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 = 'CF66D' 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 = 'CF66D' 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 FDEA201206252340Skin · misrepairedRIGHT WING NR 1 SPOILER UPPER SURFACE XISP 226 MISREPAIRED. SPOILER PANEL REPLACED IAW AMM 27-60-01-4, REV 14.3. REPAIR CLASSIFIED AS MINOR GMM 6-2-100, REV 115.SDR FDEA201206232320Fuel Control · malfunctionedFLEX PWR SET FOR 50 PERCENT, THROTTLES ADVANCED SMOOTHLY WHEN AUTOFLT SELECTED TO THE APPROPRIATE REDUCED PWR CHEVRON INDICATED SETTINGS ON THEN 1 GUAGE. THROTTLES CLAMPED NORMALLY PRIOR TO 80KTS. AFTER 80 KTS THE NR 3 ENGINE BEGAN NOTICEABLY SURGING WITH NSDR FDEA201206232307Skin · misrepairedSKIN MISREPAIRED BS 886 BETWEEN LONGERONS 39 TO 42 RT. REPAIRED IAW EA 8-5330-159852. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REV 115.SDR FDEA201206232308Skin · misrepairedLT WING OTBD AILERON LOWER SURFACE AT XOA 907 MISREPAIRED. REPAIRED IAW SRM 57-10-00, VOL 1, FIG 2, REV 98. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 115.SDR FDEA201206232309Skin · misrepairedLT WING INBD AILERON LOWER SURFACE AT XIA 329 MISREPAIRED. REPAIR CARRIED OUT IAW SRM 57-10-00, FIG 01, VOL 1, REV 99. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 115.SDR FDEA201206232311Skin · misrepairedLT WING NR 5 SLAT INNER SKIN AT XOS 722 MISREPAIRED. REPAIR CARRIED OUT IAW SRM 57-10-00, FIG 31, VOL 1, REV 98 & EO 8-5100-7-5001B2, PART 2. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 115.SDR FDEA201206042073Blade · damagedON POST FLIGHT, FOUND FOD DAMAGE TO NR 3 ENGINE FAN BLADE WITH BIRD REMAINS VISIBLE. PERFORMED FOD BOROSCOPE INSPECTION IAW MD10 AMM 72-00-00-6-1, FIG 609, ITEMS 5 AND 10 WITH NO LIMITING DEFECTS FOUND. PERFORMED FOD CLOSED COWLING INSPECTION IAW AMM 72-00-0SDR FDEA201205181838Hinge Fitting · corrodedRT WING OTBD FLAP, INBD FORWARD HINGE LOWER ATTACHMENT INBD BORE FOUND WITH CORROSION. REWORK CARRIED OUT IAW EA 8-5750-160615 PART 1 A STEPS 1, 2, 3, 4, 5 AND 6. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.SDR FDEA201202070507Throttle Cable · wornNR 2 THROTTLE WOULD NOT GO PAST, RETARD PAST 70 PERCENT AT ALT, 60 PERCENT AT 5000'. NR 2 ENG WINDMILLED APPROX 10 MINS. THROTTLE SYS APPEARED TO BE PHYSICALLY FROZEN, THROTTLE DID PHYSICALLY RETARD COMPLETELY AFTER A FEW MINUTES OF ACFT BLOCKING IN (ENGSDR FDEA201201100063Blades · damagedON TAKEOFF, WITH INITIAL ADVANCE OF THROTTLES, GOT NUMEROUS COMPRESSOR STALLS. RETARDED THROTTLES AND NOTICED ENGINE NR 3 EGT HIGH. SHUTDOWN ENG NR 3 AND RETURNED TO GATE. PERFORMED VISUAL INSPECTION OF INLET AND EXHAUST OF NR 3 ENGINE NO