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 FDEA201209263464Shear Web · crackedMAIN DECK CARGO LT OTBD SHEAR WEB AT FRAME 38.1-38.2, STRINGER 26 IS CRACKED 1 INCH. R & R IAW SRM 51-40-21, PG 36, PARA 3.Sep 26, 2012 · N660FE · Airbus A300B4622 · Fuselage Miscellaneous StructureSDR FDEA201209263453Floorboard · damagedAFT CARGO BAY FLOORBOARD 151VF HAS 25 SQUARE INCHES OF DAMAGED CORE. FABRICATED REPLACEMENT FLOORBOARD IAW DWG SRZ 25-005, REV J.Sep 26, 2012 · N660FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201209263445Shear Web · crackedMAIN DECK CARGO FRAME 79 OTBD OF SEAT TRACK 5 L, SHEAR WEB IS CRACKED AT THE MOST INBD RADIUS APPROX 2 INCHES LONG. R & R SHEAR WEB IAW SRM 51-40-21 AND REPROTECTED AREA IAW SRM 51-75-10.Sep 26, 2012 · N660FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA201209253439Floor Panel · damagedMAIN DECK CARGO FLOOR PANEL 231VG HAS FOUR AREAS OF IMPACT DAMAGE, FABRICATED REPLACEMENT FLOOR PANEL IAW DWG SRZ 25-005, REV J.Sep 25, 2012 · N660FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201209253436Floor Panel · crackedMAIN DECK CARGO FLOOR PANEL 232CF HAS THREE CRACKS FROM 2-4 INCHES. FABRICATED FLOOR PANEL IAW DWG SRZ 25-005, REV J.Sep 25, 2012 · N660FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201209253430Adapter · gougedMAIN DECK CARGO FLOOR, CLEVIS ADAPTER BETWEEN SEAT TRACK 2R-3R AT FR 61 HAS GOUGE AND ELONGATED SCALLOP. REMOVED CLEVIS ADAPTER IAW SRM 51-72-10, PARA 5. LOCATED, DRILLED, AND INSTALLED NEW CLEVIS ADAPTER IAW SRM 51-72-10, PARA. 6.Sep 25, 2012 · N660FE · Airbus A300F4605R · Fuselage Main, Attach FittingsSDR FDEA201209253429Adapter · gougedMAIN DECK CARGO FLOOR, CLEVIS ADAPTER BETWEEN SEAT TRACK 2R-3R AT FR 62 HAS GOUGE AND ELONGATED AT SCALLOP. REMOVED CLEVIS ADAPTER IAW SRM 51-72-10, PARA 5. LOCATED, DRILLED, AND INSTALLED NEW CLEVIS ADAPTER IAW SRM 51-72-10, PARA 6.Sep 25, 2012 · N660FE · Airbus A300F4605R · Fuselage Main, Attach FittingsSDR FDEA201209243423Floor Panel · delaminatedFLOOR PANEL 147BF DELAMINATED AND BROKEN AROUND THE EDGES. FABRICATED REPLACEMENT FLOOR PANEL IAW DWG SRZ 25-005, REV J.Sep 24, 2012 · N660FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201209243422Floor Panel · delaminatedFLOOR PANEL 147LF DELAMINATED. FABRICATED REPLACEMENT FLOOR PANEL IAW DWG SRZ 25-005, REV J.Sep 24, 2012 · N660FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201209243421Floor Panel · corrodedFLOOR PANEL 161GF HAS CORROSION ON BACK SIDE OF PANEL. FABRICATED FLOOR PANEL IAW DWG SRZ 25-005, REV J AND SRZ 25-011, REV E.Sep 24, 2012 · N660FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201209233406Floor Panel · damagedMAIN DECK CARGO FR 34, FLOOR PANEL 241DF MISSING ONE INSERT. FABRICATED REPLACEMENT FLOOR PANEL IAW DWG SRZ 25-005 REV. J.Sep 23, 2012 · N660FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201209233403Floor Panel · damagedMAIN DECK CARGO