N641AE
Service difficulty reports · 218
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. 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 n_number = 'N641AE' AND registry_match = 'registration' 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 n_number = 'N641AE' AND registry_match = 'registration' 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 HNAA2018021900037Anti-Ice Valve · failedNR 2 ENGINE ANTI ICE FAILED MESSAGE WITH OPEN INSCRIPTION NOT ILLUMINATED, FOLLOWED BY ICE CONDITION ANTI ICE MESSAGES. FOLLOWED FIM TASK 30-21-00-810-A. ANTI ICE VALVE FAILED CMC MESSAGE STEPS 1, 7, 15. R & R THE NR 2 ENGINE ANTI ICE VALVE IAW 30-21-00. SDR HNAA2017071200242Connector · dirtyCEILING EXIT SIGN BETWEEN ROWS 11 & 12 IS NOT ILLUMINATING ON THE AFT SIDE. UPON FURTHER INSPECTION, FOUND LOOSE ELECTRICAL CONNECTORS ON EXIT SIGN. CLEANED AND CONNECTORS. OPS CHECKED GOOD, OK FOR SERVICE.SDR HNAA2017061600209Anti-Ice Valve · malfunctionedNR 2 ENGINE ANTI-ICE MESSAGE APPEARED ON EICAS, CREW RAN THROUGH QRH PROCEDURE MESSAGE STAYED AND DIDN`T GO OUT. VALVE SECURED OPEN IAW AMM 30-21-01-040-801-A.. OPERATIONAL PROCEDURE IAW AMM TASK 30-21-01-040-801-A.SDR HNAA2017020300035Warning Message · illuminatedSPOILER FAIL EICAS CAUTION MESSAGE DURING TAXI OUT. SPOILER INDICATED CLOSED. MAINTENANCE REPORTS GROUND SPOILER ENG CHT FAULT MESSAGE ON CMC.SDR HNAA2017011800023Anti-Ice System · malfunctionedNR 2 ENGINE ANTI ICE FAILED AT 18,000 FEET. WOULD NOT CLEAR WITH ABNORMAL PROCEDURES. ENGINE ANTI-ICE VALVE DEACTIVATED. ANTI-ICE VALVE OPS CHECKED.SDR HNAA2017011300016Indication Sys · malfunctionedDURING FLIGHT, THE NR 2 ENGINE ANTI ICE INLET OPEN ENSCRIPTION EXTINGUISHED. COMPLIED WITH TASK 30-21-00-700804-A. OPS CHECKED GOOD. VALVE CONFIRMED OPEN WITH TEST. FLIGHT DECK INDICATION ONLY.SDR HNAA2016100500309Bulb · inoperativeRIGHT EXTERNAL OVER-WING EMERGENCY LIGHT IS INOPERATIVE. REMOVED AND REPLACED THE BULB IAW MM 33-50-10. OPS CHECKED GOOD.SDR HNAA2016070500208Hydraulic System · lowIN FLIGHT, HYD 1 LOW QTY MESSAGE APPEARED ON EICAS. CREW FOLLOWED QRH PROCEDURE 10-7. CREW NOTICED QTY DROPPING AND SUSPECTED NR 1 HYD SYSTEM FAILURE. CREW THEN FOLLOWED QRH 10-5 QTY INDICATION JUST ABOVE AMBER, GREEN IN FLT DECK WITH ENGINES SHUTDOWN. NR 1SDR HNAA2016052500149Circuit Breaker · pulledDURING TAKEOFF ROLL, NO CONFIGURATION WARNING. CREW ABORTED TAKEOFF. REF ETD2016-145-049640, THE NO TAKEOFF CONFIG WARNING WAS INDUCED DUE TO SPOILER IND CB PULLED IAW DDPM AND IND FAILS TO SHOW "OPEN". SPOILER IND CB CLOSED AND MAINTENANCE ACTION C/W IAW ESDR HNAA2016050200128Relay · failedWHILE ON DESCENT NR 3 PITOT INOPERATIVE. EICAS CAUTION MESSAGE APPEARED. STARTED SMELLING ODOR THAN MOMENTS LATER F/A REPORTED SMOKE IN CABIN. DECLARED EMERGENCY LANDING AND EVACUATED ACFT