N658FE

Service difficulty reports · 352

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 = 'N658FE' 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 FDEA201207282736Adapter · damagedMAIN DECK CARGO CLEVIS ADAPTER FR 51-52 BETWEEN SEAT TRACKS 2R AND 3R HAS ELONGATED FASTENER HOLES. R & R CLEVIS ADAPTER IAW SRM 51-72-10.Jul 28, 2012 · N658FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA201207282735Adapter · gougedMAIN DECK CARGO AT FR. 64 CLEVIS ADAPTER BETWEEN SEAT TRACK 1L AND 2L CROWN HAS GOUGE 1.0". R & R CLEVIS ADAPTER IAW SRM 51-72-10.Jul 28, 2012 · N658FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA201207282734Shear Plate · crackedFLOOR SHEAR WEB BETWEEN FR 79 AND FR 80 RT SIDE CRACKED. R & R SHEAR WEB IAW FSRM 51-72-10 PG2.Jul 28, 2012 · N658FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA201207282733Adapter · gougedFR 64 BETWEEN SEAT TRACKS 1R AND 2R CLEVIS ADAPTER HAS GOUGE .5". R & R CLEVIS ADAPTER FR 64 SEAT TRACKS 1R AND 2R IAW FSRM 51-72-10.Jul 28, 2012 · N658FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA201207282731Adapter · gougedMAIN DECK CARGO AT FR 71 CLEVIS ADAPTER BETWEEN SEAT TRACK 3R AND 4R CROWN GOUGED .5". R & R CLEVIS ADAPTER IAW SRM 51-72-10.Jul 28, 2012 · N658FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA201207272711Adapter · damagedCLEVIS ADAPTER SCALLOPS GOUGED 2 SQ". LOCATED FR 58 BETWEEN SEAT TRACKS 4L AND 5L. REMOVED CLEVIS ADAPTER ON FR 58 BETWEEN SEAT TRACK 4L AND 5L IAW SRM 51-72-10. LOCATED AND DRILLED ADAPTER IAW SRM 51-72-10. INSTALLED NEW ADAPTER SRM 51-72-10. REPROTECTEJul 27, 2012 · N658FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA201207262708Floorboard · damagedFLOORDBOARD 251BH, IMPACT DAMAGE 6" AT SURF AROUND CLEVIS CUT OUT. FABRICATED REPLACEMENT FLOORDBOARD IAW DWG SRZ 25-005, REV J.Jul 26, 2012 · N658FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201207262707Floorboard · damagedFLOORBOARD 252YG CRUSHED AT UPPER SURFACE AROUND CLEVIS ADAPTER CUTOUT. FABRICATED REPLACEMENT FLOORBOARD IAW DWG SRZ 25-005, REV J.Jul 26, 2012 · N658FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201207262706Floorboard · damagedFLOORBOARD 242ZJ, THREE AREAS AROUND THE CLEVIS OUTER PLY CRUSHED AND THREE BAD INSERTS. FABRICATED REPLACEMENT FLOORBOARD IAW DWG SRZ 25-00, REV J.Jul 26, 2012 · N658FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201207262705Floorboard · damagedFLOORBOARD 242EK, HAS IMPACT AT CLEVIS ADAPTOR CUT-OUT DEFECT MEASURES 10 INCHES LONG, UPPER SURFACE. FABRICATED REPLACEMENT FLOORBOARD IAW DWG SRZ 25-005, REV J.Jul 26, 2012 · N658FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201207262704Floorboard · crackedFLOORBOARD IDENTIFIED AS 232RG IS CRACKED DOWN THE WIDTH CENTER. FABRICATED REPLACEMENT FLOORBOARD IAW DWG SRZ 25-005, REV J.Jul 26, 2012 · N658FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201207262703Floorboard · damagedFLOORBOARD 252VF CRUSHED AT THE EDGE AND AROUND THE CLEVIS ADAPTOR CUT OUT. FABRICATED REPLACEMENT FLOORBOARD DWG SRZ 25-005, REV J.Jul 26, 2012 · N658FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201207262702Floor Panel · crackedMAIN CARGO DECK FLOOR PANEL NR 251 JF IS CRACKED IN HALF AT A44 CLEVIS AREA, FABRICATED REPLACEMENT FLOOR PANEL IAW DWG SRZ 25-005, REV J.Jul 26, 2012 · N658FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201207252668Floorbeam · corrodedFWD CARGO COMPT AT FR34, FLOORBEAM LOWER SURFACE HAS CORROSION. REMOVED CORROSION AND FOUND OUT OF LIMITS IAW SRM 51-24-10 PG 205. REMOVED DAMAGED SECTION FLOORBEAM, FABRICATED REPAIR ANGLES AND INSTALLED IAW WITH EA 6-5310-160164 AND DWG A53781959 AND SRM Jul 25, 2012 · N658FE · Airbus A300F4605R · Fuselage Main, Floor BeamSDR FDEA201207252667Seat Track · corrodedNR 1 SEAT TRACK FROM FR71.4 TO FR73 HAS COROSSION AND GOUGE ON CROWN. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-10-16 PG 105 FIG 102 , CUT AND REMOVED DAMAGED SECTION, SPLICE REPAIRED SEAT TRACK IAW SRM 53-10-16 PG 203 - 208 FIG 201.Jul 25, 2012 · N658FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201207252680Clevis · damagedCLEVIS ADAPTER AT FR61 BETWEEN SEAT TRACK 2R AND 3R SCALLOP IS BROKEN. R & R CLEVIS ADAPTER BETWEEN SEAT TRACK 2R AND 3R AT FR61 IAW SRM 51-72-10, PAGE 1-2.Jul 25, 2012 · N658FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA201207252677Floorboard · damagedFLOORBOARD 131QF HAS 45 INCHES OF EDGE DAMAGE. FABRICATED REPLACEMENT FLOORBOARD IAW DWG SRZ 25-005, REV J.Jul 25, 2012 · N658FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201207252676Floorboard · damagedFLOORBOARD 131SG HAS 1 X 9 INCH PIECE TORN OFF & 6 INCHES OF DELAMINATED. FABRICATED REPLACEMENT FLOORBOARD IAW DWG SRZ 25-005, REV J.Jul 25, 2012 · N658FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201207252675Floorboard · damagedFWD CARGO BAY FLOORBOARD 131NG HAS PUNCTURED, CRACKED & EDGE DISBONDED. FABRICATED REPLACEMENT FLOORBOARD IAW DWG SRZ 25-005, REV J.Jul 25, 2012 · N658FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201207252674Floorboard · damagedFLOORBOARD 252UH OUTER PLY AFT OF CUTOUT CRUSHED APPROX 6 INCHES. FABRICATED REPLACEMENT FLOORBOARD IAW DWG SRZ 25-005, REV J.Jul 25, 2012 · N658FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201207252673Floorboard · crackedFLOORBOARD 232YG HAS PUNCTURE AND CRACK ON FORWARD EDGE (5"), AND PUNCTURE AND CRACKED 8 INCHES AROUND CLEVIS ADAPTER CUTOUT. FABRICATED REPLACEMENT FLOORBOARD IAW DWG SRZ 25-055, REV J.Jul 25, 2012 · N658FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201207252672Floorboard · damagedFLOORBOARD 232JG HAS AREA OF IMPACT DAMAGE, 9", ON INBD SIDE, AND