OBVIOUS DEFECTSDR FDEA201111184968Compressor · stalledAT ROTATION NR 1 ENG COMPRESSOR STALLED. HEARD A LOUD BANG WITH YAW AND TEMP AT 1097 DEGREES. N2 INDICATION HAD AN X WITH NO INFORMATION SHOWING. REMOVED AND REPLACED THE ENGINE.SDR FDEA201111114874Sensor · failedAIR MANIFOLD 2 FAIL ENROUTE. REPLACED SENSING ELEMENT D1-49C.SDR FDEA201108313593Sensor · failedFIVE MINUTES INTO CRUISE NR 3 ENGINE SHOWED N1 EXCEEDANCE UP TO 209.3 PERCENT BROUGHT NR 3 THROTTLE TO IDLE. INDICATIONS CAME BACK TO NORMAL, FIVE MINUTES LATER NR 3 N1 JUMPED AROUND THEN BACK TO NORMAL FOR REST OF FLIGHT. TROUBLESHOT IAW FIM MANUAL 77-11-SDR FDEA201108173302Controller · malfunctionedDURING CRUISE FL350, RECEIVED A MASTER CAUTION LEVEL 1 ALERT FOR HYD PUMPS. ALL 3 LEFT EDPS WERE IN THE OFF POSITION (NO PRESSURE AUTO MODE ). SELECTED HYD CONTROL SYS FROM AUTO MODE TO MANUALLY MODE AND ALL 3 LT PUMPS TURNED ON AND PRODUCED PRESSURE. SHUTSDR FDEA201108153279Lamp · inoperativeENTRY DOOR LIGHTED EMERGENCY EXIT SIGN HAS SEVERAL INOPERATIVE BULBS, DIM ILLUMINATION. RELAMPED THE LT EXIT LIGHT'S IAW SMP CHECKED OK.SDR FDEA201108123252Mec · failedON DECENT, NR 3 ENGINE BECAME UNCONTROLLABLE, A/T OFF OR A/T ON, ENGINE SURGE +/- 20 PERCENT ALL INDICATION. ENGINE SHUTDOWN PERFORMED AND WINDMILLED APPROX 20 MINUTES. R & R NR 3 ENGINE CIT SENSOR, REF AMM 73-20-02-2. INSTALLED NR 3 ENGINE MEC AND FUEL PUSDR FDEA201108113201Engine · stalledON CLIMBOUT, PASSING FL 290 FELT 2 FIRM JOLTS WITH YAW TO THE LT ENG INDICATIONS NORMAL IN COCKPIT. FELT LIKE COMPRESSOR STALL ON NR 1 ENG. ENG RPM'S AT THE TIME WERE ATS CET 101 PERCENT. REMOVED AND REPLACED NR 3 ENG. LEAK AND OPS CHECKED GOOD. ACFT OKSDR FDEA201108083140Floor Support · corrodedCTR CARGO FLOOR SUPPORT AT STA 1521 Y "0" HAS CORROSION. REMOVED ROLLER TRAY FOR ACCESS. REMOVED CORROSION. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-01, FIG 1B. FABRICATED REPAIR ANGLES AND FILLER. INSTALLED REPAIR PARTS IAW SRM 53-00-1 FIG 7, SHEET 3, INSTASDR FDEA201108043102Engine · overtempENG 3 EXCEEDENCE ON TAKEOFF. REJECTED TAKEOFF AT 93 KTS NR 3 N2 SHOWED 101.0 AMM 72-00-00-6-0, NR 3 ENGINE N2 OVERSPEED, 101.0, REQUIRES BORESCOPE OF CORE COMPRESSOR & HPT WITHIN 10 CYCLES. AMM 72-00-00-6-0. DEBRIEFED CREW NO HIGH BRAKE TEMP DURING REJECT OSDR FDEA201107212885Pitot Line · damagedON TAKEOFF, AIRSPEED STAGNATED THEN BECAME ERRATIC. COMPLIED WITH QRH. RETURNED TO FIELD. R & R 3 PITOT TUBES IAW MM 34-11-02-2. PERFORMED A LOW RANGE LEAK TEST ON PITOT AND STATIC SYS. ALL TESTS NORMAL. NO LEAKS IN SYS OR LEAK DOWN. ALL PITOT LINES SDR FDEA201107202850Engine · failedNR3 ENGINE FAILURE ON TAKEOFF. GOOD