N584HA, cancelled Dec 17, 2013

Service difficulty reports · 215

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 = 'N584HA' AND deregistration_id = 'N584HA-2013-12-17'
  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.

SDR HALA2013021200018Connector · brokenAT DEPARTURE TIME CREW REPORTS MID GALLEY EMERGENCY LIGHTING FLOOR STRIP LT SIDE CONNECTOR BROKE LOOSE. RESECURED MID GALLEY EMERGENCY LIGHT FLOOR STRIP WIRES. OPS CK OK IAW AMM 33-51-00.Feb 12, 2013 · N584HA · Boeing 7673G5 · Light System WiringSDR HALA2012091700208Warning Light · false activationNR 1 ENGINE AND APU FIRE LOOP SHOWED EICAS MESSAGE NO TEST. PERFORMED ENG AND APU FIRE LOOP TEST IAW FIM 26-15 FIG 803 & 804. OPS CHECKED GOOD, NO FAULTS NOTED.Sep 17, 2012 · N584HA · Boeing 7673G5 · Fire DetectionSDR HALA2012071800176Relief Valve · leakingRIGHT FUEL TANK QUANTITY DECREASED 1500 LBS DURING CLIMB WHILE BOTH CENTER TANK PUMPS ARE ON AND OPERATING. FOUND PRESSURE RELIEF VALVE LEAKING. REPLACED PRESSURE RELIEF VALVE IAW AMM 28-21-08. OK TO CLOSE RT MAIN TANK ACCESS DOOR 541HB. LEAK CHECK OF PANELJul 18, 2012 · N584HA · Boeing 7673G5 · Fuel Controlling SystemSDR HALA2012071000170Bypass Valve · leakingAPU AUTO SHUTDOWN AT GATE. BITE APU IAW FIM HIGH OIL TEMP FAULT IAW FIM 49-11-00, FIG 110. NO OTHER FAULTS FOUND. IAW FIM REPLACED OIL COOLER BYPASS VALVE IAW AMM 49-27-10. LEAK CHECKED FAILED. REPLACED OIL COOLER BYPASS VALVE WITH ANOTHER NEW VALVE LEAKJul 10, 2012 · N584HA · Boeing 7673G5 · APU Oil SystemSDR HALA2012070200166Starter · seizedNR 2 ENGINE WOULD NOT START, NO N1 OR OIL PRESSURE NOTED. PNEU PRESSURE WAS NORMAL & START VALVE OPENED AND CLOSE NORMAL. FOUND NR 2 ENGINE STARTER SEIZED. R & R NR 2 ENGINE STARTER IAW AMM 80-11-01. NR 2 ENGINE START, OPS GOOD. ALL ENGINE INDICATIONS NORMJul 2, 2012 · N584HA · Boeing 7673CB · Engine StarterSDR HALA2012070200165Coupling · shearedRT ENGINE STARTER TO GEARBOX COUPLING SHEARED. R & R STARTER DRIVE COUPLING IAW AMM 72-61-09.Jul 2, 2012 · N584HA · Boeing 7673G5 · Engine StarterSDR HALA2012060500159Warning Light · false activationRT ENG BLEED OFF EICAS AND LIGHT APPEARED TWICE DURING FLIGHT. FIRST DURING CLIMB FOR 30 SECONDS, SECOND DURING CRUISE DESCENT FOR 10-15 SECONDS. RAN NR NR 2 ENGINE IAW AMM 71-00-00. NO FAULTS OR ABNORMALITIES NOTED. OPS CHECKED GOOD. NO FAULTS NOTED ON AIJun 5, 2012 · N584HA · Boeing 7673G5 · Pneumatic SystemSDR HALA2012042900127Sensor · openCLIMBING THROUGH 9,000' RECEIVED "RT FWD WINDOW" LIGHT AND INOPERATIVE LIGHT ON, FOLLOWED