N723FD

Service difficulty reports · 143

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 = 'N723FD' 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 FDEA201706241756Damper · malfunctionedAFTER TAKEOFF, THE LANDING GEAR WOULD NOT RETRACT. PERFORMED LANDING GEAR RETRACTION TEST IAW AMM 32-31-00-5 ON SYSTEMS 1 & 2. TEST WAS SATISFACTORY. REMOVED AND REPLACED THE LT PITCH DAMPER IAW AMM 32-11-15-04 AND PERFORMED FULL SREVICING IAW AMM 12-12-32Jun 24, 2017 · N723FD · Airbus A300B4622R · Landing Gear Retraction/Extension SystemSDR FDEA201705181455Static Inverter · failedJUST PRIOR TO TAKEOFF, ALL FUEL INDICATIONS DISPLAYED XX AND ALL FUEL INDICATIONS ON OVERHEAD PANEL WENT BLANK. ACRID ODOR AND SMOKE WAS PRESENT AND TWO LOUD BANGS WERE HEARD FROM THE E& E COMPARTEMENT. SHUTDOWN ENGINES AND ALL ELECTRICAL POWER TO THE AIRMay 18, 2017 · N723FD · Airbus A300B4622R · Pitot/Static SystemSDR FDEA201703301022Warning Light · false activationNR 2 ENGINE THRUST REVERSER LIGHT ON DURING TAKE OFF. REJECTED THE TAKE OFF. TROUBLESHOOTING PERFORMED IAWTSM 78-31-40. PERFORMED ADJUSTEMENT ON THE NR 2 ENGINE, RT SIDE OF TRANSLATING SLEEVE MASTER AND SLAVE ACTUATORS IAW MM 78-31-15-02. PERFORMED FURTHEMar 30, 2017 · N723FD · Airbus A300B4622R · Engine Thrust ReverserSDR FDEA201703020725Servo Valve · leakingRECEIVED A GREEN HYDRAULIC SYSTEM LOW PRESSURE ECAM, FOLLOWED BY GREEN RESERVOIR LOW LEVEL ECAM. FOLLOWED QRH INCLUDING MLG GRAVITY EXTENSION AND LANDED. OVERHEAD GREEN RESERVOIR GAUGE INDICATED AT THE BOTTOM OF THE YELLOW BAND. REMOVED AND REPLACED ARTIMar 2, 2017 · N723FD · Airbus A300B4622R · Hydraulic System, MainSDR FDEA201612184490Warning System · inoperativeON CABIN FINAL PREP, R1 DOOR SLIDE WOULD NOT ARM. FOUND NONE OF THE DOOR WARNING OR SLIDE INDICATIONS WORKING. RESET APSCU AND COMPLIED WITH ADJUSTMENT AND TEST IAW AMM 52-73-00-05-01. PAR 1. OPS CHECKED GOOD. ACFT OK FOR SERVICE.Dec 18, 2016 · N723FD · Airbus A300B4622R · Emergency EquipmentSDR FDEA201512244074Smoke Detector · faultyAT CRUISE ALTITUDE ECAM INDICATION OF AVIONICS SMOKE. OPERATING THE SNIFFER FAN IAW QRH YIELDED NO SMOKE INDICATIONS. THE ECAM ALERT EXTINGUISHED AFTER 3 MINUTES. THE SITUATION REOCCURRED UPON LANDING. REPLACED AVIONICS SMOKE DETECTORS 11WA & 13WA.Dec 24, 2015 · N723FD · Airbus A300B4622R · Smoke DetectionSDR FDEA201511183756Seat Track · damagedLOBE DAMAGE TO SEAT TRACK AT C33. NO RESTRICTION REF SR30-53-003 LOBE DAMAGE AT LOCK POS A840. OK IAW SR 30-53-003. INSPECTED DAMAGED AREA IAW SR 30-53-003. TRACK ONLY HAS LOBE DAMAGE. REMOVED FLOORBOARDS IAW AMM 53-10-23-04, REMOVED LOADING SYS IAW AMM 25Nov 18, 2015 · N723FD · Airbus A300B4622R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201510083119Stiffener · crackedNR 1 PYLON SPAR STIFFENER, FOUND CRACKED BETWEEN RIB 9 & 10 DURING NDT. REPAIRED IAW EA 6-5450-T0320597 P1. MAJOR REPAIR IAW GMM 6-2-100.Oct 8, 2015 · N723FD · Airbus A300B4622R · Nacelle/Pylon, Main FrameSDR FDEA201509272968Cover Plate · crackedFORWARD CARGO DOOR INNER COVER PLATE, JUST AROUND THE ACTUATOR ATTACH FITTING, FOUND CRACKED. REPAIRED IAW EA 6-5230-T0320449 P1. MAJOR REPAIR IAW GMM 6-2-100.Sep 27, 2015 · N723FD · Airbus A300B4622R · Cargo/Baggage DoorsSDR FDEA201509172889Floorbeam · crackedMAIN