N431FE

Service difficulty reports · 69

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 = 'N431FE' 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 FDEA201301080054Unknown · unknownATS LEVER TRIPPED OFF AT TOGA ON TAKEOFF. RESET ATS LEVER AND SELECTED TOGA AGAIN, SAME RESULT. ABORTED TAKEOFF. AT BLOCK IN CREW REPORTED THAT AFTER RESETTING YAW DAMP AND TRIM SWITCHES, AUTOTHROTTLE OPERATED NORMALLY THE WHOLE FLT. PERFORMED MTP TEST ANJan 8, 2013 · N431FE · Airbus A310203 · Auto Throttle SystemSDR FDEA201210103586Actuator · leakingDURING RETRACTION OF THE LANDING GEAR, LEFT ECAM ANNUNCIATED GREEN HYD SYS QUANTITY/PRESSURE LOSS. COMPLIED WITH ECAM AND QRH MANUALLY EXTENDING THE LANDING GEAR FOR UNEVENTFUL LANDING AT DEPARTURE AIRPORT. FOUND LT KRUGER FLAP ACTUATOR SWIVEL BLOWN OUT. Oct 10, 2012 · N431FE · Airbus A310203 · Leading Edge Slat ActuatorSDR 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 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 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 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 FDEA200905091594Computer · malfunctionedON TAKEOFF ROLL AT ABOUT 75 KNOTS ATS LEVER TRIPPED OFF DISPLAYED ECAM MESSAGE. REJECTED TAKEOFF COMPLIED WITH QRH AND ECAM. ATS LEVER WOULD NOT RESET. COMPLIED WITH MEL AND DEPARTED WITH ATS LEVER OFF. REMOVED AND REPLACED THE TCC PER MM 22-36-34-4 AFS TMay 9, 2009 · N431FE · Airbus A310203 · Auto Throttle SystemSDR FDEA200905091593Computer · malfunctionedOAK - ON TAKEOFF ROLL AT ABOUT 75 KNOTS ATS LEVER TRIPPED OFF DISPLAYED ECAM MESSAGE. REJECTED TAKEOFF COMPLIED WITH QRH AND ECAM. ATS LEVER WOULD NOT RESET. COMPLIED WITH MEL AND DEPARTED WITH ATS LEVER OFF. R & R THE TCC IAW MM 22-36-34-4 AFS TEST AND LMay 9, 2009 · N431FE · Airbus A310203 · Auto Throttle SystemSDR FDEA200903130916Structure · corrodedLWR SURFACE OF CENTER WING BOX LT SIDE AT FR 47 BETWEEN SUPPORT STRUCTURE Y953 AND Y1456 HAS APPROX 12 SQ IN OF CORROSION EXTENDING UNDER 12 EA LOCK FASTENERS. DESEALED, CLEANED AND RESEALED 20 EA FASTENER CWT BOTTOM SURFACE LT SIDE ON FR 47 IAW SRM 51-76-20,Mar 13, 2009 · N431FE · Airbus A310203 · Wing, Center BoxSDR FDEA200903130915Support · corrodedLWR SURFACE OF CENTER WING BOX LT SIDE AT FR 47 BETWEEN SUPPORT STRUCTURE Y1456 AND Y1908 HAS APPROX 20 SQ IN OF CORROSION EXTENDING UNDER 18 EA LOCK FASTENER. DESEALED, CLEANED AND RESEALED 18 FASTENERS CWT BOTTOM SURFACE LT SIDE ON FR 47 IAW A310 SRM 51-76-Mar 13, 2009 · N431FE · Airbus A310203 · Wing, Center BoxSDR FDEA200903120912Fitting · corrodedNR 2 PYLON SPIGOT BEARING RECEPTACLE CORRODED REMOVED AND REPLACED NR 2 PYLON SPIGOT FITTING PER EA NR 6-5450-124230.Mar 12, 2009 · N431FE · Airbus A310203 · Nacelle/Pylon Miscellaneous StructureSDR FDEA200903120911Fitting · corrodedNR 1 PYLON SPIGOT RECEPTACLE FITTING HAS CORROSION ON INSIDE THE HOLE. REMOVED AND REPLACED NR 1 PYLON SPIGOT FITTING PER EA NR 6-5450-124229.Mar 12, 2009 · N431FE · Airbus A310203 · Nacelle/Pylon Miscellaneous StructureSDR FDEA200903100878Frame · chafedLT FRAME 34, STRINGER 14, FRAME