N382HA
Service difficulty reports · 176
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 = 'N382HA' 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 = 'N382HA' 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 HALA2018060400276Warning Light · false activationNR 1 ENGINE MINOR FAULT ECAM ILLUMINATED DURING LANDING. PERFORMED AN OP CHECK IAW TSM 73-21-71-810-863-A. NO FAULTS NOTED. MESSAGE CLEARED. OK FOR SERVICE.SDR HALA2018032000114Actuator · malfunctionedETOPS SIGNIFICANT SYSTEM, FUEL T TANK XFR FAULT ON ECAM. REPLACED LT OUTER TANK INLET VALVE ACTUATOR PER AMM 28-25-57-400
-801-A. OPS CHK OK. OK FOR SVC.SDR HALA2018031500106Warning System · false activationETOPS SIGNIFICANT SYSTEM - ELECT APU BATT SYS FAULT ECAM. PERFORMED RESET PROCEDURE PER AMI 24-38. NO FAULT NOTED. CK NORMAL.SDR HALA2018030500068Warning Message · false activationDURING CLIMB OUT, ECAM FOR AIR BLEED LO TEMP DISPLAYED. PERFORMED ECAM ACTIONS, BUT ECAM DID NOT CLEAR. LEFT ENGINE INTERCOOLER TEMP DISPLAYED IN AMBER AT 190 C, BUT THIS IS WITHIN THE NORMAL RANGE FOR THE INTERCOOLER OUTLET TEMP. MOST LIKELY A FAULTY SESDR HALA2018030100062Apu · auto shutdownAPU AUTO SHUTDOWN. FOUND FUEL SPLY, FCU, FLOW DIVIDER ASSY FAULTED ON TAXI IN. APU TESTED OK ON THE GROUND IAW AMM 49-00-00-710-801-A. APU STARTED SUCCESSFULLY THREE TIMES. RAN APU FOR 1 HOUR, NO FAULTD NOTED.SDR HALA2018010500004Light · looseEMERGENCY LIGHT STRIP FOUND LOOSE AT SEAT 40 - 41HJ. SECURED THE LIGHT STRIP.SDR HALA2017110300255Transceiver · failedRETURNED TO DEPARTURE DUE TO THE NR 1 HF FAILED. REPLACED THE NR 1 HF COUPLER AND TRANSCEIVER.SDR HALA2017092500248Fire Loop · faultedNR 2 ENGINE FIRE LOOP B FAULTED.SDR HALA2017050300128Exciter · failedAPU FAULT. APU FAILED AFTER 3 ATTEMPS AFTER LANDING. REMOVED AND REPLACED IGNITION EXCITER BOX IAW AMM 49-41-38. OPS CHECKED OK. 1ST ATTEMPT GOOD START.
OK FOR SERVICE.SDR HALA2017040200092Limiter · failedAPU BATTERY SYS FAULTED ON ECAM, DURING CRUISE. REMOVED & REPLACED THE BATTERY CHARGE LIMITER IAW AMM 24--38-35-000-801-A, & 24-38-35-400-801-A. OPS CHECKED GOOD. OK FOR SERVICE.SDR HALA2016121300543Transmitter · erraticDURING T/O ROLL ENG NR 1 FUEL USED DIGITAL COUNTER "HUNDREDS" DOUBLE HORIZ AMBER LINE OUT. FUEL TOTAL COUNTER AMBER LINE OUT THROUGH "TENS". FUEL FLOW TRANSMITTER (E1-4070KS) WITH HISTORY. REPLACED FF XMITTER PER AMM 73-31-11, OPS OK. METER, FUEL FLO OFF 43SDR HALA2016120700524Thermostat · damagedAT APPROX 3000' ON INITIAL CLB ECAM AIR ENG 1 BLEED FAULT DISPLAYED. FOLLOWED ECAM PROCEDURE CONTACTED DISP & MX. INSTRUCTED BY MX TO PERFORM QRH PROG