N665FE

Service difficulty reports · 201

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 = 'N665FE' 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 FDEA201411183748Floor Panel · damagedAFT CARGO FLOOR PANEL151UF DAMAGED. FABRICATED NEW FLOOR PANEL 151UF ON T14 1104476 IAW DWG SRZ 25-005. REPAIR CLASSIFIED AS CAT A MAJOR REPAIR.Nov 18, 2014 · N665FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201411183747Floor Panel · crackedFORWARD CARGO FLOOR PANEL 132PG DAMAGED CRACKED. FABRICATED FLOOR PANEL 132PG ON T14 1104475 IAW DWG SRZ-25-005. REPAIR CLASSIFIED AS A CAT A MAJOR REPAIR.Nov 18, 2014 · N665FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201411183746Floor Panel · damagedAFT CARGO FLOOR PANEL 151VF DAMAGED. FABRICATED NEW FLOOR PANEL 151VF ON T14 1104477 IAW DWG SRZ 25-005. REPAIR CLASSIFIED AS CAT A MAJOR REPAIR.Nov 18, 2014 · N665FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201411094089Case · crackedE & E COMPARTMENT CREW OXYGEN BOTTLE UPPER CARTER HAS CRACK 2 PLACES. PERFORMED WELD REPAIR IAW EA 6-3510-T0313645 PT 1. CREW OXYGEN SYS, CREW BOTTLE CASING ASSEMBLY CRACKED. CLASSIFIED AS MAJOR REPAIR CAT A.Nov 9, 2014 · N665FE · Airbus A300F4605R · Crew Oxygen SystemSDR FDEA201411074077Skin · delaminatedLEFT WING FIXED TE, OTBD OF OTBD FLAP, 2 AREAS OF SKIN SEPARATION, RIVETS POPPED. REPAIRED IAW EA 6-5730-T0313385. CLASSIFIED AS MAJOR CAT A REPAIR.Nov 7, 2014 · N665FE · Airbus A300F4605R · Wing, Plate/SkinSDR FDEA201411073844Floorboard · crackedMDC COMPARTMENT FLOORBOARD BETWEEN FRAME 57.1 - 58, BL 0 & -Y450 IS CRACKED. INSTALLED & SEALED NEW MDC COMPARTMENT FLOORBOARD IAW AMM 53-10-25-04-02, AMM 51-24-00 & SRZ-25-005. FABRICATED FLOOR PANEL ON T14 1104506 IAW DWG SRZ-25-005. CLASSIFIED AS CAT A MNov 7, 2014 · N665FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201411073843Floor Panel · crackedMDC COMPARTMENT FLOORBOARD BETWEEN FRAME 62 - 65, BL -Y1456 & -Y1959 IS CRACKED. FABRICATED FLOOR PANEL 252YG ON T14 1104747 IAW DWG SRZ-25-005. INSTALLED FLOOR PANEL 252YG IAW AMM 53-10-25-04-02. CLASSIFIED AS CAT A MAJOR REPAIR.Nov 7, 2014 · N665FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201411063769Floor Panel · crackedMCD FLOOR PANEL 242QJ IS CRACKED. FABRICATED NEW FLOOR PANEL 242QJ ON T14 1104480 IAW DWG SRZ-25-005. REPAIR CLASSIFIED AS CAT A MAJOR REPAIR.Nov 6, 2014 · N665FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201411063762Floor Panel · damagedMCD FLOOR PANEL 241TH HAS EDGE DAMAGE TO COMPOSITE AROUND ADAPTOR CUT OUT. FABRICATED NEW FLOOR PANEL ON T14 1104478 IAW SRZ-25-005. REPAIR