HAS CHAFE MARK ON OUTSIDE RADIUS OF CORNER .015 INCH DEEP FRAME THICKNESS AT .245 INCH. BLENDED AREA AND PERFORMED REPAIR AT FR 34, STRINGER 14 LT IAW EA 6-5310-124228, RELEASE DATE 18 FEBRUARY, 2009.Mar 10, 2009 · N431FE · Airbus A310203 · Fuselage Main, FrameSDR FDEA200903100877Frame · chafedLT FRAME 34, STRINGER 13 - FRAME HAS CHAFE MARK ON OUTSIDE RADIUS OF CORNER .014 INCH DEEP FRAME THICKNESS AT .245 INCH. BLENDED AREA AND PERFORMED REPAIR AT FR 34, STRINGER 13 LT IAW EA 6-5310-124228, RELEASE DATE 18 FEBRUARY, 2009.Mar 10, 2009 · N431FE · Airbus A310203 · Fuselage Main, FrameSDR FDEA200903100876Frame · chafedLT FRAME 34,STRINGER 16 - FRAME HAS CHAFE MARK ON OUTSIDE RADIUS OF CORNER. .187 IN DIA BY .075 DEEP FRAME THICKNESS AT .245 INCH. BLENDED AREA AND PERFORMED REPAIR AT FR 34, STRINGER 16 LT IAW EA 6-5310-124228, RELEASE DATE 18 FEBRUARY, 2009.Mar 10, 2009 · N431FE · Airbus A310203 · Fuselage Main, FrameSDR FDEA200903060855Lug · corrodedRT WING MLG BAY RIB NR 5 FWD LUG HAS CORROSION IN HOLE BORE AND ON FWD AND AFT SPOTFACE. REMOVED LEVEL 1 CORROSION AND REPAIRED RT RIB NR 5 LUG IAW EA 6-5710-124226 .Mar 6, 2009 · N431FE · Airbus A310203 · Wing, Attach FittingsSDR FDEA200903060854Lug · corrodedLT WING MLG BAY RIB NR 5 FWD LUG HAS CORROSION IN HOLE BORE AND ON FWD AND AFT SPOTFACE. REMOVED LEVEL 1 CORROSION AND REPAIRED LT RIB NR 5 LUG IAW EA 6-5710-124226.Mar 6, 2009 · N431FE · Airbus A310203 · Wing, Attach FittingsSDR FDEA200903060853Seat Track · gougedMAIN DECK SEAT TRACK NR 5 LT HAS 2 GOUGED SCALLOPS LOCATED 5 INCHES AFT OF FR 54.2 AND 12 INCHES AFT OF FR 54.2. REMOVED AND REPLACED SEAT TRACK SECTION AT TRACK NR 5 LT BETWEEN FR 54.2 AND FR 58 IAW A310-200 SRM 51-72-10.Mar 6, 2009 · N431FE · Airbus A310203 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA200902270765Web · crackedAVIONICS COMPARTMENT RT UPPER FLOOR STRUCTURE BETWEEN FR 9 AND 10 INTERCOSTAL WEB HAS 1 INCH CRACK AT FWD LOWER CORNER. REMOVED AND FABRICATED WEB IAW DWG A553610270. INSTALLED WEB IAW A310-200 SRM 51-40- 21.Feb 27, 2009 · N431FE · Airbus A310203 · Fuselage Miscellaneous StructureSDR FDEA200902270749Floorbeam · corrodedMAIN CABIN FLOORBEAM FR 14 LT, Y1600 HAS CORROSION ON TOP CAP. .030 IN DEEP BY 2.50 IN BY .500 IN. REMOVED LEVEL 1 CORROSION. REWORKED AREA AFTER CORROSION REMOVED AND INSTALLED FLOOR CROSSBEAM FLANGE REPAIR AT FR 14 LT, Y1600 IAW A310 SRM 53-12-15, FIG 206Feb 27, 2009 · N431FE · Airbus A310203 · Fuselage Main, Floor BeamSDR FDEA200902260743Seat Track · damagedMAIN DECK CARGO COMPT SEAT TRACK 2R HAS SCALLOPS BROKEN OUT AT FR 62 REMOVED DAMAGED TRACK AND REPLACED WITH NEW TRACK SECTION IAW SRM 53-10-16 FIG 202.Feb 26, 2009 · N431FE · Airbus A310203 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA200902260742Seat Track · damagedMDCC SEAT TRACK 4R HAS ELONGATED SCALLOPS AT FR 62. REPLACED SEAT TRACK 4R FROM FR 62 TO FR 65 IAW SRM 51-23-10 AND 51-75-10 AND SRM 53-10-16 FIG 208 SHEET 1. INSTALLED REPLACEMENT SEAT TRACK AND SPLICED IAW SRM 53-10-16 FIG 208.Feb 26, 2009 · N431FE · Airbus A310203 