N675FE

Service difficulty reports · 248

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 = 'N675FE' 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 08FDEA02685Floorboard · damagedMAIN CABIN FLOOR PANEL 231 JH UPPER SURFACE HAS PUNCTURES FROM BALL BEARINGS. REPAIRED DAMAGED FLOOR PANEL IN REF TO A300-600 SRM 53-10-20, FIG 202.Jul 3, 2008 · N675FE · Airbus A300F4605R · Fuselage Floor PanelSDR 08FDEA02684Floorboard · damagedMAIN CARGO DECK FLOOR PANEL 232 FG HAS NUMEROUS PUNCTURES AND BALL BEARINGS STUCK TO THE TOP SURFACE. REPAIRED DAMAGED FLOOR PANEL IN REF TO A300-600 SRM 53-10-20; FIG 201.Jul 3, 2008 · N675FE · Airbus A300F4605R · Fuselage Floor PanelSDR 08FDEA02683Floorboard · damagedMAIN CARGO DECK FLOOR PANEL 232 CF HAS NUMEROUS PUNCTURES AND BEARINGS IN THE TOP SURFACE. REPAIRED DAMAGED FLOOR PANEL IN REF TO A300-600 SRM 53-10-20; FIG 201.Jul 3, 2008 · N675FE · Airbus A300F4605R · Fuselage Floor PanelSDR 08FDEA02682Floorboard · damagedMAIN CARGO DECK FLOOR PANEL 232 GG HAS NUMEROUS PUNCTURES AND BEARINGS STUCK IN THE TOP SURFACE. REPAIRED DAMAGED FLOOR PANEL IN REF TO A300-600 SRM 53-10-20; FIG 202.Jul 3, 2008 · N675FE · Airbus A300F4605R · Fuselage Floor PanelSDR 08FDEA02681Floorboard · damagedMAIN CARGO DECK FLOOR PANEL 232 SG HAS PUNCTURES AND BALL BEARINGS STUCK TO THE TOP SURFACE. REPAIRED DAMAGED FLOOR PANEL IN REF TO A300-600 SRM 53-10-20; FIG 202.Jul 3, 2008 · N675FE · Airbus A300F4605R · Fuselage Floor PanelSDR 08FDEA02680Floorboard · damagedMAIN CARGO DECK FLOOR PANEL 232 TG HAS PUNCTURES AND BALL BEARINGS IN THE TOP SURFACE. REPAIRED DAMAGED FLOOR PANEL IN REF TO A300-600 SRM 53-10-20; FIG 202.Jul 3, 2008 · N675FE · Airbus A300F4605R · Fuselage Floor PanelSDR 08FDEA02679Floorboard · damagedMAIN CARGO DECK FLOOR PANEL 232 UG HAS BALL BEARINGS (4 PLACES) STUCK IN THE TOP SURFACE. REPAIRED DAMAGED FLOOR PANEL IN REF TO A300-600 SRM 53-10-20, FIG 202.Jul 3, 2008 · N675FE · Airbus A300F4605R · Fuselage Floor PanelSDR 08FDEA02678Floorboard · damagedMAIN CARGO DECK FLOOR PANEL NR 232 VH HAS BALL BEARINGS (2 PLACES) STUCK IN THE TOP SURFACE. REPAIRED DAMAGED FLOOR PANEL IN REF TO A300-600 SRM 53-10-20, FIG 202.Jul 3, 2008 · N675FE · Airbus A300F4605R · Fuselage Floor PanelSDR 08FDEA02677Floorboard · damagedMAIN CARGO DECK FLOOR PANEL 232 NG HAS BALL BEARINGS (2 PLACES) STUCK IN THE TOP SURFACE. REPAIRED DAMAGED FLOOR PANEL IN REF TO A300-600 SRM 53-10-20, FIG 202.Jul 3, 2008 · N675FE · Airbus A300F4605R · Fuselage Floor PanelSDR 08FDEA02676Floorboard · damagedMAIN CARGO DECK FLOOR PANEL FROM FRAME 22 TO FRAME 26, RBL 37 TO RBL 57 HAS NUMEROUS BALL BEARINGS STUCK AND PUNCTURES ON THE TOP SURFACE. REPAIRED DAMAGED FLOOR PANEL IN REF TO A300-600 SRM 53-10-20, FIG 202.Jul 3, 2008 · N675FE · Airbus A300F4605R · Fuselage