N803FD, cancelled Mar 2, 2024

Service difficulty reports · 205

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 = 'N803FD' AND deregistration_id = 'N803FD-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 FDEA201706291786Actuator · failedDURING CLIMB. RIGHT OUTER TANK DECREASEED TO 3.32 LBS AND RIGHT INNER INCREASEDTO 14.4. LEFT OUTER WAS 6.13 & LEFT INNER WAS 11.91. WAS ABLE TO STOP R/O DECREASE BY TRINING OFF R/O PUMPS., BUT RIGHT INNER DID NOT DECREASE. AT 37000 LEVEL OFF L/O 6.16 L/IJun 29, 2017 · N803FD · Airbus A310 · Aircraft Fuel Distribution SystemSDR FDEA201706201716Pitot Tube · obstructedDURING TAKEOFF, FIRST OFFICER`S AIRSPEED TAPE SHOWED BETWEEN 40 - 45 KNTS, WITH CAPTAIN`S AIRSPEED TAPE AND STANDBY AIRSPEED BETWEEN 100 - 110 KNTS. ABORTED SHORTLY THERE AFTER. PERFORMED RTO CHECK LIST, NO OTHER DESCRPENCIES NOTED. INSPECTED THE FIRSTJun 20, 2017 · N803FD · Airbus A310324 · Pitot/Static SystemSDR FDEA201701170209Jackscrew · fluid lossSLATS 1 AND 2 FAULTED OFF DURING SLATS EXTENSION. SLATS REMAINED AT THE RETRACT POSITION AND DID NOT MOVE WHEN THE HANDLE WAS RECYCLED. COMPLIED WITH QRH AND LANDED WITH SLATS RETRACTED AND FLAPS 40. FOUND RIGHT WING INBOARD JACKSCREW EMPTY OF FLUID, REMOJan 17, 2017 · N803FD · Airbus A310324 · Leading Edge Slat Control SystemSDR FDEA201701160199Computer · failedDURING APPROACH WHEN EXTENDING SLATS, NO MOVEMENT. CYCLED, RAN QRH, LANDED WITH SLATS UP AND FLAPS 40. REMOVED & REPLACED BOTH NR 1 & 2 SFCC'S IAW AMM 27-51-18-04 & BOTH OPS CHECKED GOOD IAW AMM 27-51-00-05.Jan 16, 2017 · N803FD · Airbus A310324 · Leading Edge Slat Control SystemSDR FDEA201511213745Flap · stuckFLAP SYS 1 & 2 FAULT, FLAPS STUCK. REMOVED TWO BOLTS FROM RT TORQUE LIMITED COUPLER TO FOM. DRAINED FLUID FROM RT WING NR 1 FLAP DRIVE GEAR BOX FOR INSPECTION PURPOSE. GPS OVERRIDE SWITCH IN COCKPIT, CAPTAINS RIGHT KNEE, REQUIRES SAFETY. FOUND JAM FAULTS ONov 21, 2015 · N803FD · Airbus A310324 · Trailing Edge Flap Control SystemSDR FDEA201508252695Stringer · damagedREMOVED STRINGER 44 AT FRAME 19 - 20 TO FOM. REMOVED SHEAR TIE & COUPLING. COUPLING & STRINGER FOUND TO BE DAMAGED. FABRICATED NEW STRINGER ON T15 1157203. RECEIVED NEW COUPLING, INSTALLED SHEAR TIE, COUPLING & STRINGER 44 AT FRAME 19 - 20 IAW SRM 51-40-21Aug 25, 2015 · N803FD · Airbus A310324 · Fuselage Main, Longeron/StringerSDR FDEA201506181846Crossbeam · corrodedBULK CARGO FRAME 67 -Y-940, CROSSBEAM WITH INNER GRANULAR CORROSION. REPLACED THE CORRODED CROSSBEAM OF BULK CARGO IAW SRM 51-40-21. THIS REPAIR CATEGORY A, MAJOR REPAIR IAW GMM6-2-100.Jun 18, 2015 · N803FD · Airbus A310324 · Fuselage Miscellaneous StructureSDR FDEA201506151817Repair · delaminatedAGEING INSPECTION, EXISTING REPAIR ON RT OUTER FLAP, UPPER SKIN OUT OF RIB 10 REQUIRES EVALUATION FOR CONFORMITY. THE EXISTING REPAIR WAS EVALUATED & FOUND IN CONFORMITY WITH APPROVED DATA. BUT INSPECTION FOUND DELAMINATION ON OLD REPAIR. REPAIRED THE DAMAGJun 15, 2015 · N803FD · Airbus A310324 · Trailing Edge FlapsSDR FDEA201506151816Repair · delaminatedAGEING INSPECTION, EXISTING REPAIR ON RT OUTER FLAP, UPPER SKIN OUT OF RIB 10 REQUIRES EVALUATION FOR CONFORMITY. THE EXISTING REPAIR WAS EVALUATED & FOUND IN CONFORMITY WITH APPROVED DATA. BUT INSPECTION FOUND DELAMINATION ON OLD REPAIR. REPAIRED THE DAMAGJun 15, 2015 · N803FD · Airbus A310324 · Trailing Edge FlapsSDR FDEA201506151815Skin · delaminatedAGEING INSPECTION, EXISTING REPAIR ON RT OUTER FLAP UPPER SKIN OUT OF RIB 10 REQUIRES EVALUATION FOR CONFORMITY. THE EXISTING REPAIR WAS EVALUATED & FOUND IN CONFORMITY WITH APPROVED DATA. BUT INSPECTION FOUND DELAMINATION ON OLD REPAIR. REPAIRED THE DAMAGEJun 15, 2015 · N803FD · Airbus A310324 · Trailing Edge FlapsSDR FDEA201506151812Skin · crackedRIGHT WING FIXED TE LOWER SKIN AT RIBS 11 - 12 CRACKED 1 INCH. REPAIRED IAW EA 6-5730-T0318078 & R57249152. MAJOR REPAIR IAW GMM 6-2-100.Jun 15, 2015 · N803FD · Airbus A310324 · Wing, Plate/SkinSDR FDEA201506101748Floor Support · crackedMAIN DECK CARGO FRAME 15A Y1456 FLOOR SUPPORT CRACKED APPROX 1.0 INCH IN LENGTH. REPAIRED IAW SRM 53-12-15-201 PARA 5G. MAJOR REPAIR IAW GMM6-2-100.Jun 10, 2015 · N803FD · Airbus A310200 · Fuselage Miscellaneous StructureSDR FDEA201407171832Windshield · crackedEN ROUTE LT WINDOW HEAT FAULT, FOLLOWED BY WINDSHIELD CRACKING. NUMEROUS CRACKS IN LOWER RT CORNER. QRH FOLLOWED, DIVERTED. REMOVED L1 WINDSHIELD IAW MM 56-11-11-04.Jul 17, 2014 · N803FD · Airbus A310324 · Flight Compartment WindowsSDR FDEA201405090992Thrust Reverser · damagedNUMBER 1 ENG THRUST REVERSER OTBD TRANSLATING SLEEVE AFT 8 INCHES IS MISSING TOP TO BOTTOM, WHITE COWL. ALL COCKPIT THRUST REVERSER LIGHTS EXTINGUISHED, NORMAL. NR 1 ENG OIL SERVICE DOOR WAS OPEN & BOTTOM HINGE PIN MISSING. INNER BARREL MESH IS MISSING & May 9, 2014 · N803FD · Airbus A310324 · Engine Thrust ReverserSDR FDEA201403190525Sensor · malfunctionedDURING CRUISE FLIGHT, NR 2 RT ENGINE OIL TEMP BEGAN TO FLUCTUATE FROM NORMAL CRUISE TEMP OF 116C UP TO 230C. STAYED ABOVE 160C FOR MORE THAN 9 MINUTES BUT CONTINUED TO FLUCTUATE BETWEEN NORMAL & A HIGH OF 230 C. FINALLY TEMP STAYED ABOVE 160 C FOR MORE THAMar 19, 2014 · N803FD · Airbus A310324 · Engine Oil Indicating SystemSDR FDEA201401230181Computer · malfunctionedDURING TAKEOFF, TOGA WOULD NOT ENGAGE. NO OTHER WARNINGS, COULD MANUALLY ADVANCE THROTTLES WITH NO RESTRICTIONS. REMOVED AND REPLACED TCC COMPUTOR IAW AMM 22-36-34-04-01 AND REPFORMED A AFS/LAND TEST. ALL SYSTEM TESTED NORMAL.Jan 23, 2014 · N803FD · Airbus A310324 · Auto Throttle SystemSDR FDEA201303030491Floorboard · delaminatedAFT CARGO BAY FLOORBOARD BETWEEN 1R AND 2R RAIL TRACKS, 2 FEET FWD OF BALL MAT HAS 24"OF DELAMINATION. FLOORBOARD WAS DAMAGED BEYOND ECONOMICAL REPAIR. FABRICATED A REPLACEMENT FLOORBOARD IAW DWG SRZ-25-005, REV J.Mar 3, 2013 · N803FD · Airbus A310324 · Fuselage Floor PanelSDR FDEA201302270475Ferrule · crackedNR 2 PYLON FERRULE IS CRACKED COMPLIED WITH EA 6-5450-T0300139 REV NR PS P1 - NACELLES/PYLON PRECOOLER FERRULE CRACK ON NR 2 PYLON REF WR 54-50 6954.Feb 27, 2013 · N803FD · Airbus A310324 · Nacelle/Pylon, Main FrameSDR FDEA201302190374Frame · corrodedFUSELAGE AFT PRESSURE BULKHEAD FWD FACE LWR RIM FR 80/82 HAS 3 EA AREAS OF EXFOLIATED CORROSION & 1 EA AREA OF CORROSION EXTENDING INTO THE CLEAT PROFILE. DEFECT MEASURES 15"SQ. AFTER REMOVAL OF LEVEL 1 CORROSION, FOUND ANGLES TO BE OUT OF LIMITS IAW SRMFeb 19, 2013 · N803FD · Airbus A310324 · Fuselage Main, FrameSDR FDEA201302080306Skin · dentedRT WING OTBD FLAP L/E APPROX WING RIB 25 HAS A DENT WITH FIELD REPAIR APPROX 1.5 X 1.5 X .200D. CUT OUT DAMAGED AREA. FABRICATED, HEAT TREATED, LOCATE AND DRILLED REPAIR PARTS IAW SRM 57-53-12, FIG 213. PROTECTED REPAIR PARTS AND THE CUT OUT AREA ON RT FLAPFeb 8, 2013 · N803FD · Airbus A310324 · Trailing Edge FlapsSDR FDEA201302060288Floorboard · delaminatedMLG BAY LT AFT WALKWAY PANEL 148 BF HAS 60 SQ" AREA OF DELAMINATION. FABRICATED REPLACEMENT PANEL 148 BF IAW DWG SRZ 25-005, REV J.Feb 6, 2013 · N803FD · Airbus A310324 · Fuselage Floor PanelSDR FDEA201012204727Power Supply · failedEMERGENCY LIGHTS FAIL OPS CHECK FROM COURIER AREA TEST SWITCH. R & R THE POWER SUPPLY UNIT AND BATTERY IAW AMM 33-51-14-04. PERFORMED A SATISFACTORY TEST OF THE EMERGENCY LIGHTS IAW AMM 33-51-14-04.Dec 20, 2010 · N803FD · Airbus A310324 · Emergency LightingSDR FDEA201012164699Rib · damagedLT WING T/E RIB AT WIAX 62.70 HAS EDGE DAMAGE ON THE SPAR ATTACH FLANGE. REMOVED DAMAGE FROM THE SPAR AREA IAW EA 6-5730-136705.Dec 16, 2010 · N803FD · Airbus A310324 · Wing, Rib/BulkheadSDR FDEA201011044253Support · crackedRT WING ALL SPEED AILERON ACTUATOR UPPER PANEL SUPPORT IS CRACKED ON THE OTBD SIDE. PARTIALLY REMOVED OTBD UPPER AILERON PANEL AND REMOVED CRACKED LANDING. INSTALLED NEW PANEL LANDING PN A5724275920300, PO 691739.5 AND RE-INSTALLED OTBD UPPER