Airbus A310-324

Service difficulty reports · 1,439

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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 aircraft_model_key = 'A310324'
  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 FDEA201010194111Skin · dentedLT SIDE FUSELAGE SKIN BETWEEN FRAMES 73 TO 73A AND BETWEEN STRINGERS 29 TO 31 LT HAS A DENT AND CREASE MEASURING 9 IN X 305 IN AND .019 IN DEEP. ALSO THE DENT CROSSED OVER STRINGER 30 LT. EVALUATED DAMAGE AND FOUND DENT BETWEEN FR 73 AND 73A AND BETWEEN STROct 19, 2010 · N815FD · Airbus A310324 · Fuselage Main, Plate/SkinSDR FDEA201010194103Warning Message · false indicationON TAKEOFF ROLL APPROX 80 KTS GOT ECAM WARNING FOR PITCH FEEL SYS 1 AND 2 AND RUDDER TRAVEL SYS 1 AND 2 FAULTS. ALL 4 LIGHTS WERE ILLUMINATED ON OVHD PANEL. ABORTED TAKEOFF, COMPLETED APPROPRIATE CHECKLISTS AND RETURNED TO BLOCKS. ACCOMPLISHED AFS/LAND TEOct 19, 2010 · N809FD · Airbus A310324 · Central WarningSDR 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 FDEA201010093981Damper · leakingLANDING GEAR WOULD NOT RETRACT ON DEPARTURE, RETURNED TO RPVM, HAD LANDING GEAR RETRACTION FAULT PROX. DETECTION BOX FAULTED TO "BR" - BOGIE RIGHT FAIL. ON INSPECTION RT MAIN GEAR, FOUND PITCH DAMPER BUTTON POPPED OUT. FAILED RETRACTION ON BOTH SYSTEMS. COct 9, 2010 · N804FD · Airbus A310324 · Landing Gear Retraction/Extension SystemSDR FDEA201010073974Selector Valve · failedLOWERED MLG HANDLE (WITH SYS 2, POSITION DET SELECTED) GOT UNLOCK LIGHTS BUT NO MLG DOWN, SELECTED SYS 1, NO CHANGE, RAISED MLG HANDLE, LIGHTS WENT OUT, LOWERED MLG AGAIN IN SYS 2, AND MLG CAME DOWN NORMALLY. BITE ON PROX BOX, NO FAULT REGISTERED, FOLLOWED TSOct 7, 2010 · N804FD · Airbus A310324 · Landing Gear Retraction/Extension SystemSDR FDEA201010063954Door · damagedCLIMING OUT, PASSING 15,000' RECEIVED VIBRATION IN AIRFRAME THAT BEGAN GRADUAL AND INCREASED WITH INCREASE IN AIRSPEED. VIBRATION SEEMED TO BE AT PILOTS POSITION OR FWD. VIBATION DECREASED WITH RECREASE IN AIRSPEED. IT WAS GONE AT 250 KTS AND BELOW. ACFT IOct 6, 2010 · N814FD · Airbus A310324 · Service DoorsSDR FDEA201009303820Pickup · malfunctionedON FINAL APPROACH, WHEN FLAPS WERE SELECTED TO 40 DEG RECEIVED ECAM. FLAPS STUCK. ALSO RECEIVED SYS 1 AND 2 FAULT LIGHT ON OVERHEAD PANEL. FLAPS STUCK BETWEEN 20 DEG -40 DEG. COMPLIED WITH QRH AND ECAM. REPLACED LT APPU 29CV PER AMM 27-56-11-04. PERFORMED OSep 30, 2010 · N809FD · Airbus A310324 · Trailing Flap Position Indicating SystemSDR FDEA201009303819Filter · leakingDURING DESCENT RECEIVED ECAM GREEN HYD SYS LOW LEVEL WARNING. HYD QTY ON OVERHEAD PANEL INDICATED ZERO. CONSULTED THE QRH AND MANUALLY EXTENDED THE LANDING GEAR. FOUND HYD LEAKAGE CAME FROM THE GREEN SERVO CONTRO FILTER. REMOVED AND REPLACED THE PUMP DELIVSep 30, 2010 · N811FD · Airbus A310324 · Hydraulic System, MainSDR 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 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 FDEA201009263716Computer · malfunctionedON TAKEOFF ROLL, MASTER WARNING REPETITIVE CHIME, AT APPROX 130 KTS RTO. ECAM SHOWED PITCH TRIM 2 YD 2 OFF. PITCH TRIM 2 YD 2 BOTH RESET OK. BRAKE 3 670 DEGREES. WHILE WAITING FOR HOT BRAKES TO COOL, FUEL WENT BELOW RQR FOR FOR TO. SO RETURN TO GATE, OSep 26, 2010 · N812FD · Airbus A310324 · Fuel Indicating SystemSDR FDEA201009263715Connector · dirtyCLIMBING THROUGH FL330 GOT RT R1 DOOR NOT CLOSED COMPLIED WITH QRH AND DESCENTED BELOW 10,000. GOING THROUGH FL200 THE WARNING WENT AWAY. ATC WOULD NOT LET US CONTINUE AT 10,000 SO RETURNED TO DEPARTURE. CABIN PRESSURE WAS GOOD. ALL NORMAL, CLEANED THE CONSep 26, 2010 · N804FD · Airbus A310324 · Electrical Power System WiringSDR 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 FDEA201009203584Actuator · malfunctionedON FINAL TO 15L ICN SELECTING FLAPS 40 HAD AMBER SPOILER 5 FAULT, REPEAT HAPPENED 2 TIMES. DID MISSED APPROACH AND WHILE DOING QRH PROCEDURE ACFT COMMANDED 15 DEG LT