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 aircraft_model_key = '72725' 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 aircraft_model_key = '72725' 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 EISA98145Fire Loop · malfunctionedNR 3 ENGINE FIRE WARNING TEST IMPROPERLY. GENERATED FROM MAINTENANCE REPORT. REPAIRED WIRE TO NR 3 ENGINE FIRE LOOP. OPS CHECK GOOD PER MM 26-00. (M)SDR EISA98143Smoke Detector · malfunctionedMAIN CARGO SMOKE DETECTOR INDICATOR 'CARGO SMOKE' ILLUMINATED WILL NOT EXTINGUISH. WILL NOT TEST. REPLACED NR 3 SMOKE DETECTOR, SYSTEM CHECKED NORMAL PER MM 26-10-00, REMOVED PLACARD. (M)SDR EISA98128Smoke Detector · damagedCARGO SMOKE ILLUMINATED 4 TIMES, VERIFIED NO SMOKE. GENERATED FROM PILOT REPORT. REMOVED ALL SMOKE DETECTORS, BLEW OUT ALL LINES WITH NITROGEN. REPLACED 3 EACH DAMAGED FLEX LINES, REINSTALLED ALL DETECTORS. NO DEECTS NOTED. UNABLE TO DUPLICATE. IAW 26-10SDR EISA98120Smoke Detector · contaminatedON LAST LEG, CARGO SMOKE LIGHT ILLUMINATED HALF WAY THROUGH FLIGHT. NO SMOKE FOUND IN CARGO COMPARTMENT. GENERATED FROM PILOT REPORT. PURGED ALL SMOKE DETECTOR HOSES WITH NITROGEN. SMOKE DETECTOR SYSTEM CHECKS NORMAL ON GROUND IAW AERONAUTICAL MANUAL. (X)SDR 98FDEA00384Floorbeam · corrodedNR 0914, UPPER LOBE BS 680, CORROSION ON FLOORBEAM RBL 2 - RBL 13. REMOVED CORROSION REPAIRED PER 53-10-07 IN SRM.SDR 98FDEA00383Floorbeam · corrodedNR 0866, UPPER LOBE, BS 620, LBL 63 - RBL 8, FLOORBEAM CORRODED. REMOVED CORROSION PERFORMED FLOORBEAM REPAIR FROM RBL 9- LBL 39, BS 620, PER SRM 53-10-8 FIG 3.SDR EISA98121Detector · malfunctionedCARGO SMOKE LIGHT ILLUMINATED IN-FLIGHT. SYSTEM WILL NOT TEST IN-FLIGHT. TEST OK ON GROUND. GENERATED FROM PILOT REPORT. REMOVED AND REPLACED NR 2 CARGO SMOKE DETECTOR IAW AERONAUTICAL MM. CHECKS GOOD. (X)SDR EISA98116Smoke Detector · malfunctionedCARGO SMOKE LIGHT ON IN FLIGHT ILLUMINATED DURNIG CLIMB. WILL NOT TEST IN FLIGHT, EXTINGUISHED DURING DESCENT BELOW 10,000. GENERATED FROM PILOT REPORT. COULD NOT DUPLICATE MALFUNCTION. CARGO SMOKE DETECTORS. OPS CHECK OK ON GROUND PER AERONAUTICAL MANUALSDR EISA98113Smoke Detectors · malfunctionedCARGO SMOKE DETECTOR LIGHT COMES ON IN CRUISE. NO SMOKE DETECTED. EXTINGUISHES ON GROUND AFTER LANDING. GENERATED FROM PILOT REPORT. PURGED SMOKE DETECTORS TUBES PER MM 26-00. GROUND TEST NORMAL. (M)SDR EISA98110Smoke Detector · malfunctionedCARGO SMOKE LIGHT CAME ON IN DESCENT TO BRU, RECYCLED SWITCH NO FURTHER PROBLEMS. GENERATED FROM PILOT REPORT. PERFORMED OPERATIONAL CHECK OF MAIN CARGO SMOKE