ON P636.01AA FOR RESET UNSUCCESSFUL. REMOVED PANEL 452 CL, REMOVED THERMOSTAT P/N 398E020000 S/N01954 SENSE SDR HALA2016110700512Thermostat · damagedATB, AT APPROX 3000' ON INITIAL CLB ECAM AIR ENG 1 BLEED FAULT DISPLAYED. FOLLOWED ECAM PROCEDURE CONTACTED DISP & MX INSTRUCTED BY MX TO PERFORM QRH PROG ON P636.01AA FOR RESET UNSUCCESSFUL. REMOVED PANEL 452 CL, REMOVED THERMOSTAT P/N 398E020000 S/N01954 SSDR HALA2016110600511Filter · cloggedATB, INTERMITTENT ENG 1 BLEED FAULT DURING CLIMB OUT. T/S IAW TSM 36-21-00-810-925-A22, FOUND FAN-AIR VALVE CONTROL THERMOSTAT FILTER CLOGGED. CLEAN FLITER CHECK GOOD. OK FOR SVC.SDR HALA2016110200406Cooling Fan · contaminatedAPU COOLING FAN ASSY FOUND WITH EVIDENCE OF OIL CONTAMINATION. APU COOLING FAN REPLACED IAW AMM 49-52-51. REFER OM12 ITEM 5 FOR LEAK AND OP CHECK. TASK COMPLETE. FAN ASSY OFF 33-4952-9-0002 00684 ON 33-4952-9-0002 01376.SDR HALA2016110200405Roller Tray · corrodedAFT CARGO ROLLER TRAY BETWEEN FR58 AND FR65 -Y805 HAS CORROSION AT FR62. CORROSION REMOVED IAW SRM 51-74-00 R 91.00, BLEND IS OUT OF LIMIT IAW SRM 51-74-00 REV 91.00. NEW ROLLER TRAY INSTALLED IAW AMM 25-51-21 R55. JOB COMPLETESDR HALA2016110200404Oil Cooler · failedAPU OIL LEAK EVIDENT FROM APU OIL COOLER AIR EXIT DUCT. NEWLY INSTALLED AIR/OIL COOLER FTN 3KYIT6 BAD FROM STOCK. INTERNAL LEAKAGE IDENTIFIED DURING OPS TEST OF APU. AIR OIL COOLER REPLACED IAW AMM 49-91-44 REV 55. AIR/OIL COOLER P/N 160242-2 S/N 902 FTN 6SDR HALA2016110200403Panel · looseACCESS REQUIRED UNDER LT ENGINE FADEC SUITCASE TO RECTIFY OGV INFILL PANELS LOOSE UPPER LT SIDE. INFILL PANELS LOOSE UPPER LT SIDE. LEFT HAND ENGINE FADEC SUITCASE AND CONTENTS REMOVED FOR ACCESS TO OGV'S, RE-INSTALLED AND TESTED SERVICEABLE IAW AMM 73-21-34SDR HALA2016110200402Seat Track · corrodedSEAT TRACK +450 BETWEEN FRAMES 53.2 TO 53.5 CORRODED. THE SEAT TRACK WAS REPLACED IAW DWG F53326912004, F53325686004, F53329385002, AND SRM 51-72-11 REV 91.SDR HALA2016110200401Connector · damagedNR 1 ENGINE BLEED PRESSURE REGULATOR VALVE CONNECTOR HAS LOOSE BACKSHELL. CONNECTOR REPLACED IAW ESPM 20-33-45 REV 32.00, AMM 36-11-52 REV 55.00, AMM 70-50-02 REV 55.00 AND 73-21-00 REV 55.00.SDR HALA2016110200400Roller Track · corrodedAFT CARGO ROLLER TRAY BETWEEN FRAMES 58 AND 65. CORROSION REMOVED IAW SRM 51-74-00 REV 91. REPAIR CARRIED OUT IAW ERA 552192-14 AND TELAIR CMM 25-51-83 REV 4. BLENDED AND REPAIRED AREAS PRIMED AND PAINTED IAW SRM 51-75-12 ROLLER TRACK REINSTALLED IAW SRM 51SDR HALA2016110200399Seat Track · corrodedSEAT TRACK -2462 BETWEEN FRAMES 58 - 62 CORRODED. CORROSION REMOVED