N393HA
Service difficulty reports · 185
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 = 'N393HA' 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 = 'N393HA' 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 HALA2023051100175Unknown · unknownSHIP 393 DURING CCK AT SIAEC (SIN), THE LHW RIB 6 FITTING FWD AND AFT BORES WERE FOUND CORRODED. NEW BUSHES WERE MANUFACTURED AND INSTALLED. THIS WAS COMPLETED IAW REFERENCE REPAIR INSTRUCTIONS (R575-58471 ISSUE E)SDR HALA2023051100174Unknown · unknownDURING C CK, THE RHW RIB 6 FITTING FWD LUG WAS FOUND CORRODED. RH WING MLG RIB 6 FWD LUG, FWD SPT FACE FOUND CORROSION BEYOND WORK CARD, TO CARRY OUT CORROSION REMOVAL. CORRECTIVE ACTION: NEW OVERSIZE BUSHES WERE MANUFACTURED AND INSTALLED IN ACCORDANCE WITH RSDR HALA2023020300029Not Reported · not reportedSHIP 393 FLOOR STRIP PANEL IN F/C FRONTING STOWAGE F104 & F105 IS DEFECTIVE (PEELING OFF). CORRECTIVE ACTION: RESECURED FLOOR STRIP AT F/C AREA. (9792680)SDR HALA2023051000173Unknown · unknownSHIP 393 HAL 393 EXPERIENCED SEVERE TURBULENCE EVENT WHICH CAUSED DAMAGE TO THE WALLS AND CEILINGS OF LAV H (L53) AND LAV V (L81) (REFERENCE ER/A 605060-14 FOR TIME LIMITED REPAIRS). THE OEM FOR BOTH DISCREPANT LAVATORIES IS DIEHL AVIATION. DIEHL PROVIDED TN-TSDR HALA2022101300330Deu · inoperativeSHIP 393 2L CABIN PRESSURE LIGHT INOP DUE TO DEU B INOP AT 2L STATION. OK TO CONTINUE PER MEL 52-71-1H. CORRECTIVE ACTION: REMOVED AND REPLACED DEU B FIN (300RH3) PER AMM 23-73-47. (9752241)SDR HALA2022092700295None · noneSHIP 393 - ATB - THS WHEEL MOVES ERRATICALLY AND FAST WHEN AUTOPILOT IS ON. WHEN AUTOPILOT IS OFF, TRIM FEELS NORMAL. CORRECTIVE ACTION: "FCPC 1 (2EC1) PITCH TRIM ACT (1CS) OVERRIDE SWITCH" FAULT ON PFR. T/S. REMOVED AND REPLACED PITCH TRIM ACTUATOR. OPS CHECKSDR HALA2022081800148None · noneETOPS - PER MOC GVI OF APU COMPARTMENT NEEDED DUE TO OIL SMELL, REF LOG PAGE 7732245 & 7732248. CHECK FOUND OIL LEAKING FROM FWD DRAIN MAST. REPLACED SEAL BETWEEN FUEL CONTROL UNIT AND OIL PUMP UNIT. LEAK CHECK OK. OK FOR SERVICE.SDR HALA2022080200244None · noneSHIP 393 2L DOOR SLIDE PRESSURE IN YELLOW ZONE. CORRECTIVE ACTION: OPERATED DOOR AND ARMED SLIDE. COULD NOT DUPLICATE FAULT. (9335902)SDR HALA2022060800221None · noneSHIP 393 1L DOOR INTERMITTENT. CORRECTIVE ACTION: NO LAST LEG FAULTS OR CURRENT FAULTS ON PSCU. 1L DOOR OPERATION/ INDICATION OK. (9317657)SDR HALA2022030700069None · noneETOPS - FUEL R STBY