DECK CARGO BAY FRAME 15A, Y1456, FLOORBEAM CRACKED APPROX 3.0 INCH LENGTH. REPAIRED IAW SRM 53-12-15 FIG 207. MAJOR REPAIR IAW GMM 6-2-100.Sep 17, 2015 · N723FD · Airbus A300B4622R · Fuselage Main, Floor BeamSDR FDEA201509172893Floor Support · corrodedBULK CARGO FRAME 66, -Y140, FLOOR SUPPORT WITH EXFOLIATING CORROSION. REPLACED THE FLOOR SUPPORT IAW SRM 51-40-21. MAJOR REPAIR IAW GMM 6-2-100.Sep 17, 2015 · N723FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR FDEA201509172892Web · crackedMAIN DECK CARGO BAY FRAME 47, Y953 - Y1456, WEB CRACKED APPROX 1.0 INCH IN LENGTH. REPLACED THE WEB IAW SRM 51-40-21. MAJOR REPAIR IAW GMM 6-2-100.Sep 17, 2015 · N723FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR FDEA201509172891Web · crackedMAIN DECK CARGO BAY FRAME 47, Y450 - Y0, WEB CRACKED APPROX 1.0 INCH IN LENGTH. REPAIRED IAW SRM 53-15-15 FIGURE 201. MAJOR REPAIR IAW GMM 6-2-100.Sep 17, 2015 · N723FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR FDEA201509172890Web · crackedMAIN DECK CARGO COMPARTMENT FRAME 47, -Y450 - Y0, WEB CRACKED APPROX 1.0 INCH IN LENGTH. REPAIRED IAW DWG A53832100. REPLACED THE CRACKED WEB OF MDCC FRAME 47, -Y450 - Y0 IAW SRM 51-40-21. MAJOR REPAIR IAW GMM 6-2-100.Sep 17, 2015 · N723FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR FDEA201509152878Fitting · crackedCENTER WING BOX, FRAME 47 RT SIDE, CORNER ANGLE FITTING K HOLE FOUND CRACKED. COMPLIED WITH EA 6-5710-150908 A P 3. MAJOR REPAIR IAW GMM 6-2-100.Sep 15, 2015 · N723FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR FDEA201509152877Fitting · crackedAFT CARGO DOOR ACTUATOR ATTACH FITTING FOUND CRACK. REPLACED THE ACTUATOR FITTING OF AFT CARGO DOOR IAW SRM 51-40-21. MAJOR REPAIR IAW GMM 6-2-100.Sep 15, 2015 · N723FD · Airbus A300B4622R · Cargo/Baggage DoorsSDR FDEA201509152876Fitting · crackedFORWARD CARGO DOOR ACTUATOR ATTACH FITTING CRACKED. REPLACED THE CRACKED FITTING OF FWD CARGO DOOR IAW SRM 51-40-21. MAJOR REPAIR IAW GMM 6-2-100.Sep 15, 2015 · N723FD · Airbus A300B4622R · Cargo/Baggage DoorsSDR FDEA201509142859Cover Plate · crackedAFT CARGO DOOR INNER COVER PLATE, JUST AROUND THE ACTUATOR ATTACH FITTING FOUND CRACKED. REPAIRED IAW EA 6-5230-T0320275 P1. MAJOR REPAIR IAW GMM 6-2-100.Sep 14, 2015 · N723FD · Airbus A300B4622R · Cargo/Baggage DoorsSDR FDEA201412194155Sealant · missingAFTER THE INITIAL REPAIR OF THE PREVIOUS FUEL QTY INDICATION PROBLEM, THE PROBLEM REOCCURRED & THEN SMELL OF SMOKE BECAME EVIDENT. FUEL QTY INDICATING IS NORMAL. GVI CHECKED FOUND 90VU, 80VU,107VU & T CAS COMPUTER UMBRELLA PANEL AREA WATER DROP FROM CEILING Dec 19, 2014 · N723FD · Airbus A300B4622R · Cargo CompartmentsSDR FDEA201408192221Battery · dischargedCOURIER COMPARTMENT INTERIOR EMER LIGHTS TEST INOPERATIVE. MANUAL TEST OK. R & R THE EMER POWER SUPPLY BATTERY, TEST NORMAL IAW AMM33-51-14-04-09. PART INFO SEE WR I 05-25 1105.Aug 19, 2014 · N723FD · Airbus A300B4622R · Emergency LightingSDR FDEA201404240840Rib · corrodedRIGHT RIB NR 5 HAS CORROSION IN BORE & FACE. REPAIRED IAW EA 6-5710-T0307642 P2.Apr 24, 2014 · N723FD · Airbus A300B4622R · Wing, Rib/BulkheadSDR FDEA201404240839Rib · corrodedLEFT RIB NR 5 HAS CORROSION IN BORE & FACE. REPAIRED IAW EA 6-5710-T0307642 P1.Apr 24, 2014 · N723FD · Airbus A300B4622R · Wing, Rib/BulkheadSDR FDEA201402050339Floor Panel · damagedMAIN CABIN FLOOR PANEL 241KK HAS BROKEN EDGE. FABRICATED FLOOR PANEL IAW DWG SRZ-25-005.Feb 5, 2014 · N723FD · Airbus A300B4622R · Fuselage Floor PanelSDR FDEA201402040340Floor Panel · crackedMAIN DECK CARGO FLOOR PANEL 242LK CRACKED. FABRICATED FLOOR PANEL IAW DWG SRZ-25-005.Feb 4, 2014 · N723FD · Airbus A300B4622R · Fuselage Floor PanelSDR FDEA201402030347Floor Panel · puncturedMAIN CARGO COMPARTMENT FLOOR PANEL 252GF HAS PUNCTURE. FABRICATED FLOOR PANEL 252G IAW DWG SRZ-25-005 ON STAM TRAVELER T14 1049828.Feb 3, 2014 · N723FD · Airbus A300B4622R · Fuselage Floor PanelSDR FDEA201301310240Check Valve · leakingMAIN CARGO DECK SMOKE DETECTOR ACTIVATED WHEN APU BLEED SELECTED ON. SMOKE FILLED MAIN DECK. CLOSED APU BLEED AND SHUTDOWN APU, BATTERIES. FOUND BOTH RELIEF VALVES STUCK OPEN ON BOTH SIDES. REPLACED APU PRESSURE LINE CHECK VALVE IAW MM 29-14-17-04, REPLACJan 31, 2013 · N723FD · Airbus A300B4622R · Hydraulic System, MainSDR FDEA201205011698Warning Light · false activationAT CRUISE, ECAM ALERT GREEN SYS HYD LO LEVEL, ECAM SHOWED GREEN SYS NEAR ZERO. C/W 11-3-05 "HYD RSVR LO LEVEL" PROCEDURE. MANUAL GEAR EXTENSION. EMERGENCY DECLARED. NO NOSEWHEEL STEERING. AFTER LANDING, GREEN HYD SYS QUANTITY SHOWED IN NORMAL RANGE. WMay 1, 2012 · N723FD · Airbus A300B4622R · Hydraulic Indicating SystemSDR FDEA201204151430Cable · disconnectedLEFT WING ASA OTBD PCA JAM DETECTION CABLE FOUND CAPPED AND STOWED. CABLE RECONNECTED AND HYD ACTUATION (AILERON) TEST CARRIED OUT IAW AMM 27-14-00-05. ALL OPS SERVICEABLE IAW SERVO CONTROL JAMMING DETECTION TEST.Apr 15, 2012 · N723FD · Airbus A300B4622R · Aileron Control SystemSDR FDEA201108233426Smoke Detector · inoperativeAFTER GEAR UP, IN-FLIGHT AVIONICS SMOKE ON ECAM ON GND CONTINUOUS ECAM WARNING. INSPECTED AVIONICS BAY FOR SMOKE/EVIDENCE OF OVERHEATING, NONE FOUND. TESTED AVIONICS COMPARTMENT DETECTORS IAW TSM 26-15-00-05, FOUND MAIN BAY AND MINIMUM EQUIPMENT BAY DETECAug 23, 2011 · N723FD · Airbus A300B4622R · Smoke DetectionSDR FDEA201108223407Smoke Detector · false activationAFTER GEAR UP, IN FLIGHT "AVIONICS SMOKE" ON ECAM. ON GROUND CONTINUOUS ECAM WARNING. INSPECTED AVIONICS BAY FOR SMOKE & EVIDENCE OF OVERHEATING NONE FOUND.Aug 22, 2011 · N723FD · Airbus A300B4622R · Smoke DetectionSDR FDEA201108163298Panel · chafedNR 1, PYLON HYD LINE UNIONS AT AFT FAIRING DISCONNECT POINT FRETTING IN WING REAR SPAR FITTING. REWORK ACCOMPLISHED ON EA 6-5720-150921.Aug 16, 2011 · N723FD · Airbus A300B4622R · Wing Miscellaneous StructureSDR FDEA201108163297Panel · chafedLT PYLON HYD LINE UNIONS AT AFT FAIRING DISCONNECT POINT FRETTING IN WING REAR SPAR FITTING. REWORKED ACCOMPLISHED ON EA 6-5720-150921.Aug 16, 2011 · N723FD · Airbus A300B4622R · Wing Miscellaneous StructureSDR FDEA201108163296Panel · chafedRT PYLON HYD LINE UNIONS AT AFT FAIRING DISCONNECT POINT FRETTING IN WING REAR SPAR FITTING REWORKED, ACCOMPLISHED ON EA 6-5720-150920.Aug 16, 2011 · N723FD · Airbus A300B4622R · Wing Miscellaneous StructureSDR FDEA201108113222Angle · bentAFT CARGO DOOR CUTOUT FWD UPPER ANGLE FOUND DISTORTED. AFT CARGO DOOR CUTOUT UPPER ANGLE REPLACED.Aug 11, 2011 · N723FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR FDEA201119063290Roller Track · corrodedROLLER TRACK AT FR32-FR38.2 Y1420 CORRODED ON INBD SIDE, BEYOND SRM 53-10-15 LIMITS ROLLER TRACK REPLACED IAW AMM 25-52-21-04-0.Aug 6, 2011 · N723FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR FDEA201108063121Fitting · chafedSUSPECT WEAR CHAFE DAMAGE TO LUG FITTING MID RUDDER PCA FITTING AT RUDDER ATTACHMENT. ATTACHMENT CUT OUT ON EA 6-5500-150939 AND RAS 70550958/003/2011.Aug 6, 2011 · N723FD · Airbus A300F4622R · Rudder StructureSDR FDEA201108063120Fitting · chafedSUSPECT WEAR CHAFE DAMAGE TO LUG FITTING, LWR RUDDER PCA FITTING AT RUDDER ATTACHMENT. REWORK C/OUT ON EA 6-5500-150939 AND RAS 7055.Aug 6, 2011 · N723FD · Airbus A300B4622R · Rudder StructureSDR FDEA201107293023Panel · misrepairedREPAIR FOUND AT FR 52-53 RT FUSE SKIN MLG BAY CUTOUT AREA AFT CORNER, SKIN EVALUATED ON NRC N00570 AND FOUND TO NOT CONFORM TO ANY APPROVED DOCUMENTATION. DOUBLER REPAIR INSTALLED ON EA 6-5315-150928Jul 29, 2011 · N723FD · Airbus A300B4622R · Fuselage Main, Plate/SkinSDR FDEA201107252936Floor Support · corrodedFLOOR SUPPORT FOUND CORRODEDJul 25, 2011 · N723FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR FDEA201107252935Floor Support · corrodedFLOOR SUPPORT FOUND CORRODED.Jul 25, 2011 · N723FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR FDEA201107252934Seat Track · corrodedSEAT TRACK FOUND CORRODED.Jul 25, 2011 · N723FD · Airbus A300B4622R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201107252933Seat Track · corrodedSEAT TRACK FOUND CORRODED.Jul 25, 2011 · N723FD · Airbus A300B4622R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201107252932Seat Track · corrodedSEAT TRACK FOUND CORRODED.Jul 25, 2011 · N723FD · Airbus A300B4622R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201107232918Skin · corrodedAFT CARGO HOLD FR54 TO 54.1, S57R FUSELAGE SKIN CORRODED. REPAIR ACCOMPLISHED ON EA 6-5316-150940.Jul 23, 2011 · N723FD · Airbus A300B4622R · Fuselage Main, Plate/SkinSDR FDEA201107232916Angle · corrodedBULK CARGO DOOR SILL INNER ANGLE FR67-69 FOUND CORRODED AT FR67 BULK CARGO DOOR SILL INNER ANGLE FR67-69 REPLACED.Jul 23, 2011 · N723FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR FDEA201107232915Floorbeam · corrodedFLOORBEAM FR67 Y-430 CORRODED FLOORBEAM, FR67 Y-430, REPLACED.Jul 23, 2011 · N723FD · Airbus A300B4622R · Fuselage Main, Floor BeamSDR FDEA201107222900Seat Track · corrodedSEAT TRACK FOUND CORRODED AT Y450, FR14 TO 15A. SEAT TRACK REPLACED.Jul 22, 2011 · N723FD · Airbus A300B4622R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201107222899Seat Track · corrodedSEAT TRACK FOUND CORRODED AT -Y953, FR15A TO 18/19. SEAT TRACK REPLACED.Jul 22, 2011 · N723FD · Airbus A300B4622R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201107222894Seat Track · corrodedSEAT TRACK FOUND CORRODED AT Y-450, FR 14 TO 15A. SEAT TRACK REPLACED.Jul 22, 2011 · N723FD · Airbus A300B4622R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201107222896Floor Support · corrodedFLOOR SUPPORT Y953 FOUND CORRODED AT FR 11-13 AREA FLOOR SUPPORT Y953 REPLACED FROM FR11 TO FR15A IAW SRM 51-40-21Jul 22, 2011 · N723FD · Airbus A300B4622R · Fuselage Miscellaneous Structure
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