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 DLM88050822Engine · overspeedSUSPECT RIGHT COMPRESSOR STALL. EPR PEGGED ABOVE 2, N1 ABOUT 108 PERCENT SHUTDOWN IN FLIGHT. FOLLOWED SEVERE DAMAGE CHECKLIST THERE WAS SOME SMELL OF SMOKE WHICH CLEARED WHEN THE ENGINE WAS SECURED. EDP SHOWED N1 109 PERCENT FOR 30 SEC. PERFORMED BORO NO DSDR ASMF200501201Engine · vibrationCAPTAIN REPORTED THAT DURING FLIGHT WITH EPR BETWEEN 1.0 AND 1.2 IN THE LT ENGINE; VIBRATION AMPLITUDE OCCASIONALLY WITH PEAKS FROM 4 TO 0 AND WHEN THE LT ENGINE WAS SHUTDOWN, VIBRATION WAS FELT IN ALL THE AIRCRAFT. THE LT ENGINE CHIP DETECTORS, ACCESSORIES, PSDR CA051223014Engine · making metalDURING FLIGHT, SMOKE WAS DETECTED IN THE CABIN AIR ACCOMPANIED BY A REDUCTION IN ENGINE OIL PRESSURE. THE AIRCRAFT DIVERTED FOR A UNSCHEDULED LANDING. SUBSEQUENT INSPECTION REVEALED METAL DEBRIS IN THE ENGINE OIL SYSTEM. P&WC WILL INVESTIGATE THE EVENT AND SDR CA051223013Engine · making metalDURING CRUISE, THE ENGINE LOW OIL PRESSURE WARNING ANNUNCIATED ACCOMPANIED BY OIL PRESSURE FLUCTUATIONS. THE ENGINE WAS SHUT DOWN IN FLIGHT AND THE AIRCRAFT DIVERTED TO POINT OF DEPARTURE. SUBSEQUENT INSPECTION REVEALED METAL DEBRIS ON THE TURBOMACHINE CHIP SDR IXXA0500196OEngine · flamed outDURING FLIGHT FROM KLRD TO KLRD LEVELING AT 17000 FT NR 1 ENGINE FLAMED OUT. ACCOMPLISHED FLAMEOUT CHECK LIST ENGINE STARTED NORMALLY. AFTER WARM UP PERIOD THROTTLE WAS ADVANCED WITH NO RESPONSE FROM ENGINE. THE ENGINE SHUTDOWN. OIL PRESSURE WENT TO 0 AT TSDR CA060106002Engine · failedWHILE IN FINAL DESCENT, THE FLIGHT CREW DISCOVERED THAT THEY DID NOT HAVE FULL AUTHORITY OVER THE LEFT ENGINE. THE LEFT ENGINE COULD NOT BE REDUCED BELOW 800 LBS TORQUE. ENGINE CONTROL WAS STILL AVAILABLE IN A RANGE FROM 800 LBS TO MAX TORQUE. FLIGHT CREW OPTSDR QXEA200501842Engine · malfunctionedSMF FLIGHT NR 2307: AT 25,000' SMOKE WARNING LIGHT FOLLOWED IN 1 TO 2 MINUTES BY THE NR 2 ENGINE OIL PRESS WARNING LIGHT. SHUTDOWN THE NR 2 ENGINE. MAINTENACE REMOVED AND REPLACED THE NR 2 ENGINE, NR 2 PROP, (P/N 697070003, S/N DAP0217), NR 2 AC GENERATOR (PSDR ASMF200512017Blade · damagedDURING TRANSIT CHECK, A BLADE OF THE RT ENGINE WAS DETECTED WITH DAMAGE AND THE NOISE SUPPRESSOR LINER HAD INCRUSTED A FOD. INSPECTION WAS PERFORMED, DETECTING A DENT OF 0.75 X 0.25 AND .1875 OF LENGTH IAW MM 72-00-00. THE RT ENGINE BLADE WAS REWORKED IAW 72-0SDR ALG2006F00002Engine · oil consumptionDURING FLIGHT IT WAS NOTED THAT THE ENGINE OIL PRESSURE INDICATOR WAS FLUCTUATING. CONTINUED FLIGHT AND OIL PRESSURE AND TEMPERATURE REMAINED WITHIN LIMITS. THE