PUMP CB A11 TRIPPED// REMOVED AND REPLACED RH FUEL STBY PUMP PER AMM 28-21-51. LEAK CHECK OK. OPS CHCEK GOOD. PUMP, FUEL, AD; OFF 33-2822-9-0007 S/N 05409 ON 33-2821-9-0003 S/N 03972SDR HALA2022020100036None · noneNEED TO REPLACE EEC DUE TO MCC REQUEST (MULTIPLE MINOR FAULTS) #1 ENGINE // REMOVED AND REPLACED #1 ENGINE EEC PER AMM 73-21-34 AWAITING CAT 3 AUTOLAND TEST PAUL JOHNSON 2172396 31JAN22 PERFORMED CAT 3 CAPABILITY TEST PER MM 22-97-00 ALL TESTS PASS NO FAULT NSDR HALA2022011900019Generator · defectiveETOPS - APU GEN FAULT BEFORE ENGINE START // PERFORMED FIM 24-20-00-810-985-A. REMOVED AND REPLACED APU GEN PER AMM UP TO STEP 4. C. 3. SIGNED 2069773 01/19/2022 INSTALLED INLET AND PERFORMED LEAK/OPS CHECK REF AMM 24-23-51-400-801-A FROM STEP 4.C.3. NO DEFECTSDR HALA2022010300004Controller · inoperativeATB - AFTER T/O ENG 2 CTL SYS FAULT AIR TURN BACK AVOID RAPID THR CHANGES // PERFORMED WIRE CHECKS PER TSM 75-33-00-810-808-A. WIRES CHECKS GOOD NO FAULTS FOUND 12/30/21 MECH 634066PER TSM 75-33-00-810-808A. REMOVED AND REPLACED #2 VENG VSV CONTROL UNIT PER SDR HALA2021122300198Valve · inoperativeETOPS - ON DESCENT AMBER A ICE L INR WING HI PR ON ECAM DISPLAY // REPLACED L/W INNER (10DL1) WING ANTI ICE VALVE PER AMM 30-11-51. OPS CK OK.A/C OK FOR SVC. VALVE, ANTI-ICE OFF 33-3011-9-0001 S/N 12050 ON 33-3011-9-0001 S/N 08016SDR HALA2021112900214Door · damagedSHIP 393 DAMAGE FOUND ON FWD CARGO DOOR. FWD PANEL 821AR. CORRECTIVE ACTION: REWORKED FWD CARGO DOOR PANEL 821AR PER SRM 52-31-00. INSTALLED. (8447327)SDR HALA2021110800199None · noneSHIP 393 DENT DAMAGE NEXT TO THE L2 DOOR DUE TO A TOWING IMPACT. THE DENT IS IN THE SKIN AT STR 28L/FR32. STRINGER 28L IS ALSO VISIBLY DISTORTED. IT IS LOCATED 2.2" FWD OF FR31, WHICH IS AT A BUTT SPLICE. THE DAMAGE IS BEYOND ALLOWED LIMITS. CORRECTIVE ACTION:SDR HALA2021102900185None · noneSHIP 393 FIRST CLASS GALLEY FLOOR LUMINOUS STRIP IS LOOSE. CORRECTIVE ACTION: SECURED LOOSE STRIP. (7716877)SDR HALA2021090200125Slide · no testSHIP 393 UPON ACCOMPLISHING 1L DOOR SLIDE SCHEDULED REPLACEMENT, PERFORMED EPSU SYS TEST AND FOUND "ESCAPE SLIDE LT SW/EPSU (13WL ) DOOR 2 FAULT". CORRECTIVE ACTION: PERFORMED TSM TASK 25-62-00. FOUND 7910MS SLIDE/RAFT DOOR 2 LH BAD. REPLACED 2L DOOR SLIDE. (7SDR HALA2021083100106Display · faultedETOPS - THIRD (CENTER) MCDU BACKLIGHT IS VERY DIM ON BRIGHTEST SETTING // REMOVED AND REPLACED THIRD MCDU PER AMM 22-82-12. OPS CHECK OK.
