N679FE

Service difficulty reports · 176

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 = 'N679FE' 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 FDEA201109073731Rib · crackedRT WING T/E SPOILER SHROUD RIB CRACKED ABOUT .3750" BELLOW NR 3 SPOILER INBD EDGE. REMOVED THE CRACKED RIB AND INSTALLED A NEW RIB IAW SRM 51-40-21 AND 51-72-10. REPAIR CLASSIFIED AS MINOR.Sep 7, 2011 · N679FE · Airbus A300F4605R · Wing, Rib/BulkheadSDR FDEA201109073736Floor Panel · damagedFOUND IMPACT DAMAGE ON FLOOR PANEL. FOUND OUT OF ALLOWABLE LIMITS. FABRICATED A NEW FLOOR PANEL, IAW SRM 53-10-20, AND DWG 17A53279962. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.Sep 7, 2011 · N679FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201109073735Floor Panel · damagedBULK CARGO COMP'T 161AF FLOOR PANEL EDGE AREA GOT IMPACT DAMAGED. MEASURED THE DAMAGED AREA IS 17" LONG IS OUT OF THE ALLOWABLE DAMAGE LIMITS. FABRICATED A NEW PANEL WITH EDGE FILLER, INSERTS AND ADHESIVE IAW SRM 53-10-20, AND DWG 17A53279966. THE REPAIR CSep 7, 2011 · N679FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201109043664Floor Panel · damagedAFT CARGO COMPARTMENT 152TF FLOOR PANEL EDGE AREA GOT IMPACT DAMAGED. REMOVED FLOOR PANEL IAW AMM 53-10-33-04. DAMAGED AREA IS NOT WITHIN THE ALLOWABLE DAMAGE LIMITS. FABRICATED A NEW FLOOR PANEL IAW SRM 53-10-20 AND DWG 10-A532-79904. REPAIR EVALUATED PSep 4, 2011 · N679FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201109043663Floor Panel · damagedAFT CARGO COMPARTMENT 151TF FLOOR PANEL EDGE AREA HAS IMPACT DAMAGE. REMOVED AFT FLOOR PANEL IAW AMM 53-10-33-04. DAMAGED AREA IS NOT WITHIN THE ALLOWABLE DAMAGE LIMITS. FABRICATED A NEW PANEL IAW SRM 53-10-20 AND DWG 10-A532-79904. REINSTALLED FLOOR PANESep 4, 2011 · N679FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201109033653Floor Panel · damagedFWD CARGO COMPARTMENT FLOOR PANEL (132PG) HAS IMPACT DAMAGE. REMOVED THE FLOOR PANEL FOR REPAIR IAW AMM 53-10-29-04. DAMAGED AREA IS OUT OF THE ALLOWABLE DAMAGE LIMITS IAW SRM 53-10-20. FABRICATED A NEW FLOOR PANEL IAW SRM 53-10-20 AND DWG 14-A532-79978. Sep 3, 2011 · N679FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201109033652Floor Panel · damagedFWD CARGO COMPARTMENT FLOOR PANEL (132RG) HAS IMPACT DAMAGE. REMOVED FLOOR PANEL FOR REPAIR IAW AMM 53-10-29-04. DAMAGED AREA IS NOT WITHING THE ALLOWABLE DAMAGE LIMITS. FABRICATED A NEW FLOOR PANEL IAW SRM 53-10-20, AND DWG 14-A532-79979. REPAIR EVALUATSep 3, 2011 · N679FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201109033651Floor Panel · damagedFWD CARGO COMPARTMENT FLOOR PANEL (131NG) HAS IMPACT DAMAGE. REMOVED FLOOR PANEL FOR REPAIR IAW AMM 53-10-29-04. THE DAMAGED AREA IS OUT OF THE ALLOWABLE DAMAGE LIMITS. FABRICATED A NEW FLOOR PANEL IAW SRM 53-10-20, AND DWG 14A53279978. REPAIR CLASSIFIEDSep 3, 2011 · N679FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201109033650Floor Panel · damagedAFT CARGO COMPARTMENT 152RF FLOOR