N680FE

Service difficulty reports · 219

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 = 'N680FE' 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 FDEA200908313179Floor Panel · puncturedMAIN CABIN FLOORBOARD 242 UJ IS PUNCTURED AND CRUSHED FROM FRAME 43 TO FRAME 47. REMOVED DAMAGED FLOOR PANEL 242 UJ. FABRICATED NEW FLOOR PANEL 242 UJ, IAW DWG SRZ 25-005, REV "H". INSTALLED PANEL IAW AMM 53-10-23-4.Aug 31, 2009 · N680FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA200908313178Floorboard · puncturedMAIN CABIN FLOORBOARD 241 AJ IS PUNCTURED AND CRUSHED FROM FRAME 47 TO FRAME 51. FABRICATED FLOORBOARD IAW (DWG SRZ 25-005, REV "H"). PART MARKED FLOORBOARD IAW GMM 7-0-1000.Aug 31, 2009 · N680FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA200908313177Floorboard · puncturedMAIN CABIN FLOORBOARD 242 AJ IS PUNCTURED AND CRUSHED FROM FRAME 47 TO FRAME 51. LOCATED FASTENER HOLES AND PREPED EDGE FOR POTTING IAW (DWG SRZ 25-005, REV "H"). PART MARKED IAW GMM 7-0-1000.Aug 31, 2009 · N680FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA200908313176Floorboard · puncturedMAIN CABIN FLOORBOARD 242 ZJ IS PUNCTURED AND CRUSHED FROM FRAME 47 TO FRAME 51. FABRICATED FLOORBOARD IAW (DWG SRZ 25-005, REV "H"). PART MARKED FLOORBOARD IAW GMM 7-0-1000.Aug 31, 2009 · N680FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA200908313175Floorboard · puncturedMAIN CABIN CARGO COMPARTMENT FLOORBOARD 242 EK IS PUNCTURED AND CRUSHED FROM FRAME 51 TO FRAME 54. REMOVED DAMAGED FLOOR PANEL 242 EK. FABRICATED NEW FLOOR PANEL 242 EK, IAW DWG SRZ 25-005, REV "H". INSTALLED PANEL IAW AMM 53-10-23-4.Aug 31, 2009 · N680FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA200908313174Floorboard · puncturedMAIN CABIN CARGO COMPARTMENT FLOORBOARD 251 PH IS PUNCTURED AND CRUSHED FROM FRAME 58 TO FRAME 60. DAMAGED FLOOR PANEL 252 PH REMOVED. NEW PANEL 252 PH FABRICATED AND INSTALLED IAW AMM 53-10-23-4 AND DWG SRZ 25-005, REV "H".Aug 31, 2009 · N680FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA200908313173Floorboard · puncturedMAIN CABIN CARGO COMPARTMENT FLOORBOARD 252 UH IS PUNCTURED AND CRUSHED FROM FRAME 62 TO FRAME 63. DAMAGED FLOOR PANEL (252 UH) REMOVED. NEW PANEL (252 UH) FABRICATED AND INSTALLED IAW AMM 53-10-23-4 AND DWG SRZ 25-005, REV "H".Aug 31, 2009 · N680FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA200908313172Floorboard · puncturedMAIN CABIN CARGO COMPARTMENT FLOORBOARD 251 UH IS PUNCTURED AND CRUSHED FROM FRAME 62 TO FRAME 63. DAMAGED FLOOR PANEL REMOVED. NEW PANEL (251 UH) FABRICATED AND INSTALLED IAW AMM 53-10-23-4 AND DWG SRZ 25-005, REV "H".Aug 31, 2009 · N680FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA200908313171Seat Track · damagedMAIN CABIN SEAT TRACK SCALLOP IS BROKEN BETWEEN FR 63 AND FR 64; RT BUTTLINE 37 INCHES FROM CTR. REMOVED DAMAGED AREA REF SRM 71-73-10, PARA F. MATERIAL LOSS ALLOWED 0.016. MATERIAL REMOVED 0.155; FOUND TO BE OUT OF LIMITS IAW SRM 53-10-16; PG 105. INSTAug 31, 2009 · N680FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR 08FDEA02843Damper · failedUNABLE TO RETRACT GEAR IN EITHER SYS 1 OR SYS 2. PERFOMED