Airbus A310-203

Service difficulty reports · 2,392

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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 = 'A310203'
  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 FDEA201207122560Shock Absorber · gougedLEFT MLG THRU HOLE FOR BOGIE BEAM PIN STRUT SIDE, LT INBD BUSHING GOUGED IN SEVERAL PLACES. DEEPEST GOUGE MEASURES .014" WITH MECHANICAL GAGE COMPLIED WITH EA 6-3210-160132 LANDING GEAR LT MLG BOGIE BEAM BUSH DAMAGE. ADDITIONAL WORK COMPLIED ON N00960.Jul 12, 2012 · N403FE · Airbus A310203 · Main Landing Gear Strut/Axle/TruckSDR FDEA201207122557Web · crackedNR 2 ENGINE PYLON OTBD LATERAL PANEL BETWEEN RIB 6 -7 HAS TWO CRACKS BOTH MEASURE .75 OF AN INCH. STOP DRILLED CRACKS IAW SRM 54-52-31, PG 212, 213, 214 CONFIG 1 INSTALLED. REPAIR DOUBLER IAW A310-200, 54-52-31, PG 215.Jul 12, 2012 · N403FE · Airbus A310203 · Nacelle/Pylon Miscellaneous StructureSDR FDEA201207032461Floorbeam · misrepairedFLOORBEAM MISREPAIRED. REPAIRED IAW EA 6-5310-161396 COMPLING WITH PART 1 OF EA AND RDAS REF 70563824/003/2012 ISSUE A. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.Jul 3, 2012 · N403FE · Airbus A310203 · Fuselage Main, Floor BeamSDR FDEA201207032460Floorbeam · failedMAIN CABIN FLOORBEAM MISREPAIRED. REPAIRED IAW EA 6-5310-161396 COMPLING WITH PART 2 OF EA AND RDAS REF 70563824/003/2012 ISSUE A. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.Jul 3, 2012 · N403FE · Airbus A310203 · Fuselage Main, Floor BeamSDR FDEA201206272367Frame · damagedFRAME 24 AT STRINGER 13R WAS FOUND WITH VISIBLE DISTORTION TO UNDERLYING FRAME SPLICES. FOUND FRAME SECTION DAMAGE BEYOND ECONOMICAL REPAIR AND R & R FRAME SECTIONS BETWEEN STRINGERS 8R TO 22R IAW SRM 51-72-10, PAGES 1 TO 3, SRM 51-40-21, PG 10 TO 22, DRILLEJun 27, 2012 · N403FE · Airbus A310203 · Fuselage Main, FrameSDR FDEA201206222295Floor Panel · crackedDURING INSTALLATION, FOUND FLOOR PANEL 252BF CRACKED. FABRICATED REPLACEMENT FLOOR PANEL IAW DWG SRZ 25-005, REV J.Jun 22, 2012 · N403FE · Airbus A310203 · Fuselage Floor PanelSDR FDEA201206202281Wedge · debondedLEFT ELEVATOR T/E WEDGE AT RIB 11 AND 14 SPLICES UPPER AND LOWER SURFACES ARE DEBONDING AND CORRODED. REPAIRED IAW A300-600 SRM 55-21-11 C1 PARA. 5.I. FIG. 209.Jun 20, 2012 · N403FE · Airbus A310203 · Elevator StructureSDR FDEA201206202282Skin · delaminatedRT ELEVATOR LOWER SKIN AT RIB 17 HAS 2EA AREAS OF DELAMINATION.Jun 20, 2012 · N403FE · Airbus A310203 · Elevator, Plate/SkinSDR FDEA201206192268Seat Track · damagedFLOOR CLEVIS ADAPTER BETWEEN SEAT TRACK 2R AND 3R INSTALLED NOT ALIGN AND HAS 2 EA ELONGATED FASTENER HOLES. R & R DUMMY TRACK IAW SRM 51-72-10.Jun 19, 2012 · N403FE · Airbus A310203 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201206192267Seat Track · damagedFLOOR SEAT TRACK 2R HAS 5 EA ELONGATED HOLES FROM FRAME 54 TO 54.2 AT RT FLANGE. R & R SEAT TRACK 2R BETWEEN FRAMES 54 AND 54.2 IAW SRM 51-72-10.Jun 19, 2012 · N403FE · Airbus A310203 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201206182256Floorbeam · bentFLOORBEAM TOP FLANGE IS BENT 10 SQUARE INCHES AT CLEVIS ADAPTER BETWEEN SEAT TRACKS 2L AND 3L AND FRAME 37. CUT, REMOVED DAMAGED SECTION & SPLICED IN NEW SECTION OF CROSSBEAM IAW SRM 53-10-15, FIG 