N1 BUT AMBER X ON N2. R & R NR 3 ENGINE.SDR FDEA201106212366Throttle · bindingAFTER LEVEL OFF, NR 1 THROTTLE STUCK AT CLIMB POWER. DISCONNECTED AUTO THROTTLES, NO HELP. AFTER 10 MIN, THROTTLE CAME FREE. CONTINUED WITH AUTO THROTTLE DISCONNECTED. THROTTLES WORKED NORMALLY THRU ENTIRE FLT. INSPECTED PUSH-PULL CABLE & PUSH-PULL CABLESDR FDEA201106152255Engine · malfunctionedRTO BELOW 80 KNOTS FOR LVL 1 ENG 2 EXCEEDANCE ALERT. MAX N2 101.1. PREVIEWED QRH FOR LVL1 AND RTO. ADVISED MX. RETURNED TO GATE. COMPLIED WITH VISUAL INSP OF NR 2 ENG EXHAUST AREA IAW AMM 72-00-00-6, NO DAMAGE NOTED. INSPECTED WHEELS TIRES BRAKES AND MLG DSDR FDEA201106062129Support · corrodedCENTER CARGO AFT WALL, CORROSION ON VERTICAL SUPPORT BEAM JUST RIGHT OF CTR AND JUST ABOVE FLOOR LINE. INSTALLED NEW VERTICAL SUPPORT BEAM AT STA 1781 IAW DWG AFA3225 AND SRM 51-35-01, VOL II.SDR FDEA201105171860Engine · damagedAFTER T/O AT 1500 AGL, EXPERIENCED HEAD WINDSHEAR ALERT AND DURING ESCAPE MANUEVER NR 3 N2 EXCEEDED LIMITS AT MAX OF 101.2 FLAPS WERE 14.2 DEG GEAR WAS UP. COMPLIED WITH INSPECTION OF NR 3 ENGINE INLET AND EXHAUST AREAS REF AMM 72-00-00-6-1. INTERRIGATED VISDR FDEA201105041747Fuel Control · failedAT FL360, ENCOUNTERED TURB ACFT WAS SLOWING TO .80M FROM .83 NR 2 ENG FLAMED OUT W/ AUTO RESTART FROM IGNITION OVERIDE ON , EAI ON OAT -58C. MIGHT POSSIBLY HAVE HAPPENED ON PREVIOUS FLIGHT AT TOP OF DECENT. CHECKED ACFT FUEL TANK SUMPS FOR WATER IAW AMM CH SDR FDEA201104261632Connector · corrodedWE RECEIVED AN ENG 2 OIL FILTER, LEVEL 2 ALERT. FOLLOWING QRH ENG 2 WAS SHUTDOWN. REMOVED AND REPLACED THE SCAVANGE AND MAIN LUBE OIL FILTERS, NO CONTAMINATION WAS FOUND REF. AMM MD10-79-20-02 AND 79-20-01, LEAK CHECK WAS GOOD. COMPLETED A 5 MINUTES GROUSDR FDEA201103311255Warning Light · illuminatedCLIMBING THRU 13,000' GOT LVL 3" BLD AIR 1 TEMP HI", COMPLIED WITH QRH. PERFORMED RTS ON ALL 3 AIU'S, ALL TESTS PASSED. PERFORMED RTS ON PNEUMATIC SYS CONTROLLER NR 1. INSPECTED NR 1 ENGINE BLEED CONTROL VALVE SENSE LINES AND CONNECTORS, NO DEFECTS NOTED. SDR FDEA201103311265Oil System · leakingDURING CRUISE, NR 2 ENG OIL QTY STARTED DROPPING 1 GAL EVERY 8 MIN. WHEN QUANTITY HIT 3 AND AMBER, WE ALSO GOT AN ENG 2 OIL PRESSURE LOW ALERT AND IT STAYED ON WITH ENG THROTTLE AT IDLE. SHUTDOWN ENGINE IAW QRH. CREW VERBAL ON DEBRIEF: ENGINE WAS ALREADYSDR FDEA201103221110Control Cable · bindingNR 2 THROTTLE JAMMED AT CRUISE POWER SETTING. UNABLE TO CONTROL THROTTLE POSITION DURING DESCENT AND APPROACH. SHUTDOWN NR 2 ENG IAW QRH. AFTER LANDING DURING TAXI-IN, WAS ABLE TO MOVE THROTTLE FREELY. ENG WAS SHUTDOWN FOR LAST 10 MINS OF FLIGHT. DEPARTSDR