N664FE

Service difficulty reports · 307

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 = 'N664FE' 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 FDEA202602040125Controller · faultedAT FLIGHT LEVEL 370 GOT AN ECAM DUE TO HIGH CABIN PRESSURE, SHORTLY AFTER THAT THE NR 2 PRESSURE REGULATOR FAULTED, DONED OXYGEN MASKS STARTED A DECENT AND RAN THE ECAM. ALL PRESSURE REGULATING VALVES SHOWED CLOSED ON ECAM. THE CABIN PRESSURE CONTINUED TO CLIFeb 4, 2026 · N664FE · Airbus A300F4605R · Cabin Pressure ControllerSDR FDEA202512092225Battery Pack · no testCOURIER COMPARTMENT EXIT DOORS EMERGENCY LIGHTS NOT TESTING. RELEASED FOR SERVICE PER MEL 33-51-05-01. COURIER COMPARTMENT INTERIOR EMERGENCY LIGHTS, DOORS EXIT SIGN INOPERATIVE. NO JUMPSEATERS ALLOWED TO OCCUPY THE COURIER AREA. EMERGENCY LIGHT TEST SDec 9, 2025 · N664FE · Airbus A300F4605R · Emergency LightingSDR FDEA202502260297Spcc · failedFLAPS WOULD NOT RETRACT FROM INITIAL 15/15 POSITION USED ON TAKEOFF. CYCLED FLAP HANDLE AND FLAPS WOULD NOT MOVE - POSSIBLE FLAP OVER SPEED DURING CYCLE OF 1-2 KTS. USED QRH AND LANDED WITH FLAPS 30/40 - FLAPS EXTENDED NORMALLY FOR LANDING. EMERGENCY DECFeb 26, 2025 · N664FE · Airbus A300F4605R · Trailing Edge Flap Control SystemSDR FDEA202412111793Fitting · not reportedREPLACE MAIN DECK CARGO DOOR ACTUATOR BEARING FITTING AT FRAME 24 PER EO NO:E6- 5230-E0378588 A P5 REPLACED MAIN DECK CARGO DOOR ACTUATOR BEARING FITTING AT FRAME 24 PER FEDEX EO NO :E6-5230-E0378588 A P5 , SEQ NO :944 , TITLE :DOORS-CARGO DOOR/HYD SYS - DEDec 11, 2024 · N664FE · Airbus A300F4605R · Cargo/Baggage DoorsSDR FDEA202412111792Fitting · not reportedREPLACE MAIN DECK CARGO DOOR ACTUATOR BEARING FITTING AT FRAME 23 PER EO NO:E6- 5230-E0378588 A P5 REPLACED MAIN DECK CARGO DOOR ACTUATOR BEARING FITTING AT FRAME 23 PER FEDEX E.O NO :E6-5230-E0378588 A P5 , SEQ NO :944 , TITLE :DOORS-CARGO DOOR/HYD SYS - DDec 11, 2024 · N664FE · Airbus A300F4605R · Cargo/Baggage DoorsSDR FDEA202411201704Skin · damaged1EA WATER TRAPPED AREA (60MM*65MM) WAS FOUND AT L/H ELEVATOR TOP SKIN PANEL, ER2 210MM, 730MM FROM T/E. REPAIRED THE DAMAGE AREA WITH CORE AND PLIES AT L/H ELEVATOR TOP SKIN PANEL ER2 210MM, 730MM FROM T/E. I.A.W A300-600F SRM 55-21-12-201, PARA5J PAGE26Nov 20, 2024 · N664FE · Airbus A300F4605R · Elevator, Plate/SkinSDR FDEA202411201703Skin · cracked1EA CRACK (5MM) WAS FOUND AT R/H WING CENTER FLAP RIB27 AFT AREA OF TOP SURFACE RIB FLANGE. PERFORMED CUT OUT DAMAGED FLANGE AND INSTALLED REPAIR ANGLE AT RIB27, S-2.7~S-2.8 AND EXTERNAL PLATE AT RIB26~27,S-2.2~S-2.1 FOR REPAIR I.A.W FEDEX EA NO:T6-5750- Nov 20, 2024 · N664FE · Airbus A300F4605R · Trailing Edge FlapsSDR FDEA202411201702Skin · cracked1EA CRACK (25MM) WAS FOUND AT R/H WING CENTER FLAP RIB26 AFT AREA OF TOP SURFACE RIB FLANGE. PERFORMED CUT OUT DAMAGED FLANGE AND INSTALLED REPAIR ANGLE AT RIB26, S-2.7~S-2.8 AND EXTERNAL PLATE AT RIB26~27,S-2.2~S-2.1 