THE WARNING FOR RT GENERATOR OFF ACTIVATESDR AALA201511259010Engine · bird ingestionUPON APPROACH, SEVERAL MEDIUM SIZED BIRDS HIT THE LT ENG COWLING. THE FLIGHT CREW DID NOT DECLARE AN EMER, BUT ATC HAD EMER TRUCKS RESPOND. THE FLIGHT LANDED SAFELY WITH NO INCIDENTS. INSPECTED THE ACFT & DISCOVERED THAT THE LT ENG HAD INGESTED BIRDS. MAINSDR CA151201005Engine · fluctuates(CAN) THE FLIGHT DEPARTED WITHOUT ISSUES NOTED. THE ACFT REFUELED AND DEPARTED FOR FINAL INTENDED DESTINATION. AFTER 1 HR INTO THE FLIGHT AT 40 KFT THE ACFT RAN INTO HEAVY TURBULENCE WITH ALTITUDE FLUCTUATIONS OF 400 FT TOTAL AND SPEED FLUCTUATIONS OF 40 KNOSDR CA151127002Engine · malfunctioned(CAN) CREW EXPERIENCED MODERATE TO SEVERE TURBULENCE. THEY WERE UNABLE TO MAINTAIN ALTITUDE AND TRACK. THEY REQUESTED LOWER AND STARTED TO DESCEND, THIS WAS NOT POSSIBLE DUE TO AN INCREASE IN VERTICAL SHEAR. AT THIS POINT, THE BELIEVED THEY HAD A COMPRESSOR STSDR CA151201006Engine · power loss(CAN) ON APPROACH, WITH POWER SET AT 400-500 FT/LBS, THE RT ENGINE TORQUE DROPS AWAY AND RETURNS MULTIPLE TIMES. TORQUE IS DROPPING AS LOW AS 150 LBS.SDR AALA201511259009Engine · failedINFLIGHT ENG SHUTDOWN. FLIGHT DIVERTED DUE TO A LT ENG FAILURE. AN EMER WAS DECLARED & THE ACFT LANDED SAFELY WITHOUT INCIDENT. MAINTENANCE REPLACED THE LEFT ENGINE PER TASK CARD 19L40071001.SDR AALA20151121001Engine · leakingDURING FLIGHT, RT ENG LOST 10 QUARTS OF OIL IN 5.5 HRS. FLIGHT DIVERTED & LANDED WITHOUT FURTHER INCIDENT. ACFT WAS REMOVED FROM SERVICE. TROUBLE SHOT SYS & FOUND TUBE B SCAVENGE LEAKING THRU GASKET IAW IPC IAW 79-21-00-01 DETAIL N ITEM 112. REPLACED GASKESDR CA151201009Engine · failed(CAN) AFTER STARTING A NORMAL DESCENT, PILOT REPORTED THAT THE PROP RPM FOLLOWED THE N1 AS THE POWER WAS REDUCED. THE PILOT INCREASED THE N1 AGAIN TO FIND THE PROP RPM ALSO INCREASED. THEN, THEY HEARD AN UNUSUAL ENGINE SOUND AND THE PROP FEATHERED ITSELF. TSDR CA151201003Engine · malfunctioned(CAN) NR 2 ENGINE EXPERIENCED PARTIAL RUNAWAY POWER DECREASE FOLLOWED BY RUNAWAY POWER INCREASE. PILOT SHUTDOWN ENGINE AND CARRIED OUT A CONTROLLED SINGLE ENGINE LANDING. ENGINE MFG REQUESTED FDR DATA TO REVIEW.SDR CA151120005Engine · overtemp(CAN) ON DEPARTURE CLIMB, CREW HAD LT ENGINE EGT GO IN AND OUT OVER LIMITS, LT ENGINE SHOWED 90 DEGREES HOTTER ON EGT. CREW HAD TO MANAGE THRUST TO MAINTAIN UNDER LIMIT.SDR CALA2015112394857Engine · making metalLEFT ENG HAD AUDIBLE SURGE DURING POWER REDUCTION AT TOP OF DESCENT. THROTTLE REDUCED TO IDLE. NO ENG LIMITS WERE EXCEEDED. WHEN THROTTLE WAS ADVANCED TO 61%, 1 AT FL 230 IT SURGED AGAIN. THROTTLE REDUCED TO IDLE FOR REMAINDER OF FLIGHT. VISUAL CHECKS IAWSDR AALA20151119010Engine · failedRIGHT ENG AUTO SHUTDOWN IN FLIGHT, CRUISE ALTITUDE 360, WITH NO ABNORMAL INDICATIONS PRIOR. RECEIVED RT ENG LP PUMP EICAS MSG AT SHUTDOWN. ATTEMPTED RE-START, NO FUEL FLOW DURING ATTEMPT. EMERGENCY DECLARED, FLIGHT LANDED WITHOUT FURTHER INCIDENT. NO VIBRATSDR CA151119001Engine · making metal(CAN) CREW REPORTED RTF FOR VISIBLE SMOKE IN CABIN AND COCKPIT, WITH LAV SMOKE WARNING GOING OFF. THE CREW TURNED THE BLEEDS OFF AND THE SMOKE STARTED TO CLEARED, SMELLED LIKE GLYCOL BUT WAS NOT DEICED. THE ACFT WAS DE-ICED THOUGH THE PRIOR FLIGHT IN DEN. NOSDR CA151130009Engine · vibration(CAN) IN LEVEL FLIGHT, AT FL400 THE LT ENGINE BEGAN VIBRATING BADLY. POWER WAS REDUCED, BUT THE VIBRATION CONTINUED AND THE ITT BECAME VERY HOT. THE ENGINE WAS THEN SHUTDOWN MANUALLY. 