ENGINE WAS REMOVED DO TO OIL CONSUMPTION. (K)SDR 2005UALA01478Engine · bird ingestionRETURN TO FIELD DUE TO BIRD STRIKE TO NR 2 ENGINE & ASSOCIATED HIGH VIBRATIONS. AFTER FAN BLADE SET REPLACEMENT HIGH ENGINE VIBRATION CONTINUED AND ENGINE WAS REPLACED. THE ENGINE SHOP VERIFIED CORRECT FAN BLADE SPACER, SHIM, RETAINER AND PROPER FAN BLADE WEISDR AALA20050825Engine · stalledMIA - DURING CLIMBOUT LEFT ENGINE VIBRATION INDICATED 3.4 ON N3. PULLED THROTTLE BACK AND CAUTION INDICATION WENT OUT. AFTER ADVANCING THROTTLE LEFT ENGINE EXPERIENCED A COMPERSSOR STALL. PULLED THROTTLE BACK AND LEFT ENGINE STABILIZED AND OPERATIVE NORMALLSDR CA051223012Engine · vibrationON DESCENT, THE ENGINE WAS REPORTED TO VIBRATE ACCOMPANIED BY AN UNCOMMANDED POWER ROLL-BACK AND SHUT DOWN. A SUCCESSFUL IN-FLIGHT RELIGHT WAS ACCOMPLISHED. P&WC WILL INVESTIGATE THE EVENT AND ADVISE OF ROOT CAUSE ONCE ESTABLISHED.SDR CA051223011Engine · vibrationIN FLIGHT, ODORS WERE DETECTED IN THE CABIN. SUBSEQUENTLY ENGINE VIBRATIONS OCCURRED ACCOMPANIED BY AN INDICATED LOSS OF TORQUE. THE ENGINE WAS SHUTDOWN IN FLIGHT. INSPECTION REVEALED NOISES INTERNAL TO THE ENGINE ON ROTATING THE PROPELLER. P&WC WILL INVESSDR DHL2005805005Engine · surgesAFTER ENG START ON NR1 WITH NORMAL INDICATIONS, DURING NR4 ENG STAT NR1 ENG SURGED THEN FAILED. DURING RESTART ATTEMPT NO FUEL FLOW. INSP FUEL FILTER NO CONTAMINATION NOTED. RAN NR1 ENG IAW JRH 11.8 CROSSFEEDING FROM NR2 MAIN TANK OPS NORM. SW BACK TO NR1 MSDR 05FDEA04369Engine · unknownT/O FROM RWY 23R IND WIND 120/09 T/O ROLL SEEMED NORMAL UNTIL ABOUT 110KTS. ACCELERATION SLOWED AT APPROX 125KNTS N1S BOTH ENGS STARTED TO ROLL BACK. TARGET N1 WAS 96.1. ABORTED AT 130KTS WHILE N1 WAS DECELERATING THRU 89%. V1 139, VR 139, V2 143.SDR ASMF200512013Blade · fodDURING TRANSIT CHECK, A BLADE OF THE LT ENGINE WAS DETECTED WITH DAMAGE BY FOD. INSPECTION WAS PERFORMED, DETECTING A CRACK OF 0.125 X 0.250 BEING WITHIN LIMITS IAW MM 72-00-00. THE LT ENGINE BLADE WAS REWORKED IAW 72-00-00 PAGE 618, TESTED CORRECT.SDR REXA200500156Engine · damagedWHEN LEVEL AT FL300 THE RT ENGINE SHUTDOWN. FLIGHT CREW FOLLOWED COMPANY PROCEDURES AND LANDED WITH NO OTHER PROBLEMS. MAINTENANCE FOUND SEVER DAMAGE TO THE ENGINE'S FAN SECTION. THE ENGINE WAS REPLACED AND THE AIRCRAFT RELEASED FOR SERVICE. DAMAGED ENGINE WISDR AU510002091Engine · making metalLT ENGINE OIL SYSTEM CHIP DETECTOR CONTAMINATED WITH METAL FUZZ. ANALYSIS FOUND THE METAL TO BE BEARING MATERIAL.SDR AU510002061Engine · contaminated(AUS) OILY FUMES IN COCKPIT AND CABIN. AIRCRAFT TURNED BACK AND OVERWEIGHT