CLASSIFIED AS CAT A MAJOR REPAIR.Nov 6, 2014 · N665FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201411063761Floor Panel · damagedMCD FLOOR PANEL 242ZJ HAS EDGE DAMAGE TO COMPOSITE & INSERTS MISSING. FABRICATED NEW FLOOR PANEL 242ZJ ON T14 1104479 IAW SRZ-25-005 DWG. REPAIR CLASSIFIED AS CAT A MAJOR REPAIR.Nov 6, 2014 · N665FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201411053764Floor Panel · crackedFWD CARGO FLOOR PANEL 131PG DAMAGED. CRACKED FABRICATED NEW FLOOR PANEL 131PG IAW DWG SRZ-25- 005. REPAIR CLASSIFIED AS CAT "A" MAJOR REPAIRNov 5, 2014 · N665FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201411053768Floor Panel · corrodedBULK CARGO COMPARTMENT FLOOR PANEL 161BF TOP SURFACE HAS SEVERAL AREAS OF CORROSION. FABRICATED NEW FLOOR PANEL 161BF ON T14 1104355 IAW DWG SRZ-25-005. REPAIR CLASSIFIED AS CAT A MAJOR REPAIR.Nov 5, 2014 · N665FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201411053766Floor Panel · delaminatedBULK CARGO COMPARTMENT FLOOR PANEL 161GF CORNER DELAMINATED. FABRICATED NEW FLOOR PANEL 161GF ON T14 1104354 & IAW DWG SRZ-25-005. REPAIR CLASSIFIED AS CAT A MAJOR REPAIR.Nov 5, 2014 · N665FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201411053763Floor Panel · crackedFORWARD CARGO FLOOR PANEL 131KG DAMAGED & CRACKED. FABRICATED FLOOR PANEL 131KG ON T14 1104472 IAW DWG SRZ-25-005. REPAIR CLASSIFIED AS CAT A MAJOR REPAIR.Nov 5, 2014 · N665FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201210223704Seat Track · corrodedCENTER MAIN DECK, LEFT SEAT TRACK CORROSION LOCATION AT FR 54 COMMON Y953. REMOVED THE SEAT TRACK AND REPLACED WITH NEW IAW AMM 20-21-12. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.Oct 22, 2012 · N665FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201210053567Floor Panel · damagedCARGO BAY FLOOR PANEL 161JF HAS IMPACT DAMAGE. REMOVED FLOOR PANEL IAW AMM 53-10-29-04. FABRICATED NEW FLOOR PANEL WITH INSERTS AND ADHESIVE IAW SRM 53-10-20 & DRAWING A53279963. INSTALLED FLOOR PANEL IAW AMM 53-10-29-04. PER GMM 6-2-100 REPAIR CLASSIFIED Oct 5, 2012 · N665FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201210053556Floor Panel · damagedFLOOR PANEL EDGE HAS IMPACT DAMAGE. REMOVED FLOOR PANEL. IAW AMM 53-10-29-04. .FABRICATED A NEW FLOOR PANEL WITH INSERTS AND ADHESIVE IAW SRM 53-10-20, & DRAWING A53279978. INSTALLED FLOOR PANEL TO NORMAL CONDITION IAW AMM 53-10-29-04. PER GMM 6-2-100. REOct 5, 2012 · N665FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201210053555Seat Track · corrodedCENTER MAIN DECK LEFT SEAT TRACK CORRODED, BETWEEN