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 FDEA201206022056Skin · misrepairedSKIN MISREPAIRED, REPAIRED IAW SRM 53-10-12, FIG 225, SHEET 1, PAGES 357 TO 362. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.Jun 2, 2012 · N403FE · Airbus A310203 · Fuselage Main, Plate/SkinSDR FDEA201206022061Floor Support · misrepairedFLOOR SUPPORT LONGERON 3L BETWEEN FRAMES 12A TO 15A MISREPAIRED. REMOVED AND REPLACED FLOOR SUPPORT IAW SRM 51-72-10. REPAIR IS A MAJOR IAW GMM 6-2-100.Jun 2, 2012 · N403FE · Airbus A310203 · Fuselage Miscellaneous StructureSDR FDEA201206022060Seat Track · misrepairedSEAT TRACK 5L Y1959 BETWEEN FRAMES 15A TO 17 MISREPAIRED. R & R SEAT TRACK IAW SRM 51-72-10, PAGES 1 TO 3. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.Jun 2, 2012 · N403FE · Airbus A310203 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201206022062Floor Support · misrepairedFLOOR SUPPORT MISREPAIRED. REMOVED FLOOR SUPPORT ASSY AND INSTALLED NEW IAW SRM 51-72-10 PAGES 1 TO 3. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.Jun 2, 2012 · N403FE · Airbus A310203 · Fuselage Miscellaneous StructureSDR FDEA201206022059Floorbeam · misrepairedFLOORBEAM MISREPAIRED. REPAIRED PER SRM 53-10-15 FIG 203 SHEETS 1-2 PG'S 245-252.Jun 2, 2012 · N403FE · Airbus A310203 · Fuselage Main, Floor BeamSDR FDEA201206022055Skin · failedSKIN AT FRAMES 35 TO 36 & BETWEEN STRINGERS 54 LT TO 54 RT MISREPAIRED. REPAIRED SKIN WITH NEW DOUBLER IAW SRM 53-10-12, FIG 225, SHEET 1, PAGES 357 TO 362.Jun 2, 2012 · N403FE · Airbus A310203 · Fuselage Main, Plate/SkinSDR FDEA201206012050Floor Panel · crackedFLOOR PANEL 231CF HAS 28 INCHES OF CHAFFING SKIN & A 7 INCH CRACK. FABRICATED REPLACEMENT FLOOR PANEL IAW DWG SRZ 25-005, REV J.Jun 1, 2012 · N403FE · Airbus A310203 · Fuselage Floor PanelSDR FDEA201206012049Floor Panel · chafedFLOOR PANEL 231EF HAS THIRTY TWO SQUARE INCHES OF CHAFFING ON UPPER SKIN. FABRICATED REPLACEMENT FLOOR PANEL IAW DWG SRZ 25-005, REV J.Jun 1, 2012 · N403FE · Airbus A310203 · Fuselage Floor PanelSDR FDEA201206012047Floor Panel · crackedFLOOR PANEL 252WH HAS ONE, NINE INCH CRACK, FABRICATED REPLACEMENT FLOOR PANEL IAW DWG SRZ 25-005 REV JJun 1, 2012 · N403FE · Airbus A310203 · Fuselage Floor PanelSDR FDEA201206012046Floor Panel · crackedFLOOR PANEL 252PH HAS ONE, TEN INCH CRACK. FABRICATED REPLACEMENT FLOOR PANEL IAW DWG SRZ 25-005, REV J.Jun 1, 2012 · N403FE · Airbus A310203 · Fuselage Main, StructureSDR FDEA201206012045Floor Panel · damagedFLOOR PANEL 251RT BROKEN ACROSS ENTIRE MID-SECTION OF PANEL