# Service difficulty reports: N810FD, cancelled Mar 2, 2024 A list on [N810FD, cancelled Mar 2, 2024](https://openairdocs.org/deregistered/N810FD-2024-03-02.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 2 · 68 reports - [SDR FDEA201601200234](https://openairdocs.org/sdr/FDEA201601200234.md): Gcu · failed · Jan 20, 2016 · N810FD · Airbus A310324 · AC Regulator > ON 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 - [SDR FDEA201509172894](https://openairdocs.org/sdr/FDEA201509172894.md): Switch · failed · Sep 17, 2015 · N810FD · Airbus A310324 · Engine Thrust Reverser > DURING 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. - [SDR FDEA201504081201](https://openairdocs.org/sdr/FDEA201504081201.md): Altimeter · malfunctioned · Apr 8, 2015 · N810FD · Airbus A310324 · Altimeter, Barometric/Encoder > REPEAT 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 - [SDR FDEA201504071200](https://openairdocs.org/sdr/FDEA201504071200.md): Altimeter · malfunctioned · Apr 7, 2015 · N810FD · Airbus A310324 · Altimeter, Barometric/Encoder > AT 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. - [SDR FDEA201503020625](https://openairdocs.org/sdr/FDEA201503020625.md): Seat Track · damaged · Mar 2, 2015 · N810FD · Airbus A310324 · Fuselage, Seat/Cargo Attach Fittings > COMPLY 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. - [SDR FDEA201401210149](https://openairdocs.org/sdr/FDEA201401210149.md): Relay · failed · Jan 21, 2014 · N810FD · Airbus A310324 · Aircraft Fuel Distribution System > DURING 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 TRAPP - [SDR FDEA201310012366](https://openairdocs.org/sdr/FDEA201310012366.md): Smoke Detector · failed · Oct 1, 2013 · N810FD · Airbus A310324 · Smoke Detection > EQUIPMENT 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 COU - [SDR FDEA201309132202](https://openairdocs.org/sdr/FDEA201309132202.md): Fitting · corroded · Sep 13, 2013 · N810FD · Airbus A310324 · Wing, Landing Gear Attach Fittings > RT WING MLG FITTING OF RIB 5 FORWARD LUG CORRODED, COMPLY WITH EA6-5710-T0302341A. - [SDR FDEA201309132201](https://openairdocs.org/sdr/FDEA201309132201.md): Fitting · corroded · Sep 13, 2013 · N810FD · Airbus A310324 · Wing, Landing Gear Attach Fittings > LT WING MLG FITTING OF RIB 5 FORWARD LUG FOUND CORROSION, COMPLY WITH EA 6-5710-T0302340. - [SDR FDEA201206172253](https://openairdocs.org/sdr/FDEA201206172253.md): Hydraulic System · warning message · Jun 17, 2012 · N810FD · Airbus A310324 · Hydraulic System, Main > DURING 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. - [SDR FDEA201203301200](https://openairdocs.org/sdr/FDEA201203301200.md): Hydraulic System · multiple fail · Mar 30, 2012 · N810FD · Airbus A310324 · Hydraulic System, Main > DURING 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 29-11-32-0 - [SDR FDEA201102040472](https://openairdocs.org/sdr/FDEA201102040472.md): Outflow Valve · failed · Feb 4, 2011 · N810FD · Airbus A310324 · Pressure Regulator/Outflow Valve > 1 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 VA - [SDR FDEA200901140199](https://openairdocs.org/sdr/FDEA200901140199.md): Floor Panel · damaged · Jan 14, 2009 · N810FD · Airbus A310324 · Fuselage Floor Panel > FWD 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. - [SDR FDEA200901140198](https://openairdocs.org/sdr/FDEA200901140198.md): Floor Panel · damaged · Jan 14, 2009 · N810FD · Airbus A310324 · Fuselage Floor Panel > FWD 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. - [SDR FDEA200901140197](https://openairdocs.org/sdr/FDEA200901140197.md): Floor Panel · damaged · Jan 14, 2009 · N810FD · Airbus A310324 · Fuselage Floor Panel > FWD 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. - [SDR FDEA200901140196](https://openairdocs.org/sdr/FDEA200901140196.md): Floor Panel · damaged · Jan 14, 2009 · N810FD · Airbus A310324 · Fuselage Floor Panel > MAIN 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. - [SDR FDEA200901140195](https://openairdocs.org/sdr/FDEA200901140195.md): Floor Panel · damaged · Jan 14, 2009 · N810FD · Airbus A310324 · Fuselage Floor Panel > MAIN 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. - [SDR FDEA200901140194](https://openairdocs.org/sdr/FDEA200901140194.md): Floor Panel · damaged · Jan 14, 2009 · N810FD · Airbus A310324 · Fuselage Floor Panel > FWD 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. - [SDR FDEA200901130185](https://openairdocs.org/sdr/FDEA200901130185.md): Floor Panel · damaged · Jan 13, 2009 · N810FD · Airbus A310324 · Fuselage Floor Panel > MAIN DECK CARGO COMPARTMENT ZONE 231, FLOOR PANEL 231VH HAS STRUCTURAL DAMAGES. FABRICATED NEW FLOOR PANEL 231VH PER SAMPLE, ON TRAVELER NR T8 /773390. - [SDR FDEA200901130184](https://openairdocs.org/sdr/FDEA200901130184.md): Floor Panel · damaged · Jan 13, 2009 · N810FD · Airbus A310324 · Fuselage Floor Panel > MAIN 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. - [SDR FDEA200901130183](https://openairdocs.org/sdr/FDEA200901130183.md): Floor Panel · damaged · Jan 13, 2009 · N810FD · Airbus A310324 · Fuselage Floor Panel > MAIN 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. - [SDR FDEA200901130180](https://openairdocs.org/sdr/FDEA200901130180.md): Floor Panel · damaged · Jan 13, 2009 · N810FD · Airbus A310324 · Fuselage Floor Panel > MAIN 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. - [SDR FDEA200901130179](https://openairdocs.org/sdr/FDEA200901130179.md): Floor Panel · damaged · Jan 13, 2009 · N810FD · Airbus A310324 · Fuselage Floor Panel > MAIN 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. - [SDR FDEA200901130178](https://openairdocs.org/sdr/FDEA200901130178.md): Floor Panel · damaged · Jan 13, 2009 · N810FD · Airbus A310324 · Fuselage Floor Panel > MAIN 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. - [SDR FDEA200901130177](https://openairdocs.org/sdr/FDEA200901130177.md): Floor Panel · damaged · Jan 13, 2009 · N810FD · Airbus A310324 · Fuselage Floor Panel > MAIN 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. - [SDR FDEA200901130176](https://openairdocs.org/sdr/FDEA200901130176.md): Floor Panel · damaged · Jan 13, 2009 · N810FD · Airbus A310324 · Fuselage Floor Panel > FWD 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. - [SDR FDEA200901130175](https://openairdocs.org/sdr/FDEA200901130175.md): Floor Panel · damaged · Jan 13, 2009 · N810FD · Airbus A310324 · Fuselage Floor Panel > MAIN 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. - [SDR FDEA200901120167](https://openairdocs.org/sdr/FDEA200901120167.md): Floor Panel · damaged · Jan 12, 2009 · N810FD · Airbus A310324 · Fuselage Floor Panel > FWD 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. - [SDR FDEA200901120166](https://openairdocs.org/sdr/FDEA200901120166.md): Floor Panel · damaged · Jan 12, 2009 · N810FD · Airbus A310324 · Fuselage Floor Panel > MAIN 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/ 773438 - [SDR FDEA200901120165](https://openairdocs.org/sdr/FDEA200901120165.md): Floor Panel · damaged · Jan 12, 2009 · N810FD · Airbus A310324 · Fuselage Floor Panel > MAIN 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. - [SDR FDEA200901120164](https://openairdocs.org/sdr/FDEA200901120164.md): Floor Panel · damaged · Jan 12, 2009 · N810FD · Airbus A310 · Fuselage Floor Panel > MAIN 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. - [SDR FDEA200901120163](https://openairdocs.org/sdr/FDEA200901120163.md): Floor Panel · damaged · Jan 12, 2009 · N810FD · Airbus A310 · Fuselage Floor Panel > MANI 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/ 773454 - [SDR FDEA200901120162](https://openairdocs.org/sdr/FDEA200901120162.md): Floor Panel · damaged · Jan 12, 2009 · N810FD · Airbus A310324 · Fuselage Floor Panel > BULK CARGO COMPARTMENT ZONE 161,FLOOR PANEL 161GF HAS STRUCTURAL DAMAGES. FABRICATED NEW FLOOR PANEL 161GF PER SAMPLE IAW SRZ 25-011. - [SDR FDEA200901120160](https://openairdocs.org/sdr/FDEA200901120160.md): Floor Panel · damaged · Jan 12, 2009 · N810FD · Airbus A310324 · Fuselage Floor Panel > BULK CARGO