N432FE, cancelled May 10, 2010

Service difficulty reports · 95

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 = 'N432FE' AND deregistration_id = 'N432FE-2010-05-10'
  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 FDEA200805221955Engine · failedON TAKEOFF ROLL SERIES OF POPS OR BANGS, SPEED LESS THAN 40 KTS, EXPERIENCED LT SWERVE, LOW SPEED REJECT. SOUNDED LIKE POSSIBLE COMPRESSOR STALL. GVI OF NR 1 ENG SHOWS VERY SMALL METAL PARTICLES APX 1MM SIZE IN TAILPIPE. ALSO SLIGHT INTERMITTENT SQUEAL W/May 22, 2008 · N432FE · Airbus A310203 · Engine (Turbine/Turboprop)SDR 08FDEA01955Engine · failedON TAKEOFF ROLL SERIES OF POPS OR BANGS, SPEED LESS THAN 40 KTS, EXPERIENCED LEFT SWERVE, LOW SPEED REJECT. SOUNDED LIKE POSSIBLE COMPRESSOR STALL. GVI OF NR 1 ENG SHOWS VERY SMALL METAL PARTICLES APX 1MM SIZE IN TAILPIPE. ALSO SLIGHT INTERMITTENT SQUEAL WMay 22, 2008 · N432FE · Airbus A310203 · Engine (Turbine/Turboprop)SDR 07FDEA03773Coupling · corrodedFOUND CORROSION AT COUPLING, C 65, P 56 LT. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.Sep 14, 2007 · N432FE · Airbus A310203 · Fuselage Miscellaneous StructureSDR 07FDEA03771Coupling · corrodedFOUND CORROSION AT COUPLING, C 70, P 37RT. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.Sep 14, 2007 · N432FE · Airbus A310203 · Fuselage Miscellaneous StructureSDR 07FDEA03770Coupling · corrodedFOUND CORROSION AT COUPLING, C 65, P 56 LT REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.Sep 14, 2007 · N432FE · Airbus A310203 · Fuselage Miscellaneous StructureSDR 07FDEA03769Plate · corrodedFOUND CORROSION AT GROUND VALVE PLATE C 24-25 , P52-55 LT. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.Sep 14, 2007 · N432FE · Airbus A310203 · Fuselage Miscellaneous StructureSDR 07FDEA03767Coupling · corrodedFOUND CORROSION AT COUPLING P 55RH, C 65. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.Sep 14, 2007 · N432FE · Airbus A310203 · Fuselage Miscellaneous StructureSDR 07FDEA03766Coupling · corrodedFOUND CORROSION AT COUPLING P 53LT, C 55/58 REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.Sep 14, 2007 · N432FE · Airbus A310203 · Fuselage Miscellaneous StructureSDR 07FDEA03765Fitting · corrodedFOUND CORROSION AF FITTING C 54.2, P 45-46 RT. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.Sep 14, 2007 · N432FE · Airbus A310203 · Fuselage Main, Attach FittingsSDR 07FDEA03764Fitting · corrodedFOUND CORROSION AF FITTING C 54.2, P 45-46 RT. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.Sep 14, 2007 · N432FE · Airbus A310203 · Fuselage Miscellaneous StructureSDR 07FDEA03756Coupling · corrodedFOUND CORROSION ON COUPLING P 50 RH, C 69. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.Sep 14, 2007 · N432FE · Airbus A310203 · Fuselage Miscellaneous StructureSDR 07FDEA03754Stringer · corrodedFOUND CORROSION ON STRINGER P 54 RT, C 68-69 STRINGER REPAIR PERFORMED IAW SRM 53-10-14 FIG 201.Sep 14, 2007 · N432FE · Airbus A310203 · Fuselage Main, Longeron/StringerSDR 07FDEA03751Coupling · corrodedCORROSION FOUND AT COUPLING AT C 65, P 57 RT. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.Sep 14, 2007 · N432FE · Airbus A310203 · Fuselage Miscellaneous StructureSDR 07FDEA03750Coupling · corrodedCORROSION FOUND AT COUPLING AT C 65, P 55 RT. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.Sep 14, 2007 · N432FE · Airbus A310203 · Fuselage Miscellaneous StructureSDR 07FDEA03747Coupling · corrodedCORROSION FOUND AT COUPLING AT C 26/32, P 45 RT REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.Sep 14, 2007 · N432FE · Airbus A310203 · Fuselage Miscellaneous StructureSDR 07FDEA03746Angle · corrodedCORROSION FOUND ON REINFORCING ANGLE AT C38-39, P 48 LT REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.Sep 14, 2007 · N432FE · Airbus A310203 · Fuselage Miscellaneous StructureSDR 07FDEA03672Panel · corrodedFOUND CRACK ON PYLON NR 2 AT RIB 8 INBOARD AND OUTBOARD SIDE AT PANEL (ABOUT 8MM) DOUBLER REPAIR ON SIDEWALL PANELS PERFORMED IAW SRM 5451-31 FIG 201.Sep 13, 2007 · N432FE · Airbus A310203 · Nacelle/Pylon, Attach FittingsSDR 07FDEA03646Beam · crackedFOUND CRACK ON LONGITUDINBAL BEAM C 74-76, P 11 LT/RT, (LT: 8MM, RT 15MM). REPAIR PERFORMED BY INSTALLING REPAIR ANGLES IAW SRM 53-181-18 FIG 204.Sep 13, 2007 · N432FE · Airbus A310203 · Fuselage Main, StructureSDR 07FDEA03684Skin · damagedDURING FUNCTION PHASE, THE RT INBOARD FLAP TRAILING EDGE WAS DAMAGED REPAIR PERFORMED IAW SRM 57-53-12 PARA 13 (FIG 209).Sep 13, 2007 · N432FE · Airbus A310203 · Trailing Edge FlapsSDR 07FDEA03707Flange · damagedFOUR MISDRILLED HOLES AT UPPER FLANGE (BEAM) AT C 33 LT. SPLICE REPAIR PERFORMED IAW SRM 53-10-15 FIG 207.Sep 13, 2007 · N432FE · Airbus A310203 · Fuselage Miscellaneous StructureSDR 07FDEA03705Flange · damagedTWO MISDRILLED HOLES AT UPPER FLANGE (BEAM) AT C 33 LT. SPLICE REPAIR PERFORMED IAW SRM 53-10-15 FIG 207.Sep 13, 2007 · N432FE · Airbus A310203 · Fuselage Miscellaneous StructureSDR 07FDEA03704Frame · corrodedFOUND CORROSION AT MILLING FRAME C60, P 22RT REPAIR PERFORMED BY BLEND OUT CORROSION IAW RAS/DATLS/0001942/2004.Sep 13, 2007 · N432FE · Airbus A310203 · Fuselage Main, FrameSDR 07FDEA03703Flange · corrodedCORROSION FOUND ON UPPER FLANGE C25. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10Sep 13, 2007 · N432FE · Airbus A310203 · Fuselage Miscellaneous StructureSDR 07FDEA03701Splice · corrodedFOUND CORROSION AT SPLICE C20, P50 RT. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.Sep 13, 2007 · N432FE · Airbus A310203 · Fuselage Miscellaneous StructureSDR 07FDEA03700Splice · crackedFOUND CORROSION AT SPLICE C20, P46 RT. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.Sep 13, 2007 · N432FE · Airbus A310203 · Fuselage Miscellaneous StructureSDR 07FDEA03697Rib · corrodedFOUND ON LT MLG FWD LUG INNER BORE RIB 5 THE BUSHING TO BE OUT OF ROUND, AFTER REMOVAL OF BUSHING FOUND CORROSION ON THE LUG REPAIR PERFORMED BY CORROSION REMOVAL AND REAM UP THE HOLE IAW DRAWING R572-49121, APPROVED BY EA 6-5751-8106 AND RAS/BAE/0979/2004 ISep 13, 2007 · N432FE · Airbus A310203 · Wing, Rib/BulkheadSDR 07FDEA03696Rib · corrodedFOUND ON RT MLG FWD LUG INNER BORE RIB 5 THE BUSHING TO BE OUT