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 engine_model_key = 'CF680A2' 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 engine_model_key = 'CF680A2' 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 HALA2009110900516Duct · dentedOPEN - ETOPS SIGNIFICANT SYS - FOUND DAMAGE TO OTBD REV HALF DUCT WALL OF NR 2 ENG, TRIANGULAR DENT APPROX 24" AFT OF FWD DENT MEASURES 2 INCHES X 2 INCHES X 2 INCHES X 0.0625 INCHES DEEP. ALSO NUMEROUS SCRATCHES. OK TO CONTINUE IAW HALM105 FILE NR R0033.SDR HALA2009110900514Blade · missingETOPS SIGNIFICANT SYS - FOUND OGV AT 6:00 POS BROKEN WITH MOST OF BLADE MISSING NR2 ENG. REPLACED OUTLET GUIDE VANE AT 6:00 POS AND INNER AND OUTER LINER ABD FILLET PANEL AT 6:00 IAW AMM 72-33-01-0, 04-001-H00/72-33-01-404-011-H00 PLAC. PERFORMED VIBRATION SUSDR HALA2009110900515Duct · damagedSUP - ETOPS SIGNIFICANT SYS - FOUND DAMAGE TO OTBD REV HALF DUCT WALL OF NR2 ENG, TRIANGULAR DENT APPROX 24" AFT OF FWD. DENT MEASURES 2 INCHES X 2 INCHES X2 INCHES X 0.0625 INCHES DEEP. ALSO NUMEROUS SCRATCHES. REPL NR2 ENG OUTER REVERSER HALF IAW AMM 78-31SDR HALA2009102700486Liner · damagedETOPS SIGINIFICANT SYSTEM - FAN MODULE INNER AFT LINER AT 11 O'CLOCK POSITION LIFTING NR 1 ENG. REMOVED AND REPLACED INNER LINER SEGMENT AT 11 O'CLOCK POSITION IAW 72-33-01-004-001-HOO, 72-33-01-004-001-HOO, 72-33-02-004-001 AND 72-33-02-404-019-HOO. RAN ENGISDR DL76S091635Module · missingDURING EA 01-477420-12 AD REV ORIG MEO1 FOUND ENTIRE O2/MASK MODULE MISSING OVER SEAT 12AB. INST O2 MASK/GEN MODULE ASSY AT 12ABSDR HALA2009092700443Engine · overtempETOPS SIGNIFICANT SYS - RT ENGINE WENT TO AMBER RANGE ON TAKEOFF. EGT WAS 938 DEG AT ROTATION. EGT WITHIN OPERATION LIMITS. ENGINE IS BEING MONITORED BY POWERPLANT ENGINEERING IAW AMM 71-00-00.SDR HALA2009092300437Liner · damagedETOPS SIGNIFICANT SYS - DURING OVERTEMP INSP FOUND INB LINER FOR OUTLET GUIDE VANE AT 9 O'CLOCK POS LOOKING FROM FWD LOOKING AFT LIFTING DUE TO DAMAGE AROUND FASTENERS. RMVD INBD LINER AND OGV AND FAIRINGS IAW AMM 72-33-03. INSTLD ACCOUSTICAL LINER SEGMENTS SDR HALA2009092200432Indication Sys · malfunctionedETOPS SIGNIFICANT SYSTEM - RT ENG EGT WENT TO RED RANGE. EEC WAS ON. PEAK EGT 946 DEG. TIME ABOVE LIMIT APROX LESS THAN 20 SECONDS. ACCOMP AMM 71-00-00-862-002-600 STEP G6 A(3)THRU(3)G. 9-23-09 NEED TO CONT STEP G6A(3)H. AS PER POWERPLANT ENGINEER CAUSE OF OSDR HALA2009091800429Pump · leakingETOPS SIGNIFICANT SYSTEM - ON WALKAROUND FOUND NR 1 ENG LEAKING HYD . FLUID. R&R NR 1 ENG HYD PUMP (ED0) PER AMM29-11-05 OPS & LEAK CHECK GOOD.SDR DL76L091253Oxygen Bottle · low pressureCREW O2 NEEDS SERVICING. REMOVED AND REPLACED CREW O2 BOTTLE IAW