N379HA
Service difficulty reports · 100
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 = 'N379HA' 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 = 'N379HA' 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 HALA2021101100156None · noneSHIP 379 FOUND CORROSION AT SEAT TRACK AT Y1959 FR40-47. CORRECTIVE ACTION: SEAT TRACK REMOVED. HOLES PICKED UP ON NEW SEAT TRACK IAW SRM 51-44-11. NEW SEAT TRACK INSTALLED IAW SRM 51-42-11. BONDING CHECK CARRIED OUT. (1978092)SDR HALA2021101100155None · noneSHIP 379 FOUND CORROSION AT SEAT TRACK AT Y1959 FR47-53.2. CORRECTIVE ACTION: SEAT TRACK REMOVED. HOLES PICKED UP FOR NEW SEAT TRACK IAW SRM 51-44-11. SEAT TRACK INSTALLED IAW SRM 51-42-11. (1978087)SDR HALA2021101100154None · noneSHIP 379 FOUND CORROSION AT SEAT TRACK Y-2462, FR47-FR53.2. CORRECTIVE ACTION: SEAT TRACK REMOVED. HOLES PICKED UP FOR NEW SEAT TRACK IAW SRM 51-44-11. NEW SEAT TRACK INSTALLED IAW SRM 51-42-11. (1978081)SDR HALA2021101100152None · noneSHIP 379 FOUND CORROSION AT SEAT TRACK Y-1959 FR47-FR53.2. CORRECTIVE ACTION: SEAT TRACK REMOVED. HOLES PICKED UP FOR NEW SEAT TRACK. NEW SEAT TRACK INSTALLED IAW SRM 51-42-11. (1978098)SDR HALA2021080200108Sign · detachedSHIP 379 2L EXIT SIGN FELL OFF. CORRECTIVE ACTION: INSTALLED EXIT SIGN. (7721857)SDR HALA2021071200100Warning Message · false activationSHIP 379 1R DOOR UNARMED INDICATION ON 1L PANEL DURING FINAL DESCENT. SELF CLEARED. CORRECTIVE ACTION: PERFORMED BITE OF CIDS. TEST OK. VERIFIED 1R DOOR DAMPENER HAS SUFFICIENT PRESSURE. (5882279)SDR HALA2021061400071Generator · abnormalDUE TO APU GEN FAULT T/S PER TASK 24-20-00-810-986-A. PERFORM RESISTANCE CHECKS PER THIS TSM TO CONFIRM FAULT PER STEP 4A. IF NO TROUBLE IS FOUND IN THE WIRING CHECKS PLEASE REPLACE APU GEN.
ACCOMPLISHED TSM 24-20-00-810-986-A. RESISTANCE CHECK OF APU GEN PMSDR HALA2021042600071Receptacle · shearedSHIP 379 - ATO - ON T.O. ROLL AT 70KTS ECAM, BRAKES RELEASED, BRAKE #4 RELEASED. CORRECTIVE ACTION: FOUND TACH DRIVE SPLINE RECEPTACLE ON HUB CAP #4 TIRE SHEARED. REPLACED WITH NEW HUB CAP. REMOVED AND REPLACED #4 MLG TIRE.SDR HALA2021042200049Brake · malfunctionedATO - BTB- ON T.O. ROLL AT 70KTS ABORT ECAM: BRAKES RELEASED, BRAKE 4 RELEASED // APPLIED MEL 32-42-1 #4 MLG BRAKE DEACTIVATED "M" PROCEDURES C/W. DMI # 518076 A/C OK FOR SVC. MEL & PLACARD INSTALLED.SDR HALA2021011900341Battery Pack · no testWHILE INSTALLING EPSU BATTERIES, EPSU BOX WOULD NOT TEST AT DOOR 1R (12WL). CORRECTIVE ACTION: REMOVED AND REPLACED EPSU BATTERY, PER