DETECTOR SYSTEM, PER AERONAUTICAL MANUAL, NO DEFECT NOTED. (M)SDR EISA98109Smoke Detector · malfunctionedCARGO SMOKE RED LIGHT ILLUMINATED ON DESCENT INTO CPH, NO SMOKE SEEN AFTER LANDING LIGHT WENT OFF. GENERATED FROM PILOT REPORT. RAN APU TO HEAT UP AND CHECK OUT SMOKE DETECTORS. OPS CHECK GOOD, MM 26-00. NO DEFECTS NOTED. (M)SDR EISA98111Detector · malfunctionedRED CARGO SMOKE LIGHT CAME ON IN FLIGHT. VISUAL INSPECTION NO SMOKE DETECTED. ON TAXI, IN RIGHT PACK SWITCH TURNED OFF AND LIGHT EXTINGUISHED. GENERATED FROM PILOT REPORT. OPS CHECKS GOOD ON GROUND IAW MM CHAPTER26-00. (M)SDR CA980521005Bulb · failed(CAN) WHEN LANDING GEAR SELECTED DOWN, RT MLG DOWN INDICATOR FAILED TO LIGHT. MISSED APPROACH PROCEDURE CARRIED OUT. INDICATOR RELAMPED AND SYSTEM INDICATION TESTED NORMAL. NORMAL LANDING CARRIED OUT.SDR CA980818011Nut · loose(CAN) ON TOP OF DESCENT, CREW ATTEMPTED TO RETARD THE THRUST LEVERS TOWARDS FLIGHT IDLE. THE NR 2 ENGINE CONTROL WOULD NOT MOVE. THE ENGINE WAS SHUTDOWN. POST-FLIGHT INSPECTION FOUND THE NR 2 ENGINE CROSS SHAFT RETAINING NUT HAD BACKED OFF AND RESTRICTED THSDR EISA98104Smoke Detector · malfunctionedFROM TAMPERE (TMP) TO BRUSSELS (BRU) - CARGO SMOKE LIGHT ILLUMINATED IN NORMAL FLIGHT CONDITIONS IN CARGO HOLD. UNEVENTFUL LANDING. GENERATED FROM PILOT REPORT. PURGED SMOKE DETECTOR OF MOISTURE, ALL SMOKE DETECTORS CHECKED GOOD PER AERONAUTICAL MANUAL. (XSDR EISA98103Smoke Detector · failedCARGO SMOKE LIGHT ILLUMINATED DURING CRUISE FROM TMP TO BRU, VISUALLY CHECKED CARGO COMPT FOUND NORMAL. RESET SWITCH. CONDITION REAPPEARED, LIGHT WENT OUT ON DESCENT UNEVENTFUL LANDING AT BRU. GENERATED FROM PILOT REPORT. REMOVED AND REPLACED NR 1 SMOKE DETSDR 98FDEA00252Engine · failedNR 2 ENGINE OIL PRESSURE EXCEEDED RED RADIAL DURING DEPARTURE AT ALL POWER SETTINGS ABOVE IDLE. OIL TEMPERATURE 118C, PRESS 60 PSI PRESS 52 PSI AT IDLE. FOUND BREATHER PRESSURE AT 5.6 PSI OUT OF LIMITS. REMOVED AND REPLACED NR 2 ENGINE FOR HIGH BREATHER PRESDR 98FDEA00217Stall Computer · failedON ROTATION, STICK SHAKER ENABLE AND REMAINED ON THROUGHOUT FLIGHT. RETURNED TO BASE. TROUBLESHOT SYSTEM FOUND STALL COMPUTER FAULTED. REMOVED AND REPLACED STALL COMPUTER SYSTEM, OPERATIONAL CHECKS GOOD.SDR 98FDEA00170Manifold · rupturedNR 2 ENGINE FIRE LIGHT IN FLIGHT APPROXIMATELY 11,000 FEET AFTER TAKEOFF. CHECKLIST FOLLOWED AND FIRE LIGHT EXTINGUISHED WHEN THROTTLE RETARDED TO IDLE. ENGINE INDICATIONS WERE NORMAL. REMOVED AND REPLACED FUEL HEAT MANIFOLD, LEAK CHECK OK.SDR 98FDEA00166Oil Temp Bulb · failedSHUT DOWN NR 3, HIGH OIL