2 PILOTS, 1 PASSENGER. THE CREW LANDED AT INTENDED DESTINATION. TROUBLESSDR YENA20151116576Engine · failedSUP: FLIGHT DIVERTED. OIL QUANTITY WAS NORMAL AT TAKEOFF, ABOUT 2 HRS PLUS INTO FLIGHT, OIL QUANTITY BEGAN TO STEADILY DECREASE AND CONTINUED UNTIL IT READ ZERO, NO OTHER INDICATIONS, PRESSURE AND TEMPERATURE WERE NORMAL. R & R NR 1 ENGINE IAW AMM 71-00-20.SDR CALA2015111894845Engine · making metalON DESCENT FL370, AFTER THRUST REDUCTION, EXPERIENCED SEVERAL COMPRESSOR STALLS LT ENG. POWER REDUCED TO IDLE FOR REMAINDER OF DESCENT FROM FL230, EMER DECLARED. FOUND METAL PARTICLES IN THE ENG TURBINE EXHAUST REQUIRING ENG REMOVAL.SDR DXTA2015111306125Valve · failedIN LEVEL FLIGHT AT FL400 THE LT ENG BEGAN VIBRATING BADLY. POWER WAS REDUCED, BUT THE VIBRATION CONTINUED & THE ITT BECAME VERY HOT. THE ENG WAS THEN SHUTDOWN MANUALLY. R & R PRESS REGULATING & SHUTOFF VALVE IAW G450 CMP 361106 & G450 CMP 361215. OPERATIONSDR CA151130006Engine · smoke(CAN) IT WAS REPORTED THAT, DURING THE ENGINE START, COCKPIT SMOKE WAS NOTICED AND THE LAVATORY SMOKE DETECTORS WERE ACTIVATED. NR 2 ENGINE WAS STARTED WITH ITS BLEED SWITCH SELECTED AT PROP FEATHER POSITION. NO 1 ENGINE WAS STARTED THEREAFTER, ITS BLEED SWITCSDR SIMA20151115001Engine · shutdownNR 1 ENGINE SHUTDOWN DURING CLIMB OUT BELOW 2000 FT. R & R LT ENGINE IAW WC 71-000-00. GROUND RAN ACFT. OPS CHECKED GOOD, NO DEFECTS NOTED.SDR CA151130004Engine · unknown(CAN) ( XIAN- MA 60) WHILE PERFORMING AN EMERGENCY LANDING, THE ACFT EXITED THE END OF THE RUNWAY. THE ACFT SUFFERED DAMAGE TO THE LANDING GEAR AND TAIL SECTION, OTHER DAMAGES LIKELY TO BE PRESENT BUT NOT VISIBLE. WITNESSES REPORTED POSSIBLE ENGINE ISSUES. SDR ZESA20151113001Engine · shutdownIN DECENT AT 3000 FEET, CLEAR AIR, NO MOISTURE, CLEARED FOR VISUAL, REDUCED POWER FROM APPROX 75% N1 TO 68% N1 TO START DESCENT. THE MASTER WARNING ILLUMINATED & THE RT ENG SHUTDOWN UNCOMMAND. NO OTHER OBSERVATIONS NOTED TO CAUSE OCCURRENCE. COULD NOT DUPLISDR CA151201004Engine · flamed out(CAN) FLIGHT CREW REPORTED UN-COMMANDED ENGINE FLAMEOUT AND AUTO RELIGHT ON THE LT ENGINE AFTER 08 SEC DURING CLIMB AT FL215. THE PROBLEM WAS NOT REPRODUCED DURING THE TROUBLESHOOTING. THE AFU WAS REPLACED AS A PRECAUTIONARY MEASURE AND THE ACFT IS BACK IN OPSDR CA151117019Engine · malfunctioned(CAN) THE ACFT DESCENDED FROM FL200 WITH THE ENGINE THROTTLE AT IDLE, 61 PERCENT. BEFORE LANDING THE PILOT TRIED TO INCREASE POWER AND THERE WAS NO RESPONSE FROM THE ENGINE. HE ATTEMPTED TO CHANGE THE PROPELLER SPEED TO OBTAIN A CHANGE IN ENGINE POWER THEN TH
Back to JASC 7200