N390HA

Service difficulty reports · 161

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 = 'N390HA' 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.

SDR HALA2021032600056Bottle · low pressureSHIP 390 FAP CHECK DOOR PRESSURE MESSAGEAT 3L DOOR. 3L DOOR SLIDE SHOWED ARMED ABOUT 10 SECONDS AFTER OTHER DOORS. CORRECTIVE ACTION: SERVICE 3L DOOR DAMPER PER AMM 52-22.(4491949)Mar 26, 2021 · N390HA · Airbus A330243 · Passenger/Crew DoorsSDR HALA2021031200052Door · bindingSHIP 390 1L DOOR GOT STUCK IN THE DOOR WAY AFTER OPENING HANDLE. PUSHED ON DOOR AND SLIDE DEPLOYED. CORRECTIVE ACTION: REF NON ROUTINE CARD. REPLACED SLIDE. CHECKED DOOR SLIDE RIG PER HAL A330 AMM 52-11-14. SERVICED DOOR ASSIST BOTTLE. (1752681)Mar 12, 2021 · N390HA · Airbus A330243 · Passenger/Crew DoorsSDR HALA2021020900013Switch · faultedSHIP 0390 2L SLIDE LT SW FAULT. CORRECTIVE ACTION: REMOVED AND REPLACED 2L SLIDE. (7267001)Feb 9, 2021 · N390HA · Airbus A330243 · Emergency EquipmentSDR HALA2021020900014Battery Pack · faultedSHIP 0390 4R EPSU 18WL BAT FAULT. NEEDS BATTERY . CORRECTIVE ACTION: REMOVED & INSTALL NEW BATTERY AT 4R EPSU PER AMM 33-51. OPS CK OK. (7267000)Feb 8, 2021 · N390HA · Airbus A330243 · Emergency LightingSDR HALA2021020900012Battery Pack · faultedSHIP 0390 3L EPSE 15WL BAT FAULT. CORRECTIVE ACTION: REMOVE & INSTALL NEW BATTERY AT 3L EPSU PER AMM 33-51-00. OPS CK OK. (7250399)Feb 8, 2021 · N390HA · Airbus A330243 · Emergency LightingSDR HALA2021011900343Tie Bolt · missingPDA NR 4 MAIN WHEEL TIE BOLT MISSING. CORRECTIVE ACTION: REPLACED NR 4 MLG TIRE, PER A330 AMM 32-41. SPIN AND SECURITY CHECK GOOD.Jan 15, 2021 · N390HA · Airbus A330243 · Wheel/Ski/FloatSDR HALA2020060400119Pump · leakingETOPS SIGNIFICANT SYSTEM - NR 2 ENG HYD EDP LEAKING (GREEN). REMOVED AND INSTALLED NR 2 ENG HYD EDP (GREEN) PER AMM 29-11-51-400-810-A. LEAK CHECK OK. OK TO CONTINUE.Jun 2, 2020 · N390HA · Airbus A330243 · Hydraulic Pump (Electric/Engine), MainSDR HALA2019111400482Engine · vibrationATB - DUE TO HIGH VIBRATIONS. // NEED TO ACCOMPLISH VERIFICATION FLIGHT DUE TO DUAL FAN BLADE LUBE. AIRCRAFT RELEASED TO ETOPS SERVICE IAW HAL ETOPS MAINTENANCE MANUAL FOR VERIFICATION FLIGHT DUE TO DUAL FAN BLADE LUBE. VERIFICATION FLIGHT FOR DUAL ENGINE FANNov 13, 2019 · N390HA · Airbus A330243 · Engine (Turbine/Turboprop)SDR HALA2019111200480Bleed Valve · unknownETOPS SIGNIFICANT SYSTEM - ECAM: AIR APU BLEED FAULT --UPON TURNING ON APU BLEED WHEN PULLING IN TO GATE. // REMOVED AND REPLACED APU BLEED VALVE PER AMM 49-51-51. REPLACED BLEED VALVE FILTER PER AMM 49-51-51-960-801-A. CHK OK. NO DEFECTS NOTED. OK FOR SERVINov 11, 2019 · N390HA · Airbus A330243 · APU Bleed Air SystemSDR HALA2019091900378Liner · damagedETOPS SIGNIFICANT SYSTEM - DURING WALK AROUND FOUND NR 1 ENG ATTRITION LINER AT 6'OCLOCK POS LIFTING UP.