LANDING WAS CARRIED OUT. OVERWEIGHT LANDING INSPECTION CARRIED OUT WITH NIL FAULTS. SUSPECT FUMES CAUSED BY INHIBITING FLUID REMAINING IN ENGINE FOLLOWING ENGINE CHANGE. INVESTIGATION CSDR AU510002026Engine · seizedRT ENGINE SEIZED. INVESTIGATION CONTINUING.SDR AU510001952Engine · failedPASSENGER REPORTED `FLAMES OF RED METAL COMING FROM LEFT ENGINE 3-4 METRES BACK` AND AN EMERGENCY LANDING WAS CARRIED OUT. ENGINEERING INSPECTION THE IGV`S, FIRST STAGE COMPRESSOR, AFT FACE OF POWER TURBINE ASSEMBLY FOUND NIL DAMAGE. A GROUND POWER ASSURANCESDR AU510001937Engine · fluctuates(AUS) RT ENGINE EXPERIENCED 20 PERCENT TO 30 PERCENT TORQUE DROP WITH ASSOCIATED EGT FLUCTUATIONS. MAINTENANCE INVESTIGATION COULD NOT FIND ANY FAULTS AND ENGINE PARAMETERS WERE NORMAL. AIRCRAFT RETURNED TO SERVICE. (CASA NR 510001937)SDR AU510001772Turbine Blades · damaged(AUS) NR 1 ENGINE MAKING (POPPING) SOUNDS. SOUNDS INCREASED WHEN THRUST LEVER INCREASED AND DECREASED WHEN THRUST LEVER RETARDED. BORESCOPE INSPECTION FOUND HPC BLADES DAMAGED BEYOND LIMITS. INVESTIGATION CONTINUING. (CASA NR 510001772)SDR AU510001739Engine · malfunctionedNR 2 ENGINE CHIP DETECTOR MAGNETIC PLUGS (3OFF) CONTAMINATED WITH TYPE 3 FUZZ. PREVIOUS SOAP ANALYSIS NORMAL. ENGINE REMOVED FOR REPAIR AND INVESTIGATION.SDR AU510001677Engine · fluctuates(AUS) LT ENGINE EGT, TORQUE AND FUEL FLOW FLUCTUATING. LT FUEL BYPASS VALVE AND LT EGT SHORT LEAD CHANGED. GROUND RUNS AND TEST FLIGHT CARRIED OUT WITH NIL DEFECTS EVIDENT.SDR COMA0560714Engine · failedFLIGHT 5482 - LEFT ENGINE EXCEEDED ITT LIMITS. IFSD. REPLACED THE LEFT ENGINE.SDR EIA2005259Engine · failedDURING CLIMB-OUT AT 5,000 FT AGL, NR 3 ENG EMITTED A BIG BANG AND STALLED. CAUSE OF DAMAGE UNDETERMINED. REMOVED AND REPLACED ENGINE PER WORK CARD F7201-7204 AND 7207.SDR WRNA20050029Engine · malfunctionedCLIMBING OUT THRU 16K FT, NR 2 ENGINE SHUTTERED, ACCOMPANIED BY LOUD NOISE. HIGH EGT, EPR AND OIL PRESSURE, TEMP ALL WITHIN LIMITS. SHUT DOWN NR 2 ENGINE. AIRCRAFT RETURNED TO FIELD, LANDING NORMAL.SDR HAEA200500187Engine · fodCREW PERFORMED A STATIC TO. BOTH ENGINES INDICATED NORMAL. AT 1500 AGL CREW HEARD AN ABNORMAL NOISE FROM THE LT ENGINE ACCOMPANIED BY HIGH EGT INDICATION. CREW REDUCED POWER ANDNOTED THAT THE NOISE ENDED. AN EMERGENCY WAS DECLARED AND THE ACFT RETURNED TO SDR ASMF200512011Engine · fodDURING TRANSIT CHECK, THE RT ENGINE BLADES FIRST STAGE WERE DETECTED WITH AND THE NOISE SUPPRESSOR HAD INCRUSTED A FOD. INSPECTION WAS PERFORMED, DETECTING 20 COMPRESSOR BLADES OF FIRST STAGE WITH DAMAGE OUT OF LIMITS IAW MM 72-00-00. AIRCRAFT WAS