N386HA
Service difficulty reports · 155
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 = 'N386HA' 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 = 'N386HA' 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 HALA2021092900128None · noneETOPS - FOUND CANNON PLUG BACK SHELL 4041KS-A OFF OIL PRESSURE SWITCH (OIL FILTER DIFFERENTIAL) BROKEN // REMOVE REPLACED4041KS-A BACKSHELL, PNR ESC75E08,PER ESPM 20-44-10. OPS CHECK PENDING MECH 1932291 27 SEP 21 RAN ENGINE AT IDLE PER AMM 71-00-00-860-810A OSDR HALA2021091400115Transmitter · faultedETOPS - INFO TO MX: DURING CRUISE ENG #1 OIL PRESSURE STAYED VARIABLE BETWEEN 58-80 PSI WHILE ENG #2 HELD EXACTLY 72-76 PSI. // ACCOMPLISHED TSM 79-31-00-810-848 A. REMOVED AND REPLACED ENG 1 OIL PRESS TRANSMITTER #1 AND #2 PER AMM 79-33-11-400-803 A. ACCOMPLISDR HALA2021082500122Glowstrip · missingSHIP 386 FWD GALLEY FORWARD LUMINOUS FLOOR STRIP MISSING. CORRECTIVE ACTION: INSTALLED FWD GALLEY FLOOR STRIP PER AMM 33-51. (7737335)SDR HALA2020122900228Control Unit · defectiveETOPS-BTB AFTER NR 1 ENGINE START ECAM ENGINE NR 1 CTL SYS FAULT, PER MOC SHUT DOWN NR 1 ENGINE RESTART SAME FAULT. REMOVED AND REPLACED LT ENG VSV CONTROL UNIT, PER AMM A330 75-33-51. OPERATIONS CHECK GOOD LEAK CHECK GOOD RAN NR 1 ENGINE NO FAULTS OK FOR SESDR HALA2020111000200Generator · defectiveODOR/FUMES, WET SOCK SMELL ON GROUND USING APU BLEED AIR. ONCE ENGINE BLEEDS ON, SMELL DISSIPATED. DURING DESCENT SMELL RETURNED AT 11,000 AND LASTED UNTIL PARKING. NO GO ODI CHECKLIST ATA 2172 SMOKE AND FUMES PRESENT C/W GENERATOR, APU, OFF 33-2423-9-0001 SDR HALA2020110200196Probe · malfunctionedETOPS-WHILE ACCOMPLISHING MC LOG 1643531 FOUND ENGINE NR 2 LOAD TGT FOUND PROBES 4045KS8 AND 4045KS10 INSULATION RESISTANCE BAD, PER AMM 77-21-00-710-801-A. TGT PROBES 4045KS8 AND 4045KS10 DISCONNECTED FROM HARNESS 10/30/20 824976. REPLACED TGT PROBES 4045KSSDR HALA2020072400155Autothrottle Sys · malfunctionedETOPS SIGNIFICANT SYSTEM - AUTO THRUST DID NOT ENGAGE ON T.O. BUT EPR SETTING & INDICATION WERE CORRECT,SET THRUST MANUALLY. UNABLE TO ENGAGE W/ A/THRUST BUTTON. ENGAGE A/P 1, UNABLE TO ENGAGE A/THR. W/A.P.2 A/THR ENGAGED NORMALLY, ENGAGED AP1 AGAIN THIS TIME SDR HALA2020060100118Cowling · scratchedSCRATCH FOUND ON NR 2 ENGINE INLET COWL, AROUND 7 O'CLOCK POSITION. DAMAGE ASSESSMENT CARRIED OUT IAW SRM 54-10-01. REFER TO ATTACHED FOR DETAILS. COMPOSITE REPAIR ON NR 2 ENGINE INLET COWL AROUND 7 O'CLOCK