N664FE

Service difficulty reports · 307

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 = 'N664FE' 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 FDEA201311132758Proximity Sensor · failedAFTER TAKEOFF, GEAR WOULD NOT RETRACT, SYSTEM 2. SWITCHED TO SYSTEM 1 AND GEAR RETRACTED. CAUSED LOSS OF ADC 2, ALL PITOT HEAT, CABIN REGULATOR 2, AUTOTHROTTLES, AUTOPILOT 2. COULD NOT RECOVER ANY OF IT. FOUND PEU WITH SEVERAL FAULTS FOR FAILED PROXIMITY Nov 13, 2013 · N664FE · Airbus A300F4605R · Main Landing GearSDR FDEA201307121550Smoke Detector · false activationAVIONICS SMOKE WARNING ON AND OFF SEVERAL TIMES DURING DESCENT. NO OTHER INDICATIONS OF SMOKE. ACFT TOOK ON SOME WATER AT DEPARTURE RAMP THAT MAY HAVE GONE INTO AVIONICS COMPARTMENT. CLEANED AVIONICS AREA OF WATER. PERFORMED OPS TEST OF SMOKE DETECTION SJul 12, 2013 · N664FE · Airbus A300F4605R · Smoke DetectionSDR FDEA201302120330Fitting · damagedAFT CARGO DOOR ACTUATOR PAN FOUND AN ADDITIONAL HOLE ON FRAME FITTING. REPAIRED AFT CARGO DOOR FRAME FITTING IAW EA 6-5317-T0300077 AT FRAME 61, STR 27RT.Feb 12, 2013 · N664FE · Airbus A300F4605R · Fuselage Main, Attach FittingsSDR FDEA201302120328Skin · damagedLT WING LOWER SURFACE INBD PYLON PANEL 484BR HAS CHAFED WING APPROX 11" X 50" X .040". COMPLIED WITH EA 6-5710-T0300089 AND WRI 57105072.Feb 12, 2013 · N664FE · Airbus A300F4605R · Wing, Plate/SkinSDR FDEA201301170117Floor Panel · delaminatedCENTER WHEEL WELL FLOOR PANEL 147EF BOTTOM SURFACE HAS FOUR AREAS OF DELAMINATION. FABRICATED REPLACEMENT CTR WHEEL WELL PANEL IAW DWG SRZ 25-005, REV J.Jan 17, 2013 · N664FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201301110083Mount · corrodedNR 2 ENG PYLON FWD ENG MOUNT FITTING, ALL 4 TENSIL BOLT HOLES AND SPOT FACES HAVE OXIDATION AT UPPER SURFACE. ALL TENSILE BOLT HOLES IN LIMITS AFTER OXIDATION REMOVAL IAW FSRM 54-51-81, 2 FIG, 104 SHT 2. BOTH INBD AND OTBD AFT SPOTFACES FOUND TO BE OUT OF LIJan 11, 2013 · N664FE · Airbus A300F4605R · Nacelle/Pylon, Main FrameSDR FDEA201301100061Floorbeam · crackedCARGO BAY FLOORBEAM UNDER FR 67 RT ADJACENT TO BULK DOOR FWD LOWER CORNER CRACKED 3 INCHES LONG. R & R FLOOR SUPPORT IAW SRM 51-72-10, PGS 1 -3.Jan 10, 2013 · N664FE · Airbus A300F4605R · Fuselage Main, Floor BeamSDR FDEA201212304401Support · corrodedBULK CARGO COMPARTMENT FR 70 CEILING PANEL PROFILE HAS FOUR AREAS OF CORROSION AT LOWER SURFACE DEFECT MEASURES FIVE SQUARE INCHES. AFTER REMOVAL OF LEVEL 1 CORROSION, FOUND THREE AREAS TO BE OUT OF LIMITS IAW SRM 51-73-11. REPAIRED 3 EA AREAS WITH FABRICATDec 30, 2012 · N664FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA201212304400Seat Track · damagedSEAT TRACK 2R, SIX SCREW HOLES ELONGATED BETWEEN FR 41-FR 45 AT RT FLANGE. R & R SEAT TRACK IAW SRM 51-72-10.Dec 30, 2012 · N664FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201212274387Adapter · corrodedMAIN DECK CABIN FLOOR STRUCTURE CLEVIS FR66 BETWEEN SEAT TRACK 2R & 3R HAS CORROSION INSIDE OF TRACK. CORROSION WAS FOUND TO BE OUT OF LIMITS IAW SRM 53-10-15 FIG 103. R & R CLEVIS ADAPTER IAW FSRM 51-72-10. REPROTECTED IAW FSRM 51-75-10.Dec 27, 2012 · N664FE · Airbus A300F4605R · Fuselage Main, StructureSDR FDEA201212274385Floorboard · damagedFLOORBOARD 242QJ CRUSHED AT UPPER SURFACES. FABRICATED REPLACEMENT FLOORBOARD IAW DWG SRZ 25-005, REV J.Dec 27, 2012 · N664FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201212264378Floorboard · damagedFLOORBOARD 242EK IS CRUSHED ON UPPER SURFACE OUT CLEVIS CUTOUTS. FABRICATED REPLACEMENT FLOORBOARD IAW DWG SRZ 25-005, REV J.Dec 26, 2012 · N664FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201212264379Floorboard · damagedFLOORBOARD 242UJ IS CRUSHED ON UPPER SURFACE AT CLEVIS CUTOUTS. FABRICATED FLOORBOARD IAW DWG SRZ25-005, REV J.Dec 26, 2012 · N664FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201212254373Floorboard · damagedFLOORBOARD 242ZJ ON UPPER SURFACE CRUSHED AT CLEVIS CUTOUTS. FABRICATED REPLACEMENT FLOORBOARD IAW DWG SRZ25-005, REV J.Dec 25, 2012 · N664FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201212234366Plate · damagedFWD CARGO DOOR AFT LOWER CORNER DENTED APPROX L=2" AND W=.5" CORNER PLATE NOT REPAIRABLE IAW SRM 52-31-00, CONFIG 2, PG 9, ITEM 85; R & R CORNER PLATE ON FWD CARGO DOOR AFT LOWER CORNER IAW SRM 51-72-10, PGS 1-3.Dec 23, 2012 · N664FE · Airbus A300F4605R · Cargo/Baggage DoorsSDR FDEA201212224364Seat Track · gougedMAIN CABIN ZONE 230, FR 20 TO FR 21 SEAT TRACK 2R HAS GOUGED SCALLOP THREE SPOTS. COMPLIED WITH EA6-5313-T0300083, REV NR PS P.Dec 22, 2012 · N664FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201212224362Adapter · corrodedMAIN CABIN FLOOR STRUCTURE CLEVIS ADAPTER AT FR 58 BETWEEN SEAT TRACKS 2R AND 3R, HAS CORROSION INSIDE OF TRACK. REMOVED LEVEL 1 CORROSION ON CLEVIS ADAPTER AT FR 58 BETWEEN SEAT TRACK 2R AND 3R IAW FSRM 51-74-10, PG 205, PARA 3. FOUND THE CLEVIS ADAPTER TODec 22, 2012 · N664FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA201212214356Floorboard · crackedFLOORBOARD 241DF HAS A 10 INCH CRACK. FABRICATED REPLACEMENT FLOORBOARD IAW DWG SRZ 25-005, REV J.Dec 21, 2012 · N664FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201212214355Floor Panel · crackedFLOOR PANEL NR 231YG HAS A CRACKED TOP SKIN. FABRICATED REPLACEMENT FLOOR PANEL IAW DWG SRZ 25-005, REV J.Dec 21, 2012 · N664FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201212214358Floorboard · brokenFLOORBOARD 242LK BROKEN. FABRICATED REPLACEMENT FLOORBOARD IAW DWG SRZ 25-005, REV J.Dec 21, 2012 · N664FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201212214359Floor Panel · crackedFLOOR