OK FOR SERVICE UNIT, DISPLAY, OFF P/N 33-2282-9-0003 S/N 49347 ON P/N 33-2282-9-0003 S/N 05685SDR HALA2021082300121Unknown · unknownSHIP 393 DOOR 4R DISARM HANDLE WILL NOT MOVE TO DISARM POSITION. CORRECTIVE ACTION: OPS CHECK MOVEMENT OF 4R ARM/DISARM HANDLE. NO DEFECTS NOTED. FAP AND ECAM INDICATIONS NORMAL. (7274938)SDR HALA2021082300118Lever · faultedSHIP 393 4R DOOR ARMING LEVER IS NOT MOVING TO THE FULL DISARM POSITION. PERFORMED OPERATIONAL CHECK OF 4R DOOR IAW AMM 52-13-00. NO FAULTS NOTED. OK TO CONTINUE. ARMING LEVER FUNCTIONS CORRECTLY.SDR HALA2021050600056Display · defectiveETOPS - MCDU #3 INTERMITTENTLY LOSES POWER & BLANKS OUT. WHEN IT HAPPENS, ATSU ON OTHER MCDUS INOP. // REMOVED AND REPLACED #3 MCDU PER AMM 22-82-12-400-801-A. OPS CHK GOOD. UNIT, DISPLAY, OFF 33-2282-9-0003 14214 ON 33-2282-9-0003 49347SDR HALA2021041900067Skin · corrodedSHIP 393 FUSELAGE SKIN CORRODED AT LWR SIDE OF AFT LAV FWD EXHAUST PORT. CORRECTIVE ACTION: BLENDED AND CHECKED LIMITS PER A330 SRM 53-41-11. REMOVED CORROSION. REMOVED .008. REMAINING SKIN THICKNESS IS .090 WITHIN LIMITS PER A330 SRM 53- 41-11. PERFORMED UT. SDR HALA2021041900066Skin · corrodedSHIP 393 LWR FUSELAGE- FUSELAGE SKIN CORRODED AT LWR SIDE OF AFT LAV AFT EXHAUST PORT. CORRECTIVE ACTION: REMOVED .022 MATERIAL REMAINING SKIN THICKNESS IS .076 WITHIN LIMITS PER A330 SRM 53-41-11. PERFORMED UT. TREATED, PRIMED, AND PAINTED AREA.(1783498)SDR HALA2021032600058Door · obstructedSHIP 393 4R DOOR DIFFICULT TO DISARM. CORRECTIVE ACTION: REMOVED DEBRIS. (7261048)SDR HALA2021030100021Lever · inoperativeSHIP 0393 4R ARMING LEVER INOP. CORRECTIVE ACTION: CHECKED 4R ARMING LEVER FOR DEBRIS AND EASE OF MOVEMENT. COULD NOT REPLICATE FAULT. (7249422)SDR HALA2021021600016Pitot Tube · cloggedATO - RTO FOR NO AIRSPEED INDICATION ON CAPT PFD. MAX SPD INDICATION FROM FO PFD WAS APPROX. 80 KTS // PITOT PROBE #1 (9DA1) CLOGGED. REMOVED AND REPLACED PROBE #1 PER AMM 34-11-15. #1 PHC OPS TEST GOOD. FLUSHED TOTAL PRESSURE LINE PER AMM 34-11-00. DATA GATHESDR HALA2021020800010Bottle · low pressureSHIP 0393 3R DOOR ASSIST BOTTLE LOW PRESSURE. CORRECTIVE ACTION: RECHARGED DOOR 3R DAMPER AND EMERGENCY OPERATION CYLINDER PER A330 AMM 52-10. (7269966)SDR HALA2021011900007Cylinder · low pressureEMERGENCY EQUIPMENT, 3R DOOR EMERGENCY OPERATION CYLINDER PRESSURE LOW. SERVICED 3R DOOR EMERGENCY OPERATION CYLINDER, PER A330 AMM 52-10-00. OPERATIONS CHECKS GOOD. REQUIRED INSPECTION ITEMS COMPLETED 794859 QC2009.SDR HALA2020110400197Apu · odorODOR/FUMES OIL SMELL IN