PANEL EDGE AREA GOT IMPACT DAMAGED. REMOVED AFT CARGO 152RF FLOOR PANEL IAW AMM 53-10-33-04. THE DAMAGED AREA IS OUT OF THE ALLOWABLE DAMAGE LIMITS. FABRICATED A NEW FLOOR PANEL IAW SRM 53-10-20, AND DWG 10 A532 79903. RESep 3, 2011 · N679FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201109033648Floor Panel · damagedFWD CARGO BAY FLOOR PANEL 131SG HAS IMPACT DAMAGE. NOT WITHIN THE ALLOWABLE DAMAGE LIMITS. FABRICATED A NEW FLOOR PANEL IAW SRM 53-10-20, AND DWG 14A53279979. THE REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.Sep 3, 2011 · N679FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201109033649Floor Panel · damagedFLOOR PANEL EDGE AREA HAS IMPACT DAMAGED. THE DAMAGED AREA IS OVER 10% OF FLOOR PANEL AND IS OUT OF THE ALLOWABLE LIMITS. FABRICATED A NEW PANEL IAW SRM 53-10-20 AND DWG 10 A532 79903. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100 .Sep 3, 2011 · N679FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201009213592Control Unit · failedON APP, AT 8,000' F/O WAS FLYING WE WERE CLEARED FOR THE ILS 25L APP. CAT3 LOX SO SECOND A/P WAS ENGAGED AFTER LAND WAS SELECTED. AFTER G/S & LOC CAPTURE AUTO PILOTS DISCONNECTED AND ALL FMA'S WENT BLANK AND ILS INFO. ATTEMPTED AGAIN WITH SAME RESULT. THEN Sep 21, 2010 · N679FE · Airbus A300F4605R · Autopilot SystemSDR FDEA200904161310Floorbeam · crackedAFT CARGO COMPARTMENT FRAME 58 BETWEEN SEAT TRACKS NR 2RT AND NR 3RT CABIN FLOORBEAM HAS 1 INCH CRACK CUT OUT DAMAGED AREA AND INSTALLED CROSSBEAM REPAIR AT CRACKED STIFFENER AT FRAME 58 CROSSBEAM BETWEEN SEAT TRACKS NR 2 RT AND NR 3 RT IAW A300-600 FREIGHTERApr 16, 2009 · N679FE · Airbus A300F4605R · Fuselage Main, Floor BeamSDR FDEA200904151301Mount · corrodedNR 2 PYLON ENGINE FWD MOUNT BOTH AFT FASTENER HOLES CORRODED, 6 SQ IN REMOVED LEVEL 1 CORROSION. FABRICATED AND INSTALLED REPAIR BUSHINGS ON NR 2 PYLON FWD MOUNT AFT FASTENER HOLES IAW FEDEX EA6-5450-124253. RELEASE DATE 8 APRIL, 2009Apr 15, 2009 · N679FE · Airbus A300F4605R · Engine Mount SectionSDR FDEA200812205252Pin · bindingLANDING GEAR LEVER WOULD NOT GO UP PAST THE OFF POSITION IN SYS 1 OR SYS 2. CHECKED PSEU ON ARRIVAL FOUND FAULT LIGHT ON WITH FAULT CODE "BL" BOGIE LT FAIL. VERIFIED FAULT ON PROX BOX "BL",GREASED LT BOGIE AND JACKED ACFT (NITROGEN DESERVICE OF L/R BOGIE TDec 20, 2008 · N679FE · Airbus A300F4605R · Landing Gear Retraction/Extension SystemSDR 07FDEA04800Pitot Tube · cloggedON TAKEOFF ROLL AT 80KNOT CALL F/O AIRSPEED INDICATOR SHOWED 40KTS, REF MM 34-11-15-6/34-10-00-5. INSPECTED F/O'S PITOT TUBE. DISCOVERED SLIGHT BLOCKAGE. CLEANED PITOT TUBE, PERFORMED AIRSPEED ADJUSTMENT AND TEST. TESTED BOTH CAPT'S AND F/O'S INDICATION OFNov 16, 2007 · N679FE · Airbus A300F4605R · Airspeed/Mach IndicatorSDR 07FDEA01680Floorbeam · bentAFT CARGO PIT, CABIN FLOORBEAM LOWER FLANGE BENT, FR60, STA X3991, BL - Y1750 TO 2050. REPAIRED LOWER FLANGE ON FLOORBEAM FR60, STA X3991, BL - Y1750-2050 IAW FED EX EA 6-5310-109141.May 