FLOOR PANEL 232YG HAS TWELVE SQUARE INCHES OF IMPACT DAMAGE. FABRICATED REPLACEMENT FLOOR PANEL IAW DWG SRZ 25-005 REV. J.Sep 23, 2012 · N660FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201209233399Floorboard · damagedMAIN DECK CARGO FLOORBOARD 252VH CRUSHED AT TWO PLACES UPPER SURFACE AND ONEINSERT MISSING. FABRICATED REPLACEMENT FLOORBOARD IAW DWG SRZ 25-005 REV. J.Sep 23, 2012 · N660FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201209233417Floor Support · crackedRIGHT MAIN DECK CARGO FLOOR SUPPORT BETWEEN FR. 38 AND 38.1 CRACKED 1.5" LONG STRINGER 26-27. R & R FLOOR SUPPORT IAW SRM 51-72-10.Sep 23, 2012 · N660FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA201209233416Floor Support · brokenRT MAIN DECK CARGO FLOOR SUPPORT STRUCTURE STRINGER 26 PROFILE BETWEEN FR 37 AND 38 BROKEN. R & R FLOOR SUPPORT IAW SRM 51-72-10.Sep 23, 2012 · N660FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA201209233415Floor Support · brokenRIGHT MAIN DECK CARGO FLOOR SUPPORT BETWEEN FR 38.1 AND 38.2 BROKEN. R & R FLOOR SUPPORT IAW SRM 51-72-10.Sep 23, 2012 · N660FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA201209223398Floor Panel · damagedMAIN DECK CARGO FLOOR PANEL 252YG CRUSHED AT UPPER SIDE. FABRICATED REPLACEMENT FLOOR PANEL IAW DWG SRZ 25-005, REV J.Sep 22, 2012 · N660FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201209223397Floor Panel · damagedMAIN DECK CARGO FLOOR PANEL 241GF CRUSHED AND INSERT MISSING. FABRICATED REPLACEMENT FLOOR PANEL IAW DWG SRZ 25-005, REV J.Sep 22, 2012 · N660FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201209223396Floor Panel · damagedMAIN DECK CARGO FLOOR PANEL 242QJ CRUSHED AT CLEVIS ADAPTOR CUTOUT. FABRICATED REPLACEMENT FLOOR PANEL IAW DWG SRZ 25-005, REV J.Sep 22, 2012 · N660FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201209213387Floor Panel · damagedMAIN DECK CARGO LT SIDE FLOOR PANEL 251QH CRUSHED AT CLEVIS ADAPTER CUT OUT. FABRICATED REPLACEMENT FLOOR PANEL IAW DWG SRZ 25-005, REV J.Sep 21, 2012 · N660FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201209203364Adapter · damagedLEFT SIDE FR 32 BETWEEN SEAT TRACKS 4L & 5L CLEVIS ADAPTER GOUGED .5"L X .060"D. REMOVED AND REPLACED ADAPTER IAW SRM 51-72-10.Sep 20, 2012 · N660FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA201209203365Adapter · damagedLEFT FR59 BETWEEN SEATS 3L & 4L CLEVIS ADAPTER BROKEN IN HALF. REMOVED AND REPLACED CLS ADAPTER IAW SRM 51-72-10.Sep 20, 2012 · N660FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA201209203370Floorboard · damagedFLOORBOARD 261QF IS BROKEN THROUGH BOTTOM PLY AND HONEYCOMB ACROSS ENTIRE AFT SECTION OF PANEL. FABRICATED REPLACEMENT FLOORBOARD IAW DWG SRZ 25-005, REV J.Sep 20, 2012 · N660FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201209203369Floorboard · damagedAFT CARGO PIT FLOORBOARD 151TF, BROKEN AT PDU CUT OUT ON THE SIDES AND CRUSHED AT 7 PLACES