OF ROUND, AFTER REMOVAL OF BUSHING FOUND CORROSION ON THE LUG REPAIR PERFORMED BY CORROSION REMOVAL AND REAM UP THE HOLE IAW DRAWING R572-49121, APPROVED BY EA 6-5751-8106 AND RAS/BAE/0979/2004 ISSep 13, 2007 · N432FE · Airbus A310203 · Wing, Rib/BulkheadSDR 07FDEA03690Skin Panel · wornELONGATED HOLES FOUND ON RT WING TO PYLON HYDRAULIC FITTING RIB 8 REPAIR PERFORMED BY REAM UP AND BUSH INSTALLATION IAW DRAWING R572-49184, APPROVED BY EA 6-5720-79595 AND RAS/BAE/0931/2004 ISS A.Sep 13, 2007 · N432FE · Airbus A310203 · Wing, Plate/SkinSDR 07FDEA03688Skin Panel · wornFOUND ELONGATED HOLES ON LT WING TO PYLON HYDRAULIC FITTING HOLES RIB 8 REPAIR PERFORMED BY REAM UP AND INSTALL BUSHINGS IAW DRAWING R572-49184 , APPROVED BY EA 6-5720-79594 AND RAS/BAE/0931/2004 ISS A.Sep 13, 2007 · N432FE · Airbus A310203 · Wing, Plate/SkinSDR 07FDEA03686Vane · dentedFOUND DENT ON LT INBOARD FLAP VANE NOSE SKIN, RIB 7-8 REPAIR PERFORMED BY CUTTING THE DAMAGED AREA AND INSTALLING A NEW SKIN WITH INNER STRAPS IAW EA 6-5752-81059 AND RAS/DABRE/7004146/2004 ISS A.Sep 13, 2007 · N432FE · Airbus A310203 · Trailing Edge FlapsSDR 07FDEA03682Skin · delaminatedFOUND ON LT INBOARD FLAP LOWER SKIN AT TRAILING EDGE, RIB 3-4, DELAMINATION. IN THIS AREA FOUND ON UPPER SKIN AN OLD DOUBLER INSTALLED. REPAIR PERFORMED BY REMOVAL OF THE OLD REPAIR ON UPPER SKIN AND RENEW THE REPAIR ON LOWER AND UPPER SURFACE IAW SRM 57-Sep 13, 2007 · N432FE · Airbus A310203 · Trailing Edge FlapsSDR 07FDEA03681Skin · corrodedDURING REMOVAL OF BOLT 642, NOTED IN SB A310-57-2028 FOUND CORROSION INSIDE THE FITTING BORE, LT WING AREA OF RIB 5 REPAIR PERFORMED BY OVERSIZING THE HOLE IAW EA 6-5721-81050 AND RAS/BAE/0928/2004 ISS A.Sep 13, 2007 · N432FE · Airbus A310203 · Wing, Plate/SkinSDR 07FDEA03679Spar · corrodedCORROSION FOUND ON RT ELEVATOR FRONT SPAR WEB NEAR RIB 2A AROUND ONE BONDING POINT REPAIR PERFORMED BY BLENDOUT UNTIL CORROSION REMOVAL IAW EA 6-5520-79603 AND RAS/CASA/3692/2004 ISS A.Sep 13, 2007 · N432FE · Airbus A310203 · Elevator, Spar/RibSDR 07FDEA03675Skin · wornFOUND ON PYLON NR 1 AT RIB 8 INBOARD AND OUTBOARD SIDE THE HOLE FOR SUPPORT WORN DOUBLER REPAIR PERFORMED IAW SRM 54-51-31 FIG 201.Sep 13, 2007 · N432FE · Airbus A310203 · Nacelle/Pylon, Plate/SkinSDR 07FDEA03673Fitting · wornAT RT SPIGOT FITTING FWD OUTBOARD SIDE FOUND WEAR MARKS REPAIR PERFORMED BY BLEND OUT TO SMOOTH CONTOUR IAW EA 6-5720-79605 AND RAS/BAE/0818/2004 ISS A.Sep 13, 2007 · N432FE · Airbus A310203 · Wing Miscellaneous StructureSDR 07FDEA03671Attach Fitting · chafedFOUND CHAFING MARKS, ENLARGED HOLES AND NOT CORRECT INSTALLED BUSHINGS AT PYLON NR 2 PYLON TO WING ATTACH FITTING LUGS AT RIB 12. REPAIR PERFORMED BY OVERSIZING THE BORES AND INSTALLING NEW REPAIR BUSHS IAW DRAWING R571-40283, APPROVED BY EA 6-5450-81064 AND Sep 13, 2007 · N432FE · Airbus A310203 · Nacelle/Pylon, Attach FittingsSDR 07FDEA03667Fitting · corrodedFOUND CORROSION AT RUN OUT FITTING AT P 44, C16A-17A LT. REPAIR PERFORMED BY REPLACEMENT OF RUNOUT FITTING IAW DRAWING R536-10440.Sep 13, 2007 · N432FE · Airbus A310203 · Fuselage Main, Attach