Airbus A310-203
Service difficulty reports · 2,392
Newest first. General aviation reporting is voluntary.
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 = '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.
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
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR FDEA201101200313Floor Support · damagedBULK CARGO FLOOR SUPPORT LONGITUDINAL PROFILE BROKEN BETWEEN FRAMES 65 AND 66 LT STR 52 LT. R & R PROFILE SECTION FR65 TO FR66 LT ABOVE STR52L IAW SRM 51-72-10.SDR FDEA201101200312Floorbeam · crackedMAIN CABIN FLOORBEAM CRACKED IN RADIUS FR36 BETWEEN L2 AND L3 SEAT TRACK. REPAIRED CROSSBEAM AT FR36 BETWEEN SEAT TRACKS 2L AND 3L IAW SRM 53-10-15.SDR FDEA201101200303Crossbeam · corrodedREAR FUSELAGE FR 85 , APPROX 15 INCHES INBD OF STR16 RT, HORIZONTAL CROSSBEAM HAS EXFOLIATION CORROSION ON LOWER FLANGE REMOVED CORROSION FROM CROSSBEAM AT FR 85 INBD OF STR 16R AND CHECKED LIMITS IAW SRM 53-19-47 AND SRM 53-10-00, FIG 105 . REMOVED CROSSBEAM SDR FDEA201101190290Seat Track · corrodedAFT SEAT TRACK 1-R HAS CORROSION, FR78 - FR79, 20 SQUARE INCHES. R & R SEAT TRACK BETWEEN FR76 AND FR79 SEAT TRACK 1 IAW SRM 51-40-21, PG 24, 51-27-00, PG1, 51-40-40, PG1, 51-74-10, PG210, 51-21-10, PG6 -7, 53-10-16, PG101 - 103, 51-75-10, PG206.SDR FDEA201101120127Seat Track · corrodedAFT SEAT TRACK 1 HAS CORROSION FR 75 TO FR 77 ABOUT 30 SQUARE INCHES, REMOVED, FABRICATED AND INSTALLED SEAT TRACK 1, FR75 TO FR79 ALL IAW SRM 51-40-21, PG 24 PARA 7, 51-27-00, PG 1, 51-27-11 PG 1, 51-40-40 PG 1, 51-75-10 PG 206, PARA 4.SDR FDEA201101100099Floorbeam · corrodedBULK CARGO COMPARTMENT UNDERFLOOR, FR69, 17" TO 19" RT OF ACFT CENTERLINE, AXIAL FLOOR PANEL SUPPORT ANGLE HAS CORROSION/SWELLING ABOUT 6 SQUARE INCHES. BULK CARGO COMPARTMENT R & R PROFILE SECTION FR66 TO FR69 RBL17 TO RBL19 IAW SRM 51-72-10, PGS 1-3.SDR FDEA201101100098Beam · corrodedBULK CARGO, AFTER REMOVING LATERAL BEAM AT FR67 FOUND AXIAL BEAM CORRODED THROUGH 100 PERCENT PN A53974261202, BULK CARGO. R & R PROFILE BEAM FR66 - FR69 (Y535) IAW SRM 51-72-10, PGS 1-3.SDR FDEA201101100097Floor Support · damagedAFT CARGO FLOORBEAM RUNNING FWD AND AFT BETWEEN FR66 AND FR65 APPROX 2' RT OF ACFT CTR IS BROKEN. R & R PROFILE SECTION FR65 TO FR66, RBL18 TO RBL24 IAW SRM 51-72-10, PGS 1-3.SDR FDEA201101090092Floorbeam · corrodedBULK CARGO UNDERFLOOR AXIAL FLOOR SUPPORT ANGLE HAS CORROSION/SWELLING, LT 4" TO 7" FR67 ABOUT 6 SQUARE INCHES. R & R PROFILE SECTION FR66 TO FR69 LT 4" TO 7" IAW SRM 51-72-10, PGS 1-3.SDR FDEA201101090091Floorbeam · crackedFWD CARGO COMPARTMENT FOUND 1EA CRACK (.1250" DEEP) IN RADIUS OF UPPER