TEMPERATURE, PREFLIGHT INDICATION LOW OIL QUANTITY ON NR 3, 1.7 GALLON. SERVICED TO 2.2 AFTER MOTORING. ON TAKEOFF NOTICED QUANTITY 4.2, IN FLIGHT TEMPERATURE WENT TO EDGE OF RED BAND, SHUT DOWN AS TEMPERATURE CLIMBED INTO RED BAND. SDR 98FDEA00138Skin · damagedWORKING FASTENERS IN RT SIDE OF FUSELAGE OF NR 2 ENGINE AT BS 1342 BETWEEN RAIN GUTTER AND ACCESS PANEL. *S/D* REMOVED DAMAGED SECTION OF SKIN BS 1328 TO 1342, STR 20 RT TO STR 27 RT PER FED-EX SRM 53-30-3 FIG 15A. FABRICATED REPAIR PARTS AND INSTALLED REPASDR 98FDEA00147Outflow Valve · failedAIRCRAFT WOULD NOT PRESSURE AFTER TAKEOFF WITH TWO PACKS ON AND OUTFLOW VALVE CLOSED. COMPLETED UNSCHEDULED CABIN PRESSURE CHANGE CHECK LIST WITH NEGATIVE RESULTS. PERFORMED PRESSURIZATION TEST PER MAINTENANCE MANUAL 21-30-0 PAGE 501 TO 503. FOUND LEFT OUTFSDR 98FDEA00094Web · corrodedNR 0400 006 WHILE WORKING NR0259, FOUND CORROSION ON FLOOR WEB BS 294-328, RBL 15-30, WL 168. FOUND CORROSION ON FLOOR WEB BS 294-328, RBL 15-30, WL 168 TO BE OUT OF LIMITS IAW FED-EX SRM 53-10-1. FABRICATED NEW WEB BS 294 TO 350, RBL 15-30, WL 168 IAW FED-ESDR 98FDEA00093Web · corrodedWHILE WORKING NR0159 FOUND CORROSION BETWEEN THE NOSE WHEEL WELL HORIZONTAL WEB AND BONDED DOUBLER AT BS 306, WL 182, LBL 14 TO RBL 14. *S/D* FOUND CORROSION ON WEB BS 306, WL 182, LBL 14 TO RBL 14 TO BE OUT OF LIMITS IAW FED-EX SRM 53-10-1. REPAIRED WEB BYSDR 98FDEA00090Actuator · failedNR 2 LED WOULD NOT RETRACT AFTER T/O. ACCOMPLISHED RED TABS. REMOVED AND REPLACED NR 2 SLAT ACT THRU STEP G AS PER M/M 27-81-32 PG 408.80531. COMPLETED INSTALLATION, CONNECTED ROD END AND INSTALLED PANELS, LEAK AND OPS CK OK.SDR 98FDEA00088Chord · corrodedNR 0401 004 WHILE WORKING NR 0259 FOUND CORROSION BS 300, WL 168, RBL 16 ON NOSE WHEEL WELL CHORD. REMOVED AND REPLACED NOSE WHEEL WELL CHORD BS 300, WL 168, RBL 16 IAW FED-EX DRAWING 65-18415 AND FED-EX SRM 51-30-2.SDR 98FDEA00087Chord · corrodedCORROSION (C53- 224-03) BS 351.2, WL 168, LBL 16 ON NOSE WHEEL WELL CHORD. *S/D* CORROSION BS 351.2, WL 168, LBL 16 ON NOSE WHEEL WELL CHORD FOUND TO BE OUT OF LIMITS PER FED-EX SRM 53-10-1. REMOVED LT MED CHORD BS 294.5 -0 350 AND REPLACED WITH NEW (P/N 65SDR 98FDEA00084Fitting · corrodedNR 0145 001, CORROSION (C53-224-04) ON BRACKET AT BS 1180, RBL 66, WL 208. CORROSION ON BRACKET AT BS 1180, RBL 66, WL 208 FOUND TO BE OUT OF LIMITS. REMOVED .060 FROM .080 ORIGINAL THICKNESS MATERIAL AS PER FED-EX SRM 53-10-1. REMOVED AND REPLACED BRACKET SDR 98FDEA00082Frame · corrodedNR 0265 002, CORROSION (C53-224-03(1 AND 2) ON FRAME AT BS 