N668FE

Service difficulty reports · 250

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 = 'N668FE' 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 FDEA201309032108Cargo Track · wornCARGO TRACK WORN FR 58-59 AT STA -1456 BETWEEN FLOOR PANELS 252RH AND 252QH MCD. CARGO TRACK REPLACED IAW SRM 53-10-16, FIG 201.Sep 3, 2013 · N668FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201309032105Floor Support · damagedCABIN FLOOR STRUCTURE, SEAT TRACK FR 14-17 AT Y450 HAS EVIDENCE OF SURFACE DETERIORATION SEAT TRACK AT FR 14-17, STA Y450. REPLACED IAW SRM 51-40-21. REPAIR CLASSED AS MAJOR.Sep 3, 2013 · N668FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA201309022104Floor Support · damagedCABIN FLOOR SUPPORT STRUCTURE FR 14-17 AT STA -Y1959, EVIDENCE OF SURFACE DETERIORATION AND DAMAGE AROUND FASTENER HOLES -Y1959 CABIN FLOOR TOP CAP SUPPORT STRUCTURE REPLACED IAW SRM 51-40-21 AND SRM 51-72-10 AT FR 14-17 AT STA -Y1959. REPAIR CLASSED AS MAJORSep 2, 2013 · N668FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA201309012098Seat Track · corrodedSEAT TRACK AT FWD CABIN LT SIDE FR12-17, Y1959 HAS EVIDENCE OF CORROSION. SEAT TRACK AT FWD CABIN LT SIDE FR12-17, Y1959 REPLACED IAW SRM 51-40-44.Sep 1, 2013 · N668FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201308312096Crossbeam · damagedFWD CARGO BAY, LT SIDE CROSSBEAM AT FR38, INBD OF SEAT RAIL Y953, EVIDENCE OF DAMAGE ON THE FWD FACE FWD CARGO BAY, LT SIDE CROSS BEAM AT FR38, INBD OF SEAT RAIL Y953 FWD FACE BLENDED IAW SRM 51-75-00 AND EA 6-5314-T0302193 P1, SURFACE REPROTECTED IAW SRM Aug 31, 2013 · N668FE · Airbus A300F4605R · Fuselage Main, StructureSDR FDEA201308312094Floor Support · corrodedCABIN FLOOR SUPPORT STRUCTURE, FR11-16, Y953 HAS VARIOUS AREAS OF SURFACE DETERIORATION AND BARE METAL. CABIN FLOOR STRUCTURE FROM FR11-16, Y953 REPLACED IAW SRM 51-72-10 AND DWG A53612550.Aug 31, 2013 · N668FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA201308312093Floor Support · corrodedCABIN FLOOR SUPPORT STRUCTURE FR11-14 Y730 FOUND HEAVILY CORRODED. CABIN FLOOR SUPPORT STRUCTURE FR11-14 LT Y730 REPLACED IAW SRM 53-12-15 AND DWG A53612214.Aug 31, 2013 · N668FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA201308312092Seat Track · corrodedSEAT TRACK Y-1959 FR45-54 HAS SIGNS OF CORROSION ON OTBD FLANGE BETWEEN FR50-51. FABRICATED SEAT TRACK Y-1959 FR45-54 INSTALLED IAW SRM 51-72-10.Aug 31, 2013 · N668FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201308312090Seat Track · corrodedSEAT TRACK FR15-17 Y-450 HAS EVIDENCE OF SURFACE DETERIORATION. REPLACED IAW SRM 51-72-10.Aug 31, 2013 · N668FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201308302080Spar · crackedRT WING FRAME 47, VERTICAL HOLE G, REF EO 6-5710-7-3305PT4 HAS CRACK INDICATION HOLE DIA 0.515". REPAIRED IAW EA 6-5710-T0301726.Aug 30, 2013 · N668FE · Airbus A300F4605R · Wing SparSDR FDEA201308282058Seat Track · corroded-Y953, FRAMES 51-54 SEAT TRACK HAS TWO AREAS OF CORROSION. REMOVED CORROSION IAW SRM 51-22-00. FOUND TO BE OUT OF LIMITS IAW SRM 53-10-16. SEAT TRACK REPLACED IAW SRM 51-40-21 AND SRM 51-72-10. MAJOR REPAIR.Aug 28, 2013 · N668FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201308272047Seat Track · corrodedSEAT TRACK -Y953 FRAMES 45-46 HAD SIGNS OF