FLOORBEAM FR38, BETWEEN UPPER SEAT TRACK 4L AND 5L CROSSBEAM REPAIRED AT CRACKED STIFFENER FR38 BETWEEN SEAT TRACKS 4L AND 5L IAW A310 SRM 53-10- 15 PGS 246 - 251/252 FIG. 203SDR FDEA201101080089Floorbeam · corrodedMAIN CABIN COURIER AREA UNDER FLOOR, CORROSION ON LONGITUDINAL MEMBER AT FLOOR SUPPORT ANGLE 7" FWD OF FLOORBEAM AT FR13, 40" TO LT FROM ACFT CENTERLINE. AMM 53-12-00-06, 57" FROM ACFT CENTERLINE ABOUT 2 SQARE INCHES. REMOVED AND INSTALLED NEW T-CAP TO LONSDR FDEA201101080088Seat Track · corrodedCORROSION IN CTR TOP OF SEAT TRACK 2L FRAME 51 ABOUT 5"X1". R & R DAMAGED SEAT TRACK 2L FR49.5 TO FR54 AND INSTALLED A SPLICE REPAIR ON SEAT TRACK 2L AT FR49.5 ALL IAW SRM 53-10-16, FIG 205.SDR FDEA201101080087Floorbeam · crackedFWD CARGO COMPARTMENT, UPPER FLOORBEAM FR33 HAS 1EA CRACK IN RADIUS BETWEEN SEAT TRACKS 2R AND 3R. CROSSBEAM REPAIRED AT FR33 BETWEEN SEAT TRACKS 2R AND 3R IAW SRM 53-10-15, FIG 203.SDR FDEA201101080086Seat Track · corrodedMAIN CABIN CORROSION ON SEAT TRACK 5L APPROX 1"X 2" BETWEEN FRAME 35 AND 36. R & R SEAT TRACK 5L AT FR35-FR36 AND 4EA SEAT TRACK SPLICES IAW SRM 53-10-16, PG 244, PGS 250A/250B FIG 208A.SDR FDEA201101080085Seat Track · corrodedCORROSION ON OTBD FLANGE OF SEAT TRACK 4R 2" AFT OF FRAME 34 1"X4 ". REMOVED DAMAGED SEAT TRACK 4R FR26 -FR36 IAW SRM 53-10-16, FIG 208. INSTALLED REPLACEMENT SEAT TRACK AND SPLICES IAW SRM 53-10-16, FIG 208.SDR FDEA201101080084Floor Support · corrodedBULK CARGO UNDERFLOOR FR69 10" LT FROM ACFT CENTERLINE, FLOOR SUPPORT ANGLE HAS CORROSION ABOUT 3 SQUARE INCHES. FABRICATED 1 EA FITTING IAW DWG A53974329. R & R FITTING AT FR69 10" LBL IAW SRM 51-72-10, PGS 1-3.SDR FDEA201101080083Floor Support · corrodedBULK CARGO UNDERFLOOR, FR69 CORROSION ON CARGO NET CLEVIS SUPPORT ANGLE, (ABOUT 2 SQUARE INCHES) R & R BULK CARGO UNDERFLOOR CARGO NET CLEVIS SUPPORT FITTING, FR69 IAW SRM 51-72-10, PGS 1-3.SDR FDEA201101080082Seat Track · corrodedSEAT TRACK 4R HAS CORROSION AT 8" AFT OF FR51 (-1959) R & R SEAT TRACK SEGMENT AND SPLICE REPAIR AT FR51 TO FR52 SEAT TRACK 4R IAW SRM 51-72-10, PGS1-3 AND 53-10-16 FIG 205.SDR FDEA201101060041Skin · corrodedFUSELAGE TAIL SECTION EXTERNAL SKIN HAS SURFACE CORROSION AT FWD OF FR 78,BETWEEN STR 2LT AND STR 3LT,ABOUT 8 SQ INCHES. CORROSION AT FUSELAGE EXTERNAL SKIN FOUND TO BE OUT OF LIMITS IAW SRM 53-19- 12 FIG 102 PAR 5. REPAIRED AREA WITH INTERNAL DOUBLER AND FSDR FDEA201101060054Profile · corrodedRT VERTICAL STABILIZER T/E HORIZ PANEL LANDING SUPPORT STRAP BETWEEN RIBS 21-22 HAS 8 INCH CORROSION IN AND AROUND 3 EA FASTENERS AND ALONG UPPER INTERIOR MATING SURFACE. R & R EDGE PROFILE RT VERT STAB T/E PANEL