N692FE

Service difficulty reports · 65

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 = 'N692FE' 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 FDEA201110124442Floor Panel · dentedMAIN DECK CARGO COMPARTMENT AFT AREA FLOOR PANEL NR 251BF FOUND WITH DENT AT FRAME 56, LBL 30. FLOOR PANEL REPAIRED AS PER SRM 53-10-20 REV 21. REPAIR CLASSIFIED MAJOR PER GMM 6-2-100 REV 113.Oct 12, 2011 · N692FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201110124441Floor Panel · dentedMAIN DECK CARGO COMPARTMENT MID AREA FLOOR PANEL NR 241RJ FOUND WITH DENT AT FRAME 40, LBL 60. FLOOR PANEL REPAIRED AS PER SRM 53-10-20 REV 21. REPAIR CLASSIFIED MAJOR PER GMM 6-2-100 REV 113.Oct 12, 2011 · N692FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201110124440Floor Panel · dentedMAIN DECK CARGO COMPARTMENT MID AREA FLOOR PANEL NR 242LT FOUND WITH DENT AT FRAME 35, RBL 10. FLOOR PANEL REPAIRED AS PER SRM 53-10-20 REV 21. REPAIR CLASSIFIED MAJOR PER GMM 6-2-100 REV 113.Oct 12, 2011 · N692FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201110124439Floor Panel · dentedMAIN DECK CARGO COMPARTMENT FWD AREA FLOOR PANEL NR232XG FOUND WITH DENT AT FRAME 30, RBL 20. FLOOR PANEL REPAIRED AS PER SRM 53-10-20 REV 21. REPAIR CLASSIFIED MAJOR PER GMM 6-2- 100 REV 113.Oct 12, 2011 · N692FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201110124438Floor Panel · dentedMAIN DECK CARGO COMPARTMENT FORWARD AREA FLOOR PANEL NR 231YG FOUND WITH DENT AT FRAME 29, LBL 36. FLOOR PANEL REPAIRED AS PER SRM 53-10-20 REV 21. REPAIR CLASSIFIED MAJOR PER GMM 6-2-100 REV 113.Oct 12, 2011 · N692FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201110124437Floor Panel · dentedMAIN DECK CARGO COMPARTMENT FORWARD AREA FLOOR PANEL NR 232YG FOUND WITH DENT AT FRAME 28, RBL 36. FLOOR PANEL REPAIRED AS PER SRM 53-10-20 REV 21. REPAIR CLASSIFIED MAJOR PER GMM 6-2-100 REV 113Oct 12, 2011 · N692FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201110124436Floor Panel · dentedMAIN DECK CARGO COMPARTMENT FWD AREA FLOOR PANEL NR 232SG FOUND WITH DENT AT FRAME 26, RBL 20. FLOOR PANEL REPAIRED AS PER SRM 53-10-20 REV 21. REPAIR CLASSIFIED MAJOR PER GMM 6-2-100 REV 113.Oct 12, 2011 · N692FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201110074358Floor Panel · dentedMAIN DECK CARGO COMPARTMENT FLOOR PANEL FOUND DENTED. REPAIRED AS PER SRM 53-10-20 REV 21. REPAIR CLASSIFIED MAJOR PER GMM 6-2-100 REV 113.Oct 7, 2011 · N692FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201110074357Floor Panel · dentedMAIN DECK CARGO COMPARTMENT FORWARD AREA FLOOR PANEL FOUND DENTED. REPAIRED AS PER SRM 53-10-20 REV 21. REPAIR CLASSIFIED MAJOR PER GMM 6-2-100 REV 113.Oct 7, 2011 · N692FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201110074356Floor Panel · dentedMAIN DECK CARGO COMPARTMENT MID AREA FLOOR PANEL FOUND DENTED. REPAIRED AS PER SRM 53-10-20 REV 21.Oct 7, 2011 · N692FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201110074355Floor Panel · dentedMAIN DECK CARGO COMPARTMENT FORWARD AREA FLOOR PANEL FOUND DENTED. REPAIRED AS PER SRM 53-10-20 REV 21. REPAIR CLASSIFIED MAJOR PER GMM 6-2-100 REV 113Oct 7, 2011 · N692FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201008082874Pitot Tube · obstructedCAPTAINS AIRSPEED ON PFD INDICATED GREATER THAN 100KTS. F/O AIRSPEED INDICATED AROUND 70KTS ON TAKEOFF ROLL. TAKEOFF WAS REJECTED. ON WALK AROUND, FOUND F/O PITOT TUBE OBSTRUCTED BY WHAT APPEARS TO BE A BEE. REMOVED PIECES OF BEE BUT SOME STILL REMAIN. WILAug 8, 2010 · N692FE · Airbus A300F4605R · Pitot/Static SystemSDR FDEA200910303728Pitot Tube · dirtyNO AIRSPEED INDICATION ON CAPT PFD AT 80 KTS, CALL BY F/O. REJECTED AT APPROX 90KTS. RTB. PERFORMED CAPT PITOT PROBE FLUSH IAW MM:34-10-00-3. FOUND PITOT TUBE OBSTRUCTED. REMOVED 41DA PITOT TUBE FROM ACFT MM 34-11-15-4. REMOVED AND REPLACED THE CAPT PITOTOct 30, 2009 · N692FE · Airbus A300F4605R · Pitot/Static SystemSDR FDEA200910303725Module · failedNO CAPTAINS AIRSPEED INDICATION WHEN F/O CALLED 80 KNOTS. REJECTED TAKEOFF AT APPROX 90-95 KNOTS. ACCOMPLISHED RTO CHECKLIST AND RTB. PERFORMED ACCURACY AND LEAK TEST OF CAPT'S PITOT/AIRSPEED IND SYS IAW MM 34-10-00-5. NO LEAKAGE AND CAPT'S AIRSPEED MATCHEOct 30, 2009 · N692FE · Airbus A300F4605R · Air Data ComputerSDR 07FDEA03370Computer · failedON TAKEOFF, THE FLAPS WOULD NOT RAISE PAST 20. RECYCLED SEVERAL TIMES NO CHANGE. ON APPROACH, THE FLAPS WOULD NOT GO PAST 20. ON LANDING, THE FLAPS RETURNED TO 0 DURING AFTER LANDING CHECK BOTH SFCC'S REPLACED. RAN ENGINES, OPERATED FLAPS FULL TRAVEL SEVERSep 5, 2007 · N692FE · Airbus A300F4605R · Trailing Edge Flap Control System
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