N810FD, cancelled Mar 2, 2024

Service difficulty reports · 68

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 = 'N810FD' AND deregistration_id = 'N810FD-2024-03-02'
  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 FDEA201601200234Gcu · failedON TAKEOFF AT 80 KNOTS GEN II FAILED, THEN FOLLOWED BY GEN 1, TOTAL ELEC FAILURE. REJECTED TAKEOFF, CLEARED RUNWAY & RAN QRH. REJECTED AT 100 KNOTS. INTERROGATED GPCU & FPUND BOTH 1 & 2, GCU FAILED. R & R BOTH GCU'S IAW MM 24-22-12-04. RAN BOTH ENGS IAW Jan 20, 2016 · N810FD · Airbus A310324 · AC RegulatorSDR FDEA201509172894Switch · failedDURING TAKEOFF ROLL, RECEIVED A MOMENTARY NR 2 THRUST REVERSER UNLOCKED ALERT & INSTRUMENT CLUSTER TOP LIGHT. LIGHT EXTINGUISHED & TAKEOFF WAS CONTINUED. AFTER TAKEOFF & WHEELS UP, THE ALERT CAME BACK ON. NO ADVERSE CONTROL WAS NOTICED. COMPLIED WITH ECAM.Sep 17, 2015 · N810FD · Airbus A310324 · Engine Thrust ReverserSDR FDEA201504081201Altimeter · malfunctionedREPEAT WRITE UP, STBY ALTIMETER WITHIN 30' OF PRIMARY ALTIMETERS ON THE GND. AT FL 300 STBY ALTIMETER WAS 160 FT HIGHER, AT FL 148 STBY ALTIMETER WAS 250 FT HIGHER. R & R THE STBY ALTIMETER IAW AMM 34-12-22-04. INTEGRAL LIGHTING OPERATIONAL TEST NORMAL IAW Apr 8, 2015 · N810FD · Airbus A310324 · Altimeter, Barometric/EncoderSDR FDEA201504071200Altimeter · malfunctionedAT CRUISE ALTITUDE 35,000, STBY ALTIMETER INDICATES 250 HIGHER THAN BOTH CAPTAINS & COPILOTS ALTIMETERS. R & R THE STBY ALTIMETER IAW AMM 34-12-22-04. INTEGRAL LIGHTING OPERATIONAL TEST NORMAL IAW AMM 33-13-00-05. ACFT OK FOR SERVICE.Apr 7, 2015 · N810FD · Airbus A310324 · Altimeter, Barometric/EncoderSDR FDEA201503020625Seat Track · damagedCOMPLY WITH WRI 25-50/0216 & 0217, REPAIR THE SEAT TRACK ASSEMBLY OF MDC FRAME 54.2 - 58 RESTRAINT ID N1199. REPAIRED THE SEAT TRACK IAW SRM 53-10-16 FIGURE 202. THIS REPAIR CATEGORY A. MAJOR REPAIR IAW GMM 6-2-100.Mar 2, 2015 · N810FD · Airbus A310324 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201401210149Relay · failedDURING DESCENT, RECEIVED AN INTERMITTENT CHIME, WITH NO ECAM ALERT, INVESTIGATION FOUND LOW FUEL TANK AT 1.5 & RO AT 1.7. THE CENTER TANK WAS FEEDING & TRIM TANK TRANSFERRING FWD. UNABLE TO RECOVER INNER FUEL TANK & APPROXIMATELY 17600 LBS OF FUEL WAS TRAPPJan 21, 2014 · N810FD · Airbus A310324 · Aircraft Fuel Distribution SystemSDR FDEA201310012366Smoke Detector · failedEQUIPMENT BAY SMOKE INDICATION, SEVERAL MINUTES AFTER, HEARD A LOUD BANG. UNKNOWN WHERE SOUND COME FROM. FIRE WARNING