ON GROUND. NO HISTORY CX DAMAGE INSPECTION OVERHEAT BURN DAMAGE FOUNSDR HNAA2016041500104Warning Light · false activationBAGGAGE DOOR OPEN INDICATION ON T/O ROLL. ABORTED T/O, RETURN TO GATE AND CONFIRMED DOOR CLOSED.SDR SIMA20160218003Skin · crackedRIGHT UPPER FUSELAGE SKIN CRACKED AT FRAME 75, THE FIRST FASTENER BELOW STRINGER 2R. REPAIRED RT UPPER FUSELAGE SKIN CRACK IAW ERS-EM-53MR-1930.SDR SIMA20160218004Skin · crackedLEFT UPPER FUSELAGE SKIN CRACKED AFT OF FRAME 75 & ABOVE STRINGER 2L. REPAIRED LT UPPER FUSELAGE SKIN CRACK IAW ERS-EM-53MR-1930.SDR SIMA20160209005Stringer · corrodedSTRINGER 20R IS CORRODED, BETWEEN FRAME 13 - 14. CORROSION IS ACCEPTED AS IS IAW ERS-EM-5300-1920.SDR SIMA20160201008Support · corrodedTOILET WASTE VLV SUPPORT CORRODED. FABRICATED & PREPPED REPAIR DOUBLER IAW SRM 53-31-02.SDR SIMA20160130002Yoke · crackedRIGHT FWD PYLON LOWER YOKE CRACKED ON THE FWD FLANGE. REMOVED & INSTALLED SERVICEABLE YOKE IAW EO EM-54MR-386.SDR SIMA20160128021Firewall · crackedINTERNAL APU FIREWALL SKIN CRACKED ABOVE RT VERTICAL SUPPORT UPPERMOST RIVET. REPAIRED INTERNAL APU FIREWALL SKIN ABOVE RT VERTICAL SUPPORT UPPERMOST RIVET IAW EO EM-53AD-1883R5.SDR SIMA20160128020Beam · crackedSERVICE DOOR LOWER BEAM CRACKED AT AFT END. SEE NRTC E491285 FOR CORRECTIVE ACTION. ENTIRE BEAM IS BEING REPLACED UNDER THAT NRTC.SDR SIMA20160128018Light · dirtyPASSENGER DOOR EMER LIGHT INOPERATIVE. CLEANED PAX DOOR EMER LIGHT IAW CPM 51-14-00. OPERATIONS CHECKED GOOD.SDR SIMA20160128017Skin · crackedEXTERNAL FUSELAGE SKIN ONE POSSIBLE CRACK AT RIVET ON FRAME 78, BETWEEN STRINGER 5L & 6L. UPON FURTHER INVESTIGATION ALSO FOUND CRACK ON FRAME 78, BETWEEN STRINGER 3L - 4L. PERFORMED REPAIR ON FUSELAGE SKIN IAW ERS-EM-5300-1919.SDR SIMA20160128016Strip · brokenEMERGENCY LIGHT STRIPS 5 & 8 ARE BROKEN. R & R EMER LIGHT STRIPS 5 & 8 IAW AMM 33-50-12. SEE WIPS & TASKS FOR DETAILS OF WORK PERFORMED.SDR SIMA20160128014Spar · crackedLEFT WING SPAR I LOWER FLANGE CRACKED AT NUTPLATE HOLE AT RIB 9, VERIFIED BY HFEC. REPAIRED LT WING SPAR I LOWER FLANGE CRACK AT NUTPLATE HOLE AT RIB 9 IAW ERS-EM-57MR-583. SEE WIPS & TASKS FOR DETAILS OF WORK PERFORMED.SDR SIMA20160128013Wire · brokenSERVICE DOOR HINGE COVER EMER LIGHT HAS A BROKEN WIRE. REPAIRED WIRES ON SERVICE DOOR HINGE COVER EMER LIGHT IAW SWPM 20-21-00.SDR SIMA20160128012Crossbeam · corrodedCROSSBEAM AT FRAME 20 IS CORRODED. REMOVED & REPLACED CROSSBEAM AT FRAME 20 IAW SRM 51-40-02 & ETN-EM-53-139.SDR SIMA20160128015Support · crackedLEFT OMEGA BEAM OTBD SUPPORT IS CRACKED, BETWEEN FRAME 47 - 48. REMOVED CRACKED, BETWEEN FRAME 47 - 48. LEFT OMEGA BEAM OTBD SUPPORT & INSTALLED SERVICEABLE BEAM SUPPORTS IAW SRM 53-23-02.SDR SIMA20160128010Check Valve · failedRETURN LINE CHECK VLV OF THE EMER & PARKING BRAKE SYS FAILED