LANDING BETWEEN RIBS 21 AND 22 IAW SRM 51-72SDR FDEA201101060058Rib · corrodedVERTICAL STABILIZER, RIB 1 TOP SURFACE HAS CORROSION (ABOUT 4 SQ INCHES) RT STRINGER 5 RT TO STR 7 RT. FABRICATED REPAIR PARTS AND INSTALLED REPAIR IAW SRM 53-31-19, PG 209-211, FIG 203.SDR FDEA201101060056Mount · corrodedVERT STABILIZER AFT RT MOUNT LUG FITTING HAS CORROSION ON INTERIOR SURFACE BETWEEN STRINGER 1 RT AND STRINGER 2 RT,ABOUT 2 SQ INCHES. REPAIRED VERT STAB AFT RT LUG FITTING INTERIOR SURFACE BETTWEEN STR1R AND STR2R IAW EA 6-5530-145539.SDR FDEA201101060055Mount · corrodedVERTICAL STABILIZER LT AFT MOUNT LUG HAS CORROSION FROM STR 1 LT TO STR 4 LT, ABOUT 70 SQ INCHES. REPAIRED VERT STAB LT AFT MOUNT LUG BETWEEN S1L TO S4L IAW EA 6-5530-145538.SDR FDEA201101060053Crossbeam · corrodedREAR FUSELAGE FRAME 86, STR 16, LT TO THS DRIVE UNIT SUPPORT, FWD CROSSBEAM HAS EXFOILIATION CORROSION. REMOVED LEVEL 1 CORROSION. REWORKED CROSSBEAM ON FR 86 AT STR 16 LT IAW SRM 51-74-10. MATERIAL LOSS .006 IN. REMAINING THICKNESS WITHIN LIMITS IAW SRM SDR FDEA201101060052Support Beam · corrodedREAR FUSELAGE FRAME 87-88, STR 16, RT HORIZ STAB CUTOUT SUPPORT BEAM INBD FACE CORRODED AT 1 EA LOCK FASTENER APPROX 1 SQ INCH. REMOVED CORROSION IAW SRM 51-74-10, FOUND TO BE WITH IN MFG TOLERANCES IAW DWG A53985426 AND DAN11304 NDT INSP IAW NTM 51-10-08 NO SDR FDEA201101060051Stringer · corrodedREAR FUSELAGE FRAME 87-89, STR 16, LT HORIZ STAB CUTOUT INNER FWD STRAP HAS EXFOILIATION CORROSION APPROX 4 SQ INCHES. R & R THS CUTOUT FWD FITTING IAW DWG A53985135 AND A310 SRM 51-40-21, PG 46.SDR FDEA201101060050Fitting · corrodedREAR FUSELAGE FRAME 87-89, STR 16 RT, THS CUTOUT INNER FWD STRAP HAS EXFOILIATION CORROSION APPROX 4 INCHES AT AFT ATTACH. R & R THS CUTOUT UPPER FWD CORNER FITTING FR87 TO FR89, STR 16R IAW SRM 51-72-10.SDR FDEA201101060049Frame · corrodedREAR FUSELAGE FRAME 85, APPROX 15 INCHES INBD OF STR 16 RT HORIZ CROSSBEAM HAS EXFOILIATION CORROSION ON LOWER FLANGE. REMOVED LEVEL 1 CORROSION. FRAME R & R IAW SRM 53-19-47 WITH FABRICATED PART REF SDR NR 11-0303.SDR FDEA201101060045Spar · crackedCRACK AT FRONT SPAR CONNECTING SECTION AT RIB 1,2.5 INCH LONG. REMOVED TRANSVERSE FITTING AT VERTICAL STAB FWD SPAR RIB 1 AND REMOVED CONNECTION SECTION AT RIB 1 IAW SRM 51-72-10 PG 1-3. CLEANED AREA IAW AMM 12-21-11. REPROTECTED AREA IAW SRM 51-75-10 PG 3SDR FDEA201101060044Skin · corrodedFUSELAGE TAIL SECTION EXTERNAL SKIN HAS SURFACE CORROSION AT FR 87, STR 5LT, ABOUT 3 SQ INCHES. CLEANED FUSELAGE TAIL SEC EXTERNAL SKIN IAW AMM 12-21-12. UPON FURTHER INSPECTION NO CORROSION FOUND. REPROTECTED AREA IAW SRM 51-21-10 PG 2 PARA 2 AND 