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA200902260740Seat Track · damagedMDCC SEAT TRACK 2R HAS SCALLOPS BROKEN OUT AT FR 60 REMOVED DAMAGED TRACK AND REPLACED WITH NEW TRACK SECTION IAW SRM 53-10-16 FIG 202.Feb 26, 2009 · N431FE · Airbus A310203 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA200902230674Skin · dentedLOWER FUSELAGE SKIN BETWEEN FR 57/58 AND FR 59,STRINGER 42 RT HAS 1 DENT MEASURING 2.00 INCH BY 1.00 INCH BY .038 IN DEEP. EVALUATED AND DETERMINED DENT TO BE OUT OF LIMITS IAW SRM 53-10-00,TABLE 102. REMOVED DAMAGED SECTION OF SKIN AND INSTALLED EXTERNAL Feb 23, 2009 · N431FE · Airbus A310203 · Fuselage Main, Plate/SkinSDR 08FDEA02820Fitting · looseON CLIMB-OUT PASSING 15000 FT GOT NR 2 BLEED FAULT. COMPLIED WITH ECAM, RETURNED TO DFW. FOUND SENSE LINE FOR NUMBER 2 ENG PNEU PRESSURE REGULATOR LOOSE AT PYLON FITTING SECURED FITTING. PERFORMED FUNCTIONAL CHECK OF THE NUMBER 2 ENG BLEED REF MM 36-11-00-6Jul 10, 2008 · N431FE · Airbus A310203 · Pneumatic Distribution SystemSDR 07FDEA02437Unknown · unknownIN CRUISE FLT, LT INNER FUEL GAUGE READ 5 K LESS THAN RT. RAN CK LIST RESET SYSTEM C/B'S IAW QRH STILL SHOWED IMBALANCE. DIVERTED DUE TO SUSPECTED LEAK. WING DIPPED ON FINAL AS IF RIGHT WING WAS HEAVY. GAUGES SHOWED 6000 LB LOSS IN LEFT INNER IN CHOCKS. CKJul 11, 2007 · N431FE · Airbus A310203 · Aircraft Fuel SystemSDR 06FDEA04097Seat Track · wornSTRUCTURES-A300/A310 REPAIR IDENTIFICATION AND SUPPLEMENTAL MAINTENANCE COMPLY WITH EO 6-5100-7-5000 REV NR B POS PT1. CABIN FLOOR TRACK Y-450 WORN BETWEEN FRAMES 60 AND 61. REPAIRED PER SRM 53-10-16 FIG 208 SHEET 1. REPAIR EVALUATED PER GMM 6-2-100 AND CLNov 22, 2006 · N431FE · Airbus A310203 · Fuselage, Seat/Cargo Attach FittingsSDR 06FDEA04096Seat Track · wornSTRUCTURES-A300/A310 REPAIR IDENTIFICATION AND SUPPLEMENTAL MAINTENANCE COMPLY WITH EO 6-5100-7-5000 REV NR B POS PT1. CABIN, FLOOR TRACK Y-952 WORN BETWEEN FRAMES 60 AND 61. REPAIRED PER SRM 53-10-16 FIG 208 SHEET 1. REPAIR EVALUATED PER GMM 6-2-100 AND CNov 22, 2006 · N431FE · Airbus A310203 · Fuselage, Seat/Cargo Attach FittingsSDR 06FDEA04089Seat Track · wornSTRUCTURES-A300/A310 REPAIR IDENTIFICATION AND SUPPLEMENTAL MAINTENANCE COMPLY WITH EO 6-5100-7-5000 REV NR B POS PT1. CABIN FLOOR TRACK Y-450 WORN BETWEEN FRAMES 60 AND 61. REPAIRED PER SRM 53-10-16 FIG 208 SHEET 1.Nov 22, 2006 · N431FE · Airbus A310203 · Fuselage, Seat/Cargo Attach FittingsSDR 06FDEA04088Seat Track · wornSTRUCTURES-A300/A310 REPAIR IDENTIFICATION AND SUPPLEMENTAL MAINTENANCE COMPLY WITH EO 6-5100-7-5000 REV NR B POS PT1. CABIN FLOOR TRACK Y-952 WORN BETWEEN FRAMES 60 AND 61 REPAIRED PER SRM 53-10-16 FIG 201 SHEET 1.Nov 22, 2006 · N431FE · Airbus A310203 · Fuselage, Seat/Cargo Attach FittingsSDR 06FDEA04087Floorbeam · crackedSTRUCTURES-A300/A310 REPAIR IDENTIFICATION AND SUPPLEMENTAL MAINTENANCE COMPLY WITH EO 6-5100-7-5000 REV NR B POS PT1. CABIN FLOOR,TRANSVERSAL BEAM BETWEEN TRACKS Y-450 AND Y-953 AT FRAME 44 FOUND CRACKED REPLACED PER AMM 53-10-00.Nov 22, 2006 · N431FE · Airbus A310203 · Fuselage Main, Floor BeamSDR 