ILLUMINATED SEVERAL TIMES. DID NOT SMELL SMOKE. PERFORMED SMOKE DETECTION OPS TEST IAW AMM 26-15-00-05, FOUND SMOKE ECAM WARNING AND COUOct 1, 2013 · N810FD · Airbus A310324 · Smoke DetectionSDR FDEA201309132202Fitting · corrodedRT WING MLG FITTING OF RIB 5 FORWARD LUG CORRODED, COMPLY WITH EA6-5710-T0302341A.Sep 13, 2013 · N810FD · Airbus A310324 · Wing, Landing Gear Attach FittingsSDR FDEA201309132201Fitting · corrodedLT WING MLG FITTING OF RIB 5 FORWARD LUG FOUND CORROSION, COMPLY WITH EA 6-5710-T0302340.Sep 13, 2013 · N810FD · Airbus A310324 · Wing, Landing Gear Attach FittingsSDR FDEA201206172253Hydraulic System · warning messageDURING CLIMB, HAD GREEN SYS OVERHEAT ECAM. COMPLIED WITH CHECKLIST, MANUALLY EXTENDED LANDING GEAR TOWED OFF RUNWAY. DRAINED AND SERVICED GREEN SYS HYD RESERVIOUR PER MM 29-14-00-03. RAN NR 1 AND 2 ENGINES IAW JRH. ALL INDICATIONS AND PARAMETERS NORMAL. Jun 17, 2012 · N810FD · Airbus A310324 · Hydraulic System, MainSDR FDEA201203301200Hydraulic System · multiple failDURING CRUISE FLIGHT, HYD GREEN SYS RESERVOIR OVERHEAT ILLUMINATED ON ECAM. GREEN HYD PUMPS SECURED UNTIL APPROACH. TURNED BACK ON LOW POWER LIGHTS ILLUMINATED, NO GREEN HYD QUANTITY INDICATED. R & R NR 1 AND NR 2 ENGINE PUMPS OF GREEN SYS IAW MM 29-11-32-0Mar 30, 2012 · N810FD · Airbus A310324 · Hydraulic System, MainSDR FDEA201102040472Outflow Valve · failed1 HR INTO FLIGHT, CABIN PRESSURE EXCEEDED TOLERANCE (AROUND 9.0 ON DEFFERENTIAL PRESSURE) AND BOTH CONTROLLERS FAILED. HAD TO SELECT MANUAL AGAIN TO BRING PRESSURE BACK DOWN. REACTIVED AFT OUTFLOW VALVE IAW MEL21-31-04-01-A, PERFORMED BITE TEST FOUND "AFT VAFeb 4, 2011 · N810FD · Airbus A310324 · Pressure Regulator/Outflow ValveSDR FDEA200901140199Floor Panel · damagedFWD CARGO COMPARTMENT FLOOR PANELS ZONE 131, FLOOR PANEL 131QG HAS STRUCTURAL DAMAGES. FABRICATED NEW FLOOR PANEL NR 131QG PER SAMPLE IAW SRZ 25-005, ON TRAVELER NR T8/773386.Jan 14, 2009 · N810FD · Airbus A310324 · Fuselage Floor PanelSDR FDEA200901140198Floor Panel · damagedFWD CARGO COMPARTMENT FLOOR PANELS ZONE 132, FLOOR PANEL 132YF HAS STRUCTURAL DAMAGES. FABRICATED NEW FLOOR PANEL NR 132YF PER SAMPLE IAW SRZ 25-005,ON TRAVELER NR T8/773385.Jan 14, 2009 · N810FD · Airbus A310324 · Fuselage Floor PanelSDR FDEA200901140197Floor Panel · damagedFWD CARGO COMPARTMENT FLOOR PANELS ZONE 132, FLOOR PANEL 132RF HAS STRUCTURAL DAMAGES. FABRICATED NEW FLOOR PANEL NR 132RF PER SAMPLE IAW SRZ 25-005, ON TRAVELER NR T8/773389.Jan 14, 2009 · N810FD · Airbus A310324 · Fuselage Floor PanelSDR FDEA200901140196Floor Panel · damagedMAIN DECK CARGO COMPARTMENT ZONE 232, FLOOR PANEL 323RG HAS STRUCTURAL DAMAGES. FABRICATED NEW FLOOR PANEL NR 232RG PER SAMPLE IAW SRZ 25-005, ON TRAVELER NR T8/773437.Jan 14, 2009 · N810FD · Airbus A310324 · Fuselage Floor PanelSDR FDEA200901140195Floor Panel · damagedMAIN DECK CARGO COMPARTMENT ZONE 231, FLOOR PANEL 231QG HAS STRUCTURAL DAMAGES. FABRICATED NEW PANEL NR 231QG PER SAMPLE IAW SRZ 25-005, ON TRAVELER NR T8/773436.Jan 14, 2009 · N810FD · Airbus A310324 · Fuselage Floor PanelSDR FDEA200901140194Floor Panel · damagedFWD CARGO COMPARTMENT FLOOR PANELS ZONE 132, FLOOR PANEL 132ZF HAS STRUCTURAL DAMAGES. FABRICATED NEW FLOOR PANEL NR 132ZF PER SAMPLE IAW SRZ 25-005,ON TRAVELER T8/773387.Jan 14, 2009 · N810FD · Airbus A310324 · Fuselage Floor PanelSDR FDEA200901130185Floor Panel · damagedMAIN DECK CARGO COMPARTMENT ZONE 231, FLOOR PANEL 231VH HAS STRUCTURAL DAMAGES. FABRICATED NEW FLOOR PANEL 231VH PER SAMPLE, ON TRAVELER NR T8 /773390.Jan 13, 2009 · N810FD · Airbus A310324 · Fuselage Floor PanelSDR FDEA200901130184Floor Panel · damagedMAIN DECK CARGO COMPARTMENT ZONE 241, FLOOR PANEL 241WH HAS STRUCTURAL DAMAGES. FABRICATED NEW FLOOR PANEL 241WH PER SAMPLE IAW SRZ 25-005 ,ON TRAVELER NR T8/773451.Jan 13, 2009 · N810FD · Airbus A310324 · Fuselage Floor PanelSDR FDEA200901130183Floor Panel · damagedMAIN DECK CARGO COMPARTMENT ZONE 231, FLOOR PANEL 231LH HAS STRUCTURAL DAMAGES. FABRICATED NEW PANEL PER SAMPLE IAW SRZ 25-005,ON TRAVELER NR T8/773432.Jan 13, 2009 · N810FD · Airbus A310324 · Fuselage Floor PanelSDR FDEA200901130180Floor Panel · damagedMAIN DECK CARGO COMPARTMENT ZONE 231, FLOOR PANEL 231NH HAS STRUCTURAL DAMAGES FABRICATED NEW PANEL PER SAMPLE IAW SRZ 25-005, ON TRAVELER 3 T8/773431.Jan 13, 2009 · N810FD · Airbus A310324 · Fuselage Floor PanelSDR FDEA200901130179Floor Panel · damagedMAIN DECK CARGO COMPARTMENT ZONE 252, FLOOR PANEL 252UH HAS STRUCTURAL DAMAGES FABRICATED NEW FLOOR PANEL NR 252UH PER SAMPLE IAW SRZ 25-005 ON TRAVELER NR T8/773453.Jan 13, 2009 · N810FD · Airbus A310324 · Fuselage Floor PanelSDR FDEA200901130178Floor Panel · damagedMAIN CARGO COMPARTMENT ZONE 241, FLOOR PANEL NR 241BK HAS STRUCTURAL DAMAGES. FABRICATED NEW FLOOR PANEL PER SAMPLE IAW SRZ 25-005 ON TRAVELER NR T8/773452.Jan 13, 2009 · N810FD · Airbus A310324 · Fuselage Floor PanelSDR FDEA200901130177Floor Panel · damagedMAIN DECK CARGO COMPARTMENT ZONE 241, FLOOR PANEL 241QJ HAS STRUCTURAL DAMAGES. FABRICATED NEW CARGO PANEL NR 241QJ PER SAMPLE IAW SRZ 25-005 ON TRAVELER NR T8/773440.Jan 13, 2009 · N810FD · Airbus A310324 · Fuselage Floor PanelSDR FDEA200901130176Floor Panel · damagedFWD CARGO COMPARTMENT FLOOR PANELS ZONE 132, FLOOR PANEL 132QF HAS STRUCTURAL DAMAGES. FABRICATED NEW FLOOR PANEL NR 132QF PER SAMPLE IAW SRZ 25-005 ON TRAVELER NR T8/773388.Jan 13, 2009 · N810FD · Airbus A310324 · Fuselage Floor PanelSDR FDEA200901130175Floor Panel · damagedMAIN DECK CARGO COMPARTMENT ZONE 252, FLOOR PANEL 252CH HAS STRUCTURAL DAMAGES. FABRICATED NEW MAIN DECK PANEL NR 252CH PER SAMPLE IAW SRZ 25-005 ON TRAVELER NR T8/773455.Jan 13, 2009 · N810FD · Airbus A310324 · Fuselage Floor PanelSDR FDEA200901120167Floor Panel · damagedFWD CARGO COMPARTMENT FLOOR PANEL, ZONE 131 FLOOR PANEL 131 HG HAS STRUCTURAL DAMAGES FABRICATED NEW FWD CARGO COMPARTMENT FLOOR PANEL PER SAMPLE , PANEL 131 HG IAW SRZ 25-005 ON TRAVELER T8/ 773384.Jan 12, 2009 · N810FD · Airbus A310324 · Fuselage Floor PanelSDR FDEA200901120166Floor Panel · damagedMAIN DECK CARGO COMARTMENT, ZONE 231 FLOOR PANEL 231 AJ HAS STRUCTURAL DAMAGES FABRICATED NEW MAIN CARGO DECK COMPARTMENT FLOOR PANEL 231 AJ PER SAMPLE IAW SRZ 25-005 ON TRAVELER T8/ 773438Jan 12, 2009 · N810FD · Airbus A310324 · Fuselage Floor PanelSDR FDEA200901120165Floor Panel · damagedMAIN CARGO DECK COMPARTMENT, ZONE 231 FLOOR PANEL 231 XH HAS STRUCTURAL DAMAGES FABRICATED NEW MAIN DECK CARGO COMPARTMENT FLOOR PANEL 231 XH PER SAMPLE IAW SRZ 25-005 ON TRAVELER T8/ 773439.Jan 12, 2009 · N810FD · Airbus A310324 · Fuselage Floor PanelSDR FDEA200901120164Floor Panel · damagedMAIN CARGO DECK COMPARTMENT, ZONE 231 FLOOR PANEL 231 XH HAS STRUCTURAL DAMAGES FABRICATED NEW MAIN DECK CARGO COMPARTMENT FLOOR PANEL 231 XH PER SAMPLE IAW SRZ 25-005 ON TRAVELER T8/ 773439.Jan 12, 2009 · N810FD · Airbus A310 · Fuselage Floor PanelSDR FDEA200901120163Floor Panel · damagedMANI DECK CARGO COMPARTMENT,ZONE 251 FLOOR PANEL 251 ZH HAS STRUCTURAL DAMAGES. FABRICATED NEW MAIN DECK CARGO COMPARTMENT FLOOR PANEL 251 ZH PER SAMPLE IAW SRZ 25-005 ON TRAVELER T8/ 773454Jan 12, 2009 · N810FD · Airbus A310 · Fuselage Floor PanelSDR FDEA200901120162Floor Panel · damagedBULK CARGO COMPARTMENT ZONE 161,FLOOR PANEL 161GF HAS STRUCTURAL DAMAGES. FABRICATED NEW FLOOR PANEL 161GF PER SAMPLE IAW SRZ 25-011.Jan 12, 2009 · N810FD · Airbus A310324 · Fuselage Floor PanelSDR FDEA200901120160Floor Panel · damagedBULK CARGO COMPARTMENT, ZONE 161 FLOOR