N660FE

Service difficulty reports · 227

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 = 'N660FE' 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 FDEA201608082836Floor Panel · crackedAFT CARGO FLOOR PANEL 152WF CRACKED, FABRICATED FLOOR PANEL 152WF ON T16/1221962 IAW SRZ-25-005, CAT-A. MAJOR REPAIR.Aug 8, 2016 · N660FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201608062830Floor Panel · damagedAFT CARGO FLOOR PANEL 152QF HAS SEVERAL DAMAGED AND MISSING INSERTS. FABRICATED FLOOR PANEL 152QF ON T16/1221900 IAW SRZ-25-005, CAT-A, MAJOR REPAIR.Aug 6, 2016 · N660FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201608042818Floor Panel · delaminatedFLOOR PANEL 252UH IS DELAMINATED. FABRICATED A NEW FLOOR PANEL IAW SRZ-25-005. MAJOR.Aug 4, 2016 · N660FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201608042817Floor Panel · delaminatedFLOOR PANEL 252DH DELAMINATED. FABRICATED A NEW FLOOR PANEL IAW SRZ-25-005. MAJOR.Aug 4, 2016 · N660FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201608042816Floor Panel · crackedFLOOR PANEL 242EK CRACKED. FABRICATED A NEW FLOOR PANEL IAW SRZ- 25-005. MAJOR REPAIR.Aug 4, 2016 · N660FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201608042809Floor Panel · brokenMDCC FLOOR PANEL 241FJ BROKEN. FABRICATED A NEW FLOOR PANEL IAW SRZ-25-005. MAJOR REPAIR.Aug 4, 2016 · N660FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201608042808Floor Panel · damagedMAIN CABIN FLOOR PANEL 231GH PUNCTURED IN MULTIPLE AREAS. FABRICATED A NEW FLOOR PANEL IAW SRZ-25-005. MAJOR REPAIR.Aug 4, 2016 · N660FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201608042807Floor Panel · brokenMAIN CABIN FLOOR PANEL 231HH BROKEN. FABRICATED A NEW FLOOR PANEL IAW SRZ-25-005. MAJOR REPAIR.Aug 4, 2016 · N660FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201608042806Floor Panel · brokenMAIN CABIN FLOOR PANEL 232HG BROKEN. FABRICATED FLOOR PANEL IAW SRZ-25-005. MAJOR REPAIR.Aug 4, 2016 · N660FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201608042805Floor Panel · puncturedMAIN CABIN FLOOR PANEL 231LG PUNCTURED IN MULTIPLE PLACES. FABRICATED A NEW FLOOR PANEL IAW SRZ-25-005. MAJOR REPAIR.Aug 4, 2016 · N660FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201608042804Floor Panel · puncturedMAIN CABIN FLOOR PANEL 231VG PUNCTURED IN MULTIPLE AREAS. FABRICATED A NEW FLOOR PANEL IAW SRZ-25-005. MAJOR REPAIR.Aug 4, 2016 · N660FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201608042803Floor Panel · brokenMDCC FLOOR PANEL 242UJ BROKEN. FABRICATED A NEW FLOOR PANEL IAW SRZ-25-005. MAJOR REPAIR.Aug 4, 2016 · N660FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201608042802Floor Panel · brokenMDCC FLOOR PANEL 231YG BROKEN. FABRICATED A NEW FLOOR PANEL IAW SRZ-25-005. MAJOR REPAIR.Aug 4, 2016 · N660FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201608042801Floor