POSITION 03 OFF AREAS. CARRIED OUT AS IAW TV NO 2SDR HALA2020042900100Oil System · overservicedON T/OFF FA'S SMELLED AN FUME ODOR (BO-MUSTY SMELL IN CABIN). LASTED A FEW MINS. OPS NORMAL. // TROUBLE SHOT FUME SMELL PER TSM 21-00-00-810-805-A. FOUND #2 ENG OIL OVER SERVICED. DRAINED OIL PER AMM 12-13-79-680-801. PERFORMED IDLE ENG RUN WITH BOTH ENGINES.SDR HALA2020041700089Actuator Valve · faultyETOPS SIGNIFICANT SYSTEM - FUEL AFT TRANSFER INOP ECAM AFTER 2ND ENG START RESET BOTH FCMC AND FWC BTB.// REMOVED AND REPLACED OUTER TANK FUEL INLET VALVE ACTUATOR
500QU1 PER 28-25-57 OPS CHECK OK OK FOR SVC.SDR HALA2020030300049Thrust Reverser · delaminatedDURING U/T INSPECTION OF OUTER FIXED STRUCTURE ON #2 O/B T/R ON AMDS WORK CARD 7830-01499-01B DE-LAMINATION FOUND . REPAIR OF THE OFS IS REQUIRED PER ROLLS ROYCE STRUCTURAL REPAIR MANUAL SRM, FRSX016. // REPAIRED PER RB211 TRENT SRM 54-30-01 REPAIR NO. 10.SDR HALA2020011000012Light · malfunctionedCREW REPORT EMERGENCY LIGHTS ON IN ARM POSITION. // RESET CIDS 1 & 2 AND PERFORMED EMERGENCY LIGHT. OPS TEST PER AMM
33-51-38. NO FAULTS NOTED. OK FOR SERVICE.SDR HALA2020010800004Switch · malfunctionedEMERGENCY LIGHT ILLUMINATED IN ARMED POSITION. RE-CYCLED FAP/EMERGENCY LIGHT SWITCH. LP 7226221SDR HALA2020010700002Switch · malfunctionedEMERGENCY LIGHT CAME ON IN ARM POSITION. // RECYCLED FAP/EMER LIGHT S/W.THEN CHECKED & OK FOR SERVICE.LOG
ITEM CLOSED.REF A330 AMM 33-51-00.SDR HALA2019110600467Light · looseLAV A FLOOR LIGHT STRIP CAME LOOSE. // RE-SECURED EMERGENCY ESCAPE PATH FLOOR LIGHT STRIP AT LAV A OK
FOR SERVICE.SDR HALA2019070200339Warning System · false activationETOPS SIGNIFICANT SYSTEM - ECAM FUEL CTR TO INNER FAULT. PFR INTERROGATED MSG # 282653 FUEL INNER TANK VALVE (603QL2) SHOWN. TSM 28-26-00-810-802 C/OUT SYSTEM TEST AND VALVES TEST OK, MSG CLEARED.SDR HALA2019032200138Warning System · false activationETOPS SIGNIFICANT SYSTEM - FUEL T TANK XFR- FAULT. T/S PER TSM 28-27-00-810-828-A PERFORMED A BITE OF FCMC 1 AND FCMC 2 PER AMM 28-51-00-700-801-A BOTH TESTS PASSED, NO CURRENT FAULTS. AC OK FOR SVC.SDR HALA2019031800132Warning System · false activationETOPS SIGNIFICANT SYSTEM - ON CLIMB ECAM "FUEL T TANK XFR FAULT". FUEL AFT XFR VALVE 1 CLASS 1 FAULT IN PFR & PER TSM 28-