FDEA201103171056Bulb · failedDURING CLIMB AT FL295, CLIMBING TO FL310 REC'D LEVEL II ALERT " ENG NR 1 OIL TEMP HIGH "TEMP INDICATED 203 DEG INITIALLY. AFTER SHUTDOWN TEMP CLIMBED TO 237 DEG. DURING DESCENT TEMP AVERAGED APPROX 160-165 DEG, EMERGENCY DECLARED. NO FUEL DUMPED. GENERALSDR FDEA201103030834Web · crackedCTR WHEEL RT SIDE WALL, BETWEEN THE SECOND AND THIRD STATIONS AFT OF THE FWD BULKHEAD APPROX STA 1381 TO 1401. THERE ARE 9 CRACKS IN A DOUBLER. REMOVED AND REPLACED BARREL KEEL SPLICE DOUBLER. REF SRM 51-33-01 VOL 2 AND E.A. 8-5310-149330 AND E.A. 8-5310-148SDR FDEA201102180622Tee Fitting · corrodedRT WHEEL WELL SLANT PANEL OTBD VERTICAL TEE IS CORRODED AT LWR CORNER. REMOVED CORROSION. REF EA 8-5340-148481.SDR FDEA201102180623Angle · corrodedRT MAIN WHEEL WELL REAR SPAR CAP ANGLE (APB7080-2) HAS 2 CRACKS (2' CRACK INDICATION AFTER BLEND OUT) REMOVED AND INSTALLED REPAIR ANGLE. SRM 53-40-00, FIG 11.SDR FDEA201102150566Engine · vibrationSHUTDOWN ENG NR 1 INFLIGHT FOR UNUSUAL VIBRATIONS. VIBES START AT 91 PERCENT - AND VERY NOTICABLE ABOVE 94 PERCENT - LIGHT TO MEDIUM "SHUDDER" RAPTED VIBRATION. REMOVED NR 1 ENGINE SPINNER ASSY & FIRST STAGE FAN ROTOR BLADES IAW MM 72-21-00-4. LUBED IAW AMMSDR FDEA201102040475Frame · crackedCAC, FWD PRESSURE BULKHEAD RT SIDE MAIN FRAME CRACKED ALLTHE WAY THROUGH AT BS 1157 BETWEEN LONGERON 27R AND 28R. REMOVED DAMAGED PARTS, FABRICATED NEW PARTS AND TREATED PARTS IN ACCORDANCE WITH EA 8-5310-142572. INSTALLED PARTS AND SEALED AS REQUIRED PER SSDR FDEA201102020451Push-Pull Cable · inoperativeABOUT 1 HR FROM DESTINATION, AFTER 2.5 HRS INTO FLIGHT, ENG 2 THROTTLE WOULD NOT KEEP UP WITH 1 OR 3, HAD 7-8 ENG FAILS WHICH WE CLEARED. DECENDING INTO DESTINATION, MANUAL THROTTLES. TRIED TURNING ATS OFF 2-3 TIMES AND RE-ENGAGING, THROTTLE FROZEN AT 83 PERSDR FDEA201101170194Fuel Cell · corrodedMAIN DECK - OVERWING TANK UPPER SURFACE AT STATION 1227, X= -80 TO X= -101 FOUND SEVERAL AREAS OF CORROSION. CORROSION REPAIRED IAW EA NR1-5710-143826, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 111.SDR FDEA201101090090Longeron · corrodedLOWER CTR CARGO COMPARTMENT - BILGE AREA STA 5-123 LONGERON 44R FOUND WITH CORROSION. CARRIED OUT REPAIR AS PER SRM 53-00-05 REPAIR 1 FIGURE 202 REVISION 45 AND E.A. 1-5310-143504, CLASSIFIED AS MAJOR REPAIR AS PER GMM 6-2-100 REVISION 111.SDR FDEA201012314788Bottle · dischargedON PREFLIGHT F/O FOUND L1 DOOR EMERGENCY BOTTLE DISCHARGED. RESET L1 DOOR EMERGENCY ASSIST SYS AND RECHARGED L1 DOOR ACCUMULATOR IAW MM 52-10-01-2-0. OP'S CHECK NORMAL.SDR FDEA201012294761Control Unit · failedDURING CRUISE FL360 F/O'S MCDU BLANKED OUT FOR