# Service difficulty reports: N431FE

A list on [N431FE](https://openairdocs.org/aircraft/N431FE.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Page 1 of 2 · 69 reports

- [SDR FDEA201301080054](https://openairdocs.org/sdr/FDEA201301080054.md): Unknown · unknown · Jan 8, 2013 · N431FE · Airbus A310203 · Auto Throttle System
  > ATS 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 AN
- [SDR FDEA201210103586](https://openairdocs.org/sdr/FDEA201210103586.md): Actuator · leaking · Oct 10, 2012 · N431FE · Airbus A310203 · Leading Edge Slat Actuator
  > DURING 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.
- [SDR FDEA201109063710](https://openairdocs.org/sdr/FDEA201109063710.md): Skin · misrepaired · Sep 6, 2011 · N431FE · Airbus A310203 · Fuselage Main, Plate/Skin
  > SKIN 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.
- [SDR FDEA201108263514](https://openairdocs.org/sdr/FDEA201108263514.md): Floor Panel · broken · Aug 26, 2011 · N431FE · Airbus A310203 · Fuselage Floor Panel
  > FORWARD 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.
- [SDR FDEA201108263492](https://openairdocs.org/sdr/FDEA201108263492.md): Support Fitting · cracked · Aug 26, 2011 · N431FE · Airbus A310203 · Trailing Edge Flaps
  > RT 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.
- [SDR FDEA201108263491](https://openairdocs.org/sdr/FDEA201108263491.md): Support Fitting · broken · Aug 26, 2011 · N431FE · Airbus A310203 · Trailing Edge Flaps
  > RT 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.
- [SDR FDEA201108263513](https://openairdocs.org/sdr/FDEA201108263513.md): Floor Panel · damaged · Aug 26, 2011 · N431FE · Airbus A310203 · Fuselage Floor Panel
  > MAIN 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.
- [SDR FDEA201108253468](https://openairdocs.org/sdr/FDEA201108253468.md): Spar · cracked · Aug 25, 2011 · N431FE · Airbus A310203 · Wing Spar
  > HIGH 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 CARR
- [SDR FDEA201108253467](https://openairdocs.org/sdr/FDEA201108253467.md): Spar · cracked · Aug 25, 2011 · N431FE · Airbus A310203 · Wing Spar
  > HIGH 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 FREQ
- [SDR FDEA201108253471](https://openairdocs.org/sdr/FDEA201108253471.md): Skin · damaged · Aug 25, 2011 · N431FE · Airbus A310203 · Wing, Plate/Skin
  > HIGH 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.
- [SDR FDEA201108253470](https://openairdocs.org/sdr/FDEA201108253470.md): Spar · damaged · Aug 25, 2011 · N431FE · Airbus A310203 · Wing, Center Box
  > HIGH 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.
- [SDR FDEA201108233411](https://openairdocs.org/sdr/FDEA201108233411.md): Skin · damaged · Aug 23, 2011 · N431FE · Airbus A310203 · Fuselage Main, Plate/Skin
  > HIGH 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.
- [SDR FDEA201108233414](https://openairdocs.org/sdr/FDEA201108233414.md): Skin · damaged · Aug 23, 2011 · N431FE · Airbus A310203 · Fuselage Main, Plate/Skin
  > HIGH 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.
- [SDR FDEA201108233412](https://openairdocs.org/sdr/FDEA201108233412.md): Skin · damaged · Aug 23, 2011 · N431FE · Airbus A310203 · Fuselage Main, Plate/Skin
  > HIGH 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.
- [SDR FDEA201108233410](https://openairdocs.org/sdr/FDEA201108233410.md): Skin · damaged · Aug 23, 2011 · N431FE · Airbus A310203 · Fuselage Main, Plate/Skin
  > HIGH 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.
- [SDR FDEA201108173304](https://openairdocs.org/sdr/FDEA201108173304.md): Floorbeam · cracked · Aug 17, 2011 · N431FE · Airbus A310203 · Fuselage Main, Floor Beam
  > FORWARD 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.
