# Service difficulty reports: N657FE

A list on [N657FE](https://openairdocs.org/aircraft/N657FE.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 4 · 179 reports

- [SDR FDEA202605150598](https://openairdocs.org/sdr/FDEA202605150598.md): Iru · failed · May 15, 2026 · N657FE · Airbus A300F4605R · Integrated Flight System
  > DURING INITIAL TAKEOFF, APPROXIMATELY 60 KIAS, MASTER WARNING CHIME AND IRS 3 FAULT, REJECTED TAKEOFF. RELEASED FOR SERVICE PER MEL: 34-25-01. R & R IRU 3 IAW 34-25-34-04. OPS CHKD NORMAL.
- [SDR FDEA202605090575](https://openairdocs.org/sdr/FDEA202605090575.md): Outflow Valve · faulted · May 9, 2026 · N657FE · Airbus A300F4605R · Pressure Regulator/Outflow Valve
  > EXCESSIVE CABINET ALTITUDE WARNING DURING DECENT PASSING THROUGH 14,000FT. COMPLIED WITH ECAM & EXPEDITED OUR DECENT. BOTH OUTFLOW VALVES SHOWED CLOSED & AMBER AND OUTFLOW VALVE WAS FULLY OPEN.
- [SDR FDEA202605060564](https://openairdocs.org/sdr/FDEA202605060564.md): Smoke Detector · false activation · May 6, 2026 · N657FE · Airbus A300F4605R · Smoke Detection
  > AVIONICS SMOKE CLIMBING THROUGH 13000. SNIFFER FAN REVEALED NO SMOKE. RETUNED MEM. SMOKE WARNING CLEARED APPROACHING BLOCKS, BUT THEN WARNING RETURNED AFTER A MINUTE. UPON SHUTDOWN AND OPENING COCKPIT DOOR WE SMELLED SMOKE IN CABIN. REMOVED AND REPLAC
- [SDR FDEA202602180252](https://openairdocs.org/sdr/FDEA202602180252.md): Shaft · sheared · Feb 18, 2026 · N657FE · Airbus A300F4605R · Escape Slide
  > THE SLIDE L1 RAFT SEPARATION MECHANISM SHAFT SHEARED WHILE ACCOMPLISHING FEA. 6-2560-F0386375 A. PREMATURE REMOVAL/INSTALLATION. REMOVED AND REPLACED L1 ESCAPE SLIDE IAW MM 25-61-21-04. ACFT OK FOR SERVICE.
- [SDR FDEA202602180229](https://openairdocs.org/sdr/FDEA202602180229.md): Safety Wire · wrong part · Feb 18, 2026 · N657FE · Airbus A300F4605R · Escape Slide
  > WHILE PERFORMING INSPECTION E.A. 6-2560-F0386375 REV A, FOUND EJECTOR BAG RELEASE CABLE SAFTIED WITH WRONG WIRE. AMM: 25-61-20-05-01 INSTALLED CORRECT SAFETY WIRE ON R1 DOOR SLIDE EJECTOR BAG CABLE IAW A300MM 25-61-20-05-01. A/C OK FOR SERVICE.