QRH. LIGHT STAYED ON, RETURNED TO DEPARTURE. ACCOMPLISHED FIM 30-41-00/101, FIG 104, FOUND 1R WINDOW MAIN SENSOR OPEN CIRCUIT. SWAPPED TO SPARE WINDOW SENSOR IAW AMM 3Apr 29, 2012 · N584HA · Boeing 7673G5 · Windshield/Door Rain/Ice RemovalSDR HALA2012042900126Control Unit · malfunctionedCLIMBING THROUGH APPROX 25,000' RECEIVED RT FWD WINDOW EICAS MESSAGE AND INOPERATIVE LIGHT ON THE RT FWD WINDOW LIGHT SWITCH. FOLLOWED QRH. LIGHT STAYED ON. RETURNED TO DEPARTURE. ACCOMPLISHED FIM 30-41-00, FIG 104. NO FAULTS NOTED. 1R WINDOW HEATER AND Apr 29, 2012 · N584HA · Boeing 7673G5 · Windshield/Door Rain/Ice RemovalSDR HALA2012021800126Control Unit · malfunctionedCLIMBING THROUGH APPROX 25,000', RECEIVED RT FWD WINDOW EICAS MESSAGE AND INOPERATIVE LIGHT ON THE RT FWD WINDOW LIGHT SWITCH. FOLLOWED QRH. LIGHT STAYED ON. ACCOMPLISHED FIM 30-41-00, FIG 104. NO FAULTS NOTED. 1R WINDOW HEATER AND SENSOR RESISTANCE CHECKApr 29, 2012 · N584HA · Boeing 7673G5 · Windshield/Door Rain/Ice RemovalSDR HALA2012031800113Connector · unsecureON OVERNIGHT CHECK, FOUND EMERGENCY FLOOR LIGHTING BETWEEN L1 & R1 DOOR INOPERATIVE. RECONNECTED AND RESECURED LOOSE EMERGENCY FLOOR LIGHT CONNECTOR. OPS CHECKED IAW AMM 33-51-00.Mar 18, 2012 · N584HA · Boeing 7673G5 · Light System WiringSDR HALA2012022600081Warning Message · false activationLEFT PACK TEMPERATURE EICAS MESSAGE. LT PACK INOP ON OVERHEAD MULTIPLE TIMES AT 5 SECS EACH TIME, SELECTED STANDBY IAW QRH. BITE CHECKED LT PACK CONTROLLER, NO FAULTS. RAN PACK AND OPS CHECKED GOOD.Feb 26, 2012 · N584HA · Boeing 7673G5 · Cabin Cooling SystemSDR HALA2012011900045Engine · malfunctionedETOPS SIGNIFICANT SYSTEM - LEFT ENGINE STARTED NORMALLY TILL 50 PERCENT, THEN REMAINED AT 50 PERCENT FOR 50 SECOUNDS BEFORE SLOWLY ACCELERATING - TOTAL TIME FROM FUEL ON TILL ENGINE STABLE TOOK 110 SECONDS, PEAK TEMP EGT WAS 397. TROUBLESHOT IAW FIM 73-21-00/Jan 19, 2012 · N584HA · Boeing 7673G5 · Engine (Turbine/Turboprop)SDR HALA2012011700041Generator · malfunctionedETOPS SIGNIFICANT SYS - GENERATOR FIELD MANUAL RESET (RT) FIELD OFF LIGHT ON. BITE CHECKED BPCU AND NO FAULTS NOTED. RAN NR 2 ENGINE RESET NR 2 GENERATOR. OPS CHECKED OK IAW 24-20-00, OK FOR SERVICE.Jan 17, 2012 · N584HA · Boeing 7673G5 · AC Generator-AlternatorSDR HALA2012011600035Display · malfunctionedETOPS SIGNIFICANT SYS - F/O RADAR SCREEN FLICKERS IN WX MODE. REPLACED F/O EMSI DISPLAY. OPS CHECKED OK IAW MM 34-22-00. PERFORMED MCDP TEST 30 TEST PASSED.Jan 16, 2012 · N584HA · Boeing 7673G5 · Independent