EDGE FILLER MISSING ALONG ENTIRE AFT EDGE. FABRICATED FLOORBOARD IAW DWG SRZ 25-005 REV J.Jul 25, 2012 · N658FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201207252671Floorboard · crackedFLOORBOARD 232HG HAS IMPACT DAMAGED AND CRACK (5") AT AFT OTBD CORNER. FABRICATED FLOORBOARD IAW DWG SRZ25-005, REV J.Jul 25, 2012 · N658FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201102090513Control Unit · unsecureSHORTLY AFTER T/O AT APPROX 600' ALL FLT CONTROL SPOILERS FAULTED. FOLLOWED ECAM TO SELECT THEM OFF. TRIED TO RESET, BUT THEY ALL REMAINED FAULTED. RETURNED TO DEPARTURE. FOUND LOWER EFCU (2CP) FALLING OUT OF RACK. INSTALLED COMPUTER BACK IN RACK. ALL OPFeb 9, 2011 · N658FE · Airbus A300F4605R · Drag Control SystemSDR FDEA201005031429Web · crackedNR 2 ENG /PYLON---PYLON WEB STRUCTURE IS CRACKED IN 2 PLACES AS SEEN THROUGH NACELLE ACCESS PANEL 421 CL. STOP DRILLED CRACKS IAW SRM 54-52-11. INSTALLED REPAIR IAW SRM 54-21-11, FIG 201, PGS 205 / 206, CONFIG 2 AND SRM 51-40-30. DISPLACED AND REINSTALLED WMay 3, 2010 · N658FE · Airbus A300F4605R · Nacelle/Pylon Miscellaneous StructureSDR FDEA201004231318Floor Support · corrodedMAIN CABIN FLOOR SUPPORT STRUCTURE IS CORRODED AT FRAME 13A TO FRAME 13A; LBL 18 TO LBL 18. REMOVED CORROSION IAW SRM 51-73-10, PG 207. ORIGINAL THICKNESS 0.079. REMOVED 0.028. MATERIAL REMAINING 0.051 AND FOUND TO BE OUT OF LIMITS IAW SRM 53-10-00. LOCATApr 23, 2010 · N658FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA201004231317Floor Support · corrodedMAIN CABIN FLOOR SUPPORT STRUCTURE IS CORRODED AT FRAME 13A TO FRAME 13A; LBL 18 TO LBL 18. REMOVED CORROSION IAW SRM 51-73-10, PG 207. ORIGINAL THICKNESS 0.079. REMOVED 0.028. MATERIAL REMAINING 0.051 AND FOUND TO BE OUT OF LIMITS IAW SRM 53-10-00. LOCATApr 23, 2010 · N658FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA201004221280Bolt · shearedLT WING / SIDE LOAD FITTING AFT INBD BOLT FOUND SHEARED AT THE SPAR INSIDE THE TANK. (FOUND WHILE CLEANING TANK FOR CLOSE). REMOVED BOLT IAW 51-40-21 PARA 5. PERFORMED BHEC INSP OF THE BOLT HOLE IAW NTM 51-10-01. NO CRACKS NOTED. INSTALLED NEW BOLT PART Apr 22, 2010 · N658FE · Airbus A300F4605R · Wing Main, Frame StructureSDR FDEA201004151197Wedge · crackedRT WING INBD FLAP TAIL AT RIB 25A IS CRACKED. FABRICATED AND BONDED NEW WEDGE SKIN; DOUBLER; SPAR BRACKET AND CORE OF END FLAP TAIL WEDGE PN 57960014 IAW EA 6-5750-136642 "WING - RT INBD FLAP T/E WEDGE AT RIB 25A"; DWG A57960014 AND TPS 1001 REV "E".Apr 15, 2010 · N658FE · Airbus A300F4605R · Trailing Edge FlapsSDR FDEA201004151194Floor Support · corrodedMAIN CABIN FLOOR SUPPORT STRUCTURE IS CORRODED FROM BS 14A TO BS 14A; RBL 9. FOUND SURFACE CORROSION OUT OF LIMITS PRE FREIGHTER SRM 53-10-16, PG 103. AFTER DAMAGED WAS REMOVED IAW SRM 51-73-10, PG 207, MAX ALLOWABLE MATERIAL WAS 