- [SDR FDEA202512052220](https://openairdocs.org/sdr/FDEA202512052220.md): Pin · missing · Dec 5, 2025 · N657FE · Airbus A300F4605R · Escape Slide
  > R1 DOOR SLIDE DEACTIVATION PIN IS MISSING RED FLAG. AMM 52-10-00-03-02 NO MEL OR OIL RELIEF, DUE TO THIS FLAG BEING EMERGENCY EQUIPMENT A/C MAY NOT ENTER INTO SERVICE UNTIL FLAG AND PIN ASSY IS INSTALLED. IAW AMM 52-10-00-03-02 INSTALLED SERVICEABLE PIN
- [SDR FDEA202507311345](https://openairdocs.org/sdr/FDEA202507311345.md): Fitting · not reported · Jul 31, 2025 · N657FE · Airbus A300F4605R · Cargo/Baggage Doors
  > DETAILED VISUAL INSPECTION OF THE MAIN DECK CARGO DOOR ACTUATOR BEARING FITTINGS AT FRAME 23 & 24. COMPLIED WITH EO 6-5230-E0378588 B P5. REPLACED THE MAIN DECK CARGO DOOR ACTUATOR BEARING FITTINGS AT FRAME 23 AND 24. THIS IS CATEGORY B REPAIR. FOLLOW UP INS
- [SDR FDEA202507151200](https://openairdocs.org/sdr/FDEA202507151200.md): Skin · no discrepancy · Jul 15, 2025 · N657FE · Airbus A300F4605R · Standard Practices/Structures
  > EXISTING REPAIR ON RH WING CENTER FLAP LEADING EDGE SKIN BETWEEN RIB13 AND RIB16 REQUIRESEVALUATION FOR CONFORMITY THE EXISTING REPAIR ON RH WINGCENTER FLAP LEADING EDGE SKIN BETWEEN RIB15 AND RIB16 WAS EVALUATION AND FOUND IN CONFORMITY WITH EA 6-5750-T03
- [SDR FDEA202507151193](https://openairdocs.org/sdr/FDEA202507151193.md): Stringer · corroded · Jul 15, 2025 · N657FE · Airbus A300F4605R · Fuselage Main, Longeron/Stringer
  > AFT CARGO COMPARTMENT LOWER STRINGER CORRODED AT FR61 - FR62 S55R REPAIRED THE AFT CARGO COMPARTMENT CORRODED STRINGER AT STGR55RH BETWEEN FR61 AND FR62 PER A300-600F SRM53-10-14-201 PARA.5. THIS IS CATEGORY B REPAIR AND IT MUST BE INSPECTED AT DEFINED INT
- [SDR FDEA202507071127](https://openairdocs.org/sdr/FDEA202507071127.md): Frame · no discrepancy · Jul 7, 2025 · N657FE · Airbus A300F4605R · Fuselage Main, Frame
  > EXISTING REPAIR ON MAIN DECK FRAME 13A BETWEEN STGR20RH AND STGR26RH REQUIRES EVALUATION FOR CONFORMITY. THE EXISTING REPAIR ON MAIN DECK FRAME 13A BETWEEN STGR20RH AND STGR26RH WAS EVALUATED AND FOUND IN CONFORMITY WITH A300-600F SRM53-12-13-201 FIG 201.
- [SDR FDEA202507071129](https://openairdocs.org/sdr/FDEA202507071129.md): Repair · no discrepancy · Jul 7, 2025 · N657FE · Airbus A300F4605R · Standard Practices/Structures
  > MAIN DECK CARGO COMPARTMENT - EXISTING WEB REPAIR BETWEEN FR13A AND FR13B, BETWEEN STRINGER 20RH AND 22RH REQUIRES EVALUATION TO DETERMINE IF MAJOR OR MINOR AND IF THE REPAIR CONFORMS TO FAA APPROVED DATA. THE EXISTING REPAIR ON MAIN DECK CARGO COMPARTMENT
- [SDR FDEA202507061124](https://openairdocs.org/sdr/FDEA202507061124.md): Seat Track · no discrepancy · Jul 6, 2025 · N657FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach Fittings