FABRICATED. REPLACEMENT FLOOR PANEL IAW DWG SRZ 25-005, REV J.Jun 1, 2012 · N403FE · Airbus A310203 · Fuselage Floor PanelSDR FDEA201205292006Floor Panel · delaminatedFORWARD CARGO COMPARTMENT FLOOR PANEL 131ZF HAS FOUR AREAS OF DELAMINATION ON EDGES. FABRICATED REPLACEMENT FLOOR PANEL IAW DWG SRZ 25-005, REV J.May 29, 2012 · N403FE · Airbus A310203 · Fuselage Floor PanelSDR FDEA201205292005Floor Panel · damagedFORWARD CARGO COMPARTMENT FLOOR PANEL 131QF HAS PUNCTURE ALONG AT TIRE EDGE (BACK SIDE). FABRICATEDED FLOOR PANEL IAW DWG SRZ 25-005, REV J.May 29, 2012 · N403FE · Airbus A310203 · Fuselage Floor PanelSDR FDEA201203311201Pressure Switch · failedNR 2 ENGINE FUEL FILTER CLOG ECAM/ MASTER CAUTION IMMEDIATELY AFTER TAKE OFF. ECAM CAUTION EXTINGUISHED AROUND 80 PERCENT N1 WHEN THROTTLES RETARDED. REMOVED AND INSPECTED NR 2 ENGINE FUEL FILTER. NO DEBRIS FOUND. INSTALLED NEW FILTER IAW MM 73-12-03-02.Mar 31, 2012 · N430FE · Airbus A310203 · Engine Fuel Indicating SystemSDR FDEA201203130923Computer · inoperativeFLAP SYS 1 FAULT LIGHT IN FLIGHT RELEASED FOR SERVICE IAW MEL: 27-51-01-01 CATEGORY: C, "MEL 27-51-01-01: NR 2 SLATS/ FLAPS CONTROL COMPUTER - INOP. SLAT/FLAP WING TIP BRAKE TEST HAS BEEN ACCOMPLISHED." SFCC PN 49-079-05 (SYS NR 1) GOOD. SFCC PN 49-079-05 Mar 13, 2012 · N436FE · Airbus A310203 · Trailing Edge Flap Control SystemSDR FDEA201203130922Handle · dirtyFLAP/SLAT HANDLE FAILED TO MOVE PAST 15/0 SETTING ON RETRACTION AND 20/20 SETTING ON LANDING. T/S SFCC FAULTED SUPPLY PSW. PARTS ID ARE FOR T/S, ADDITIONAL PARTS MAY BE REQUIRED. HIGH PRESS SW. REMOVED FLAP/SLAT HANDLE, CLEANED SPRING AND RE-ASSEMBLE. OPMar 13, 2012 · N425FE · Airbus A310203 · Trailing Edge Flap Control SystemSDR FDEA201202070508Pin · misinstalledAFTER TAKEOFF, FLAP LEVER WOULD NOT RETRACT BEYOND 15/0 POSITION. LEVER WOULD NOT DROP DOWN INTO GATE. SLAT/FLAP POSITION REMAINED AT 15/15. ON APPROACH, FLAPS CAME TO 20/20, BUT LEVER WOULD NOT GO INTO 30/40 POSITION. CHECKED UNDER CENTER PEDESTAL FOR DEFeb 7, 2012 · N425FE · Airbus A310203 · Trailing Edge Flap Control SystemSDR FDEA201201130164Skin · failedR1 DOOR AFT EXTERNAL SKIN PANEL REQUIRES REMOVAL TO SUPPORT FRAME 16A REPAIR. SKIN PANEL TO BE REPLACED AFTER FRAME 16A REPAIR. R & R R1 AFT EXTERNAL SKIN PANEL IAW SRM 51-72-10, 51-40-21 AND 51-40-44.Jan 13, 2012 · N425FE · Airbus A310203 · Fuselage Main, Plate/SkinSDR FDEA201201110098Failsafe · failedR1 DOOR FAILSAFE RING REQUIRES REMOVAL TO FOM FARME 16A RT FRAME REPAIR. REMOVED FAIL SAFE RING IAW SRM 51-40-21 AND EA 