OPERATIONAL CHECK. R & R EMER & PARKING BRAKE SYS RETURN LINE CHECK VLV IAW AMM 32-44-08. LEAK CHECKED GOOD.SDR SIMA20160128009Floorbeam · corrodedRIGHT OTBD AFT CARGO FLOORBEAM HAS CORROSION AROUND SCREW HOLE. REMOVED & INSTALLED RT OTBD AFT CARGO FLOORBEAM, FLOORBOARD SUPPORT, IAW SRM 51-40-02.SDR SIMA20160128008Connector · disconnectedEMERGENCY LIGHT FLOOR STRIPS 3 & 4 INOPERATIVE. RECONNECTED PLUG P8031 J8031 AT NR 3 BATTERY IAW SWPM 20-21-00 & AMM 20-50-00. OPERATIONS CHECKED GOOD IAW AMM 33-50-00.SDR SIMA20160128011Wire · damagedSERVICE DOOR EMER LIGHT WIRE IS DAMAGED. REPAIRED SERVICE DOOR EMER EXIT LIGHT WIRE IAW SWPM 20-21-00.SDR SIMA20151114005Mount Bracket · brokenREAR CABIN FLASHLIGHT MOUNTING BRACKET BROKEN. R & R REAR CABIN FLASHLIGHT ASSEMBLY IAW AMM 33-50-16. OPERATIONS CHECKED GOOD.SDR SIMA20150814001Bleed Valve · malfunctionedABORTED TAKEOFF, DUE TO BLD 2 VALVE FAIL EICAS MSG, AFTER THRUST SET ON TAKEOFF. 1 TAKEOFF IAW MEL GOT MSG SPEED WDS 30-40 KTS. R & R ENG 2 BLEED VALVE IAW AMM 36-11-05. OPERATIONS CHECKED GOOD AT THIS TIME.SDR SIMA20150513005Warning System · activatedEICAS MSG, SPOILER FAIL IN FLIGHT SPOILERS INDICATED CLOSED. CB PULLED IAW AOM 1 CHECKLIST. POST FLIGHT INSPECTION FOUND LT INBD SPOILER PANEL FLOATING SLIGHTLY. PERFORMED OPERATIONAL TEST OF SPOILER SYS IAW AMM 27-63-01. SYS OPERATIONS CHECKED NORMAL AT TSDR SIMA20150511001Cradle · brokenCAPTAIN'S EMER FLASHLIGHT CRADLE BROKEN. R & R CAPTAIN`S EMER FLASHLIGHT CRADLE IAW EMB TASK 33-50-16-000-801-A & TASK 33-50-16-400-801-A. OPERATIONS CHECKED GOOD.SDR SIMA20150504004Proximity Sensor · failedAFTER LANDING NOSE WHEEL STEERING NOT WORKING. TOWED TO THE GATE. R & R NLG WOW PROXIMITY SWITCH IAW AMM 32-63-02. OPERATIONS CHECKED GOOD IAW ETN-EM-32-176 & FIM TASK 32-50-00-810-803-REF ITEM 2 LG 3673600.SDR SIMA20150322003Bracket · brokenREAR FLASHLIGHT CRADLE BROKEN. DEFERRED IAW MEL 25-53. M PROCEDURES COMPLIED WITH. R & R AFT EMER FLASHLIGHT BRACKET IAW AMM 33-50-16. OPERATIONAL CHECK GOOD, MEL RESTORED.SDR SIMA20150310003Sensor · contaminatedDURING LEVEL CRUISE FLIGHT AT 17,000 FEET & 310 KIAS, SPOILER FAIL, PRESENTED & MAINTAINED ON EICAS. COMPLIED WITH ABNORMAL PROCEDURE & CFR MET US ON LANDING. FOUND LT & RT OTBD SPOILER SENSORS CONTAMINATED & NOT PROPERLY WRAPPED. CLEANED & REWRAPPED BOTH SSDR SIMA20150226005Anti-Ice Valve · failedNR 2 ENGINE ANTI-ICE FAILED INFLIGHT AFTER AOM 1 PROCEDURE. R & R ANTI-ICE VALVE IAW AMM 30-21-01. OPS CHECKED GOOD IAW AMM 30-00-00-700-802-A & 30-00-00-700-803-A.SDR SIMA20141014008Light · inoperativeMAIN DOOR EMER LIGHT INOPERATIVE. R & R MAIN DOOR EMER LIGHT LAMP IAW AMM 33-50-06-000-801-A & 33-50-06-400-801-A. OPERATIONS CHECKED GOOD.SDR SIMA20140806009Unknown · fumesAFTER 15 MIN IN CRUISE COCKPIT STARTED FILLING WITH FUMES. EMER