FittingsSDR 07FDEA03666Skin Panel · dentedFOUND DENT ON SKIN C 94-95, P3-4 RT OUT OF LIMIT. DOUBLER REPAIR PERFORMED IAW SRM 53-19-12 FIG 201.Sep 13, 2007 · N432FE · Airbus A310203 · Fuselage Main, Plate/SkinSDR 07FDEA03661Stringer · corrodedFOUND CORROSION ON STRINGER P 56 RT, C 64-65 OUT OF LIMIT STRINGER REPAIR PERFORMED IAW SRM 53-10-14 FIG 201.Sep 13, 2007 · N432FE · Airbus A310203 · Fuselage Main, Longeron/StringerSDR 07FDEA03660Floorbeam · corrodedFOUND CORROSION AT CROSSBEAM C 67, C66. CROSSBEAM REPAIR PERFORMED IAW SRM 53-10-15 FIG 207 .Sep 13, 2007 · N432FE · Airbus A310203 · Fuselage Main, Floor BeamSDR 07FDEA03657Stringer · corrodedFOUND CORROSION ON STRINGER P50 AT C80, LT. STRINGER REPAIR PERFORMED IAW SRM 53-10-14 FIG 201.Sep 13, 2007 · N432FE · Airbus A310203 · Fuselage Main, Longeron/StringerSDR 07FDEA03654Beam · corrodedCORROSION FOUND ON LOWER SILL BEAM OF AFT CARGO DOOR AT C59A. REPAIR PREFORMED BY TRIM OUT THE AFFECTED AREA AND FABRICATE A STRAP IAW EA 6-5310-79580 AND RAS/DATLS/0001970/2004 ISS A.Sep 13, 2007 · N432FE · Airbus A310203 · Fuselage Main, StructureSDR 07FDEA03652Skin Panel · corrodedCORROSION FOUND ON SKIN PANEL C78/80, P 45-50 RT, IN SERVICE PANEL AREA. REPAIR PERFORMED BY BLEND OUT UNTIL CORROSION REMOVAL AND REPLACING THE TOILET SERVICE DOOR WITH COVER A539-809076-200 IAW EA 6-5330-79575 AND RAS/DATLS/0001961/2004 ISS A.Sep 13, 2007 · N432FE · Airbus A310203 · Fuselage Main, Plate/SkinSDR 07FDEA03649Angle · corrodedFOUND CORROSION AFT PRESSURE BULKHEAD CIRCUMFERENTIAL STRAP, INNER RIM ANGLE AND FRAME COUPLING AT C80/82, P25LH TO 36RH. REPAIR PERFORMED BY CUT OUT OF DAMAGED PARTS, REINSTALLING NEW PARTS IAW DRAWING R539-70603, APPROVED BY 6-5318-79562 AND RAS/DAHAM/40182Sep 13, 2007 · N432FE · Airbus A310203 · Fuselage Miscellaneous StructureSDR 07FDEA03643Stringer · corrodedFOUND CORROSION ON STRINGER P 57 LT, C 69-70 OUT OF LIMIT. STRINGER REPAIR PERFORMED SRM 53-10-14 FIG 201.Sep 13, 2007 · N432FE · Airbus A310203 · Fuselage Main, Longeron/StringerSDR 07FDEA03639Stringer · corrodedFOUND CORROSION ON STRINGER CONNECTION AT C80, P 38 LT REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.Sep 13, 2007 · N432FE · Airbus A310203 · Fuselage Main, Longeron/StringerSDR 07FDEA03638Stringer · corrodedCORROSION FOUND AT STRINGER P38, C79-80. STRINGER REPAIR PERFORMED IAW SRM 53-10-14 FIG 201Sep 13, 2007 · N432FE · Airbus A310203 · Fuselage Main, Longeron/StringerSDR 07FDEA03636Skin Panel · corrodedCORROSION FOUND ON INTERNAL SKIN C-37-38, P55LT-55RT DOUBLER REPAIR PERFORMED IAW SRM 53-10-12 FIG 221 AND 203.Sep 13, 2007 · N432FE · Airbus A310203 · Fuselage Main, Plate/SkinSDR 07FDEA03635Stringer · corrodedFOUND CORROSION AT STRINGER P 37 RT, C37 STRINGER REPAIR PERFORMED IAW SRM 53-10-14 FIG 201.Sep 13, 2007 · N432FE · Airbus A310203 · Fuselage Main, Plate/SkinSDR 07FDEA03584Stringer · corrodedFOUND CORROSION ON CLIP AT C 71, P57-56RT. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.Sep 11, 2007 · N432FE · Airbus A310203 · Fuselage Main, Longeron/Stringer
Back to N432FE, cancelled May 10, 2010