PANEL 161BF HAS STRUCTURAL DAMAGES. FABRICATED NEW FLOOR PANEL NR 161BF PER SAMPLE, IAW SRZ 25-011 ON TRAVELER.Jan 12, 2009 · N810FD · Airbus A310324 · Fuselage Floor PanelSDR FDEA200901120159Floor Panel · damagedBULK CARGO COMPARTMENT ZONE 162, FLOOR PANEL 162HF HAS STRUCTURAL DAMAGES. FABRICATED NEW FLOOR PANEL 162HF PER SAMPLE IAW SRZ 25-011 ON TRAVELER.Jan 12, 2009 · N810FD · Airbus A310324 · Fuselage Floor PanelSDR FDEA200901120156Floor Panel · damagedAFT CARGO COMPARTMENT FLOOR PANELS ZONE 151, FLOOR PANEL 151AF HAS STRUCTURAL DAMAGE. FABRICATED NEW FLOOR PANEL 151AF PER SAMPLE IAW SRZ 25-005, ON TRAVELER NR T8/775133.Jan 12, 2009 · N810FD · Airbus A310324 · Fuselage Floor PanelSDR FDEA200901120151Rib · crackedLEFT WING TIP RIB WY489 CRACKED REMOVED CRACKED RIB WY489.0 IAW SRM 51-40-21. FABRICATED NEW RIB ON TRAVELER NR T8/773917, BATCH NR 436186A1. INSTALLED RIB IAW SRM 51-40-21, AND 57-30-11.Jan 12, 2009 · N810FD · Airbus A310324 · Wing, Rib/BulkheadSDR FDEA200901020002Doubler · damagedTHE LT MAIN GEAR WHEEL WELL DOOR INNER AFT TIRE RECESS HAS A 1 INCH GROVE AT THE FWD OTBD SIDE BLENDED AREA ORIG MAT .063 REMAINING MAT IS OUT OF LIMITS, REMOVED DAMAGE. HFEC, NO CRACKS FOUND. FABRICATED AND INSTALLED DOUBLER IAW SRM51-71-30 FIG 102.Jan 2, 2009 · N810FD · Airbus A310324 · Fuselage Miscellaneous StructureSDR FDEA200812305320Floor Panel · crackedFWD CARGO COMPARTMENT FLOOR PANELS, ZONE 131, FLOOR PANEL 131 HG HAS STRUCTURAL DAMAGES FABRICATED NEW FWD CARGO COMPARTMENT FLOOR PANEL, IAW SAMPLE,PANEL 131 HG, IAW SRZ-25-005,ON TRAVELER, NR T8/773384.Dec 30, 2008 · N810FD · Airbus A310 · Fuselage Floor PanelSDR FDEA200812245272Structure · corrodedAIR CONDITIONING COMPT BETWEEN FR44 AND FR45, STR 38R AND 39R HAS SURFACE CORROSION. REMOVED LIGHT SURFACE CORROSION IAW SRM 51-74-10, MATERIAL LOSS .001 IN. TREATED AND PRIMED IAW SRM 51-21-10, PAINTED IAW MM 75-10-08.Dec 24, 2008 · N810FD · Airbus A310324 · Fuselage Main, StructureSDR FDEA200812185224Seat Track · corrodedMAIN CARGO DECK SEAT TRACK AT RBL 18 HAS EXFOLIATION FROM FR 19 TO FR 14B. REMOVED SEAT TRACK IAW SRM 51-40-21, LOCATED AND DRILLED NEW SEAT TRACK IAW SRM 51-40-44, P/N A538320202400 BATCH 0001549861. INSTALLED SEAT TRACK IAW SRM 51-40-21.Dec 18, 2008 · N810FD · Airbus A310324 · Fuselage, Seat/Cargo Attach FittingsSDR 08FDEA03601Computer · failedON APPROACH TO KBUR APPROX 5000' MSL, WHEN SELECTING 20 DEGREES FLAP, T/E FLAPS STUCK AT 15 DEGREES WITH SYS 1 AND 2 FLAP FAULT LIGHTS ILLUMINATED. DIVERTED