51-75-10 SDR FDEA201101060043Skin · scratchedFUSELAGE TAIL SECTION EXTERIOR SKIN IS SCUFFED AT 4 INCHES FWD OF FR 80/82 BETWEEN S2-3R. BLENDED AREA TO A SMOOTH CONTOUR IAW SRM 51-73-10 PG 209. CHECKED LIMITS BEFORE 0.197, AFTER 0.0191, LOSS 0.006 WHICH IS WITHIN LIMITS IAW SRM 53-19-12 FIG 102 PARA 5.SDR FDEA201101060042Skin · dentedFUSELAGE TAIL SECTION EXTERNAL SKIN HAS DINGS ON SURFACE AT 4 INCHES AFT OF FR 87, BETWEEN RIB 2LT AND RIB 3LT ABOUT 4 SQ INCHES. BLENDED FUSELAGE TAIL SECTION SKIN SURFACE DENTS IAW SRM 51-73-10 PG 209 PARA F DEEPEST BEFORE 0.197 AFTER 0.191, LOSS 0.006. SDR FDEA201101060039Bracket · brokenFUSELAGE TAIL SECTION EXTERIOR GAIRING SUPPORT BRACKET BROKEN OFF AT 5 INCHES AFT OF FR 79, STR 4 RT. R & R MOUNTING BRACKET AT FUSELAGE TAIL SECTION EXTERIOR AT FR 79 AND STR 4R IAW SRM 51-72-10, PG 1-3 AND SRM 51-40-21, PARA 7, PG 24-55.SDR FDEA201101060038Skin · corrodedFUSELAGE TAIL SECTION STR 5RT AFT OF FR 83, EXTERNAL SKIN HAS CORROSION ABOUT 4 SQ INCHES. CLEANED AREA OF FUSELAGE TAIL SECTION STR 5R AFT OF FR 83 IAW AMM 12-21-12. UPON FURTHER INSP, NO CORROSION NOTED. REPROTECTED AREA IAW SRM 51-75-10, PG 225, PARA 10SDR FDEA201101060037Finger Doubler · gougedFUSELAGE TAIL SECTION, 7 INCHES AFT OF FR 87, BETWEEN STR 5RT AND STR 4RT, FUSELAGE FINGER DOUBLER HAS A GOUGE, 0.010 INCH DEPTH X 0.25 INCH WIDTH X 0.25 INCH LENGTH APPROX. BLENDED GOUGE ON TAIL SECTION 7" AFT OF FR 87 BETWEEN STR 4R AND STR 5R IAW SRM 51-73SDR FDEA201101060036Finger Doubler · gougedFUSELAGE TAIL SECTION 7 INCHES AFT OF FR 87 BETWEEN STR 4 LT AND STR 5 LT FUSELAGE SKIN FINGER DOUBLER HAS A GOUGE, .010 IN DEPTH X 0.25 INCH WIDTH X 0.25 INCH LENGTH APPROX. BLENDED GOUGE ON FUSELAGE TAIL SECTION 7" AFT OF FR 87 BETWEEN STR 4L AND 5L IAW SRMSDR FDEA201101060035Skin · corrodedFUSELAGE TAIL SECTION EXTERNAL FUSELAGE SKIN HAS SURFACE CORROSION AT FR 84, STR 5 LT ABOUT 7 SQ INCHES. CLEANED FUSELAGE TAIL SEC EXTERNAL SKIN BETWEEN FR 85 AND FR 86 AND STR 5R AND 6R IAW AMM 12-21-12. AFTER FURTHER INSP, NO CORROSION NOTED. REPROTECTEDSDR FDEA201101060034Skin · corrodedFUSELAGE TAIL SECTION EXTERNAL SKIN HAS SURFACE CORROSION AT FR 85 BETWEEN STR 5 RT AND STR 6 RT ABOUT 5 SQ INCHES. CLEANED FUSELAGE TAIL SECTION EXTERNAL SKIN AT FR 85, STR 5 R AND STR 6 R IAW AMM 12-21-12. UPON FURTHER INSP, NO CORROSION FOUND. REPROTECTESDR FDEA201101060033Skin · corrodedFUSELAGE TAIL SECTION EXTERNAL SKIN HAS SURFACE CORROSION BETWEEN FR 85 AND FR 86, BETWEEN STR 5 LT AND STR 6 LT. CLEANED FUSELAGE TAIL SECTION EXTERNAL SKIN BETWEEN FR 85 AND FR 86 BETWEEN STR 5L AND 6L IAW AMM 12-21-12. UPON FURTHER INSPECTION NO CORROSIONSDR