ON THE EDGE AT BOTTOM SIDE. FABRICATED REPLACEMENT FLOORBOARD IAW DWG SRZ 25-005, REV J.Sep 20, 2012 · N660FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201202020427Outflow Valve · failedBOTH CABIN PRESSURE REGULATORS FAILED IMMEDIATELY AFTER TAKE-OFF. ACCOMPLISHED BITE CHECKS OF BOTH CABIN PRESSURE CONTROLLERS IAW TSM 21-30-00, AND FOUND BOTH CONTROLLERS FAULTING THE FWD OUTFLOW VALVE. R & R FWD OUTFLOW VALVE IAW MM 21-31-12-04-0. CHECKS GOFeb 2, 2012 · N660FE · Airbus A300F4605R · Pressure Regulator/Outflow ValveSDR FDEA201012164701Skin · dentedON POST FLIGHT OF ACFT DISCOVERED DENT ON LT SIDE OF ACFT JUST FWD OF NOSE WHEEL AREA. REMOVED DAMAGED AREA BY PERFORMING CUT OUT OF DENT. CUT WAS 3.25 IN LONG X 1.8 IN WIDE. INSTALLED EXTERNAL DOUBLER WITH INTERNAL FILLER IAW SRM 53-12-12, FIG 201, PAGESDec 16, 2010 · N660FE · Airbus A300F4605R · Fuselage Main, Plate/SkinSDR FDEA201012144665Seat Track · corrodedCABIN SEAT TRACK 4 LT HAS CORROSION AT 5 IN AFT OF FR 45. REMOVED LEVEL 1 CORROSION. REMOVED DAMAGED SECTION OF TRACK 4 LT BETWEEN FR 45 TO FR 49 AND INSTALLED SEAT TRACK REPAIR, CTR SECTION FLOORBEAM RAIL SPLICING METHOD IAW SRM 53-10-16, FIG 205, PAGE 231/Dec 14, 2010 · N660FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201012064597Seat Track · wornAFT CARGO FR54 TO 54.2 DUMMY TRACK LT NR2 EXCEEDS MINIMUM GAP VALUE (0.0240) IAW EO6-5310-7-3322B, PART 1, PG 5, STEP 11I. REMOVED DUMMY 2L AFT CARGO FR54 TO 54.2 IAW SRM51-40-21, PAR 5 ROUTED TO BACKSHOP FOR REPAIR. REPAIRED AND REINSTALLED DUMMY TRACK 2L ATDec 6, 2010 · N660FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201012064596Seat Track · wornFWD CARGO FR 38.2 TO 40 DUMMY TRACK LT NR3 EXCEEDS MINIMUM GAP VALUE (0.0235) IAW EO6-5310-7-3322B, PART 1, PG 5, STEP 11I. REMOVED DUMMY TRACK 3L AT FR38.2 TO 40 IAW SRM51-40-21, PAR 5. INSTALLED NEW DUMMY TRACK IAW SRM 51-40-21, PAR 5.Dec 6, 2010 · N660FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201012064595Seat Track · wornAFT CARGO FR54 TO 54.2 DUMMY TRACK LT NR4 EXCEEDS MINIMUM GAP VALUE (0.048) IAW EO6-5310-7-3322B, PART 1, PG5 STEP 11I. REMOVED DUMMY TRACK 4L AFT CARGO FR54 TO 54.2 IAW SRM51-40-21, PAR 7. ROUTED TO BACK SHOP FOR REPAIR. REPAIRED IAW SRM 53-15-16, PGS 203-Dec 6, 2010 · N660FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201012054590Seat Track · wornAFT CARGO FR54 TO 54.2 DUMMY TRACK RT NR2 EXCEEDS MINIMUM GAP VALUE (0.0350) IAW EO6-5310-7- 3322B, PT1, PG5, STEP11I. REMOVED DUMMY TRACK 2R FROM AFT CARGO FR54 TO 54.2 IAW SRM 51-40-21, PAR 7. REMOVED 12EA BRACKETS FROM THE OLD DUMMY TRACK 2R AND INSTALLEDec 5, 2010 · N660FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201012054589Seat Track · corrodedMDCC, SEAT TRACK FLANGE 3R AT FR45 HAS APPROX 12" OF CORROSION. R & R SEAT TRACK 3R BETWEEN FR44 AND FR50 IAW SRM 53-10-16, FIG 203, PG 211/212.Dec 5, 2010 · N660FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201012054588Seat