  > EXISTING REPAIR ON MAIN DECK SEAT TRACK AT Y1456 BETWEEN FR18 AND FR27 REQUIRES EVALUATION FOR CONFORMITY. THE EXISTING REPAIR ON MAIN DECK SEAT TRACK AT Y1456 BETWEEN FR18 AND FR27 WAS EVALUATED AND FOUND IN CONFORMITY WITH DWG: A53781931(ISSUE. H). EO: 6
- [SDR FDEA202507061123](https://openairdocs.org/sdr/FDEA202507061123.md): Repair · no discrepancy · Jul 6, 2025 · N657FE · Airbus A300F4605R · Fuselage Main, Structure
  > EXISTING REPAIR ON MAIN DECK CROSSBEAM AT FR60 BETWEEN Y450 AND Y953 REQUIRES EVALUATION FOR CONFORMITY. THE EXISTING REPAIR ON MAIN DECK CROSSBEAM AT FR60 BETWEEN Y450 AND Y953 WAS EVALUATED AND FOUND IN CONFORMITY WITH A300-600F SRM53-10-15-201 FIG211. E
- [SDR FDEA202507021097](https://openairdocs.org/sdr/FDEA202507021097.md): Frame · cracked · Jul 2, 2025 · N657FE · Airbus A300F4605R · Fuselage Main, Frame
  > CENTER WING BOX - INSPECTION OF REAR SPAR AND BOTTOM PANEL AT JUNCTION WITH FUSELAGE FR47 LH SIDE, FASTENER "F" HOLE FOUND CRACK SIGNAL COMPLIED WITH EA: 6-5710-T0383930 P1. TITLE: WINGS - BASIC WING STRUCTURE - FR47LH REAR SPAR HOLE C AND F CRACK REPAIR -
- [SDR FDEA202507021096](https://openairdocs.org/sdr/FDEA202507021096.md): Frame · cracked · Jul 2, 2025 · N657FE · Airbus A300F4605R · Fuselage Main, Frame
  > MAIN DECK - FUSELAGE FRAME AT FR22 BETWEEN STGR9RH AND STGR10RH DEFORMED REPLACED THE DEFORMED FRAME AND COUPLING AT MAIN DECK FUSELAGE FRAME AT FR22 BETWEEN STGR9RH AND STGR12RH WITH FABRICATED PARTS PER A300-600F SRM51-40-21 AND DWG: A53771694 (ISSUE.B) AN
- [SDR FDEA202507021095](https://openairdocs.org/sdr/FDEA202507021095.md): Frame · cracked · Jul 2, 2025 · N657FE · Airbus A300F4605R · Fuselage Main, Frame
  > CENTER WING BOX - INSPECTION OF REAR SPAR AND BOTTOM PANEL AT JUNCTION WITH FUSELAGE FR47 RH SIDE, FASTENER "C" HOLE FOUND CRACK SIGNAL COMPLIED WITH EA: 6-5710-T0383894 P1. TITLE: WINGS - BASIC WING STRUCTURE - FR47RH REAR SPAR HOLE C CRACK REPAIR - SB A3
- [SDR FDEA202507021094](https://openairdocs.org/sdr/FDEA202507021094.md): Frame · cracked · Jul 2, 2025 · N657FE · Airbus A300F4605R · Fuselage Main, Frame
  > CENTER WING BOX - INSPECTION OF REAR SPAR AND BOTTOM PANEL AT JUNCTION WITH FUSELAGE FR47 LH SIDE, FASTENER "C" HOLE FOUND CRACK SIGNAL COMPLIED WITH EA: 6-5710-T0383930 P1. TITLE: WINGS - BASIC WING STRUCTURE - FR47LH REAR SPAR HOLE C AND F CRACK REPAIR -
- [SDR FDEA202507021093](https://openairdocs.org/sdr/FDEA202507021093.md): Door · cracked · Jul 2, 2025 · N657FE · Airbus A300F4605R · Cargo/Baggage Doors
  > MAIN DECK CARGO DOOR UPR EDGE AT PT1 BETWEEN FR23 AND FR24 FOUND CRACK SIGNAL ON 3EA FASTENER HOLES COMPLIED WITH EA: 6-5230-T0384017 P1. TITLE: DOORS - CARGO DOOR/HYD SYS - CRACKED HOLES ON MAIN DECK CARGO DOOR UPPER LONGERON. REPAIRED THE MAIN DECK CARGO
- [SDR FDEA202506301082](https://openairdocs.org/sdr/FDEA202506301082.md): Stringer · corroded · Jun 30, 2025 · N657FE · Airbus A300F4605R · Fuselage Main, Longeron/Stringer