AILERON PANELNov 4, 2010 · N803FD · Airbus A310222 · Wing Miscellaneous StructureSDR FDEA201010254167Fairing · crackedNR 1 PYLON INBD APRON FAIRING SKIN IS CRACKED. INSTALLED REPAIR DOUBLER ON THE NR1 PYLON INBD APRON FAIRING IN REF TO SRM 54-56-10, FIG 201.Oct 25, 2010 · N803FD · Airbus A310324 · Nacelle/Pylon Miscellaneous StructureSDR FDEA201010144081Skin · gougedLEFT HORIZONTAL STAB LOWER EXTERIOR SKIN IS GOUGED AT THE FUEL ACCESS PANEL 333 FB CUTOUT. SMOOTHED AREA. ORIGINAL 0.268. REMAINING 207. FOUND IN LIMITS IAW EA 6-510-136714 REV "A"; HORIZONTAL STABILIZER - LOWER PANEL GOUGED AROUND ACCESS HOLE BETWEEN RIB Oct 14, 2010 · N803FD · Airbus A310324 · Horizontal Stabilizer, Plate/SkinSDR FDEA201010134042Support · crackedFUSELAGE UNDER THE LT AIR CONDITIONING AFT FAIRING THE AFT INBD EXHAUST SHIELD SUPPORT IS CRACKED. REMOVED SUPPORT BRACKET IAW SRM 51-40-21. RECEIVED NEW SUPPORT BRACKET FROM STORES, PO 693873.1. INSTALLED NEW BRACKET IAW SRM 51-72-10, PAGES 1-3.Oct 13, 2010 · N803FD · Airbus A310324 · Fuselage Miscellaneous StructureSDR FDEA201010124021Floor Panel · delaminatedAIR CONDITIONING COMPARTMENT FLOOR PANEL 143 DF HAS A LARGE CORNER THAT IS DELAMINATED AND CONTAMINATED. FABRICATED NEW AIR CONDITIONING COMPARTMENT FLOOR PANEL 143 DF IAW DWG SRZ 25-005, REV "H".Oct 12, 2010 · N803FD · Airbus A310324 · Fuselage Floor PanelSDR FDEA201009303818Sleeve · crackedNR 2 ENG RT THRUST REVERSER SLEEVE IS CRACKED AND DAMAGED JUST BELOW THE NR 6 BLOCKER DOOR. REPAIRED NR 2 THRUST REVERSER JUST BELOW THE NR 6 BLOCKED DOOR BY CLEANING EXISTING POTTING AND RE-POTTING DAMAGED AREA AND CURING IAW SRM 54-05- 01, PARA 9.Sep 30, 2010 · N803FD · Airbus A310324 · Engine Thrust ReverserSDR FDEA201009273750Floor Panel · crackedMAIN CABIN FLOOR PANEL NR232 RG HAS THE FWD RT EAR CRACKED. FABRICATED NEW PANEL, POTTED EDGES AND INSTALLED INSERTS IAW DWG SRZ 25-005, REV "H".Sep 27, 2010 · N803FD · Airbus A310324 · Fuselage Floor PanelSDR FDEA201009273746Floorboard · crackedMAIN DECK FLOORBOARD 242 BR IS CRACKED AT FRAME 39. FABRICATED NEW FLOORBOARD, POTTED EDGES, INSTALLED INSERTS, APPLIED ANTI-SKID AND PART MARKED IAW DWG SRZ 25-005, REV "H".Sep 27, 2010 · N803FD · Airbus A310324 · Fuselage Floor PanelSDR FDEA201009273743Floor Panel · crackedMAIN CABIN FLOOR PANEL 222 CF IS CRACKED ACROSS THE BOTTOM. FABRICATED NEW FLOOR PANEL, POTTED EDGES AND INSTALLED INSERTS IAW DWG SRZ 25-005, REV "H".Sep 27, 2010 · N803FD · Airbus A310324 · Fuselage Floor PanelSDR FDEA201009273749Floor Panel · damagedMAIN CABIN FLOOR PANEL NR251 RG IS CRUSHED FROM APPROX FRAME 60 - FRAME 62; LBL 60. FABRICATED