6-5310-135257B. LOCATED AND DRILLED NEW FAIL SAFE RING AT R1 DOOR IAW DWG 12R53610899 AND SRM 51-40-44. INSTALLED NEW FAIL SAFE RING AT R1Jan 11, 2012 · N425FE · Airbus A310203 · Fuselage Main, StructureSDR FDEA201201050027Frame · damagedFRAME 16A RT DAMAED. REMOVED FRAME IAW SRM 51-40-21, PG 1 AND EA 6-5310-135257B. LOCATED AND DRILLED NEW FRAME IAW SRM 51-40-44, PG 9. INSTALLED NEW FRAME IAW SRM 51-40-21, PG 19 AND EA 6-5310-135257B, STEP 18, PG 4.Jan 5, 2012 · N425FE · Airbus A310203 · Fuselage Main, FrameSDR FDEA201201050026Depressor · damagedR1 DOOR FRAME 16A SEAL DEPRESSOR DAMAGED FRAME 16A. REPAIR REMOVED SEAL DEPRESSOR IAW SRM 51-72-10. LOCATED AND DRILLED NEW SEAL DEPRESSOR IAW A310 51-40-44. INSTALLED NEW SEAL DEPRESSOR IAW SRM 51-40-21 AND 51-72-10.Jan 5, 2012 · N425FE · Airbus A310203 · Fuselage Miscellaneous StructureSDR FDEA201111225002Duct · leakingDURING CLIMB ECAM ALERT RECEIVED FOR NR 1 BLEED LEAK COMPLIED WITH ECAM QRH. DIVERTED TO AVOID ICING. REMOVED AND REPLACED NR 1 SYS ANTI-ICE DUCT IN PYLON PER AMM 20-26-00-000. PERFORMED LEAK CHECK WITH APU AIR, FOUND NO LEAKS AT DUCT. ACFT OK FOR SERVICENov 22, 2011 · N411FE · Airbus A310203 · Air Intake Anti/De-Ice SystemSDR FDEA201111225003Warning Light · illuminatedDURING CLIMB, ECAM ALERT RECEIVED FOR NR 1 BLEED LEAK, COMPLIED WITH ECAM QRH. DIVERTED TO AVOID ICING. OPENNov 22, 2011 · N411FE · Airbus A310203 · Pneumatic Distribution SystemSDR FDEA201111164941Flap System · stickingON CLIMB OUT, AFTER SLATS RETRACT, KRUGER FLAP DID NOT RETRACT. RE-CYCLED AND KRUGER WOULD NOT RETRACT. ACCOMPLISHED CHECKLIST AND RETURNED TO DEPARTURE. BITE TESTED SFCC 1. FAULTED LT RETRACT SWITCH. FOUND LT RETRACT SWITCH TO BE STICKING FREED STUCK SWNov 16, 2011 · N436FE · Airbus A310203 · Leading Edge Slat Control SystemSDR FDEA201109213999Actuator · failedFAILURE OF THE MLG DOOR ACTUATOR AS NOTED ON EA 6-5310-145668. R & R RT MLG DOOR FITTING AND ACTUATOR IAW EA 6-5310-145668. REF N00005 AND N00010 FOR ALL WORK PERFORMED.Sep 21, 2011 · N404FE · Airbus A310203 · Landing Gear Door ActuatorSDR FDEA201109203977Support Bracket · crackedOFF ACFT PART, RT KEELBEAM AT FR 61, HYD LINE SUPPORT BRACKET CRACKED FROM HOLE TO CORNER 1 IN LONG VERIFIED MATERIAL, FABBED BRACKET IAW DWG A534100616, HEAT TREATED IAW SRM 51-25-00, ROCKWELL TESTED IAW SRM 51-28-10, CONDUCTIVITY TESTED IAW NTM 51-10-17, ASep 20, 2011 · N404FE · Airbus A310203 · Fuselage Miscellaneous StructureSDR FDEA201109063710Skin · misrepairedSKIN AT R1 PASSENGER DOOR LOWER AT FS 1187 FRAME 