AMM 12-15-08, LEAK CHECK GOOD. CHECKED ALL MASKS, CHECK GOOD.SDR HALA2009072100317Engine · overtempETOPS SIGNIFICANT SYSTEM - RT ENGINE RED LINED AT 946 EGT FOR 11 SECONDS INDICATED ON ENGINE EXCEEDENCE EICAS PG, AUTO EVENT. RT ENG OK FOR SERVICE IAW MM 71-00-00 FIG 207A, INSP AREA A C/W.SDR DL76S091252Engine · cokedWHILE WORKING MCO ON LT ENGINE OVERHEAT DETECTION SYSTEM LOOP 2 OBSERVED SEVERE COKING ON UPPER ENGINE CASE AND HEAT DAMAGE TO PYLON INSULATION AND ELECTRICAL CONNECTORS AT J BOX. INSULATION AND ELECTRICAL CONNECTORS ON PYLON REPLACED. ENGINE SENT TO SHOP FOSDR HALA2009071500298Rub Strip · missingETOPS SIGNIFICANT SYS. DURING WAC FOUND NR 2 ENG RUB STRIP UNDER FAN BLADE MISSING SECTION 1 INCH X 1 INCH, 0.025 INCH DEEP, 0930 POSITION. OK TO GO IAW AMM 72-33-04-206-001.SDR HALA2009062900267Engine · overheatedETOPS SIGNIFICAN SYS - DURING CLIMB NR 2 ENG EGT REACHED 839 (AMBER) WITH BOTH ENGINES SET AT CLIMB THRUST. EGT CONTINOUSLY 25-35 DEGREES HOTTER THAN NR 1 ENG. NR 2 ENG EGT W/IN LIMITS IAW AMM71-00-00-201, FIG 207A ENG OVERTEMP INSP REQUIREMENT CHART. NO FUSDR HALA2009062800265Fuel/Oil Cooler · leakingETOPS SIGNIFICANT SYS - IAW FLT CREW FLUID (OIL) DRIPPING FROM NR 2 ENG. FOUND OIL LEAK FROM NR 2 ENG "GANG DRAIN" FOUND SOURCE AS FUEL/OIL COOLER BYPASS DRAIN PORTS. GRD RUN UP ENG AT IDLE NO LEAKS NOTED. STATIC LEAK CK OK IAW AMM71-71-00 OK FOR SVC.SDR HALA2009061600243Throttle · malfunctionedETOPS SIGNIFICANT SYSTEM, ENG THRUST LEVER MISALIGNED 1 KNOB DURING TAKEOFF CLIMB, CRUISE WITH EEC'S OFF ALIGNMENT NOT CHECKED WITH EEC'S ON. ALL PARAMETERS NORMAL. PERFORMED FIM 76-11-00 NR 1 THROTTLE 5 LBS FWD PUSH 4 LBS PULL BACK. NR 2 THROTTLE 5.5 LBS PSDR HALA2009061600244Eec · malfunctionedETOPS SIGNIFICANT SYSTEM, RT ENG EGT WENT INTO RED RANGE EEC WAS OFF 943 DEG FOR 2 SEC. BOROSCOPE PERFORMED RT ENG, NO DEFECTS NOTED PER TASK 71-00-00-862-002-900.SDR HALA2009061500245Engine · overtempETOPS SIGNIFICANT SYSTEM, RT EGT AMBER EICAS ENGINE PERFORMANCE MAINTENANCE PAGE FAULT. RT EGT AMBER RECORDED 895 + - 03.1 897 MAX OK PER AMM 71-00-00/201 FIG 207A ENGINE OVER TEMPERATURE INSPECTION REQUIREMENTS CHART. OK FOR CONTINUED SERVICE. NO FURTHER ASDR HALA2009052700203Idg · inoperativeETOPS SIGNIFICANT SYSTEM - EICAS R-GEN OFF ILLUMINATED. CONDITION RETURNED TO NORMAL AFTER GENERATOR RESET, 1ST TIME ON ENG START, 2ND TIME 3 HRS INTO FLT, 3RD TIME 1 HR BEFORE LDG FRM 24224802. REMOVED AND REPLACED R GCU IAW AMM 24-22-00-404-001 AND 24-22-0SDR HALA2009052300195Fan Blade · damagedNR 1 ENG BLADE (FAN) NR 28 HAS NICK ON L/E 7.5 INCHES FROM TIP, 3/16 INCH DEEP. BLENDED BLADE PER MM72-31-02 BLEND WITHIN LIMITS. OK FOR SERVICE.SDR