Airbus A310-203

Service difficulty reports · 2,392

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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 aircraft_model_key = 'A310203'
  ORDER BY difficulty_date DESC"

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SDR FDEA201103171052Support Fitting · corrodedVERTICAL STABILIZER INTERIOR, RUDDER HINGE NR 4 SUPPORT FITTING AT REAR SPAR, RIB-13 HAS CORROSION ON BOTTOM EDGE , ABOUT 10 SQUARE INCHES. R & R NR 4 RUDDER HINGE SUPPORT FITTING AT REAR SPAR RIB 13 IAW A310 SRM 51-72-10, PGS 1-3.Mar 17, 2011 · N443FE · Airbus A310203 · Vertical StabilizerSDR FDEA201103171051Stringer · corrodedAFT FUSELAGE, INTERNAL, RT STRINGER 4 END FITTING AT AFT SIDE OF FRAME 87 HAS SEVERE EXFOLIATION CORROSION APPROX 1 SQUARE INCH. R & R STR 4R END FITTING AT FR87 AFT SIDE IAW SRM 51-72-10, PGS 1-3.Mar 17, 2011 · N443FE · Airbus A310203 · Fuselage Main, Longeron/StringerSDR FDEA201103130952Skin · corrodedFUSELAGE TAIL SECTION FR 87 BETWEEN STR 2R AND 3R CORROSION. (SURFACE) ON SPLICE PLATE, ABOUT 4 SQ INCHES. REMOVED LEVEL 1 CORROSION IAW SRM 51-74-10 , CHECKED LIMITS FOUND TO BE OUT OF LIMITS IAW SRM 53-19-10, FIG 102. FABRICATED STRAP JOINT IAW DWG A539Mar 13, 2011 · N443FE · Airbus A310203 · Fuselage Main, Plate/SkinSDR FDEA201103082037Battery · failedEMERGENCY LIGHTS WILL NOT TEST USING PUSH-BUTTON OR OVERHEAD PANEL LIGHT SWITCH. R & R EMERGENCY LIGHT BATTERY LOCATED ADJACENT LT PASSENGER ENTRY DOOR IAW MM 33-51-14-04-0. EMERGENCY LIGHT TEST GOOD IAW MM 33-55-0 0-05. R & R EMERGENCY LIGHT BATTERY LOCMar 8, 2011 · N423FE · Airbus A310203 · Emergency LightingSDR FDEA201103080904Connector · dirtyAFTER TAKEOFF KRUGER FLAPS DID NOT RETRACT. CYCLED TO NO AVAIL. AFFECTED SURFACE DEACTIVATED IN RETRACTED POSITION. OBSERVE AFM PERFORMANCE LIMITATIONS FOR INOPERATIVE KRUGER FLAPS." REACTIVATED KRUEGER FLAPS IAW MM 27-87-00-09-0. FOUND CONNECTOR ON KRUEGMar 8, 2011 · N410FE · Airbus A310203 · Flight Control System WiringSDR FDEA201103040844Angle · corrodedUPON REMOVAL OF LAV SERVICE BOX AND SKIN STIFFENERS, FOUND EXCESSIVE CORROSION EXTENDING UNDER FR 12A LT AT STR 37L. REMOVED LEVEL ONE CORROSION IAW SRM 51-74-10. MATERIAL LOSS WAS 100 PERCENT OF ANGLE AT FR 12A AND STR 37L, FOUND TO BE OUT OF LIMITS IAW Mar 4, 2011 · N443FE · Airbus A310203 · Fuselage Miscellaneous StructureSDR FDEA201103010805Frame · crackedAVIONICS COMPARTMENT FORWARD DOOR INT SIDE, AFT FRAME IS CRACKED IN 2 PLACES AT LIGHTENING HOLES. CRACKED DOOR FRAME WAS REMOVED PER SRM 51-40-21, PARA 6. NEW FRAME WAS FABRICATED PER DWG A52110744, ISSUE "F". FRAME WAS ALODINED PER SRM 