N721FD

Service difficulty reports · 231

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 = 'N721FD' 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 FDEA202609291451Drain Line · misinstalledDURING THE CLIMB TO FL160 WE NOTICED THE GREEN HYD SYS QITY DECREASING. GREEN HYD SYSTEM CONTINUED TO ZERO ON BOTH ECAM AND OVERHEAD GAUGE. THE BLUE OVER-HEAD HYD SYSTEM QUANTITY INCREASED TO SHOWING OFF SCALE FULL. FOLLOWED ECAM & QRH PROCEDURES INCLUDINGSep 29, 2026 · N721FD · Airbus A300B4622R · Hydraulic System, MainSDR FDEA202609091296Slide · malfunctionedAT BLOCK IN L1 DOOR SLIDE WILL NOT DISARM. MEL 09SEP26 18:17 IND RELEASED FOR SERVICE IAW MEL 52-11-01-01, CATEGORY : C EXPIRATION : 19SEP26 MEL 52-11-01-01: CREW ENTRY DOOR ESCAPE SLIDE L1 - INOP. SLIDE REMAINS INSTALLED ON DOOR. MEL: 52-11-01-01 C/Sep 9, 2026 · N721FD · Airbus A300B4622R · Escape SlideSDR FDEA202602040120Slide · brokenR1 DOOR SLIDE ASSEMBLY HAS BROKEN BATTERY HARD SHELL. RELEASED FOR SERVICE PER MEL: 52-11-01-01, CATEGORY: C. R1 DOOR ESCAPE SLIDE INOP. SLIDE REMAINS INSTALLED ON DOOR. REMOVED AND REPLACED R1 DOOR SLIDE IAW AMM 25-61-22-04-01. OPS CHECKS GOODFeb 4, 2026 · N721FD · Airbus A300B4622R · Escape SlideSDR FDEA202602020137Slide Raft · inoperativeSMIS 721 25-60 MOD TYPE F MOD NO. 6-2560-F0386261 REV NO. PS P1 EQUIPMENT AND FURNISHINGS - EMERGENCY EVACUATION EQU IPMENT - VERIFICATION OF SAFETY WIRE MATERIAL ON SLIDE PACK BOARD RELEASE CABLE. :CPN 2513882 MPN D30546- 509 L1/R1 DOOR SLIDE. COMPLIED Feb 2, 2026 · N721FD · Airbus A300B4622R · Escape SlideSDR FDEA202511132170Door · faultedL1 DOOR WILL NOT DISARM. REVERSED MEL 52-11-01-01. FOUND WITH LOWER COVER REMOVED DOOR DISARMS AND ARMS NORMALLY. REINSTALLED LOWER COVER AND DOOR CONTINUES TO OPERATE NORMALLY. LOWER COVER WAS DAMAGED AND PLACED ON OIL REF WRI 52-10/5586.Nov 13, 2025 · N721FD · Airbus A300B4622R · Passenger/Crew DoorsSDR FDEA202511132169Slide · dislodgedLEFT FORWARD ENTRY DOOR WILL NOT DISARM. THE LEVER WILL NOT MOVE ALL THE WAY TO THE DISARM POSITION. MEL: 52-11-01-02 ESCAPE SLIDE CAME LOOSE FROM L1 DOOR, ESCAPE SLIDE REMOVED FROM DOOR, BUT REMAINS ONBOARD IN HAZMAT CONTAINER.Nov 13, 2025 · N721FD · Airbus A300B4622R · Escape SlideSDR FDEA202511132168Slide · faultedLEFT FORWARD ENTRY DOOR WILL NOT DISARM. THE LEVER WILL NOT MOVE ALL THE WAY TO THE DISARM POSITION. THIS ITEM WAS ON MEL 52-11-01-01. THE ESCAPE SLIDE HAS COME LOOSE FROM THE STORE, TRANSFERRING WRI 52-10/5579 TO THIS WRI AND PLACING ITEM ON MEL 52-11-Nov 13, 2025 · N721FD · Airbus A300B4622R · Passenger/Crew DoorsSDR FDEA202506060848O-Ring · failedDURING DESCENT THROUGH FL200 ECAM INDICATED LOSS OF GREEN HYDRAULIC QUANTITY BELOW RED DOT. HYD RESV LOW. COMPLIED WITH ECAM AND QRH. PERFORMED MANUAL GEAR EXTENSION AND LANDED WITH NO FURTHER ISSUES. AFTER THE GEAR WAS EXTENDED GREEN HYDRAULIC SYSTEM RJun 6, 2025 · N721FD · Airbus A300B4622R · Hydraulic System, MainSDR FDEA202502010199Rib · crackedRH WING CENTER FLAP PERFORM EA NO.:6-5750-T0381883 P1 STEP 4.A. DVI FOUND RIB 27 FLANGE CRACK BETWEEN STRINGER 2.7 AND REAR SPAR AREA. PERFORMED CUT OUT DAMAGED FLANGES AND INSTALLED REPAIR ANGLES AT RH WING CENTER FLAP RIB27, S-2.7~REAR SPAR AND EXTERNAFeb 1, 2025 · N721FD · Airbus A300B4622R · Trailing Edge FlapsSDR FDEA202501210207Stringer Splice · wornSPLICE HOLE ELONGATION AT FR54 STGR 44RH SIDE. REPLACED THE DAMAGED SPLICE WITH NEW FABRICATED SPLICE AT LOWER FUSELAGE FR54, S- 44R. I.A.W A300-600 SRM 51-72-10-001, PAGE.2& AIRBUS DWG NO:A53812405, REV.C00& FEDEX GMM 07-0-1001. THIS REPAIR IS CLASSIFIED AJan 21, 2025 · N721FD · Airbus A300B4622R · Fuselage Main, Longeron/StringerSDR FDEA202501200239Fitting · not reportedREPLACE MAIN DECK CARGO DOOR ACTUATOR BEARING FITTING AT FRAME 24 PER EO NO: E6- 5230-E0378588 B P5 REPLACED MAIN DECK CARGO DOOR ACTUATOR BEARING FITTING AT FRAME 24, LONGN1~3. I.A.W FEDEX EO NO: E6-5230-E0378588 B P5, SEQ NO:981, TITLE: DOORS-CARGO DOOR/HJan 20, 2025 · N721FD · Airbus A300B4622R · Fuselage Structure (General)SDR FDEA202501200238Fitting · not reportedREPLACE MAIN DECK CARGO DOOR ACTUATOR BEARING FITTING AT FRAME 23 PER EO NO: E6- 5230-E0378588 B P5 REPLACED MAIN DECK CARGO DOOR ACTUATOR BEARING FITTING AT FRAME 23, LONGN1~3. I.A.W FEDEX EO NO: E6-5230-E0378588 B P5, SEQ NO:981, TITLE: DOORS-CARGO DOOR/HJan 20, 2025 · N721FD · Airbus A300B4622R · Fuselage, Landing Gear Attach FittingsSDR FDEA202501190220Rib · gougedTHE UPPER BORE GOUGE ON OUTBD JACK RIB OF R6 SPLR. ACCOMPLISHED THE REINFORCEMENT REPAIR AT R6 SPOILER OUTBD JACK RIB UPPER BORE I.A.W FEDEX EA NO:T6-5740-T0382066 P1, SEQ NO:1014, TITLE:WINGS-ATTACH FITTINGS-RH WING #6 SPOILER JACK RIB AT STA SP1X31.675 AJan 19, 2025 · N721FD · Airbus A300B4622R · Wing, Rib/BulkheadSDR FDEA202501190219Rib · gougedTHE UPPER BORE GOUGE ON INBD JACK RIB OF R6 SPLR. ACCOMPLISHED THE REINFORCEMENT REPAIR AT R6 SPOILER INBD JACK RIB UPPER BORE I.A.W FEDEX EA NO:T6-5740-T0382066 P1, SEQ NO:1014, TITLE:WINGS-ATTACH FITTINGS-RH WING #6 SPOILER JACK RIB AT STA SP1X31.675 ANDJan 19, 2025 · N721FD · Airbus A300B4622R · Wing, Rib/BulkheadSDR FDEA202501190218Rib · gougedTHE LWR BORE GOUGE ON OUTBD JACK RIB OF R4 SPLR. ACCOMPLISHED THE REINFORCEMENT REPAIR AT R4 SPOILER OUTBD JACK RIB LWR BORE I.A.W FEDEX EA NO:T6-5740-T0382065 P1, SEQ NO:1013, TITLE:WING-ATTACH FITTINGS-RH WING #4 SPOILER JACK RIB AT STA ABX112.525-BEAM AJan 19, 2025 · N721FD · Airbus A300B4622R · Wing, Rib/BulkheadSDR FDEA202501170198Rib · cracked1EA CRACK (15MM) 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 RH WING CENTER FLAP RIB26, S-2.8~REAR SPAR AND EXTERNAL PLATE AT RIB26~27,S-2.2~REAR SPAR FOR REPAIRJan 17, 2025 · N721FD · Airbus A300B4622R · Trailing Edge FlapsSDR FDEA202501170166Stringer · deformedTAIL STRUCTURAL FOUND S-36R STRAP DEFORM AT