// FERRY FLIGHT REQUIRED. THIS AIRCRAFT HAS BEEN INSPECTED THIS DATE (09-19-2019) AND IS SAFE FOR THE INTENDED FLIGHT. REPLACED ENGINE IAW AMDS 7100-9402-1-Sep 18, 2019 · N390HA · Airbus A330243 · Turbine Engine Air Inlet SectionSDR HALA2019090900373Actuator · faultyETOPS SIGNIFICANT SYSTEM - FUEL TRANSFER VALVE INOP UNABLE TO FUEL A/C. GRND SCAN SHOWS INLET VALVE ACTUATOR 603QL1 FAILED CLOSED. REMOVED AND REPLACED INLET VALVE ACTUATOR 603QL1 PER AMM 28-26-53 OPS OK OK FOR SVC.Sep 7, 2019 · N390HA · Airbus A330243 · Fuel Transfer ValveSDR HALA2019070500348Warning System · false activationETOPS SIGNIFICANT SYSTEM - UPON LANDING WE GOT A ENG 2 OIL CHIP DETECTED MSG. TS PER TSM 79-20-00-810-822A AND MM 7-21. CHIP DETECTOR CLEAN, NO TROUBLE FOUND. NO 30 DAY HISTORY OK FOR SERVICE.Jul 4, 2019 · N390HA · Airbus A330243 · Engine Oil Indicating SystemSDR HALA2019062760333Warning Message · false activationETOPS - ATB - THRUST REVERSER NR 2 INOPERATIVE. TROUBLESHOT IAW TSM 24-30, RESET OK.Jun 26, 2019 · N390HA · Airbus A330243 · Engine Thrust ReverserSDR HALA2019061800304Autopilot Sys · malfunctionedETOPS SIGNIFICANT SYSTEM - ON CLIMB OUT AUTOPILOT 1 ENGAGED, RECEIVED AUTO FLT A/THR OFF ECAM WOULD NOT STAY IN ENGAGED IN EITHER AP 1 OR AP2. // RESET FMG EC #1 AND #2. OPERATIONAL CHECK OK PER AMM 22-96-00-740-801-A. AIRCRAFT TO REMAIN IN LAND 3 STATUS.Jun 16, 2019 · N390HA · Airbus A330243 · Autopilot SystemSDR HALA2019061400108Cover · missingLEFT WING NR 3 FLAP TRACK FAIRING OUTBOARD AFT COVER PLATE MISSING. DEFERRED PER CDL 57-07-REPLACED NBR 3 FLAP TRACK FAIRING PLATE.Jun 12, 2019 · N390HA · Airbus A330243 · Trailing Edge FlapsSDR HALA2019061100287Fairing · missingL WING #3 FLAP MOVEABLE FARING MISSING COVER. REPLACED COVER ON WING #3 FLAP MOVEABLE FAIRING.Jun 6, 2019 · N390HA · Airbus A330243 · Trailing Edge FlapsSDR HALA2019061260102Sign · unsecureDOOR 3R EXIT SIGN ON CEILING FELL OFF. RESECURED DOOR 3R EXIT SIGN. LP 5881247Jun 4, 2019 · N390HA · Airbus A330243 · Emergency LightingSDR HALA2019052900263Warning System · false activationETOPS SIGNIFICANT SYSTEM - ENG 2 REV FAULT ECAM AFTER LANDING. MSG ENG 2 REV FAULT TR STOW SW 9E2-4104KS2)/JUNCTION BX(E2-4110KS) ON PFR. PERFORMED TSM 78-30-00 OPS TEST OF ENG2 T/R & PASSED & NO FAULT PER AMM 78-31. A/C OK FOR SVC.May 28, 2019 · N390HA · Airbus A330243 · Engine Thrust ReverserSDR HALA2019050100211Actuator · failedETOPS SIGNIFICANT SYSTEM - BTB - FUEL TRIM LINE FAULT. REMOVED AND REPLACED FUEL ISOLATION VALVE ACTUATOR PER AMM 28-29 -51-000-801-A. OPS GOOD. NO FAULTS NOTED. OK FOR SVC.Apr 30, 