  > BAY AFT OF FWD CARGO COMPT.- FUSELAGE STRINGER AT STGR44RH BETWEEN FR38.2 AND FR39 FOUND HEAVY CORROSION REPAIRED THE BAY OF FWD CARGO COMPT. CORRODED FUSELAGE STRINGER AT STGR44RH BETWEEN FR38.2 AND FR39 PER SRM 53-10-14-201 FIGURE 208 AND EA 6-5310-T038392
- [SDR FDEA202501070050](https://openairdocs.org/sdr/FDEA202501070050.md): Battery Pack · failed · Jan 7, 2025 · N657FE · Airbus A300F4605R · Service Doors
  > R1 ENTRY DOOR SLIDE NOT SHOWING SLIDE INDICATION ON ECAM WITH LEVER IN THE ARMED POSITION. REMOVED AND REPLACED AUTONOMOUS STANDBY UNIT IAW AMM 52-73-18-04 OPS CHECK FAILED R1 DOOR SLIDE INDICATION STILL DOES NOT SHOW ON ECAM WHEN DOOR IS ARMED. REQUIRES
- [SDR FDEA202501070030](https://openairdocs.org/sdr/FDEA202501070030.md): Control Unit · inoperative · Jan 7, 2025 · N657FE · Airbus A300F4605R · Door Warning System
  > R1 ENTRY DOOR SLIDE NOT SHOWING SLIDE INDICATION ON ECAM WITH LEVER IN THE ARMED POSITION. REMOVED AND REPLACED AUTONOMOUS STANDBY UNIT IAW A300 AMM 52-73-18-04 OPS CHECK FAILED R1 DOOR SLIDE INDICATION STILL DOES NOT SHOW ON ECAM WHEN DOOR IS ARMED. RE
- [SDR FDEA202406070776](https://openairdocs.org/sdr/FDEA202406070776.md): Wire · damaged · Jun 7, 2024 · N657FE · Airbus A300F4605R · Equipment/Furnishings Wiring
  > R1 ESCAPE SLIDE AUDIABLE BUZZER - INOP, LIGHT WORKS. R1 CREW ENTRY DOOR ESCAPE SLIDE WARNING SYSTEM BUZZERS INOP. MEL: 52-73-01-02 C/7398901. TERMINATED WIRE 5273-1083-CF22 AND INSTALLED ON SWITCH 40WN AND RESET BREAKERS 1WN AND 2WN IAW ESPM 20-48-11 A
- [SDR FDEA202404040439](https://openairdocs.org/sdr/FDEA202404040439.md): Pressure Switch · leaking · Apr 4, 2024 · N657FE · Airbus A300F4605R · Hydraulic Indicating System
  > DURING CRUISE AT FL310, GOT AMBER HYD GREEN RSVR LO LEVEL ECAM. COMPLIED WITH ECAM AND QRH PROCEDURES. DIVERTED BACK TO KIND. DECLARED EMERGENCY WITH INDY CENTER. EMERGENCY GEAR EXTENSION SUCCESSFUL. LANDED 23L KIND UNEVENTFULLY. TOWED TO GATE. REMOVED
- [SDR FDEA202304150654](https://openairdocs.org/sdr/FDEA202304150654.md): Unknown · cracked · Apr 15, 2023 · N657FE · Airbus A300* · Window/Windshield System
  > COCKPIT RH 2# WINDOW UPPER RAIL 1EA HOLE CRACKED. PERFORMED THE REPAIR ON THE CRACKED HOLE AT ENTABLATURE AND UPPER RAIL OF RH 2# WINDSHIELD STRUCTURE AS PER FEDEX EA#: 6-5310-T0373929 P1, MAJOR REPAIR IAW GMM 6-2-100.
- [SDR FDEA202304150653](https://openairdocs.org/sdr/FDEA202304150653.md): Unknown · cracked · Apr 15, 2023 · N657FE · Airbus A300* · Window/Windshield System
  > COCKPIT LH 2# WINDOW UPPER RAIL 1EA HOLE CRACKED PERFORMED THE REPAIR ON THE CRACKED HOLE AT ENTABLATURE AND UPPER RAIL OF LH 2# WINDSHIELD STRUCTURE AS PER FEDEX EA#: 6-5310-T0373930 P1, THIS REPAIR CATEGORY B. MAJOR REPAIR IAW GMM 6-2-100.