27-00. PERFORMED VLV TEST & TEST OK. NO ECAM MSG NOTED. A/C OK FOR SVC.SDR HALA2019031800130Actuator · failedETOPS SIGNIFICANT SYSTEM - DURING FUEL ECAM "FUEL T TANK XFR FAULT". FUEL VALVES TEST SHOWS OUTER TANK INLET VALVE 1 FAILED OPEN. REMOVED AND REPLACED INLET VALVE ACTUATOR PER AMM 28-25-57-400-801-A. OPS CHECK OK.SDR HALA2019011400025Warning System · false activationETOPS SIGNIFICANT SYSTEM - FUEL TRIM LINE FAULT ECAM @ CRUISE FL 400, ECAM CLEARED IT SELF AFTER 30 SEC. PERFORMED FCMS FUEL VALVES TEST OF TRIM TANK ISO VALVE PER AMM 28-51-00-710-801-A. OPERATIONAL CHECK GOOD. OK FOR SERVICE.SDR HALA2019011400024Warning Message · false activationETOPS SIGNIFICANT SYSTEM - FUEL TRIM LINE FAULT ECAM @ CRUISE FL 400, ECAM CLEARED IT SELF AFTER 30 SEC. PERFORMED FCMS FUEL VALVES TEST OF TRIM TANK ISO VALVE PER AMM 2
8-51-00-710-801-A. OPERATIONAL CHECK GOOD. OK FOR SERVICE.SDR HALA2018121700662Not Reported · malfunctionedETOPS SIGNIFICANT SYSTEM - APU DID NOT START AFTER 3 TRIES. C/W TSM 49-62-00-810-838A. NO FAULTS NOTED. STARTED APU TWICE ON GROUND WITH NO FAULTS. DUE TO LACK OF HISTORY. OK FOR CONTINUED SERVICE.SDR HALA2018121840364Anti-Ice Valve · inoperativeAIRCRAFT 386 DIV, DIVERTED TO LAX DUE TO THE ANTI-ICE LEFT AND RIGHT WING HIGH PRESSURE ECAM AND ASSOCIATED AMBER TRIANGLE AND AMBER ANTI-ICE DEPICTED ON BLEED PAGE. TURNING OFF THE WING ANTI-ICE PUSHBUTTON, ECAM MESSAGE DISAPPEARED. CORRECTIVE ACTION: REPLACESDR HALA2018121700657Anti-Ice Valve · malfunctionedATB - ETOPS SIGNIFICANT SYSTEM - ENCOUNTERED ICING CONDITIONS ECAM DIRECTED US TO TURN ON WING ANTI-ICE. AFTER APPROX 2 MINUTES OBSERVED A ICE L AND R WING HI PR ECAM AND ASSOCIATED AMBER TRIANGLE AND AMBER "ANTI ICE" DEPICTED ON BLEED PAGE. RECYCLED WING ANTISDR HALA2018121200648Transceiver · faultedETOPS SIGNIFICANT SYSTEM - PWS ON WX RADAR NR 2 INOP. PULLED POST FLIGHT REPORT. FOUND WXR2 RTU (13SQ2) FAULTED. REPEATED WRITE UP 4 EVENTS WITHIN 60 DAYS. REMOVED AND REPLACED TRANSMITTER RECEIVER UNIT (13SQ2) PER AMM 34-41-51. BITE TEST OK. OK FOR SVC.SDR HALA2018121100645Apu · malfunctionedETOPS SIGNIFICANT SYSTEM - INFO TO MX APU DID NOT START BETWEEN 7000' - 3000' TWICE. STARTED SUCCESSFULLY ON GROUND AT 3RD ATTEMPT. // NOTED BY MAINTENANCE PERFORMED TROUBLESHOOTING OF APU AUTO SHUT DOWN PER TSM TASK 49-62-00-810-838-A. PERFORMED FAULT CONFIRMSDR HALA2018120600634Valve · malfunctionedETOPS SIGNIFICANT SYSTEM - ECAM: ENGINE AIR BLEED NOT CLOSED NR 2 ENG. REMOVED AND REPLACED NR 2 ENG PRV PER AMM 36-11-52. OPS CK & LEAK CK OK. A/C OK FOR SVC.SDR HALA2018101000276Sign · detachedDOOR 3R EXIT SIGN FELL OFF. RE-ATTACHED EXIT SIGN. LP 4970613SDR