2019 · N390HA · Airbus A330243 · Fuel Selector/Shut-Off ValveSDR HALA2019040500175Warning Light · false activationETOPS SIGNIFICANT SYSTEM - APU AGENT DISCHARGE LIGHT ILLUMINATED DURING DESCENT. PERFORMED BITE TEST OF THE APU FIRE AND OVERHEAT DETECTION SYSTEM PER AMM 26-13-00-740-801-A. NO FAULTS NOTED. OK FOR SERVICE.Apr 4, 2019 · N390HA · Airbus A330243 · Extinguishing SystemSDR HALA2019031800133Warning System · false activationETOPS SIGNIFICANT SYSTEM - AFTER TAKEOFF ENGINE ONE BLEED FAULT. RESET ENG 1 BLEED, OPS NORMAL. PERFORMED BMC 1 BITE PER AMM 36-11-00-740-804-A. BITE PASS, NO DEFECTS NOTED. OK FOR SVC.Mar 16, 2019 · N390HA · Airbus A330243 · Pneumatic Indicating SystemSDR HALA2019031300124Structure · corrodedBULK CARGO FLOOR STRUCTURE AT FR 67 AND APPROX -Y600 SUSPECT CORROSION AS MARKED. CORROSION REMOVED BY BLENDING. BLEND MEASURED AND FOUND TO BE BEYOND SRM LIMITS, CORROSION REPORTED AS LEVEL 2. STRUCTURE COMPONENTS REPLACED. ALL IAW SRM 51-74-00, 51-42-11, 51-Mar 13, 2019 · N390HA · Airbus A330243 · Fuselage Miscellaneous StructureSDR HALA2019031300123Seat Track · corrodedSEAT TRACK BETWEEN FRAME 25 AND 37.4 AT -Y450 IS CORRODED AT LOCATIONS: 29+9, 31+2, 31+5, 31+19, 32+14. CORROSION REMOVED BY GRINDING AS PER SRM 51-74-00 REV 98.01. DAMAGE DIMENSIONS:1. FR 29+9" IVA L=.50" CORROSION ALSO SPREAD TO INNER VERTICAL WALL AREA. UNAMar 13, 2019 · N390HA · Airbus A330243 · Fuselage, Seat/Cargo Attach FittingsSDR HALA2019031201617Structure · corrodedVERTICAL STABILIZER TRAILING EDGE LT #2 T CHORD CORRODED. REPLACED T CHORD PER SRM 51-44-11, 51-21-11, AND 51-46-11. LP 0980976Mar 12, 2019 · N390HA · Airbus A330243 · Vertical Stabilizer Miscellaneous StructureSDR HALA2019031201616Structure · corrodedVERTICAL STABILIZER TRAILING EDGE RT NR 3 T CHORD CORRODED. REPLACED T CHORD PER SRM 51-44-11, 51-21-11, AND 51-46-11. LP 0980967Mar 12, 2019 · N390HA · Airbus A330243 · Vertical Stabilizer Miscellaneous StructureSDR HALA2019031201615Structure · corrodedVERTICAL STABILIZER TRAILING EDGE RT NR 2 T CHORD CORRODED. REPLACED T CHORD PER SRM 51-44-11, 51-21-11, AND 51-46-11. LP 0980963Mar 12, 2019 · N390HA · Airbus A330243 · Vertical Stabilizer Miscellaneous StructureSDR HALA2019031201614Seat Track · corrodedDURING H CHECK, SEAT TRACK BETWEEN 25.5-37.4, -Y1456 FOUND CORRODED. REPLACED SEAT TRACK PER SRM 51-72-11. LP 0980971Mar 12, 2019 · N390HA · Airbus A330243 · Fuselage, Seat/Cargo Attach FittingsSDR HALA2019031201613Seat Track · corrodedDURING H CHECK, SEAT TRACK BETWEEN 25.5-37.4, -Y2462 FOUND CORRODED. REPLACED SEAT TRACK PER SRM 51-72-11 AND DRAWING F53276421. LP 0980924Mar 12, 2019 · N390HA · Airbus A330243 · Fuselage, Seat/Cargo Attach FittingsSDR