- [SDR FDEA202304060569](https://openairdocs.org/sdr/FDEA202304060569.md): Spoiler · delaminated · Apr 6, 2023 · N657FE · Airbus A300* · Wing, Control Surfaces
  > RH WING #5 SPOILER CENTER I/B & O/B HINGE ARM LWR SURFACE FOUND DELAMINATION SIZE: (1) 20MM * 25MM, DEPTH: 2.1MM (2) 25MM * 60MM, DEPTH: 2.2MM PERFORMED THE REPAIR ON RH WING #5 SPOILER CENTER I/B & O/B HINGE ARM LWR SURFACE AS PER FEDEX EA: 6-5750-T037383
- [SDR FDEA202212303036](https://openairdocs.org/sdr/FDEA202212303036.md): Detector · failed · Dec 30, 2022 · N657FE · Airbus A300F4605R · Landing Gear Position and Warning
  > HOT BRAKE NR 5 INDICATION BEFORE TAKEOFF. BRAKE FANS WERE APPLIED AND TEMP GOT INTO NORMAL RANGE FOR TAKEOFF. PASSING 13,000 FT ON DEPARTURE, HOT BRAKE INDICATION WITH NR 5 READING 500-600 DEGREES. ELECTED TO AIRBORNE RETURN TO ORD. BRAKES DID RETURN TO NO
- [SDR FDEA202206261565](https://openairdocs.org/sdr/FDEA202206261565.md): None · none · Jun 26, 2022 · N657FE · Airbus A300* · Drag Control System
  > PDIS 657 27-60 4968 26JUN22 LBB OPEN U SPLR & SPD BRK 3 &2 FAULT ON DEP FROM MEM. FOLLOWED ECAM AND QRH PROCEDURES TO TURN SPOILER OFF. WAS UNABLE TO RECOVER SPOILER.
- [SDR FDEA202204060883](https://openairdocs.org/sdr/FDEA202204060883.md): Cylinder · failed · Apr 6, 2022 · N657FE · Airbus A300* · Passenger/Crew Doors
  > MDIS 657 52-10 4758 06APR22 MEM OPEN U R/H CREW ENTRY DOOR CYLINDER DAMPER FOUND TO BE LEAKING...... R/I 16APR22 20:36 MEM REASON CODE: PREMATURE REMOVAL/INSTALLATION
- [SDR FDEA202204060884](https://openairdocs.org/sdr/FDEA202204060884.md): Cylinder · leaking · Apr 6, 2022 · N657FE · Airbus A300* · Passenger/Crew Doors
  > MDIS 657 52-10 4758 06APR22 MEM OPEN U R/H CREW ENTRY DOOR CYLINDER DAMPER FOUND TO BE LEAKING...... MEL 06APR22 18:04 MEM U RELEASED FOR SERVICE PER MEL: 52-11-01-05 CATEGORY: C EXPIRATION: 16APR22 "MEL 52-11-01-05: CREW ENTRY DOOR
- [SDR FDEA202203150517](https://openairdocs.org/sdr/FDEA202203150517.md): Power Supply · failed · Mar 15, 2022 · N657FE · Airbus A300* · Emergency Lighting
  > MDIS 657 33-50 4711 04MAR22 ABE FACT U COURIER AREA EMERGENCY LIGHTS TEST PUSHSWITCH DOES NOT ILLUMINATE DURING TEST. PART 04MAR22 14:03 ABE U IDENTIFIED PARTS (W/KIT)EMG LIGHT P/S W/O MPN: 3214-41 CPN: 3310871 QTY: 1 PART
- [SDR FDEA202108242082](https://openairdocs.org/sdr/FDEA202108242082.md): O-Ring · failed · Aug 24, 2021 · N657FE · Airbus A300F4605R · Hydraulic System, Main