FR45 AND FR54 COMMON Y1456. R & R SEAT TRACK IAW SRM 51-72-10 & 51-41-21 & DWG 53810087. REPAIR CLASSIFIED AS MAJOR .Oct 5, 2012 · N665FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201207212632Sense Line · chafedCLIMBING OUT OF 260 TOWARD 330 RECEIVED A FIRE WARNING FOR NR 2 ENGINE ON ECAM. COMPLIED WITH PHASE 1. STILL HAD RED LIGHT. FIRED 1 BOTTLE (AGENT 1). LIGHT WENT OUT. LANDED WITHOUT MISHAP. MX FOUND HP SENSE LINE HAD BEEN RUBBING ON UPPER LOOP RAIL AND WORN HJul 21, 2012 · N665FE · Airbus A300F4605R · Fire DetectionSDR FDEA201205312037Jackscrew · failedFLAPS WOULD NOT RETRACT ON TAKEOFF. HANDLE WAS MOVED TO SLATS POSITION AND FLAP LIGHTS CAME ON. FLAPS MOVED FROM 20 TO 17 AND STUCK. ON APPROACH FLAP HANDLE WAS PLACED TO 20 WITH NO MOVEMENT. THEN HANDLE PLACED TO 40 AND FLAPS MOVED TO 40 FOR LANDING. May 31, 2012 · N665FE · Airbus A300F4605R · Trailing Edge Flap Control SystemSDR FDEA201203030740Controller · malfunctionedAFTER TAKE OFF, FLAPS STUCK AT 15' (SLATS 0' FLAPS') ECAM SHOWED FLAPS SYS 1 & 2 FAULT, FLAPS STUCK, NO SFPI FAULT LIGHT. CYCLED FLAPS TWICE, DID NOT HELP. RETURNED TO DEPARTURE. FOUND RT TORQUE LIMITER SET. RESET TORQUE LIMITER, RAN FLAPS UP. CHECK OF SFCC Mar 3, 2012 · N665FE · Airbus A300F4605R · Trailing Edge Flap Control SystemSDR FDEA201201180245Shutoff Valve · malfunctionedNR 1 ENGINE REVERSER UNLOCKED ON TAKEOFF. ECAM MESSAGE FOR NR1 THRUST REVERSER PRESSURIZED NO THROTTLE RESPONSE ON NR 1 ENGINE, THROTTLE LEVER MOVED FREELY. PERFORMED A GENERAL VISUAL INSPECTION OF THE NR 1 ENG THRUST REVERSER, CDU SWITCH CONNECTORS AND SWITCJan 18, 2012 · N665FE · Airbus A300F4605R · Engine Thrust ReverserSDR FDEA201106182330Valve · failedAFTER TAKEOFF, FLAPS STUCK AT APPROX 18 DURING RETRACTION. CYCLED FLAP HANDLE W/O ANY MOVEMENT. BOTH FLAP SYS FAULTED ON OVERHEAD. SFCC NR1 FAULTED BOX, SFCC NR2 FAULTED POWER. ARRIVING AT THE ACFT, WE FOUND THE SUPPLY PRESSURE SWITCH FAULT LOGGED IN THEJun 18, 2011 · N665FE · Airbus A300F4605R · Trailing Edge Flap Control SystemSDR FDEA201011104298Shim · migratedRT WING T/E NR4 FLAP FRONT CARRIAGE UPPER BRIDGE BOTH SIDE SHIM EXTRUDED IAW EA6-2750-141649, REPAIR ACCOMPLISHED IAW GMM 6-2-100. REPAIR CLASSIFIED AS MINOR.Nov 10, 2010 · N665FE · Airbus A300F4605R · Leading Edge DevicesSDR FDEA201011104296Shim · migratedRT WING NR6 FLAP TRACK FRONT CARRIAGE UPPER BRIDGE INBD SHIM MIGRATED IAW EA6-2750-141649, REPAIR ACCOMPLISHED IAW GMM 6-2-100. REPAIR CLASSIFIED AS MINOR.Nov 10, 2010 · N665FE · Airbus A300F4605R · Trailing Edge FlapsSDR FDEA201011104301Skin · crackedRT WING SPOILER SHROUD SUPPORT SKIN GOT CRACK ABOUT .2500" BELOW NR 5 SPOILER INBD EDGE. FABRICATE NEW PART IAW DWG A-57240194. REPLACE NEW PART IAW SRM 51-72-10, 51-40-21. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.Nov 10, 2010 · N665FE · Airbus A300F4605R · Wing, Plate/SkinSDR FDEA201011104300Frame · crackedLT SIDE FR44 BETWEEN STGR 25 AND STGR 26 HOLE B WAS FOUND CRACK INDICATION OV ER 100 PERCENT FSH. DEPTH OF CRACK INDICATION IS 3MM AT FRAME LAYER. REPLACED WITH NEW FRAME SECTION (PN A5381231020001) IAW AB6F SRM 51-72-10, 51-40-20.Nov 10, 2010 · N665FE · Airbus A300F4605R · Fuselage Main, FrameSDR FDEA201011104299Frame · damagedDURING REMOVING FRAME, FOUND FRAME FOOT 1 EA ENLARGE HOLE LOCATED POSITION B. ENLARGED HOLE AREA, TRIM OUT IAW EO 6-5310-7-5006, PT1, FIG 8.Nov 10, 2010 · N665FE · Airbus A300F4605R · Fuselage Main, FrameSDR FDEA201011104297Rib · crackedLT WING T/E AREA, 1EA RIB CRACKED POSITION UNDER NR5 SPOILER INBD SIDE. FABRICATE NEW PART IAW DWG A-57240194. REPLACE NEW PART IAW SRM 51-72-10 AND 51-40-21. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.Nov 10, 2010 · N665FE · Airbus A300F4605R · Wing, Rib/BulkheadSDR FDEA201011104295Flange · crackedENG 1 RT T/R COWL FWD RING FLANGE GOT CRACK AT UPPER EDGE. ACCOMPLISHED WORK IAW DWG NR:SRZ-78-002. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.Nov 10, 2010 · N665FE · Airbus A300F4605R · Engine Thrust ReverserSDR FDEA201011094293Shim · migratedLT WING NR3 FLAP TRACK FRONT CARRIAGE UPPER BRIDGE SHIM MIGRATED, IAW EA6-2750-141649 REPAIR ACCOMPLISHED. REPAIR CLASSIFIED AS MINOR.Nov 9, 2010 · N665FE · Airbus A300F4605R · Trailing Edge FlapsSDR FDEA201011094292Shim · misalignedLT WING NR4 FLAP TRACK FRONT CARRIAGE UPPER SHIM MIGRATED IAW EA6-2750-141649 REPAIR ACCOMPLISHED. REPAIR CLASSIFIED AS MINOR.Nov 9, 2010 · N665FE · Airbus A300F4605R · Trailing Edge FlapsSDR FDEA201011094291Shim · migratedLT WING NR 6 FLAP TRACK FRONT CARRIAGE UPPER BRIDGE SHIM MIGRATED. EA6-2750-141649 REPAIR ACCOMPLISHED IAW GMM 6-2-100. REPAIR CLASSIFIED AS MINOR.Nov 9, 2010 · N665FE · Airbus A300F4605R · Trailing Edge FlapsSDR FDEA201011094294Rib · crackedLT WING T/E AREA 1EA RIB CRACKED POSITION UNDER NR3 SPOILER INBD SIDE. FABRICATE NEW PART IAW DWG A-57240194. REPLACED NEW PART IAW SRM 51-72-10 AND 51-40-21. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.Nov 9, 2010 · N665FE · Airbus A300F4605R · Wing, Rib/BulkheadSDR FDEA201007082409Position Switch · malfunctionedGEAR HANDLE WOULD NOT RETRACT PAST NEUTRAL SYS 1, MOMENTARY GREEN HYD AIR LOW PRESSURE LIGHT. LANDING GEAR DOWN ECAM, GREEN GEAR DOWN LIGHTS AND RED UNLOCK ON ALL GEAR. LEVELED 3000 AND ACCELERATED TO 200 KTS APPROACHING 200 KTS HANDLE RELEASED AND GEAR REJul 8, 2010 · N665FE · Airbus A300F4605R · Landing Gear Position and WarningSDR FDEA201005211600Unknown · odorSMELLED SMOKE IN COCKPIT DURING FLT, NO ODOR IN JUMPSEAT AREA, SMOKE DISSIPATED AFTER A FEW MINUTES. ALSO PER CREW NO VISIABLE SMOKE. PER JRH RAN NR 1 AND 2 ENGINES WITH ENGINE PACKS ON, NO NOTICABLE ODOR. RAN COCKPIT TEMP TO FULL HOT, PACK ODOR CLEAN. DIDMay 21, 2010 · N665FE · Airbus A300F4605R · Air Distribution SystemSDR FDEA200902220629Shutoff Valve · malfunctionedON TAKEOFF ROLL AT 70 KTS AMBER ECAM "ENG 2 REV PRESSURIZED" W/MASTER CAUTION. REJECTED T/O. RELEASED FOR SERVICE PER MEL/CDL: 78-30-01-A CATEGORY: C EXPIRATION: 04MAR09 "MEL 78-30-01-A: ENGINE (IDENTIFY 1 OR 2) NR 2 THRUST REVERSER INOP. THRUST REVERSER Feb 22, 2009 · N665FE · Airbus A300F4605R · Engine Thrust ReverserSDR 08FDEA02758Light · failedL-1 AND R-1 OVERHEAD EXIT LIGHTS ARE INOP. REPLACED BOTH R-1 AND L-1 EMERGENCY LIGHT ASSEMBLIES. OPS CHECK GOOD IAW FEDEX A300-600 AMM 33-51-13-4. PARTS CANNIBILIZED FROM A/C N674FE.Jul 8, 2008 · N665FE · Airbus A300F4605R · Emergency LightingSDR 08FDEA02757Light · failedL-1 AND R-1 OVERHEAD EXIT LIGHTS ARE INOP. REPLACED BOTH R1 AND L1 EMERGENCY LIGHT ASSEMBLIES. OPS CHECK GOOD IAW FEDEX A300-600 AMM 33-51-13-4. PARTS CANNIBILIZED FROM A/C N674FE.Jul 8, 2008 · N665FE · Airbus A300F4605R · Emergency LightingSDR 08FDEA02413Floor Support · corrodedMDCC FLOOR SUPPORT HAS CORROSION BETWEEN FRAME 13 AND FRAME 13A, LBL 73.66 CM. REMOVED AND REPLACED THE FLOOR SUPPORT IAW A300 SRM 51-40-21, PARA 6.Jun 24, 2008 · N665FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR 08FDEA02412Support · crackedTHE RIGHT WING LOWER SKIN, UPPER SURFACE AFT OF THE REAR SPAR; STRAP IS CRACKED; ACCESS FROM PANEL 675 FB. COMPLIED WITH EA 6-5730-118516.Jun 24, 2008 · N665FE · Airbus A300F4605R · Wing, Attach FittingsSDR 08FDEA02391Seat Track · gougedTHECABIN CROSS SEAT TRACK IS GOUGED AT FRAME 32; LBL 70 INCH. EVALUATED GOUGE; FOUND IT TO BE OUT OF LIMITS IAW FEDEX A300-600 SRM 53-10-16; FIG 101. REMOVED ADAPTER TRACK IAW FEDEX A300-600 SRM 51-40-21. LOCATED AND DRILLED THE NEW ADAPTER P/N A537819362Jun 23, 2008 · N665FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR 08FDEA02390Floor Support · gougedTHE CABIN CROSS S-TRACK IS DAMAGED AT FRAME 31; LBL 70". EVALUATED THE GOUGE; FOUND IT TO BE OUT OF LIMITS IAW FEDEX SRM 53-10-16; FIG 101. REMOVED ADAPTER TRACK IAW FEDEX SRM 51-40-21. LOCATED AND DRILLED THE NEW ADAPTER