51-21-10, PAGE 2. PMar 1, 2011 · N430FE · Airbus A310203 · Fuselage Main, StructureSDR FDEA201102240727Transition Panel · corrodedFWD CARGO COMPARTMENT TRANSITION PANEL 131 WF HAS MULTIPLE AREAS OF CORROSION ON THE FRONT. TRANSITION PANEL WAS CORRODED AND FOUND TO BE OUT OF LIMITS IAW SRM 51-74-10. PANEL WAS REMOVED AND FABRICATED IAW DWG A53272783 AND SRM 51-71-40. PARTS WERE ALODINEDFeb 24, 2011 · N430FE · Airbus A310203 · Fuselage Miscellaneous StructureSDR FDEA201102240726Transition Panel · corrodedFWD CARGO COMPARTMENT TRANSITION PANEL 132 WF HAS MULTIPLE AREAS OF CORROSION, FRONT AND BACK. TRANSITION PANEL WAS CORRODED AND FOUND TO BE OUT OF LIMITS IAW SRM 51-74-10. PANEL WAS REMOVED AND FABRICATED IAW DWG A53272783 AND SRM 51-71-40. PARTS WERE ALODIFeb 24, 2011 · N430FE · Airbus A310203 · Fuselage Miscellaneous StructureSDR FDEA201102230701Skin · dentedLT WING INBD FLAP SKIN IS DENTED. BLENDED AREA NOTED; FOUND 100 PERCENT MATERIAL THICKNESS GONE IAW SRM 57-52-12, FIG 107. REMOVED DAMAGED SKIN AND REPAIRED IAW SRM 57-52-10, FIG 204 & PARA 4-D. ALODINED BARE SURFACES, SEALED DOUBLER & PRIMED IAW SRM 57-5Feb 23, 2011 · N430FE · Airbus A310203 · Trailing Edge FlapsSDR FDEA201102230697Arm · wornRT ELEVATOR AT 2 HINGE ARM LOWER FWD BEARING SWAGE LOOSE IN ARM - INBD TO OTBD MOVEMENT AS SEEN FROM THE TOP OF STAB. REMOVED RT ELEVATOR NR 2 HINGE ARM; R & R 2 EA FWD BEARINGS AND REINSTALLED RT NR 2 ELEVATOR HINGE ARM; FUNCTIONAL CHECK GOOD OF NR 2 ELEVAFeb 23, 2011 · N430FE · Airbus A310203 · Elevator StructureSDR FDEA201102230696Structure · damagedLT WING T/E THROUGH HOLES FOR HYD LINES ARE ELONGATED AT WS OWS 1083.Feb 23, 2011 · N430FE · Airbus A310203 · Wing Main, Frame StructureSDR FDEA201102210646Web · crackedFWD CARGO COMPARTMENT UNDER FLOOR VERTICAL WEB IS CRACKED BETWEEN FRAME 37 & FRAME 38; LBL 56. REMOVED AND REINSTALLED PALLET LATCH AT FRAME 37, RBL 33 IAW AMM 25-52-34- 04, PARA 2B1 & 2E2. REMOVED AND REINSTALLED PDU TRAY AT FRAME 37 TO 38 RT IAW SRM 51-4Feb 21, 2011 · N430FE · Airbus A310203 · Fuselage Miscellaneous StructureSDR FDEA201102210645Web · crackedFWD CARGO COMPARTMENT UNDER FLOOR VERTIVAL WEB IS CRACKED BETWEEN FRAME 36 & FRAME 37; LBL 56. UPPER AND LOWER WEBS WERE REMOVED IAW SRM 51-40-21, PARA 6. NEW WEBS LOCATED AND DRILLED IAW SRM 51-40-44, PAGE 1. BOTH WEBS INSTALLED IAW SRM 51-40-21, PARA 7.Feb 21, 2011 · N430FE · Airbus A310203 · Fuselage Miscellaneous StructureSDR FDEA201102180603Floor Panel · delaminatedTAIL COMPARTMENT WORK PLATFORM IS SPONGY AND HAS EXPOSED CORE - DIRECTLY INBD OF ACCESS DOOR 312 AR CUTOUT. REPAIRED TAIL COMPARTMENT WORK PLATFORM