W/C 3351-4002-HAL. REMOVED 1R AND 4R DOOR SLIDE AND PERFORMED WIRING CHECKS. R & R 1R DOOR SLIDE, PER AMDS CARD 2561-9403. SDR HALA2021011900340Battery Pack · no testWHILE INSTALLING NEW EPSU BATTERIES "PUSH TO TEST" AT 4R DISPLAYED BLINKING INTERIOR & EXTERIOR LIGHTS FAULT (18WL). CORRECTIVE ACTION: REMOVED AND REPLACED EPSU BATTERY, PER W/C 3351-4002 HAL. REMOVED & REPLACED 4R SLIDE, PER AMDS CARD 2561-9403 RII C/W.SDR HALA2020120900217Spline · brokenATO-ON T/O ROLL, AT APPROXIMATELY 80 KIAS, ECAM BRAKES RELEASED. BRAKE 4 RELEASED. PREVIOUS WRITE UP NR 7277029. FOUND TACHOMETER-WHEEL SPEED (14GG2)/BSCU (3GG) ON BSCU SYS TEST. OK TO CONTINUE, PER MEL 32-42-1. NR 4 BRAKE DEACTIVATED W/O BRAKE REMOVAL. SDR HALA2020120800215Spline · brokenATO-ON TO ROLL AT APPROXIMATELY 80 KIAS, ECAM BRAKES RELEASED, BRAKE 4 RELEASED. PREVIOUS WRITE UPS 7277029 AND 7277033 LOG-PAGE UPDATED AT 08DEC20 1031 UTC. PERFORMED TSM 32-40-00-810-929-S. FOUND HUB CAP DRIVE SPLINE BROKEN OFF HUB CAP. REMOVED AND REPLASDR HALA2020111200204Line · leakingETOPS-ON WALK AROUND, FOUND FUEL LEAKING FROM NR 1 ENGINE. FOUND LP FUEL LINE TO DRAINS COLLECTOR TANK CHAFED THROUGH AT A HOSE CLAMP BY FUEL PUMP. REMOVED & REPLACED FUEL LINE SECTION TO DRAIN COLLECTOR TANK. PERFORMED ENGINE IDLE RUN, LEAK CHECK OK.
SDR HALA2020092100185Engine · vibrationENG NR 2 VIB INDICATORS AMBER (X) LOG-PAGE UPDATED AT 18SEP20 2344 UTC. WHILE PERFORMING TSM 73-25-81-810-916-A, REMOVED AND REPLACED NR 2 ENGINE REMOTE CHARGE CONVERTER, PER AMM 77-32-13--400-802-A. OPS CHECK OF INDICATION FAILED. REQUIRES FURTHER TROUBLESSDR HALA2020091430182Generator · out of limitsDURING SERVICE CHECK APU GEN FAULT LIGHT NO OUTPUT POWER FROM APU, RPTD BY CHACON. GENERATOR APU, OFF 33-2423-9-0001 04304 ON 33-2423-9-0001 05088, CHECKS GOOD. VERIFIED NO VF NEEDED PER HAL MOPM, A02(5000VE). REPALCED APU GEN IAW A330 AMM 24-23. OPS AND LSDR HALA2020062200129Actuator · faultedETOPS SIGNIFICANT SYSTEM - APU START FAULT - 3 ATTEMPTS. REMOVED AND INSTALLED SERVICEABLE APU FLAP ACTUATOR PER AMM 49-16-51-000-801-A AND 49-16-51-400-801-A. OPS CHECK GOOD. OK TO CONTINUE.SDR HALA2020060500120Igniter · defectiveETOPS SIGNIFICANT SYSTEM - NR 2 ENG IGN B FAULT/ INOP. PERFORMED AUDIBLE TEST ON IGNITION B SYS PER AMM 74-00. VERY WEAK POPPING. REMOVED & INSTALLED IGNITER PER AMM 74-21 OPS CHECK NORMAL.SDR HALA2020041800091Bleed Valve · malfunctionedETOPS SIGNIFICANT SYSTEM - ECAM "ENG 2 BLEED NOT CLOSED". // REMOVED AND INSTALLED #2 ENG PRV PER AMM 36-11-52-400-804-A.
