N671FE

Service difficulty reports · 189

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 = 'N671FE' 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 FDEA201704271277Floor Panel · debondedMAIN CABIN FLOOR PANEL 242UJ HAS DISBONDED CORNER. REPAIRED DAMAGE ON MAIN CABIN FLOOR PANEL 242UJ IAW SRM 53-10-20 PARA 8B FIG 203. THIS IS A MAJOR REPAIR.Apr 27, 2017 · N671FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201704271276Seat Track · corrodedMAIN CABIN SEAT TRACK HAS CORROSION AT FR 40 -Y1456. REMOVED CORROSION FOUND TO BE OUT OF LIMITS, REMOVED SEAT TRACK AND 5EA FLOOR SUPPORTS AND DRILLED NEW SEAT TRACK, INSTALLED SEAT TRACK AND AND 5EA FLOOR SUPPORTS IAW SRM 53-10-16, 51-40-21, 51-40 40-40. THApr 27, 2017 · N671FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201704261263Floor Panel · brokenMDC FLOOR PANEL 252DH IS BROKEN. FABRICATED A NEW FLOOR PANEL IAW DWG SRZ-25-005 REV M. MAJOR REPAIR.Apr 26, 2017 · N671FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201704261262Floor Panel · brokenMDC FLOOR PANEL 262VF IS BROKEN. FABRICATED A NEW FLOOR PANEL IAW DWG SRZ-25-005 REV M. MAJOR REPAIR.Apr 26, 2017 · N671FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201704251261Floor Panel · brokenMAIN DECK CARGO FLOOR PANEL 261AH BROKEN. FABRICATED A NEW FLOOR PANEL IAW DWG SRZ-25-005 REV M, MAJOR REPAIR.Apr 25, 2017 · N671FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201704251259Floor Panel · puncturedMAIN CABIN FLOOR PANEL 241EK HAS SEVERAL PUNCTURES. FABRICATED A NEW FLOOR PANEL IAW DWG SRZ 25-005. MAJOR REPAIR.Apr 25, 2017 · N671FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201704251258Floorboard · dentedMAIN CABIN FLOORBOARD 242ZJ HAS SEVERAL DENTS. FABRICATED A NEW FLOOBOARD IAW DWG SRZ 25-005Apr 25, 2017 · N671FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201704221253Floor Panel · damagedMAIN CABIN FLOOR PANEL 251YH HAS PUNCTURED/CRACKED/DISBONDED. REPAIRED DAMAGED ON MAIN CABIN FLOOR PANEL 251YH IAW A300-600-SRM 53-10-20 PARA 8B FIG 203.Apr 22, 2017 · N671FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201704221252Floor Panel · delaminatedMAIN CABIN FLOOR PANEL 241HK IS DISBONDED. REPAIRED DAMAGE ON MAIN CABIN FLOOR PANEL 241HK IAW A300-600 SRM 53-10-20 PRA 8B FIG 203. THIS IS A MAJOR REPAIR.Apr 22, 2017 · N671FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201611214170Switch · failedON TAXI ECAM AVIONICS SMOKE WARNING. NO INDICATION OF SMOKE. FOUND AVIONICS SMOKE INDICATOR BULB CONTACTS WORN FLAT. REMOVED AND REPLACED THE BULBS AND PERFORMED SATISFACTORY ANNUCIATOR LIGHT TEST IAW AMM 33-14-00-05. STARTED TROUBLESHOOTING IAW AMM 26-15-0Nov 21, 2016 · N671FE · Airbus A300F4605R · Smoke DetectionSDR FDEA201610083507Smoke Detector · malfunctionedAVIONICS