- [SDR FDEA200905091594](https://openairdocs.org/sdr/FDEA200905091594.md): Computer · malfunctioned · May 9, 2009 · N431FE · Airbus A310203 · Auto Throttle System
  > 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. REMOVED AND REPLACED THE TCC PER MM 22-36-34-4 AFS T
- [SDR FDEA200905091593](https://openairdocs.org/sdr/FDEA200905091593.md): Computer · malfunctioned · May 9, 2009 · N431FE · Airbus A310203 · Auto Throttle System
  > OAK - 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 L
- [SDR FDEA200903130916](https://openairdocs.org/sdr/FDEA200903130916.md): Structure · corroded · Mar 13, 2009 · N431FE · Airbus A310203 · Wing, Center Box
  > LWR 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,
- [SDR FDEA200903130915](https://openairdocs.org/sdr/FDEA200903130915.md): Support · corroded · Mar 13, 2009 · N431FE · Airbus A310203 · Wing, Center Box
  > LWR 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-
- [SDR FDEA200903120912](https://openairdocs.org/sdr/FDEA200903120912.md): Fitting · corroded · Mar 12, 2009 · N431FE · Airbus A310203 · Nacelle/Pylon Miscellaneous Structure
  > NR 2 PYLON SPIGOT BEARING RECEPTACLE CORRODED REMOVED AND REPLACED NR 2 PYLON SPIGOT FITTING PER EA NR 6-5450-124230.
- [SDR FDEA200903120911](https://openairdocs.org/sdr/FDEA200903120911.md): Fitting · corroded · Mar 12, 2009 · N431FE · Airbus A310203 · Nacelle/Pylon Miscellaneous Structure
  > NR 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.
- [SDR FDEA200903100878](https://openairdocs.org/sdr/FDEA200903100878.md): Frame · chafed · Mar 10, 2009 · N431FE · Airbus A310203 · Fuselage Main, Frame
  > LT 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.
- [SDR FDEA200903100877](https://openairdocs.org/sdr/FDEA200903100877.md): Frame · chafed · Mar 10, 2009 · N431FE · Airbus A310203 · Fuselage Main, Frame
  > LT 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.
- [SDR FDEA200903100876](https://openairdocs.org/sdr/FDEA200903100876.md): Frame · chafed · Mar 10, 2009 · N431FE · Airbus A310203 · Fuselage Main, Frame
  > LT 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.
- [SDR FDEA200903060855](https://openairdocs.org/sdr/FDEA200903060855.md): Lug · corroded · Mar 6, 2009 · N431FE · Airbus A310203 · Wing, Attach Fittings
  > RT 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.
- [SDR FDEA200903060854](https://openairdocs.org/sdr/FDEA200903060854.md): Lug · corroded · Mar 6, 2009 · N431FE · Airbus A310203 · Wing, Attach Fittings
  > LT 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.
- [SDR FDEA200903060853](https://openairdocs.org/sdr/FDEA200903060853.md): Seat Track · gouged · Mar 6, 2009 · N431FE · Airbus A310203 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN 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.
- [SDR FDEA200902270765](https://openairdocs.org/sdr/FDEA200902270765.md): Web · cracked · Feb 27, 2009 · N431FE · Airbus A310203 · Fuselage Miscellaneous Structure
  > AVIONICS 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.
- [SDR FDEA200902270749](https://openairdocs.org/sdr/FDEA200902270749.md): Floorbeam · corroded · Feb 27, 2009 · N431FE · Airbus A310203 · Fuselage Main, Floor Beam
  > MAIN 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 206
- [SDR FDEA200902260743](https://openairdocs.org/sdr/FDEA200902260743.md): Seat Track · damaged · Feb 26, 2009 · N431FE · Airbus A310203 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN 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.
- [SDR FDEA200902260742](https://openairdocs.org/sdr/FDEA200902260742.md): Seat Track · damaged · Feb 26, 2009 · N431FE · Airbus A310203 · Fuselage, Seat/Cargo Attach Fittings
  > MDCC 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.
- [SDR FDEA200902260740](https://openairdocs.org/sdr/FDEA200902260740.md): Seat Track · damaged · Feb 26, 2009 · N431FE · Airbus A310203 · Fuselage, Seat/Cargo Attach Fittings
  > MDCC 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.