Position Determining SystemSDR HALA2012011500036Transceiver · failedETOPS SIGNIFICANT SYS - AMBER RADAR ALITMETER WARNING BOX ILLUMINATED ON FO ADI " NO LAND 3" APPEARS IN AUTOLAND STATUS. REPLACED RT RADIO ALTIMETER TRANSCEIVER, NOW OPS NORMAL IAW MM 34-33-01. OK FOR SERVICE.Jan 15, 2012 · N584HA · Boeing 7673G5 · Ground Proximity SystemSDR HALA2012011300024Warning Light · illuminatedETOPS SIGNIFICANT SYS - ON POST FLIGHT FOUND ENGINE NR 2 GENERATOR FIELD OFF LIGHT ILLUMINATED. ACCOMPLISHED BPCU BITE CHECK IAW AMM 24-22-00-745-071. RERACKED GCU. RESET RT GENERATOR FIELD LIGHT. RT ENGINE GROUND RUN-UP OK. SYS VOLTAGE AND FREQUENCY NORMAJan 13, 2012 · N584HA · Boeing 7673G5 · DC Generating SystemSDR HALA2012011100018Gcu · failedETOPS SIGNIFICANT SYS - FOUND RT GENERATOR FIELD LIGHT ILLUMINATED ON P61. SERVICED IDG RESET FIELD LIGHT IAW AMM 24-22-00. PERFORMED IDLE ENGINE RUN. FAULT DID NOT RETURN. DUE TO HISTORY, REPLACED RT GCU IAW AMM 24-22-02. TESTED OK IAW AMM. OK FOR SERVICE.Jan 11, 2012 · N584HA · Boeing 7673G5 · AC Generation SystemSDR HALA2012010100002Warning Light · illuminatedETOPS SIGNIFICANT SYS - EICAS MESSAGE TRACK FAIL ILLUMINATED AFTER TAKEOFF. PERFORMED TROUBLESHOOTING, PLACED IECAS COMPUTER SELECTED SWITCH TO ALTERNATE POSITION, OPENED AND RESET CIRCUIT BREAKER TO EICAS COMPUTER. ALL CHECKED GOOD.Jan 1, 2012 · N584HA · Boeing 7673G5 · Attitude and Direction Data SystemSDR HALA2011122600618Warning Light · false activationETOPS SIGNIFICANT SYS - AFTER ENGINE SHUTDOWN, NOTE GENERATOR FIELD TRIP ON RT ENG. ACCOMPLISHED FIM 24-20-00. NO FAULTS NOTED. RESET RT GEN FIELD SWITCH. GROUND RUN CHECK OK IAW AMM 24-11-00. OK FOR SERVICE.Dec 26, 2011 · N584HA · Boeing 7673G5 · AC Generator-AlternatorSDR HALA2011122500611Warning Light · false activationETOPS SIGNIFICANT SYS - AUX PANEL HAS GENERATOR FIELD OFF INDICATOR ON AFTER LANDING. PERFORMED BPCU BITE ON NR 2 BPCE IAW FIM 24-20-00, FIG 101. INSPECTED WIRING, NO DEFECTS NOTED. RESET FIELD OFF LIGHT, OPS NORMAL ON ENG RUN UP.Dec 25, 2011 · N584HA · Boeing 7673G5 · AC Generator-AlternatorSDR HALA2011122200606Sensor · out of positionON TAXI OUT LT FWD ENTRY DOOR, EICAS AND ENTRY DOORS WARNING LIGHT ILLUMINATED. UPON BEING TUGGED IN LIGHT WENT OUT BY ITSELF. FOUND LT FWD ENTRY DOOR OPEN SENSOR BINDING. REPOSITIONED SENSOR. SECURITY CHECK AND OPS CHECK OK. OK FOR SERVICE.Dec 22, 2011 · N584HA · Boeing 7673G5 · Door Warning SystemSDR HALA2011120200596Support Channel · corrodedINTERNAL SUPPORT CHANNEL CORRODED, BS 