Panel · crackedFLOOR PANEL 242RG CRACKED AROUND CUT OUT. FABRICATED A NEW FLOOR PANEL IAW SRZ-25-005. MAJOR REPAIR.Aug 4, 2016 · N660FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201608042800Floor Panel · brokenMDCC FLOOR PANEL 251QH BROKEN. FABRICATED A NEW FLOOR PANEL IAW SRZ-25-005. MAJOR REPAIR.Aug 4, 2016 · N660FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201601140149Indication Sys · faultyR1 DOOR WILL NOT SHOW SLIDE ARMED ON ECAM. RELEASED FOR SERVICE. ECAM SLIDE INDICATION SYS FOR R1 DOOR INOPERATIVE. PERFORMED OPERATIONAL CHECK IAW 52-10-11-06-02. CYCLED DOOR NUMEROUS TIMES WITH NO FAULTS NOTED. ACFT OK TO CONTINUE.Jan 14, 2016 · N660FE · Airbus A300F4605R · Door Warning SystemSDR FDEA201507162248Idg · failedDURING TAKEOFF ROLL, NR 2 GEN IDG FAIL ANNUNCIATED ON THE ECAM. TAKEOFF REJECTED. R & R NR 2 GCU.Jul 16, 2015 · N660FE · Airbus A300F4605R · AC Generator-AlternatorSDR FDEA201412224180Battery Pack · inoperativeWHEN READY TO PUSH, FIRST OFFICER TRIED TO ARM SLIDE. RT SLIDE WOULD NOT ARM. RECEIVED A GREEN DOOR LOCKED INDICATION BUT NO SLIDE ECAM. REMOVED AUTONOMOUS POWER SUPPLY UNIT & BOTH BATTERIES IAW MM 52-73-18-04. OPS CHECKED GOOD IAW MM 52-73-00-05-02. ACFDec 22, 2014 · N660FE · Airbus A300F4605R · Escape SlideSDR FDEA201412224179Battery Pack · inoperativeESCAPE SLIDE RELEASE WARNING SYS LIGHTS INOPERATIVE. R & R AUTONOMOUS POWER SUPPLY UNIT & BATTERIES IAW MM 52-73-18-04. OPERATIONS TESTED GOOD IAW MM 52-73-00-05-02. ACFT OK TO CONTINUE.Dec 22, 2014 · N660FE · Airbus A300F4605R · Escape SlideSDR FDEA201406241536Mount Fitting · damagedEXISTING REPAIR ON LT ENG FWD MOUNT FITTING ALIGN HOLE REQUIRES EVALUATION FOR CONFORMITY. THE EXISTING REPAIR WAS EVALUATED & DAMAGE WAS FOUND IN THE HOLE OF FITTING. REPORT TO ENGINEER, REPAIR THE FITTING IAW EA6-5450-853.Jun 24, 2014 · N660FE · Airbus A300F4605R · Engine Mount SectionSDR FDEA201406201493Mount Fitting · corrodedLEFT ENG FWD MOUNT FITTING OTBD SIDE AFT ATTACHED HOLE UPPER SPOT FACE & HOLE FOUND CORROSION. COMPLIED WITH SRM54-51-81-101 PARA 4 A & EA 6-545-T0308811 PT 1 REPAIR LT ENG FWD MOUNT FITTING OTBD SIDE AFT ATTACHED HOLE.Jun 20, 2014 · N660FE · Airbus A300F4605R · Nacelle/Pylon Miscellaneous StructureSDR FDEA201406131427Fitting · crackedJUNCTION BETWEEN CTR WING BOX & CRUCIFORM FITTING BETWEEN FRAME 40 - 44. AT FRAMES & STIFFENERS INSPECTION FOUND CRACK SIGNAL AT FRAME 42 7.5 INCHES STIFFENER LT SIDE INBD FASTENER HOLE.Jun 13, 2014 · N660FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA201406131426Fitting · crackedJUNCTION BETWEEN CTR WING BOX & CRUCIFORM FITTING BETWEEN FRAME 40 - 44 AT FRAMES & STIFFENERS INSPECTION FOUND CRACK SIGNAL AT FRAME 42 - 7.5 INCHES STIFFENER LT SIDE OTBD FASTENER HOLE.Jun 13, 2014 · N660FE · Airbus A300F4605R · Wing Miscellaneous StructureSDR FDEA201406131425Fitting · crackedJUNCTION BETWEEN CTR WING BOX & CRUCIFORM FITTING BETWEEN FRAME 40 - 44. AT FRAMES & STIFFENERS INSPECTION FOUND CRACK SIGNAL AT FRAME 40 7.5 INCHES STIFFENER LT SIDE INBD FASTENER HOLE.Jun 13, 2014 · N660FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA201406111403Frame · crackedFRAME 44 HAS A CRACK SIGNAL BETWEEN STRINGERS 25 - 26R. REPLACED FRAME IAW SRM 51-40-21. MAJOR REPAIR IAW GMM6-2-100.Jun 11, 2014 · N660FE · Airbus A300F4605R · Fuselage Main, FrameSDR FDEA201301100071Windshield · crackedAT FL330, RECEIVED LT WINDOW HEAT FAULT COMPLIED WITH ECAM AND TURNED OFF. NOTICED CRACK ON CAPT'S WINDSCREEN. ACCORDING TO QRH, NEED TO LEAVE WINDOW HEAT OFF FLY FL250. COMPLIED MEL REQ TO STAY OUT OF ICING COND UNABLE TO DO SO SO DIVERTED. R & R WINDSHIJan 10, 2013 · N660FE · Airbus A300F4605R · Flight Compartment WindowsSDR FDEA201210293767Structure · corrodedRT WING OTBD FIXED T/E RIB 26 TO RIB 29 HAS 3" AREA OF CORROSION AT 2ND FROM INBD END STATIC WICK BELOW BASE WITH 60 PERCENT WORKING FASTENERS AND DISBONDED EDGES ALONG ENTIRE LENGTH. R & R RT WING FIXED T/E WEDGE IAW FSRM 51-72-10.Oct 29, 2012 · N660FE · Airbus A300F4605R · Wing Main, Frame StructureSDR FDEA201210263756Wedge · dentedRT WING LWR EXTERNAL SKIN OF ALL SPEED AILERON HAS 9 EA DENTS ON T/E WEDGE. REPAIRED 9 EA DENTS ON LWR T/E WEDGE OF RT ALL SPEED AILERON IAW FSRM 57-61-11 PB 201, PARA 4E WITHOUT DEVIATION. COMPLIED WITH EA 6-5750-T030028 PT 1 FOR RSC TRACKING. NO FOLLOW UOct 26, 2012 · N660FE · Airbus A300F4605R · AileronsSDR FDEA201210263755Bracket · crackedRT WING AFT OF REAR SPAR AT NR 2 ENG PYLON INTERFACE PANEL ATTACH WEB TO BOTTOM WING SKIN CRACKED 2EA.PLACES. MEASURED 2", AND 1.8" IN LENGTHS. R & R RT WING NR 2 PYLON AFT ATTACH WEB (BRACKET) REF TO SRM 51-72-10. PERFORMED OPS CHECK AND LEAK CHECK REF TO Oct 26, 2012 · N660FE · Airbus A300F4605R · Wing, Attach FittingsSDR FDEA201210263754Bracket · crackedLEFT WING AFT OF REAR SPAR AT ENG PYLON INTERFACE ATTACH WEB TO BOTTOM WING SKIN CRACKED AT ATTACH FASTENERS. MEASURED 1.5", 1.2", AND .7" IN LENGTHS. R & R LT WING NR 1 PYLON REAR SPAR AT AFT ATTACH WEB REF TO SRM 51-72-10. LEAK AND OPS CHECKED GOOD IAW AMMOct 26, 2012 · N660FE · Airbus A300F4605R · Wing, Attach FittingsSDR FDEA201210243742Mount · corrodedNR 2 PYLON FWD ENGINE MOUNT HAS FOUR TINSILE BOLT HOLES AND SPIGOT HOLE CUTOUTS HAVE OXIDATION AND MISSING FLAME SPRAY. COMPLIED WITH EA 6-5451-T0300018 PS PT 1 ON AFT IB TENSILE BOLT HOLE. CLEANED OXIDATION IAW FSRM 51-74-10, PG 205. NTD IAW NTM 51-60-00 ANOct 24, 2012 · N660FE · Airbus A300F4605R · Engine Mount SectionSDR FDEA201210233725Seat Track · corrodedMAIN DECK CARGO SEAT TRACK 6L HAS APPROX 12 SQ IN OF SURFACE OXIDATION BETWEEN FR 24 AND FR 26. R & R SEAT TRACK 6L FROM FR 18 TO FR 29 IAW SRM 51-72-10.Oct 23, 2012 · N660FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201210173656Structure · crackedDAMAGE ON RIGHT HAND FWD ENTRY DOOR LOWER EDGE FWD CORNER HAS 1.0" CRACK AND 3.0" LONG BENT AREA. REF WC 52105108 REPAIRED R1 DOOR IAW FSRM 52-11-00, FIG 206.Oct 17, 2012 · N660FE · Airbus A300F4605R · Passenger/Crew DoorsSDR FDEA201210153614Web · crackedLINER ATTACHMENT WEB ABOVE LOWER FWD CARGO DOOR (INTERNAL, UPPER FWD) HAS 2 FASTENER HOLES WITH CRACKED/BROKEN AREAS. MEASURED .25IN X .12IN, .15IN X .10IN. REMOVED CRACKED SHEET WEB ABOVE LWR FWD CARGO DOOR IAW SRM 51-40-21, PARA 6. LOCATED, DRILLED, AND INOct 15, 2012 · N660FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA201210143612Crossbeam · crackedFWD CARGO CEILING FR 23 HAS .5 INCH CRACK IN RADIUS BETWEEN SEAT TRACKS 2R & 3R. REPAIRED CROSSBEAM FR23 BETWEEN TRACK 2R & 3R IAW FSRM 53-10-15, PARA 15, PG 397/398, FIG 212.Oct 14, 2012 · N660FE · Airbus A300F4605R · Fuselage Main, StructureSDR FDEA201210133609Angle · corrodedFWD CARGO CEILING AREA AT FR 23R UNDER SEAT TRACK R3 HAS .50"X.50" AREA OF CORROSION AT FASTENER. COMPLIED WITH MOD TYPE T MOD NO. 6-5313-T0300015 REV NO. PS P1Oct 13, 2012 · N660FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201210093582Frame · dentedDURING REMOVAL OF MAIN DECK CARGO SIDEWALL ISOLATOR MOUNT BRACKET FOUND THE INBD SIDE OF FRAME 58, STRINGER 12L TO BE DENTED IN AND 2EA. ELONGATED HOLES. CUT OUT DAMAGED SECTION OF FRAME AND REPAIRED IAW FSRM 53-10-13 FIG 103.Oct 9, 2012 · N660FE · Airbus A300F4605R · Fuselage Main, FrameSDR FDEA201210083578Seat Track · corrodedMAIN DECK CARGO AT FR50, NR 1 SEAT TRACK EXFOLIATED TWO SQUARE INCHES. REMOVED CORROSION IAW SRM 51-74-10 PAR 3. CORROSION FOUND TO BE OUT OF LIMITS IAW SRM 53-10-16 FIG 102. REMOVED AND REPLACED SEAT TRACK IAW SRM 51-72-10. FABRICATED NEW TRACK PER DWG A53Oct 8, 2012 · N660FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201210063573Adapter · crackedFOUND CLEVIS ADAPTER AT FR 64 BETWEEN SEAT TRACK 4R AND 5R HAS A 4" CRACK IN FLANGE. REMOVED CRACKED CLEVIS ADAPTER AT FR 64 BETWEEN SEAT TRACK 4R AND 5R IAW SRM 51-40-21, PG 21. LOCATED, DRILLED AND INSTALLED NEW CLEVIS ADAPTER IAW FSRM 51-40-21 AND 51-72-1Oct 6, 2012 · N660FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA201210063572Skin · corrodedUPPER FUSELAGE CROWN BETWEEN FR 78-79, VERTICAL LEADING EDGE PANEL 321AL LANDING HAS 2 AREAS AROUND FASTENER HOLES CORRODED. REMOVED LEVEL ONE CORROSION FROM 2 EA AREAS ON UPPER VERTICAL PANEL 321AL LANDING IAW SRM 51-74-10 PG 202 - 206. FOUND 321AL PANEL Oct 6, 2012 · N660FE · Airbus A300F4605R · Fuselage Main, Plate/SkinSDR FDEA201210043552Shroud · chafedLEFT WING TIP L/E CHAFED AT 2 PLACES AT RIB 29 APPROX. L =1.5" EA. R & R LT WING TIP L/E SHROUD AT RIB 29 IAW FSRM 51-72-10, PG 1-3 AND FSRM 51-40-21 PAR 6. R & R PHENOLIC FILLER IAW FSRM 51-40-21, PAR 5.Oct 4, 2012 · N660FE · Airbus