APPROX 1 MINUTE THEN CAME BACK ON. THEN WE SMELLED ELECTRICAL FIRE/FUMES. PULLED F/O, MULTI-FUNCTION DISPLAY UNIT NR 2 CB RT EMERGENCY AC BUSS, ODOR/FUMES WENT AWAY. R & R THE MULTIFUNCTION CONTROL UNIT IAW SDR FDEA201012284760Engine · fireHAD NO START ON ENG NR 3 RAN QRH ABNORMAL START CHECKLIST. GROUND CREW INFORMED FLT CREW OF TAIL FIRE. AFTER MOTORING ENGINE, STILL HAD FIRE IN ENG NR 3, BLEW FORE BOTTLE INTO NR 3 AND RAN ENGINE FIRE CHECK LIST. INSPECTED NR 3 ENGINE COWLS, PYLON, AND ENGSDR FDEA201012274755Switch · no testEMERGENCY POWER TEST FAIL DURING PRE-FLIGHT. RE-SELECTED BATTERY SWITCH AND FUEL SHUTOFF LEVERS EPT PASSED IAW-FIM-24-24. ACFT OK FOR SERVICE. RE-SELECTED BATTERY SWITCH AND FUEL SHUTOFF LEVERS EPT PASSED IAW FIM-24-24. ACFT OK FOR SERVICE. (CLOSED)SDR FDEA201012264753Pressure Switch · inoperativeON DESCENT TURNED ON ENG - WING ANTI-ICE RECEIVED "A WING A-ICE L DISAG ALERT SHORTLY AFTER RECEIVED AN AIR MANF 1 FAIL" COMPLIED WITH QRH AND DIVERTED, WITHOUT INCIDENT. R & R LT MANIFOLD FAILURE DETECTION PRESSURE SWITCH IAW MM 36-23-03-4. ALSO REPLACED NRSDR FDEA201012204728Switch · failedNR 2 ENG OIL FILTER LEVEL II ALERT. INFLT SHUT DOWN AS PER FLT CREW WITH LEVEL II ALERT, ENG HAD NORMAL OIL PRESSURE. INSPECTED FILTER ELEMENT FOR CLOGGING, ELEMENT FOUND CLEAN AND NOT CLOGGED. INSTALLED NEW FILTER ELEMENT AS PER MM 79, RAN ENG AS PER JRHSDR FDEA201012184715Cover · missingDOOR DISARM LIGHT BULB COVER IS MISSING ON LT MAIN CABIN DOOR. INSTALLED NEW DISARM INDICATOR COVER, REF AMM 52-11-00. OK FOR SERVICE. FINAL CLOSED.SDR FDEA201012124645Fire Detector · false activationAFTER STARTING ALL 3 ENGINES AND BLOCKING OUT, POWER WAS APPLIED FOR TAXI NR 1 ENGINE INDICATED MOMENTARY FIRE. ENGINE SHUTDOWN AND ALL INDICATIONS RETURNS TO NORMAL. OPS CHECK NR 1 ENG AT GATE CHECKED GOOD, NR 1 B-LOOP, OPS CHECK NORMAL IAW MEL-26-11-01-01SDR FDEA201012054600Terminal · brokenR1 DOOR SLIDE REMOTE PUSH TO TEST LIGHT/INDICATOR IS INTERMITTENTLY INOP. RELEASED FOR SERVICE IAW MEL: 25-61-01 CATEGORY: C EXPIRATION: 15DEC10 MEL 25-61-01:RT EVAC SLIDE REMOTE PRESS INDICATOR INOP IAW MEL 25-61-01, VERIFY AND RECORD IN THE AML, EVAC SLIDSDR FDEA201012044578Controller · failedAT CRUISE FL330, AIR MANF 2 FAIL. COMPLIED WITH QRH AND DIVERTED. RELEASED FOR SERVICE IAW MEL: 36-23-01-02, CATEGORY: C EXPIRATION: 13DEC10 "MEL 36-23-01-02: NR 2 MANIFOLD FAIL DETECTION LOOP NR2 INOP. NO HISTORY 99 DAYS ON SYS 2 MAN FAIL. NO CURRENT FASDR FDEA201012044580Lamp · inoperativeR1 DOOR AFT EMERGENCY LIGHT INOPERATIVE. RELAMPED IAW AMM 33-52-04-2-0. ALL OPS CHECKS NORMAL.
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