HALA2019031200121Seat Track · corrodedSEAT TRACK BETWEEN FRAME 25 AND 37.4 AT -Y2462 IS CORRODED AT LOCATIONS: 26+16, 29+11, 30+9, 31+7, 32+3, 35+17, 37.1+17. CORROSION REMOVED BY GRINDING AS PER SRM 51-74-00 REV 98.01. DAMAGE DIMENSIONS: 1. FR26+16 CENTRAL L=1.0" W=0.4" D=0.023" IVA UNABLE TO SUFMar 12, 2019 · N390HA · Airbus A330243 · Fuselage, Seat/Cargo Attach FittingsSDR HALA2019031200120Structure · corrodedVERTICAL STAB TRAILING EDGE RHS #2 T CHORD SUSPECT CORROSION AROUND FASTENER HOLES. REMOVAL OF CORROSION C/OUT IAW SRM 51-74-00 REV.98.01. CORROSION STILL EVIDENT IAW NTM 51-10-02-221-001-A REV. 96 AT BLEND DEPTH OF .058". BLEND DEPTH BEYOND 50% MATERIAL THICKMar 12, 2019 · N390HA · Airbus A330243 · Vertical Stabilizer Miscellaneous StructureSDR HALA2019031200119Structure · corrodedVERTICAL STAB TRAILING EDGE RHS #3 T CHORD SUSPECT CORROSION AROUND FASTENER HOLES. // REMOVAL OF CORROSION C/OUT IAW SRM 51-74-00 REV.98.01. CORROSION STILL EVIDENT IAW NTM 51-10-02-221-001-A REV. 96 AT BLEND DEPTH OF .058". BLEND DEPTH BEYOND 50% MATERIAL THMar 12, 2019 · N390HA · Airbus A330243 · Vertical Stabilizer Miscellaneous StructureSDR HALA2019031100090Seat Track · corrodedDURING H CHECK, SEAT TRACK BETWEEN FR 40-47, -Y1959 FOUND CORRODED. REPLACED SEAT TRACK PER SRM 51-72-11 AND DRAWING F5711057120401. LP 0979474Mar 11, 2019 · N390HA · Airbus A330243 · Fuselage, Seat/Cargo Attach FittingsSDR HALA2019031100089Seat Track · corrodedDURING H CHECK, SEAT TRACK BETWEEN FR 25.5-37.4, +Y953 FOUND CORRODED. REPLACED SEAT TRACK PER SRM 51-72-11 AND DRAWING F53276421. LP 0979153Mar 11, 2019 · N390HA · Airbus A330243 · Fuselage, Seat/Cargo Attach FittingsSDR HALA2019031200116Seat Track · corrodedSEAT TRACK BETWEEN FRAME 40 AND 47 AT -Y1959 IS CORRODED AT LOCATIONS: FR43, FR44, FR46, FR47. CORROSION REMOVED FROM SEAT TRACK @ FR43, FR44, FR46, FR47 IAW SRM 51-74-00 REV 98.01. DAMAGE DIMENSION: AT FR43 CENTRAL RE-WORK L: 4.5" W: 0.75" D: 0.030", FR44 CENMar 11, 2019 · N390HA · Airbus A330243 · Fuselage, Seat/Cargo Attach FittingsSDR HALA2019031200115Seat Track · corrodedSEAT TRACK BETWEEN FRAME 25.5 AND 37.4 AT +Y953 IS CORRODED AT LOCATIONS: 26, 26+3, 26+8, 26+6, 29+10, 29+15, 29+20, 30+2, 32+13. // CORROSION REMOVED AS SRM 51-71-00 REV 98.01. DAMAGE DIMENSIONS: 1. FR 26"" SUPERIOR L=1.5" W=0.50" DEPTH= 0.030", 2. FR 26 +3"Mar 11, 2019 · N390HA · Airbus A330243 · Fuselage, Seat/Cargo Attach FittingsSDR HALA2019031200118Seat Track · corrodedSEAT TRACK BETWEEN FRAME 25.5 AND 37.4 AT -Y1456 IS CORRODED AT LOCATIONS: 33 AND 35. CORROSION REMOVED BY GRINDING AS PER SRM 51-74-00 REV 98.01. DAMAGE DIMENSIONS: FR 33: L=1.300" W=0.350" D=0.022", FR 35: L=2.00" W=0.650" D=0.038". GAUGE