IAW SRM 51-22-00 R91. SEAT TRACK REPLACED IAW DWG F53477040006, F53477650004, F53477040006 AND SRM 51-72-11 REV 91.SDR HALA2016110200398Roller Tray · corrodedAFT CARGO ROLLER TRAY HAS CORROSION AT FRAME 65. THE AFT CARGO ROLLER TRAY WAS REPLACED IAW AMM 25-51-21-400-802-A REV 55.00.SDR HALA2016110200394Seat Track · corrodedSEAT TRACK -1959, FRAMES 53.2 TO 55 HAS CORRODED. CORROSION REMOVED IAW SRM 51-22-00 R91. SEAT TRACK REPLACED IAW DWG F53326941000, F53325686004, F53329385002 AND SRM 51-72-11 REV 91.SDR HALA2016110200397Seat Track · corrodedSEAT TRACK -1959 FROM FRAMES 58 TO 62 CORRODED. CORROSION REMOVAL CARRIED OUT IAW SRM 51-74-00 R91. SEAT TRACK REPLACED IAW DWG F53477040006, F53477650004, F53477040006 AND SRM 51-72-11 REV 91.SDR HALA2016110200396Seat Track · corrodedSEAT TRACK -450 BETWEEN FRAMES 58 - 67 CORRODED. CORROSION REMOVED IAW SRM 51-22-00 R91 BLEND OUT DIMENSIONS AS FOLLOWS: 9'' AFT OF FR 58 ON 'SUPERIOR AND LATERAL AREA' DEPTH 0.003''LENGTH 1'' WIDTH 0.5'' / 4'' AFT OF FR 61 ON 'LATERAL AREA' DEPTH 0.030'' LESDR HALA2016110200395Floor Support · corrodedSCRIBE AND CORROSION DAMAGE FOUND ON AUX FLOOR SUPPORT STRUCTURE AT BS 380, 15 INCHES AFT OF FRAME 75. CORROSION DAMAGE BLENDED IAW SRM 51-74-00 RBL 91. BLEND DIMENSIONS 5.70" X 0.5" DEPTH 0.019". ASSESSED AS OUTSIDE OF SRM 53-00-14 REV 91 LIMITS. REPLACEMESDR HALA2016110100393Seat Track · corrodedSEAT TRACK SECTION -Y1959, C26 - C38 IS CORRODED. CORROSION REMOVED IAW SRM 51-74-00 REV 91. BLEND DIMENSIONS STA17638 CROWN CENTRA/INNER VERTICAL 25MM X 10MM UNABLE TO MEASURE DEPTH DUE LOCATION. STA20598 CROWN CENTRAL/INNER VERTICAL 15MM X 5MM DEPTH 3MM, SDR HALA2016110100392Structure · corrodedFOUND SUSPECT CORROSION ON AFT CABIN FLOOR RT LONGERON -Y794.3 AT 9 INCHES AFT OF FR C75. CORROSION REMOVED IAW SRM 51-22-00 R91 BLEND OUT DIMENSIONS AS FOLLOWS. FLOOR LONGERON AT -794.3 FROM FR 74 TO 80 LENGTH 0.75" WIDTH 0.35" DEPTH 0.050" BLEND BEYOND SRMSDR HALA2016110100391Seat Track · corrodedDOOR 1 WET AREA , SEAT TRACK Y-953 BETWEEN FR 11 TO FR 18 AT FR 13A ,HAS AN AREA OF SUSPECT CORROSION ON RUN OUT AREA AS MARKED. CORROSION REMOVED IAW SRM 51-22-00 R91. BLEND OUT DIMENSIONS L=3.0", W=1.75", D=0.065" FOUND TO BE OUT OF LIMITS IAW A330 SRM 53-SDR HALA2016110100390Longeron · corrodedDOOR 1 WET AREA ,LONGERON AT Y-1959 BETWEEN FR12 AND FR18 FOUND TO HAVE SUSPECT CORROSION AT FR16A AS MARKED. CORROSION REMOVAL CARRIED OUT IAW SRM 51-22-00 REV 91. BLEND DIMENSIONS; L=1.5", W=0.75", D=0.060". BLEND AREA FOUND BEYOND LIMITS OF SRM 51-11-15SDR HALA2016110100389Intercostal · corrodedDOOR 1 WET AREA ,INTERCOSTAL BETWEEN Y - 450 TO Y- 953 AT FR 13A FOUND TO HAVE SUSPECT CORROSION. CORROSION REMOVAL CARRIED OUT IAW SRM 51-22-00 REV 91. BLEND DIMENSIONS, LENGTH 1.300" WIDTH. 