FOR REPAIR I.A.W FEDEX EA NO:T6-5750- Nov 20, 2024 · N664FE · Airbus A300F4605R · Wing, Control SurfacesSDR FDEA202411201701Skin · cracked1EA CRACK (25MM) WAS FOUND AT R/H WING CENTER FLAP RIB18 AFT AREA OF TOP SURFACE RIB FLANGE. PERFORMED CUT OUT DAMAGED FLANGE AND INSTALLED REPAIR ANGLE AT RIB18, S-2.8~REAR SPAR AND EXTERNAL PLATE AT RIB18~19,S-2.1~REAR SPAR FOR REPAIR I.A.W FEDEX EA NO:TNov 20, 2024 · N664FE · Airbus A300F4605R · Trailing Edge FlapsSDR FDEA202411201700Skin · cracked1EA CRACK (25MM) WAS FOUND AT R/H WING CENTER FLAP RIB12 AFT AREA OF TOP SURFACE RIB FLANGE. PERFORMED CUT OUT DAMAGED FLANGE AND INSTALLED REPAIR ANGLE AT RIB12, S-2.7~S-2.8 AND EXTERNAL PLATE AT RIB11~12,S-2.2~REAR SPAR FOR REPAIR I.A.W FEDEX EA NO:T6-57Nov 20, 2024 · N664FE · Airbus A300F4605R · Trailing Edge FlapsSDR FDEA202411201699Skin · cracked2EA CRACKS (20MM) & (20MM) WERE FOUND AT R/H WING CENTER FLAP RIB11 AFT AREA OF TOP SURFACE RIB FLANGE. PERFORMED CUT OUT DAMAGED FLANGE AND INSTALLED REPAIR ANGLE AT RIB11, S-2.7~REAR SPAR AND EXTERNAL PLATE AT RIB11~12,S-2.2~REAR SPAR FOR REPAIR I.A.W FENov 20, 2024 · N664FE · Airbus A300F4605R · Trailing Edge FlapsSDR FDEA202411191684Crossbeam · crackedFLOOR STRUCTURE CROSS BEAM FOUND CRACK AT FR 23, Y-450 9.5" CUT OUT THE DAMAGED AREA AND REWORKED THE REPAIR AREA. THEN INSTALLED REPAIR ANGLE AND FILLER WITH FASTENERS FOR REPAIR. I.A.W A300-600F SRM 53-10-15-201, PARA.15, PAGE.393~400, FIG.212 AND 51-40-Nov 19, 2024 · N664FE · Airbus A300F4605R · Fuselage Main, StructureSDR FDEA202411091755Crossbeam · crackedUNDER M/D FLOOR PNL FOUND A CROSSBEAM CRACK AT FR54.1, Y953~Y1456. FABRICATED A CROSSBEAM AND INSTALLED. LOCATE AT MAIN DECK FLOOR PANEL FR54.1, Y953 ~ Y1456.I.A.W A300-600F SRM 51-72-10-001, PAGE2 AND 51-40-21-001, PARA7, PAGE24~PAGE50 & AIRBUS DWG NO: ANov 9, 2024 · N664FE · Airbus A300F4605R · Fuselage Main, StructureSDR FDEA202411091697Crossbeam · crackedUNDER M/D FLOOR PNL FOUND A CROSSBEAM CRACK AT FR54.1, Y953~Y1456. FABRICATED A CROSSBEAM AND INSTALLED. LOCATE AT MAIN DECK FLOOR PANEL FR54.1 Y953 ~ Y1456. I.A.W A300-600F SRM 51-72-10-001, PAGE.2 AND 51-40-21-001, PARA.7, PAGE.24~PAGE.50 & AIRBUS DWG NNov 9, 2024 · N664FE · Airbus A300F4605R · Fuselage Main, StructureSDR FDEA202411081743Rib · damagedRH WING #7 SPOILER O/B JACK RIB TO BEAM LOWER BORE WAS FOUND IRREGULAR ALUMINIUM REPAIN BUSHING ACCOMPLISHED THE REINFORCEMENT REPAIR AT RH #7 SPOILER OUTBD JACK RIB LOWER BORE. I.A.W FEDEX EA NO:T6-5740-T0381312 P1, SEQ NO:972, TITLE:WINGS-ATTACH FITTINGSNov 8, 2024 · N664FE · Airbus A300F4605R · Wing, Rib/BulkheadSDR FDEA202411081740Rib · damagedRH WING #6 SPOILER O/B JACK RIB TO BEAM UPPER & LOWER BORES WAS FOUND IRREGULAR ALUMINIUM REPAIN BUSHING ACCOMPLISHED THE REINFORCEMENT REPAIR AT RH #6 SPOILER OUTBD JACK RIB UPPER & LOWER BORES. I.A.W FEDEX EA NO:T6-5740-T0381296 P1, SEQ NO:971, TITLE:WINNov 8, 2024 · N664FE · Airbus