Floor PanelSDR 08FDEA02675Floorboard · damagedBALL BEARINGS ARE EMBEDDED ON THE TOP SURFACE OF PANEL NR 232 GG, MAIN CARGO DECK. REPAIRED DAMAGED FLOOR PANEL IN REF TO A300-600 SRM 53-10-20, FIG 202.Jul 3, 2008 · N675FE · Airbus A300F4605R · Fuselage Floor PanelSDR 08FDEA02674Floorboard · damagedMAIN CARGO DECK FLOOR PANEL 232 RG HAS PUNCTURES AND BALL BEARINGS STUCK IN THE UPPER SURFACE. REPAIRED DAMAGED FLOOR PANEL IN REF TO A300-600 SRM 53-10-20; FIG 202.Jul 3, 2008 · N675FE · Airbus A300F4605R · Fuselage Floor PanelSDR 08FDEA02673Floorboard · damagedMAIN CARGO DECK FLOOR PANEL 232 PF HAS BALL BEARINGS STUCK IN THE TOP SURFACE AND PUNCTURES FROM FRAME 19 TO 22; RBL 57 TO RBL 77. REPAIRED DAMAGED AREAS PER A300-600 SRM 53-10-20; FIG 201.Jul 3, 2008 · N675FE · Airbus A300F4605R · Fuselage Floor PanelSDR 08FDEA02672Floorboard · damagedMAIN CABIN FLOOR PANEL 231 SG UPPER SURFACE HAS NUMEROUS PUNCTURES FROM BALL BEARINGS. REPAIRED DAMAGED FLOOR PANEL IN REF TO A300-600 SRM 53-10-20; FIG 202.Jul 3, 2008 · N675FE · Airbus A300F4605R · Fuselage Floor PanelSDR 08FDEA02671Floorboard · damagedMAIN CABIN FLOOR PANEL 231 TG UPPER SURFACE HAS NUMEROUS PUNCTURES FROM BALL BEARINGS. REPAIRED DAMAGED FLOOR PANEL IN REF TO A300-600 SRM 53-10-20; FIG 202.Jul 3, 2008 · N675FE · Airbus A300F4605R · Fuselage Floor PanelSDR 08FDEA02670Floorboard · damagedMAIN CABIN FLOOR PANEL 231 UG UPPER SURFACE HAS PUNCTURES FROM BALL BEARINGS. REPAIRED DAMAGED FLOOR PANEL IN REF TO A300-600 SRM 53-10-20; FIG 202.Jul 3, 2008 · N675FE · Airbus A300F4605R · Fuselage Floor PanelSDR 08FDEA02669Floorboard · damagedMAIN CABIN FLOOR PANEL 231 GG UPPER SURFACE HAS PUNCTURES FROM BALL BEARINGS AND THE EDGING COMPOUND IS MISSING FROM THE INBD CORNER. REPAIRED DAMAGED FLOOR PANEL IN REF TO A300-600 SRM 53-10-20; FIG 202.Jul 3, 2008 · N675FE · Airbus A300F4605R · Fuselage Floor PanelSDR 08FDEA02668Floorboard · damagedMAIN CABIN FLOOR PANEL 231 JG UPPER SURFACE HAS NUMEROUS PUNCTURES FROM BALL BEARINGS. REPAIRED DAMAGED FLOOR PANEL IN REF TO A300-600 SRM 53-10-20; FIG 202.Jul 3, 2008 · N675FE · Airbus A300F4605R · Fuselage Floor PanelSDR 08FDEA02667Floorboard · damagedMAIN CABIN FLOOR PANEL 231 FG HAS NUMEROUS PUNCTURES IN THE UPPER SURFACE FROM BALL BEARINGS. REPAIRED DAMAGED AREAS IAW A300-600 SRM 53-10-20; FIG 201.Jul 3, 2008 · N675FE · Airbus A300F4605R · Fuselage Floor PanelSDR 08FDEA02666Floorboard · damagedMAIN CABIN FLOOR PANEL 231 PG UPPER SURFACE HAS NUMEROUS PUNCTURES FROM BALL BEARINGS. REPAIRED DAMAGED FLOOR PANEL IN REF TO A300-600 SRM 53-10-20; FIG 202.Jul 3, 2008 · N675FE · Airbus A300F4605R · Fuselage Floor PanelSDR 08FDEA02665Floorboard · damagedMAIN CABIN FLOOR PANEL 231 WG UPPER SURFACE HAS NUMEROUS PUNCTURES FROM BALL BEARINGS. REPAIRED IAW A300-600 SRM 