1, 2007 · N679FE · Airbus A300F4605R · Fuselage Main, Floor BeamSDR 05FDEA03493Smoke Detector · malfunctionedINTERMITTENT AVIONICS SMOKE WARNING. DID NOT SMELL ANY SMOKE. REMOVED AND REPLACED AVIONICS SMOKE DETECTOR 11WA IAW A 300 MM 26-15-12-4. OPS CHECKS GOOD. SERVICEABLE PART CANNED FROM ACFT 653 MFG CG7GO-11. S/N ON AB1058 S/N OFF 1021. SERVICEABLE TAG B553Oct 25, 2005 · N679FE · Airbus A300F4605R · Smoke DetectionSDR 05FDEA03488Smoke Detector · malfunctionedINTERMITTENT AVIONICS SMOKE WARNING. DID NOT SMELL ANY SMOKE. REMOVED AND REPLACED AVIONICS SMOKE DETECTOR 11WA IAW A 300 MM 26-15-12-4. OPS CHECKS GOOD. SERVICEABLE PART CANNED FROM ACFT 653 MFG CG7GO-11. SN ON AB1058 SN OFF 1021. SERVICEABLE TAG B55383. Oct 25, 2005 · N679FE · Airbus A300F4605R · Fire DetectionSDR 05FDEA01368Skin · gougedA/C FUSELAGE RT SIDE FR 55 STR 39 HAS GOUGES REF N00057. BLENDED AREAS AND CHECKED LIMITS IAW SRM 53-10-00 AND 53-16-12 WITHIN LIMITS IAW SRM 53-10-12 FIG 102. FOLLOW UP INSP REQ AT OR BEFORE 1500FC AS STATED ON EA 6-5330-89211 AND SRM 53-10-12 FIG 102.May 18, 2005 · N679FE · Airbus A300B4605R · Fuselage Main, Plate/SkinSDR 05FDEA01311Skin · gougedA/C FUSELAGE RT SIDE FR 57.1STR 43 APPROX HAS GOUGES REF N00066. BLENDED AREA IAW SRM 51-73-10, AREAS OUT OF LIMITS PER SRM 53-10-00. REMOVED DAMAGED SKIN SECTIONS AND REPAIRED PER A300-600 SRM 53-10-12.May 16, 2005 · N679FE · Airbus A300F4605R · Fuselage Main, Plate/SkinSDR 05FDEA01310Adapter · unknownADAPTER BETWEEN TRACK R-1 AND R-2 AT FR 29 REF N00318. REMOVED AND REPLACED ADAPTER IAW SRM 51-72-10 AND 51-40-21.May 16, 2005 · N679FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR 02FDEA00644Pump · leakingEN ROUTE AT FL310 GREEN HYD QUANTITY WENT TO RED DOT WITH ECAM NOTIFICATION. FOLLOWED ECAM AND QRH PROCEDURES. DURING REMAINDER OF FLT GREEN HYD QTY APPEARED TO CONTINUE LEAKING BELOW THE RED DOT. GRAVITY EXT OF GEAR WAS NORMAL AND WE WERE TOWED IN. ACFT Sep 12, 2002 · N679FE · Airbus A300F4605R · Hydraulic Pump, AuxiliarySDR 00FDEA00009Switch · out of adjust00-9 - IN FLT, AFT SLAT RETRACTION SPD LIMIT ZIPPER DID NOT GO AWAY AS IT SHOULD HAVE. RECYCLED SLATS, NO HELP. FOUND VMO/MMO SWITCH IN FWD AVIONICS COMP. IN THE ALT POS. REPOSITIONED SWITCH TO NORM POS. CKS NORMAL.Dec 22, 1999 · N679FE · Airbus A300F4605R · Leading Edge Slat Position Indicating SystemSDR 99FDEA00504Mlg · malfunctioned99-287 - LAND GEAR WOULD NOT RETRACT AFTER T/O IN SYSTEM NR 1 OR NR 2. RETURN TO ORD. REMOVED AND REPLACED LAND GEAR SEL VLV I/A AMM 32-31-12-4. OPS CK NORM WITH NO LEAKS. PERF SEVERAL SUCCESSFUL GEAR SWINGS. JACK PAD ACCESS PNL REINSTALL.Dec 21, 1999 · N679FE · Airbus A300F4605R · Landing Gear Retraction/Extension SystemSDR 99FDEA00503Pilot Valve · failedNR 2 ENGINE REVERSER PRESSURE ON T/O ROLL. REMOVED AND REPLACED NR 2 DIRECTIONAL PILOT VALVE PER AMM 78-31-06-2.Dec 16, 1999 · N679FE · Airbus A300F4605R · Engine Thrust Reverser
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