OPS CHECK LEAK CHECK GOOD PER AMM 36-11-52.SDR HALA2020041800090Bleed Valve · malfunctionedETOPS SIGNIFICANT SYSTEM - ECAM "ENG 1 BLEED NOT CLOSED". // REMOVED NUMBER 1 ENG PRV PER AMM 36-11-57.
INSTALLED NUMBER 1 ENGINE PRV PER AMM 36-11-52, OPS CHECK LEAK CHECK GOOD.SDR HALA2019121700517Warning Message · false activationETOPS SIGNIFICANT SYSTEM - AFTER LANDING ECAM - AIR APU BLEED FAULT. // BMC BITE TEST 1 AND 2 C/OUT IAW AMM 3611-00. SUBSEQUENT OPS
CHECK NOW NORMAL, MSG SELF ERASED.SDR HALA2019100200397Pump · leakingETOPS SIGNIFICANT SYSTEM - NR 1 ENGINE GREEN HYDRAULIC PUMP LEAKING AT THE DRIVE PAD ATTACH POINT AND AT PUMP SPLIT LINE. // REMOVED AND REPLACED #1 GREEN HYDRAULIC PUMP GASKET AND SPLINE SEAL REF A330 AMM 29-11-51. OPS AND LEAK CHECK GOOD. OK FOR SERVICE.SDR HALA201910020396Pump · leakingETOPS SIGNIFICANT SYSTEM - #1 ENGINE GREEN HYDRAULIC PUMP LEAKING AT THE DRIVE PAD ATTACH POINT AND AT PUMP SPLIT LINE. // REMOVED AND REPLACED #1 GREEN HYDRAULIC PUMP GASKET AND SPLINE SEAL REF A330 AMM 29-11-51. OPS AND LEAK CHECK GOOD. OK FOR SERVICE.SDR HALA2019061800302Oil System · lowETOPS SIGNIFICANT SYSTEM - APU OIL SERVICE REQUIRED. APU OIL SERVICE CARRIED OUT. 3 US QTS ADDED. APU AREA INSPECTED. NIL LEAKS FOUND. OIL CAP CONFIRMATION CHECK CARRIED OUT, OK FOR SERVICE.SDR HALA2019061400296Warning Message · false activationETOPS SIGNIFICANT SYSTEM - FUEL FCMC 1 FAULT ILLUMINATED ON DESCENT. // PER INTERROGATED MSG # 285134 SHOWN. FCMC GRD TEST C/OUT REF AMM 28-51-00 ALL INDICATIONS NORMAL TEST OK MSG CLEARED.SDR HALA2019061000284Satcom · faultedETOPS SIGNIFICANT SYSTEM - COM SATCOM FAULT. RESET SITCOM SYSTEM PERFORMED BITE PER AMM 23-28-00 TESTED OK. OK FOR SVCSDR HALA2019031901820Tire · defectiveAIRCRAFT 379 ATO - ABORTED TAKEOFF AT 90-100 KNOTS DUE TO SEVERE NOSE GEAR VIBRATION. CORRECTIVE ACTION: REPLACED LEFT AND RIGHT NOSE TIRES, AND LUBED NOSE GEAR LOWER AREAS. LP 5875735SDR HALA2019031900137Tire · defectiveATO - SEVERE NOSE GEAR VIBRATION. BEGAN APPROX 60 KNOTS. AGGRESSIVELY WORSE W/SPEED. RTO @ 90-100 KTS. T/S IAW TSM 32-20-00-810-801-A DUE TO RTO & RTB. FOUND A HOP ON LT NLG TIRE AFTER JACKING AND SPINNING WHEELS. REMOVED & REPLACED LT & RT NLG TIRE ASSY IAW ASDR HALA2019010700012Oil System · lowETOPS SIGNIFICANT SYSTEM - APU LOW OIL LEVEL ADVISORY. PERFORMED TSM 49-00-00-810-815-A. FOUND APU OIL LEVEL LOW. SERVICED APU PER AMM 12-13-49. NO LEAKS NOTED. OK FOR SVC.SDR HALA2018120400626Packing · leakingATB - HYD B ENG 1 PUMP LO PR HYD B SYS LOW PR ECAM.// BLUE HYD INDICATED 1/4 FULL AT BLOCK IN. CREW REPORTED ENG 1 EDP ISOLATED AFTER MSG. NO CAVITATION TO ENG 1 EDP NOTED, ALL DPI