53-10-20; FIG 201.Jul 3, 2008 · N675FE · Airbus A300F4605R · Fuselage Floor PanelSDR 08FDEA02664Floorboard · damagedMAIN CABIN FLOOR PANEL 231 HG UPPER SURFACE HAS NUMEROUS PUNCTURES FROM BALL BEARINGS. REPAIRED DAMAGED FLOOR PANEL IN REF TO A300-600 SRM 53-10-20; FIG 202.Jul 3, 2008 · N675FE · Airbus A300F4605R · Fuselage Floor PanelSDR 08FDEA02663Floorboard · damagedMAIN CABIN FLOOR PANEL 231 GG IS PUNCTURED ON THE UPPER SURFACE IN MANY AREAS BY BALL BEARINGS. REPAIRED DAMAGED FLOOR PANEL IN REF TO A300-600 SRM 53-10-20; FIG 201.Jul 3, 2008 · N675FE · Airbus A300F4605R · Fuselage Floor PanelSDR 08FDEA02662Floorboard · damagedMAIN CABIN FLOOR PANEL 231 FG UPPER SURFACE IS PUNCTURED IN MANY AREAS BY BALL BEARINGS. REPAIRED DAMAGED FLOOR PANEL IN REF TO A300-600 MSRM 53-10-20; FIG 202.Jul 3, 2008 · N675FE · Airbus A300F4605R · Fuselage Floor PanelSDR 08FDEA02661Floorboard · damagedMAIN CABIN FLOOR PANEL NR 231 GH IS PUNCTURED ON THE UPPER SURFACE AREAS BY BALL BEARINGS. REPAIRED DAMAGED FLOOR PANEL IN REF TO A300-600 SRM 53-10-20; FIG 201.Jul 3, 2008 · N675FE · Airbus A300F4605R · Fuselage Floor PanelSDR 08FDEA02660Floorboard · damagedMAIN CABIN FLOOR PANEL NR 231 CF IS PUNCTURED IN MANY AREAS BY BALL BEARINGS. REPAIRED PER A300-600 SRM 53-10-20; FIG 201.Jul 3, 2008 · N675FE · Airbus A300F4605R · Fuselage Floor PanelSDR 08FDEA02659Floorboard · damagedMAIN CABIN FLOOR PANEL 231 DH IS WORN THROUGH THE TOP AND IS PUNCTURED. REPAIRED DAMAGED AREA IAW A300-600 SRM 53-10-20; FIG 201.Jul 3, 2008 · N675FE · Airbus A300F4605R · Fuselage Floor PanelSDR 08FDEA02658Floorboard · damagedFLOORBOARD PANEL NR 231 EP MAIN CABIN IS SCORED; GOUGED AND PUNCTURED. REPAIRED AREA PER A300-600 SRM 53-10-20; FIG 201.Jul 3, 2008 · N675FE · Airbus A300F4605R · Fuselage Floor PanelSDR 08FDEA02657Floorboard · damagedMAIN DECK FLOORBOARD NR 251 XG EDGE IS DETERIORATED. REPAIRED EDGE IAW FEDEX DWG SRZ 25-005, REV F.Jul 3, 2008 · N675FE · Airbus A300F4605R · Fuselage Floor PanelSDR 08FDEA02656Floorboard · damagedMAIN DECK FLOOR BOARD NR 251 XH IS CRACKED. REPAIRED DAMAGED AREA IAW A300-600 SRM 51-77-11.Jul 3, 2008 · N675FE · Airbus A300F4605R · Fuselage Floor PanelSDR 08FDEA02644Floor Panel · damagedMAIN CARGO DECK FLOOR PANEL 232 BH AT FRAME 28; RBL 97 HAS A BROKEN CORNER. FABBED A NEW PANEL IAW FEDEX DWG SRZ 25-005, REV F. MATERIAL ID A 402 H 35039-003IAW FEDEX DWG SRZ 25-005, REV F.Jul 3, 2008 · N675FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR 08FDEA02648Floor Panel · damagedMAIN DECK FLOORBOARD 262 HF IS BROKEN. FABBED A NEW PANEL IAW FEDEX DWG SRZ 25-005, REV F. MATERIAL ID A 402 H 35039-003 IAW FEDEX DWG SRZ 25-005, REV F. PART MARKED IAW FEDEX GMM 7-0-1000.Jul 3, 2008 · N675FE · Airbus A300F4605R · Fuselage Floor PanelSDR 08FDEA02647Floor Panel · damagedMAIN