DL76S090918Starter · overheatedAFTER APU START NOTICED ACRID SMELL IN CABIN. NO VISIBLE SMOKE. FOUND STARTER ON APU BURNED. APU BATTERY AND CHARGER DEAD. REMOVED AND REPLACED APU BATTERY/CHARGER AND STARTER IAW AMM. CHECKED SPRAG CLUTCH NTF. ACFT OK FOR SERVICE.SDR HALA2009041900156Blade · fodETOPS SIGNIFICANT SYSTEM, ON WALKAROUND FOUND FOD ON BLADE NR 21 ON NR 1 ENG. BLENDED DAMAGED AREA PER AMM 72-31-02 DAMAGE IN AREA B DAMAGE OK PER AMM 72-31-02, NO CRACKS NOTED.SDR AALA2009041100002Tube · leakingLAX LEFT HAND ENGINE WAS SHUTDOWN DUE TO ZERO OIL PRESSURE. LANDED LAX WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. FOUND OIL LINE KINKED AND LEAKING. REPLACED ENGINE OIL FILTER TUBE ASSEMBLY. SYSTEM GROUND CHECK NORMAL OPERATION. (CLOSED)SDR HALA2009033000117Unknown · unknownETOPS SIGNIFICANT SYSTEM, LT AND RT ENG IDLE OUT OF SYNC. LT ENG IS LOWER BY 2 PERCENT N1 AND 1 PERCENT N2. AT CRUISE, LT AND RT N1 SAME. N2 LT IS HIGHER BY 2 PERCENT. ACCOMP GROUND TEST FOR IDLE POWER (TEST 3) ON BOTH NR 1 AND NR 2 ENGS GRD IDLE AND APP ISDR HALA2009030500085Fan Blade · dentedETOPS SIGNIFICANT SYSTEM - NR 1 ENGINE FAN ROTOR BLADE 21 HAS DENT APPROX 5.5 INCHES FROM ROOT AREA AT LEADING EDGE. BLENDED NR 1 ENGINE FAN ROTOR BLADE 21 IAW M/M 72-31-02-801 SEE L/P 316815 ITEM 70. ACCOMPLISHED FLUORESCENT PENETRANT TEST OF NR 1 ENGINE, BSDR HALA2009022400061Connector · unsecureETOPS SIGNIFICANT SYSTEM, NO N2 ROTATION RT ENG DURING START. OPEN ENG COWL AND RESEATED START VALVE CONNECTOR. OPS CKD OK. OK FOR SERVICE, CLOSED AND SECURED RT ENG COWL.SDR HALA2009021400048Engine · stuckETOPS SIGNIFICANT SYSTEM - BTB - ENGINE NR 1 STUCK IN FLIGHT IDLE AFTER START. AS ACFT APPROACHED GATE ENGINE RETURNED TO GROUND IDLE. PERFORMED ENG RUN OF NR 1 ENG GRD, OP'S CHECK GOOD. NO DEFECTS NOTED, OK FOR SERVICE.SDR ABXA200902130012Compressor · stalledCLIMBING OUT OF KIX AT FL340, THE RIGHT ENGINE COMPRESSOR STALLED 3 TIMES, PULLED BACK THE RIGHT THROTTLE JUST A LITTLE AND THE STALLS STOPPED. THE ANTI-ICE WAS OFF, A/T WERE ON. AIRCRAFT CONTINUED TO CLIMB AND THERE WERE NO POWER CHANGES. THERE WERE NO ABNSDR HALA2009011900026Fuel Filter · warning lightETOPS SIGNIFICANT SYSTEM, ATB, DUE R ENG FUEL FILTER EICAS MSG. REPLACED E ENG FUEL FILTER IAW AMM 73-11-08 AND REPLACED CONNECTOR D2068 FOR THE BY PASS SWITCH. LEAK CK GOOD NO FAULTS. CLOSED AND SECURED COWLING.SDR HALA2009011900027Connector · unsecureETOPS SIGNIFICANT SYSTEM, ATB, DUE R ENG. FUEL FILTER EICAS MSG. REPLACED E ENG FUEL FILTER IAW AMM 73-11-08 AND REPLACED CONNECTOR D2068 FOR THE BYPASS SWITCH. LEAK CK GOOD, NO FAULTS. CLOSED AND SECURED COWLING.SDR DL76S081727Engine · failedON DESCENT