PANEL 252DF IS CRACKED AT CLEVIS OUT APPROX 8 INCHES. FABRICATED REPLACEMENT FLOOR PANEL IAW DWG SRZ 25-005, REV J.Dec 21, 2012 · N664FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201212214354Floor Panel · crackedMAIN DECK FLOOR PANEL, 232YG HAS 2 EA AREAS CRACKED, TOP SKIN.Dec 21, 2012 · N664FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201212214353Floorboard · damagedFLOORBOARD 242RG, CRUSHED AT UPPER SURFACE. REMOVED FLOORBOARD IAW AMM 53-10-23-04. FABRICATED REPLACEMENT FLOORBOARD IAW DWG SR2 25-005 REV J AND REINSTALLED.Dec 21, 2012 · N664FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201212204341Structure · crackedCARGO DOOR LOWER FWD CORNER, INTERNAL EDGE OF STRUCTURE BENT AND CRACKED 3 INCHES LONG. R & R MAIN CARGO DOOR FWD LOWER CORNER SEAL PROFILE IAW SRM 51-40-21, PAR 5 AND 6 AND SRM 51-72-10, PG 2-3. REPROTECTED AREA IAW SRM 51-21-10, PG 6 AND SRM 51-75-10, PG 2Dec 20, 2012 · N664FE · Airbus A300F4605R · Cargo/Baggage DoorsSDR FDEA201212204339Floor Panel · crackedFLOOR PANEL 252VF HAS A CRACK ON TOP SKIN. FABRICATED REPLACEMENT FLOOR PANEL IAW DWG SRZ 25-005-REV J.Dec 20, 2012 · N664FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201212204348Structure · crackedFWD CARGO DOOR FWD LOWER CORNER DENTED APPROX L=2" AND W=1" AND CRACKED APPROX L-0.25" AT THE SAME SPOT. REMOVED PROFILE SRM 51-72-10, PG 2 DRILLED AND LOCATED HOLES AND INSTALLED IAW SRM 51-72-10, PG 2 ON FWD CARGO DOOR CORNER PROFILE. REPROTECTED FASTENEDec 20, 2012 · N664FE · Airbus A300F4605R · Cargo/Baggage DoorsSDR FDEA201212204338Floor Panel · crackedFLOOR PANEL 252UH HAS TWO EIGHT INCH CRACKS AT CLEVIS CUTOUTS. FABRICATED REPLACEMENT FLOOR PANEL IAW DWG SRZ 25-005, REV J.Dec 20, 2012 · N664FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201212204345Adapter · damagedCLEVIS ADAPTER FR 32 BETWEEN SEAT TRACK 4 AND 5L HAS IMPACT DAMAGE AT UPPER SURFACE. R & R CLEVIS ADAPTER IAW FSRM 51-72-10, PGS. 1 - 3.Dec 20, 2012 · N664FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA201212204344Adapter · damagedCLEVIS ADAPTER, FR 31 BETWEEN SEAT TRACK 4 - 5L HAS IMPACT DAMAGE AT UPPER SURFACE. R & R CLEVIS ADAPTER IAW FSRM 51-72-10, PGS 1-3.Dec 20, 2012 · N664FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA201212194334Seat Track · corrodedMAIN DECK SEAT TRACK 6L BETWEEN FR 20L AND 21L HAS CORROSION INSIDE OF TRACK AREA, OUT OF LIMITS AFTER CLEAN UP IAW SRM 53-10-16, FIG 102. OUT OF LIMITS AFTER CLEAN UP IAW SRM 53-10-16, FIG 102. AFTER REMOVAL OF CORROSION, FOUND TO BE OUT OF LIMITS. R & RDec 19, 2012 · N664FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201212194325Floor Panel · delaminatedAFT CARGO FLOOR PANEL 152TF HAS DELAMINATION, PUNCTURES, AND CRUSHED CORE ALONG EDGE, 30 SQUARE INCHES. FABRICATED FLOOR PANEL IAW DWG SRZ 25-005, REV J.Dec 