TRACK IAW FEDEX A300-600 SRM 51-40-Jun 23, 2008 · N665FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR 08FDEA02367Floor Panel · damagedMAIN CABIN FLOOR PANEL 232 YG IS DAMAGED. FABBED A NEW FLOOR PANEL 232 YG BY USING THE OLD PANEL AS A TEMPLATE; POTTED; CURED AND SANDED EDGES; POTTED AND CURED INSERTS; APPLIED NON-SKID TAPE AND PART MARKED PANEL IAW FEDEX DWG SRZ 25-005, REV F.Jun 20, 2008 · N665FE · Airbus A300F4605R · Fuselage Floor PanelSDR 08FDEA02366Floor Panel · damagedMAIN CABIN FLOOR PANEL 232 NG IS DAMAGED. FABBED A NEW FLOOR PANEL 232 NG USING THE OLD PANEL AS A TEMPLATE; POTTED; CURED AND SANDED EDGES; POTTED AND CURED INSERTS; APPLIED NON-SKID TAPE AND PART MARKED PANEL IAW FEDEX DWG SRZ 25-005, REV F.Jun 20, 2008 · N665FE · Airbus A300F4605R · Fuselage Floor PanelSDR 08FDEA02365Floor Panel · damagedMAIN CABIN FLOOR PANEL 251 XG IS DAMAGED. FABBED A NEW PANEL 251 XG BY USING THE OLD PANEL AS A TEMPLATE; POTTED; CURED AND SANDED EDGES; POTTED AND CURED INSERTS; APPLIED NON-SKID TAPE AND PART MARKED PANEL IAW FEDEX DWG SRZ 25-005, REV F.Jun 20, 2008 · N665FE · Airbus A300F4605R · Fuselage Floor PanelSDR 08FDEA02364Floor Panel · damagedMAIN CABIN FLOOR PANEL 251 BH IS DAMAGED. FABBED A NEW FLOOR PANEL 251 BH USING THE OLD PANEL AS A TEMPLATE; POTTED; CURED AND SANDED EDGES; POTTED AND CURED INSERTS; APPLIED NON-SKID TAPE AND PART MARKED PANEL IAW FEDEX DWG SRZ 25-005, REV F.Jun 20, 2008 · N665FE · Airbus A300F4605R · Fuselage Floor PanelSDR 08FDEA02363Floor Panel · damagedMAIN CABIN FLOOR PANEL 251 AH IS DAMAGED. FABBED A NEW FLOOR PANEL 251 AH USING THE OLD PANEL AS A TEMPLATE; POTTED; CURED AND SANDED EDGES; POTTED AND CURED INSERTS; APPLIED NON-SKID TAPE AND PART MARKED PANEL IAW FEDEX DWG SRZ 25-005, REV F.Jun 20, 2008 · N665FE · Airbus A300F4605R · Fuselage Floor PanelSDR 08FDEA02362Floor Panel · damagedMAIN CABIN FLOOR PANEL 232 HG IS DAMAGED. FABBED A NEW FLOOR PANEL 232 HG USING THE OLD PANEL AS A TEMPLATE; POTTED; CURED AND SANDED EDGES; POTTED AND CURED INSERTS; APPLIED NON-SKID TAPE AND PART MARKED THE PANEL IAW FEDEX DWG SRZ 25-005, REV F.Jun 20, 2008 · N665FE · Airbus A300F4605R · Fuselage Floor PanelSDR 08FDEA02361Floor Panel · crackedMAIN CABIN FLOOR PANEL 232 UG IS CRACKED AND DAMAGED. FABBED A NEW FLOOR PANEL 232 UG BY USING THE OLD PANEL AS A TEMPLATE; POTTED; CURED AND SANDED EDGES; POTTED AND CURED INSERTS; APPLIED NON-SKID TAPE AND PART MARKED THE PANEL IAW FEDEX DWG SRZ 25-005, RJun 20, 2008 · N665FE · Airbus A300F4605R · Fuselage Floor Panel
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