SMOKE WARNING WITH CHIME ACTIVATED FL330 AND CONTINUED TO COME ON INTERMITTENTLY FOR REMAINDER OF FLIGHT. INSTALLED SMOKE DETECTOR 11WA AND 13 WA. OPS CHECKED GOOD IAW AMM 26-15-12-04 AND 26-15-00-05. ACFT OK FOR SERVICE IAW GMM 12-7-600.Oct 8, 2016 · N671FE · Airbus A300F4605R · Smoke DetectionSDR FDEA201610083506Smoke Detector · malfunctionedAVIONICS SMOKE WARNING WITH CHIME ACTIVATED FL330 AND CONTINUED TO COME ON INTERMITTENTLY FOR REMAINDER OF FLIGHT. INSTALLED SMOKE DETECTOR 11WA AND 13 WA. OPS CHECKED GOOD IAW AMM 26-15-12-04 AND 26-15-00-05. ACFT OK FOR SERVICE IAW GMM 12-7-600Oct 8, 2016 · N671FE · Airbus A300F4605R · Smoke DetectionSDR FDEA201608182928Warning System · malfunctionedNR 1 ENGINE GREEN SYS HYDRAULIC PUMP LOW PRESSURE. FLIGHT CREW VERIFIED GOOD PRESSURE FROM NR 1 ENGINE HYD GREEN PUMP BY SHUTTING DOWN NR 2 ENGINE AND ECAM INDICATIONS ARE NORMAL AND DID NOT GET A CHIME WHEN LIGHT ILLUMINATED. QTY IS NORMAL. RELEASED FOR SEAug 18, 2016 · N671FE · Airbus A300F4605R · Hydraulic Pressure IndicatorSDR FDEA201601200241Outflow Valve · failedPRESSURE REG 1 & 2 FAULT IN CLIMB OUT. AFTER RESET, FAILED AGAIN. AFT OUTFLOW VLV REMAINED FULL OPEN, WOULD NOT CLOSE, IN MANUAL. INSPECTED E & E, COURIER AREA & MAIN CARGO DECK. FOUND WATER IN ALL THREE AREAS. INSPECTED E & E COMPARTMENT NO WATER FOUND IJan 20, 2016 · N671FE · Airbus A300F4605R · Pressure Regulator/Outflow ValveSDR FDEA201511183703Probe · unknownAIRCRAFT AUTOPILOT DID A POOR JOB, /- 10, OF HOLDING AIRSPEED IN CLIMB & DESCENT. IN PROFILE IN DECENT AIRSPEED KEPT CREEPING INTO ZIPPER. WENT LEVEL & CHG DIALED AIRSPEED BACK WITH NO HELP. BROUGHT THROTTLES TO IDLE MANUALLY & ACFT WENT INTO THRUST LATCH &Nov 18, 2015 · N671FE · Airbus A300F4605R · Pitot/Static SystemSDR FDEA201509032786Bracket · brokenAFTER TAKEOFF LANDING GEAR WOULD NOT RETRACT IN SYS 1 OR 2. ECAM SHOWED LG RETRACTION FAULT. FOUND PROXIMITY SENSOR BRACKET BROKEN, REMOVED AND FABRICATED IAW AMM 32-11-14-04. INSTALLED PROXIMITY DETECTOR IAW AMM 32-00- 00-4. PERFORMED GEAR SWING OF SYSTSep 3, 2015 · N671FE · Airbus A300F4605R · Fuselage Main, Attach FittingsSDR FDEA201509032767Outflow Valve · failedPRESSURIZATION SAFETY VALVE SHOWED OPEN & AMBER ON ECAM. ACFT WOULD NOT PRESSURIZE MORE THAN 2.1 DIFFERENTIAL, CABIN CLIMBED TO 10,000 RETURNED. PRESSURIZED ACFT AGAIN AND FOUND NR 1 SAFETY VALVE FAULTY, REMOVED AND REPLACED THE SAFETY VALVE IAW MM 21-31-15-Sep 3, 2015 · N671FE · Airbus A300F4605R · Pressure Regulator/Outflow ValveSDR FDEA201412224162Frame · damagedMAIN DECK CARGO FRAME 27 DAMAGED STRINGER 13 - 23R. REPAIRED IAW EA 6-5310-T0314096.Dec 22, 2014 · N671FE · Airbus A300F4605R · Fuselage Main, FrameSDR FDEA201412224161Frame · damagedMAIN DECK CARGO FRAME 28 DAMAGED STRINGERS 8 - 