NEW FLOOR PANEL, POTTED EDGES AND INSTALLED INSERTS IAW DWG SRZ 25-005, REV "H".Sep 27, 2010 · N803FD · Airbus A310324 · Fuselage Floor PanelSDR FDEA201009273748Floor Panel · crackedMAIN CABIN FLOOR PANEL NR261 LF IS CRACKED FROM FRAME 74 - FRAME 75; LBL 12. FABRICATED NEW FLOOR BOARD, POTTED EDGES AND INSTALLED INSERTS IAW DWG SRZ 25-005, REV "H".Sep 27, 2010 · N803FD · Airbus A310324 · Fuselage Floor PanelSDR FDEA201009273745Floor Panel · crackedFUSELAGE INTERNAL STRUCTURE, MAIN DECK FLOOR PANEL 242 QF IS CRACKED FROM FRAME 47 TO FRAME 51. FABRICATED NEW FLOOR PANEL, POTTED EDGES AND INSTALLED INSERTS IAW DWG SRZ 25-005, REV "H".Sep 27, 2010 · N803FD · Airbus A310324 · Fuselage Floor PanelSDR FDEA201009273744Floor Panel · crackedFUSELAGE INTERNAL STRUCTURE, MAIN DECK FLOOR PANEL 241 PG IS CRACKED FROM FRAME 53 TO FRAME 54. FABRICATED NEW FLOOR PANEL, POTTED EDGES AND INSTALLED INSERTS IAW DWG SRZ 25-005, REV "H".Sep 27, 2010 · N803FD · Airbus A310324 · Fuselage Floor PanelSDR FDEA201009273739Skin · dentedLOWER FUSELAGE LEFT EXTERNAL SURFACE IS DENTED BETWEEN FRAME 38.2 & FRAME 39; STRINGER 35-36L. CUT OUT DENT, FABRICATED DOUBLER, DRILLED , DEBURRED, ALODINED, PRIMED INSTALLED AND SEALED IAW SRM 53-10-12, 51-21-10 & 51-40-21.Sep 27, 2010 · N803FD · Airbus A310222 · Fuselage Main, Plate/SkinSDR FDEA201009273747Floorboard · crackedMAIN DECK FLOORBOARD NR 241 YF IS CRACKED AT FRAME 54. FABRICATED NEW FLOORBOARD, POTTED EDGES AND INSTALLED INSERTS IAW DWG SRZ 25-005, REV "H".Sep 27, 2010 · N803FD · Airbus A310324 · Fuselage Floor PanelSDR FDEA201009213600Seat Track · gougedSEAT TRACK AT FRAME 54, RBL 48 HAS SCALLOPS GOUGED OUT OF LIMITS. R & R SEAT TRACK IAW SRM 53-10-15, FIG 201.Sep 21, 2010 · N803FD · Airbus A310324 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201009173529Skin · corrodedRT WING TOP SKIN SURFACE FRONT SPAR AREA SKIN IS CORRODED FROM RIB 17 - RIB 18. REMOVED 5 EA FASTENERS RT WING TOP SKIN UPPER SURFACE FRONT SPAR BETWEEN RIB 17 AND RIB 18. BLENDED CORROSION IAW SRM 51-74-10. FOUND TO BE WITHIN LIMITS IAW SRM 57-20-12, PGS 13Sep 17, 2010 · N803FD · Airbus A310324 · Wing, Plate/SkinSDR FDEA201009173528Skin · corrodedLT WING TOP SKIN SURFACE IS CORRODED AT THE REAR SPAR AREA FROM RIB 4 - RIB 5. REMOVED 2 EA FASTENERS LT WING TOP SKIN UPPER SURFACE REAR SPAR BETWEEN RIB 17 AND RIB 18 IAW SRM 51-40-21. BLENDED CORROSION IAW SRM 51-74-10. FOUND TO BE WITHIN LIMITS IAW SRM Sep 17, 2010 · N803FD · Airbus A310324 · Wing, Plate/SkinSDR FDEA201009173527Skin · corrodedLT WING TOP SKIN SURFACE IS CORRODED 2 EA PLACES AT THE REAR SPAR AREA FROM RIB 12 - RIB 13. REMOVED CORROSION IAW SRM 57-00-00, PG 212 AT THE LT WING TOP SKIN UPPER SURFACE T/E BETWEEN RIBS 12-13. FOUND TO BE WITHIN LIMITS IAW SRM 57-20-12, PGS 9 & 111. Sep 17, 2010 · N803FD · Airbus A310324 · Wing, Plate/SkinSDR FDEA201009173525Skin · corrodedLT WING TOP SKIN SURFACE IS CORRODED AT THE REAR SPAR AREA FROM RIB 15-RIB 16. REMOVED CORROSION ; LT WING TOP SKIN T/E AREA BETWEEN RIBS 15-16 IAW SRM 57-20-12, PG 9. FOUND TO BE WITHIN LIMITS IAW SRM 57-20-12, PGS 9 & 111. TOOL T8285D. FLAP PEENED AREA IASep 17, 2010 · N803FD · Airbus A310324 · Wing, Plate/SkinSDR FDEA201009163505Skin · corrodedRT WING TOP SKIN UPPER SURFACE, SKIN IS CORRODED FROM RIB 10 TO RIB 11. REMOVED FASTENER RT WING TOP SKIN UPPER SURFACE REAR SPAR BETWEEN RIB 10 AND RIB 11. BLENDED CORROSION IAW SRM 51-74-10. FOUND TO BE WITHIN LIMITS IAW SRM 57-20-12, PGS 13 & 110. FLAP Sep 16, 2010 · N803FD · Airbus A310324 · Wing, Plate/SkinSDR FDEA201009163504Skin · corrodedRT WING TOP SKIN UPPER SURFACE, REAR SPAR AREA SKIN IS CORRODED FROM RIB 4 TO RIB 5. REMOVED 2 EA FASTENERS RT WING TOP SKIN UPPER SURFACE AT REAR SPAR IAW SRM 51-40-21. BLENDED CORROSION IA SRM 51-74-10. FOUND TO BE WITHIN LIMITS IAW SRM 57-20-12, PGS 13 &Sep 16, 2010 · N803FD · Airbus A310324 · Wing, Plate/SkinSDR FDEA201009163503Skin · corrodedRT WING TOP SKIN UPPER SURFACE, REAR SPAR AREA SKIN IS CORRODED FROM RIB 23 TO RIB 24. REMOVED FASTENER RIGHT WING TOP SKIN UPPER SURFACE REAR SPAR BETWEEN RIB 23 AND RIB 24. BLENDED CORROSION IAW A310-300 SRM 51-74-10. FOUND TO BE WITHIN LIMITS IAW SRM 5Sep 16, 2010 · N803FD · Airbus A310324 · Wing, Plate/SkinSDR FDEA201009163502Skin · crackedLT WING BOTTOM SKIN LOWER SURFACE T/E AREA SKIN IS CRACKED FROM RIB 11 TO RIB 12. COMPLIED WITH EA 6-5730-136705.Sep 16, 2010 · N803FD · Airbus A310324 · Wing, Plate/SkinSDR FDEA201009143397Floor Panel · delaminatedAFT PIT FLOOR PANEL 152 AF IS DELAMINATED. FABRICATED NEW FLOOR PANEL, POTTED EDGES AND INSTALLED INSERTS IAW DWG SRZ 25-005, REV "H".Sep 14, 2010 · N803FD · Airbus A310324 · Fuselage Floor PanelSDR FDEA201009143413Floor Panel · puncturedMAIN CABIN FLOOR PANEL 231 QG IS PUNCTURED ON THE TOP SURFACE. FABRICATED NEW FLOOR PANEL, POTTED EDGES AND INSTALLED INSERTS IAW DWG SRZ 25-005, REV "H".Sep 14, 2010 · N803FD · Airbus A310324 · Fuselage Floor PanelSDR FDEA201009143412Floor Panel · crackedMAIN CABIN FLOOR PANEL 231 LG IS CRACKED. FABRICATED NEW FLOOR PANEL, POTTED EDGES AND INSTALLED INSERTS IAW DWG SRZ 25-005, REV "H".Sep 14, 2010 · N803FD · Airbus A310324 · Fuselage Floor Panel
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