BIT CHECK ON PROX BOX, GOT CODES P1, P2, 90, BL. REMOVED CLEANED AND LUBED BOGIE BEAM PIVOT PIN AND REINSTALLED. REPLACED PITCH DAMPNER. PERFORMED MLG SWING, OPS CHECKS NORMAL ALL INDICATIONS NORMAJul 12, 2008 · N680FE · Airbus A300B4605R · Landing Gear Retraction/Extension SystemSDR 08FDEA00326Landing Gear · malfunctionedLANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF. TRIED SYS 1 AND SYS 2. SERVICED BOTH LANDING GEAR PITCH DAMPERS FOUND WITH LOW PRESSURE AND REPLACED LANDING GEAR PROX BOX AS PRECAUTION.Jan 30, 2008 · N680FE · Airbus A300F4605R · Landing Gear Retraction/Extension SystemSDR 06FDEA03800Magnetic Seal · leakingAPPROX 1 HOUR OF FLIGHT NR 1 OIL QUANTITY STARTED TO DECREASE. ALL OTHER INDICATIONS NORMAL. AFTER APPROX 2 HOURS OF FLIGHT THE OIL PRESSURE STARTED TO FLUCTUATE PLUS OR MINUS 15 PSI. PER QRH THIS COULD BE ABNORMAL, DIVERTED TO KDEN. ENGINE NR 1 LEFT AT IOct 27, 2006 · N680FE · Airbus A300F4605R · Turbine Engine Oil SystemSDR 05FDEA03439Smoke Detector · malfunctionedON TAXI OUT, NR 1 AFT SMOKE FAULT LIGHT ILLUMINATED. TURNED OFF PER PROCEDURE. ON TAKEOFF, AFT SMOKE LIGHT ILLUMINATED. NR 2 MID SMOKE LIGHT ILLUMINATED ON LANDING ROLL. CONFIMED BOTH MID 2 AND AFT ON MX PANEL AND CONTROL UNITS ARE HARD FAULTS. REMOVED ANOct 16, 2005 · N680FE · Airbus A300F4605R · Smoke DetectionSDR 04FDEA02983Computer · malfunctionedREJECTED TAKEOFF - AIRCRAFT NI WENT TO MAX POWER (TOGA) THOUGH FLEX POWER SELECTED ENT BY: 097576 RPT BY: 097023 THIS ITEM WAS CLEARED WITH THE R&R OF THE T.C.C. PER A-300-600 M/M 22-36-34-4-01, AND OPS CHECK OF THE AUTOTHROTTLE SYSTEM PER A-300-600 M/MOct 23, 2004 · N680FE · Airbus A300B4605R · Auto Throttle SystemSDR 04FDEA02882Indicator · malfunctionedWITH POWER SET ON TAKEOFF NR 2 ENGINE N2 ANALOG INDICATION SHOWED APPROXIMATELY 20 LESS THAN THE DIGITAL INDICATION. ABORTED TAKEOFF AND RETURNED TO RAMP. REMOVED AND REPLACED NR 2 ENG N2 GAUGE PER AIRBUS M/M 77-12-21-4, OPS CHECKED PER ENG RUN PER JRH. NOOct 6, 2004 · N680FE · Airbus A300F4605R · Engine RPM Indicating SystemSDR 04FDEA01746Warning Light · illuminatedT/O PLUS 1 HR, DURING DESCENT TO FL240, GOT ECAM MESSAGE FOR LOW GREEN HYDRAULIC QUANTITY. GAGE AND ECAM SCHEMATIC SHOWED QUANTITY AT THE RED DOT LEVEL. TURNED OFF GREEN PUMPS, MANUALLY EXTENDED THE GEAR, UTILIZED THE ALTERNATE BRAKE SYSTEM AND LANDED AT MSYJun 15, 2004 · N680FE · Airbus A300F4605R · Hydraulic System, MainSDR 02FDEA00077Control Unit · malfunctionedDURING CLIMBOUT FLAPS WOULD NOT RETRACT. R&R NR 1 & 2 SFCC PER MM 27-51-18.4.Jan 29, 2002 · N680FE · Airbus A300F4605R · Trailing Edge Flap Control SystemSDR 01FDEA00970Warning Light · false indicationAFTER T/O GEAR DOOR IND UNSAFE SYS 1 & 2 FWD AND OVERHEAD PANEL, LOWERED GEAR IND SAFE, NOSE DOOR STILL SHOW UNSAFE.Nov 7, 2001 · N680FE · Airbus A300F4605R · Landing Gear Position and WarningSDR 01FDEA00163Panel · faultyNR 1 ENG AGENT NR 2 DISCHARGE LIGHT CAME ON IN FLT. REMOVED AND REPLACED NR 1 ENG OVERHEAD FIRE SHUTOFF PNL. RECHECK GOOD. OPS CK PER A300 AMM 26-12-20-4.Feb 24, 2001 · N680FE · Airbus A310 · Fire Detection
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