HALA2018100200467Sign · detachedEXIT SIGN FELL OFF AT 3R DOOR. EXIT SIGN REATTACHED NOW OK FOR FLIGHT.SDR HALA208082000388Warning Message · false activationNR 1 ENGINE, DURING SECOND START ATTEMPT THE ENG 1 IGN B INOPERATIVE ILLUMINATED. TROUBLESHOT IAW TSM 74-00-00-810-844-A, NO FAULTS NOTED. AUDIBLE TESTED OK. NO SYSTEM BITE FAULTS FOUND. NO PREVIOUS HISTORY. OK FOR SERVICE.SDR HALA2018081700381Warning Message · false activationNR 1 ENGINE, DURING SECOND START ATTEMPT: ENG 1 IGN B INOPERATIVE ILLUMINATED. TROUBLESHOT IAW TSM 74-00-00-810-844-A, NO FAULTS NOTED. AUDIBLE TEST OK. NO SYSTEM BITE FAULTS FOUND. NO PREVIOUS HISTORY. OK FOR SERVICE.SDR HALA0218080300359Warning Message · false activationON STATUS PAGE UNDER MAINTENANCE ITEMS, SMOKE WAS LISTED AFTER LANDING AT GATE. PERFORMED SMOKE DETECTION SYSTEM BITE TEST AND MESSAGE ERASED, SYSTEM OK IAW AMM 26-10-00, TSM 26-23-06.SDR HALA2018042600188Warning Light · false activationFUEL AFT TRANSFER ILLUMINATED DURING CRUISE. PERFORMED TSM 28-27-00-810-802, BITE TESTED OF FCMS & FUEL VALVE TEST. BOTH PASSED. ACFT OK FOR SERVICE.SDR HALA2018042402776Cids · malfunctionedR2 AND R3 DOOREXIT SIGNS ILLUMINATED. RESET CIDS.SDR HALA2018042400182Cids · malfunctionedR2 AND R3 DOOR EXIT SIGNS ILLUMINATED CONTINUOUSLY. RESET CIDS. OPS NORMAL. OK FOR SERVICE.SDR HALA2018040900130Seat Track · corrodedDURING H CHECK, SEAT TRACK, FRAMES 47 - 53.2, -Y1959 WAS FOUND CORRODED. REPLACED THE SEAT TRACK IAW SRM 51-72-11, AND DRAWING F53312812.SDR HALA2018040900129Seat Track · corrodedDURING H CHECK, SEAT TRACK, FRAMES 47 - 53.2, +Y2462 WAS FOUND CORRODED. REPLACED THE SEAT TRACK IAW SRM 51-72-11, AND DRAWING F53312813.SDR HALA2017040900150Seat Track · corrodedSEAT TRACK BETWEEN FRAMES 51 TO 53.1 CORRODED. CORROSION REMOVED IAW SRM 51-74-00, REV 97. THE SEAT TRACK WAS REPLACED IAW SRM 51-72-11, REV 97 AND DRAWING F53312813, ISSUE W.SDR HALA2017040900149Seat Track · corrodedSEAT TRACK CORRODED BETWEEN FRAMES 47 +115MM , 47 +185MM , 48, 49, 50 +120MM, AND 51. CORROSION REMOVED IAW SRM 51-74-00, REV 97. FOUND OUT OF LIMITS IAW SRM 53-31-15, REV 97. REPLACED THE SEAT TRACK IAW SRM 51-72-11, REV 97, AND DRAWING F53312812, ISSUE J.SDR HALA2018040900126Seat Track · corrodedDURING H CHECK, SEAT TRACK, FRAMES 47 - 53.2, -Y450 WAS FOUND CORRODED. REPLACED THE SEAT TRACK IAW SRM 51-72-11, AND DRAWING F53334771.SDR HALA2018040900125Seat Track · corrodedDURING H CHECK, SEAT TRACK, FRAMES 47 - 