JASC 7100
Service difficulty reports · 635
Reports filed under 7100 · Powerplant System, newest first.
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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 = '7100' 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 = '7100' 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 UPS03640234Engine · stalledINSPECTION TYPE: ETOP, SUSPECTED COMPRESSOR STALL LT ENGINE. VIBRATION INCREASED TO 4.4, ALL OTHER PARAMETERS NORMAL. REPLACED LT ENGINE, OPS CHECK NORMAL IAW MAINT FUNCTION TC6002.SDR LR7A03009Vane · failed#4 ENG. DECOUPLED IN-FLIGHT 25,000 FT APPROX 11,000 LB. TORQ. ENG. SHUTDOWN IAW QRH.SUSPECT INGESTION FROM PART OF 2ND STAGE COMPRESSOR VANE.REMOVED AND REPLACED #4 ENGINE ASSY PER JOB CARD HN71136 AND TEST RAN PER JC 7101. ENGINE OPS CHECKS GOOD AND LEAK CHESDR HEEA084194Engine · making metalENGINE CHIP LIGHT ILLUMINATED, FOUND NUMEROUS FLAKES AND CHIPS ON ELECTRICAL PLUG AND MO1 MAGNETIC PLUG.SDR HEEA084189Distributor · contaminatedCARBON BUILD UP IN FUEL DISTRIBUTOR CAUSING ENGINE NOT TO START DUE TO COMPRESSOR WOULD NOT TURN.SDR IXXA0300011OEngine · wornAFTER DEPARTURE FROM KBFI ENROUTE TO KPDX CREW NOTICED OIL QUANTITY IN NUMBER 2 ENGINE DROPPED ABNORMALLY. AS A PRECAUTIONARY MEASURE THE #2 ENGINE WAS SHUTDOWN AND AIRCRAFT RETURNED TO KBFI FOR AN UNEVENTFUL LANDING. POSITIVE OIL PRESSURE WAS MAINTAINED THRU SDR HEEA082420Check Valve · crackedCHECK VALVE CRACKED AND LEAKING. SCRAPPED.SDR HEEA082624Actuator · inoperativeACTUATOR INOPERATIVE.SDR HEEA082623Actuator · inoperativeNO RESPONSE FROM ACTUATOR WHEN SWITCH IN ON POSITION..SDR DHL2002750007Control Rod1) AT FL 330 ENGINE #3 THRUST LEVER WILL NOT ADVANCE PAST 81% N1.2) FOUND #3 ENGINE THROTTLE CONTROL ROD END BOLT TOO LONG AND CHAFING AGAINST FUEL ROD BOLT. REMOVED AND REPLACED CONTROL ROD BOLT. RAN #3 ENGINE, CHECKED TRIM. CHECKED GOOD IAW JRH 5.2 & 71-00SDR HEEA082593Blower · damagedBLOWER ASSY PARTICLE SEPERATOR LIGHT CAME ON. FOUND SHAFT SHEARED. TO BE SENT TO VENDOR FOR REPAIR.SDR HEEA082565Pressure Switch · malfunctionedPRESSURE SWITCH MALFUCNTIONED, BLOWER LIGHT WOULD FLICKER. PENDING VENDOR RETURN.SDR DL767021395Engine · failedLEFT ENG SURGE IN FLIGHT AND ON LANDING. ENG SHUT ITSELF DOWN ON LANDING AT 5 THOUSAND FT. ENG CHANGE IS IN WORKSDR YENA200228Service difficultyFlight #88, ONT to JFK, had fairly strong smell of burnt oil during inter stages of take off and climb out, Smell persisted and aircraft returned to ONT. Landing weight was aprx 155.500. Touchdown was smooth with minimun vertical speed. Preliminary report indiSDR 11060230Engine · flamed outBOTH ENGINES FLAMED OUT. INSPECTION DID NOT REVEL ANY MECHANICAL MALFUNCTION. AIRCRAFT LANDED SAFELY. DID NOT RELIGHT ON THEIR OWN.SDR IXXA0200154SEngine · crackedDURING ROUTINE C CHECK INSPECTION, A CRACK WAS DISCOVERED IN THE # 3 ENGINE INBOARD THRUST REVERSER HALF BLOCKER