A300F4605R · Wing, Rib/BulkheadSDR FDEA202411081735Rib · damagedRH WING #6 SPOILER I/B JACK RIB TO BEAM LOWER BORE WAS FOUND IRREGULAR ALUMINIUM REPAIR BUSHING ACCOMPLISHED THE REINFORCEMENT REPAIR AT RH #6 SPOILER INBD JACK RIB LOWER BORE. I.A.W FEDEX EA NO:T6-5740-T0381296 P1, SEQ NO:971, TITLE:WING-ATTACH FITTINGS-RNov 8, 2024 · N664FE · Airbus A300F4605R · Wing, Rib/BulkheadSDR FDEA202411081734Rib · corrodedRH SPOILER #6 INBD JACK RIB UPPER BORE CORRODED ACCOMPLISHED THE REINFORCEMENT REPAIR AT RH #6 SPOILER INBD JACK RIB UPPER BORE. I.A.W FEDEX EA NO:T6-5740-T0381296 P1, SEQ NO:971, TITLE:WING-ATTACH FITTINGS-RH WING #6 SPOILER JACK RIB AT STA SP1X31.675 ANDNov 8, 2024 · N664FE · Airbus A300F4605R · Wing, Rib/BulkheadSDR FDEA202411051742Rib · corrodedRH SPOILER #7 OUTBOARD JACK RIB UPPER BORE CORRODED ACCOMPLISHED THE REINFORCEMENT REPAIR AT RH #7 SPOILER OUTBD JACK RIB UPPER BORE. I.A.W FEDEX EA NO:T6-5740-T0381312 P1, SEQ NO:972, TITLE:WINGS-ATTACH FITTINGS-RH WING #7 SPOILER JACK RIB AT STA SP2X 4Nov 5, 2024 · N664FE · Airbus A300F4605R · Wing, Rib/BulkheadSDR FDEA202411051741Rib · corrodedN00595 LH WING #4 SPOILER O/B JACK RIB TO BEAM UPPER BORE GOT CORROSION ACCOMPLISHED THE REINFORCEMENT REPAIR AT LH #4 SPOILER OUTBD JACK RIB UPPER BORE. I.A.W FEDEX EA NO:T6-5740-T0381294 P1, SEQ NO:968, TITLE:WING-ATTACH FITTINGS-LH WING #4 SPOILER JACK Nov 5, 2024 · N664FE · Airbus A300F4605R · Wing, Attach FittingsSDR FDEA202411051736Rib · corrodedRH SPOILER #6 INBD JACK RIB UPPER BORE CORRODED ACCOMPLISHED THE REINFORCEMENT REPAIR AT RH #6 SPOILER INBD JACK RIB UPPER BORE. I.A.W FEDEX EA NO:T6-5740-T0381296 P1, SEQ NO:971, TITLE:WING-ATTACH FITTINGS-RH WING #6 SPOILER JACK RIB AT STA SP1X31.675 ANDNov 5, 2024 · N664FE · Airbus A300F4605R · Wing, Rib/BulkheadSDR FDEA202411051733Rib · corrodedRH SPOILER #5 OUTBOARD JACK RIB LOWER BORE CORRODED ACCOMPLISHED THE REINFORCEMENT REPAIR AT RH #5 SPOILER OUTBD JACK RIB LOWER BORE. I.A.W FEDEX EA NO:T6-5740-T0381293 P1, SEQ NO:970, TITLE:WING-ATTACH FITTINGS-RH WING #5 SPOILER JACK RIB AT STA ABX184.62Nov 5, 2024 · N664FE · Airbus A300F4605R · Wing, Rib/BulkheadSDR FDEA202411051732Rib · corrodedRH SPOILER #4 INBD JACK RIB UPPER BORE CORRODED ACCOMPLISHED THE REINFORCEMENT REPAIR AT RH #4 SPOILER INBD JACK RIB UPPER BORE. I.A.W FEDEX EA NO:T6-5740-T0381292 P1, SEQ NO:969, TITLE:WING-ATTACH FITTINGS-RH WING #4 SPOILER JACK RIB AT STA ABX103.775-BEANov 5, 2024 · N664FE · Airbus A300F4605R · Wing, Rib/BulkheadSDR FDEA202410311682Seat Track · corrodedMAIN DECK FLOOR STRUCTURE SEAT TRACK FOUND CORROSION NEAR FR15A, Y450 CUT THE FLOOR STRUCTURE AND FABRICATED THE REPAIR ANGLE AND FLOOR SUPPORT. INSTALLED REPAIR PART WITH NEW FASTENERS AT MAIN DECK FLOOR STRUCTURE SEAT TRACK NEAR FR15A, Y450. I.A.W A300-6Oct 31, 2024 · N664FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA202410291681Crossbeam · corrodedBULK CARGO COMPT REPAIR