53.2, +Y1959 WAS FOUND CORRODED. REPLACED THE SEAT TRACK IAW SRM 51-72-11, AND DRAWING F53312812.SDR HALA2018040900124Seat Track · corrodedDURING H CHECK, SEAT TRACK, FRAMES 47 - 53.2, +Y450 WAS FOUND CORRODED. REPLACED THE SEAT TRACK IAW SRM 51-72-11, AND DRAWING F53334771.SDR HALA2018040900123Seat Track · corrodedDURING H CHECK, SEAT TRACK, FRAMES 40 - 47, +Y1959 WAS FOUND CORRODED. REPLACED THE SEAT TRACK IAW SRM 51-72-11, AND ER/A 567452-14.SDR HALA2018040900122Seat Track · corrodedDURING H CHECK, SEAT TRACK, FRAMES 53.5 - 54, +Y450 WAS FOUND CORRODED. REPLACED THE SEAT TRACK IAW SRM 51-72-11 AND DRAWING F53326973.SDR HALA2017040900159Seat Track · corrodedSEAT TRACK BETWEEN FRAME 40 AND 47 AT -Y450 IS CORRODED AT LOCATIONS: FR 40.3 - 300MM AFT, FR 43 - 90MM AFT, FR 45 & FR 46 - 170MM AFT AS MARKED. CORROSION REMOVED BY GRINDING AS PER SRM 51-74-00 REV 97. DAMAGE DIMENSIONS: FR40.3 ? 300MM INNER VERT UNABLE TO SDR HALA2017040900158Seat Track · corrodedSEAT TRACK BETWEEN FRAME 37.4 AND 39.2 AT -Y1959 IS CORRODED AT LOCATIONS: FR 38 - 510MM AFT & FR 39 - 90MM AFT. CORROSION REMOVED BY GRINDING AS PER SRM 51-74-00 REV 97. DAMAGE DIMENSIONS: FR38+510MM INNER VERT UNABLE TO FULLY REMOVE CORROSION AND UNABLE TO MSDR HALA2017040900157Seat Track · corrodedSEAT TRACK BETWEEN FRAME 53.2 AND 53.4/53.5 AT -Y450 IS CORRODED AT LOCATIONS: FR 53.2 - 240MM AFT & FR 53.4. CORROSION REMOVED BY GRINDING AS PER SRM 51-74-00 REV 97. DAMAGE DIMENSIONS: FR53.2+240MM INNER VERT L=0.300" W=0.200" DEPTH= UNABLE TO FULLY REMOVE CSDR HALA2017040900156Seat Track · corrodedSEAT TRACK BETWEEN FRAME 58 AND 68 AT -Y450 IS CORRODED AT LOCATIONS: FR59+4", FR60+16", FR61+7", FR62+5", FR63+18", FR65+3", FR66+17".// CORROSION REMOVED BY GRINDING AS PER SRM 51-74-00 REV 97. DAMAGE DIMENSIONS: FR59 + 4? CENTRAL L=1.100? W=0.300? D=0.031?,SDR HALA2017040900155Seat Track · corrodedSEAT TRACK BETWEEN FRAME 55 AND 58 AT -Y450 IS CORRODED AT LOCATIONS: FR54+19", FR56+6", FR57+17". CORROSION REMOVED BY GRINDING AS PER SRM 51-74-00 REV 97. DAMAGE DIMENSIONS: FR54 + 19? INNER VERT UNABLE TO COMPLETELY REMOVE AND MEASURE L=1.000" W=0.200" D= 0SDR HALA2017040900154Seat Track · corrodedSEAT TRACK BETWEEN FRAME 62 AND 72 AT -Y1959 IS CORRODED AT LOCATIONS: FR63+10", FR66+10". CORROSION REMOVED BY GRINDING AS PER SRM 51-74-00 REV 97. DAMAGE DIMENSIONS: FR63+10" SUPERIOR L=0.300" W=0.200" DEPTH 0.033", 2. FR66+10" INNER VERTICAL L=1.200" W=1.00
Back to N386HA