N478HA
Service difficulty reports · 84
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 = 'N478HA' 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 = 'N478HA' 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 ASAA2026021763444Charger · faultedEMERGENCY PWR FAIL. GROUNDED - YES. PER FIM 24-24 TASK 803 RESET BATT CHARGER. MESSAGE CLEARED. OK FOR SVC.SDR ASAA2026011862922Battery · inoperativeOVERWING EMERGENCY LIGHTS INOPERATIVE. GROUNDED - YES. R & R THE EMERGENCY LIGHT BATTERY FOR OVERWING LIGHTS IAW 33-51-06. OPS CHKD GOOD. OK FOR SERVICE.SDR ASAA2025121962452Seal · lack of lubeMAIN CABIN DOOR STICKS WHEN CLOSING. GROUNDED - YES. CLOSED MAIN CABIN DOOR FROM THE OUTSIDE AND INSDIE. FOUND NO FAULTS. APPLIED VASOLINE TO MAIN CABIN DOOR SEAL. OK FOR SERVICE.SDR HALA20250804044Hydraulic System · contaminatedREJECTED T/O 8L DUE TO R HYD HIGH TEMP. UNABLE TO MITIGATE W/ MOVEMENT OF FLT CONTROLS / SPOILERS. PERFORMED FIM 29-30 TASK 803. FOUND EXCESSIVE AIR IN R HYD SYSTEM. BLEEDED AIR FROM SYSTEM AS REQUIRED. OPS CHECK GOOD. FAULT FOUND TO BE INTERMITENT. NO DEFECTSSDR HALA20250630037Warning Message · false activationATB - LEFT GEAR INDICATION RED/UNSAFE WITH GEAR HANDLE UP AFTER TAKE OFF. JACKED UP THE AIRCRAFT PER AMM 07-00-582-811. PERFORMED FUNCTIONAL TEST OF MLG AND NLG EXTENSION AND RETRACTION PER AMM 32-30-00. NO DEFECTS NOTED. PERFORMED SENSOR READOUTS FOR LT AND RSDR HALA20250204003Manifold · failed"DIVERSION TO HNL" TAIL ANTI-ICE MANIFOLD FAILED IN ICING CONDITIONS, FLAP 25 LANDING AS PER QRH. FOUND "PODS SYSTEM FAULT" ON FAULT REVIEW. REMOVED AND REPLACED PODS PER AMM 36-23-01. RTS TEST "PASS". NO FAULTS FOUND. A/C OK FOR SVCSDR HALA20240819040Control Unit · faultedAT 1300FT AUTOPILOT DISCONNECTED, AUTO THROTTLES WENT MAX POWER, ALL DU'S WENT BLANK FOR A SECOND. REMOVED AND REPLACED EPCU PER AMM 24-21-02. EPCU OP CK GOOD. PERFORMED VIA 1 &2 EIS OPS TEST PER AMM 31-61-00-720-801. ALSO PERFORMED AFS TEST ON FCC 1&2 PER AMMSDR HALA20240819039Relay · failedAFTER EPCU DOWNLOAD FOUND EMERGENCY POWER RELAY FAULT ( 54 EPR FAILED CLOSED.). REMOVED AND REPLACED EMERGENCY DC POWER RELAY PER AMM 24-34-05. FUNCTIONAL TEST GOOD PER AMM 24-24-00. OK FOR SERVICESDR HALA2023051200027Unknown · unknownCENTER CABIN OVERHEAD EMERGENCY EXIT LIGHT MOMENTARILY TURNS ON THEN GOES OUT. REPLACED BATTERY B5120 AT ROW 17DEF, PERFORMED OPS TEST OF EMERGENCY LIGHTING SYSTEM IAW AMM 33-51-00, OPS CHK GOOD, OK FOR SVC.SDR HALA2022042000095Pseu · fault messageATB - PSEU FAULT MESSAGE ON CLIMB OUT // REPLACED NLG LOCKED PROXIMITY SENSOR ASSY PER AMM 32-61-03-400-804. OPS CHK OK PER AMM 32-61-00-820-802. (FAULT CODE 326083)SDR HALA2022032100080None · noneATB - DURING CLIMB "SELECT FADEC R ALTN" MESSAGE DISPLAYED YELLOW X ON RIGHT EPR FOLLOWED QRH PROCEDURE. DID NOT RESET // FOUND LTD FAULT CODES 732115 732116ON EEC-2 REF FIM TASK 73-21 TASK 815 STEP E (1) (B) 1) NEED TO REPLACE EEC MECH 15202 03/19/22 REMOVEDSDR HALA2020070100135Pin · out of positionMED SLIDE PINS CAME OUT. REMOVED AND REPLACED MAIN ENTRY DOOR SLIDE PER AMM 25-61-01. OPS AND SECURE CHECKS GOOD.SDR HALA2019071500354Probe · out of limitsATB: ENG R SYS FAIL LIGHT ON RIGHT, TGT GAUGE X THROUGH IT. PER TSM 77-21-803 STEP F4(A) 4(O) MEASURING 8.7 OHMS. STEP K PROBES 6 & 7 OUT OF TOLERANCE 8.2 & 8.3. P1000-J8 CONNECTOR REMOVED. INSTALLED CONNECTOR P1000-J8. #2 ENGINE, NR 6 TGT PROBE INOPERABLE. SDR HALA2019061000286Eec · malfunctionedATB - ENG L SYS FAIL ENROUTE FOLLOWED BY REV L FAULT. PERFORMED EEC1 RTS TEST. TEST FAILED. EEC BOX FAULT. REMOVED & REPLACED EEC1 PER AMM 73-21-01. RTS TEST PASSED. PERFORMED FUNCTIONAL CHECK OK L REV PER AMM 78-30-00-720-801. OPS NORMAL. OK FOR SVC.SDR HALA2019050300216Power Supply · inoperativeEMERGENCY EXIT CEILING LIGHT @ ROW 17 INOP. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY POWER SUPPLY PER AMM 33-51-03. BATTERY POWER SUPPLY (B5-120). OPS. CHECK GOOD, OK FOR SVC.SDR HALA2019042320199Power Supply · inoperativeETOPS SIGNIFICATION - LEFT WING EMERGENCY EXIT LIGHT INOP // REMOVED AND REPLACED EMERGENCY LIGHT BATTERY POWER SUPPLY CONTROL MODULE. PER AMM 33-51-03. OPS CHECK OK. OK FOR SVCSDR HALA2019041500189Manifold · failedATO - TAIL MANF FAIL DURING T/O ROLL. // PER FLIGHT CREW TAIL ANTI ICE WAS NOT ON. FAULT CODE 362164. FOUND WIRE E9142-35-20 BETWEEN RIGHT & LEFT HORIZONTAL SENSORS SHORTED TO SHIELD. FABRICATED WIRE E9142-35-20 AND INSTALLED PER SWPM 20-10-01 AND WDM 36-23SDR HALA2018121000641Static Inverter · malfunctionedCA'S FMS GOES OFF ON APP WHEN EMER PWR ON MESSAGE IS ON.// REMOVE & REPLACE STATIC INVERTER PER AMM 24-24-01. OPS CK OK. REMOVED & REPLACE CAPT MCDU PER AMM 31-65-00. OPS CK OK. OK FOR SERVICE.SDR HALA2018110500560Compressor · damagedHIGH SPEED ABORT DUE TO LEFT ENGINE FAILURE / COMPRESSOR STALL.