TO LAX. LANDED WITH 30/15 IAW QRH PROCEEDURES. PERFORMED THE REMAINING OF THE T/S AND FOUND NO DEFEAug 26, 2008 · N810FD · Airbus A310324 · Trailing Edge Flap Control SystemSDR 08FDEA02261Line · leakingHYD GREEN SYSTEM LOW LEVEL IN FLIGHT. ECAM WARNING, MANUAL EXTENTION OF L/G. FOUND UPPER HYD LINE TO RT AILERON DROOP ACTUATOR LEAKING. REPAIRED SAME HYD LINE IAW AMM 20-23-11-0, LEAK CHECK GOOD. REPLENISHED GREEN HYDRAULIC SYSTEM IAW AMM 29-10-00-3. CRJun 13, 2008 · N810FD · Airbus A310324 · Hydraulic System, MainSDR 07FDEA01500Skin · corrodedDUE TO REMOVAL OF SOME FASTENERS DURING REMOVAL OF CORROSION ON OUTER SKIN AT C80, P5-6 RHS IT WAS IMPOSSIBLE TO REINSTALL SOME FASTENERS WITHOUT DAMAGING THE AFT PRESSURE BULKHEAD. REPAIR PERFORMED BY INSTALLATION OF FOUR ALTERNATE BOLTS NSA 6603-5, APPROVEDApr 13, 2007 · N810FD · Airbus A310324 · Fuselage Main, Plate/SkinSDR 07FDEA01499Shear Tie · crackedFOUND CRACKED HOLES DURING ACCOMPLISHMENT OF EO 6-5310-7-5020 PT.1, LHS (C43 HOLE H2 CRACK LENGTH 9MM; C45 HOLE H22 CRACK LENGTH 7MM; C46 HOLE H29 CRACK LENGTH 8MM). REPAIR PERFORMED BY REPLACEMENT OF FITTING A538-70064 FOR HOLE H2, OVERSIZING HOLE H22 AND H2Apr 13, 2007 · N810FD · Airbus A310324 · Fuselage Internal Mounting StructureSDR 07FDEA01498Skin Panel · corrodedFOUND CORROSION AT UPPER SKIN PANEL C91, P4 RT. REPAIR PERFORMED BY BLEND OUT IAW EA 6-5319-103315 AND RAS/DAHAM/4020861/2006 ISSUE "A".Apr 13, 2007 · N810FD · Airbus A310324 · Fuselage Main, Plate/SkinSDR 07FDEA01497Skin · dentedDENT IN OUTER SKIN AT C20, P24-25, RHS. REPAIR PERFORMED BY SMALL BLEND OUT IAW EA 6-5313-101308 AND RAS/DABRE/7006763/2006 ISSUE "A".Apr 13, 2007 · N810FD · Airbus A310324 · Fuselage Main, Plate/SkinSDR 07FDEA01496Vane · chafedCHAFING MARKS AT INBOARD FLAP VANE, RHS. REPAIR WAS PERFORMED BY BLEND OUT TO SMOOTH CONTOUR IAW EA 6-5752-101309 AND RAS/DABRE/7006736/2006 ISSUE "A".Apr 13, 2007 · N810FD · Airbus A310324 · Trailing Edge FlapsSDR 07FDEA01495Bulkhead · damagedSCRATCH IN PRESSURE BULKHEAD AT C54, TR 4 LT. REPAIR PERFORMED BY BLEND OUT IAW EA 6-5315-101318 AND RAS/045121/010/2006 ISSUE "A".Apr 13, 2007 · N810FD · Airbus A310324 · Fuselage Main, BulkheadSDR 07FDEA01494Skin · corrodedCORROSION ON SEVERAL AREAS AT AIR CONDITIONING COMPARTMENT, C39-C47, P44-P54 LT. REPAIR PERFORMED BY BLEND OUT IAW EA 6-5315-101310 AND RAS/045255/008/2006 ISSUE "A".Apr 13, 2007 · N810FD · Airbus A310324 · APU Cowling/Containment
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