CORROSION. CORROSION BLENDED IAW SRM 53-10-16 AND FOUND OUT OF LIMITS. SEAT TRACK REPLACED.Aug 27, 2013 · N668FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201308272046Seat Track · corrodedSEAT TRACK -Y953 FRAMES 47-48, HAD SIGNS OF CORROSION, BLENDED IAW SRM 53-10-16 AND FOUND OUT OF LIMITS. SEAT TRACK REPLACED.Aug 27, 2013 · N668FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201308272045Seat Track · corrodedSEAT TRACK -Y953, FRAMES 50-51 HAS SIGNS OF CORROSION IN CENTER OF TRACK. BLENDED IAW SRM 53-10-16 AND FOUND OUT OF LIMITS. SEAT TRACK REPLACED.Aug 27, 2013 · N668FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201308262037Skin · gougedRIGHT INBD FLAP UPPER SURFACE HAS TWO GOUGES FOUND APPROX 85 INCHES FROM OTBD EDGE. GOUGES ASSESSED IAW SRM 57-50-00, SHT 5, FIG 101 TO 105 AND FOUND TO BE OUT OF SRM LIMITS. REPAIRED IAW EA 6-5700-T0301962. MAJOR REPAIR.Aug 26, 2013 · N668FE · Airbus A300F4605R · Trailing Edge FlapsSDR FDEA201308201972Seat Track · wornSEAT TRACK WORN FR 60, REPLACED.Aug 20, 2013 · N668FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201308201970Seat Track · crackedLATERAL SEAT TRACK FITTING SHEARED AT FR 61. REPLACED IAW SRM 51-72-10 REF AIB DWG A53278288203, MAJOR REPAIR CAT A REPLACMENT.Aug 20, 2013 · N668FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201308201969Seat Track · crackedSEAT TRACK FITTING SHEARED AT FR 61. REPLACED IAW SRM 51-72-10 REF DWG A53278288203, MAJOR REPAIR CAT A REPLACMENT.Aug 20, 2013 · N668FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201308201968Seat Track · wornSEAT TRACK WORN FR 58. REPLACED IAW SRM 51-72-10 IAW DWG A53278286 MAJOR REPAIR CAT A REPLACMENT.Aug 20, 2013 · N668FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201308171927Floorbeam · crackedFLOORBEAM AT FR 49 BETWEEN SEAT TRACK 3RD AND 4TH IN FROM RT OTBD SIDE (-Y1456 AND -Y1959) IS CRACKED. REPLACED IAW SRM 51-40-21.Aug 17, 2013 · N668FE · Airbus A300F4605R · Fuselage Main, Floor BeamSDR FDEA201308171924Seat Track · damagedSEAT TRACK AT FR 32 BETWEEN STA Y1456 AND Y1959 DAMAGED. REPLACED SEAT TRACK IAW SRM 51-40-21.Aug 17, 2013 · N668FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201308171923Floor Support · damagedMAIN DECK FLOOR SUPPORT ANGLE AT FR 62, DAMAGED MAIN DECK FLOOR SUPPORT ANGLE REPLACED IAW SRM 51-40-21 AND DWG A53275411.Aug 17, 2013 · N668FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA201308171922Seat Track · damagedLATERAL SEAT TRACK AT FR 30 BETWEEN STA Y450 AND Y953 DAMAGED LATERAL SEAT TRACK AT FR 30 BETWEEN STA Y450 AND Y953 REPLACED IAW SRM 51-40-21.Aug 17, 2013 · N668FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201210313807Gcu · failedDURING TAKEOFF ROLL, RECEIVED GEN 2 FAULT AND OBVIOUS POWER TRANSFER. ABORTED TAKEOFF. ATTEMPTED ONE RESET IAW CHECKLIST. CSD OIL LEVEL OK DPI OK R & R GCU MM REF 24-22-12. RAN ENGINE IAW JRH, POWER TRANSFER OK VOLTS/FREQS GOOD.Oct 31, 2012 · N668FE · Airbus A300F4605R · AC Generator-AlternatorSDR FDEA201112215413Indicator · malfunctionedNR 1 N1 ANALOG NEEDLE WOULD NOT INCREASE ABOVE 45 PERCENT ON TAKEOFF. R& R NR1 ENG N1 GAUGE REF MM 77-11-21-04; OPS CHECKS GOOD. OK FOR SERVICE.Dec 21, 2011 · N668FE · Airbus A300F4605R · Engine RPM Indicating SystemSDR FDEA201104161507Rib · wornRT WING