DECK FLOORBOARD 252 DH EDGE IS BROKEN. FABBED A NEW FLOOR PANEL IAW FEDEX DWG SRZ 25-005; REV F. MATERIAL ID A 402 H 35039-003 IAW FEDEX DWG SRZ 25-005; REV F. PART MARKED IAW FEDEX GMM 7-0-1000.Jul 3, 2008 · N675FE · Airbus A300F4605R · Fuselage Floor PanelSDR 08FDEA02646Floor Panel · damagedMAIN CABIN FLOOR PANEL 231 YG UPPER SURFACE HAS NUMEROUS PUNCTURES AND THE AFT END IS CRUSHED AND BROKEN. FABBED A NEW PANEL IAW FEDEX DWG SRZ 25-005; REV F. MATERIAL ID A 402 H 35039-003 IAW FEDEX DWG SRZ 25-005; REV F.Jul 3, 2008 · N675FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR 08FDEA02645Floor Panel · crackedMAIN CARGO DECK FLOOR PANEL 232 CF IS CRACKED. FABBED A NEW FLOOR PANEL IAW FEDEX DWG SRZ 25-005; REV F. MATERIAL ID A 402 H35039-003 IAW FEDEX DWG SRZ 25-005; REV F.Jul 3, 2008 · N675FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR 08FDEA02636Bracket · corrodedMAIN CABIN, UNDER FLOOR PANEL 231 BH; THE SUB-FLOOR PANEL IS CORRODED BETWEEN FRAME 29 AND FRAME 30. CHECKED THE LIMITS FOR FLOOR PANEL 231 BH SUB-FLOOR PANEL AND FOUND IT TO BE OUT OF LIMITS REF A300-600 SRM 51-74-10 AND SRM 53-14-15. REMOVED PANEL 131 NW RJul 2, 2008 · N675FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR 08FDEA02635Bracket · corrodedMAIN CABIN UNDER FLOOR PANEL 231 AH AT FRAME 28; THE SUB-FLOOR PANEL IS CORRODED. FOUND TO BE OUT OF LIMITS REF A300-600 SRM 53-14-15. REMOVED PANEL NR 131 DC TO FOM. REF A300-600 SRM 51-40-21. LOCATED AND DRILLED BRACKET REF A300-600 SRM 51-40-44. BRACKJul 2, 2008 · N675FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR 08FDEA02630Seat Track · wornMAIN CABIN ARTICULATING SEAT TRACK RIGHT NR 6 BETWEEN FRAME 38.2 AND FRAME 40 HAS AN ATTACH HOLE THAT IS WORN OUT OF LIMITS. RECEIVED A NEW SEAT TRACK, PO 624240.1. LOCATED AND DRILLED THE NEW SEAT TRACK IAW A300-600 SRM 51-40-40. TRANSFERRED THE ATTACH CLJul 2, 2008 · N675FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR 08FDEA02616Skin · chafedLEFT WING CENTER FLAP, UPPER SURFACE IS CHAFED BY RIVETS ON THE SPOILER SUPPORT ARM BETWEEN SPOILERS NR 3 AND NR 4.Jul 1, 2008 · N675FE · Airbus A300F4605R · Trailing Edge FlapsSDR 08FDEA02508Gusset · crackedA GUSSET IS CRACKED AT STRINGER 26L AFT OF FRAME 79.Jun 26, 2008 · N675FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR 08FDEA02506Floorbeam · gougedGOUGED FLOOR SUPPORT FITTING AT THE MAIN CARGO DECK FRAME 41; LBL 77.Jun 26, 2008 · N675FE · Airbus A300F4605R · Fuselage Main, Floor BeamSDR 08FDEA02477Seat Track · corrodedMAIN DECK FLOOR SEAT TRACK HAS CORROSION, C76-C77;RBL 32. IN 2 SPOTS SEAT TRACK FOUND TO BE OUT OF LIMITS. RECEIVED A NEW TRACK P/N A5327400500053, PO 617932.1 PER SRM 53-18-16, PGS 3 AND 9. LOCATED AND DRILLED THE NEW TRACK PER A300-600 SRM 53-10-16. INJun 25, 2008 · N675FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR 08FDEA02476Seat Track · corrodedMAIN DECK FLOOR SEAT TRACK HAS CORROSION; C76-C77; RBL 32 (IN 2 SPOTS), SEAT TRACK FOUND TO BE OUT OF LIMITS. RECEIVED A NEW TRACK P/N A5327400500053; PO 617932.1 PER SRM 53-18-16; PGS 3 AND 9. LOCATED AND DRILLED THE NEW TRACK PER A300-600 SRM 53-10-16. Jun 25, 2008 · N675FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR 08FDEA02483Seat Track · corrodedMAIN DECK FLOOR SEAT TRACK HAS CORROSION; C78; BL00. BLENDED THE CORROSION AND CHECKED THE LIMITS IAW A300-600 SRM 53-10-16; FIG 102. FOUND THE SEAT TRACK TO BE OUT OF LIMITS. REMOVED THE OLD SEAT TRACK FROM FRAME C73 - C80 AND INSTALLED A NEW TRACK IAW A3Jun 25, 2008 · N675FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR 08FDEA02480Seat Track · corrodedMAIN DECK FLOOR SEAT TRACK HAS CORROSION; C76 - C77; BL 00 (2 SPOTS). BLENDED THE CORROSION AND CHECKED THE LIMITS IAW A300-600 SRM 53-10-16; FIG 102. FOUND THE SEAT TRACK TO BE OUT OF LIMITS. SEAT TRACK REPLACED ON NON-ROUTINE N00576 FROM FRAMES C 73 - Jun 25, 2008 · N675FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR 08FDEA02481Seat Track · corrodedMAIN DECK FLOOR SEAT TRACK HAS CORROSION; C77 - C78; LBL 32. REMOVED CORROSION IAW A300-600 SRM 51-74-10. FOUND TO BE OUT OF LIMITS IAW A300-600 SRM 53-10-16. REMOVED SEAT TRACK SECTION FROM EXISTING SPLICE AND FRAME 76 10 INCHES TO FRAME 80/82 IAW FEDEX A3Jun 25, 2008 · N675FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR 08FDEA02478Seat Track · corrodedMAIN DECK FLOOR SEAT TRACK HAS CORROSION; C76-C77; RBL 17 (IN 3 SPOTS) REMOVED CORROSION AND CHECKED LIMITS IAW A300-600 SRM 53-10-16; FIG 102. FOUND SEAT TRACK TO BE OUT OF LIMITS. REMOVED OLS SEAT TRACK BETWEEN C76 AND C77 AND INSTALLED A NEW SEAT TRACK IJun 25, 2008 · N675FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR 08FDEA02475Seat Track · corrodedMAIN DECK FLOOR SEAT TRACK HAS CORROSION; C75-C76; RBL 44. BLENDED CORROSION AND FOUND SEAT TRACK TO BE OUT OF LIMITS PER SRM 53-10-16. REMOVED CORRODED SEAT TRACK PER SRM 51-41-21. RECEIVED NEW SEAT TRACK P/N A5327400500053, PER SRM 53-18-16. LOCATED AND Jun 25, 2008 · N675FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR 08FDEA02474Seat Track · corrodedMAIN DECK FLOOR SEAT TRACK HAS CORROSION AT C73-C74; RBL 62.Jun 25, 2008 · N675FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR 08FDEA02421Skin · gougedRT INBD FLAP UPPER SURFACE MIDSPAN GOUGED AT 3 PLACES. BLENDED GOUGED AREAS IAW SRM 57-50-00. ALL AREAS ARE BEYOND LIMITS IAW SRM 57-50-00 FIG 101 SHEET 5. TRIMMED OUT DAMAGED AREAS OF THE SKIN & STRINGER IAW SRM 57-50-00; FIGS 205 & 206. REPAIRED AREAS IAWJun 24, 2008 · N675FE · Airbus A300F4605R · Trailing Edge Flaps
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