DOOR SUPPORT RING AT THE 11 O'CLOCK POSITION. REPAIR ACCOMPLISHED REMOVAL STOP DRILLED CRACK FABRICATION AND INSTALLATION OF REPAIR ANGLE IN ACCORDSDR UPS02539824Engine · overtempRT ENGINE TEMP CLIMBED TO 944 +. ENGINE WAS SHUT DOWN AND ONE FIRE BOTTLE WAS BLOWN. T/S PER FIM 71-05-00 FIG 110- REPLACED W-31 EGT HARNESS - PERFORMED EGT CABLE & THERMOCOUPLE TEST, CHECKED OK PER MM77-21-03-5.SEI 6 LOW COMPARED TO EICAS. W31 HARNESS. ENSDR ANCF200200020Service difficultyDURING CRUISE AT 28000 FT RH ENGINE PRESENTED A POWER LOOSE OF 50%, RH ENGINE WAS REDUCED TO IDLE AND POWERED IT AS A TEST. RIGHT AFTER, THE RH ENGINE FLAMED OUT. IN THE FIRST ATTEMPT IT DID NOT START.ADDITIONALY CABIN ALTITUDE ALARM WAS PRESENTED. CREW DECIDESDR 200201206Engine · bird ingestionNR 2 ENGINE SHUTDOWN FOR HIGH VIBS, 2.6 BOTH CHANNELS. OIL PRESSURE 19 PSI, ALL PARAMETERS NORMAL. INSPECTED INLET AND EXHAUST , REMOVED EVIDENCE OF BIRD STRIKE FROM ONE BLADE, INSPECTED CHIP DETECTORS (NO DEBRIS FOUND), RAN ENGINE ANE PERFORMED TEST NR 11. SDR 2002F00906B-Nut · loose(ORIG-CLOSED) FLIGHT NUMBER 205. DURING CRUISE EICAS MSG RT ENG OVHT DISPLAYED. EXTINGUISHED AFTER THRUST REDUCTION. MAINTENANCE TROUBLESHOT PER FIM 26-12-00 FOUND LOOSE B-NUT LINE ON PRSOV LINE. TIGHTENED LINE & TEST NR 4 COMPLIED WITH. SYSTEM CHECKED OK.SDR P5CA0200698Gearbox · failedSHORTLY AFTER T/O, #1 ENG. LOW OIL PRESSURE LIGHT ILLUMINATED. OIL PRESSURE DROPPED TO 10psi & WAS STEADY; OIL QTY SHOWED FULL & WAS STEADY. PERFORMED LOSS OF OIL PRESSURE PROCEDURE IAW AFM. COULD NOT RESTORE ENG. OIL PRESSURE OR EXTINGUISH LIGHT, THEREFORESDR C2XA02TY121Engine · corrodedTYS, During a schedule inspection corrosion was found on the left engine fancase, lower side. Maintenance removed the corrosion, applied chrome pickle solution to magnesium parts, applied corrosion resistant paint I/A/W-EC7000-01001, EC7220-01009, AE3007A-70-0SDR C2XA02TY120Engine · corrodedTYS, During a schedule inspection corrosion was found on the right engine fancase, lower side. Maintenance removed the corrosion, applied chrome pickle solution to magnesium parts, applied corrosion resistant paint I/A/W-EC7000-01001, Ec7220-01009, AE3007A-70-SDR DL76S020915Duct · wornAIR TURN BACK RT ENG OVERHEAT MSG AFTER TAKEOFF. FOUND 8TH STAGE DUCT SEPERATED ON NO.2 ENG. REPLCD DUCT BETWEEN CK VLV AND PRECOOLER.SDR CX7A194J13Engine · stoppedDuring T/O roll, Tq was 94% on both engines, ITT below 890 degrees. After rotation at 80-100 feet, a bang and shudder was felt and ITT on the right engine ran away to max. Tq reduced to zero, prop autocoarsened. Engine had failed. Emergency declared.Mx R/RSDR DL757020891Engine · failedRT ENG FAIL AT APPROX 500FT ON T/O FROM SNA ACFT. WT. 213000 FLAPS 20 DEG CA BOROSCOPED ENG FOUND 15TH-17TH STG HPC DAMAGED BEYOND LILIMITS. ENGINE CHG REQUIRED. RIILAX029439. REPL RT ENG. RAN PER PFHB. ALL CKS NMSDR 10991Control Cable · damagedCABLE