FR86 PLUS 10" AREA. REPLACED THE DAMAGE SECTION-L WITH NEW AT TAIL STRUCTURAL FR 86 PLUS 10" S-36R AREA I.A.W A300-600 SRM 51-72-10-001, PAGE 2. THIS REPAIR CLASSIFIED AS MINOR PER GMM 06-2-100.Jan 17, 2025 · N721FD · Airbus A300B4622R · Fuselage Main, Longeron/StringerSDR FDEA202501160196Seat Track · wornMAIN DECK CARGO COMPARTMENT WAS FOUND SEAT TRACK CROWN WORN AT FR58 PLUS 1", - Y1959 CUT THE DAMAGED SEAT TRACK, FABRICATED THE NEW REPAIR SEAT TRACK AND WET INSTALLED REPAIR PARTS WITH FASTENERS I.A.W A300-600 SRM 53-10-16-201, PARA 10, FIG 208, PAGE 243Jan 16, 2025 · N721FD · Airbus A300B4622R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA202501160188Angle · crackedRA COAXIAL CABLE SUPPORT BRACKET CRACK AT FR58~59, STGR 44RH SIDE. REPLACED THE CRACKED RA COAXIAL CABLE SUPPORT BRACKET, AT FR58~59, STGR 44RH SIDE. I.A.W A300-600 SRM 51-72-10-001, PAGE 2. THIS REPAIR IS CLASSIFIED AS MINOR. PER GMM 6-2- 100.Jan 16, 2025 · N721FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR FDEA202501160187Angle · crackedRA COAXIAL CABLE SUPPORT BRACKET CRACK AT FR64, STGR 50RH~51RH REPLACED THE CRACKED RA COAXIAL CABLE SUPPORT BRACKET, AT FR64, STGR 50RH~51RH. I.A.W A300-600 SRM 51-72-10-001, PAGE 2. THIS REPAIR IS CLASSIFIED AS MINOR, PER GMM 6-2-100Jan 16, 2025 · N721FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR FDEA202501160184Angle · damagedMAIN DECK CARGO COMPARTMENT AFT PRESSURE BULKHEAD RH LOWER AREA WAS FOUND 1EA SUPPORT ANGLE BROKEN AS MARKED,FR80/82 REPLACED THE BROKEN SUPPORT ANGLE, AT MAIN DECK CARGO COMPARTMENT AFT PRESSURE BULKHEAD RH LOWER AREA FR80/FR82. I.A.W A300-600 SRM 51-72-1Jan 16, 2025 · N721FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR FDEA202501150192Skin · damaged2EA WATER TRAPPED AREAS WERE FOUND AT LH RUDDER T/E SCREW LINE NO.19(30MM*40MM) FASTENER AND RH RUDDER T/E SCREW LINE NO.39(20MM*80MM) FASTENER. ACCOMPLISHED THE COMPOSITE REPAIR AT LH SKIN SCREW LINE #19 AND RH SKIN SCREW LINE #39 OF RUDDER I.A.W A300-600Jan 15, 2025 · N721FD · Airbus A300B4622R · Rudder, Plate/SkinSDR FDEA202501140195Skin · damaged1EA WATER TRAPPED AREA(80MM*80MM) WAS FOUND AT RH ELEVATOR LOWER SKIN PANEL T/E FASTENER NO.9. *COUNTING FASTENER FROM I/B TO O/B * ACCOMPLISHED THE COMPOSITE REPAIR AT RH ELEVATOR LOWER SKIN T/E FASTENER #9 I.A.W A300-600 SRM 55-21-12-201, PARA.5B, PAGE.2Jan 14, 2025 · N721FD · Airbus A300B4622R · Elevator, Plate/SkinSDR FDEA202501140194Skin · damaged2EA WATER TRAPPED AREAS(100MM*130MM ,70MM*150MM) WERE FOUND AT LH ELEVATOR LOWER SKIN PANEL T/E FASTENER NO.18 AND NO.24. *COUNTING FASTENER FROM I/B TO O/B * ACCOMPLISHED THE COMPOSITE REPAIRS AT LH ELEVATOR LOWER SKIN T/E FASTENERS #18 AND #24 I.A.W A300Jan 14, 2025 · N721FD · Airbus A300B4622R · Elevator, Plate/SkinSDR FDEA202501130197Plate · crackedSIDE PLATE CRACK AT FWD CARGO COMPT FRAME 20 TO 21, Y1420 LH UNDER FLOOR POSITION. REPLACED THE