RIB 5 FITTING HAS 2 EA SECOND OVERSIZE LOCK FASTENER INSTALLED IN HOLES 47/54. REAMED AND COUNTERSUNK HOLES 47 AND 54 TO THIRD OVERSIZE INTERFERENCE FIT 0.8095 IAW EA 6-5710-136750 AND REPAIR DWG R57150117 ISSUE B INSTALLED OVERSIZE FASTENERS IAW SApr 16, 2011 · N668FE · Airbus A300F4605R · Wing, Rib/BulkheadSDR FDEA201104161506Skin · wornLT WING RIB 5 FITTING HAS 2 EA TAPERLOKS INSTALLED AT HOLES 47/54 REWORKED SPOTFACE AND INSTALLED NEW TAPERLOKS AT HOLES 47/54 IAW EA 6-5710-136750 TITLE WINGS- AD2010-23-26-EO6-5710-7-3325-SB A300-57-6110-MLG RIB 5 SPOTFACE ON THE BOTTOM FLANGE.Apr 16, 2011 · N668FE · Airbus A300F4605R · Wing, Plate/SkinSDR FDEA201103301243Floor Panel · brokenAFT CARGO PIT FLOOR PANEL 152 XF IS BROKEN.Mar 30, 2011 · N668FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201103301242Floor Panel · brokenAFT CARGO PIT FLOOR PANEL 152 WF IS BROKEN.Mar 30, 2011 · N668FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201103221117Skin · crackedWHILE ACCOMPLISHING EO 6-5710-7-5013, PT5 FOUND CRACKS IN HOLE "G" (REF FIG 2, ITEM 21). IAW STEP 6-D. "IF ANY CRACKS ARE FOUND REFER TO EO PART 1. (ISB A300-57- 6029)". REPAIRED PER EA 6-5730-136749.Mar 22, 2011 · N668FE · Airbus A300F4605R · Wing, Plate/SkinSDR FDEA201103221116Skin · crackedWHILE ACCOMPLISHING EO 6-5710-7-5013, FOUND CRACKED HOLE "G". REPAIRED PER FEDEX EA 6-5730-136749.Mar 22, 2011 · N668FE · Airbus A300F4605R · Wing, Plate/SkinSDR FDEA201103221125Skin · crackedFOUND A CRACK ON THE LT WING LOWER SKIN IN HOLE "S" AT THE 2 O'CLOCK AND 11 O'CLOCK POSITIONS. REAMED HOLE "S" TO .639 IAW SRM 51-40-44. PERFORMED BHEC OF HOLE "S" PER NDTM PT6 51-10-01. NO CRACKS NOTED. FASTENER INSTALLED ON CARD 6-5710-7-3305, PT 3.Mar 22, 2011 · N668FE · Airbus A300F4605R · Wing, Plate/SkinSDR FDEA201103221124Skin · crackedFOUND A CRACK ON THE LEFT WING LOWER SKIN IN HOLE "Q" AT THE 8 0'CLOCK POSITION. REAMED HOLE "Q" TO .639 IAW SRM 51-40-44. PERFORMED BHEC OF HOLE "Q" PER NDTM PT6 51-10-01. NO CRACKS NOTED. FASTENER INSTALLED ON CARD 6-5710-7-3305, PT 3.Mar 22, 2011 · N668FE · Airbus A300F4605R · Wing, Plate/SkinSDR FDEA201103221123Skin · crackedFOUND A CRACK ON THE RT WING LOWER SKIN IN HOLE "G" AT THE 5 O'CLOCK POSITION. REAMED HOLE "G" TO .511 IAW A300-600 SRM 51-40-44. ACCOMPLISHED BHEC OF HOLE "G" PER NDTM PT6 51-10-01. NO CRACKS NOTED. FASTENER INSTALLED ON CARD 6-5710-7-3305, PT 4.Mar 22, 2011 · N668FE · Airbus A300F4605R · Wing, Plate/SkinSDR FDEA201103221122Skin · crackedFOUND A CRACK ON THE RIGHT WING LOWER SKIN IN HOLE "C" AT THE 2 0'CLOCK POSITION. REAMED HOLE "C" TO .526 IAW SRM 51-40-44. PERFORMED BHEC HOLE "C" PER NDTM PT6 51-10-01. CRACK INDICATORS ARE AT SHIM LOCATION LAYER NR 3. NO FURTHER ACTION REQUIRED. FASTENEMar 22, 2011 · N668FE · Airbus A300F4605R · Wing, Plate/SkinSDR FDEA201103221121Seat Track · gougedSEAT TRACK IN UPPER MAIN CABIN DECK AT FRAME 32 & 69 IS WORN & GOUGED. REMOVED AND REPLACED ADAPTER IAW SRM 51-40-21, PG 24 AND SRM 53-10-16, FIG 101.Mar 22, 2011 · N668FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201103221118Seat Track · wornRT NR 6 HALF TRACK FROM FRAME 54 TO FRAME 54.2 EXCEEDS WEAR LIMITS IAW EO 6-5310-7-3322 PT1, STEP 15. REMOVED 6 CLIPS FROM THE DAMAGED TRACK IAW SRM 51-40-21, PG 24. DRILLED & TRANSFERED HOLES