CHECKED OK. FOUND PACKING ON BLUE HP MANIFOLD LEAKING. REPLACED PACKING PER ASDR HALA2018111900593Indicator · detachedF/CTL FLAPS FAULT ECAM RAN ECAM PERFORMED EMERG LANDING. PER FLT CREW. // T/S PER A330 TSM 27-50-00-810-816A. FOUND OVER TORQUE INDICATOR
RELEASED ON INPUT GEARBOX 5 LH (5053CV). REQUIRES DRAIN AND FILL ROTARY ACTUATOR (5055CV) AND INPUT GEARBOX (5053CV). SDR HALA2018101000488Oil System · lowETOPS SIGNIFICANT SYSTEM - AFTER APU START APU OIL LEVEL MESSAGE APPEARED. OIL SERVICED NOW OK FOR SERVICE. SECOND CHECK OF CAP CARRIED OUT 2 QUARTS UPLIFTED.SDR HALA2018073000352Brake · overheatedIMMEDIATELY AFTER LIFT OFF, BEFORE GEAR UP COMMAND WAS GIVEN, ECAM CAUTION FOR HOT BRAKES DISPLAYED, NR 6 BRAKE TEMP 315, ALL OTHER BRAKES LESS THAN 200. LEFT GEAR EXTENDED UNTIL NR 6 TEMP BELOW 300,THEN RETRACTED GEAR. PUMPED BRAKES, NO BRAKE DRAG, OPS CHECKSDR HALA2018052400246Oxygen Bottle · defectiveOPEN - LAV F/L81 FLIGHT ATTENDANTS REPORTED "POPPING, RATTLING" SOUND FROM OXYGEN MASK COMPARTMENT AND AN UNFAMILIAR ODOR. SUSPECT
O2 MASK DISCHARGE.REMOVED & REPLACED EMERGENCY OXYGEN CONTAINER IN LAV F PER AMM 35-21-41. OPS CHECK OK. OK FOR SVC.SDR HALA2018040200132Oil System · lowAPU HIGH OIL UPLIFT / OIL ADD EXCEEDANCE FLAG AT APU OIL ENTRY DURING A SERVICE CHECK. ADDED 2 QTS OF OIL AT SERVICE CHECK. VERIFIED OIL FILLER CAP O-RING SERVICEABLE. RAN APU FOR 5+ MINUTES IAW AMM 49-00 & COMPLIED WITH A VISUAL LEAK INSPECTION DURING & AFSDR HALA2018032900129Actuator · malfunctionedNR 2 ENG FUEL LP VALVE FAULT ECAM MESSAGE ILLUMINATED TWICE, SHORTLY AFTER TOP OF CLIMB. MESSAGE CLEARED BOTH TIMES. NO ECAM MESSAGE SHOWED ON ARRIVAL. MESSAGE 282451, CLASS 1, HARD, NR 2 ENGINE LP VALVE, SFCC 1,SHOWED ON PFR. FOLLOWED TSM 28-24-00-810-8SDR HALA2018032700125Damper · brokenCAPTAIN`S CONTROL STICK, SEEMS TO HAVE DECREASED CONTROL FEEL WHEN APPLYING LT AILERON VS APPLYING RT AILERON. FIRST OFFICER`S STICK HAD NORMAL FEEL. REMOVED THE CAPTAIN`S STICK IAW AMM 27-92-41. THE INTERNAL DAMPENER FOUND BROKEN. REPLACED THE CAPTAIN`SSDR HALA2018021200038Unknown · smokeON LANDING, & ROLLOUT, TOWER ADVISED SMOKE COMING FROM THE MAIN LANDING GEAR AREA LEFT SIDE. INSPECTED, AND FOUND OK. TAXIED TO GATE, OPS NORMAL. INSPECTED THE LT MLG TIRES AND BRAKES. NO DEFECTS NOTED. CONDITION AND