SENT TO THE SDR 2005UALA01415Engine · unknownRETURN TO FIELD DUE TO NR 1 ENGINE REDUCED TO IDLE. ENGINE 1 REVERTED FROM EPR MODE TO N1 MODE DUE TO THE APPARENT LOSS OF P2T2 PROBE HEATER. THIS IS PER DESIGN. THIS IS A CHRONIC ISSUE ON THIS ENGINE FIRST RTF EVENT 3 DEC MX REPLACED P2T2 PROBE PER TSM. EPR SDR SWIA200515969Engine · seizedLT ENG WILL NOT ROTATE. REPLACED LEFT ENG WITH SERVICABLE UNIT IAW MM 71-00-00, P/N: PW118B S/N OFF: 115664.SDR CA051205005Engine · making metalPRELIMINARY INVESTIGATION AND TROUBLESHOOTING HAS NOTED UNUSUALLY HIGH N3 INDICATION DURING A GROUND START ATTEMPT, WHICH SUGGESTS THAT THE ACCESSORY GEARBOX MAY HAVE LOST COUPLING TO THE N3 ROTOR. AS FURTHER SUPPORTING EVIDENCE, THE MASTER CHIP DETECTOR WAS SDR DHL2005805004Engine · failedNR 3 ENGINE FAILED DURING TAXI IN. TROUBLESHOT NR 3 ENGINE PER MM 71-00-00. INSPECTED INLET AND EXHAUST PER MM 72-00-00, NO DEFECTS FOUND.SDR CA051223009Engine · shutdownON APPROACH, THE ENGINE EMITTED A LOUD NOISE ACCOMPANIED BY AN UNCOMMANDED REDUCTION IN POWER. THE ENGINE WAS SHUT DOWN IN FLIGHT. SUBSEQUENT INSPECTION REVEALED METAL DEBRIS AT THE ENGINE CHIP DETECTORS AND FILTERS. P&WC WILL INVESTIGATE THE INCIDENT AND WSDR CA051209003Engine · malfunctioned(CAN) A/C WAS IN ROUTE TO DESTINATION, WHEN 20 MINUTES INTO THE FLIGHT, THE CAPTAIN NOTICED THAT EICAS INDICATIONS FLICKERED OFF THEN ON. LT ENGINE THEN SHUTDOWN UNCOMMANDED AND CREW RECEIVED NUMEROUS EICAS MESSAGES. (TC NR 20051209003)SDR CA051205002Engine · bird ingestionON TAKEOFF ROLL, A BIRD WAS INJESTED THROUGH THE LT ENGINE. THE CREW ABORTED TAKEOFF AND SHUTDOWN. THE ENGINE AND ENGINE INLET WILL BE REPLACED AND SENT FOR REPAIR.SDR COMA0570125Engine · overheatedFLIGHT 5281- RT MOTOR OVERTEMP DURING T/O, ITT 960 C. INSPECTED ENGINE AND FOUND NO DEFECTS. OPERATIONAL CHECKS WERE NORMAL.SDR 2005UALA01391Engine · malfunctionedNR 1 ENG EPR MODE FAILURE FOLLOWED BY INCREASED FUEL BURN RATIO. ENGINE 1 REVERTED FROM EPR MODE TO N1 MODE DUE TO THE APPARENT LOSS OF THE P2T2 PROBE HEATER. THIS IS PER DESIGN. CREW DECIDED TO DIVERT DUE TO POSSIBLE INCREASED FUEL BURN, SAFETY CONSIDERATIONSDR CED2006F00012Engine · fodAFTER TAKEOFF, THE NR 1 ENGINE STALLED. THE FLIGHT CREW RETURNED TO DEPARTURE WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED THE ENGINE AND FOUND THAT THE NR 1 ENGINE HAD ICE FOD. (K)SDR QXEA200501730Engine · unknownOKC - ON PUSHBACK FOR FLIGHT 4188 DURING ENGINE START, THE NR 1 AUTO SHUTDOWN DURING START. RETURNED TO THE GATE. MAINTENANCE FOUND THE LEFT FADEC START ABORT MESSAGE IN MEMORY DUE TO SLOW N2 RESPONSE. MAINTENANCE