# Service difficulty reports: N664FE

A list on [N664FE](https://openairdocs.org/aircraft/N664FE.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Page 1 of 7 · 307 reports

- [SDR FDEA202602040125](https://openairdocs.org/sdr/FDEA202602040125.md): Controller · faulted · Feb 4, 2026 · N664FE · Airbus A300F4605R · Cabin Pressure Controller
  > AT 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 CLI
- [SDR FDEA202512092225](https://openairdocs.org/sdr/FDEA202512092225.md): Battery Pack · no test · Dec 9, 2025 · N664FE · Airbus A300F4605R · Emergency Lighting
  > COURIER 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 S
- [SDR FDEA202502260297](https://openairdocs.org/sdr/FDEA202502260297.md): Spcc · failed · Feb 26, 2025 · N664FE · Airbus A300F4605R · Trailing Edge Flap Control System
  > FLAPS 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 DEC
- [SDR FDEA202412111793](https://openairdocs.org/sdr/FDEA202412111793.md): Fitting · not reported · Dec 11, 2024 · N664FE · Airbus A300F4605R · Cargo/Baggage Doors
  > REPLACE 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 - DE
- [SDR FDEA202412111792](https://openairdocs.org/sdr/FDEA202412111792.md): Fitting · not reported · Dec 11, 2024 · N664FE · Airbus A300F4605R · Cargo/Baggage Doors
  > REPLACE 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 - D
- [SDR FDEA202411201704](https://openairdocs.org/sdr/FDEA202411201704.md): Skin · damaged · Nov 20, 2024 · N664FE · Airbus A300F4605R · Elevator, Plate/Skin
  > 1EA 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 PAGE26
- [SDR FDEA202411201703](https://openairdocs.org/sdr/FDEA202411201703.md): Skin · cracked · Nov 20, 2024 · N664FE · Airbus A300F4605R · Trailing Edge Flaps
  > 1EA 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-
- [SDR FDEA202411201702](https://openairdocs.org/sdr/FDEA202411201702.md): Skin · cracked · Nov 20, 2024 · N664FE · Airbus A300F4605R · Wing, Control Surfaces
  > 1EA 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-
- [SDR FDEA202411201701](https://openairdocs.org/sdr/FDEA202411201701.md): Skin · cracked · Nov 20, 2024 · N664FE · Airbus A300F4605R · Trailing Edge Flaps
  > 1EA 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:T
- [SDR FDEA202411201700](https://openairdocs.org/sdr/FDEA202411201700.md): Skin · cracked · Nov 20, 2024 · N664FE · Airbus A300F4605R · Trailing Edge Flaps
  > 1EA 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:T6-57
- [SDR FDEA202411201699](https://openairdocs.org/sdr/FDEA202411201699.md): Skin · cracked · Nov 20, 2024 · N664FE · Airbus A300F4605R · Trailing Edge Flaps
  > 2EA 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 FE
- [SDR FDEA202411191684](https://openairdocs.org/sdr/FDEA202411191684.md): Crossbeam · cracked · Nov 19, 2024 · N664FE · Airbus A300F4605R · Fuselage Main, Structure
  > FLOOR 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-
- [SDR FDEA202411091755](https://openairdocs.org/sdr/FDEA202411091755.md): Crossbeam · cracked · Nov 9, 2024 · N664FE · Airbus A300F4605R · Fuselage Main, Structure
  > UNDER 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: A
- [SDR FDEA202411091697](https://openairdocs.org/sdr/FDEA202411091697.md): Crossbeam · cracked · Nov 9, 2024 · N664FE · Airbus A300F4605R · Fuselage Main, Structure
  > UNDER 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 N
- [SDR FDEA202411081743](https://openairdocs.org/sdr/FDEA202411081743.md): Rib · damaged · Nov 8, 2024 · N664FE · Airbus A300F4605R · Wing, Rib/Bulkhead
  > RH 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 FITTINGS
- [SDR FDEA202411081740](https://openairdocs.org/sdr/FDEA202411081740.md): Rib · damaged · Nov 8, 2024 · N664FE · Airbus A300F4605R · Wing, Rib/Bulkhead
  > RH 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:WIN
- [SDR FDEA202411081735](https://openairdocs.org/sdr/FDEA202411081735.md): Rib · damaged · Nov 8, 2024 · N664FE · Airbus A300F4605R · Wing, Rib/Bulkhead