425, LBL 11 - RBL 11, WL 150 (FWD OF E-BAY DOOR). FOUND FRAME TO BE CORRODED BEYOND LIMITS PER FED-EX SRM 53-10-1. REMOVED AND REPLACED BS 425 FRAME LBL 11 - RBL 13, WL 150 PER BOEING DRAWING 65-1635SDR DHL98708001Connector · water contamON APPROACH AFTER GEAR EXTENSION, NOTED NO TAIL SKID LIGHT. CYCLED AT 500 FEET AGL, GOT TOO LOW GEAR ON GPWS. EXECUTED GO-AROUND. EXECUTED PROCEDURES AND CYCLED GEAR, DURING GEAR EXTENSION, TAIL SKID CAME DOWN AND LANDED NORMALLY. INSP AND TEST TAIL SKIDSDR 98FDEA00016Wire · looseWHEN PASSING THROUGH FLIGHT LEVEL 270, MAIN CARGO DOOR LIGHT ILLUMINATED WITH NO LOSS OF PRESSURIZATION. DESCENDED TO 10,000, DEPRESSURIZED AIRCRAFT. LIGHT STAYED ON UNTIL LANDED. REPRESSURIZED AFTER LANDING, NO LIGHT ON. FOUND LOOSE WIRE ON NORMALLY CLOSESDR EISA97261Smoke Light · illuminatedCARGO SMOKE WARNING LIGHT, ON CLEARING CRUISE FLIGHT. TESTED SYSTEM ON GROUND, COULD NOT DUPLICATE. SYSTEM TESTED OK IAW MM 26-00. (X)SDR 97FDEA00810Switch · malfunctionMAIN CARGO DOOR LIGHT CAME ON SHORTLY AFTER TAKEOFF. AIRCRAFT RELEASED FOR SERVICE PER MEL/CDL: 52-4A, MCD VERIFIED CLOSED. REMOVED AND REPLACED CONTROL SWITCH ARM/DISARM SWITCH. REMOVED AND REPLACED DOOR UNLOCK LT ON MANUAL HAND PUMP PANEL. C/B CARGO DOORSDR 7FDEA00791Shear Tie · crackedNR 0427 013 CORROSION (C53-113-01(2)) ON THE SHEAR TIE AT BS 1130 OUTBOARD OF STRINGER 29L. *** S/D *** REMOVED SHEAR TIE. FABRICATED NEW SHEAR TIE. INSTALLED PER FED-EX SRM 51-30-2. ALODINED, PRIMED AND PAINTED PER FED-EX SRM 51-10-2 AND PER FEDSDR 97FDEA00731Duct · leakedPASSING FLT LEVEL 270, THE A/C STARTED LOSING PRESSURE AT 1,500 FT PER MIN. TRIED CLOSING THE CARGO HEAT OUTFLOW, SWITCHING BLEEDS, RECYCLING THE PACK AND BLD VALVES, NO HELP. ABLE TO HOLD 10,000 CABIN AT 15,000 FT. SUSPECT THE NR 1 PACK INOPERTIVE. INSPECSDR 97FDEA00721Duct · cracked97-0199 ENGINE NR 2 FIRE LIFHT ILLUMINATED ON CLIMB-OUT WHILE IN CLIMB POWER. LIGHT WENT OUT WHEN THROTTLE WAS RETARDED TO IDLE. FIRE CIRCUIT TESTED GOOD. FOUND ANTI-ICE DUCT CRACKED IN HALF AT 6TH STAGE SADDLE DUCT. REPLACED DUCT OPERATIONAL AND LEAK CHESDR EISA97207Smoke Detector · inoperativeNR 1 SMOKE DETECTOR WILL NOT TEST. (FOUND ON PRE-FLIGHT). REMOVED AND REPLACED NR 1 SMOKE DETECTOR. CHECKS OK IAW MM. (X)SDR DHL97708002Engine · malfunctionedNR 1 ENGINE SLOW TO ACCELERATE. PERFORMED ENGINE RUN-UP, WITHIN LIMITS PER M/M.SDR 97FDEA00641Light · defectiveFWD ENTRY EMERGENCY EXIT LIGHT ILLUMINATED WITH SWITCH POSITION IN OFF AND PWR IS REMOVED FROM A/C. *S/D* REPLACED EMERGENCY EXIT LIGHT ASSEMBLY PER FED-EX M/M 