1425 AT DRAIN MAST FOR WASTE WATER. FITTED NEW SKIN STIFFENER IAW SRM 53-00-03.Dec 2, 2011 · N584HA · Boeing 7673G5 · Fuselage Internal Mounting StructureSDR HALA2011120200581Floor Support · crackedFLOOR SUPPORT CRACKED 1 INCH, BETWEEN BS 742 AND 764 AT RBL 40. REPLACED FLOOR SUPPORT IAW SRM 51-40-02, D634T210, REV 87.Dec 2, 2011 · N584HA · Boeing 7673G5 · Fuselage Miscellaneous StructureSDR HALA2011120100584Floorbeam · corrodedAFT CARGO HOLD, FLOOR STRUCTURE, UPPER HORIZONTAL FLANGE A FRAME STA 1197+66, HAS CORROSION OUTSIDE SRM LIMITS AND NUMEROUS CORRODED ANCHOR NUTS. INNER CHORD PN 146T1060-2, REPLACED IAW SRM 51-40-02, REV 87, CORRODED ANCHOR NUTS REPLACED IAW SRM 51-40-02, REVDec 1, 2011 · N584HA · Boeing 7673G5 · Fuselage Main, Floor BeamSDR HALA2011113000583Floorbeam · corrodedNET CARGO FLOOR STRUCTURE, UPPER HORIZONTAL FLANGE AT BS 1175, HAS CORROSION AS MARKED. REPLACED IAW SRM 51-40-02, REV 87.Nov 30, 2011 · N584HA · Boeing 7673G5 · Fuselage Main, Floor BeamSDR ANZY20111120102Stringer · corrodedON C CHECK, CORROSION OF STRINGER AT S34R HAD CAUSED MULTIPLE HOLES IN EXTRUSION TO THE POINT THAT NO STRUTURAL MATERIAL WAS LEFT. REPAIR UNDER WAY AT THIS TIME.Nov 30, 2011 · N584HA · Boeing 7673G5 · Fuselage Main, Longeron/StringerSDR HALA2011112900597Mechanism · corrodedNLG FWD DOOR OPERATING MECHANISM FOUND CORRODED BS 180.5. REPLACED NLG FWD DOOR OPERATING MECHANISM ON LT SIDE IAW AMM 32-22-04, REV 77.Nov 29, 2011 · N584HA · Boeing 7673G5 · Landing Gear Door Retract SectionSDR HALA2011112900580Stringer Clip · crackedCRACK IN STRINGER CLIP AT STA. 1678, S3R, 1". REPLACED STRINGER CLIP IAW SRM 51-40-02.Nov 29, 2011 · N584HA · Boeing 7673G5 · Fuselage Main, Attach FittingsSDR HALA2011112800602Seat Track · corrodedSEAT TRACK FOUND CORRODED AT RBL 88.5 AT STA 605. REPLACED SEAT TRACK IAW SRM 53-00-52, REV 87.Nov 28, 2011 · N584HA · Boeing 7673G5 · Fuselage, Seat/Cargo Attach FittingsSDR HALA2011112800600Seat Track · corrodedSEAT TRACK FOUND CORRODED AT RBL 88.5 AT STA 594. REPLACED SEAT TRACK IAW SRM 53-00-52, REV 87.Nov 28, 2011 · N584HA · Boeing 7673G5 · Fuselage, Seat/Cargo Attach FittingsSDR HALA2011112800601Seat Track · corrodedSEAT TRACK FOUND CORRODED AT RBL 88.5 AT STA 594. REPLACED SEAT TRACK IAW SRM 53-00-52, REV 87.Nov 28, 2011 · N584HA · Boeing 7673G5 · Fuselage, Seat/Cargo Attach FittingsSDR HALA2011128000600Seat Track · corrodedSEAT TRACK FOUND CORRODED AT RBL 88.5 AT STA 575. REPLACED SEAT TRACK IAW SRM 53-00-52, REV 87.Nov 28, 2011 · N584HA · Boeing 7673G5 · Fuselage, Seat/Cargo Attach FittingsSDR HALA2011112800599Seat Track · corrodedSEAT TRACK FOUND CORRODED AT RBL 88.5, AT STA. 565. REPLACED SEAT TRACK IAW SRM 53-00-52, REV 87.Nov 28, 2011 · N584HA · Boeing 7673G5 · Fuselage, Seat/Cargo Attach FittingsSDR HALA2011112800598Seat Track · corrodedSEAT TRACK FOUND CORRODED AT RBL 88.5 AT BS 544. REPLACED SEAT TRACK IAW 53-00-52-REV 87.Nov 28, 2011 · N584HA · Boeing 7673G5 · Fuselage, Seat/Cargo Attach FittingsSDR HALA2011112800592Wedge · debondedNR 8 SLAT OTBD END HAS A T/E WEDGE AREA OF DISBOND. REPAIRED IAW SRM 57-43-02-2R-1, REV 87 AND 51-70-10, REV 87.Nov 28, 2011 · N584HA · Boeing 7673G5 · Leading Edge DevicesSDR HALA2011112800591Skin · damagedLIGHTING STRIKE NEAR RIVET HEAD AT BS 395, 1 INCH BELOW S33L. DAMAGE REMOVED IAW SRM 53-00-01-2R-8 REV 88. FASTENER REPLACED IAW SRM 51-40-02, REV 88.Nov 28, 2011 · N584HA · Boeing 7673G5 · Fuselage Main, Plate/SkinSDR HALA2011112800582Tee Fitting · corrodedCORROSION ON TEE FITTING BETWEEN STA 808 & 933, BETWEEN RBL 10 & LBL 10. REPLACED TEE FITTING IAW SRM 51-40-02.Nov 28, 2011 · N584HA · Boeing 7673G5 · Fuselage Miscellaneous StructureSDR HALA2011113000512Engine · malfunctionedETOPS SIGNIFICANT SYS - LEFT ENGINE HESITATED AT 50 PERCENT N2 DURING ENGINE START AFTER START VALVE CLOSED AND STARTER CUTOUT WITH SELECTOR BACK IN AUTO. OTHER PARAMETERS NORMAL. GROUND RAN LT ENGINE, FOUND WITHIN LIMITS OF AMM 71-00-00. OK FOR SERVICE.Nov 13, 2011 · N584HA · Boeing 7673G5 · Engine (Turbine/Turboprop)SDR HALA2011110100500Unknown · unknownETOPS SIGNIFICANT SYS - HF DATALINK INOPERATIVE BOTH RADIOS, VOICE OK. PERFORMED A BITE TEST ON BOTH HF TRANSCEIVERS, NO FAULTS NOTED. PERFORMED A SYS TEST IAW 23-11-00-735-042, ALL CHECKED ARE GOOD.Nov 1, 2011 · N584HA · Boeing 7673G5 · VHF Communications SystemSDR HALA2011102300484Warning System · false activationETOPS SIGNIFICANT SYS - EICAS STATUS MESSAGE LT ENG EEC C1 DISPLAYED ON LOWER EICAS. TROUBLE SHOT IAW FIM 73-21-00. PIMU CHECKED AND HAD RNG FAIL-CLEARED MESSAGE. RAN ENGINE, NO FAULTS ON PIMU OR EICAS-OK FOR SERVICE.Oct 23, 2011 · N584HA · Boeing 7673G5 · Central WarningSDR HALA2011102300483Fuel Sys · malfunctionedETOPS SIGNIFICANT SYS - RT FUEL QTY DECREASED 2800 WITH CENTER TANK PUMPS ON. ELAPSED TIME 42MINS. DECREASED AN ADDITIONAL 600 NR DURING THE NEXT 56 MINS. W/C. TANK PUMPS ON. TOTALIZER INDICATED 2400 MORE THAN CALCULATED INDICATION ON FMS PROG. PAGE 2. PERFOct 23, 2011 · N584HA · Boeing 7673G5 · Fuel Quantity IndicatorSDR