CRACK WALL WITH NEW PART AT FWD CARGO COMPARTMENT BETWEEN FR20 TO FR21, Y1420 I.A.W A300-600 SRM 51-72-10-001, PAGE.2 AND 51-40-21-001, PARA.6, PAGE.7B~23. THIS Jan 13, 2025 · N721FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR FDEA202501130186Profile · crackedMAIN DECK FLOOR STRUCTURE WAS FOUND PROFILE-Z CRACK AT FR80/82,Y1447 REPLACED THE DAMAGED PART WITH NEW ONE AND INSTALLED WITH FASTENERS. I.A.W A300-600 SRM 51-72-10-001, PAGE 2 AND SRM 51-40-21-001, PARA 6, PAGE 7B~PAGE23. THIS REPAIR IS CATEGORY A AND CLJan 13, 2025 · N721FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR FDEA202501130185Floor Support · crackedMAIN DECK FLOOR STRUCTURE WAS FOUND PROFILE-Z CARCK AT FR80/82,-Y1447 REPLACED DAMAGE PROFILE-Z WITH NEW ONE AT MAIN DECK FLOOR STRUCTURE FR80/82, - Y1447. I.A.W A300-600 SRM 51-40-21-001, PARA 6 PAGE 7B - PAGE 23 & 51-72-10-001, PAGE 2. THIS REPAIR IS CLASJan 13, 2025 · N721FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR FDEA202501130183Shear Plate · crackedMAIN DECK FLOOR STRUCTURE WAS FOUND PLATE SHEAR CRACK AT FR79 PLUS 4", S-26L REPLACED THE DAMAGE PART WITH NEW ONE AND INSTALLED WITH FASTENERS. I.A.W A300-600 SRM 51-72-10-001, PAGE 2 AND SRM 51-40-21-001, PARA 7, PAGE 24~50. THIS REPAIR IS CATEGORY A ANDJan 13, 2025 · N721FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR FDEA202401050039Indicator · failedENGINE FIRE AND MULTIPLE SYSTEMS WARNINGS AND CAUTIONS AFTER ROTATION IN LIGHT RAIN. ENGINE TEMPERATURE INDICATIONS WERE NORMAL AUTOPILOT AUTOMATION WAS NOT AVAILABLE. EMERGENCY DECLARED. INDICATOR WERE ALL REPLACED AND ALL OPS CHECKS BEING SATISFACTORY. Jan 5, 2024 · N721FD · Airbus A300* · Fire DetectionSDR FDEA202312301967Control Box · failedAFTER TAKEOFF, AT GEAR RETRACT, COULDN`T RAISE MLG PAST NEUTRAL IN SYS #1, SWITCHED TO SYS #2, GEAR RETRACTED NORMAL, SEVERAL SYS FAULTED IMMEDIATELY. CABIN PRESSURE REGULATOR #1, BOTH ENGINE PER MODES FAULTED, ATS 1&2 FAULTED, PITCH TRIM #1 FAULTED, ALL PRODec 30, 2023 · N721FD · Airbus A300B4622R · Landing Gear Position and WarningSDR FDEA202210132565Proximity Sensor · failedAFTER TAKEOFF KMEM 18R. GEAR WOULD NOT RETRACT. HANDLE CAME UP. BUT AFTER DELAY ECAM DISPLAY OF GEAR WOULD NOT RETRACT. FOLLOWED ECAM AND QRH. RETURNED TO KMEM 18C. LANDING UNEVENTFUL REPLACED 64GB PROX SENSOR REF AMM 32-00-00-04. OPS CHECK GOOD. PERFOct 13, 2022 · N721FD · Airbus A300B4622R · Main Landing GearSDR FDEA202206301675Floor Panel · damagedMAIN DECK CARGO COMPT #242QH FLOOR PANEL WAS FOUND 2 EA INSERTS DAMAGED. REPLACED THE DAMAGED INSERTS WITH NEW PARTS I.A.W FEDEX DRAWING NO:SRZ-25-005Jun 30, 2022 · N721FD · Airbus A300* · Fuselage Floor PanelSDR FDEA202206301674Floor Panel · damagedAFT CARGO COMPT #151LF FLOOR PANEL WAS FOUND INSERTS DAMAGED. REPLACED THE DAMAGED INSERTS WITH NEW PARTS I.A.W FEDEX DRAWING NO:SRZ-25-005Jun 30, 2022 · N721FD · Airbus A300* · Fuselage Floor