ON NEW TRACK IAW SRM 51-72-10, PG 2. INSTALLED 6 CLIPS TO NEW TRMar 22, 2011 · N668FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201103181071Floor Panel · damagedMAIN CABIN COMPARTMENT FLOOR PANEL 252 ZF IS DAMAGED. FABRICATED NEW FLOOR PANEL 252 ZF IAW DWG SRZ 25-005, REV "H".Mar 18, 2011 · N668FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201103181070Floor Panel · damagedMAIN CABIN COMPARTMENT FLOOR PANEL 251 WG IS DAMAGED. FABRICATED NEW FLOOR PANEL 251 WG IAW DWG SRZ 25-005, REV "H".Mar 18, 2011 · N668FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201103181069Floor Panel · damagedMAIN CABIN COMPARTMENT FLOOR PANEL 251 PG IS DAMAGED. FABRICATED NEW FLOOR PANEL 251 PG IAW DWG SRZ 25-005, REV "H".Mar 18, 2011 · N668FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201103181068Floor Panel · damagedMAIN CABIN COMPARTMENT FLOOR PANEL 251 GF IS DAMAGED. FABRICATED NEW FLOOR PANEL 251 GF IAW DWG SRZ 25-005, REV "H".Mar 18, 2011 · N668FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201103181067Floor Panel · damagedMAIN CABIN COMPARTMENT FLOOR PANEL 232 FG IS DAMAGED. FABRICATED NEW FLOOR PANEL 232 FG IAW DWG SRZ 25-005, REV "H".Mar 18, 2011 · N668FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201103181066Floor Panel · puncturedTAIL COMPARTMENT AFT OF THE PRESSURE BULKHEAD; FWD LT FLOOR PANEL HAS A PUNCTURE HOLE. FABRICATED NEW FLOOR PANEL AFT TAIL TAIL COMPARTMENT IAW FEDEX DWG SRZ 25-005, REV "H".Mar 18, 2011 · N668FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201103181072Jackscrew · inoperativeDURING FLAP RETRACTION FLAPS STUCK AT 20 DEGS WITH FLAPS FAULT SYS 1 & 2 LIGHT ON OVERHEAD. FOLLOWED ECAM/QRCH FLAPS REMAINSED AT 20 DEGS AT 20 DEGS. ON APPROACH SELECTED AND GOT FLAPS 40. AFTER LANDING FLAPS RETRACTED NORMALLY-REPEAT. REMOVED AND REPLACMar 18, 2011 · N668FE · Airbus A300F4605R · Trailing Edge Flap Control SystemSDR FDEA201103171050Floor Panel · damagedMAIN CABIN COMPARTMENT FLOOR PANEL 231 TG IS DAMAGED. FABRICATED NEW FLOOR PANEL 231 TG IAW DWG SRZ 25-005, REV "H".Mar 17, 2011 · N668FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201103171049Floor Panel · damagedMAIN CABIN COMPARTMENT FLOOR PANEL 261 AH IS DAMAGED. FABRICATED NEW FLOOR PANEL 261 AH IAW DWG SRZ 25-005, REV "H".Mar 17, 2011 · N668FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201103171048Floor Panel · damagedMAIN CABIN COMPARTMENT FLOOR PANEL 252 YG IS DAMAGED. FABRICATED NEW FLOOR PANEL 252 YG IAW DWG SRZ 25-005, REV "H".Mar 17, 2011 · N668FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201103171047Floor Panel · damagedMAIN CABIN COMPARTMENT FLOOR PANEL 252 VF IS DAMAGED. FABRICATED NEW FLOOR PANEL 252 VF IAW DWG SRZ 25-005, REV "H".Mar 17, 2011 · N668FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201103171046Floor Panel · damagedMAIN CABIN COMPARTMENT FLOOR PANEL 252 TH IS DAMAGED. FABRICATED NEW FLOOR PANEL 252 TH IAW DWG SRZ 25-005, REV "H".Mar 17, 2011 · N668FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201103171045Floor Panel · damagedMAIN CABIN COMPARTMENT FLOOR PANEL 252 NH IS DAMAGED. FABRICATED NEW FLOOR PANEL 252 NH IAW DWG SRZ 25-005, REV "H".Mar 17, 2011 · N668FE · Airbus A300F4605R · Fuselage Floor Panel
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