N663FE

Service difficulty reports · 264

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 = 'N663FE' 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 FDEA201702020367Floor Panel · damagedAFT CARGO BAY FLOOR PANEL 151SF FOUND DAMAGED & DELAMINATED. FABRICATED A NEW FLOOR PANEL IAW SRZ-25-005. MAJOR REPAIR.Feb 2, 2017 · N663FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201702020366Floor Panel · damagedAFT CARGO BAY FLOOR PANEL 151QF DAMAGED AND DELAMINATED. FABRICATED A NEW FLOOR PANEL IAW SRZ-25-005. MAJOR REPAIR.Feb 2, 2017 · N663FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201702020364Floor Panel · damagedAFT CARGO FLOOR PANEL 152XF HAS A CRUSHED CORNER. FABRICATED A NEW FLOOR PANEL IAW SRZ-25-005. MAJOR REPAIR.Feb 2, 2017 · N663FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201702020363Floor Panel · damagedAFT CARGO FLOOR PANEL 152TF HAS CRUSHED CORNER. FABRICATED A NEW FLOOR PANEL IAW SRZ-25-005. MAJOR REPAIR.Feb 2, 2017 · N663FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201702020361Floor Panel · damagedAFT CARGO FLOOR PANEL 152MF HAS HOLES IN THE LOWER SKIN. FABRICATED A NEW FLOOR PANEL IAW SRZ-25-005. MAJOR REPAIR.Feb 2, 2017 · N663FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201702010301Seat Track · crackedMAIN DECK FRAME 60, LT 953 SEAT TRACK BENT AND CRACKED CHECKED LIMITS, FOUND OUT OF LIMITS IAW SRM 53-10-10. REMOVED SEAT TRACK DAMAGE, LOCATED AND DRILLED SEAT TRACK AND 2EA SPLICES. REPAIRED IAW SRM 51-40-21, FABRICATED SEAT TRACK, AND SPLICE IAW SRM 53-10Feb 1, 2017 · N663FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201702010300Shear Plate · crackedSHEAR PLATE CRACKED IN MAIN DECK CARGO COMPARTMENT BETWEEN FR79 AND FR80 Y1650. REMOVED AND REPLACED SHEAR PLATE P/N A5398111320051 IAW SRM 51-40-21, LOCATED AND DRILLED NEW PART IAW SRM 51-40-44. TOP COATED FASTENERS IAW SRM 51-75-10 ON SHEAR PLATE BETWEEN FRFeb 1, 2017 · N663FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA201502240590Priority Valve · leakingON LANDING, BLUE HYDRO SYS DUMPED FLUID TO ZERO. INSPECTED WW FOUND PRIORITY VLV FOR BLUE & GREEN HP MANIFOLD AT FAULT. R & R PRIORITY VLV 2064 IAW AMM 27-14-14-04-0. INSPECTED BLUE HYD SYS CASE DRAIN, RETURN, & DELIVERY FILTERS IAW AMM 29-00-00-03. NO REDFeb 24, 2015 · N663FE · Airbus A300F4605R · Hydraulic System, MainSDR FDEA201502190554Rib · corrodedLEFT MLG FWD LUG HAS CORROSION IN BORE & ON FWD & AFT FACES. COMPLIED WITH MOD T 6-5710-T314933 P 1 & P 2.Feb 19, 2015 · N663FE · Airbus A300F4605R · Wing, Rib/BulkheadSDR FDEA201501050255Lug · corrodedRIGHT MLG FWD LUG HAS CORROSION IN BORE & ON FWD & AFT FACES. COMPLIED WITH EA 6-5710-T0314857 WINGS, BASIC WING STRUCTURE AD 2012-15-14 & 2012-08-03 MLG RT RIB 5 FWD LUG. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR.Jan 5, 2015 · N663FE · Airbus A300F4605R · Wing, Landing Gear Attach FittingsSDR FDEA201409262799Mount · corrodedNR 2 PYLON FWD PYRAMID MOUNT LOWER MATING SURFACE & UPPER SURFACE TO INCLUDE SPOT FACES ARE RUSTY. REMOVED RUST IAW SRM 51-74-10. ACCOMPLISHED REPAIR ON EA 6-5450-143832 B PART 2. NACELLES PYLONS PYLON STRUCTURE NR 2 ENG PYLON TO ENG OTBD BASE PLATE FITTISep 26, 2014 · N663FE · Airbus A300F4605R · Nacelle/Pylon, Attach FittingsSDR FDEA201409192784Adapter · out of alignmentMCD SEAT TRACK ADAPTER AT FRAME 66, Y1458 DOES NOT ALIGN WITH CARGO LOADING SYS. R & R SEAT TRACK ADAPTER IAW SRM 51-40-21 PN A5327411202 AT FRAME 66 Y1458. CLASSIFIED AS CAT A MAJOR REPAIR.Sep 19, 