INTO ATL THE LEFT ENGINE ROLLED BACK. PERFORMED IN FLIGHT SHUTDOWN OF ENGINE. INSP INLET AND EXHAUST NTF. CHECKED CHIP DETECTORS NTF. RAN ENG IDLE AND T/O POWER ALL PARAMETERS NORMAL. SUMPED LEFT TANK BEF RUN NTF. REMOVED FUEL PUMP AND MEC. RSDR RYNA200800044Fan Blade · out of balanceDURING CLIMB AND LEVEL OFF AT F/L 370 RIGHT ENGINE VIBRATION REACHED 3.9 UNITS. THE AIRCRAFT DIVERTED TO ATLANTA FOR MAINTENANCE TO DELTA AIRLINES MAINTENANCE CENTER. ACCOMPLISHED BORESCOPE INSPECTION, FAN BLADE LUBRICATION, RIGGED VSV & VBV SYSTEM AND BALANSDR DL76S081236Engine · making metalNR 2 ENGINE OIL PRESSURE WENT TO ZERO, HEARD AUDIBLE STALL. CREW SHUT OFF FUEL LEVER. MTC FOUND METAL IN THE TAIL PIPE. NR 2 ENG REPLACED PER TRANS 1T145.SDR ABXA200810270254Engine · defectiveLEFT FAN ENGINE VIBRATION HIGH 4.7. OTHER VIBRATION INDICATIONS WERE: AIRPLANE VIBRATION, AUDIBLE NOISE, VIBRATION FOLLOWS THRUST CHANGE. REPLACED NR 1 ENGINE PER WORK CARD NR 7010. OPS CHECK NORMAL.SDR DL76S081112Gasket · leakingHAD FUEL IMBALANCE DURING FLIGHT. LEFT SIDE WAS 1300-1400 LBS LOWER THAN RIGHT. AFTER BALANCED TOTAL FUEL WAS LESS THAN CALCULATED. DETERMINED FUEL LEAK WAS POSSIBLE AND DIVERTED TO LAS. FOUND FUEL LINE FROM FCU TO FUEL PUMP LINE GASKET LEAKING. REPLACED SDR ABX2008F00002Battery Pack · dischargedEMERGENCY LIGHT BATTERY PACK M734 WOULD NOT ILLUMINATE EMERGENCY LIGHTS. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK M734 IAW MM 33-51-07. OPS CHECKED GOOD. (K)SDR DL76S080845Engine · failedDURING CRUISE FLT FELT VIBS AND HEARD UNUSUAL NOISE VIBS AT5.0. WHILE PERFORMING WALKAROUND CHECK FOUND METAL IN TAILPIPE OF THE NR 2 ENG. ENG CHG IN PROGRESS.SDR HALA0800596Eec · inoperativeETOPS SIGNIFICANT SYSTEM, RT ENGINE HAD A 945 EGT EXCEEDENCE FOR 8 SECONDS. EGT OVERTEMP CAUSED BY OPERATION WITH EEC INOP/OFF. REF DMI NR 78256 PERFORMED INSP PER MM 71-00-00. NO
FAULTS NOTED A/C OK FOR CONTINUED SERVICE.SDR HALA0800585Transmitter · inoperativeETOPS SIGNIFICANT SYSTEM , RT OIL PRESSURE NO DIGITAL READING ON MONITOR. REMOVED AND REPLACED RT ENG OIL PRESS XMTR PER AMM 79-32-01 OPS AND LEAK CHECKED GOOD.SDR HALA0800587Eec · inoperativeATB - ETOPS SIGNIFICANT SYSTEM, EICAS L ENG EEC INOP. REMOVED AND REPLACED THE EEC IAW 73-21-07 ACCOMPLISHED EEC PMC TEST. NEED TO ACCOMPLISH TASK 71-00-00-735-202-G00 (CONT. BELOW). ACCOMPLISHED TEST 11 EEC (PMC)/MAIN ENGINE CONTROL (MEC) TEST, TESTED GOODSDR HALA0800533Heat Exchanger · leakingETOPS SIGNIFICANT SYSTEM, ON ARRIVAL AT GATE FOUND NR 2 ENGINE HEAT EXCHANGER AIR OIL LEAKING. REMOVED AND REPLACED AIR OIL HEAT EXCHANGER PER AMM 79-21-09-404-013-N00 AND AMM 71-00-00/501. OPS CHECK GOOD AND LEAK CHECK GOOD.