HALA2011100900441Overheat Sys · malfunctionedETOPS SIGNIFICANT SYS - FOUND LEFT ENGINE OVERHEAT LOOP 2 STATUS MESSAGE ON ETOPS CHECK. ACCOMPLISHED FIM 26-11-00, FIG 104. SWAPPED LT ENGINE O/H CARDS, RERACKED AND REINSTALLED IN ORIGINAL POSITION. FAULT MESSAGE CLEARED AND LT ENGINE O/H DETECTION TEST COct 9, 2011 · N584HA · Boeing 7673G5 · Overheat DetectionSDR HALA2011100600434Indicator · inoperativeETOPS SIGNIFICANT SYS -CAPTS ALTIMETER OFF FLAG FLICKERS CONTINUOUSLY. REPLACED CAPT ALTIMETER INDICATOR IAW AMM 34-13-01-404-004, TEST GOOD.Oct 6, 2011 · N584HA · Boeing 7673G5 · Altimeter, Barometric/EncoderSDR HALA2011091700405Oil System · leakingETOPS SIGNIFICANT SYS - OIL FOUND IN LT ENGINE FAN COWL. OIL LEAKAGE BELOW IDLE SPEED IS WITHIN LIMITS IAW AMM 71-00-00-795-003-N00. OK FOR SERVICE.Sep 17, 2011 · N584HA · Boeing 7673G5 · Turbine Engine Oil SystemSDR HALA2011082100377Apu · malfunctionedETOPS SIGNIFICANT SYS - AFTER TURNING OFF THE LT PACK AT THE GATE APU AUTO SHUTDOWN NOTE: JUST BEFORE SHUTDOWN APU BLEED DUCT PRESSURE DROPPED TO APPROX 10 PSI. PERFORMED APU ECU BITE IAW FIM 49-11-00. FAULT MSG SHOWED REVERSE FLOW, RESTARTED APU AND NO DEFEAug 21, 2011 · N584HA · Boeing 7673G5 · Airborne Auxiliary Power Unit (APU) SystemSDR HALA2011081900379Duct · damagedETOPS SIGNIFICANT SYS - 2 FLEXIBLE DUCT SEGMENTS ON THE APU OVER PRESSURE VENT DUCT HAVE HOLES IN THEM. R & R 2 FLEXIBLE DUCT SEGMENTS ON THE APU OVERPRESSURE VENT DUCT. OPS NORMAL IAW AMM 49-00.Aug 19, 2011 · N584HA · Boeing 7673G5 · APU Bleed Air SystemSDR HALA2011081600371Transmitter · malfunctionedETOPS SIGNIFICANT SYS - ASA NO LAND 3 DISPLAYED CENTER RADIO ALTIMETER. RA FLAG DISPLAYED FROM T/O TO CRUISE ALT, THEN RESUMED NORMAL OPS. R & R RADIO ALTIMETER TRANSMITTER IAW 34-33-01-004-001. OPS TEST GOOD. -40 TEST REQUIRED. GROUND TEST OF AUTO LAND SYAug 16, 2011 · N584HA · Boeing 7673G5 · Altimeter, Barometric/EncoderSDR HALA2011081400365B-Nut · looseETOPS SIGNIFICANT SYS - NR 1 ENG TOOK 6 PINT DURING SERVICING. TIGHTENED OIL INLET TUBE B-NUT IAW 79-21-01, LEAK CHECKED GOOD. (AT OIL COOLER) (ACFT M/M 79-21-011).Aug 14, 2011 · N584HA · Boeing 7673G5 · Turbine Engine Oil SystemSDR HALA2011080400348Flex Line · leakingC-HYD QTY DECREASED TO 0.58 IN FLIGHT, 0.40 ON GROUND. REPLACED NR 4 BRAKE FLEX LINE ABOVE RT MLG IAW AMM 32-42-02. REF IPC 32-41-62-05, ITEM 172. LEAK AND OPS CK GOOD. RESERVICED CTR HYD SYS.Aug 4, 2011 · N584HA · Boeing 7673G5 · Hydraulic System, Main
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