2014 · N663FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201409152701Angle · corrodedFRAME FEET RT SIDE FRAME 46 FOUND CORRODED ANGLE WHILE ACCOMPLISHING EO 6-5310-7-5015 PT 2. FRAME 46 RT ANGLE CORRODED, BLENDED AREA IAW SRM 51-74-10 & OUT OF LIMITS IAW SRM 53-15-13, DIMENSIONS L=2.0 INCHES W=1.0 INCH D=0.035 INCHES. REMOVED ANGLE, FABRICASep 15, 2014 · N663FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA201409112587Floorboard · damagedMAIN DECK BETWEEN FRAMES 62 & 65 FROM SEAT TRACK -Y1456 & -Y1959. FLOORBOARD 252YG HAS DAMAGE. REMOVED FLOORBOARD IAW AMM 53-10-25. FABRICATED FLOORBOARD IAW T14 1089703 IAW DWG SR2 25-005. INSTALLED FLOORBOARD IAW AMM 53-10-25. CLASSIFIED CAT A MAJOR RESep 11, 2014 · N663FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201409112590Floor Panel · damagedMAIN DECK BETWEEN FRAME 65 & 69 & FROM SEAT TRACK Y1456 & Y1959 FLOORBOARD IS DAMAGED. REMOVED & INSTALLED PANEL 251BH IAW AMM 53-10-25. FABRICATED PANEL IAW T14 1090225 IAW DWG SR2 25-005. CLASSIFIED AS CAT A MAJOR REPAIR.Sep 11, 2014 · N663FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201409112589Floor Panel · damagedMAIN DECK BETWEEN FRAME 55 & 57.1 & FROM SEAT TRACK -Y953 & -Y1456 FLOORBOARD FASTENER HOLE DAMAGED. REMOVED PANEL 252MG IAW AMM 53-10-25. FABRICATED PANEL IAW T14 1089706 IAW DWG SR2 25-005. INSTALLED PANEL IAW AMM 53-10-25. CLASSIFIED AS CAT A MAJOR RESep 11, 2014 · N663FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201409112588Floor Panel · damagedMAIN DECK BETWEEN FRAME 61 & 62 & FROM SEAT -Y1456 & -Y1959 FLOORBOARD HAS DAMAGED. REMOVED PANEL 252WH IAW AMM 53-10-25. FABRICATED PANEL IAW T14 1089704 IAW DWG SR2 25-005. INSTALLED PANEL IAW AMM 53-10-25. CLASSIFIED AS CAT A MAJOR REPAIR.Sep 11, 2014 · N663FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201409112586Floor Panel · damagedMDC FLOOR PANEL 241QJ DAMAGED INSERTS. FABRICATED NEW FLOOR PANEL 241QJ ON 14/1088978 IAW DWG SR2 25-005 REV K, CLASSIFIED AS MAJOR CAT A REPAIR.Sep 11, 2014 · N663FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201409112585Floor Panel · crackedMDC FLOOR PANEL 242EK CRACKED. FABRICATED NEW FLOOR PANEL ON T14 1088833 IAW DWG SR2 25-005 REV K, CLASSIFIED AS MAJOR CAT A REPAIR.Sep 11, 2014 · N663FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201409102560Floorboard · crackedMAIN DECK BETWEEN FRAMES 30 & 34, FROM SEAT TRACK Y1959 TO Y1456 FLOORBOARD HAS CRACKED DAMAGE. REMOVED FLOORBOARD 241DF IAW SRM 51-40-00. FABRICATED NEW FLOORBOARD IAW DWG SR2 25-005 & REINSTALLED FLOORBOARD IAW AMM 53-10-23-04. CLASSIFIED AS MAJOR CAT A RSep 10, 2014 · N663FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201409102551Floor Panel · crackedMDC FLOOR PANEL 242UJ CRACKED. FABRICATED NEW PANEL ON T14 1088834 IAW DWG SR2 25-005 REV K, CLASSIFIED AS MAJOR CAT A REPAIR.Sep 10, 2014 · N663FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201409102550Floor Panel · crackedMDC FLOOR PANEL 241AJ CRACKED. FABRICATED NEW PANEL ON T14 1088974 IAW DWG SR2 25-005 REV K CLASSIFIED AS MAJOR CAT A REPAIR.Sep 10, 2014 · N663FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201409072529Floor Panel · crackedMDC FLOOR PANEL 241TH CRACKED. FABRICATED NEW PANEL ON T14 1088971 IAW DWG SR2 25-005 REV K, CLASSIFIED AS MAJOR CAT A REPAIR.Sep 7, 2014 · N663FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201409072528Floor Panel · crackedMDC FLOOR PANEL 242LK CRACKED. FABRICATED NEW PANEL ON T14 1089707 IAW DWG SR2 25-005 REV