TURN WITH CONTROL WHEEL. SELECTED FLIGHT CONTROLS AND NOTED SPOILERS LT 5,6,7 WERE ALL UP Sep 20, 2010 · N811FD · Airbus A310324 · Drag Control ActuatorSDR 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 PanelSDR FDEA201009143411Floor Panel · crackedMAIN CABIN FLOOR PANEL 241 PK IS CRACKED. FABRICATED NEW FLOOR PANEL, POTTED EDGES, INSTALLED INSERTS, APPLIED ANTI-SKID AND PART MARKED IAW DWG SRZ 25-005, REV "H".Sep 14, 2010 · N803FD · Airbus A310324 · Fuselage Floor PanelSDR FDEA201009143410Floor Panel · crackedMAIN CABIN FLOOR PANEL 241 ZJ 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 PanelSDR FDEA201009143409Floor Panel · crackedMAIN CABIN FLOOR PANEL 232 MH 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 PanelSDR FDEA201009143408Floor Panel · crackedMAIN CABIN FLOOR PANEL 252 BH HAS AN EAR CRACKED OFF THE AFT END OF THE PANEL. FABBED NEW FLOOR PANEL, POTTED EDGES AND INSTALLED INSERTS IAW DWG SRZ 25-005, REV "H".Sep 14, 2010 · N803FD · Airbus A310324 · Fuselage Floor PanelSDR FDEA201009143407Floor Panel · crackedMAIN CABIN FLOOR PANEL 251 PH IS CRACKED ON THE BOTTOM SIDE. 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 FDEA201009143406Floor Panel · crackedMAIN CABIN FLOOR PANEL 251 EH HAS A CRACKED CORNER. 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 FDEA201009143405Floor Panel · crackedMAIN CABIN FLOOR PANEL 252 BG 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 PanelSDR FDEA201009143404Panel · dentedBULK PIT SIDEWALL PANEL 161 GW IS DENTED. FABRICATED NEW FLOOR PANEL, POTTED EDGES AND INSTALLED INSERTS IAW DWG SRZ 25-005, REV "H". TRIMMED AND BONDED METAL PLATE IAW DWG SRZ 25-011, REV "C".Sep 14, 2010 · N803FD · Airbus A310324 · Fuselage Miscellaneous StructureSDR FDEA201009143403Floor Panel · delaminatedBULK PIT FLOOR PANEL 162 HF IS DELAMINATED. FABRICATED NEW FLOOR PANEL, POTTED EDGES AND INSTALLED INSERTS IAW DWG SRZ 25-005, REV "H". TRIMED AND BONDED A METAL PLATE IAW DWG SRZ 25-011, REV "C".Sep 14, 2010 · N803FD · Airbus A310324 · Fuselage Floor PanelSDR FDEA201009143402Floor Panel · delaminatedBULK PIT FLOOR PANEL 161 AF IS DELAMINATED. FABRICATED NEW PANEL, POTTED EDGES AND INSTALLED INSERTS IAW DWG SRZ 25-005, REV "H". FABRICATED, TRIMED AND BONDED A METAL PLATE IAW DWG SRZ 25-011, REV "C".Sep 14, 2010 · N803FD · Airbus A310324 · Fuselage Floor PanelSDR FDEA201009143401Floor Panel · delaminatedBULK PIT FLOOR PANEL 161 HF IS DELAMINATED. FABRICATED NEW FLOOR PANEL, POTTED EDGES AND INSTALLED INSERTS IAW DWG SRZ 25-005, REV "H". TRIMMED AND BONDED METAL PLATE IAW DWG SRZ 25-011, REV "C".Sep 14, 2010 · N803FD · Airbus A310324 · Fuselage Floor PanelSDR FDEA201009143400Panel · delaminatedAFT PIT CEILING PANEL 152 DC IS DELAMINATED. REPAIRED AFT PIT CEILING PANEL BY REMOVING THE METAL DOUBLER DAMAGE, FIBERGLASS DAMAGE ON THE EXTERIOR AND INNER SURFACE, CLEANING, FABRICATING METAL DOUBLER, PREPPING AREA TO BOND METAL AND FIBERGLASS REPAIR PLIESSep 14, 2010 · N803FD · Airbus A310324 · Fuselage Miscellaneous StructureSDR FDEA201009143399Floor Panel · delaminatedAFT PIT FLOOR PANEL 152 BF IS DELAMINATED. FABRICATED NEW FLOOR PANEL, IAW DWG SRZ 25-005, REV "H". POTTED EDGES AND INSTALLED INSERTS IAW DWG SRZ 25-005, REV "H".Sep 14, 2010 · N803FD · Airbus A310324 · Fuselage Floor PanelSDR FDEA201009143398Floor Panel · delaminatedAFT PIT FLOOR PANEL 152 DF 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 FDEA201009143396Floor Panel · crackedFWD CARGO COMPARTMENT FLOOR PANEL 132 RF IS CRACKED AND HAS EDGE DAMAGE IN NUMEROUS PLACES. 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 FDEA201009143395Floor Panel · puncturedBULK PIT FLOOR PANEL 161 BF IS PUNCTURED. FABRICATED NEW FLOOR PANEL, POTTED EDGES AND INSTALLED INSERTS IAW DWG SRZ 25-005, REV "H". TRIMMED AND INSTALLED METAL PLATE IAW DWG SRZ 25-011, REV, "C"Sep 14, 2010 · N803FD · Airbus A310324 · Fuselage Floor Panel
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