PanelSDR FDEA202206301748None · unknownAIRCRAFT REPAIR ASSESSMENT:EXISTING EXTERNAL DOUBLER REPAIR FOUND ON #1 PYLON O/B SIDE, AT RIB 8 POSITION. COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, TITLE: A300/A310 RPR IDENT&SUPPLEMENTAL MX REQ(SMR) TRK, INSPECTION OF EXISTING REPAIR DETERJun 30, 2022 · N721FD · Airbus A300* · Nacelle/Pylon StructureSDR FDEA202206301750None · unknownAIRCRAFT REPAIR ASSESSMENT : EXISTING FLOOR BEAM REPAIR FOUND ON AFT CARGO COMPARTMENT AT FR 59, BTW -Y805 ~ -Y1470 POSITION. COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, TITLE: A300/A310 RPR IDENT&SUPPLEMENTAL MX REQ(SMR) TRK, INSPECTION OF EXJun 30, 2022 · N721FD · Airbus A300* · Fuselage Structure (General)SDR FDEA202206301749None · unknownAIRCAFT REPAIR ASSESSMENT EXISTING EXTERNAL DOUBLER REPAIR FOUND ON #2 PYLON O/B SIDE, AT RIB 8 POSITION COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, TITLE: A300/A310 RPR IDENT&SUPPLEMENTAL MX REQ(SMR) TRK, INSPECTION OF EXISTING REPAIR DETERJun 30, 2022 · N721FD · Airbus A300* · Nacelle/Pylon StructureSDR FDEA202206301747None · unknownAIRCRAFT REPAIR ASSESSMENT:EXISTING EXTERNAL DOUBLER REPAIR FOUND ON #1 PYLON I/B SIDE, AT RIB8 POSITION. COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, TITLE: A300/A310 RPR IDENT&SUPPLEMENTAL MX REQ(SMR) TRK, INSPECTION OF EXISTING REPAIR DETERMJun 30, 2022 · N721FD · Airbus A300* · Nacelle/Pylon StructureSDR FDEA202206301746Skin · unknownAIRCRAFT REPAIR ASSESSMENT:EXISTING EXTERNAL DOUBLER REPAIR FOUND ON FUSELAGE SKIN AT FR85,BTW STGR41L-44L. COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, TITLE: A300/A310 RPR IDENT&SUPPLEMENTAL MX REQ(SMR) TRK, INSPECTION OF EXISTING REPAIR DETEJun 30, 2022 · N721FD · Airbus A300* · Fuselage Main, Plate/SkinSDR FDEA202206301740Skin · unknownAIRCRAFT REPAIR ASSESSMENT:EXISTING EXTERNAL DOUBLER REPAIR FOUND AROUND RH WING LWR SKIN L/E 613AB PANEL AT FWD O/B CUT OUT AREA. COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, TITLE: A300/A310 RPR IDENT&SUPPLEMENTAL MX REQ(SMR) TRK, INSPECTION Jun 30, 2022 · N721FD · Airbus A300* · Wing StructureSDR FDEA202206301739Skin · unknownAIRCRAFT REPAIR ASSESSMENT:EXISTING EXTERNAL DOUBLER REPAIR FOUND AROUND LH WING LWR SKIN L/E 513AB PANEL AT FWD O/B CUT OUT AREA. COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, TITLE: A300/A310 RPR IDENT&SUPPLEMENTAL MX REQ(SMR) TRK, INSPECTION Jun 30, 2022 · N721FD · Airbus A300* · Wing StructureSDR FDEA202206251804None · cracked1EA CRACK INDICATION WAS FOUND AT RIGHT SIDE FR54 STGR44 FASTENER HOLE. ACCOMPLISHED THE WORK BY REAMING THE HOLE THIS IS CATE.B REPAIR I.A.W EA NO:6-5330- T0369235 P1, SEQ NO:000909, TITLE:FUSELAGE-PLATES & SKINS-RH JUNCTION BETWEEN LATERAL SKIN PANEL AND Jun 25, 2022 · N721FD · Airbus A300* · Fuselage Main, Plate/SkinSDR FDEA202206251701Seat Track · corrodedMAIN DECK SEAT TRACK FOUND CORROSION NEAR FR 17 , Y 450 REMOVED DAMAGE PARTS & NEW TRACK INSTALLED WORK INSTRUCTION IAW A600-600 SRM 51- 40-21-001 PARA.6 , PAGE.7B-23 & SRM 51-76-20-201 PARA.4E , PAGE.210~211 , FIG.204.Jun 25, 2022 · N721FD · Airbus A300* · Fuselage Structure (General)SDR FDEA202206241785None · noneTHE LH LOWER FUSELAGE SKIN WAS FOUND DENT FR67 STGR35 ACCOMPLISHED THE CATE.B DOUBLER REPAIR TO THE LH FUSELAGE SKIN I.A.W A300-600 SRM 53- 10-12-201 PARA.5 PAGE.343-346 FIG.224(SHEET-4) & 53-17-12-001 PAGE.42-43 & SRI:53-10-12-201 IIR:53-10-12-2-004-00 PARJun 24, 2022 · N721FD · Airbus A300* · Fuselage Main, Plate/SkinSDR FDEA202206241702Seat Track · corrodedMAIN DECK SEAT TRACK FOUND CORROSION NEAR FR 15C , Y 950 REPLACED THE SEAT TRACK WITH NEW ONE I.A.W A300-600 SRM 51-72-10-001 PAGE.2 & 51-40-21- 001 PARA.6 , PAGE7B-23.Jun 24, 2022 · N721FD · Airbus A300* · Fuselage Structure (General)SDR FDEA202206241700Seat Track · corrodedMAIN DECK SEAT TRACK FOUND CORROSION NEAR FR 12A 2" , Y 700 REPLACED THE SEAT TRACK WITH NEW ONE I.A.W A300-600 SRM 51-72-10-001 PAGE.2 & 51-40-21- 001 PARA.6 , PAGE.7B~23 .Jun 24, 2022 · N721FD · Airbus A300* · Fuselage Structure (General)SDR FDEA202206231909Stiffener · corrodedWASTE WATER SERIVE PANEL COMP'T LOWER CUTOUT STIFFENER AREA CORROSION AT FR12A POSITION. REPLACED THE SIFFENER WITH NEW ONE I.A.W A300-600 SRM 51-72-10-001 , PAGE.2 .Jun 23, 2022 · N721FD · Airbus A300* · Fuselage Main, StructureSDR FDEA202110062474Actuator · nonePDIS 721 29-02 1252 06OCT21 MEM OPEN U GREEN SYSTEM HAD HYD LOW PRESSURE. COMPLIED WITH QRH. INFO 06OCT21 04:43 MC1 R LOST GREEN HYD SYSTEM QUANTITY DOWN TO BOTTOM OF YELLOW BAND. FOLLOWED BY LOSS OF SYSTEM PRESSURE. COMPLIED WITH QRH. MOct 6, 2021 · N721FD · Airbus A300B4622R · Hydraulic Power SystemSDR FDEA202108122007Altimeter · failedAT FL 360 THE STANDBY ALTIMETER WAS READING 300 FEET HIGHER THAN THE CAPTAIN AND FO ALTIMETERS. AT LOWER ALTITUDES IT RETURNED TO NORMAL. REF GMM 12-7-600. STANDBY ALTIMETER, CREW REPORTED MAIN ALTIMETERS OPS NORMAL. REMOVED AND REPLACED STANDBY ALTAug 12, 2021 · N721FD · Airbus A300B4622R · Altimeter, Barometric/EncoderSDR FDEA202108071990Adc · malfunctionedON GROUND F/O, CAPT , STBY ALTIMETER W/IN 50 FEET. AT 290 F/O AND CAPT ALTIMETER AGREED . AT 330 F/O READ 32.6 AND STBY READ 330 . F/O AIRSPEED WAS 10 TO 15 KTS SLOWER THAN CAPTAIN R/I 07AUG21 01:33 SNA U REASON CODE : PREMATURE REMOVAL/INSTALLATION Aug 7, 2021 · N721FD · Airbus A300B4622R · Flight Environment DataSDR FDEA202105061140Valve · contaminatedON APPROACH SELECTED GEAR DOWN. THE LEFT MAIN GEAR AND DOOR WERE SLOW ENOUGH TO CAUSE A GEAR NOT DOWN ECAM, BUT CANCELLED A FEW MOMENTS LATER AS THE CYCLE COMPLETED. NORMAL OPS THEEAFTER. DISCOVERED MATERIAL IN L/H MLG RESTRICTOR VALVE. REMOVED AND REPLMay 6, 2021 · N721FD · Airbus A300B4622R · Landing Gear Retraction/Extension System
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