K, CLASSIFIED AS MAJOR CAT A REPAIR.Sep 7, 2014 · N663FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201409072527Floor Panel · delaminatedFLOOR PANEL 161AF TOP SKIN IS DIS BONDED AT EDGE AREA AS MARKED. FABRICATED PANEL ON T14 1089394 IAW DWG SR2 25-005 REV K, CLASSIFIED AS MAJOR CAT A REPAIR.Sep 7, 2014 · N663FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201409072526Floor Panel · delaminatedFLOOR PANEL 161JF EDGE IS DELAMINATED. FABRICATED NEW PANEL ON T14 1089393 IAW DWG SR2 25-005 REV K, CLASSIFIED AS MAJOR CAT A REPAIR.Sep 7, 2014 · N663FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201409072524Floor Panel · damagedFLOOR PANEL 161GF EDGES ARE BROKEN. FABRICATED NEW PANEL ON T14 1089391 IAW DWG SR2 25-005 REV K, CLASSIFIED AS MAJOR CAT A REPAIR.Sep 7, 2014 · N663FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201409072523Floor Panel · damagedFLOOR PANEL 152VF HAS BROKEN EDGES. FABRICATED NEW PANEL ON T14 1089387 IAW DWG SR2 25-005 REV K, CLASSIFIED AS MAJOR CAT A REPAIR.Sep 7, 2014 · N663FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201409072522Floor Panel · damagedFLOOR PANEL 161BF TOP SKIN HAS SEVERAL PUNCTURED AREAS AS MARKED. FABRICATED NEW PANEL ON T14 1089395 IAW DWG SR2 25-005 REV K, CLASSIFIED AS MAJOR CAT A REPAIR.Sep 7, 2014 · N663FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201409072521Floor Panel · damagedFLOOR PANEL 151VF CORNER EDGES ARE BROKEN. FABRICATED NEW PANEL ON T14 1089388 IAW DWG SR2 25-005 REV K, CLASSIFIED AS MAJOR CAT A REPAIR.Sep 7, 2014 · N663FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201409072520Floor Panel · damagedFLOOR PANEL 131PG EDGES ARE BROKEN AS MARKED. FABRICATED NEW PANEL ON 14 1089396 IAW DWG SR2 25-005 REV K, CLASSIFIED AS MAJOR CAT A REPAIR.Sep 7, 2014 · N663FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201409072519Floor Panel · damagedFLOOR PANEL 151WF CORNER IS PUNCTURED. FABRICATED NEW PANEL ON T14 1089389 IAW DWG SR2 25-005 REV K, CLASSIFIED AS MAJOR CAT A REPAIR.Sep 7, 2014 · N663FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201409072518Floor Panel · damagedFLOOR PANEL 131MG EDGES ARE BROKEN AS MARKED. FABRICATED NEW PANEL ON T14 1089398 IAW DWG SR2 25-005 REV K, CLASSIFIED AS MAJOR CAT A REPAIR.Sep 7, 2014 · N663FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201409072517Floor Panel · damagedFLOOR PANEL 131KG EDGES ARE BROKEN. FABRICATED NEW PANEL ON T14 1089397 IAW DWG SR2 25-005 REV K, CLASSIFIED AS MAJOR CAT A REPAIR.Sep 7, 2014 · N663FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201409072516Floor Panel · damagedFLOOR PANEL 132PG EDGES ARE BROKEN. FABRICATED NEW PANEL ON T14 1089400 IAW DWG SR2 25-005 REV K, CLASSIFIED AS MAJOR CAT A REPAIR.Sep 7, 2014 · N663FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201409072515Floor Panel · damagedFLOOR PANEL 132MG EDGES ARE BROKEN AS MARKED. FABRICATED NEW PANEL ON T14 1089399 IAW DWG SR2 25-005 REV K, CLASSIFIED AS MAJOR CAT A REPAIR.Sep 7, 2014 · N663FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201409072514Floor Panel · damagedFLOOR PANEL 152XF EDGES ARE BROKEN. FABRICATED NEW PANEL ON T14 1089390 IAW DWG SR2 25-005 REV K, CLASSIFIED AS MAJOR CAT A REPAIR.Sep 7, 2014 · N663FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201409072513Floor Panel · damagedMDC FLOOR PANEL 241UH PUNCTURED. FABRICATED NEW PANEL ON T14 1088976 IAW DWG SR2 25-005 REV K, CLASSIFIED AS MAJOR CAT A REPAIR.Sep 7, 2014 · N663FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201409062484Floor Panel · crackedMDC FLOOR PANEL 241UJ CRACKED. FABRICATED NEW FLOOR PANEL ON T14 1088835 IAW DWG SR2 25-005 REV K, CLASSIFIED AS MAJOR CAT A REPAIR.Sep 6, 2014 · N663FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201409062497Track · misinstalledRIGHT DUMMY SEAT TRACK FRAME 38.2 TO .40 NR 3 TRACK, GAP VALUE GREATER THAN .0393 INCHES. FABRICATED INSERT ON T14 1089710 IAW SRM-53-15-16 FIG 201. REPAIRED RT DUMMY SEAT TRACK IAW-A300-SRM-53-15-16 FIG. 201. INSTALLED TRACK IAW-SRM-53-15-16 FIG 201 CAT A Sep 6, 2014 · N663FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201409062496Dummy Rail · misinstalledLEFT NR 5 DUMMY SEAT TRACK FRAME 54 TO 54.2, GAP VALUE IS GREATER THAN .0393 INCHES. FABRICATED INSERT ON T14 1089753 IAW-SRM-53-15-16, REPAIRED IAW SRM-53-15-16 FIG 201 & INSTALLED TRACK IAW-SRM-53-15-16 FIG 201 CAT A MAJOR REPAIR.Sep 6, 2014 · N663FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201409062495Dummy Rail · misinstalledRIGHT NR 5 DUMMY SEAT TRACK FRAME 54 TO 54.2 GAP VALUE IS GREATER THAN .0393 INCHES. FABRICATED INSERT ON T14 1089751 IAW-SRM-53-15-16 FIG 201. REPAIRED IAW-SRM-53-15-16, INSTALLED TRACK IAW-SRM-53-15-16 FIG 201 CAT A MAJOR REPAIR.Sep 6, 2014 · N663FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201409062494Dummy Rail · misinstalledLEFT NR 4 DUMMY SEAT TRACK FRAME 54 TO 54.2 GAP VALUE IS GREATER THAN .0393 INCHES. FABRICATED INSERT ON T14 1089752 IAW-SRM-53-15-16 FIG 201. REPAIRED IAW SRM-53-15-16 CAT A. MAJOR REPAIR.Sep 6, 2014 · N663FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201409062483Floor Panel · crackedMDC FLOOR PANEL 242ZJ CRACKED. FABRICATED NEW PANEL ON T14 1088977 IAW DWG SR2 25-005 REV K, CLASSIFIED AS MAJOR CAT A REPAIR.Sep 6, 2014 · N663FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201409052467Floor Panel · crackedMDC FLOOR PANEL 241RH PUNCTURED. FABRICATED NEW PANEL ON T14 1088973 IAW DWG SR2 25-005 REV K CLASSIFIED AS MAJOR CAT A REPAIR.Sep 5, 2014 · N663FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201409052466Floor Panel · crackedMDC FLOOR PANEL 242UH PUNCTURED. FABRICATED FLOOR PANEL ON T14 1088836 IAW DWG SR2 25-005 REV K CLASSIFIED AS MAJOR CAT A REPAIR.Sep 5, 2014 · N663FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201409052462Floor Panel · crackedMDC FLOOR PANEL 241HK CRACKED. FABRICATED NEW PANEL ON T14 1088832 IAW DWG SR2 25-005 REV K CLASSIFIED AS MAJOR CAT A REPAIR.Sep 5, 2014 · N663FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201409042461Floor Panel · crackedMDC FLOOR PANEL 242WH CRACKED. FABRICATED NEW PANEL ON T14 1088975 IAW DWG SR2 25-005 REV K, CLASSIFIED AS MAJOR CAT A REPAIR.Sep 4, 2014 · N663FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201409022558Crossbeam · corrodedMCD CROSSBEAM FRAME 38.2 TO 40 CORRODED RT NR 3. FABRICATED NEW CROSSBEAM ON T14 1090761 IAW DWG A53813164 & SRM 53-15-15. INSTALLED NEW CROSSBEAM IAW SRM 51-40-21. CLASSIFIED AS CAT A MAJOR REPAIR.Sep 2, 2014 · N663FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA201408252617Adapter · wornSEAT TRACK ADAPTER BETWEEN Y-450 & Y-953 AT FRAME 46 HAS EXCESSIVE PLAY. R & R FLOOR ADAPTER IAW SRM 51-40-21. RECEIVED NEW SEAT TRACK ADAPTOR WITH PN A5381293220100 BATCH 0002680562. LOCATED & DRILLED NEW ADAPTOR IAW SRM 51-40-44. CLASSIFIED AS CAT A MAJOAug 25, 2014 · N663FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach Fittings
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