// FOUND #1 ENG HP COMPRESSOR STAGE 5 TO 6 DAMAGE DURING BORESCOPE. // REMOVED AND REPLACED #1 ENGINE. OPS AND LEAK CHECK OK. OK FOR SERVICE.SDR HALA2018061800285Actuator · malfunctionedHYD RT TEMP CAUTION LIGHT ON WHILE TAXING TO GATE. ACCOMPLISHED FIM 29-30-TASK 803, BLED THE RT HYDRAULIC SYSTEM TEMP ACTUATORS. OK, WITHIN LIMITS, OK FOR SERVICESDR HALA2016040400111Support Fitting · corrodedWING TO BS 832 LOWER END OF SUPPORT FAIRING CORRODED. LT SIDE, ON EXISTENT REPAIR. REMOVED CORROSION AT WING TO BS 832 LOWER END OF SUPPORT FAIRING LT SIDE ON EXISTENT REPAIR, FOUND 100 PERCENT TO BE OUT OF LIMITS IAW SRM 53-00-00 AND R & R PREVIOUS REPAIR ISDR HALA2016032800107Spar · crackedLT WING AFT SPAR CRACKED AT XR 5324 INSIDE OF FUEL TANK ACCESS PANEL 520HB. REPAIRED THE SPAR IAW PRI EA 16126- P1 AND FINAL EA 16126, REV IR AND E105-478280-PERM.SDR HALA2016032300110Fitting · corrodedWING TO BS 832 FITTING ON LONGERON 30 CORRODED. REMOVED CORROSION AT WING TO BODY BS 832 FITTING ON LONGERON 30 ORIGINAL MATERIAL 125" REMAINING .098" AND LOSS OF .027", FOUND OUT OF LIMITS IAW SRM 53-00-00. R & R FITTING IAW DWG 5971098, REV E AND DWG S1440SDR HALA2016032200109Fitting · corrodedLT WING FLAP INBD FLAP TRACK FITTING CORRODED. REMOVED CORROSION ON L/W FLAP INBD FLAP TRACK FITTING EDGE DAMAGED. REMOVED OVER .100, OUT OF LIMITES IAW SRM 57-00-00 R & R FITTING IAW MM-57-55-25.SDR HALA2016032800108Keelbeam · crackedKEELBEAM BARREL BS 696 OTBD END OF FORMER CRACKED. RT SIDE. R & R EXISTING REPAIR DAMAGE, REPAIR AT KEELBEAM BARREL BS 696 OTBD END OF FORMER RT SIDE IAW DW6 9923453 REV C AND T/C E 105-B10214-PERM.SDR HALA2016020300025Fms · malfunctionedAIR TURNBACK. BOTH FMS LOCKED IN STANDBYE F-PLAN MODE. DOWN POWERED ACFT. ACCOMPLISHED VIA 1 & 2 RTS. NO FAULTS NOTED, AMM 31-43-00.SDR HALA2015122400251Fairing · damagedDURING DESCENT, THE PLANE MOMENTARILY OVERSPEED TO 341 KNOTS. PERFORMED OVER SPEED INSPECTION IAW AMM TASK 05-51-05-210-801. NO DAMAGE FOUND IN SKIN OR STRUCTURE. FOUND FAIRING BROKEN ON LT SIDE OF HORIZONTAL STABILIZER. REMOVED HORIZONTAL STABILIZER UPPER SDR HALA2015111500236Girt Bar · unsecureESCAPE SLIDE GIRT BAR HANGING FROM CASING. REINSTALLED ESCAPE SLIDE GIRT BAR IAW AMM25-61-01. SECURITY CHECK GOOD, OK TO CONTINUE SERVICE.SDR HALA2013040600035Tire · failedAIR TURN BACK, NR 1 TIRE FAILURE ON TAKE OFF. R & R NR 1 MLG WHEEL IAW AMM 32-41-01. SPIN CHECK OK. MLG TIRES 2,3,4 CONDITION AND SECURITY CHECKED OK.SDR HALA2012072100181Tire · damagedLEFT MAIN OTBD TIRE DAMAGED. R & R LT MAIN OTBD TIRE IAW AMM 32-41-01.SDR HALA2012011400029Slide · bindingSERVICE DOOR SLIDE UNSAFE, BINDING. R & R SERVICE DOOR SLIDE IAW AMM 25-61-03. SECURITY