22L. REPAIRED IAW EA 6-5310-T0314096.Dec 22, 2014 · N671FE · Airbus A300F4605R · Fuselage Main, FrameSDR FDEA201412084078Union · looseLEFT PYLON AFT FAIRING FROM FWD TO AFT NR 4 HYD TUBE CONNECTOR LOOSE. REMOVED THE FITTING OF THE HYD TUBE BETWEEN WING AND PYLON IAW AMM 29-00-00-04 & DWG A29011098. MINOR REPAIR IAW GMM 6-2-100Dec 8, 2014 · N671FE · Airbus A300F4605R · Hydraulic System, MainSDR FDEA201412034043Cargo Track · corrodedMAIN DECK CARGO TRACK FOUND CORRODED BETWEEN FRAME 56 - 57. REPAIRED IAW SRM 53-10-16-201 PARA.4 FIG 201. MAJOR REPAIR IAW GMM 6-2-100.Dec 3, 2014 · N671FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201412034041Seat Track · crackedMDCC Y1456 SEAT TRACK FOUND CRACK BETWEEN FRAME 71 - 72.Dec 3, 2014 · N671FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201412024024Seat Track · crackedMDCC Y0 SEAT TRACK FOUND CRACK BETWEEN FRAME 57.3 - 58.Dec 2, 2014 · N671FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201411223861Frame · crackedFRAME 40 CRACKED. REPAIRED IAW EA 6-5710-T0313842. MAJOR REPAIR IAW GMM 6-2-100.Nov 22, 2014 · N671FE · Airbus A300F4605R · Fuselage Main, FrameSDR FDEA201411223860Frame · crackedFRAME 40 CRACKED. REPAIRED IAW EA 6-5710-T0313842. MAJOR REPAIR IAW GMM 6-2-100.Nov 22, 2014 · N671FE · Airbus A300F4605R · Fuselage Main, FrameSDR FDEA201411223859Frame · crackedFRAME 40 CRACKED. EA 6-5710-T0313842. MAJOR REPAIR IAW GMM 6-2-100.Nov 22, 2014 · N671FE · Airbus A300F4605R · Fuselage Main, FrameSDR FDEA201411213839Skin · crackedINSPECTION OF REAR SPAR BOTTOM SKIN AROUND E HOLE FOUND CRACKED. REPAIRED IAW EA6-5710-T0313870. MAJOR REPAIR IAW GMM6-2-100.Nov 21, 2014 · N671FE · Airbus A300F4605R · Fuselage Main, Plate/SkinSDR FDEA201411213838Skin · crackedRIGHT FUSELAGE SKIN FOUND CRACKED. REPAIRED IAW EA6-5710-T0313870. MAJOR REPAIR IAW GMM 6-2-100.Nov 21, 2014 · N671FE · Airbus A300F4605R · Fuselage Main, Plate/SkinSDR FDEA201404150735Rib · corrodedRIGHT RIB 5 HAS CORROSION IN BORE & FWD & AFT FACES. COMPLIED WITH EA 6-5710-T0307409 WINGS BASIC WING STRUCTURE RT RIB 5 BORE CORROSION.Apr 15, 2014 · N671FE · Airbus A300F4605R · Wing, Rib/BulkheadSDR FDEA201404040653Lug · corrodedLEFT MLG FITTING FWD LUG CORRODED ON FWD & AFT FACE & IN THE BORE. REPAIRED IAW EA 6-5710-T0307354 PART 1.Apr 4, 2014 · N671FE · Airbus A300F4605R · Wing, Landing Gear Attach FittingsSDR FDEA201305241078Warning Message · false indicationGREEN HYD LOW QTY, ECAMS DURING FLIGHT WAS INTERMITTENT AT FIRST BUT THEN BECAME STEADY. QTY OVERHEAD INDICATED JUST ABOVE RED DOT, ECAM INDICATION WAS AT TO SLIGHTLY ABOVE MIN LEVEL (RED). COMPLIED WITH ECAM AND TURNED OFF GREEN PUMPS. FOUND NO EVIDENCE OMay 24, 2013 · N671FE · Airbus A300F4605R · Hydraulic System, MainSDR FDEA201206262354Cargo Track · corrodedMAIN DECK CARGO TRACK 3R CORRODED AT APPROXIMATEY EIGHT INCHES AFT OF FR 69, R & R CARGO TRACK IAW FSRM 51-72-10.Jun 26, 2012 · N671FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201206262351Seat Track · corrodedSEAT TRACK 4L HAS 2SQ CORROSION BETWEEN FR 75 AND FR 76. AFTER REMOVAL OF LEVEL 1 CORROSION FROM SEAT TRACK 4L BETWEEN FR 75 AND 76. FOUND TO BE OUT OF LIMITS IAW FSRM 53-10-16, PG 103, FIG 101. FABRICATED AND INSTALLED NEW SEAT TRACK 4L BETWEEN FR 74 AND Jun 26, 2012 · N671FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201206252342Seat Track · corrodedSEAT TRACK 3R AT APX 11" FWD OF FR57.2 HAS CORROSSION. AFTER REMOVAL OF LEVEL 1 CORROSION SEAT TRACK WAS FOUND TO BE OUT OF LIMITS IAW SRM 53-10-16, FIG 101. R & R SEAT TRACK IAW SRM 53-10-16.Jun 25, 2012 · N671FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201206242334Floor Panel · corrodedFLOOR PANEL NR 162HF HAS CORROSION TOP SURFACE. FABRICATED REPLACEMENT FLOOR PANEL IAW DWG SRZ 25-005, REV J.Jun 24, 2012 · N671FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201206242333Floor Panel · delaminatedFLOOR PANEL NR 161CF BACK SIDE HAS DELAMINATION ON EDGE. FLOOR PANEL DAMAGE IS BEYOND REPAIR. FABRICATED FLOOR PANEL IAW DWG SRZ-25-005 REV J & DWG SRZ-25-011, REV D.Jun 24, 2012 · N671FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201206242332Seat Track · crackedMAIN CABIN DUMMY TRACK CENTER LINE SEAT TRACK 1 BETWEEN FR 38.2 AND FR 40 HAS A BROKEN SCALLOP. R & R MAIN CABIN DUMMY TRACK CENTER LINE SEAT TRACK 1 BETWEEN FR 38.2 AND FR 40 IAW FSRM 51-72-10, PG 2, PARA 6, FSRM 53-15-16, PG 3 AND AMM 20-21-12. DUE MATEJun 24, 2012 · N671FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201206232306Floor Panel · damagedFLOOR PANEL 241LK IS BROKEN. FABRICATED REPLACEMENT FLOOR PANEL IAW DWG SRZ 25-005, REV J.Jun 23, 2012 · N671FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201206232305Floor Panel · damagedAFT CARGO FLOOR PANEL 151UF HAS TWO DAMAGED CORNERS APPROX TEN SQUARE INCHES. FABRICATED REPLACEMENT FLOOR PANEL IAW DWG SRZ 25-005, REV J.Jun 23, 2012 · N671FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201206232304Floor Panel · damagedAFT CARGO FLOOR PANEL 151WF HAS TWO DAMAGED CORNERS APPROX NINE SQUARE INCHES. FABRICATED REPLACEMENT FLOOR PANEL IAW DWG SRZ 25-005, REV J.Jun 23, 2012 · N671FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201206222299Floor Panel · crackedFLOOR PANEL 242QJ, HAS TWO, TEN INCH CRACKS. FARICATED REPLACEMENT FLOOR PANEL IAW DWG SRZ 25-005, REV J.Jun 22, 2012 · N671FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201206222298Floor Panel · damagedFLOOR PANEL 132MG, BACKSIDE OF PANEL HAS SEVERAL CRUSHED HONEYCOMB CORE & FOUR MISSING INSERTS. FABRICATED REPLACEMENT FLOOR