A300F4605R · Wing Miscellaneous StructureSDR FDEA201210023542Seat Track · crackedSEAT TRACK 3R HAS ONE SCREW HOLE CRACKED APPROX. .25 IN. AT LT FLANGE 6" AFT OF FR 56. FOUND IT TO BE OUT OF LIMITS IAW SRM 53-10-16, FIG 101, PG 103. REMOVED DAMAGED SECTION OF 3R SEAT TRACK AT FR 56 TO FR 57. FABRICATED SEAT TRACK IAW SRM 53-10-16 PG 212.Oct 2, 2012 · N660FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201209293516Floor Panel · crackedFLOOR PANEL 231YG HAS A CRACK ON TOP SKIN. FABRICATED REPLACEMENT FLOOR PANEL IAW DWG SRZ 25-005, REV J.Sep 29, 2012 · N660FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201209293514Fitting · crackedANGLE FITTING ON REAR SPAR AND FRAME 47R INBD OF WING RIB 1, FOUND HOLE "H" TO BE CRACKED WHEN ROTO PROBE WAS PERFORMED TO SATISFY AD 2005-23-08. STEP REAMED HOLE "H" FROM .381" TO .436" IAW EO 6-5310-7-3319 B2 PT 3. ROTO PROBED HOLE IAW NTM 57-10-50, PARTSep 29, 2012 · N660FE · Airbus A300B4622R · Fuselage Main, Attach FittingsSDR FDEA201209293510Adapter · damagedMAIN DECK CARGO LT SIDE, CLEVIS ADAPTER AT FRAME 64 BETWEEN SEAT TRACKS 4L AND 5L HAS 1EA. ELONGATED SCALLOP. REMOVED, FABRICATED REPLACEMENT CLEVIS ADAPTER AND INSTALLED AT FR 64 BTWN SEAT TRACKS 4L AND 5L IAW DWG A53278286, ISSUE A AND FSRM 51-72-10, PG 1-3Sep 29, 2012 · N660FE · Airbus A300F4605R · Fuselage Main, StructureSDR FDEA201209283505Floor Support · corrodedFLOOR SUPPORT AT LAV AREA FR 12A TO FR 13 30" TO LEFT OF CENTER HAS EXFOLIATED CORROSION 6 SQUARE INCHES TWO AREAS. R & R FLOOR SUPPORT IAW SRM 51-72-10, PG 2, PARA 6.Sep 28, 2012 · N660FE · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR FDEA201209283506Floor Support · corrodedCOURIER AREA LT SIDE FRAME 13A TO 15, NR 3 BEAM BELOW FLOOR STRUCTURE 40" INBD OF CENTERLINE HAS CORROSION. R & R FLOOR SUPPORT AT Y953, FR 11 L TO FR 15A L IAW FSRM 51-72-10, PARA 6.Sep 28, 2012 · N660FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA201209283502Adapter · damagedMAIN DECK CARGO COMPARTMENT LT SIDE BETWEEN SEAT TRACKS 4L AND 5L CLEVIS ADAPTER HAS 2 GOUGES, BOTH MEASURING 0.500" X 0.060" DEEP. R & R CLEVIS ADAPTER AT FR 31 L IAW FSRM 57-72-10, PARA 5 AND 6.Sep 28, 2012 · N660FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA201209273484Seat Track · damagedMAIN DECK CARGO SEAT TRACK 2R HAS SIX SCREW HOLES GOUGED AND ELONGATED AT RT FLANGE BETWEEN FR 47 TO FR 51. REMOVED AND REPLACED SEAT TRACK IAW SRM 51-72-10. FABRICATED SEAT TRACK IAW DWG A53832211. DRILLED AND LOCATED HOLES ON SEAT TRACK IAW SRM 51-40-44. RSep 27, 2012 · N660FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201209273468Floorboard · damagedMAIN DECK CARGO FLOORBOARD 242ZJ CRUSHED AT UPPER SIDE. FABRICATED REPLACEMENT FLOORBOARD IAW DWG SRZ 25-005, REV J.Sep 27, 2012 · N660FE · Airbus A300F4605R · Fuselage Floor Panel
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