CABIN AND FLIGHT DECK. REMOVED & REPLACED APU. OPERATIONS & LEAK CHECK OK. NO ODOR PRESENT IN CABIN & FLIGHT DECK. APU, AUXILIARY OFF 43-4910-9-0010 01519 ON 43-4910-9-0010 01780.SDR HALA2020072090150Control Valve · malfunctionedETOPS SIGNIFICANT SYSTEM, PACK 1 TEMP CONTROL VALVE ECAM MSG. REPLACED PACK 1 TEMP CONTROL VALVE IAW AMM 21-53-53-400-801A. OPS CHECKED OK.SDR HALA2020071900149Fmu · leakingETOPS SIGNIFICANT SYSTEM, FUEL LEAKING FROM NR 2 ENGINE DRAIN MAST. MECHANIC FOUND LEAK COMING FROM FMU LINE. LINE DISCONNECTED FOR PARKING. RECONNECTED FMU LINE PER AMM 73-21-52-400-802-A. REMOVED AND REPLACED THE NR 2 ENGINE FMU IAW AMM 73-21-52-400-8SDR HALA2020030400051Cover · missingOPEN - LEFT HAND WING FIXED FLAP FAIRING #5 MISSING FWD MOST COVER. // AWAITING PARTS. REPLACED MISSING FLAP FAIRING COVER. SECURITY CHK OK.SDR HALA2020021000033Oil Filter · cloggedETOPS SIGNIFICANT SYSTEM - DURING DESCENT BELOW 12000 FEET ECAM MESSAGE ENG 1 OIL FILTER CLOG. // REMOVED & REPLACED #1 ENGINE OIL FILTER PER A330 AMM 79-22 NO DEBRIS FOUND A/C OK FOR SVCSDR HALA2019100800405Apu · faultedETOPS SIGNIFICANT SYSTEM - APU FAULT, AUTO SHUTDOWN. NO FAULTS SHOWN ON PFR OR PREVIOUS FLY LEGS, TROUBLESHOT IAW TSM 49-62-00-810-870A APU OPERATION NORMAL. C/W OPS TEST OF AIR INTAKE FLAP IAW AMM 49-16-51-710-802A, OPS TEST NORMAL NO PREVIOUS SHUTDOWN FASDR HALA2019100293151Exciter · failedAIRCRAFT FAILED APU COLD SOAK START 3 ATTEMPTS AT OAT -56, -50, -30, FL 400, 350, 270. REPLACED IGNITION EXCITER.SDR HALA2019093000391Exciter · faultyETOPS SIGNIFICANT SYSTEM - APU INFLIGHT START OAT - -56 -51 -30 FL 400 350 270 # ATTEMPTS - 3 UNSUCCESSFUL. // R/R APU EXCITER PER A330 AMM 49-41 AND SYSTEM A IGNITER AND LEAD
R/R PER A330 AMM 49-41. OPT CHK NML.SDR HALA2019091900354Liner · damagedOPEN - ETOPS SIGNIFICANT SYSTEM - NR 1 ENGINE ATTRITION LINER DAMAGED. ACFT TO MX FERRY FOR REPAIRS.SDR HALA2019073100376Actuator · inoperativeETOPS SIGNIFICANT SYSTEM - RT WING FUEL TANK OUTER INLET VALVE ACTUATOR INOP. REPLACED RT WING OUTER TANK INLET VALVE ACTUATOR FIN # 500QU2 PER AMM 28-25-57-400-801-A. OPS CHECK OK.SDR HALA2019061000283Warning Message · false activationETOPS SIGNIFICANT SYSTEM - ELECTRIC APU BAT SYSTEM FAULT ECAM. // T/S PER REF 24-30-00-810-833A. PERFORMED BCL APU TEST. NO FAULTS FOUND DURING TEST. A/C OK FOR SVC.SDR HALA2019053000267Warning System · false activationETOPS SIGNIFICANT SYSTEM - FUEL CTR TO INNER FAULT ILLUMINATED IN CRUISE WITH CENTER FUEL TANK QUANTITY ZERO. FUEL AFT XFR ALSO SHOWN ON STATUS PAGE