06FDEA04086Skin · dentedREPAIR IDENTIFICATION AND SUPPLEMENTAL MAINTENANCE COMPLY WITH EO 6-5100-7-5000 REV NR B POS PT1. DENT BETWEEN FS 64-65 AND BETWEEN STRINGER 42-43 RT SEE N462 FOR RDF DATA WAS REPAIRED PER SRM 53-10-12 FIG 226 SHEET 2 SPECIFIC MAINTENANCE REQUIREMENTS. REPANov 22, 2006 · N431FE · Airbus A310203 · Fuselage Main, Plate/SkinSDR 06FDEA04085Skin · dentedREPAIR IDENTIFICATION AND SUPPLEMENTAL MAINTENANCE COMPLY WITH EO 6-5100-7-5000 REV NR B POS PT1. DENT BETWEEN FS 64-65 AND BETWEEN STRINGER 40-41 RT REPAIRED PER SRM 53-10-12 FIG 226 SHEET 2. REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS "MAJOR".Nov 22, 2006 · N431FE · Airbus A310203 · Fuselage Main, Plate/SkinSDR 06FDEA04084Floorbeam · crackedSTRUCTURES-A300/A310 REPAIR IDENTIFICATION AND SUPPLEMENTAL MAINTENANCE COMPLY WITH EO 6-5100-7-5000 REV NR B POS PT1. CABIN, FLOOR TRANSVERSAL BEAM BETWEEN TRACKS Y-450 AND Y-953 AT FRAME 43 FOUND CRACKED REPLACED PER AMM 53-10-00.Nov 22, 2006 · N431FE · Airbus A310203 · Fuselage Main, Floor BeamSDR 06FDEA03885Stringer · misrepairedREPAIR IDENTIFICATION AND SUPPLEMENTAL MAINTENANCE COMPLY WITH EO 6-5100-7-5000 REV NR B POS PT1. PREVIOUS STRINGER REPAIR FOUND IN AFT PIT, LT SIDE, FS 3437-3484, FS 64 AND STRINGER 56. REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION AND IF THE REPNov 4, 2006 · N431FE · Airbus A310203 · Fuselage Main, Longeron/StringerSDR 06FDEA03868Skin · misrepairedSTRUCTURES-A300/A310 REPAIR IDENTIFICATION AND SUPPLEMENTAL MAINTENANCE COMPLY WITH EO 6-5100-7-5000 REV NR B POS PT1. PREVIOUS COMPOSITE REPAIR FOUND LOCATED ON RT ELEVATOR LOWER SURFACE AFT OF NUMBER 5 ATTACH POINT. REPAIR REQUIRES EVALUATION REPAIR EVALNov 4, 2006 · N431FE · Airbus A310203 · Elevator, Plate/SkinSDR 06FDEA03865Skin · misrepairedSTRUCTURES-A300/A310 REPAIR IDENTIFICATION AND SUPPLEMENTAL MAINTENANCE COMPLY WITH EO 6-5100-7-5000 REV NR B POS PT1. BY: 067708 (N252) PREVIOUS COMPOSITE REPAIR FOUND LOCATED ON RT INB FLAP, UPPER SURFACE OUTB END, FLAP RIB 19. REPAIR REQUIRES EVALUATION Nov 4, 2006 · N431FE · Airbus A310203 · Trailing Edge FlapsSDR 06FDEA03866Skin · misrepairedSTRUCTURES-A300/A310 REPAIR IDENTIFICATION AND SUPPLEMENTAL MAINTENANCE COMPLY WITH EO 6-5100-7-5000 REV NR B POS PT1. PREVIOUS COMPOSITE REPAIR LOCATED ON RT WING LEADING EDGE, WS 1182, RIB 19, REPAIR LOCATED BETWEEN NUMBER 2 AND 3 SLAT. REPAIR REQUIRES EVNov 4, 2006 · N431FE · Airbus A310203 · Wing, Plate/SkinSDR 06FDEA03882Skin · misrepairedPREVIOUS REPAIR FOUND LOCATED ON R1 DOOR LOWER AFT END FS 1260 AND FR 16 EXTERNAL DOUBLER. REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA EXISTING REPAIR EVALUATED AND FOUND NOT TO CONFORMNov 4, 2006 · N431FE · Airbus A310 · Passenger/Crew DoorsSDR 06FDEA03881Skin · misrepairedPREVIOUS REPAIR FOUND LOCATED ON R1 DOOR LOWER FWD END FS 1187 AND FR 14A EXTERNAL DOUBLER. REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. EXISTING REPAIR EVALUATED AND FOUND NOT TO CONFONov 4, 2006 · N431FE · Airbus A310 · Passenger/Crew Doors
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