0.012. MATERIAL REMOVED 0Apr 15, 2010 · N658FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA201004151193Cargo Track · brokenMAIN CABIN TIE DOWN TRACK SCALLOP IS BROKEN FROM FRAME 65 TO FRAME 65; RBL 48 TO RBL 48. REMOVED TIE DOWN ADAPTER IAW SRM 51-72-10. LOCATED AND DRILL HOLES IN NEW TIE DOWN ADAPTER PART NR A5327828821200, PO NR 679551.1 IAW SRM 51-72-10. INSTALLED NEW TIE DOApr 15, 2010 · N658FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201004141183Strip · crackedHORIZONTAL L/E PANEL 331 DB JOINT STRIP IS CRACKED AT RIB 33A. REMOVED JOINT STRIP IAW SRM 51-40-21, PARA 5. MATERIAL ID 2024-T3, 0.071, PO NR 618569.1. FOR THE DOUBLER AND 2024-T3 0.063, PO NR 652264.1 FOR THE FILLER IAW SRM 55-12-28. FABBED REPAIR IAW SRM Apr 14, 2010 · N658FE · Airbus A300F4605R · Horizontal Stabilizer Miscellaneous StructureSDR FDEA201004131175Track · damagedADAPTER TRACK IS DAMAGED AT FRAME 32; LBL 30. INSTALLED NEW ADAPTER TRACK IAW SRM 51-72-10.Apr 13, 2010 · N658FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA201004121158Skin · crackedFWD CARGO DOOR UPPER INNER SKIN IS CRACKED AND DENTED AT FRAME 24. COMPLIED WITH EA 6-5230-136647 "DOORS - FWD LOWER CARGO DOOR INNER SKIN AND FRAME 24 CRACK".Apr 12, 2010 · N658FE · Airbus A300F4605R · Cargo/Baggage DoorsSDR FDEA201004121153Web · crackedLT WING WEB A5796011424600 AT RIB 25A IS CRACKED R & R WEB REF SRM 51-40-21, PARA 7 AND SRM 51-72-10.Apr 12, 2010 · N658FE · Airbus A300F4605R · Wing Miscellaneous StructureSDR FDEA201004121151Skin · crackedRT INBD FLAP SKIN PANEL COVERING RIB 25A (REMOVED AT THE TIME OF INSP), INDICATES MULTIPLE CRACKS WITH EDDY CURRENT, ALL PROTRUDING FOR AND AFT ALONG RIB 25A LOCATION. LOCATED, DRILLED AND COUNTERSUNK SKIN SECTION REF SRM 51-72-10. FOR INSTALLATION SEE EO EApr 12, 2010 · N658FE · Airbus A300F4605R · Trailing Edge FlapsSDR FDEA201004091124Fitting · gougedRADOME INTERIOR FRAME LOWER RT CORNER IA GOUGED AT THE LATCH FITTING. REMOVED GUSSET IAW SRM 51-40-21, PARA 6, PG 7. FABRICATED GUSSET IAW DWG A92320606. ALODINED GUSSET IAW SRM 51-21-10, PARA A, PG 2. PRIMED GUSSET IAW SRM 51-23-10, PARA B, PG 2. PAINTED Apr 9, 2010 · N658FE · Airbus A300F4605R · Aerodynamic FairingsSDR FDEA201004091123Fitting · gougedRADOME INTERIOR FRAME; LOWER LT CORNER IS GOUGED AT THE LATCH FITTING. REMOVED GUSSET IAW SRM 51-40-21, PARA 6, PG 7. FABRICATED GUSSET IAW DWG A92320606. ALODINED GUSSET IAW SRM 51-21-10, PARA A, PG 2. PRIMED GUSSET IAW SRM 51-23-10, PARA B, PG 2. PAINTEApr 9, 2010 · N658FE · Airbus A300F4605R · Aerodynamic FairingsSDR FDEA201004081107Floor Support · corrodedFLOOR SUPPORT HAS CORROSION FROM FRAME 13 TO FRAME 14; LBL 20.Apr 8, 2010 · N658FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA201004081106Floor Panel · damagedMAIN CABIN 251 QH FLOOR PANEL IS DAMAGED. FABRICATED NEW