FLOOR BEAM UPPER SURFACE CORRODED AT FR66,-Y1117 POSITION. REPLACED CORRODED BEAM WITH NEW FASTENERS ON BULK CARGO COMPT AT FR66, -Y1117 POSITION. I.A.W A300-600F SRM 51-72-10-001, PAGE.2& 51-40-21-001, PARA.7, PAGE.24~50, THE REPOct 29, 2024 · N664FE · Airbus A300F4605R · Fuselage Main, StructureSDR FDEA202410291650Repair · noneAIRCRAFT REPAIR ASSESSMENT : EXISTING FLUSH DOUBLER REPAIR FOUND ON LH I/B FLAP NOSE SKIN BTW RIB 12~14 COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, TITLE: STRUCTURES - REPAIR CATALOG - A300/A310 REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14Oct 29, 2024 · N664FE · Airbus A300F4605R · Standard Practices/StructuresSDR FDEA202410291635Skin · noneAIRCRAFT REPAIR ASSESSMENT : EXISTING FLUSH DOUBLER REPAIR FOUND ON RH I/B FLAP NOSE SKIN BTW RIB 20D~24B COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, TITLE: STRUCTURES - REPAIR CATALOG - A300/A310 REPAIR IDENTIFICATION & TRACKING REQUIREMENTS Oct 29, 2024 · N664FE · Airbus A300F4605R · Trailing Edge FlapsSDR FDEA202410281790Fitting · damagedSEQ0944, E6-5230-E0378588P5 DOORS - CARGO DOOR/HYD SYS - DETAILED VISUAL INSPECTION OF THE MAIN DECK CARGO DOOR (MDCD) ACTUATOR BEARING FITTINGS AT FRAME 23 AND 24 PERFORMED NEW BEARING FITTING INSTALLATION I.A.W EO: E6-5230-E0378588P5 DOORS - CARGO DOOR/HOct 28, 2024 · N664FE · Airbus A300F4605R · Cargo/Baggage DoorsSDR FDEA202410281789Fitting · damagedCARGO DOOR/HYD SYS - DETAILED VISUAL INSPECTION OF THE MAIN DECK CARGO DOOR (MDCD) ACTUATOR BEARING FITTINGS AT FRAME 23 AND 24 PERFORMED NEW BEARING FITTING INSTALLATION I.A.W EO: E6-5230-E0378588P5 DOORS - CARGO DOOR/HYD SYS - DETAILED VISUAL INSPECTION Oct 28, 2024 · N664FE · Airbus A300F4605R · Cargo/Baggage DoorsSDR FDEA202410281729Skin · damaged1EA WATER TRAPPED AREA (90MM*340MM) WAS FOUND AT R/H ELEVATOR BOTTOM SKIN PANEL T/E AREA, BETWEEN FASTENER NO.10 TO NO.12. *COUNTING T/E FASTENER FROM I/B TO O/B* ACCOMPLSIEHD THE COMPOSITE REPAIR AT RH ELEVATOR LOWER SKIN TRAILING EDGE BETWEEN FASTENER NOOct 28, 2024 · N664FE · Airbus A300F4605R · Elevator, Plate/SkinSDR FDEA202410281728Skin · damaged2EA WATER TRAPPED AREAS (470MM*100MM, 50MM*80MM) WERE FOUND AT R/H ELEVATOR TOP SKIN PANEL T/E AREA, BETWEEN FASTENER NO.9 TO NO.11 *COUNTING T/E FASTENER FROM I/B TO O/B* ACCOMPLSIEHD THE COMPOSITE REPAIR AT RH ELEVATOR TOP SKIN TRAILING EDGE BETWEEN FAOct 28, 2024 · N664FE · Airbus A300F4605R · Elevator, Plate/SkinSDR FDEA202410271618Profile · crackedMAIN DECK FLOOR STRUCTURE FOUND 1EA PROFILE-Z CRACK NEAR FR82, Y1450 REPLACED CRACK PROFILE-Z WITH NEW ONE. I.A.W A300-600F SRM 51-72-10-001, PAGE.2 AND 51- 40-21-001, PARA.6, PAGE.7B-23. THIS REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100 AT MAIN DECK FR82, Y1Oct 27, 2024 · N664FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA202410271617Profile · crackedMAIN DECK FLOOR STRUCTURE FOUND 1 EA PROFILE-Z CRACK NEAR FR82, Y-1450 