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 FDEA201306051198Skin · corrodedRT ELEVATOR NR 2 T/E UPPER SURFACE CORRODED. REPAIRED THE DAMAGE IAW SRM 55-21-11/201 (C-1) FIG 209.SDR FDEA201305301143Skin · crackedAFT CARGO DOOR EXTERIOR SKIN FWD LOWER CORNER EDGE CRACKED. COMPLIED WITH EA6-5230-168203.SDR FDEA201305301142Skin · corrodedREAR FUSELAGE SKIN LOWER HORIZONTAL STAB CUTOUT BETWEEN FR 87-89, S27-31R FOUND CORRODED. COMPLED WITH EA6-5330-168201.SDR FDEA201305301141Skin · corrodedREAR FUSELAGE SKIN LOWER HORIZONTAL STAB CUTOUT BETWEEN FR 87-89, S27-31 LT FOUND CORRODED. COMPLIED WITH EA6-5330-168201.SDR FDEA201305221067Frame · damagedCENTER FUSELAGE FRAME 46 RT SIDE HOLE H25 AND H27: IN THE FRAME FOOT, FRAME REINFORCING, FRAME HOLE DIMENSION AT 9.92MM PRESENT NO CRACK INDICATION, STRAP AT 7.26MM PRESENT, NO CRACK INDICATION. COMPLIED WITH EA6-5310-168229.SDR FDEA201305221066Frame · damagedCENTER FUSELAGE FRAME 45, RT SIDE HOLE H22: IN THE FRAME FOOT AND FRAME DOUBLER HOLE DIMENSION AT 14MM WITH NO CRACK INDICATION, IN THE FRAME HOLE DIMENSION AT 9.92 WITH NO CRACK INDICATION. COMPLIED WITH EA6-5310-168229.SDR FDEA201305221065Frame · damagedCENTER FUSELAGE FRAME 45, LT HOLE H15: IN THE FRAME FOOT, FRAME DOUBLER, FRAME AND BRACKET FR45 HOLE DIMENSION AT 9.92 MM WITH NO CRACK INDICATION; HOLE H22: IN THE FRAME FOOT, FRAME DOUBLER AND FRAME HOLE DIMENSION AT 9.92MM WITH NO CRACK INDICATION; HOLESDR FDEA201305221064Frame · damagedCENTER FUSELAGE FRAME 44 RT HOLE H12 AND H13 DIMENSION AT 8.73MM PRESENT NO CRACK INDICATION, HOLE H10 DIMENSION AT 6.76MM PRESENT NO CRACK INDICATION, HOLE H11 DIMENSION AT 7.52MM PRESENT NO CRACK INDICATION. COMPLIED WITH EA6-5310-168229.SDR FDEA201305221063Frame · crackedCENTER FUSELAE FRAME 44 LT SIDE HOLE H5 WITH NO CRACK INDICATION & HOLE DIMENSION IS 19MM, AND FRAME 44 LT SIDE HOLE H13 WITH SHORT EDGE DISTANCE, HOLE H13 EDGE DISTANCE IS 11.17 MM LESS THAN 12 MM REQUIRED IN THE SB53-2124. COMPLIED WITH EA 6-5310-168229SDR FDEA201305211051Stringer · corrodedBULK CARGO STRINGER 55 RT CORRODED FR 65-66. CUT DAMAGE STRINGER & DEBURR SHAPE EDGES OF CUTOUT IAW SRM 53-10-14, FIG 201. APPLY WASH PRIMER & PRIMER TO THE CUTOUT EDGES IAW SRM 53-10-14, FIG 201. MAKE REPAIR PROFILE AND REPAIR SPLICES IAW SRM 53-10-14, FISDR FDEA201305211050Stringer · corrodedBULK CARGO STRINGER 56R CORRODED FR 65-66. CUT DAMAGE STRINGER & DEBURR SHAPE EDGES OF CUTOUT IAW SRM 53-10-14/201, PAR 4.A, FIG 201. MAKE REPAIR PARTS IAW SRM 53-10-14/201 PAR 4A, FIG 201. DRILL HOLES AND DEBURR REPAIR PARTS IAW SRM 53-10-14/201, PAR 4.A, SDR FDEA201305171014Frame · damagedCENTER FUSELAGE, THE UPPER FRAME 45 BASE-TO-ARCHES