  > DURING CRUISE ECAM INDICATED YELLOW SYSTEM LOW PRESSURE. FOLLOWED ECAM AND QRH AND TURNED OFF PUMP. FLUID STABILIZED SLIGHTLY ABOVE THE RED DOT. DECLARED EMERGENCY WITH APPROACH CONTROL AND LANDED UN EVENTFULLY. FOUND YELLOW SYSTEM NON RETURN CHECK VAL
- [SDR FDEA202105181291](https://openairdocs.org/sdr/FDEA202105181291.md): Transfer Pump · malfunctioned · May 18, 2021 · N657FE · Airbus A300F4605R · Fuel Transfer Valve
  > PDIS 657 28-40 3702 18MAY21 BUR FACT U APPROX 8K ON DECENT RECEIVED TRIM TO AFT XFR NOT AVAIL, SECURED ALL INNER TANKS PER ECAM. SHORTLY THERE AFTER NOTICED FUEL ECAM DISPLAY ONLY INDICATED 1.3K IN RT OUTER, CTR 3.0K, LT OUTER 7.1K. OVERHE
- [SDR FDEA202103110619](https://openairdocs.org/sdr/FDEA202103110619.md): Computer · malfunctioned · Mar 11, 2021 · N657FE · Airbus A300F4605R · Autopilot System
  > ON DEPARTURE FROM KMEM ECAM DISPLAYED PITCH TRIM 2 FAULT, ATS LEVER TRIPPED, F/O LOST HIS FD. PERFORMED ECAM PROC AND COULD NOT RESET PITCH TRIM NR 2 ( NR1 PITCH TRIM ALREADY DEFERRED) OR ATS LEVER. PERFORMED QRH PROC. DECLARED EMERGENCY AND RETURNED TO
- [SDR FDEA202010092759](https://openairdocs.org/sdr/FDEA202010092759.md): Skin · dented · Oct 9, 2020 · N657FE · Airbus A300F4605R · Trailing Edge Flaps
  > AICRAFT DAMAGE DENT ON CENTER FLAP LOCATED TRAILING EDGE BETWEEN TRACK 3 TO TRACK 4 RT WING. PERFORMED PERMANENT REPAIR ON CENTER FLAP LOCATED TRAILING EDGE BETWEEN TRACK 3 TO TRACK 4 RT WING, IAW EA 6-5750-T0357421 (P1). TITLE: RT CENTER FLAP TRAILING EDGE
- [SDR FDEA202010052716](https://openairdocs.org/sdr/FDEA202010052716.md): Floor Panel · delaminated · Oct 5, 2020 · N657FE · Airbus A300F4605R · Fuselage Floor Panel
  > DEBONDED METALIC DOUBLER ON FLOOR PANEL 161GF IN BULK CARGO COMPARTMENT BONDED DOUBLER ON FLOOR PANEL 161GF IN BULK CARGO COMPARTMENT, AS PER EA 6-5317-T0357750 (P1), EA TITTLE: FUSELAGE AFT INTERMEDIATE SECTION-BULK CARGO COMPARTMENT-FLOOR PANELS 161AF AND 16
- [SDR FDEA202010052572](https://openairdocs.org/sdr/FDEA202010052572.md): Floor Panel · cracked · Oct 5, 2020 · N657FE · Airbus A300F4605R · Fuselage Floor Panel
  > BROKEN FLOOR PANEL 251WH IN PASSENGER CABIN (1 EA) MANUFACTURED FLOOR PANEL 251WH IN PASSENGER CABIN, AS PER DRAWING SRZ-25-005 REV R AUG-22-2019. MARKED NEW FLOOR PANEL WITH P/N A30B5327027800200 FX, AS PER GMM 7-0-1001, FOR TRACEABILITY MATERIAL P/0: 2020-
- [SDR FDEA202010052571](https://openairdocs.org/sdr/FDEA202010052571.md): Floor Panel · cracked · Oct 5, 2020 · N657FE · Airbus A300F4605R · Fuselage Floor Panel