COMPARTMENT, ZONE 161 FLOOR PANEL 161BF HAS STRUCTURAL DAMAGES. FABRICATED NEW FLOOR PANEL NR 161BF PER SAMPLE, IAW SRZ 25-011 ON TRAVELER. - [SDR FDEA200901120159](https://openairdocs.org/sdr/FDEA200901120159.md): Floor Panel · damaged · Jan 12, 2009 · N810FD · Airbus A310324 · Fuselage Floor Panel > BULK CARGO COMPARTMENT ZONE 162, FLOOR PANEL 162HF HAS STRUCTURAL DAMAGES. FABRICATED NEW FLOOR PANEL 162HF PER SAMPLE IAW SRZ 25-011 ON TRAVELER. - [SDR FDEA200901120156](https://openairdocs.org/sdr/FDEA200901120156.md): Floor Panel · damaged · Jan 12, 2009 · N810FD · Airbus A310324 · Fuselage Floor Panel > AFT 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. - [SDR FDEA200901120151](https://openairdocs.org/sdr/FDEA200901120151.md): Rib · cracked · Jan 12, 2009 · N810FD · Airbus A310324 · Wing, Rib/Bulkhead > LEFT 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. - [SDR FDEA200901020002](https://openairdocs.org/sdr/FDEA200901020002.md): Doubler · damaged · Jan 2, 2009 · N810FD · Airbus A310324 · Fuselage Miscellaneous Structure > THE 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. - [SDR FDEA200812305320](https://openairdocs.org/sdr/FDEA200812305320.md): Floor Panel · cracked · Dec 30, 2008 · N810FD · Airbus A310 · Fuselage Floor Panel > FWD 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. - [SDR FDEA200812245272](https://openairdocs.org/sdr/FDEA200812245272.md): Structure · corroded · Dec 24, 2008 · N810FD · Airbus A310324 · Fuselage Main, Structure > AIR 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. - [SDR FDEA200812185224](https://openairdocs.org/sdr/FDEA200812185224.md): Seat Track · corroded · Dec 18, 2008 · N810FD · Airbus A310324 · Fuselage, Seat/Cargo Attach Fittings > MAIN 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. - [SDR 08FDEA03601](https://openairdocs.org/sdr/08FDEA03601.md): Computer · failed · Aug 26, 2008 · N810FD · Airbus A310324 · Trailing Edge Flap Control System > ON 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 DEFE - [SDR 08FDEA02261](https://openairdocs.org/sdr/08FDEA02261.md): Line · leaking · Jun 13, 2008 · N810FD · Airbus A310324 · Hydraulic System, Main > HYD 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. CR - [SDR 07FDEA01500](https://openairdocs.org/sdr/07FDEA01500.md): Skin · corroded · Apr 13, 2007 · N810FD · Airbus A310324 · Fuselage Main, Plate/Skin > DUE 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, APPROVED - [SDR 07FDEA01499](https://openairdocs.org/sdr/07FDEA01499.md): Shear Tie · cracked · Apr 13, 2007 · N810FD · Airbus A310324 · Fuselage Internal Mounting Structure > FOUND 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 H2 - [SDR 07FDEA01498](https://openairdocs.org/sdr/07FDEA01498.md): Skin Panel · corroded · Apr 13, 2007 · N810FD · Airbus A310324 · Fuselage Main, Plate/Skin > FOUND 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". - [SDR 07FDEA01497](https://openairdocs.org/sdr/07FDEA01497.md): Skin · dented · Apr 13, 2007 · N810FD · Airbus A310324 · Fuselage Main, Plate/Skin > DENT 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". - [SDR 07FDEA01496](https://openairdocs.org/sdr/07FDEA01496.md): Vane · chafed · Apr 13, 2007 · N810FD · Airbus A310324 · Trailing Edge Flaps > CHAFING 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". - [SDR 07FDEA01495](https://openairdocs.org/sdr/07FDEA01495.md): Bulkhead · damaged · Apr 13, 2007 · N810FD · Airbus A310324 · Fuselage Main, Bulkhead > SCRATCH 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". - [SDR 07FDEA01494](https://openairdocs.org/sdr/07FDEA01494.md): Skin · corroded · Apr 13, 2007 · N810FD · Airbus A310324 · APU Cowling/Containment > CORROSION 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". Next page: https://openairdocs.org/deregistered/N810FD-2024-03-02/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 = 'N810FD' AND deregistration_id = 'N810FD-2024-03-02' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N810FD-2024-03-02/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.