33-50-101.SDR 97FDEA00628Flap · delaminatedRT WING O/B MIDFLAP HAS TWO AREAS OF DELAMINATION ON UPPER SURFACE OF T/E WEDGE. * S/D* REMOVED AREAS OF DELAMINATION FROM RT WING O/B MIDFLAP AND REPAIRED IAW FED-EX SRM 51-40-06.SDR 97FDEA00632Pump · leakedHYDRAULIC SYSTEM-B QUANTITY WENT TO ZERO IN CRUISE FLIGHT. CHANGED NR 2 B-PUMP INBOARD PUMP AND CHANGED CASE DRAIN FILTER, LEAK CHECKS OK.SDR 97FDEA00620Flap · delaminatedRT WING INBD FOREFLAP DELAMINATED 96 FROM INBD END. *S/D* REMOVED 8 BY 8 AREA OF DELAMINATION. REPAIRED PER FED-EX SRM 51-40-06.SDR 97FDEA00602Skin · corrodedCORROSION (C53-224-05) ON UPPER FUEL CELL SKIN BS 850 TO 865, LBL 46 TO 67, WL 190. CORROSION APPEARS TO RUN UNDER 850 STUB BEAM AND 70.5 AND CHORD. * S/D* REMOVED CORROSION FOUND TO BE WITHIN LIMITS. FLAP PEENED AREA. ALODINED AND PRIMED AREA.SDR 97FDEA00600Pressurization · malfunctionedAIRCRAFT CABIN WOULD NOT PRESSURIZE ON CLIMBOUT, AUTO AND MANUAL NO HELP. CHECKED ALL DOORS ON AIRCRAFT FOR SECURITY, ALL CLOSED. PRESSURIZED AIRCRAFT 4 TIMES AFTER CLEANING OUTFLOW VALVES, OPERATIONAL CHECKS OK AND PRESSURIZES OK AS PER MAINTENANCE MANUAL 2SDR DHL97708001Clamp · looseON SHORT FINAL GPWS SOUNDED TOO LOW GEAR WITH ALL OTHER INDICATIONS NORMAL. MADE GO-AROUND AND RECYCLED GEAR, NO FAULT ON 2ND APPROACH AND LANDING. FOUND LT LOCK OUT GRND SPOILER CLAMP LOOSE, TIGHTENED.SDR EISA97173Web · crackedDURING B-SERVICE AND THE ACCOMPLISHMENT OF CPCP CARD NR C53-224-01, FOUND CRACK AT FLOOR WEB, FS 1050 - FS 1070. TT: 73,279:23 HOURS. TC: 55,830. (X)SDR EISA97172Cross Rib · crackedDURING B-SERVICE AND THE ACCOMPLISHMENT OF CPCP CARD NR C53-224-01, FOUND CROSS-RIB CRACKED AT FS 1110 BETWEEN SEAT TRACKS. FABRICATED AND INSTALLED REPAIR SRM 51-30-02. TT: 73,279:23 HOURS. TC: 55,830. (X)SDR EISA97171Angle · corrodedDURING B-SERVICE AND THE ACCOMPLISHMENT OF CPCP CARD NR C53-111-01, FOUND CORROSION ON ANGLE IN LOWER LOBE, FS 196.5. REMOVED ANGLE, FABRICATED AND INSTALLED NEW ANGLE PER SRM 51-10-1. TT: 73,279:23 HOURS. TC: 55,830. (X)SDR EISA97170Support · crackedDURING B-SERVICE AND THE ACCOMPLISHMENT OF CPCP CARD NR C53-113-01, FOUND FLOOR SUPPORT CRACK AT FS 540, STR 27. FABRICATED AND INSTALLED REPAIR DOUBLER PER SRM 53-10-8. TT: 73,279:23 HOURS. TC: 55,830. (X)SDR EISA97169Floor Beam · crackedDURING B-SERVICE AND THE ACCOMPLISHMENT OF CPCP CARD NR 53-113-01, FOUND CRACK IN FLOOR SUPPORT AT FS 600 - FS 620, STR 27R, FORWARD CARGO PIT AREA. FABRICATED AND INSTALLED REPAIR DOUBLER PER SRM 53-10-8. TT: 73,279:23 HOURS. TC: 55,830. (X)
Back to Boeing 727-25