CHECKED GOOD.SDR HALA2011070400304Indication Sys · malfunctionedUPON GEAR RETRACTION OUT OF DEPARTURE, LT MAIN GEAR RED ( UNSAFE INDICATION) CAME BACK TO DEPARTURE. RETRACTION CHECK IAW MM 32-30-00, LT MAIN GEAR LIGHTS GOOD. SECURITY AND CONDITION OK. ADJUSTMENT AND TEST OF LT-MLG UP LATCH PROX SENSOR GOOD IAW AMM 32-61SDR HALA2011052600230Proximity Sensor · malfunctionedAFTER TAKEOFF WITH THE GEAR HANDLE UP, THE LT MAIN GEAR LIGHT WAS ILLUMINATED RED. WITH THE GEAR HANDLE DOWN, ALL 3 LIGHTS GREEN. TROUBLESHOT IAW SRM 32-61-0 IAW WDM 32-61-00. ADJUSTED DIMENSION "A" OF PROX SENSOR D1-1057 IAW AMM 32-61-00-820-804. DIMENSIOSDR HALA2011052300222Eec · malfunctionedSELECT FADEC ALTN FOR LT ENG DISPLAYED, DID NOT RESET TO NORMAL MODE WHEN CHECKLIST ACCOMP. BITE EEC FAULT 732115/732116. R & R P2/T2 PROBE IAW MM 73-21-05. RTS FAILED. CK GENERATOR/ WIRING IAW WDM 73-23-00. NO DEFECTS NOTED. R & R EEC 1 IAW MM 73-21-01. OSDR HALA2011052200214Proximity Sensor · malfunctionedLT MAIN GEAR UNSAFE LIGHT ILLUMINATED AFTER GEAR RETRACTION. DISCONNECTED D1-1057, LT MLG UPLATCH PROX SENSOR & CLAMPS. REPLACED LT MLG UP & LATCHED PROXIMITY SENSOR ASSY AMM32-61-02. OPS CHECKED GOOD, OPS CHECKED MLG EXTENSION & RETRACTION IAW AMM32-30-00-SDR HALA2010051100209Wire · damagedATB: DURING CLIMB ENG RT SYS FAIL ILLUMINATED. RETURNED HNL PER DISPATCH AND MOC. FOUND FAULT (772263) ACCOMPLISHED FIM 77-22 TASK 803. REPAIRED WIRING AT TURBINE BRG O/H SENSOR. ENG RUN-UP OPS CHECK GOOD.SDR HALA2010042400188Thrust Reverser · malfunctionedAFTER LANDING, ACFT WENT INTO EMERGENCY REVERSE FOR APPROX 5 SECONDS. INSP NR1 & NR2 ENGINES IAW MM 71-00-05. NO DEFECTS NOTED. OK FOR SERVICE.SDR HALA2010033100143Smoke Detector · malfunctionedLAVATORY SMOKE WARNING WILL NOT EXTINGUISH AFTER TESTING. RESET LAV SMOKE DETECTOR. OPS CK GOOD.SDR HALA2010031600118Pin · faultyRETURNED TO HNL, ATB, NOSE GEAR WOULD NOT RETRACT. NOSE GEAR PIN FAULTY. WHEN REMOVED AFTER TOW, PORTION REMAINED IN GEAR LOCK, CLEARED LOCK.SDR HALA2010020800081Floor Support · corrodedLEVEL 2 CORROSION ON FLOOR SUPPORT ANGLE, 3EA SPOTS, BY L-1 ENTRY DOOR BETWEEN STA 160-200. REMOVED CORROSION AT L-1 ENTRY DOOR BETWEEN STA 160-200, IAW SRM 51-10-40. CORROSION FOUND TO BE OUT OF LIMITS, IAW SRM 53-00-00. REMOVED DAMAGE SECTION OF FLOOR SUPPSDR HALA2010020800068Floorbeam · corrodedLEVEL 2 CORROSION ON FWD CABIN FLOOR SUPPORT ANGLE AT STATION 200, RBL 19 TO RBL 31. REMOVED CORROSION AT FWD CABIN FLOOR SUPPORT ANGLE AT STA 200, RBL 19 - RBL 31 PER REF 717 SRM 51-10-04, ORIGINAL MAT THICKNESS .070 INCH, MAT. REMOVED .018 INCH, REMAINING SDR HALA2010020700069Stiffener · gougedSTIFFENER GOUGED AT FWD ENG AT LT W/W HYD SYSTEM SERVICING STATION INTERIOR UPPER. REMOVED STIFFENER AT LT W/W HYD SYSTEM SERVING STATION INTERIOR UPPER SIDE PER REF SPM 51-40-02. FABRICATED NEW STIFFENER PER BOEING DRAWING 5910784. HEAT TREATED STIFFENER FSDR HALA2009122000591Dcu · malfunctionedAFTER TAKEOFF CREW REPORTED MULTIPLE ALERT ILLUMINATED, RUDDER PITOT FAIL, AOA HEAT L/R FAIL, RAT PROBE FAIL. PERFROMED FIM TASK ON AOA HEAT (L) IAW TASK 30-30 TASK 808. AOA HEAT IAW TASK 30-30 TASK 809. RUD PITOT FAIL TASK 30-30 TASK 809. RAT PROBE FAIL SDR HALA2009121600586Pseu · malfunctionedWITH AC CONFIGURED FOR LANDING OUT OF 1000 FT FINAL APPROACH PSEU FAIL FLASHED ON AND OFF SEVERAL TIMES, A/S FAST REF +10, AUTO THROTTLES WENT INTO LO SPEED PROTECT MODE, AND WENT FWD AUTO. REMOVED AND REPLACED PROX SENSE ELEC UNIT IAW AMM 32-41-01. RTS TEST SDR HALA2009101600471Duct · disconnectedWHILE AT FL LEVEL 270, HEARD A BOOM FOLLOWED BY PACK R FLOW DISAGREE ALERT. JUST PRIOR TO LANDING, ALL ALERTS WENT AWAY. FOUND RT A/C PACK DUCT DISLODGED. RECONNECTED A/C DUCT OPS CK GOOD, OK FOR SERVICE.SDR HALA2009052300186Via · failedATB - AIR DATA 1 FAIL, GPWS FAIL, DCU FAIL, VIA FAIL, COLUMN DISC, FCC 1 FAIL, PROBLEM IS UNKNOWN. REPLACED NR 2 VIA GND OPS CHK OK AMM 31-43-01.SDR HALA2009052200186Via · multiple failATB - AIR DATA 1 FAIL, GPWS FAIL, DCU FAIL, VIA FAIL, COLUMN DISC, FCC 1 FAIL, PROBLEM IS UNKNOWN. REPLACED NR 2 VIA GND OPS CHK OK AMM 31-43-01.SDR HALA2009041000138Indicator · malfunctionedATO - ON TAKEOFF LEVEL 3 STAB TRIM IN "RED" ABORT RTN TO RAMP. PERFORMED INSP OF ACFT AFTER HIGH ENERGY RTO STOP IAW AMM 05-53-01. NO DEFECTS NOTED. PERFORMED RTS ON FCC NR 2 PER AMM 22-00-00. ELEVATOR AND STAB TEST PASS. REMOVED AND REPLACED NR 1 VIA PERSDR HALA2009032000095Warning Light · false activationWING ANTI-ICE MANIFOLD FAIL LIGHT ILLUMINATED AT FL220 THEN WENT AWAY AT 6,000. PERFORMED DODS RTS TEST OK. NO FAULTS NOTED. PERFORMED FIM 30-81-00-810-801. NO FAULTS NOTED. OK FOR SERVICE.SDR HALA2009022500066Bearing · damagedIN ORDER TO FLY STRAIGHT AND LEVEL THE AILERON TRIM AND RUDDER TRIM HAD TO BE ALIGNED GREATLY TO THE RIGHT. VISUAL CKS OF A/C FLT CONTROL, CONDITION SECURE CKS OK. NO DEFECTS NOTED. FOUND RT INBD MOVEABLE VANE TRACK SUPPORT BOTTOM BEARING DAMAGED. REMOVED
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