PANEL IAW DWG SRZ 25-005, REV J.Jun 22, 2012 · N671FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201206222297Floor Panel · crackedFLOOR PANEL 242ZJ HAS ONE, TEN INCH CRACK. FABRICATED REPLACEMENT FLOOR PANEL IAW DWG SRZ 25-005, REV J.Jun 22, 2012 · N671FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201206222296Floor Panel · crackedFLOOR PANEL 242EK HAS TWO, TEN INCH CRACKS. FABRICATED REPLACEMENT FLOOR PANEL IAW DWG SRZ 25-005, REV J.Jun 22, 2012 · N671FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201107132688Handle · inoperativeON TAKEOFF WITH GEAR DETECTION SYS NR 2 DEFERRED, GEAR HANDLE WOULD NOT RAISE PAST NEUTRAL POSITION USING SYS NR 1. SWUNG GEAR IN SYS 1 & 2 SEVERAL TIMES IN EA. AND WAS ABLE TO DUPLICATE PROBLEM DEPENDING ON SPEED OF HANDLE MOVEMENT. R & R HANDLE MODULE IN RJul 13, 2011 · N671FE · Airbus A300F4605R · Landing Gear SelectorSDR FDEA201106092178Power Supply · failedCOURIER EMERGENCY LIGHT TEST NOT FUNCTIONING. COURIER EMERGENCY LIGHTING POWER SUPPLY REPLACED IAW AMM 33-51-14-04-0. OP CHECKS OK. PREMATURE REMOVAL/INSTALLATION. COURIER EMERGENCY LIGHTING POWER SUPPLY REPLACED IAW AMM 33-51-14-04-0. OPS CHECKS OK.Jun 9, 2011 · N671FE · Airbus A300B4622 · Emergency LightingSDR FDEA201104231592Radar · inoperativeRADAR WENT INOP AFTER TAKEOFF ON SYS 1 & 2, REMOVED BOTH WEATHER RADARS T/R AND CLEANED CONECTORS AND SWAPPED BOTH T/R IAW AMM34-41-33-04-02, AND OPS CHECK OUT BOTH WEATHER RADARS AMM-34-41-00-05-01, ALL OPS CHECKED GOOD.Apr 23, 2011 · N671FE · Airbus A300F4605R · Weather Radar SystemSDR FDEA201101150182Selector Valve · inoperativeDURING T/O AT GEAR RETRACTION, ECAM INDICATED AUTO BRAKES FAULT ALONE WITH ILLUMINATION OF THE BRAKE FAIL LIGHT. COMPLIED WITH ECAM SELECTED AUTOBRAKES TO ALTN/OFF. AFTER LANDING BRAKE FAIL LIGHT OUT. DURING TAXING IN, SELECTED NORMAL (BRK-ANTISKID SWITCH)Jan 15, 2011 · N671FE · Airbus A300F4605R · Landing Gear Retraction/Extension SystemSDR FDEA201007232650Proximity Sensor · malfunctionedLANDING GEAR FAILED TO RETRACT. COULD NOT MOVE HANDLE TO "UP" POSITION. REMOVED AND REPLACED PROXIMITY ELEC UNIT PER AMM REF 32-31-71-04. REMOVED AND REPLACED LEFT MAIN LANDING GEAR BOGIE BEAM PROXIMITY DETECTORS FOR SYSTEM NR 1 AND 2. PRESSURE LUBRICATEJul 23, 2010 · N671FE · Airbus A300F4605R · Landing Gear Position and WarningSDR FDEA201007202630Proximity Sensor · failedUNSAFE GEAR ON RETRACTION; HANDLE WOULD NOT PASS DET ENT 3 RED UNSAFE; GEAR LOWERED AND GOT 3 GREEN DOWN AND LOCKED, LANDED, NO FURTHER INCIDENT-INFO: AUTO THROTTLE ALSO INOP. PILOT SAID NO OVERWEIGHT LANDING WAS MADE. INTERRAGATED 54GB. FOUND FAULT CODE 63Jul 20, 2010 · N671FE · Airbus A300F4605R · Landing Gear Position and Warning
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