FDEA201101060032Skin · corrodedFUSELAGE TAIL SECTION EXTERNAL SKIN AT FR 87 BETWEEN STR 5LT AND STR 6LT, CORROSION ON SPLICE PLATE ABOUT 4 SQ INCHES. REPAIRED FUSELAGE EXTERIOR SKIN AT FR87 BETWEEN STR5L AND STR6L IAW EA 6-5310-145562.SDR FDEA201101060031Fitting · corrodedVERTICAL STABILIZER LT AFT FITTING HAS CORROSION ON OTBD FACE, 2 LOCALIZED AREAS ABOUT 3 SQ INCHES. REMOVED LEVEL 1 CORROSION, COMPLIED WITH EA 6-5530-145557.SDR FDEA201101060030Fitting · corrodedVERTICAL STABILIZER RT AFT MOUNT FITTING HAS CORROSION ON OTBD FACE ABOUT 10 SQ INCHES. REMOVED LEVEL 1 CORROSION, COMPLIED WITH EA 6-5530-145557.SDR FDEA201101060029Fitting · corrodedVERTICAL STABILIZER RT CTR MOUNT FITTING HAS CORROSION OTBD SURFACE ABOUT 8 SQ INCHES. REMOVED LEVEL 1 CORROSION, COMPLIED WITH EA 6-5530-145557.SDR FDEA201101060028Fitting · corrodedVERTICAL STABILIZER RT FWD MOUNT FITTING OUTER FACE HAS CORROSION JUST AT SKIN EDGE AREA ABOUT 0.5 SQ INCHES. REMOVED LEVEL 1 CORROSION, COMPLIED WITH EA 6-5530-145557.SDR FDEA201101060027Structure · corrodedVERTICAL STABILIZER RT CHORD BETWEEN RIB 18 AND RIB 25 HAS SURFACE CORROSION AROUND NUTPLATES, 3 PLACES, APPROX 3 SQ INCHES. REMOVED LEVEL 1 CORROSION, COMPLIED WITH EA 6-5530-145551.SDR FDEA201101060026Structure · corrodedVERTICAL STABILIZER REAR SPAR LT CHORD, RIB 10 TO RIB 16 HAS CORROSION AT 11 EA NUT PLATES LOCATIONS. REMOVED LEVEL 1 CORROSION, COMPLIED WITH EA 6-5530-145551.SDR FDEA201101060025Angle · corrodedVERTICAL STABILIZER REAR SPAR FWD FACE RIB 9, HORIZ ANGLE HAS CORROSION ABOUT 3 SQ INCHES. REMOVED HORIZONTAL ANGLE AT FWD FACE OF RIB 9 IAW SRM 51-40-21, PG 22 PARA 7. REMOVED CORROSION IAW SRM 51-74-10, PG 205, PARA 3. NOMINAL THICKNESS IS 0.063, REMAINSDR FDEA201101060024Stiffener · corrodedVERTICAL STABILIZER INTERIOR REAR SPAR HORIZ STIFFENER BETWEEN RIB 9 AND RIB 10 HAS CORROSION ABOUT 3 SQ INCHES. REMOVED HORIZ STIFFNER AND DIAGONAL STIFFNER BETWEEN RIB 9 AND 10 AT VERT STAB REAR SPAR. REMOVED CORROSION ON HORIZ STIFFNER, NOMINAL 0.050, RESDR FDEA201101060023Rib · corrodedVERTICAL STABILIZER INTERIOR DIAGONAL ANGLE AT RT JOINT OF RIB 9 AND STR 2 HAS CORROSION ABOUT 4 SQ INCHES. REMOVED DIAGONAL BRACE AT RIB 10 AND REAR SPAR ON VERTICAL STABILIZER IAW SRM 51-72-10, PG 1-3. REMOVED CORROSION IAW SRM 51-76-10, PG 205, PARA 6. SDR FDEA201101060022Fitting · corrodedUPON REMOVAL OF LOWER WEB AT VERTICAL STAB FOUND CORROSION ON AFT FITTING AT LT ATTACH POINT. REMOVED CORROSION ON AFT TRAVERSE FITTING ON VERT STAB AT REAR SPAR IAW SRM 51-74-10, PG 5. BEFORE THICKNESS 0.557, AFTER 0.448. LOSS OF 0.069 IS OUT OF LIMITS IAW
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