  > RH 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-R
- [SDR FDEA202411081734](https://openairdocs.org/sdr/FDEA202411081734.md): Rib · corroded · Nov 8, 2024 · N664FE · Airbus A300F4605R · Wing, Rib/Bulkhead
  > RH 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 AND
- [SDR FDEA202411051742](https://openairdocs.org/sdr/FDEA202411051742.md): Rib · corroded · Nov 5, 2024 · N664FE · Airbus A300F4605R · Wing, Rib/Bulkhead
  > RH 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 4
- [SDR FDEA202411051741](https://openairdocs.org/sdr/FDEA202411051741.md): Rib · corroded · Nov 5, 2024 · N664FE · Airbus A300F4605R · Wing, Attach Fittings
  > N00595 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
- [SDR FDEA202411051736](https://openairdocs.org/sdr/FDEA202411051736.md): Rib · corroded · Nov 5, 2024 · N664FE · Airbus A300F4605R · Wing, Rib/Bulkhead
  > RH 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 AND
- [SDR FDEA202411051733](https://openairdocs.org/sdr/FDEA202411051733.md): Rib · corroded · Nov 5, 2024 · N664FE · Airbus A300F4605R · Wing, Rib/Bulkhead
  > RH 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 ABX184.62
- [SDR FDEA202411051732](https://openairdocs.org/sdr/FDEA202411051732.md): Rib · corroded · Nov 5, 2024 · N664FE · Airbus A300F4605R · Wing, Rib/Bulkhead
  > RH 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-BEA
- [SDR FDEA202410311682](https://openairdocs.org/sdr/FDEA202410311682.md): Seat Track · corroded · Oct 31, 2024 · N664FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach Fittings
  > MAIN 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 A300-6
- [SDR FDEA202410291681](https://openairdocs.org/sdr/FDEA202410291681.md): Crossbeam · corroded · Oct 29, 2024 · N664FE · Airbus A300F4605R · Fuselage Main, Structure
  > BULK 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 REP
- [SDR FDEA202410291650](https://openairdocs.org/sdr/FDEA202410291650.md): Repair · none · Oct 29, 2024 · N664FE · Airbus A300F4605R · Standard Practices/Structures
  > AIRCRAFT 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 14
- [SDR FDEA202410291635](https://openairdocs.org/sdr/FDEA202410291635.md): Skin · none · Oct 29, 2024 · N664FE · Airbus A300F4605R · Trailing Edge Flaps
  > AIRCRAFT 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
- [SDR FDEA202410281790](https://openairdocs.org/sdr/FDEA202410281790.md): Fitting · damaged · Oct 28, 2024 · N664FE · Airbus A300F4605R · Cargo/Baggage Doors
  > SEQ0944, 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/H
- [SDR FDEA202410281789](https://openairdocs.org/sdr/FDEA202410281789.md): Fitting · damaged · Oct 28, 2024 · N664FE · Airbus A300F4605R · Cargo/Baggage 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/HYD SYS - DETAILED VISUAL INSPECTION
- [SDR FDEA202410281729](https://openairdocs.org/sdr/FDEA202410281729.md): Skin · damaged · Oct 28, 2024 · N664FE · Airbus A300F4605R · Elevator, Plate/Skin
  > 1EA 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 NO
- [SDR FDEA202410281728](https://openairdocs.org/sdr/FDEA202410281728.md): Skin · damaged · Oct 28, 2024 · N664FE · Airbus A300F4605R · Elevator, Plate/Skin
  > 2EA 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 FA
- [SDR FDEA202410271618](https://openairdocs.org/sdr/FDEA202410271618.md): Profile · cracked · Oct 27, 2024 · N664FE · Airbus A300F4605R · Fuselage Miscellaneous Structure
  > MAIN 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, Y1
- [SDR FDEA202410271617](https://openairdocs.org/sdr/FDEA202410271617.md): Profile · cracked · Oct 27, 2024 · N664FE · Airbus A300F4605R · Fuselage Miscellaneous Structure
  > MAIN 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
- [SDR FDEA202410261760](https://openairdocs.org/sdr/FDEA202410261760.md): Shear Panel · cracked · Oct 26, 2024 · N664FE · Airbus A300F4605R · Fuselage Miscellaneous Structure
  > WALL (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, -