BUT CLEARED ITSELF. PREVIOUS HISTORY WITH LT INR TK INLET VLV T/S PER TSM 28-26-00. TRANSFER CK OK. BITE TEST OSDR HALA2019052800261Panel · damagedETOPS SIGNIFICANT SYSTEM - RAMP REPORTED DAMAGES IN AFT CARGO ON PANEL 41P. DAMAGE MEASURES 3IN X .25IN AND 1.5IN X.25IN. PERFORMED SPEED PATCH REPAIR PER AMM 25-53-00-00-801-A. A/C OK FOR SVC.SDR HALA2019052100253Controller · malfunctionedETOPS SIGNIFICANT SYSTEM - ONCE ON GROUND AND INFLIGHT HOT AIR 2 TRIM AIR VALVE CLOSED AUTOMATICALLY. AMBER LINE FROM VALVE TO MANIFOLD ON COND PAGE. X BLEED VALVE OPENED. RESET ZONE CONTROLLER. PERFORMED BITE TEST CAB TEMP ECS PER AMM 21-63-00. OPS TEST PASSESDR HALA2019041600191Oil Cooler · leakingETOPS - DURING H1 CHECK IN BNE FOUND R/H ENGINE AIR OIL COOLER HAS EVIDENCE OF OIL LEAKAGE FROM HEAT
EXCHANGER AIR MATRIX // ENGINE AIR OIL COOLER REPLACED IAW A330 AMM 79-21-51 FUEL AND
OIL LEAK TEST CARRIED OUT IAW A330 AMM 71-00-00 - NIL LEAKS. COOLER,SDR HALA2019040502239Profile · corrodedDURING H CHECK, VERTICAL STAB TRAILING EDGE RIGHT HAD SIDE VERTICAL PROFILE ABOVE NBR 2 T CHORD FOUND CORRODED. REPLACED CHORD TO VERTICAL STAB TRAILING EDGE PER SRM 51-42-11 AND AIRBUS DRAWING F55371707. LP 1017034SDR HALA2019040502233Seat Track · corrodedDURING H CHECK, SEAT TRACK BETWEEN FR 54-58, -Y1959 FOUND CORRODED. REPLACED SEAT TRACK PER SRM 51-72-11 AND AIRBUS DRAWING F53476200. LP 1017007SDR HALA2019040502232Seat Track · corrodedDURING H CHECK, SEAT TRACK BETWEEN FR 53.2-54.5 , -Y1959 FOUND CORRODED. REPLACED SEAT TRACK PER SRM 51-72-11 AND AIRBUS DRAWING F53326941. LP 1017000SDR HALA2019040500174Seat Track · corrodedSEAT TRACK BETWEEN FRAME 53.2 AND 54.5 AT -Y1959 IS CORRODED AT LOCATIONS: FR53.5+10", FR53.2 +5", FR53.5+16". // CORROSION REMOVED AS PER SRM 51-74-00 REV 98.01. CORROSION AT
LOCATIONS FR53.5+10?, FR53.2+5?, FR53+16? DAMAGE LOCATED IN THE INNER VERTICAL ASDR HALA2019040500173Seat Track · corrodedSEAT TRACK BETWEEN FRAME 54 AND 58 AT -Y1959 IS CORRODED AT LOCATIONS: FR57+12". // CORROSION REMOVED AS PER SRM 51-74-00 REV 98.01. CORROSION LOCATED AT FR57+12? DAMAGE LOCATED IN THE INNER VERTICAL AREA OF THE SEAT TRACK CROWN, DUE TO RESTRICTED ACCESS UNABLSDR HALA2019040500172Tee Fitting · corrodedVERTICAL STAB TRAILING EDGE RHS #2 T CHORD SUSPECT CORROSION AROUND FASTENER HOLES. #2 RHS VERT FIN T/E T-CHORD CORROSION BLENDED BEYOND LIMITS IAW
HAL A330 SRM 51-74-00 REV 98.01. CHORD REPLACED IAW HAL A330 SRM 51-42-11, REV 98.01 AND AIRBUS DWG F553 717
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