STIFF, THIS CABLE RUNS THROUGH THE FIRE WALL AND WITHIN THE TURBO REGION. HEAT GENERATED FROM TURBO ASSEMBLY AFFECTS INSIDE LINNING. RECOMMEND A FIRE JACKET OR ALTERNATE MEANS TO SHIELD CABLE ASSEMBLY FROM HEAT.SDR P2EA2002M049EngineDuring flight from LGA to MCI the right engine flamed out at 35,000 ft. Attempt to re-start was unseccessful. Performed unscheduled landing at PIT without incedent. Removed and replaced right engine IAW Job Card 80VG-1A-1. This closes SDR ...M049.SDR DL76S020611Engine · unserviceableON TAKE OFF ROLL ABOUT 130 KIAS, LEFT ENGINE TEMP WENT TO 975, PULLED THROTTLE BACK TO KEEP WITHIN LIMITS, CONTINUED TAKE OFF AT 150 AGL, LEFT ENGINE ROLLED BACK TO IDLE AND TEMPWENT TO 1100. POWER CAME BACK TO IDLE AND RETURNED TO FIELD.THE ENGINE WAS NOT SSDR HEEA078912Bearing · wornWORN BEARINGS.SDR 0201619883EngineDURING TAKEOFF, THE CREW REPORTED SMOKE IN THE AFT CABIN AREA WITH ASSOCIATED LEFT LAV SMOKE DETECTOR WARNING. AIRCRAFT RETURNED TO FAR AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE RIGHT ENGINE. AIRCRAFT RETURNED TO SERVICE.SDR UPS02438085EngineINSPECTION TYPE:N/A SHORTLY AFTER DECENT, SMOKE CAME INTO COCPIT FROM UNDETERMINED SOURC E. ENTERED FROM VENTS WITH ALL SYSTEMS OPERATING NORMALLY. PER DISCUSSION W/FLT CREW, SMOKE TO BE VERY LIGHT & OF OILY NATURE T/S PER M/M 71-00-44. FOUND #3 ENG N2 GRNSDR IXXA0200018OCowling · damagedDURING A ROUTINE MAINTENANCE PREFLIGHT IN TER, MINOR EVIDENCE OF DAMAGE TO #1 ENGINE OUTBOARD COWLING. MAINTENANCE INSPECTED THE ENGINE IN ACCORDANCE WITH AN APPROVED DER ENGINEERING DIRECTIVE EDQ11-1. NO ADDITIONAL DAMAGE WAS NOTICED AND THE ENGINE PERFORMANCSDR CA020606003Gear · wrong part(CAN) ENGINE WAS PUT TOGETHER WITH THE WRONG CAMSHAFT GEAR. THE ENGINE WOULD RUN BUT THE MAGNETO DROP WAS HIGH. ALSO IF YOU EXERCISED THE PROP AT ABOUT 1700 RPM THE ENGINE WOULD STALL OUT. THROTTLE RESPONSE AT LOWER RPMS WAS SLUGGISH AND WOULD MAKE THE ENGINE SDR VNAA0203044Contactor · failedAFTER TAKE OFF THE CREW REPORTED THE RIGHT HAND ENGINE HAD A LOW POWER TORQUE SPILT AND RETURNED TO PIT. MAINTENANCE INSPECTED AND REPAIRED A CONTACTOR ON THE TRIM SWITCH IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 71-00-00. OPERATIONAL CHECKS WERE PERFORSDR EVA200201Engine · damaged1. During initial climb, Captain notice the L Engine N1 vibration indicationin on the EICAS is up to 3.3 and N2 up to 5.0. All the rest parameters are normal.2. After 2 hours in cruise, "L ENG OIL FILTER" message appeared in the EICAS. Pilto followed the QRH pSDR S02271003PowerplantB18771 A/C RREJECT T/O DUE TO #3 ENG SURGE AND ALL MAIN WHEEL TIRES DEFLATE.C/A:1.ENG CHANGE FOR SHOP INVESTIGATION/RPLD ALL MAIN WHEEL TIRES. 