PN: 2417S, SN: VUDMar 8, 2019 · N390HA · Airbus A330243 · Fuselage, Seat/Cargo Attach FittingsSDR HALA2019031300118Seat Track · corrodedSEAT TRACK BETWEEN FRAME 40 AND 47 AT -Y450 IS CORRODED AT LOCATIONS: FR44, FR45, FR46. CORROSION REMOVED AS PER SRM 51-74-00 REV 98.01. DAMAGE DIMENSIONS: 1. FR44 CENTRAL REWORK L: 3.5" W: 0.75" D: 0.032", 2. FR45 CENTRAL REWORK L: 5.5" W: 0.75" D: 0.022", 3.Mar 8, 2019 · N390HA · Airbus A330243 · Fuselage, Seat/Cargo Attach FittingsSDR HALA2019031200117Seat Track · corrodedSEAT TRACK NR 8 BETWEEN FRAME 40 AND 47 AT -Y450, P/N F57112436201 REQ'S FABRICATING. SEAT TRACK ASSEMBLY P/N F5711243620100 UNABLE TO BE PROCURED DURING THIS MAINTENANCE CHECK. SEAT TRACK ASSEMBLY CONSIDERED TO BE A CATEGORY 3 PART. SEAT TRACK FABRICATED AS PMar 8, 2019 · N390HA · Airbus A330243 · Fuselage, Seat/Cargo Attach FittingsSDR HALA2019030700107Seat Track · corrodedSEAT TRACK BETWEEN FRAME 18 AND 25.5 AT +Y953 IS CORRODED AT LOCATIONS: 19+10, 22+17, 24+18. CORROSION REMOVED IAW SRM 51-74-00 REV 98.01. DAMAGE DIMENSIONS: 1. FR 18 +2" SUPERIOR L=1.0" W=0.50" DEPTH= 0.022", 2. FR 19 + 10" SUPERIOR L=1.0" W=0.50" DEPTH=0.04Mar 7, 2019 · N390HA · Airbus A330243 · Fuselage, Seat/Cargo Attach FittingsSDR HALA2019030700106Support Angle · corrodedDOOR 1R FLOOR SUPPORT STRUCTURE FWD LWR SUPPORT ANGLE @ FR13A Y-2061 IS CORRODED WHERE INDICATED. CORROSION DAMAGE DIMENSIONS: L=0.300" W=0.500" DEPTH=0.020". DEPTH GAUGE USED P/N: 2417 S/N: IRFE5005A9EQ. UNABLE TO FIND SRM LIMITS FOR THIS COMPONENT. RII CARRIMar 7, 2019 · N390HA · Airbus A330243 · Fuselage Miscellaneous StructureSDR HALA2019030700105Seat Track · corrodedSEAT TRACK BETWEEN FRAME 53.2 AND 54 AT +Y1959 IS CORRODED AT LOCATIONS: FR53.3, FR53.5+10". CORROSION REMOVED BY GRINDING AS PER SRM 51-74-00 REV 98.01. DAMAGE DIMENSIONS: FR53.3 CENTRAL REWORK L: 4.5" W: 0.75" D: 0.052", FR53.5(+10") SUPERIOR REWORK L: 3" W:Mar 7, 2019 · N390HA · Airbus A330243 · Fuselage, Seat/Cargo Attach FittingsSDR HALA2019030700104Seat Track · corrodedSEAT TRACK BETWEEN FRAME 47 AND 53.2 AT +Y1959 IS CORRODED AT LOCATIONS: FR47+6", FR48+16", FR51+14" AND FR53.1+14". CORROSION REMOVED BY GRINDING AS PER SRM 51-74-00 REV 98.01. DAMAGE DIMENSIONS: FR47(+6") INNER VERTICAL L: 1" W: 0.2" D:0.020", FR48(+16") CENMar 7, 2019 · N390HA · Airbus A330243 · Fuselage, Seat/Cargo Attach FittingsSDR HALA2019030600099Seat Track · corrodedSEAT TRACK BETWEEN FRAME 53.2 AND 54 AT -Y2462 IS CORRODED AT LOCATIONS: FR53.3. CORROSION REMOVED BY GRINDING AS PER SRM 51-74-00 REV 98.01. DAMAGE DIMENSIONS: (1) FR53.3 SUPERIOR REWORK L: 1.25" W: 0.5" D: 0.035"DEPTH GAUGE USED P/N: 2417 S/N: IRFE5005A9EQ. Mar 6, 2019 · N390HA · Airbus A330243 · Fuselage, Seat/Cargo Attach FittingsSDR HALA2019030600098Seat Track · corrodedSEAT TRACK BETWEEN FRAME 53.2 AND 53.4 AT -Y450 IS CORRODED AT LOCATIONS: FR53.2+8" AND FR53.4. CORROSION REMOVED BY GRINDING AS PER SRM 51-74-00 REV 98.01. DAMAGE DIMENSIONS: (1) FR53.2(+8") CENTRAL REWORK L: 1" W: 0.75" D: 0.022"(2) FR53.4 CENTRAL REWORK L: Mar 6, 2019 · N390HA · Airbus A330243 · Fuselage, Seat/Cargo Attach FittingsSDR HALA2019030600097Seat Track · corrodedSEAT TRACK NR 7 BETWEEN FRAME 31 AND 35 AT +Y1552 IS CORRODED AT LOCATIONS: 33+4. CORROSION REMOVED BY GRINDING AS PER SRM 51-74-00 REV 98.01. DAMAGE DIMENSIONS: FR33+4? L=1.250", W=1.0 ", D+.044". DEPTH GAUGE USED P/N: 2417 S/N: IRFE5005A9EQ. DAMAGE ASSESSED Mar 6, 2019 · N390HA · Airbus A330243 · Fuselage, Seat/Cargo Attach FittingsSDR HALA2019030600096Seat Track · corrodedSEAT TRACK BETWEEN FRAME 25 AND 337.4 AT +Y1456 IS CORRODED AT LOCATIONS: 35+17. CORROSION REMOVED BY GRINDING AS PER SRM 51-74-00 REV 98.01. DAMAGE DIMENSIONS: FR35+17 SUPERIOR L=2.0", W=0.5", D+.030" & OUTER VERTICAL WALL DEPTH = .050". ASSESSED AS OUTSIDE OMar 6, 2019 · N390HA · Airbus A330243 · Fuselage, Seat/Cargo Attach FittingsSDR HALA2019030600095Seat Track · corrodedSEAT TRACK BETWEEN FRAME 25+5 AND 37.4 AT +Y1959 IS CORRODED AT LOCATIONS: 33.1. CORROSION REMOVED BY GRINDING AS PER SRM 51-74-00 REV 98.01. DAMAGE DIMENSIONS: DAMAGE DIMENSION AT LOCATION FRAME 33 + 1" SUPERIOR L = 1.5" W = 0.5" D = .040". IVA UNABLE TO SUFMar 6, 2019 · N390HA · Airbus A330243 · Fuselage, Seat/Cargo Attach FittingsSDR HALA2019030600094Seat Track · corrodedSEAT TRACK BETWEEN FRAME 53.2 AND 54 AT -Y1959 IS CORRODED AT LOCATIONS: FR53.3, FR53.5+9" AND FR53.9+12". CORROSION REMOVED BY GRINDING AS PER SRM 51-74-00 REV 98.01. DAMAGE DIMENSIONS: FR53.3 SUPERIOR REWORK L: 2" W: 1" D: 0.040", FR53.5(+9") INNER VERTICAL Mar 6, 2019 · N390HA · Airbus A330243 · Fuselage, Seat/Cargo Attach FittingsSDR HALA2019030600089Seat Track · corrodedSEAT TRACK BETWEEN FRAME 53.2 AND 54 AT -Y2462 IS CORRODED AT LOCATIONS: FR53.3. CORROSION REMOVED BY GRINDING AS PER SRM 51-74-00 REV 98.01. DAMAGE DIMENSIONS: (1) FR53.3 SUPERIOR REWORK L: 1.25" W: 0.5" D: 0.035"DEPTH GAUGE USED P/N: 2417 S/N: IRFE5005A9EQ. Mar 5, 2019 · N390HA · Airbus A330243 · Fuselage, Seat/Cargo Attach FittingsSDR HALA2019030600088Seat Track · corrodedSEAT TRACK BETWEEN FRAME 53.2 AND 53.4 AT -Y450 IS CORRODED AT LOCATIONS: FR53.2+8" AND FR53.4. // CORROSION REMOVED BY GRINDING AS PER SRM 51-74-00 REV 98.01. DAMAGE DIMENSIONS: (1) FR53.2(+8") CENTRAL REWORK L: 1" W: 0.75" D: 0.022"(2) FR53.4 CENTRAL REWORK Mar 5, 2019 · N390HA · Airbus A330243 · Fuselage, Seat/Cargo Attach Fittings
Back to N390HA