SUSPECTED ICING. PERFORMED GROUND RUN OF ESDR AT0500045Engine · inoperativeDURING CLIMB OUT, AT ABOUT 18,500 FT, 2 LOUD BANGS HEARD, RT ENGINE SPOOLED DOWN, EGT ROSE, SEVERE DAMAGE SUSPECTED RAN QRH. REMOVED AND REPLACED NR 2 ENGINE IAW TC 603. ALL OPS NORMAL. A/C OK FOR SVC.SDR CA051223006Warning Light · illuminatedDURING SPIN RECOVERY MANEUVERS THE ENGINE CHIP DETECTOR WARNING ANNUNCIATED ACCOMPANIED BY VIBRATION. THE AIRCRAFT DIVERTED FOR AN UNSCHEDULED LANDING. P&WC WILL INVESTIGATE THE EVENT AND ADVISE OF ROOT CAUSE ONCE ESTABLISHED.SDR CHQA200500207Engine · making metalE2 OIL IMPENDING BYPASS MESSAGE DURING CRUISE. OIL QUANTITY DROPPED TO 6 QUARTS, OIL TEMPERATURE WAS OPERATING AROUND 12.5 THEN WENT INTO RED. MOVED LEVERS ACCORDINGLY TO KEEP IN GREEN. LATER IN DESCENT, MOVED TO IDLE AND ENGINE 2 LOW OIL PRESSURE MESSAGE RSDR CA051223003Engine · overtempDURING CLIMB, THE ENGINE EMITTED A LOUD NOISE ACCOMPANIED BY AN INDICATED ITT OVER-TEMPERATURE. THE PILOT SHUT THE ENGINE DOWN IN FLIGHT AND DIVERTED TO POINT OF ORIGIN. SUBSEQUENT INSPECTION REVEALED FRACTURED POWER TURBINE BLADES. PWC WILL INVESTIGATE THESDR GAIA05034OPEngine · leakingDURING TAKEOFF ROLL THE COCKPIT FILLED WITH SMOKE. TAKEOFF WAS ABORTED AND THE AIRCRAFT TAXIED TO THE RAMP. INVESTIGATION FOUND OIL IN THE NR1 ENGINE BLEED SADDLE DUCTS. ENGINE REMOVED, AIRCRAFT PARKED. (K)SDR PNSA051106Engine · misriggedWHILE SETTING CTOT TO 80 PERCENT POWER AUTOCOARSEN ARMED LIGHT WENT FROM HIGH TO LOW WITH A POWER FLUCTUATION. FLIGHT CREW REDUCED POWER AND ABORTED TAKEOFF. MAINTENANCE FOUND MANUAL ENGINE RIGGING TO BE INTERFERING WITH AUTOCOARSEN ELECTRICAL SETTINGS. ENGISDR 05FDEA04010Engine · bird ingestionON DEPARTURE BIRD STRIKE LT NR 1 ENGINE. ENGINE VIB MAX APPROX 3.7 AT 85 PERCENT. AT IDLE APPROX 1.6; EGT NORMAL, N1 + N2 NORMAL OTHERWISE. REDUCED POWER FOR APPROACH. ENGINE HAS BEEN APPROVED FOR REMOVAL (DAMAGE) NEW ENGINE EXPECTED OMA 12/05/05 (THIS SDR CA051223001Engine · flamed outDURING CRUISE AT 38K FEET, BOTH ENGINES FLAMED-OUT. IN-FLIGHT RELIGHT ATTEMPTS WERE UNSUCCESSFUL AND THE AIRCRAFT DIVERTED FOR A DEAD-STICK LANDING. P&WC WILL PARTICIPATE IN THE INVESTIGATION OF THIS INCIDENT AND WILL ADVISE OF ROOT CAUSE ONCE ESTABLISHED.SDR DJFA2005168Engine · power lossEN ROUTE, SHORTLY AFTER POWER WAS REDUCED TO BEGIN DESCENT FROM CRUISE ALTITUDE, BOTH ENGINES EXPERIENCED A SUSTAINED POWER LOSS. UNABLE TO RESTART EITHER ENGINE IN FLT. EMERGENCY DECLARED & ACFT DIVERTED. UNDER NTSB INVESTIGATION. MX REPLACED AIRFRAME & E
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