14A. MISREPAIRED. REPAIR CARRIED OUT AS PER E.A. 6-5210-143668, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 112.Sep 6, 2011 · N431FE · Airbus A310203 · Fuselage Main, Plate/SkinSDR FDEA201109013620Floorboard · delaminatedKEELBEAM IN WHEEL WELL HAS FLOORBOARD 147AF HAS 5 SQ IN APPROX DELAMINATION ON EDGE FABRICATED FLOORBOARD 147AF IAW DWG SRZ 25-005, REV J MAJOR REPAIR IAW GMM6-2-000.Sep 1, 2011 · N404FE · Airbus A310203 · Fuselage Floor PanelSDR FDEA201108263514Floor Panel · brokenFORWARD CARGO FLOOR PANEL 132YF FOUND BROKEN. FLOOR PANEL REMOVED AND REPLACED AS PER AMM 53-10-29 REV.30 FLOOR PANEL FABRICATED AS PER DWG SRZ-25-005 REV J. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REV 112.Aug 26, 2011 · N431FE · Airbus A310203 · Fuselage Floor PanelSDR FDEA201108263492Support Fitting · crackedRT WING NR 2 FLAP TRACK FORWARD FIXED FAIRING FORWARD SUPPORT FITTING FOUND CRACKED. REMOVED AND REPLACED AS PER SRM 51-40-21 REV 79. REPAIR CLASSIFIED MINOR AS PER GMM 6-2-100 REV 112.Aug 26, 2011 · N431FE · Airbus A310203 · Trailing Edge FlapsSDR FDEA201108263491Support Fitting · brokenRT WING NR 3 FLAP TRACK FORWARD FIXED FAIRING FWD SUPPORT FITTING BROKEN. REMOVED AND REPLACED AS PER SRM 51-40-21 REV 79. FUEL LEAK CHECK CARRIED OUT AS PER AMM 28-11-00-05-0 REV 30. FOUND SATISFACTORY. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100 REV 112.Aug 26, 2011 · N431FE · Airbus A310203 · Trailing Edge FlapsSDR FDEA201108263513Floor Panel · damagedMAIN DECK CARGO COMPARTMENT BETWEEN FRAME 53 AND FRAME 54 RT OTBD FLOOR PANEL FOUND DAMAGED. FABRICATED FLOOR PANEL PER DWG SRZ 35-005 REV J AND INSTALLED AS PER AMM 53-10-25 REV 30. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REV 112.Aug 26, 2011 · N431FE · Airbus A310203 · Fuselage Floor PanelSDR FDEA201108253468Spar · crackedHIGH FREQUENCY EDDY CURRENT INSPECTION CARRIED OUT AND FOUND RT WING REAR SPAR LOWER CHORD NEAR RIB 1 HAS A CRACKED INDICATION. RT WING REAR SPAR REAMED TO DIAMETER 0.560" IAW EO 6-5710-7-3322 PART 1, WORK STEP 4.G. HIGH FREQUENCY EDDY CURRENT INSPECTION CARRAug 25, 2011 · N431FE · Airbus A310203 · Wing SparSDR FDEA201108253467Spar · crackedHIGH FREQUENCY EDDY CURRENT OPEN HOLE INSP CARRIED OUT AND FOUND HOLE ITEM 29 ON RT WING REAR SPAR, NEAR RIB 1 WITH CRACK INDICATION. RT WING REAR SPAR CRACKED FASTENER HOLE REAMED TO DIAMETER 0.560 INCH IAW EO 6-5710-7-3322, PART 1, WORK STEP 4G. HIGH FREQAug 25, 2011 · N431FE · Airbus A310203 · Wing SparSDR FDEA201108253471Skin · damagedHIGH FREQUENCY EDDY CURRENT INSPECTION CARRIED OUT AT LT WING REAR SPAR AND FOUND DAMAGE. REPAIRED IAW EO 6-5710-7-3322 B1 PT 1. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100 REV112.Aug 25, 2011 · N431FE · Airbus A310203 · Wing, Plate/SkinSDR FDEA201108253470Spar · damagedHIGH FREQUENCY EDDY CURRENT INSPECTION CARRIED OUT AT LT CENTER TANK REAR SPAR AND FOUND DAMAGED AT APPROX 6 O`CLOCK. REPAIRED IAW EO 6-5710-7-3322B1 PT 1. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100 REV112.Aug 25, 2011 · N431FE · Airbus A310203 · Wing, Center BoxSDR FDEA201108253484Skin · crackedEVIDENCE OF FUSELAGE SKIN CRACK UNDER LAV SERVICE DOOR. REPAIRED IAW RDAS ISSUE A AND EA 6-5330-154038 PARTS 1 AND 2.Aug 25, 2011 · N429FE · Airbus A310203 · Fuselage Main, Plate/SkinSDR FDEA201108243464Bellcrank · failedDURING LANDING GEAR FREE FALL EXTENTION TEST PROCEDURES, THE LT AND RT MLG FAILED TO EXTEND AFTER HANDLE REACHED MAXIMUM ALLOWABLE TURNS OF 20.5. REMOVED AND REINSTALLED FLOOR PANELS FOR ACCESS IAW AMM 53-23-04. R & R FREE FALL CONTROL BELL CRANK IAW SRM 51-Aug 24, 2011 · N411FE · Airbus A310203 · Landing Gear Retraction/Extension SystemSDR FDEA201108243463Skin · corrodedCENTER WING BOX LT FR 49 HAS OXIDATION AT UPPER SURFACE BETWEEN STR 27-28. BELOW SEAT TRACK 6L DEFECT MEASURES 8 SQ INCHED IN THE CORNER. CLEANED UPPER SURFACE OF CWT BOX FR 49 STR 27-28 AT ST 6L IAW SRM 51-74-10. R & R FASTENER IAW SRM 51-40-21. REMOVED AAug 24, 2011 · N411FE · Airbus A310203 · Fuselage Main, Plate/SkinSDR FDEA201108243458Attach Fitting · corrodedCTR WING BOX BETWEEN SEAT TRACK L5-L6 HYD LINES ATTACHMENT FITTING CORRODED FR 49-50. CLEANED 6 EA LINES AND FITTING FOUND TO BE OUT OF LIMIT IAW AMM 12-21-12-02 R & R 6EA FITTING IAW 51-40-10 PRESSURE AND LEAK CK SATISFACTORY IAW AMM29 10-00-04.Aug 24, 2011 · N411FE · Airbus A310203 · Fuselage Main, Attach FittingsSDR FDEA201108233411Skin · damagedHIGH FREQUENCY EDDY CURRENT INSPECTION CARRIED OUT. LOWER FORWARD DOOR CUTOUT FOUND DAMAGED. REPAIRED IAW EO 6-5310-7-3318, PT 17. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100, REV 112.Aug 23, 2011 · N431FE · Airbus A310203 · Fuselage Main, Plate/SkinSDR FDEA201108233414Skin · damagedHIGH FREQUENCY EDDY CURRENT INSPECTION CARRIED OUT ON CREW DOOR CUTOUT & FOUND DAMAGED. REPAIRED IAW EO 6-5310-7-3318 PT 15. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100 REV 112.Aug 23, 2011 · N431FE · Airbus A310203 · Fuselage Main, Plate/SkinSDR FDEA201108233412Skin · damagedHIGH FREQUENCY EDDY CURRENT INSPECTION CARRIED OUT ON SKIN & FOUND DAMAGED. REPAIRED IAW EO 6-5310-7-3318 PT 15. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100 REV 112.Aug 23, 2011 · N431FE · Airbus A310203 · Fuselage Main, Plate/SkinSDR FDEA201108233410Skin · damagedHIGH FREQUENCY EDDY CURRENT OPEN HOLE INSP CARRIED OUT ON RT AFT CREW DOOR. UPPER FORWARD CUTOUT FOUND DAMAGED. REPAIRED PER EO#6-5310-7-3318 PT 18 STEP 8. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100 REV 112.Aug 23, 2011 · N431FE · Airbus A310203 · Fuselage Main, Plate/SkinSDR FDEA201108193388Panel · corrodedRT ELEVATOR, L/E PANEL 345DT, OTBD LANDING HAS 1 EA CORRODED FASTNER HOLE, 2EA MISDRILLED HOLES, AND CORROSION ON THE WEB ATTACHMENT STRAP. REMOVED LEVEL 1 CORROSION AT RT ELEVATOR L/E PANEL FASTNER HOLE AND WEB ATTACHMENT STRAP IAW SRM 51-74-10, PAGE 204. FAug 19, 2011 · N435FE · Airbus A310203 · Elevator, Plate/SkinSDR FDEA201108183365Skin · gougedRT WING FIX L/E IS GOUGED APPROX 6" LONG BETWEEN SLAT TRACK 5 AND 6, FROM CONTACT WITH NR 2 SLAT LOWER SKIN FASTENERS. SMOOTHED AND BLENDED AREA IAW SRM 51-75-10 AT RT WING FIX L/E SLAT TRACK 5 AND 6. NDT FOR CRACK AND LIMITS, NO LIMIT REMAINING THICKNESS.Aug 18, 2011 · N435FE · Airbus A310203 · Wing, Plate/SkinSDR FDEA201108183356Skin · gougedRT HORIZONTAL STAB L/E PANEL 341AB, EXTERNAL SKIN SCRATCHED AND GOUGED, ENTIRE LENGTH OF INBD EDGE. BLENDED OUT AREAS (4EA) ON RT HORIZONTAL STAB L/E PANEL 341AB EXTERNAL SKIN IAW SRM 51-73-10; CHECKED LIMITS FOUND AREAS (3EA) WITHIN LIMITS, 1 AREA OUT OF LAug 18, 2011 · N435FE · Airbus A310203 · Horizontal Stabilizer, Plate/SkinSDR FDEA201108173304Floorbeam · crackedFORWARD CARGO COMPARTMENT MAIN DECK FLOORBEAM AT FRAME 36, RBL 27 FOUND CRACKED. REPAIR CARRIED OUT AS PER SRM 53-10-15 FIG.203 SHT 1 REV. 18 REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REV 112.Aug 17, 2011 · N431FE · Airbus A310203 · Fuselage Main, Floor BeamSDR FDEA201108173303Attach Fitting · corrodedLT WING RIB 5 FWD LUG BORE DIAMETER HAS CORROSION THAT HAS EXCEEDED MAX ALLOWABLE REWORK DIMENSIONS "4.8405 IN". REMOVED LEVEL 1 CORROSION FROM LT WING RIB 5 BY OVERSIZING THE BORE AND SPOT FACING THE AFT LUG FACE, NDT INSPECTED (NIL FINDING) INCLUDED ACID Aug 17, 2011 · N435FE · Airbus A310203 · Wing, Attach FittingsSDR FDEA201108163289Adapter · crackedCLEVIS ADAPTER AT FR 46 BETWEEN SEAT TRACKS 2R & 3R IS CRACKED APPROX.2" LONG AT FWD & AFT FLANGE. R & R CLEVIS ADAPTER AT FR 46, BETWEEN TRACKS 2R AND 3R IAW SRM 51-72-10, PG. 1-3.Aug 16, 2011 · N435FE · Airbus A310203 · Fuselage Main, Attach Fittings
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