  > BROKEN FLOOR PANEL 262AH IN PASSENGER CABIN (1 EA) MANUFACTURED FLOOR PANEL 262AH IN PASSENGER CABIN, AS PER DRAWING SRZ-25-005 REV R AUG 22 2019. MARKED NEW FLOOR PANEL WITH P/N: A30B5327032200300 FX, AS PER GMM 7-0-1001 FOR TRACEABILITY MATERIAL P/O:2020-1
- [SDR FDEA202010052570](https://openairdocs.org/sdr/FDEA202010052570.md): Floor Panel · cracked · Oct 5, 2020 · N657FE · Airbus A300F4605R · Fuselage Floor Panel
  > BROKEN FLOOR PANEL 231FF IN PASSENGER CABIN (1 EA) MANUFACTURED FLOOR PANEL 231FF IN PASSENGER CABIN, AS PER DRAWING SRZ-25-005 REV R AUG-22-2019. MARKED NEW FLOOR PANEL WITH P/N: A30B5327049100000 FX, AS PER GMM 7-0-1001 FOR TRACEABILITY MATERIAL P/O: 2020-
- [SDR FDEA202010052589](https://openairdocs.org/sdr/FDEA202010052589.md): Floor Panel · cracked · Oct 5, 2020 · N657FE · Airbus A300F4605R · Fuselage Floor Panel
  > BROKEN FLOOR PANEL 261KF IN PASSENGER CABIN (1 EA). MANUFACTURED FLOOR PANEL 261KF, AS PER DWG SRZ-25-005 REV R AUG-22-2019. MARKED NEW FLOOR PANEL P/N: FX B5327031600400, AS PER GMM 7-0-1001 FOR TRACEABILITY MATERIAL P/O: 2020-161577/001.
- [SDR FDEA202010052544](https://openairdocs.org/sdr/FDEA202010052544.md): Floor Panel · delaminated · Oct 5, 2020 · N657FE · Airbus A300F4605R · Fuselage Floor Panel
  > DEBONDED METALIC DOUBLER IN FLOOR PANEL 162CF IN BULK CARGO COMPARTMENT. REPLACED FLOOR PANEL 162CF IN BULK CARGO COMPARTMENT, IAW DWG A53279950 ITEM 52 52 SHEET 14 ISSUE C RELEASE DATE AUG-11-1992.
- [SDR FDEA202010052473](https://openairdocs.org/sdr/FDEA202010052473.md): Floor Panel · corroded · Oct 5, 2020 · N657FE · Airbus A300F4605R · Fuselage Floor Panel
  > CORROSION FLOOR PANEL 162DF IN BULK CARGO COMPARTMENT REPLACED ACCESS FLOOR PANEL 162DF IN BULK CARGO COMPARTMENT, DUE TO NOT FOUND ALLOWABLE DAMAGE. REPLACEMENT, IAW SRM A300-600 51-72-10.
- [SDR FDEA202010052472](https://openairdocs.org/sdr/FDEA202010052472.md): Floor Panel · corroded · Oct 5, 2020 · N657FE · Airbus A300F4605R · Fuselage Floor Panel
  > CORROSION FLOOR PANEL 161CF IN BULK CARGO COMPARTMENT REPLACED ACCESS FLOOR PANEL 161CF IN BULK CARGO COMPARTMENT DUE TO NOT FOUND ALLOWABLE DAMAGE. REPLACEMENT IAW SRM A300-600 51-72-10.
- [SDR FDEA202010052471](https://openairdocs.org/sdr/FDEA202010052471.md): Floor Panel · corroded · Oct 5, 2020 · N657FE · Airbus A300F4605R · Fuselage Floor Panel
  > CORROSION ON FLOOR PANEL 161BF IN BULK CARGO COMPARTMENT. REPLACED ACCESS FLOOR PANEL 161BF IN BULK CARGO COMPARTMENT DUE TO NOT FOUND ALLOWABLE DAMAGE. REPLACEMENT IAW A300-600 SRM 51-72-10.