WITH THE FABRICATION OF A NEW FLOOR PANEL USING THE OLD FLOOR PANEL AS A TEMPLATE IAW DWG SRZ 25-005, REV "HFeb 18, 2011 · N430FE · Airbus A310203 · Fuselage Floor PanelSDR FDEA201102180606Angle · damagedAFT PIT SHEAR PLATE TOP "L" ANGLE HAS PREVIOUSLY DOUBLE DRILLED HOLES BETWEEN FRAME 64 AND FRAME 65; STRINGER 44L. REMOVED ANGLE IAW SRM 51-40-21, PARA 6. FABBED NEW ANGLE IAW DWG A53974252, ISSUE "G". ALODINED IAW SRM 51-21-10, PG 1. PRIMED IAW SRM 51-Feb 18, 2011 · N430FE · Airbus A310203 · Fuselage Miscellaneous StructureSDR FDEA201102180605Angle · damagedAFT PIT SHEAR PLATE TOP "L" ANGLE HAS PREVIOUS DOUBLE DRILLED HOLES BETWEEN FRAME 65 AND FRAME 66; STRINGER 44LT. REMOVED ANGLE IAW SRM 51-40-21, PARA 6. FABRICATED NEW ANGLE IAW DWG A53974254, ISSUE "D". ALODINED IAW SRM 51-21-10, PG 1. PRIMED IAW SRM 5Feb 18, 2011 · N430FE · Airbus A310203 · Fuselage Miscellaneous StructureSDR FDEA201102180604Web · dentedFWD CARGO COMPARTMENT UNDER FLOOR VERTICAL WEB IS DENTED BETWEEN FRAME 34 - FRAME 35; LBL 56. REMOVED WEB IAW SRM 51-40-21, PARA 6. DISPLACED, CAPPED AND STOWED WIRING THROUGH WEB IAW AMM 20-33-22. LOCATED & DRILLED NEW WEB IAW SRM 51-40-44, PG 1. INSTALFeb 18, 2011 · N430FE · Airbus A310203 · Fuselage Miscellaneous StructureSDR FDEA201102170592Seat Track · corrodedMAIN CABIN SEAT TRACK BETWEEN FRAME 72 AND 73 LBL 34 IS CORRODED. REMOVED CORROSION IAW SRM 53-10-16. CHECKED LIMITS, ORIGINAL THICKNESS 0.140. MATERIAL LOSS 0.041. MATERIAL REMAINING 0.099. FOUND TO BE OUT OF LIMITS. REMOVED SEAT TRACK SECTION, MATERIAL Feb 17, 2011 · N430FE · Airbus A310203 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201102160571Spar · crackedNR 2 PYLON HORIZ HEAT SHIELD BELOW THE LOWER SPAR IS CRACKED AND MISSING PIECES. WELD REPAIRED IAW EA 6-5750-136739.Feb 16, 2011 · N430FE · Airbus A310203 · Nacelle/Pylon, Frame/Spar/RibSDR FDEA201102160570Spar · crackedLT PYLON HORIZ HEAT SHIELD BELOW THE LOWER SPAR IS CRACKED AND MISSING PIECES. WELD REPAIRED IAW EA 6-5750-136739.Feb 16, 2011 · N430FE · Airbus A310203 · Nacelle/Pylon, Frame/Spar/RibSDR FDEA201102160572Seat Track · corrodedMAIN DECK SEAT TRACK IS CORRODED BETWEEN FRAME 75 AND FRAME 76; LBL 30. REMOVED CORROSION IAW SRM 51-74-10. CHECKED LIMITS, ORIGINAL THICKNESS 0.0140. MATERIAL REMOVED 0.058. MATERIAL REMAINING 0.082. FOUND TO BE OUT OF LIMITS IAW SRM 51-31-20 & SRM 53-10Feb 16, 2011 · N430FE · Airbus A310203 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201102140565Floorboard · corrodedBULK CARGO COMPARTMENT FLOORBOARD 162 HF METAL TOP IS CORRODED. REMOVED TOP SHEET IAW DWG SRZ 25-011, REV "C". TOP SHEET MATERIAL ID 