REPLACED CRACK PROFILE-Z WITH NEW ONE. I.A.W A300-600F SRM 51-72-10-001 PAGE.2 AND 51- 40-21-001, PARA .6, PAGE.7B-23. THIS REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100 AT MAIN DECK FR82 Oct 27, 2024 · N664FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA202410261760Shear Panel · crackedWALL (SHEAR) CRACK AT FWD CARGO COMPT, POSITION FR38, -Y1410, -Z2090 SIDE. REPLACED CRACK WALL WITH NEW ONE. I.A.W A300-600F SRM 51-72-10-001, PAGE2 AND 51-40-21- 001 PARA6 PAGE7B-23.THIS REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.AT FWD CARGO COMPT FR38, -Oct 26, 2024 · N664FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA202410251616Shear Plate · crackedMAIN DECK FLOOR STRUCTURE 1 EA SHEAR PLATE CRACK NEAR FR79 PLUS 3", Y1600 REPLACED CRACK SHEAR PLATE WITH NEW ONE. I.A.W A300-600F SRM 51-72-10-001, PAGE.2 AND 51-40-21-001, PARA.6, PAGE.7B-23. THIS REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. AT MAIN DECK Oct 25, 2024 · N664FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA202410251615Shear Plate · crackedMAIN DECK FLOOR STRUCTURE 1EA SHEAR PLATE CRACK NEAR FR79 PLUS 7", Y-1600 REPLACED CRACK SHEAR PLATE WITH NEW ONE. I.A.W A300-600F SRM 51-72-10-001, PAGE.2 AND 51-40-21-001, PARA.6 PAGE.7B-23. THIS REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. AT MAIN DECK FOct 25, 2024 · N664FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA202410231632Angle · bentAFT CGO COMPT CEILING PLATE DEFORM NEAR LIFT ACTUATOR FWD SIDE AREA. REPLACED THE DAMAGE PLATE WITH NEW ONE. I.A.W A300-600F SRM 51-72-10-001, PAGE.2. LOCATION AT AFT CGO COMPT CEILING NEAR LIFT ACTUATOR FWD SIDE AREA. THIS REPAIR CLASSIFIED AS MINOR PER GOct 23, 2024 · N664FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA202410221589Floor Panel · noneAIRCRAFT REPAIR ASSESSMENT : EXISTING DOUBLER REPAIR FOUND ON BULK CARGO COMPARTMENT FLOOR PANEL 162DF COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, TITLE: STRUCTURES - REPAIR CATALOG - A300/A310 REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 Oct 22, 2024 · N664FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA202410211593Floorbeam · crackedCABIN FLOOR STRUCTURE CROSSBEAM ANGLE FITTING CRACK AT -Y953 ON AVIONICS COMPT. CRACKED ANGLE FITTING REPLACED NEW PART AT AVIONICS COMPT -Y953. INSTALLED WITH RIVETS. I.A.W A300-600F SRM 51-72-10-001, PAGE.2 AND 51-40-21-001, PARA.6, PAGE.7B-23. THIS REPAOct 21, 2024 · N664FE · Airbus A300F4605R · Fuselage Main, Floor BeamSDR HNAA2024100101050Skin · noneEXISTING DOUBLER REPAIR FOUND ON FUSELAGE SKIN BTW FR26~27, S-33R~35R COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 CFR 121.707, INSPECTION OF EXISTING DOUBLER REPAIR ON FUSELAGE SKIN BTW FR26~27Oct 18, 2024 · N664FE · Airbus A300F4605R · Standard Practices/StructuresSDR FDEA202410181595Skin · noneEXISTING DOUBLER REPAIR FOUND ON FUSELAGE SKIN BTW FR26~27, S-33R~35R COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 CFR 121.707, INSPECTION OF EXISTING DOUBLER REPAIR ON FUSELAGE SKIN BTW FR26~27Oct 18, 2024 · N664FE · Airbus A300F4605R · Standard Practices/StructuresSDR FDEA202308081391Bushing · corrodedVERTICAL STABILIZER, #4 RUDDER ATTACH FORK FITTING BUSHINGS (UPPER AND LOWER) HAVE SURFACE CORROSION. 