0.900" DEPTH. 0.035" MATERIAL THICKNESS 0.085". BLEND AREA FOUND SDR HALA2016110100388Structure · corrodedFOUND CABIN FLOOR LONGERON Y0 CORRODED WHERE IT INTERSECT WITH FLOOR CROSSBEAM AT FR 75. CORROSION REMOVED AS PER SRM 51-74-00 REV 91. DAMAGE DIMENSIONS: 0.500" X 1.000" MAX DEPTH: 0.032". DAMAGE BEYOND ACCEPTABLE LIMITS AS PER SRM 53-00-14 REV 91. RII OF SDR HALA2016110100387Floor Support · corrodedSUSPECT CORROSION FOUND ON LONGITUDINAL AUX FLOOR SUPPORT LOCATED I/B OF LONGERON Y450 LT, 9 INCHES FWD. CORROSION REMOVED IAW SRM 51-74-00 REV 91. DAMAGE DIMENSIONS 8.200" X 0.500" MAX DEPTH 0.034". ASSESSED AS OUTSIDE OF SRM 53-41-14 REV 91 LIMITS. RII OSDR HALA2016110100386Seat Track · corrodedSEAT TRACK +450 FROM FR 58 TO 67 HAS CORROSION. CORROSION REMOVAL IAW SRM 51-74-00 R91. BLEND MEASUREMNETS, FR 63, LATERAL AREA DEPTH 0.010'' LENGTH 0.5''. CORROSION UNABLE TO BE FULLY REMOVED FROM INNER VERTICAL AREAS IAW SRM 51-74-00 R91. DUE TO NIL ACCSDR HALA2016110100385Seat Track · corrodedSEAT TRACK +1959 FROM FR 55 T0 58 HAS CORROSION. CORROSION REMOVED IAW SRM 51-22-00 R91. DURING REMOVAL OF CORROSION FROM CENTRAL AREA CORROSION FOUND TO PENETRATE INNER VERTICAL AREA. CORROSION UNABLE TO BE FULLY REMOVED FROM INNER VERTICAL AREA IAW SRM 51SDR HALA2016110100384Seat Track · corrodedSEAT TRACK +1959 FROM FR 58 TO FR 62 HAS CORROSION. CORROSION UNABLE TO BE FULLY REMOVED FROM INNER VERTICAL AREAS IAW SRM 51-74-00 R91 DUE TO NIL ACCESS. FULL EXTENT OF CORROSION UNABLE TO BE DETERMINED. CORROSION RII FOR LVL 2 CORROSION IAW GMM VOL1 CHAPTSDR HALA2016110100383Seat Track · corrodedSEAT TRACK +2462 BETWEEN FR62 - FR72 CORRODED. CORROSION REMOVED IAW SRM 51-22-00 R91. BLEND OUT DIMENSIONS, 13'' AFT OF FR62 ON LATERAL AREA DEPTH 0.004'' LENGTH 0.25'' WIDTH 0.25'' ON FR65. ON SUPERIOR AREA DEPTH 0.063'' LENGTH 2'' WIDTH 0.5'' 11'' AFT OFSDR HALA2016110100382Seat Track · corrodedSEAT TRACK +1959 FROM FR 62 TO FR 71 HAS CORROSION. CORROSION REMOVAL IAW SRM 51-74-00 R91. DUE TO NIL ACCESS. FULL EXTENT OF CORROSION UNABLE TO BE DETERMINED. CORROSION RII FOR LVL 2 CORROSION IAW GMM VOL1 CHAPTER 5 1.8.2 REV 43. SEAT TRACK Y+1959 FR62 SDR HALA2016110100381Floorbeam · corrodedCORROSION FOUND ON FRAME C75 FLOORBEAM. CORROSION REMOVED IAW SRM 51-74-00 REV 91. HFEC INSPECTION CARRIED OUT IAW NTM 51-10-02, NO CRACKING OR FURTHER DAMAGE EVIDENT, FLAP PEEN CARRIED OUT IAW SRM 51-29-11 REV 