2024-T3 IAW DWG SRZ 25-011, REV "C". FABRICATED TOP SHEET IAW DWG SRZ 25-011, REV "C". BONDED TOP SHEET TO FLOORBOARD IAWFeb 14, 2011 · N430FE · Airbus A310203 · Fuselage Floor PanelSDR FDEA201102140556Seat Track · corrodedMAIN DECK SEAT TRACK IS CORRODED BETWEEN FRAME 75 & FRAME 76; LBL 43. REPAIRED MAIN DECK SEAT TRACK BETWEEN FRAME 74 TO FRAME 76 WITH 35 INCHES OF SEAT TRACK SECTION AND SPLICE IAW SRM 53-10-16, FIG 208, SHEET 1, LBL 43.Feb 14, 2011 · N430FE · Airbus A310203 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201102090511Skin · corrodedFWD CARGO DOOR INNER SKIN IS CORRODED UNDER THE LOWER SEAL RETAINER. REMOVED AND REPLACED SECTION OF SKIN IAW A310-200 SRM 51-40-21, PARA 6, 7 & 13.Feb 9, 2011 · N430FE · Airbus A310203 · Cargo/Baggage DoorsSDR FDEA201102090512Skin · corrodedFUSELAGE INTERGAL PLATE HAS CORROSION AT FRAME 38.2; STRINGER 52R. REMOVED CORROSION PER SRM 51-74-10. FOUND TO BE OUT OF LIMITS PER SRM 53-14-12, FIG 101. FABRICATED REPAIR PARTS PER SRM 53-14-12, REPAIRS 4 & 5. ALODINED PER SRM 51-21-10. PRIMED PER SRM Feb 9, 2011 · N430FE · Airbus A310203 · Fuselage Main, Plate/SkinSDR FDEA201102080499Floor Panel · crackedMAIN CABIN FLOOR PANEL 241 YN IN ZONE 240 IS CRACKED. FABRICATED NEW FLOOR PANEL 241 YN IAW DWG SRZ 25-005, REV "H".Feb 8, 2011 · N430FE · Airbus A310203 · Fuselage Floor PanelSDR FDEA201102080498Floor Panel · crackedMAIN CABIN FLOOR PANEL 231 R IN ZONE 230 IS CRACKED. FABRICATED NEW FLOOR PANEL 231 RG IAW DWG SRZ 25-005, REV "H".Feb 8, 2011 · N430FE · Airbus A310203 · Fuselage Floor PanelSDR FDEA201102080497Floor Panel · crackedMAIN CABIN FLOOR PANEL 241 NK IS CRACKED ; ZONE 240. FABRICATED NEW FLOOR PANEL 241 NK IAW DWG SRZ 25-005, REV "H".Feb 8, 2011 · N430FE · Airbus A310203 · Fuselage Floor PanelSDR FDEA201102080496Floorboard · damagedMAIN CABIN FLOORBOARD HAS A BROKEN OFF OTBD FWD CORNER FROM FRAME 25-FRAME 27; RBL 78 TO RBL 100. FABRICATED NEW FLOORBOARD 231 VG IAW DWG SRZ 25-005, REV "H".Feb 8, 2011 · N430FE · Airbus A310203 · Fuselage Floor PanelSDR FDEA201102080495Floor Panel · damagedMAIN CABIN FLOOR PANEL FROM FRAME 40- FRAME 41; LBL 85. FABRICATED NEW FLOOR PANEL 241 VJ IAW DWG SRZ 25-005, REV "H".Feb 8, 2011 · N430FE · Airbus A310203 · Fuselage Floor PanelSDR FDEA201102080494Floorboard · delaminatedAFT CARGO COMPARTMENT FLOORBOARD 152 BF TOP SKIN IS DELAMINATED. FABRICATED NEW FLOORBOARD 152 BF IAW DWG SRZ 25-005, REV "H".Feb 8, 2011 · N430FE · Airbus A310203 · Fuselage Floor PanelSDR FDEA201102080493Skin · crackedAFT CARGO COMPARTMENT FLOORBOARD 152 AF TOP SKIN IS CRACKED. FABRICATED NEW FLOORBOARD 152 AF IAW DWG SRZ 25-005, REV "H".Feb 8, 2011 · N430FE · Airbus A310203 · Fuselage Floor PanelSDR FDEA201102080492Floorboard · damagedAFT CARGO COMPARTMENT FLOORBOARD 151EF TOP SKIN IS TORN AND THE CORNER IS CRUSHED. FABRICATED NEW FLOORBOARD 151 EF IAW DWG SRZ 25-005, REV "H".Feb 8, 2011 · N430FE · Airbus A310203 · Fuselage Floor PanelSDR FDEA201102080491Skin · damagedAFT CARGO COMPARTMENT FLOORBOARD 151 CF FASTENER HOLE IS BROKEN AND THE BOTTOM SKIN IS TORN. FABRICATED NEW FLOORBOARD 151 CF IAW DWG SRZ 25-005, REV "H".Feb 8, 2011 · N430FE · Airbus A310203 · Fuselage Floor PanelSDR FDEA201102080490Floorboard · damagedFWD CARGO COMPARTMENT FLOORBOARD 132 RF, MULTIPLE CORNERS ARE BROKEN, THE EDGES ARE DAMAGED AND MISSING EDGE FILLER. FABRICATED NEW FLOORBOARD 132 RF IAW DWG SRZ 25-005, REV "H".Feb 8, 2011 · N430FE · Airbus A310203 · Fuselage Floor PanelSDR FDEA201102080489Floorboard · crackedFWD CARGO COMPARTMENT FLOORBOARD 131 RF IS CRACKED ON AND THE CORNERS ARE DAMAGED. FABRICATED NEW FLOOR BOARD 131 RF IAW DWG SRZ 25-005, REV "H".Feb 8, 2011 · N430FE · Airbus A310203 · Fuselage Floor PanelSDR FDEA201102080488Floorboard · crackedFWD CARGO COMPARTMENT FLOORBOARD 131 HG IS CRACKED ON THE BACK AND THE EDGE IS BROKEN. FABRICATED NEW 131 HG IAW DWG SRZ 25-005, REV "H".Feb 8, 2011 · N430FE · Airbus A310203 · Fuselage Floor PanelSDR FDEA201102030462Floorbeam · corrodedAFT CARGO COMPARTMENT RT FLOORBEAM STRUCTURE HAS DOUBLE DRILLED HOLES AND IS CORRODED AT THE NUTPLATES. CROSSBEAM WAS REMOVED PER SRM 51-40-21, PARA 6 & 7. DRILLED AND INSTALLED NEW PART PER SRM 51-72-10, PG 2Feb 3, 2011 · N430FE · Airbus A310203 · Fuselage Main, Floor BeamSDR FDEA201102030461Floorbeam · damagedBULK CARGO COMPARTMENT FLOORBEAM T-CAP HAS 2 DRILL STARTS ON THE UPPER SURFACE AT FRAME 66, LBL 3". DAMAGE REMOVED PER SRM 51-40-21 AND NEW T-CAP WAS FITTED AND DRILLED PER SRM 51-40-44 AND INSTALLED PER SRM 51-40-21; PARA 6 & 7.Feb 3, 2011 · N430FE · Airbus A310203 · Fuselage Main, Floor BeamSDR FDEA201102020450Plate · crackedAFT CARGO COMPARTMENT DOOR CUTOUT CEILING STRUCTURE SEAL PLATE IS CRACKED BETWEEN FRAME 60 AND FRAME 61. TRIMMED OUT DAMAGED AREA IAW SRM 51-71-40, PG 202. FABRICATED REPAIR DOUBLER AND FILLER IAW SRM 51-71-40. DRILLED IAW SRM 51-40-44. ALODINED FILLER AND Feb 2, 2011 · N430FE · Airbus A310203 · Fuselage Miscellaneous StructureSDR FDEA201102020449Retainer · crackedAFT CARGO COMPARTMENT DOOR CEILING PANEL RETAINER IS CRACKED BETWEEN FRAME 60 AND FRAME 61; STRINGER 21R TO STRINGER 23R. REMOVED AFT CARGO COMPARTMENT DOOR CEILING PROFILE IAW SRM 51-40-21, PARA 5. LOCATED AND DRILLED IAW SRM 51-40-44. INSTALLED CEILING