201, SHT 3.Jun 18, 2012 · N403FE · Airbus A310203 · Fuselage Main, Floor BeamSDR FDEA201206182254Floorboard · delaminatedFLOORBOARD 231NG DELAMINATED IN MULTIPLE AREAS APPROX 30 SQUARE INCHES. FABRICATED REPLACEMENT FLOORBOARD IAW DWG SRZ 25-005, REV J.Jun 18, 2012 · N403FE · Airbus A310203 · Fuselage Floor PanelSDR FDEA201206092174Skin · failedRT WING NR 2 SLAT NOSE SKIN BETWEEN RIBS 35 TO 37 IS 4.3" X 2.8" MISREPAIRED. REPAIRED IAW SRM 57-43-11, FIG 202 SHEETS 6 AND 14 PAGES 219 AND 227. COMPLIED WITH EA 6-5750-157852. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.Jun 9, 2012 · N403FE · Airbus A310203 · Leading Edge DevicesSDR FDEA201206092171Stringer · failedSTRINGER 55 RIGHT MISREPAIRED. REPAIRED IAW SRM 53-10-14, FIG 201, PAGES 203 TO 206. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.Jun 9, 2012 · N403FE · Airbus A310203 · Fuselage Main, Longeron/StringerSDR FDEA201206082163Stringer · misrepairedSTRINGER 53 LEFT MISREPAIRED BETWEEN FRAMES 63 AND 64. REPAIRED IAW SRM 53-10-14, FIG 201 PAGES 203 TO 206. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.Jun 8, 2012 · N403FE · Airbus A310203 · Fuselage Main, Longeron/StringerSDR FDEA201206082155Stringer · misrepairedSTRINGER 53 LEFT MISREPAIRED BETWEEN FRAMES 61 TO 63. REPAIRED IAW SRM 53-10-14. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.Jun 8, 2012 · N403FE · Airbus A310203 · Fuselage Main, Longeron/StringerSDR FDEA201206082165Stringer · misrepairedSTRINGER 54L BETWEEN FRAMES 65 AND 66 MISREPAIRED. REPAIRED SRM 53-10-14, FIG 201, PAGES 203 TO 206. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.Jun 8, 2012 · N403FE · Airbus A310203 · Fuselage Main, Longeron/StringerSDR FDEA201206082164Stringer · misrepairedSTRINGER 53L BETWEEN FRAMES 66 AND 69 MISREPAIRED. REPAIRED IAW SRM 53-10-14 FIG 201, PAGES 203 TO 206. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.Jun 8, 2012 · N403FE · Airbus A310203 · Fuselage Main, Longeron/StringerSDR FDEA201206082154Stringer · misrepairedSTRINGER 51 LEFT MISREPAIRED BETWEEN FRAMES 61 TO 63. REPAIRED IAW SRM 53-10-14, FIG 201, PAGES 203 TO 206. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.Jun 8, 2012 · N403FE · Airbus A310203 · Fuselage Main, Longeron/StringerSDR FDEA201206082166Stringer · misrepairedSTRINGER 56 LEFT MISREPAIRED. REPAIRED IAW SRM 53-10-14 FIG. 201 PGS. 205/206.Jun 8, 2012 · N403FE · Airbus A310203 · Fuselage Main, Longeron/StringerSDR FDEA201206082160Stringer · misrepairedSTRINGER 54 LEFT MISREPAIRED. REPAIRED IAW SRM 53-10-14 FIG. 201 PGS. 205/206Jun 8, 2012 · N403FE · Airbus A310203 · Fuselage Main, Longeron/StringerSDR FDEA201206082157Stringer · misrepairedSTRINGER 53 LEFT MISREPAIRED. REPAIRED IAW A310 SRM 53-10-14 FIG. 201 PGS. 205/206.Jun 8, 2012 · N403FE · Airbus A310203 · Fuselage Main, Longeron/StringerSDR FDEA201206082156Stringer · misrepairedSTRINGER 55 LEFT MISREPAIRED. REPAIRED IAW A310 SRM 53-10-14 FIG. 201 PGS. 205/206.Jun 8, 2012 · N403FE · Airbus A310203 · Fuselage Main, Longeron/StringerSDR FDEA201206082158Floorboard · damagedFLOORBOARD 162HF HAS IMPACT DAMAGE OVER 50 PERCENT OF PANEL. FABRICATED REPLACEMENT FLOORBOARD IAW DWG SRZ 25-005 REV J, REF DWG SRZ 25-011.Jun 8, 2012 · N403FE · Airbus A310203 · Fuselage Floor PanelSDR FDEA201206072136Stringer · misrepairedSTRINGER 53 LEFT, MISREPAIRED. REPAIRED PER SRM 53-10-14 FIG 201 PAGES 203 TO 206. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Jun 7, 2012 · N403FE · Airbus A310203 · Fuselage Main, Longeron/StringerSDR FDEA201206072132Stringer · misrepairedSTRINGER 50 LEFT MISREPAIRED, FRAMES 59 TO 60. REPAIRED PER SRM 53-10-14 FIG 201 PAGES 203 TO 206. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Jun 7, 2012 · N403FE · Airbus A310203 · Fuselage Main, Longeron/StringerSDR FDEA201206072131Stringer · misrepairedSTRINGER 47 LEFT MISREPAIRED, FRAMES 59 TO 60. REPAIRED PER SRM 53-10-14 FIG 201 PAGES 203 TO 206. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Jun 7, 2012 · N403FE · Airbus A310203 · Fuselage Main, Longeron/StringerSDR FDEA201206072120Seat Track · corrodedSEAT TRACK 3R UPPER SURFACE BETWEEN SCALLOPS CORRODED 2 EA AREAS BET, FR 38.2 AND FR.40 MEASURED 6 SQ". REMOVED LEVEL 1 CORROSION ON SEAT TRACK 3R (AREA 1)BET 38.2 AND FR 40 IAW SRM 51-74-10, PG 205. FOUND TO BE OUT OF LIMITS IAW SRM 53-10-16, PG 103. R & Jun 7, 2012 · N403FE · Airbus A310203 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201206062114Stringer · misrepairedSTRINGER 51 LEFT MISREPAIRED. REPAIRED IAW SRM 53-10-14, FIG 201, PAGES 203-206.Jun 6, 2012 · N403FE · Airbus A310203 · Fuselage Main, Longeron/StringerSDR FDEA201206062112Floorboard · damagedFWD CARGO FLOORBOARD 132RF DAMAGE ON THE EDGE ABOUT 3 FT. LONG. FABRICATED REPLACEMENT FLOORBOARD IAW DWG SRZ 25-005, REV J.Jun 6, 2012 · N403FE · Airbus A310203 · Fuselage Floor PanelSDR FDEA201206062111O-Ring · failedPASSING FL 280, DURING DECENT. THE ECAM "HYD LO PRESS" GREEN HYD SYS RESERVOIR LEVEL WAS DOWN TO RED DOT. WITHING 30 SEC USING ECAM TURNED GREEN PUMPS OFF. LATER ECAM INDICATED "LO RESV LEVEL". GRAVITY EXTENDED GEAR. GREEN LEVEL RETURNED TO NORMAL. R & Jun 6, 2012 · N445FE · Airbus A310203 · Hydraulic System, MainSDR FDEA201206062110Floorboard · delaminatedFLOORBOARD 242ZJ DELAMINATED. FABRICATED REPLACEMENT FLOORBOARD IAW DWG SRZ 25-005, REV J.Jun 6, 2012 · N403FE · Airbus A310203 · Fuselage Floor PanelSDR FDEA201206062109Floorboard · damagedFLOORBOARD 231AH HAS FIVE CRUSHED AREAS. FABRICATED REPLACEMENT FLOORBOARD IAW DWG SRZ 25-005, REV J.Jun 6, 2012 · N403FE · Airbus A310203 · Fuselage Floor PanelSDR FDEA201206062108Floorboard · damagedFLOORBOARD 231NH HAS THREE CRUSHED AREAS 5 INCHES LONG. FABRICATED REPLACEMENT FLOORBOARD IAW DWG SRZ 25-005, REV J.Jun 6, 2012 · N403FE · Airbus A310203 · Fuselage Floor PanelSDR FDEA201206052096Floorbeam · misrepairedFLOORBEAM MISREPAIRED AT FRAME 36. REPAIRED IAW SRM 53-10-15, FIG 207, PAGES 237 TO 242. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.Jun 5, 2012 · N403FE · Airbus A310203 · Fuselage Main, Floor BeamSDR FDEA201206052099Stringer · misrepairedSTRINGER 56 LEFT MISREPAIRED, FRAMES 73 TO 75. REPAIRED IAW SRM 53-10-14, FIG 201, PAGES 203 TO 206 FLAG NOTE 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.Jun 5, 2012 · N403FE · Airbus A310203 · Fuselage Main, Longeron/StringerSDR FDEA201206052098Stringer · misrepairedSTRINGER 40 LEFT MISREPAIRED FRAMES 73 TO 74. REPAIRED IAW SRM 53-10-14, FIG 201, PAGES 203 TO 206 FLAG NOTE 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.Jun 5, 2012 · N403FE · Airbus A310203 · Fuselage Main, Longeron/StringerSDR FDEA201206052094Floorbeam · misrepairedFLOORBEAM MISREPAIRED. REPAIRED IAW SRM 53-10-15, FIG 207, PG 241/242. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.Jun 5, 2012 · N403FE · Airbus A310203 · Fuselage Main, Floor BeamSDR FDEA201206052097Stringer · misrepairedSTRINGER MISREPAIRED. REPAIRED IAW SRM 53-10-14, FIG 201, PAGES 203 TO 206. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.Jun 5, 2012 · N403FE · Airbus A310203 · Fuselage Main, Longeron/StringerSDR FDEA201206052095Floorboard · damagedFLOORBOARD 241MK CRUSHED ON EDGE & FOUR SEPARATE DELAMINATION AREAS ON UPPER SURFACE. FABRICATED REPLACEMENT FLOORBOARD IAW DWG SRZ 25-005, REV J.Jun 5, 2012 · N403FE · Airbus A310203 · Fuselage Floor PanelSDR FDEA201206052093Floorboard · corrodedFLOORBOARD 251GH HAS CORROSION AT HONEYCOMB CORE OUTER EDGES. FABRICATED REPLACEMENT FLOORBOARD IAW SRZ 25-005, REV J.Jun 5, 2012 · N403FE · Airbus A310203 · Fuselage Floor PanelSDR FDEA201206052092Floorboard · delaminatedFLOORBOARD 242EK DELAMINATED. FABRICATED REPLACEMENT FLOORBOARD IAW DWG SRZ 25-005, REV J.Jun 5, 2012 · N403FE · Airbus A310203 · Fuselage Floor PanelSDR FDEA201206052091Floorboard · damagedFLOORBOARD 162EF HAS COMPOSIT DAMAGE TO LOWER SURFACE AND HAS ONE DAMAGED HOLE GROMET, FABRICATED REPLACEMENT FLOORBOARD IAW DWG SRZ 25-005, REV J & SRZ 25-011.Jun 5, 2012 · N403FE · Airbus A310203 · Fuselage Floor PanelSDR FDEA201206052090Thrust Plate · corrodedTHRUST PLATE BETWEEN FRAME 34 AND 35 LOCATED BETWEEN SEAT TRACKS 5L AND 6L HAS 1 SQUARE INCH OF CORROSION. REMOVED CORROSION, ORIGINAL THICKNESS .094", 7EA AREAS MAX LOSS .008, REMAINING .086". AT AREA "7" MAX LOSS .016" REMAINING .078". R & R THRUST PLATE BEJun 5, 2012 · N403FE · Airbus A310203 · Fuselage Miscellaneous StructureSDR FDEA201206052089Shear Plate · crackedSHEAR PLATE LT SIDE WEB CRACKED BETWEEN FR79-FR80. R & R SHEAR PLATE WEB ON FLOOR LT SIDE BETWEEN FR79-FR80 IAW SRM 51-72-10, PG 1.Jun 5, 2012 · N403FE · Airbus A310203 · Fuselage Floor PanelSDR FDEA201206042080Floor Panel · crackedFLOOR PANEL 242UJ HAS TWO, 10 INCH CRACKS. FABRICATED FLOOR PANEL 242 UJ IAW DWG NR SRZ 25-005, REV J.Jun 4, 2012 · N403FE · Airbus A310203 · Fuselage Floor PanelSDR FDEA201206042079Floorboard · delaminatedFLOORBOARD 231HG UPPER SURFACE DISBONDED AT AFT OTBD CORNER 10 SQUARE INCHES. FABRICATED REPLACEMENT FLOORBOARD IAW DWG SRZ 25-005, REV J.Jun 4, 2012 · N403FE · Airbus A310203 · Fuselage Floor PanelSDR FDEA201206042078Floorboard · damagedFLOORBOARD 232NG HAS 7 PUNCTURES ON TOP SURFACE, FABRICATED REPLACEMENT FLOORBOARD IAW DWG SRZ 25-005, REV J.Jun 4, 2012 · N403FE · Airbus A310203 · Fuselage Floor PanelSDR FDEA201206042077Floorboard · delaminatedMLG WHEEL WELL FLOORBOARD 147AF TOP COATING IS DEBONDED ABOUT 12 FT SQUARE. FABRICATED REPLACEMENT FLOORBOARD IAW DWG SRZ 25-005, REV J.Jun 4, 2012 · N403FE · Airbus A310203 · Fuselage Floor PanelSDR FDEA201206042076Floor Panel · damagedFLOOR PANEL 232YH UPPER SURFACE GOUGED 8 SQUARE INCHES. FABRICATED REPLACEMENT FLOOR PANEL IAW DWG SRZ 25-005, REV J.Jun 4, 2012 · N403FE · Airbus A310203 · Fuselage Floor Panel
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