- [SDR FDEA202009292717](https://openairdocs.org/sdr/FDEA202009292717.md): Floor Panel · delaminated · Sep 29, 2020 · N657FE · Airbus A300F4605R · Fuselage Floor Panel
  > DEBONDED FLOOR PANEL 161AF IN BULK CARGO COMPARTMENT BONDED DOUBLER ON FLOOR PANEL 161AF IN BULK CARGO COMPARTMENT, AS PER EA 6- 5317-T0357750 (P1), EA TITTLE: FUSELAGE AFT INTERMEDIATE SECTION-BULK CARGO COMPARTMENT-FLOOR PANELS 161AF AND 161GF-METALLIC DOUB
- [SDR FDEA202009292575](https://openairdocs.org/sdr/FDEA202009292575.md): Floor Panel · cracked · Sep 29, 2020 · N657FE · Airbus A300F4605R · Fuselage Floor Panel
  > BROKEN FLOOR PANEL 162HF IN BULK CARGO COMPARTMENT. MANUFACTURED FLOOR PANEL 162 HF IN BULK CARGO COMPARTMENT, AS PER DRAWING SRZ-25-005 REV R AUG-22-2019. MARKED NEW FLOOR PANEL WITH P/N: A30A5327996200200 FX, AS PER GMM 7-0-1001, FOR TRACEABILITY P/O: 2020
- [SDR FDEA202009282634](https://openairdocs.org/sdr/FDEA202009282634.md): Frame · dented · Sep 28, 2020 · N657FE · Airbus A300F4605R · Fuselage Main, Frame
  > DENT FRAME 23 AT LEVEL STRINGER 13 RT SIDE IN PASSENGER CABIN (MAIN DECK). REPLACED FRAME 23 AT LEVEL STRINGER 13 RT SIDE TO STRINGER 22R, IAW A300-600F SRM 51-40-21 AND DWG A53773275 ISSUE F SHEET 01.
- [SDR FDEA202009282633](https://openairdocs.org/sdr/FDEA202009282633.md): Skin · dented · Sep 28, 2020 · N657FE · Airbus A300F4605R · Fuselage Main, Plate/Skin
  > DENT EXTERNAL SKIN LOCATED FR 14A MORE 4 INCHES AT LEVEL STR 33L AT LOWER FUSELAGE. PERFORMED PERMANENT REPAIR ON EXTERNAL SKIN LOC FR 15 TO FR 15A AND 13" DOWN STR 30L AT LOWER FUSELAGE, IAW EA N: 6-5310-T0357390. P1 EA TITLE: FUSELAGE NOSE SECTION-SKIN PAN
- [SDR FDEA202009282573](https://openairdocs.org/sdr/FDEA202009282573.md): Floor Panel · cracked · Sep 28, 2020 · N657FE · Airbus A300F4605R · Fuselage Floor Panel
  > CRACK FLOOR PANEL 151VF IN AFT CARGO COMPARTMENT. MANUFACTURED FLOOR PANEL 151VF IN AFT CARGO COMPARTMENT, AS PER DRAWING SRZ-25-005 REV R AUG-22-2019. MARKED FLOOR PANEL WITH P/N A30R532B114500000 FX, AS PER GMM 7-0-1001, FOR TRACEABILITY P/O: 2020-16157710
- [SDR FDEA202009282590](https://openairdocs.org/sdr/FDEA202009282590.md): Floor Panel · cracked · Sep 28, 2020 · N657FE · Airbus A300F4605R · Fuselage Floor Panel
  > CRACK FLOOR PANEL 151MF IN AFT CARGO COMPARTMENT. MANUFACTURED FLOOR PANEL 151MF, AS PER DWG SRZ-25-005 REV R AUG-22-2019. MARKED NEW FLOOR PANEL P/N: FX A53279902000, AS PER DWG A53279915 ISSUE B SHEET 1 ITEM 0 AND GMM 7-0-1001 FOR TRACEABILITY MATERIAL P/O

Next page: https://openairdocs.org/aircraft/N657FE/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 = 'N657FE' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N657FE/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.