PAFeb 2, 2011 · N430FE · Airbus A310203 · Cargo/Baggage DoorsSDR FDEA201102010445Frame · corrodedREAR FUSELAGE FRAME 87- 89, STR 16L, HORIZ STAB CUTOUT. INNER FWD STRAP HAS EXFOLIATION CORROSION APPROX 4 IN. R & R THS CUTOUT FWD UPPER FITTING IAW DWG A53985135 AND SRM 51-40-21.Feb 1, 2011 · N423FE · Airbus A310203 · Fuselage Main, FrameSDR FDEA201101310424Skin · damaged.5" X .5" SHALLOW PUNCTURE ON RUDDER LT OUTER SKIN ABOUT 22" AFT OF THE NR 4 ATTACH FITTING. REPAIRED RUDDER L/T OUTER SKIN ABOUT 22" AFT OF THE NR4 ATTACH FITTING IAW SRM 55-41-12 PARA 30 WET LAYUP REPAIR. NO CORE DAMAGE EXIST AT 22" AFT OF NR4 ATTACH FITTIJan 31, 2011 · N423FE · Airbus A310203 · Rudder, Plate/SkinSDR FDEA201101300418Rib · corrodedLT WING RIB 5 FWD LUG HAS CORROSION. REPAIRED IAW EA 6-5710-145518 WING-AD 2008-17-02 - WING GEAR RIB 5 FWD LUG BORE REWORK (LT SIDE), SB A310-57-2090, EO 6-5710-7-5010.Jan 30, 2011 · N423FE · Airbus A310203 · Emergency Flotation SectionSDR FDEA201101300417Rib · corrodedRT WING, RIB 5, FWD LUG HAS CORROSION REPAIRED IAW EA 6-5710-145517, WING-AD2008-17-02, WING GEAR, RIB5 FWD LUG BORE REWORK (RT SIDE), SB A310-57-2090, EO 6-5710-7-5010.Jan 30, 2011 · N423FE · Airbus A310203 · Emergency Flotation SectionSDR FDEA201101280401Profile · crackedBULK CARGO LONGITUDINAL PROFILE CRACKED 1" PN A53974259202, FR64 - 65 24" LT OF CTR OF ACFT. R & R LONGITUDINAL PROFILE FR 64 TO FR65 Y805 IAW SRM 51-72-10, PGS 1-3.Jan 28, 2011 · N423FE · Airbus A310203 · Fuselage Miscellaneous StructureSDR FDEA201101270386Seat Track · corrodedAFT SEAT TRACK 1 HAS CORROSION FR 71 TO FR 75 (ABOUT 70 SQUARE INCH). REMOVED CORROSION FROM SEAT TRACK IAW SRM 51-74-10, CHECKED LIMITS IAW SRM 53-10-16, PAGE 101-103. FOUND TO BE OUT OF LIMITS. REMOVED SEAT TRACK NR1 BETWEEN FR71 & FR 75, FABRICATED SEAT Jan 27, 2011 · N423FE · Airbus A310203 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201101270385Skin · dentedUPON REMOVAL OF RUBSTRIP ON NR N00391 RT WING OTBD FLAP UPPER MAIN SKIN BETWEEN RIBS 4 AND 5 ALSO BETWEEN THE MAIN SPAR CHORD AND REAR SPAR CORD HAS 8 DENTS WHICH 2 EA ARE VISABLE UNDER THE RUBSTIPS. DAMAGE IS IN A 10 IN X 12 IN AREA. CUTOUT DAMAGE AREA ANJan 27, 2011 · N423FE · Airbus A310203 · Trailing Edge FlapsSDR FDEA201101210330Channel · corrodedFRAME LOCATION 87, BETWEEN STR 15 AND 16 FOUND CORROSION ON LT SIDE AFT UPPER "U" CHANNEL (CROSS STRUT). 1 AREA OF CORROSION ON UPPER FLANGE APPROX 1 SQ IN. R & R CROSS STRUT AT FR87 BETWEEN STR15 AND 16 IAW SRM 51-40-21.Jan 21, 2011 · N423FE · Airbus A310203 · Fuselage Miscellaneous Structure
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