- [SDR FDEA202410251616](https://openairdocs.org/sdr/FDEA202410251616.md): Shear Plate · cracked · Oct 25, 2024 · N664FE · Airbus A300F4605R · Fuselage Miscellaneous Structure
  > MAIN 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
- [SDR FDEA202410251615](https://openairdocs.org/sdr/FDEA202410251615.md): Shear Plate · cracked · Oct 25, 2024 · N664FE · Airbus A300F4605R · Fuselage Miscellaneous Structure
  > MAIN 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 F
- [SDR FDEA202410231632](https://openairdocs.org/sdr/FDEA202410231632.md): Angle · bent · Oct 23, 2024 · N664FE · Airbus A300F4605R · Fuselage Miscellaneous Structure
  > AFT 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 G
- [SDR FDEA202410221589](https://openairdocs.org/sdr/FDEA202410221589.md): Floor Panel · none · Oct 22, 2024 · N664FE · Airbus A300F4605R · Fuselage Floor Panel
  > AIRCRAFT 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
- [SDR FDEA202410211593](https://openairdocs.org/sdr/FDEA202410211593.md): Floorbeam · cracked · Oct 21, 2024 · N664FE · Airbus A300F4605R · Fuselage Main, Floor Beam
  > CABIN 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 REPA
- [SDR HNAA2024100101050](https://openairdocs.org/sdr/HNAA2024100101050.md): Skin · none · Oct 18, 2024 · N664FE · Airbus A300F4605R · Standard Practices/Structures
  > EXISTING 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 FR26~27
- [SDR FDEA202410181595](https://openairdocs.org/sdr/FDEA202410181595.md): Skin · none · Oct 18, 2024 · N664FE · Airbus A300F4605R · Standard Practices/Structures
  > EXISTING 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 FR26~27
- [SDR FDEA202308081391](https://openairdocs.org/sdr/FDEA202308081391.md): Bushing · corroded · Aug 8, 2023 · N664FE · Airbus A300* · Rudder Structure
  > VERTICAL 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.
- [SDR FDEA202302240341](https://openairdocs.org/sdr/FDEA202302240341.md): Valve · failed · Feb 24, 2023 · N664FE · Airbus A300F4605R · Cabin Pressure Control System
  > PDIS 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 P
- [SDR FDEA202205221269](https://openairdocs.org/sdr/FDEA202205221269.md): None · none · May 22, 2022 · N664FE · Airbus A300* · Fuselage Main, Structure
  > FR54/54.2 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.
- [SDR FDEA202205201261](https://openairdocs.org/sdr/FDEA202205201261.md): Seat Track · corroded · May 20, 2022 · N664FE · Airbus A300* · Fuselage Floor Panel
  > COURIER 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.
- [SDR FDEA202205141216](https://openairdocs.org/sdr/FDEA202205141216.md): None · damaged · May 14, 2022 · N664FE · Airbus A300F4605R · Fuselage Floor Panel
  > THE #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.2
- [SDR FDEA202205141279](https://openairdocs.org/sdr/FDEA202205141279.md): Floor Panel · damaged · May 14, 2022 · N664FE · Airbus A300* · Fuselage Floor Panel
  > THE #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.
- [SDR FDEA202205141215](https://openairdocs.org/sdr/FDEA202205141215.md): Floor Panel · damaged · May 14, 2022 · N664FE · Airbus A300* · Fuselage Floor Panel
  > THE #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.
- [SDR FDEA202205141213](https://openairdocs.org/sdr/FDEA202205141213.md): Floor Panel · damaged · May 14, 2022 · N664FE · Airbus A300* · Fuselage Floor Panel
  > THE #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.201
- [SDR FDEA202205081340](https://openairdocs.org/sdr/FDEA202205081340.md): Hinge Arm · cracked · May 8, 2022 · N664FE · Airbus A300* · Vertical Stabilizer
  > VERTICAL 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 REPL

Next page: https://openairdocs.org/aircraft/N664FE/reports.md?page=2

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
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
```

This list as a web page: https://openairdocs.org/aircraft/N664FE/reports

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.