0000490349 : THOMAS, BILLY W - 09-AUG-2023 04:43 REMOVED AND REPLACED BUSHINGS PER AIRBUS CMM 55-40-11 PG.6019 SECT. 2.Aug 8, 2023 · N664FE · Airbus A300* · Rudder StructureSDR FDEA202302240341Valve · failedPDIS 664 21-30 5359 24FEB23 ABQ OPEN U 2 HOURS INTO WHILE USING PRESS REG #1, PRESS REG ONE FAULTED. WE TURNED SYST #1 OFF PER ECAM. THE SYSTEM SWITCHED TO REG #2. PRESS REG #2 FAULTED SHORTLY AFTER. WE DESELECTED #2 PER ECAM. ECAM PRESS PFeb 24, 2023 · N664FE · Airbus A300F4605R · Cabin Pressure Control SystemSDR FDEA202205221269None · noneFR54/54.2 LH NO.4 DUMMY SEAT TRACK SLOT GAP OVER GAP VALUE(A) 0.0393 INCHES(1.0MM) BUT LESS THAN 0.0846 INCHES(2.15MM).SLOT GAP ACTUAL VALUE 1.20MM. I.A.W A300-600 SRM 53-15-16-201 PARA 5A PAGE 201-210 FIG.201 PERFORM RAIL HOLE REPAIR ACCOMPLISHED.May 22, 2022 · N664FE · Airbus A300* · Fuselage Main, StructureSDR FDEA202205201261Seat Track · corrodedCOURIER AREA FLOOR SEAT TRACK GOT CORROSION LOCATION AT FR15A 6" AND Y953 REMOVED CORROSION SEAT TRACK AND INSTALLED NEW SEAT TRACK I.A.W A300-600F SRM 51-72-10-001 PAGE.2 & 51-40-21-001 PARA.6 PAGE.7B-23.May 20, 2022 · N664FE · Airbus A300* · Fuselage Floor PanelSDR FDEA202205141216None · damagedTHE #241RG FLOOR PANEL WAS FOUND INSERT DAMAGED WITH MARK REPLACED THE DAMAGED INSERT WITH NEW INSERT I.A.W A300-600F SRM 51-72-10-001, P.2May 14, 2022 · N664FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA202205141279Floor Panel · damagedTHE #131SG FLOOR PANEL WAS FOUND INSERT DAMAGED REPLACED THE DAMAGED INSERTS WITH NEW INSERTS I.A.W A300-600F SRM 51-72-10-001, P.2 AND FEDEX DRAWING NO: SRZ-25-005.May 14, 2022 · N664FE · Airbus A300* · Fuselage Floor PanelSDR FDEA202205141215Floor Panel · damagedTHE #242NH FLOOR PANEL WAS FOUND INSERT DAMAGED WITH MARK REPLACED THE DAMAGED INSERT WITH NEW INSERT I.A.W A300-600F SRM 51-72-10-001, P.2 AND FEDEX DRAWING NO: SRZ-25-005.May 14, 2022 · N664FE · Airbus A300* · Fuselage Floor PanelSDR FDEA202205141213Floor Panel · damagedTHE #241MF FLOOR PANEL WAS FOUND EDGE DAMAGED WITH MARK ACCOMPLISHED THE FLOOR PANEL REPAIR I.A.W A300-600F SRM 53-10-20-201, PARA.8A, P.201-205, FIG.201May 14, 2022 · N664FE · Airbus A300* · Fuselage Floor PanelSDR FDEA202205081340Hinge Arm · crackedVERTICAL STABILIZER TO RUDDER NO.4 HINGE ARM FOUND LOWER PART CRACK AT LH-FWD AREA (RIB 10). REPLACED THE LOWER HINGE ARM WITH NEW ONE I.A.W EA NO:6-5530-T0368481 P1, SEQ NO:001036, TITLE:STABILIERS-VERTICAL STABILIZER RUDDER HINGE ARM #4 DAMAGE AND REPLMay 8, 2022 · N664FE · Airbus A300* · Vertical Stabilizer
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