Track · corrodedMDCC SEAT TRACK 5L ALONG FR27 HAS CORROSION APPR .25" INCH ON OTBD FLANGE. REMOVED DAMAGED SEAT TRACK 5L SECTION BETWEEN FR26.5 AND FR 31.5 AND REPAIRED SEAT TRACK 5L IAW FREIGHTER SRM 53-10-16, PB 204, 205, 208, FIG 201.Dec 5, 2010 · N660FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201012054587Seat Track · corrodedMDCC, SEAT TRACK 6R HAS CORROSION BETWEEN FR30 AND FR32, SEAT TRACK 6R AT FR32 HAS A DOUBLE DRILL HOLE. CUT OUT SEAT TRACK FROM FR29 TO FR33, REPAIRED SEAT TRACK IAW SRM 53-10- 16 FIG 208.Dec 5, 2010 · N660FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201012054586Seat Track · corrodedMDCC SEAT TRACK 6L BETWEEN FR22 TO FR 4 HAS APPR 2" SQ INCHES OF EXFOLIATION CORROSION. REPAIRED SEAT TRACK 6L BETWEEN FR22 AND FR24 IAW 300/600 SRM 53-10-16, FIG 101.Dec 5, 2010 · N660FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201012054585Crossbeam · crackedMDC FLOORBEAM AT FRAME 60 HAS 1250" CRACK ON AFT FACE OF VERTICLE ANGLE, BETWEEN SEAT TRACK 4R AND 5R. BLENDED OUT CRACK DAMAGE AND REPAIRED FLOOR BEAM AT FR 60 BETWEEN SEAT TRACKS 4R AND 5R IAW SRM 53-10-15, PB 201, FIG 211.Dec 5, 2010 · N660FE · Airbus A300F4605R · Fuselage Main, StructureSDR FDEA201012054584Skin · crackedRT WING, RIB 9 LWR T/E SKIN PANEL HAS A CRACK APPROX 0.080", NDT VERIFIED CRACK TO BE APPROX .5" INCH LONG. REPAIRED RT WING SKIN IAW WITH DWG NR R57340199 AND EA 6-5730-145507 INSTUCTIONS.Dec 5, 2010 · N660FE · Airbus A300F4605R · Wing, Plate/SkinSDR FDEA201012054583Skin · crackedLT WING, RIB 9, LOWER T/E SKIN HAS APPR 0.80" INCH CRACK FROM FASTENER HOLE TO T/E OF SKIN. REPAIRED IAW DWG R57340199 AND EA 6-5730-145507 INSTRUCTIONS.Dec 5, 2010 · N660FE · Airbus A300F4605R · Wing, Plate/SkinSDR FDEA201012054582Mount · gougedNR1 PYLON FWD ENGINE MOUNT FITTING CTR GUIDE PIN HOLE HAS A GOUGE ON INNER DIAMETER. (SPIGOT GUIDE HOLE). REMOVED NR1 PYLON FWD MOUNT FITTING IAW SRM 51-40-21, PG 7 AND SRM 54-51-81, FIG 1, PG 202. REPAIRED NR1 PYLON FWD MOUNT FITTING (SPIGOT GUIDE HOLE BY Dec 5, 2010 · N660FE · Airbus A300F4605R · Engine Mount SectionSDR FDEA201012054581Skin · damagedAFT CARGO DOOR CUT OUT LOWER FWD EDGE IS DAMAGED APPROX 6 IN LONG AND 0.25 IN WIDE. REPAIRED AFT CARGO DOOR CUT OUT FWD EDGE SKIN IAW SRM 53-17-12, FIG 201, SHEET 1. USING DOUBLER REPAIR SCHEME. COMPLIED WITH EA 6-5310-145512.Dec 5, 2010 · N660FE · Airbus A300F4605R · Fuselage Main, Plate/SkinSDR FDEA201002240505Line · rupturedON TAKE OFF KRDU UPON GEAR RETRACTION GOT ECAM FOR GREEN HYDRAULIC PRESS LOW. OVERHEAD PANEL CONFIRMED THAT ALL GREEN HYD FLUID HAD BEEN LOST. DIVERTED TO GSO. FOUND GREEN SYSTEM RIGHT AILERON PRESSURE FLEX LINE RUPTURED, REPLACED SAME PER AMM 27-14-12-4.Feb 24, 2010 · N660FE · Airbus A300F4605R · Hydraulic System, MainSDR FDEA200906302415Connector · misinstalledENGINE NR 2 REV PRESSURIZED IN FLIGHT IAW QRH REDUCED NR 2 