- [SDR FDEA200902230674](https://openairdocs.org/sdr/FDEA200902230674.md): Skin · dented · Feb 23, 2009 · N431FE · Airbus A310203 · Fuselage Main, Plate/Skin
  > LOWER 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
- [SDR 08FDEA02820](https://openairdocs.org/sdr/08FDEA02820.md): Fitting · loose · Jul 10, 2008 · N431FE · Airbus A310203 · Pneumatic Distribution System
  > ON 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 36-11-00-6
- [SDR 07FDEA02437](https://openairdocs.org/sdr/07FDEA02437.md): Unknown · unknown · Jul 11, 2007 · N431FE · Airbus A310203 · Aircraft Fuel System
  > IN 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. CK
- [SDR 06FDEA04097](https://openairdocs.org/sdr/06FDEA04097.md): Seat Track · worn · Nov 22, 2006 · N431FE · Airbus A310203 · Fuselage, Seat/Cargo Attach Fittings
  > STRUCTURES-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 CL
- [SDR 06FDEA04096](https://openairdocs.org/sdr/06FDEA04096.md): Seat Track · worn · Nov 22, 2006 · N431FE · Airbus A310203 · Fuselage, Seat/Cargo Attach Fittings
  > STRUCTURES-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 C
- [SDR 06FDEA04089](https://openairdocs.org/sdr/06FDEA04089.md): Seat Track · worn · Nov 22, 2006 · N431FE · Airbus A310203 · Fuselage, Seat/Cargo Attach Fittings
  > STRUCTURES-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.
- [SDR 06FDEA04088](https://openairdocs.org/sdr/06FDEA04088.md): Seat Track · worn · Nov 22, 2006 · N431FE · Airbus A310203 · Fuselage, Seat/Cargo Attach Fittings
  > STRUCTURES-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.
- [SDR 06FDEA04087](https://openairdocs.org/sdr/06FDEA04087.md): Floorbeam · cracked · Nov 22, 2006 · N431FE · Airbus A310203 · Fuselage Main, Floor Beam
  > STRUCTURES-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.
- [SDR 06FDEA04086](https://openairdocs.org/sdr/06FDEA04086.md): Skin · dented · Nov 22, 2006 · N431FE · Airbus A310203 · Fuselage Main, Plate/Skin
  > REPAIR 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. REPA
- [SDR 06FDEA04085](https://openairdocs.org/sdr/06FDEA04085.md): Skin · dented · Nov 22, 2006 · N431FE · Airbus A310203 · Fuselage Main, Plate/Skin
  > REPAIR 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".
- [SDR 06FDEA04084](https://openairdocs.org/sdr/06FDEA04084.md): Floorbeam · cracked · Nov 22, 2006 · N431FE · Airbus A310203 · Fuselage Main, Floor Beam
  > STRUCTURES-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.
- [SDR 06FDEA03885](https://openairdocs.org/sdr/06FDEA03885.md): Stringer · misrepaired · Nov 4, 2006 · N431FE · Airbus A310203 · Fuselage Main, Longeron/Stringer
  > REPAIR 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 REP
- [SDR 06FDEA03868](https://openairdocs.org/sdr/06FDEA03868.md): Skin · misrepaired · Nov 4, 2006 · N431FE · Airbus A310203 · Elevator, Plate/Skin
  > STRUCTURES-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 EVAL
- [SDR 06FDEA03865](https://openairdocs.org/sdr/06FDEA03865.md): Skin · misrepaired · Nov 4, 2006 · N431FE · Airbus A310203 · Trailing Edge Flaps
  > STRUCTURES-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
- [SDR 06FDEA03866](https://openairdocs.org/sdr/06FDEA03866.md): Skin · misrepaired · Nov 4, 2006 · N431FE · Airbus A310203 · Wing, Plate/Skin
  > STRUCTURES-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 EV
- [SDR 06FDEA03882](https://openairdocs.org/sdr/06FDEA03882.md): Skin · misrepaired · Nov 4, 2006 · N431FE · Airbus A310 · Passenger/Crew Doors
  > PREVIOUS 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 CONFORM
- [SDR 06FDEA03881](https://openairdocs.org/sdr/06FDEA03881.md): Skin · misrepaired · Nov 4, 2006 · N431FE · Airbus A310 · Passenger/Crew Doors
  > PREVIOUS 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 CONFO

Next page: https://openairdocs.org/aircraft/N431FE/reports.md?page=2

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
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
```

This list as a web page: https://openairdocs.org/aircraft/N431FE/reports

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