91 AND SURFACE PROTECTED IAW SRM 51-75 -12 RESDR HALA2016110100380Fire Detector · chafedZONE 3 FIRE DETECTORS 4021WD-S AND 4022WD-S ON R ENG CHAFED AT 6 O'CLOCK POSITION AT LOWEST POINT ABOVE BIFURCATION JUNCTION. NR 2 ENG, ZONE 3 FIRE DETECTOR ASSY REPLACED IAW AMM 26-12-17 REL 55.00. NR 2 ENG, ZONE 3 FIRE DETECTOR ASSY TESTED IAW AMM 26-12-00SDR HALA2016103100378Seat Track · corrodedAUX SEAT TRACK SECTION -Y1552, FRAME C29 - C35 IS CORRODED. CORROSION REMOVED IAW 51-74-00 REV 91. DAMAGE DIMENSIONS, STA 20148 CROWN CENTRAL 40MM X 25MM DEPTH 1.1MM. STA 20338 CROWN SUPERIOR/LATERAL 40MM X 7MM DEPTH 0.8MM, ASSESSED AS LEVEL 2 CORROSION (OUSDR HALA2016103100377Seat Track · corrodedSEAT TRACK SECTION -Y1959, C47-C53.2 IS CORRODED. CORROSION REMOVED IAW SRM 51-74-00 REV 91. BLEND DIMENSIONS STA33113 CROWN SUPERIOR 15MM X 3MM MAX DEPTH 0.6MM. STA36328 CROWN SUPERIOR 4MM X 2MM DEPTH 0.6MM 3. STA36578 CROWN SUPERIOR 45MM X 10MM DEPTH 1MM,SDR HALA2016103100376Seat Track · corrodedSEAT TRACK SECTION -Y1959, C26 - C38 IS CORRODED. CORROSION REMOVED IAW SRM 55-74-00 REV 91. DAMAGE DIMENSIONS STA 29968 CROWN CENTRAL/LATERAL 13MM X 5MM DEPTH 1MM, STA 31578 CROWN CENTRAL/LATERAL 10MM X 5MM DEPTH 1MM, 3 STA 33188 CROWN SUPERIOR 40MM X 10MM SDR HALA2016102900161Seat Track · corrodedSEAT TRACK AT C53.2-55, Y953 FOUND CORRODED. REPLACED THE SEAT TRACK AND U CHANNEL IAW SRM 51-72-11, AND DRAWING F53326963001.SDR HALA2016102900160Seat Track · corrodedSEAT TRACK AT C26-38, Y450 FOUND CORRODED. INSTALLED A NEW SEAT TRACK REPAIR SPLICE IAW SRM 53-21-15 AND DRAWINGS F53276421004, F53271910000, AND F53328090001.SDR HALA2016102900159Seat Track · corrodedSEAT TRACK AT C26-38, -Y450 WAS FOUND CORRODED. A NEW SEAT TRACK SPLICE REPAIR SECTION INSTALLED IAW SRM 53-21-15 AND DRAWINGS F53276421004, F53271910000 AND F53328090001.SDR HALA2016072600145Controller · malfunctionedAIR TURNBACK TO DEPARTURE DUE TO ANTI-ICE WINDSHIELD HEAT MESSAGE DISPLAYED. PERFORMED RESET OF WHC 1 AND 2 TWICE WITH NO HELP, MESSAGE RETURNED 20 SECONDS LATER. REPLACED CAPTAIN'S WINDSHIELD AND WINDOW HEAT CONTROLLER. LP 8071481.SDR HALA2016072500298Windshield · inoperativeAIR TURNBACK DUE TO ANTI ICE LT WINDSHIELD HEAT INOPERATIVE. R & R WINDSHIELD IAW MM 56-11-11-400-801A, OPS CHECKED OK.SDR HALA2016052700226Stator · damagedETOPS SIGNIFICANT SYSTEM, ENGINE 1 FADEC SYS FAULT ECAM/ENG 1 OVERSPEED PROTECTION. T/S IAW TSM 73-21-89-810-818A AND FOUND J3 CONNECTOR ON PMA READING OPEN FIELD. R & R PMA STATOR IAW AMM 73-21-51. OPS NORMAL. ACFT OK FOR SERVICE.
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