2.PERFORM #3 ENG REPLACEMENT IAW 4L71-301A, ENG R/U TEST COND NML. 3.ALL MAIN WHEEL TIRES(16EA)AND BRAKES(16EA)RPLD, SDR VNAA0202015Engine · failedAFTER BEING CLEAR FOR A VISUAL APPROACH, THE CREW REPORTED ENTERING AN AREA OF MODERATE TURBULENCE. THERE WAS A SINGLE JOLT, NOBODY SUSTAIN ANY SERIOUS INJURIES. THE LEFT HAND ENGINE WAS REPORTED TO SHUT DOWN DURING THE EVENT. WITHOUT SUFFICIENT TIME FOR A SDR EVAS91004Hmu · failedDURING TAKE OFF, NR 1 ENGINE LOW N2 THEN FLAME OUT. ON GROUND REPLACED EEC & HMU, OPR CHECKED NORMAL.SDR 0200229754ExciterDURING RIGHT ENGINE START, THE EGT WOULD NOT RISE. TAKEOFF WAS ABORTED. AFTER ENGINE RESTART, THE TOWER REPORTED SMOKE AND FIRE IN THE RIGHT ENGINE TAILPIPE. CREW SHUT DOWN THE RIGHT ENGINE, DISCHARGED TWO FIRE BOTTLES, AND AN EMERGENCY PASSENGER EVACUATION OFSDR CA020117004Engine · failed(CAN) AIRCRAFT DEPARTED WASHINGTON DULLES INTERNATIONAL AIRPORT ON FLIGHT 7187, THE FLIGHT CREW DETECTED A SEVERE VIBRATION AND RESULTANT ENGINE SHUTDOWN WITHOUT PILOT'S INPUT. THE AIRCRAFT RETURNED TO THE ORIGINATING AIRPORT AND DECLARED AN EMERGENCY. ENSDR DL76S011984Manifold · leakingIR - LOST R ENG OIL PRESS (PRESS INDICATING 4 PSI) ENG SHUTDOWN 20 MIN BEFORE LNDG. (4 PSI INDICATING WHILE WINDMILLING. CA - FOUND FUEL POURING FROM FUEL MANIFOLD AT 5 OCLOCK POS. FROM UPPER BRANSDR S01271035Oil SystemB-18751 # 1 ENG BREATHER TEMP REACH 220 DEG C DURING CLB. OIL TEMP HIGH BUT OIL TEMP INCREASE GRADUALLY TO AMBER BAND. THEN OIL QTY DROP DOWN TO ZERO. ENG IN FLT S/D. C/A:1.REPLENISHED # 1 ENG OIL TO NORMAL LEVEL THEN MOTORING CK FOUND OIL LEAKING FROM LH # 3 SDR HEEA076956Engine · making metalENGINE MAKING METAL.SDR HEEA077010Tube · wrong partINCORRECT LINE. REPLACED WITH SERVICEABLE TUBE.SDR HEEA076803Engine · leakingLOW POWER, LEAKING.SDR HEEA076465Control Unit · failedCAUSING TORQUE SPLITS. REPLACED WITH SERVICEABLE TORQUE CONTROL UNIT.SDR XJ22002F00001Retainer · corrodedSERVO WAS REMOVED FOR HOWLING NOISE IN FLIGHT, UNIT WAS DISASSEMBLED FOR OVERHAUL AND PN 41002521 COVER TO RETAIN VALVE, ID CORRODED AND PN RS62 RETAINER TO RETAIN BYPASS VALVE SPRING WAS RUSTED IN HALF. IF RETAINER FAILED THE SERVO WOULD GO INTO BYPASS AND PSDR MASAM01101Service difficultyIN FLIGHT, THE PILOT NOTICED AN OILY HAZE IN THE COCKPIT AND CABIN. THE PILOT SECURED THE NR 1 ENGINE BLEED WHICH SEEMED TO DISIPATE THE HAZE. THE AIRCRAFT RETURNED TO THE FIELD WITH AN UNEVENTFUL LANDING WHERE MAINTENANCE TROUBLESHOT THE PROBLEM. ON 8/13 MSDR ARWA0010806Fan Blade · bindingDuring cruise # 2 engine shut down due to vibration enroute to CLO. Continue Flt., landing CLO.Corrective Action: Inspected # 2 engine IAW MM fault isolation 71-91-00, configuration 2, figure 103, and no damage found. Blades # 11 and # 12 found to be lockedSDR UPS01536490Engine · unserviceableINSPECTION TYPE:N/A ATB-LEFT ENGINE FAILED AT T/O LOAD COMPRESSOR STALL WAS HEARD. FLAM ES WERE SEEN COMING FROM ENGINE PARTS. STRUCTURAL DAMAGE TO AIRCRAFT WAS NOTED ***SUPPLEMENTAL MRR*** R&R LEFT ENGINE PER TC 5001 AND TESTED ENGINE PER TC 5002. RUN C
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