SECURITY CHECKED OK.SDR HALA2017122700323Transfer Sys · malfunctioned500 LBS OF FUEL IN CENTER TANK DID NOT FEED. ON PFR, FOUND MESSAGE FCMC 1, RESET AND SYSTEM TEST OF FCMC AND FUEL VALVES TEST PERFORMED IAW AMM 28-51-00-740-801A, AND 28-51-00-710-801A, BOTH TESTS PASSED. OK FOR SERVICE.SDR HALA2017122200313Warning Message · illuminatedECAM FAULT, FUEL FCMC 2 FAULT. RESET FCMC 2, AND MESSGAE CLEARED. PERFORMED SYSTEM TEST IAW AMM 28-51-00-740-801-A. TEST PASSED, OK FOR SERVICE.SDR HALA2017121800301Unknown · odorDURING PRE FLIGHT F/A NOTED A FAINT BURNING ODOR IN THE LDCRM. INSPECTED LDCRM FOR THE ODOR. NO SMOKE ODOR DETECTED. OK FOR SERVICE.SDR HALA2017111700260Sign · brokenEXIT SIGN AT SEAT 37L BROKEN, RE-SECURED EXIT SIGN.SDR HALA2017053100134Warning Message · unknownENROUTE, BOTH FMGEC -EFOB ON F-PLN PAGE BEGAN TO FLUCTUATES REGULARLY BY AS MUCH AS 2000 LBS. FUEL BURN NORMAL. INDICATIONS CAUSED REFILE OF ALTERNATE AIRPORT FOR EFOB CALCULATIONS. PFMD VIS FUEL LEAK FROM TKS AND ENGS -NO FUEL LEAK FOUND. PFMD AFS TEST SHOWSSDR HALA2017031700071Idg · lowETOPS SIGNIFICANT SYSTEM - IDG 2 SYS FAULT. SERVICED NR 2 IDG AND PERFORMED BITE TEST OF THE ELECTRIC POWER GEN
SYS (EPGS) AND GCU AND GAPCU PER TASK AMM 24-41-00 OPS CHECK GOOD. OK FOR SVC. BITE TEST PASSED.SDR HALA2017020200018Wire · misinstalledOVERHEAD EMERGENCY LIGHT INOPERATIVE AT SEAT 26GE. FOUND WIRES WERE CROSSED. PUT WIRES IN THE CORRECT POSITION. LP 8983037SDR HALA2017020100021Light · inoperativeOVERHEAD EMERGENCY LIGHT INOP AT 26GE. OK TO CONTINUE PER MEL 33-51-1A.SDR HALA2016122300220O-Ring · failedRETURNED TO DEPARTURE DUE TO THE LOSS OF YELLOW HYDRAULIC QUANTITY. REPLACED YELLOW SYSTEM HP MANIFOLD O-RING.SDR HALA2016122300557O-Ring · leakingDURING CRUISE, LOST YELLOW HYD QUANTITY ATB. FOUND O-RING ON YELLOW SYSTEM HP MANIFOLD BLOWN OUT FROM FITTING. REMOVED AND REPLACED ORING. OPS TEST OF YELLOW HYD SYSTEM PER AMM 29-13-00-00-710-801-A. NO LEAKS NOTED OPS CHECK OK. SVC HYD SYSTEM. OK FOR SERSDR HALA2016102100373Bolt · missingNR 4 MAIN TIRE TIE BOLT MISSING. REMOVED AND REPLACED THE NR 4 MAIN TIRE AND WHEEL ASSY IAW AMM 32-41. OK FOR SERVICE.SDR HALA2016052700130Skin · dentedDURING WALK AROUND, A DENT WAS FOUND ON THE LEFT NR 1 SLAT TOP SKIN LOCATED AT WFX 6584 COMMON TO THE FREE EDGE DUE TO A BIRD STRIKE. DENT MEASURED 2.35" X 1.75" AND .250" DEEP. PERMANENT REPAIR IAW SRM 57-40-00 FIG 222 AND ER/A 547433-14.
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