FLOOR PANEL 251 QH IAW DWG SRZ 25-005, REV "H".Apr 8, 2010 · N658FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201004081105Frame · crackedLT SIDE CTR WING BOX LOWER SURFACE AT FRAME 47. ROTATING PROBE EDDY CURRENT INSP REVEALED INDICATION OF POSSIBLE CRACKS OR OTHER HOLE DAMAGE IN HOLES B, F, G, Q AND S. VISUAL INSP OF EACH HOLE REVEALS HOLE BORE DAMAGE IN AREAS OF INDICATIONS, MAKING TApr 8, 2010 · N658FE · Airbus A300F4605R · Wing, Center BoxSDR FDEA201004081104Elbow · looseLT WING NR 1 PYLON AFT END; 2 HYD ELBOWS ARE LOOSE. REMOVED HYD LINES AND FITTINGS IAW AMM 29-11-33-4 AND AMM 54-54-00-4 FROM THE NR 1 PYLON TO WING AREA. REPAIRED ELONGATED HOLES IAW EA 6-5730-136645. REINSTALLED LINES AND FITTINGS IAW AMM 54-54-00-4; AMApr 8, 2010 · N658FE · Airbus A300F4605R · Hydraulic System, MainSDR FDEA201004071091Support Angle · crackedAVONICS COMPARTMENT TRANSPONDER AND TCAS RACK; FWD/OTBD VERTICAL SUPPORT ANGLE IS CRACKED AT THE BASE. REMOVED PROTECTIVE COVER TO FOM IAW PMS 01-05-17. REMOVED SUPPORT ANGLE IAW SRM 51-72-10. RECEIVED NEW SUPPORT ANGLE PN A9253146900100, PO 678898.2. LOCATApr 7, 2010 · N658FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA201004071090Plate · dentedFWD CARGO COMPARTMENT DOOR; FWD LOWER CORNER IS DENTED. REMOVED LOWER FWD CORNER IAW SRM 51-40-21, PARA 6. RECEIVED NEW CORNER PN A5237008120600, PO 678647.1. LOCATED AND DRILLED IAW SRM 1-40-44. INSTALLED NEW CORNER IAW SRM 51-40-21, PARA 6.Apr 7, 2010 · N658FE · Airbus A300F4605R · Cargo/Baggage DoorsSDR FDEA201004061075Floor Panel · damagedMAIN CABIN FLOOR PANEL 252 VH IS DAMAGED. FABRICATED NEW FLOOR PANEL 252 VH IAW DWG SRZ 25-005, REV "H".Apr 6, 2010 · N658FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201004061074Floor Panel · damagedMAIN CABIN FLOOR PANEL 252 UH IS DAMAGED. FABRICATED NEW FLOOR PANEL 252 UH IAW DWG SRZ 25-005, REV "H".Apr 6, 2010 · N658FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201004061073Floor Panel · damagedMAIN CABIN FLOOR PANEL 251 UH IS DAMAGED. FABRICATED NEW FLOOR PANEL 251 UH IAW DWG SRZ 25-005, REV "H".Apr 6, 2010 · N658FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201004061072Floor Panel · damagedMAIN CABIN FLOOR PANEL 232 HG IS DAMAGED. FABRICATED NEW FLOOR PANEL 232 GH IAW DWG SRZ 25-005, REV "H".Apr 6, 2010 · N658FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201004061071Floor Panel · damagedMAIN CABIN FLOOR PANEL 232 YG IS DAMAGED. FABRICATED NEW FLOOR PANEL 232 YG IAW DWG SRZ 25-005, REV "H".Apr 6, 2010 · N658FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201004061070Floor Panel · damagedMAIN CABIN FLOOR PANEL 232 TG IS DAMAGED. FABRICATED NEW FLOOR PANEL 232 TG IAW DWG SRZ 25-005, REV "H".Apr 6, 2010 · N658FE · Airbus A300F4605R · Fuselage Floor Panel
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