19, 2012 · N664FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201212194324Floor Panel · crackedFLOOR PANEL 242SF HAS CRACKS IN TOP SKIN. FABRICATED REPLACEMENT FLOOR PANEL IAW DWG SRZ-25-005, REV J.Dec 19, 2012 · N664FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201212194336Seat Track · failedLEFT NR 6 SEAT TRACK AT FR 54-54.2 FAILED GAP CHECK. REMOVED & REINSTALLED 6L DUMMY TRACK AT FR 54-54.2 IAW SRM 53-15-16. REPAIRED 6L SEAT TRACK IAW SRM 53-15-16, FIG 201. REMOVED & REINSTALLED IAW SRM 51-40-21, PARA 6 & 7.Dec 19, 2012 · N664FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201212194335Seat Track · failedLEFT NR 5 SEAT TRACK AT FR54-54.2 FAILED GAP CHECK. REMOVED & REINSTALLED IAW SRM 53-16-15. REPAIRED SEAT TRACK IAW SRM 53-15-16, FIG 201.Dec 19, 2012 · N664FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201212194337Adapter · crackedMAIN DECK CLEVIS ADAPTOR AT FR 54.1L BETWEEN 5L AND 6L DUMMY TRACK CRACKED ON INBD SIDE. REPLACED CLEVIS ADAPTOR IAW FSRM 51-72-10, PG 1, PARA 3.Dec 19, 2012 · N664FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA201212194333Floor Panel · delaminatedFWD CARGO FLOOR PANEL 131SG UPPER SURFACE HAS DELAMINATED EDGES AND LOWER SURFACE HAS IMPACT DAMAGE, APPROX 12 SQUARE INCHES TOTAL. FABRICATED FLOOR PANEL IAW DWG SRZ 25-005, REV J.Dec 19, 2012 · N664FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201212194332Floor Panel · delaminatedAFT CARGO FLOOR PANEL 151SF HAS DELAMINATION AND CRUSHED CORE ALONG EDGE, 72 SQUARE INCHES. FABRICATED FLOOR PANEL IAW DWG 25-005, REV J.Dec 19, 2012 · N664FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201212194331Floor Panel · crackedFLOOR PANEL 252PH HAS CRACKED TOP SKIN, FABRICATED FLOOR PANEL IAW DWG SRZ 25-005, REV J.Dec 19, 2012 · N664FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201212194330Floor Panel · damagedFWD CARGO FLOOR PANEL 131LG HAS CRUSHED CORE AT CUTOUT AND ALONG EDGE, AND SEVERAL BROKEN, MISSING, AND CORRODED INSERTS. FABRICATED REPLACEMENT FLOOR PANEL IAW DWG SRZ 25-005, REV J.Dec 19, 2012 · N664FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201212194329Floorboard · delaminatedFLOORBOARD 251BH DELAMINATED AT LWR SURFACE AROUND CLEVIS CUT-OUT. FABRICATED REPLACEMENT FLOORBOARD IAW DWG SRZ 25-005, REV J.Dec 19, 2012 · N664FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201212194328Floor Panel · delaminatedFWD CARGO FLOOR PANEL 132RG DELAMINATED ALONG BOTH EDGES, 70". FABRICATED REPLACEMENT FLOOR PANEL IAW DWG SRZ 25-005, REV J.Dec 19, 2012 · N664FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201212194327Floor Panel · crackedFLOOR PANEL 242BF HAS A CRACK IN TOP SKIN, FABRICATED REPLACEMENT FLOOR PANEL IAW DWG SRZ 25-005, REV J.Dec 19, 2012 · N664FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201212184318Mount · corrodedNR 1 ENG PYLON MOUNT HAS CORROSION ON AFT OTBD AND INBD SPOT FACES AND AFT OTBD AND INBD TENSILE BOLT HOLES. REMOVED CORROSION AFT I/B & O/B SPOT FACE & INNER BORE OF HOLES, FOUND TO BE WITHIN LIMITS IAW SRM 54-51-01 CONFIG 2 FIG 104, REMOVED CORROSION AT Dec 18, 2012 · N664FE · Airbus A300F4605R · Nacelle/Pylon, Attach FittingsSDR FDEA201212184323Seat Track · corrodedSEAT TRACK 3R CORRODED AT LT FLANGE 10 INCHES LONG AND ON RT FLANGE 5 INCHES LONG BETWEEN FR 50 AND FR 51. CORROSION FOUND TO BE OUT OF LIMITS AFTER REMOVAL IAW SRM 53-10-16, FIG 201, PG 105. REMOVED CORROSION SEAT TRACK IAW SRM 51-74-10, CHECK LIMITS MAT'LDec 18, 2012 · N664FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201212184322Seat Track · corrodedSEAT TRACK 2L HAS FOUR AREAS OF CORROSION BETWEEN FR 67 AND 69. AFTER CORROSION REMOVAL THREE AREAS WERE OUT OF LIMITS IAW SRM 53-10-16, FIG 102. REMOVED CORROSION ON SEAT TRACK IAW SRM 51-74-10, FOUND TO BE OUT LIMITS IAW 53-10-16 PB 101 PG 105 FIG 102, RDec 18, 2012 · N664FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201212184319Seat Track · corrodedCORROSION IN SCALLOPED AREA ON SEAT TRACK 1 AT FRAME 78. AFTER REMOVING CORROSION, FOUND TO BE OUT OF LIMITS IAW SRM 53-10-16, FIG 102. MAX ALLOWABLE IS 0.028" AREA OF CORROSION REMOVED IS 0.032'. REMOVED CORROSION ON SEAT TRACK 1 AT FR 78 IAW SRM 51-74-10,Dec 18, 2012 · N664FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201212184317Skin · corrodedNR 1 ENG SKIN HAS CORROSION AT SPIGOT HOLE AND LIGHT SURFACE CORROSION ON SKIN LOWER SURFACE. DEFECT MEASURES 6". REMOVED CORROSION, MEASURED REMAINING THICKNESS AND CHECKED LIMITS IAW 51-74-10 AND 54-51-81. NDT OK, PREPPED AND REPROTECTED AREAS IAW SRM 54-5Dec 18, 2012 · N664FE · Airbus A300F4605R · Nacelle/Pylon, Plate/SkinSDR FDEA201212184321Seat Track · corrodedSEAT TRACK 1 HAS 3 AREAS OF CORROSION BETWEEN FR 66 AND 67. AFTER CORROSION REMOVAL FOUND ONE AREA TO BE OUT OF LIMITS. MATERIAL LOSS LIMITS IS 0.039. LOSS AFTER REMOVAL 0.069 IAW SRM 53-10-16, FIG 101. REMOVED CORROSION IAW SRM 51-74-10, TWO AREAS IN LIDec 18, 2012 · N664FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201212184320Seat Track · corrodedSEAT TRACK 1 BETWEEN FR 27 AND FR 28 TOP SURFACE CORROSION. AFTER CORROSION REMOVAL AREA IS OUT OF LIMITS. ORIG THICKNESS 0.078. THICKNESS AFTER REMOVAL 0.053. OUT OF LIMITS IAW SRM 53-10-16, PG 105, FIG A. REMOVED CORRSION FROM FLOOR STRUCTURE FR 27-FR 28 SDec 18, 2012 · N664FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201212174314Floor Panel · delaminatedFLOOR PANEL 231EF TOP SKIN HAS EXPOSED HONEYCOMB CORE. FABRICATED REPLACEMENT FLOOR PANEL IAW DWG SRZ 25-005, REV J.Dec 17, 2012 · N664FE · Airbus A300F4605R · Fuselage Floor Panel
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