THROTTLE TO IDLE AT 31.4 PERCENT, N1 AND 67.4 PERCENT, N2 WARNING EXTINGUISHED. OPENED NR 2 ENG FAN COWLS. FOUND PRESSURE SWITCH CONNECTOR STILL CONNECTED TO DIRECTIONAL PILOT VALVE PRESSURE SWITCH.Jun 30, 2009 · N660FE · Airbus A300F4605R · Engine Thrust ReverserSDR 08FDEA03855Indication Sys · malfunctionedCLIMBING THROUGH 20,000 FT ECAM INDICATED AUTO FUEL FEED FAULT 2 CTR PUMPS FAULTED. TURNED CTR PUMPS OFF THEN LT OUTER SHOWED XXS OVERHEAD BLANK. RT OUTER TANK QTY DROPPED STEADILY TO 870 LBS THEN SHOWED XXS INNER TANKS THEN STEADILY DROPPED TO BELOW 5000 INSep 12, 2008 · N660FE · Airbus A300F4605R · Fuel Indicating SystemSDR 08FDEA02717Skin · dentedEXTERNAL SURFACE OF MD CARGO DOOR HAS DENT 2" (L) BY 1.2 INCH WIDE BY .060" DEEP. EDGE OF NEAREST RIB TO DEEPEST POINT APROX. .950". LOCATED LONGERON 4, BELOW STR 14 AFT OF FR21. COMPLIED WITH EA6-5230-121322 BY INSTALLING EXTERNAL SKIN REPAIR IAW A300-600 Jul 6, 2008 · N660FE · Airbus A300F4605R · Cargo/Baggage DoorsSDR 08FDEA02708Skin · wornRT WING INBD FLAP LEADING EDGE AND UPPER SURFACE HAS 7 IN BY .250 IN WEAR MARK AT WS 80. REPAIRED RT WING INBD FLAP LEADING EDGE BETWEEN FLAP RIB 18 AND RIB 20D IAW A300-600M SRM 57-50-00, FIG 208.Jul 4, 2008 · N660FE · Airbus A300F4605R · Trailing Edge FlapsSDR 08FDEA02705Skin · dentedRT WING INBD FLAP LOWER SURFACE HAS DENT, APPROX WS 140, DIMENSIONS 4 IN BY 2 IN BY .125 IN DEEP. REPAIRED RT WING INBD FLAP LOWER SURFACE IAW FEDEX EA 6-5750-121297, RELEASE DATE 9 JUNE, 2008.Jul 4, 2008 · N660FE · Airbus A300F4605R · Trailing Edge FlapsSDR 08FDEA02511Floorbeam · crackedTHRU AFT CARGO COMPT CEILING, FR 62 CABIN FLOORBEAM BETWEEN SEAT TRACKS NR 3 RT AND NR 4RT, AFT FACE VERTICLE STIFFENER CRACKED, .250 IN LONG REMOVED CRACK AND INSTALLED CROSSBEAM REPAIR AT CRACKED STIFFENER AT FR 62 FLOORBEAM BETWEEN SEAT TRACK NR 3RT AND NJun 27, 2008 · N660FE · Airbus A300F4605R · Fuselage Main, Floor BeamSDR 08FDEA02485Floorbeam · crackedTHRU FWD CARGO FRAME 31, MDCC FLOORBEAM BETWEEN SEAT TRACK NR 4 LT AND NR 5 LT HAS .250 INCH CRACK REMOVED DAMAGED SECTION AND INSTALLED CROSSBEAM REPAIR AT FR 31 BETWEEN SEAT TRACK NR 4 LT AND NR 5 LT IAW A300-600 SRM 53-10-15, FIG 206.Jun 25, 2008 · N660FE · Airbus A300F4605R · Fuselage Main, Floor BeamSDR 08FDEA02484Seat Track · corrodedMDCC SEAT TRACK NR 2 LT HAS AREA OF CORROSION BETWEEN FR 14A AND FR 17 REMOVED LEVEL 1 CORROSION. REMOVED AND REPLACED SEAT TRACK WITH NEW PART AT TRACK NR 2 LT BETWEEN FR 14A AND FR 17 IAW A300-600 SRM 51-40-21.Jun 25, 2008 · N660FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR 08FDEA02457Seat Track · corrodedMDCC SEAT TRACK NR 3 LT HAS CORROSION BETWEEN FR 15 AND FR 17 REMOVED LEVEL 1 CORROSION. REMOVED AND REPLACED SEAT TRACK WITH NEW PART AT TRACK NR 3 LT BETWEEN FR 15 AND FR 17 IAW A300-600 SRM 51-40-21.Jun 25, 2008 · N660FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach Fittings
Back to N660FE