N657FE

Service difficulty reports · 179

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 = 'N657FE' 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 FDEA202605150598Iru · failedDURING 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.May 15, 2026 · N657FE · Airbus A300F4605R · Integrated Flight SystemSDR FDEA202605090575Outflow Valve · faultedEXCESSIVE 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.May 9, 2026 · N657FE · Airbus A300F4605R · Pressure Regulator/Outflow ValveSDR FDEA202605060564Smoke Detector · false activationAVIONICS 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 REPLACMay 6, 2026 · N657FE · Airbus A300F4605R · Smoke DetectionSDR FDEA202602180252Shaft · shearedTHE 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.Feb 18, 2026 · N657FE · Airbus A300F4605R · Escape SlideSDR FDEA202602180229Safety Wire · wrong partWHILE 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.Feb 18, 2026 · N657FE · Airbus A300F4605R · Escape SlideSDR FDEA202512052220Pin · missingR1 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 Dec 5, 2025 · N657FE · Airbus A300F4605R · Escape SlideSDR FDEA202507311345Fitting · not reportedDETAILED 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 INSJul 31, 2025 · N657FE · Airbus A300F4605R · Cargo/Baggage DoorsSDR FDEA202507151200Skin · no discrepancyEXISTING 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-T03Jul 15, 2025 · N657FE · Airbus A300F4605R · Standard Practices/StructuresSDR FDEA202507151193Stringer · corrodedAFT 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 INTJul 15, 2025 · N657FE · Airbus A300F4605R · Fuselage Main, Longeron/StringerSDR FDEA202507071127Frame · no discrepancyEXISTING 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. Jul 7, 2025 · N657FE · Airbus A300F4605R · Fuselage Main, FrameSDR FDEA202507071129Repair · no discrepancyMAIN 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 COMPARTMENTJul 7, 2025 · N657FE · Airbus A300F4605R · Standard Practices/StructuresSDR FDEA202507061124Seat Track · no discrepancyEXISTING 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: 6Jul 6, 2025 · N657FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA202507061123Repair · no discrepancyEXISTING 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. EJul 6, 2025 · N657FE · Airbus A300F4605R · Fuselage Main, StructureSDR FDEA202507021097Frame · crackedCENTER 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 -Jul 2, 2025 · N657FE · Airbus A300F4605R · Fuselage Main, FrameSDR FDEA202507021096Frame · crackedMAIN 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) ANJul 2, 2025 · N657FE · Airbus A300F4605R · Fuselage Main, FrameSDR FDEA202507021095Frame · crackedCENTER 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 A3Jul 2, 2025 · N657FE · Airbus A300F4605R · Fuselage Main, FrameSDR FDEA202507021094Frame · crackedCENTER 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 -Jul 2, 2025 · N657FE · Airbus A300F4605R · Fuselage Main, FrameSDR FDEA202507021093Door · crackedMAIN 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 CARGOJul 2, 2025 · N657FE · Airbus A300F4605R · Cargo/Baggage DoorsSDR FDEA202506301082Stringer · corrodedBAY 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-T038392Jun 30, 2025 · N657FE · Airbus A300F4605R · Fuselage Main, Longeron/StringerSDR FDEA202501070050Battery Pack · failedR1 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. REQUIRESJan 7, 2025 · N657FE · Airbus A300F4605R · Service DoorsSDR FDEA202501070030Control Unit · inoperativeR1 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. REJan 7, 2025 · N657FE · Airbus A300F4605R · Door Warning SystemSDR FDEA202406070776Wire · damagedR1 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 AJun 7, 2024 · N657FE · Airbus A300F4605R · Equipment/Furnishings WiringSDR FDEA202404040439Pressure Switch · leakingDURING 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. REMOVEDApr 4, 2024 · N657FE · Airbus A300F4605R · Hydraulic Indicating SystemSDR FDEA202304150654Unknown · crackedCOCKPIT 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.Apr 15, 2023 · N657FE · Airbus A300* · Window/Windshield SystemSDR FDEA202304150653Unknown · crackedCOCKPIT 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.Apr 15, 2023 · N657FE · Airbus A300* · Window/Windshield SystemSDR FDEA202304060569Spoiler · delaminatedRH 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-T037383Apr 6, 2023 · N657FE · Airbus A300* · Wing, Control SurfacesSDR FDEA202212303036Detector · failedHOT 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 NODec 30, 2022 · N657FE · Airbus A300F4605R · Landing Gear Position and WarningSDR FDEA202206261565None · nonePDIS 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.Jun 26, 2022 · N657FE · Airbus A300* · Drag Control SystemSDR FDEA202204060883Cylinder · failedMDIS 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 Apr 6, 2022 · N657FE · Airbus A300* · Passenger/Crew DoorsSDR FDEA202204060884Cylinder · leakingMDIS 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 Apr 6, 2022 · N657FE · Airbus A300* · Passenger/Crew DoorsSDR FDEA202203150517Power Supply · failedMDIS 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 Mar 15, 2022 · N657FE · Airbus A300* · Emergency LightingSDR FDEA202108242082O-Ring · failedDURING 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 VALAug 24, 2021 · N657FE · Airbus A300F4605R · Hydraulic System, MainSDR FDEA202105181291Transfer Pump · malfunctionedPDIS 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. OVERHEMay 18, 2021 · N657FE · Airbus A300F4605R · Fuel Transfer ValveSDR FDEA202103110619Computer · malfunctionedON 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 Mar 11, 2021 · N657FE · Airbus A300F4605R · Autopilot SystemSDR FDEA202010092759Skin · dentedAICRAFT 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 EDGEOct 9, 2020 · N657FE · Airbus A300F4605R · Trailing Edge FlapsSDR FDEA202010052716Floor Panel · delaminatedDEBONDED 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 16Oct 5, 2020 · N657FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA202010052572Floor Panel · crackedBROKEN 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-Oct 5, 2020 · N657FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA202010052571Floor Panel · crackedBROKEN 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 :2020-1Oct 5, 2020 · N657FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA202010052570Floor Panel · crackedBROKEN 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-Oct 5, 2020 · N657FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA202010052589Floor Panel · crackedBROKEN 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.Oct 5, 2020 · N657FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA202010052544Floor Panel · delaminatedDEBONDED 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.Oct 5, 2020 · N657FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA202010052473Floor Panel · corrodedCORROSION 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.Oct 5, 2020 · N657FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA202010052472Floor Panel · corrodedCORROSION 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.Oct 5, 2020 · N657FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA202010052471Floor Panel · corrodedCORROSION 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.Oct 5, 2020 · N657FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA202009292717Floor Panel · delaminatedDEBONDED 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 DOUBSep 29, 2020 · N657FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA202009292575Floor Panel · crackedBROKEN 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: 2020Sep 29, 2020 · N657FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA202009282634Frame · dentedDENT 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.Sep 28, 2020 · N657FE · Airbus A300F4605R · Fuselage Main, FrameSDR FDEA202009282633Skin · dentedDENT 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 PANSep 28, 2020 · N657FE · Airbus A300F4605R · Fuselage Main, Plate/SkinSDR FDEA202009282573Floor Panel · crackedCRACK 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: 2020-16157710Sep 28, 2020 · N657FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA202009282590Floor Panel · crackedCRACK 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/OSep 28, 2020 · N657FE · Airbus A300F4605R · Fuselage Floor Panel
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