PROC COMPLIED WITH, CONTINUED TO LANDING & EMER DECLARED COMPLIED WITH ETN-EM-72-034. COULD NOT DETECT FUMES IN COCKPIT OR CABIN THROUGHOUT PROCEDURE. REMOVED PACK ACCESS PANEL 191EL & INSPECTESDR SIMA20140801007Wire Harness · defectiveEMERGENCY EXIT LIGHT UNDER FLIGHT DECK DOOR INOPERATIVE. R & R STEP LIGHT HARNESS IAW MM 33-26-06. OPERATIONS TEST OF EMER LIGHT GOOD IAW MM 33-50-00 & OPERATIONS TEST OF STEP LIGHT GOOD IAW MM 33-26-00.SDR SIMA20140617004Warning Light · false activationEMER LIGHTS NOT ARMED EICAS MSG, MOMENTARILY ILLUMINATED IN FLIGHT. CREW IS NOT SURE IF EMER LIGHTS ILLUMINATED. PERFORMED OPERATIONAL CHECK OF EMER LIGHTING SYS, NO DEFECTS NOTED AT THIS TIME IAW WORK CARD 33-700-17.SDR SIMA20140528002Controller · failedDURING CLIMB OUT ON FLIGHT 3362 CREW REPORTED A LOUD SQUEAL HEARD IN COCKPIT. AT FLT 20,000, CABIN ALT 2600, CABIN RATE AT 0, CAB DELTA P AT 6.6 CABIN RATE DID NOT CHANGE. DECLARED EMERGENCY FOR CABIN PRESS THE ACFT WAS REMOVED FROM SERVICE. BONDED LOWER SESDR SIMA20140406005Warning System · activatedAPU FAIL MSG AFTER APU WAS RUNNING. STRONG ODOR OF FUEL AFTER APU STARTED. DEFERRED IAW MEL 49-1 & COMPLIED WITH MX PROCEDURE. EXAMINED THE FUEL LINE & CONNECTION FOR LEAKS, PERFORM OPERATION CHECK ON APU. OPERATIONS CHECKED GOOD, NO LEAKS IAW AMM 49-13-00SDR SIMA20140306002Acm · seizedA LITTLE SMOKE IN COCKPIT AFTER ENG NR 1 WAS STARTED 30 SEC LATER PACK NR 1 OVERHEAT MSG. FOUND NR 1 ACM SEIZED. R & R NR 1 ACM IAW AMM 21-51-03, OPERATIONS CHECKED GOOD AT THIS TIME. PERFORMED ETN EM 72-034 ENG ODOR EVENT SUPPLEMENT, NO DEFECTS NOTED AT THSDR SIMA20140302002Brake · failedFLAP FAIL MSG WHEN FLAP LEVER MOVED TO 9. INDICATION REMAINED AT 0 ON EICAS. ACFT HAD VERY SLIGHT TENDENCY TO ROLL RIGHT. R & R RT FLAP TRANSMISSION BRAKE IAW AMM 27-51-01, OPERATIONS CHECKED GOOD.SDR SIMA20140226003Warning System · activatedWHEN SETTING FLAPS FROM FULL UP, O DEGREES TO 9 DEGREES ON FINAL APPROACH FOR LANDING WE GOT, FLAP FAIL, MSG ON EICAS. PERFORMED FIM TASK 27-51-00-810-816-A. MSG CHANGED TO FLAP LOW SPEED.SDR SIMA20140204002Actuator · faultyWHEN THRUST REVERSER WERE STOWED AFTER LANDING EICAS ENG 2 REVERSER DISAGREE MSG WAS PRESENTED & REMAINED ON AFTER SHUT DOWN. R & R E2 TERTIARY LOCK ACTUATOR IAW AMM 78-32-05. OPERATIONS CHECK & LEAK CHECKED GOOD.SDR SIMA20140131001Skin · corrodedINTERNAL FUSELAGE SKIN CORRODED BETWEEN FRAME 13 - 14, STRINGER 18R - 20R. PERFORMED REPAIR IAW AEA ERS-EM-53MR-210.SDR SIMA20140113017Yoke · crackedLEFT PYLON FWD LOWER YOKE I CRACKED BY ENG MOUNT. R & R LT PYLON FWD LOWER YOKE I IAW EO EM-54MR-386.SDR SIMA20131230016Stringer · corrodedSTRINGER 21L IS CORRODED AT FRAME 13. INSTALLED NEW STRINGER 21L & INSTALLED STRINGER SPLICE IAW SRM 51-40-02.
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