SDR HALA0800479Eec · malfunctionedETOPS SIGNIFICANT SYSTEM, LEFT ENG CONTROL EICAS ILLUMIN BTB. ACCOMP FIM 73-21-00 FIG 112. NO FAULTS NOTED. RESET LEFT ENG EEC DISCREDE C/B. ACCOMP GROUND RUN UP OF LEFT ENG, OPS CK GOOD. EICAS MSG CLEARED. OK FOR SERVICE.SDR HALA0800420Overheat Loop · malfunctionedETOPS SIGNIFICANT SYSTEM, INTERMITTENT EICAS STATUS MSG, R ENG OH LP2 DISPLAYED. REPLACED NR 2 ENG FWD UPPER LOOP PER AMM 26-11-02. OPS CHK PER AMM 26-11-00. ENGINE HIGH PWR RUN, NO DEFECTS NOTED.
SDR HALA0800427Structure · damagedNR 1 ENGINE I/B CORE COWL HAS VARIOUS DEFECTS ALONG THE BOTTOM STRUCTURE. BLENDED THE DAMAGE AREA IAW SRM 54-41-02, FIG 101.SDR DL76S080362Apu · malfunctionedSMOKE DETECTORS AT STATIONS 214-215-219 SOUNDED DUE TO LIGHT OIL MIST IN THE CABIN, ALL 3 MID LAVS. THIS HAPPENS ONLY ON THE GROUND WITH APU AIR AND NO ENGS RUNNING. FWD APU TO MCO AND PLACARD PER MEL 49-11-01A. REPLACED APU PER M/M. LEAK CKS GOOD. GENERASDR HALA0800374Attach Bracket · gougedNR 2 ENGINE NOSE INLET COWL TO FAN CASE ATTACHMENT BRACKETS AT 5 O'CLOCK POSITION GOUGED. DAMAGE AT 5 O'CLOCK POSITION ON NOSE COWL AFT BULKHEAD INNER RING BLENDED IAW SRM 54-11-02/1A01, FIGURE 101, DETAIL 111, WITHIN SRM LIMITS.SDR HALA0800375Attach Bracket · gougedAT 2 ENG NOSE INLET COWL TO FAN CASE ATTACHMENT BRACKETS AT 7 O'CLOCK POSITION GOUGED. DAMAGE ON NOSE COWL AFT BULKHEAD INNER RING, 7 O'CLOCK POSITION BLENDED IAW SRM 54-11-02/1A01, FIG 101, DETAIL 111, WITHIN SRM LIMITS.SDR DL76L080298O-Ring · cutFLIGHT 117 - DECLARED EMERGENCY INTO ATL DUE TO LOSS OF CENTER SYSTEM HYD QTY AND PRESS LOST. UNEVENTFUL LANDING AND TAXI. FOUND CUT O-RING ON CTR SYS LCCA FILTER BOWL. REPLACED SAME CKS OK.SDR DL76S080297Elbow · crackedL ENG FIRE LP1 STATUS MESSAGE ABOUT 15 MINUTES INTO FLIGHT FOLLOWED BY ILLUMINATION OF L ENGINE FIRE WARNING LIGHTS. ENGINE SHUTDOWN IN ACCORDANCE WITH QRH. NOTE, FIRE SWITCH WAS PULLED, HOWEVER, FIRE BOTTLE WERE NOT DISCHARGED. FOUND NR 1 ENG LT HIGH PRESSSDR ABXA080192Mec · defectiveRT ENG COMPRESSOR STALL AT LEVEL OFF 37000` ENG STABLE AT POWER REDUCTION. ENG PARAMETERS NORMAL EVENT RECORDED. RIGGED VSV, CHECKED FEEDBACK CABLE, WITHIN LIMITS. COMPLIED WTIH BOROSCOPE INSPECTION. NO DAMAGE NOTED IAW B767 MM 75-31-03-5-72-00-00-6. REMO
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