JUNCTION FOUND HOLE NR 22 WITH CRACK SIGNAL AND THE CRACK IS ELIMINATED WHEN THE HOLE DIMENSION IS 0.551" (RT SIDE). COMPLIED WITH EA6-5310-168229.SDR FDEA201305171013Fitting · damagedCENTER FUSELAGE UPPER FRAME 44 BASE-TO-ARCHES JUNCTION FOUND HOLE NR 5 WITH CRACK SIGNAL AND THE CRACK IS ELIMINATED WHEN THE HOLE DIMENSION IS 0.472". (LT SIDE) COMPLIED WITH EA6-5310-168229SDR FDEA201305150992Crossbeam · corrodedFWD CARGO FR 38.1 -Y140 CROSSBEAM CORRODED. REPAIRED CROSSBEAM IAW SRM 53-10-15, FIG 207.SDR FDEA201305140981Stringer Splice · corrodedBULK CARGO STRINGER SPLICE CORRODED, LOCATED AT FR65,STGR43 LT 1. REMOVED AND REPLACED CORRODED SPLICE IAW SRM 51-40-21. REPAIRED IAW SRM51-40-44.SDR FDEA201305080936Frame · crackedCERNTER FUSELAGE UPPER FRAME 43 BASES-TO-ARCHES JUNCTION ROTAING PROBE INSPECTION FOUND HOLE NR 2 WITH CRACK SIGNAL & THE HOLE DIMESION IS 0.313" (RT SIDE). COMPLIED WITH EA6-5310-168229.SDR FDEA201305080935Fitting · crackedCENTER FUSELAGE, UPPER FRAME 43 BASES-TO-ARCHES JUNCTION ROTATING PROBE INSPECTION FOUND HOLE NR 2 WITH CRACK SIGNAL & THE HOLE DIMESION IS 0.313" (LT SIDE).COMPLIED WITH EA6-5310-168229.SDR FDEA201304150784Skin · crackedNDT INSPECTION OF LT FRAME 54, SKIN JOINT BETWEEN S36 AND 37L, SHOWS SIX HOLES WITH POSITIVE CRACK INDICATIONS. INDICATIONS ARE AT MULTIPLE CLOCK POSITIONS. POSITIVE HOLES ARE 1, 5, 6, 8, 11 AND 13. REF ALI 53-15-90. COMPLIED WITH EA 6-5315-T0300240, REV.SDR FDEA201304020712Shear Tie · damagedWHILE ACCOMPLISHING WC E6-5310-7-5020 A PT2, FOUND FR 43 SHEAR TIE HAS SHORT E.D. REMOVED AND REPLACED IAW SRM 51-72-10 AND DWG 57112116SDR FDEA201303170590Seat Track · damagedDUMMY TRACK 4L FR 54 / 54.2 FAILED GAP CHECK. REMOVED, REPAIRED AND INSTALLED DUMMY TRACK IAW SRM 53-15-16, FIG 203.SDR FDEA201303150574Seat Track · looseDUMMMY TRACK 3R FR 38.2 /40 FAILS GAP CHECK. REMOVED DUMMY TRACK AT FR 38.2 /40 IAW SRM 51-40-21, PAR 5 & PAR 7. REPAIRED DUMMY TRACK IAW SRM 53-15-16 PG 209 -216, REINSTALLED TRACK AT FR 38.2 /40 IAW SRM 51-40-21, PAR 5-7. REPROTECTED AREA IAW SRM 51-75-10SDR FDEA201303140568Seat Track · wornDUMMY TRACK 2R FR 54 TO 54.2 FAILS GAP CHECK. REMOVED DUMMY TRACK 2R FR 54/54.2 IAW SRM 53-15-16. REPAIRED DUMMY TRACK 2R FR 54/54.2 IAW SRM 53-15-16. INSTALLED REPAIRED DUMMY TRACK 2R FR 54/54.2 IAW SRM 51-40-21 AND SRM 53-15-16.SDR FDEA201303130567Floorbeam · corrodedUPON REMOVAL OF SEAT TRACK SECTION, FOUND CORROSION ON FLOORBEAM UPPER TEE TOP SURFACE AT FR 16A, Y1959 (5L)(APPROX 1 SQ IN TOTAL)SDR FDEA201303120556Seat Track · corrodedSEAT TRACK 5L AT FR 18 HAS CORROSION ON TOP SURFACE. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS. REMOVED, FABRICATED IAW DWG. A53610798, AND REPLACED SEAT TRACK IAW SRM 51-40-21 PARA. 6 AND 13.SDR FDEA201303110547Floor Panel · damagedFLOOR PANEL 252GF CRUSHED. FABRICATED REPLACEMENT FLOOR PANEL IAW DWG SRZ 25-005 REV. J.SDR FDEA201303110548Floor Panel · damagedFLOOR PANEL 252MF CRUSHED. FABRICATED REPLACEMENT FLOOR PANEL IAW DWG SRZ25-005 REV J. REMOVED AND INSTALLED FLOOR PANEL IAW AMM 53-10-25-04SDR FDEA201303090534Angle · crackedUPON INSP/NDT OF HOLES H1 AND H2 AT ARCH FITTING AT FR43 LT SHOWS INDICATION OF CRACK ON BRACKET SIDE. REMOVED AND REPLACED ANGLE IAW SRM 51-72-10.SDR FDEA201303090533Attach Angle · crackedFOUND UPPER ATTACH ANGLE TO BE VISIBLY CRACKED. R & R FR 43 UPPER FWD ATTACH ANGLE AT ARCH FITTING IAW SRM 51-72-10.SDR FDEA201303090530Floor Panel · damagedPANEL 232XH CRUSHED AT CLS. FABRICATED REPLACEMENT PANEL232XH IAW DWG SRZ-25-005, REV Z.SDR FDEA201303080526Floor Panel · crackedFLOOR PANEL 252 UF HAS 10 INCH CRACK. FABRICATED REPLACEMENT FLOOR PANEL IAW DWG SRZ 25-005 REV. J.SDR FDEA201303080522Floor Panel · crackedFLOOR PANEL 251GF HAS 12 INCH CRACK. FABRICATED REPLACEMENT FLOOR PANEL IAW DWG SRZ25-005 REV J. REMOVED AND REPLACED FLOOR PANEL IAW AMM 53-10-25-04.SDR FDEA201303080518Floor Panel · damagedFLOOR PANEL 252SF CRUSHED AT CUTOUTS. FABRICATED REPLACEMENT FLOOR PANEL IAW DWG SRZ-25-005, REV J.SDR FDEA201303080517Floor Panel · damagedFLOOR PANEL 252BF CRUSHED AT CUTOUT. FABRICATED REPLACEMENT FLOOR PANEL IAW DWG SRZ-25-005, REV J.SDR FDEA201303080527Floorboard · damagedFLOORBOARD 242UJ CRUSHED AT CLS CUTOUT. FABRICATED REPLACEMENT FLOORBOARD IAW DWG SRZ 25-005, REV J.SDR FDEA201303080525Floorboard · delaminatedFLOORBOARD 232LT IS CRUSHED AT CLS CUTOUT. FABRICATED REPLACEMENT FLOORBOARD IAW DWG SRZ 25-005, REV J.SDR FDEA201303080524Floorboard · damagedFLOORBOARD 232SF IS CRUSHED AT CLS CUTOUT. FABRICATED FLOORBOARD IAW DWG SRZ 25-005, REV J.SDR FDEA201303080523Floor Panel · damagedFLOOR PANEL 242QJ CRUSHED AT CLS CUTOUT. FABRICATED FLOOR PANEL IAW DWG SRZ 25-005, REV J.SDR FDEA201303070506Floor Panel · crushedFLOOR PANEL 242ZJ CRUSHED AT CUTOUT. FABRICATED REPLACEMENT PANEL IAW DWG SRZ-25-005, REV J.SDR FDEA201303070505Floor Panel · crushedFLOOR PANEL 242EK CRUSHED AT CUTOUT. FABRICATED REPLACEMENT FLOOR PANEL IAW DWG SRZ-25-005, REV J.SDR FDEA201303070507Floor Panel · damagedFLOOR PANEL 241NK IS BROKEN IN HALF AT CLS CUTOUT. FABRICATED REPLACEMENT FLOOR PANEL IAW DWG SRZ-25-005 REV. J.SDR FDEA201303060500Floor Panel · damagedFLOOR PANEL 147AF EDGE SEALANT SOFTENED & MISSING BY A PERIMETER LENGTH OF 50". FABRICATED REPLACEMENT FLOOR PANEL IAW DWG SRZ 25-005, REV J.SDR FDEA201302280479Longeron · crackedWHILE PERFORMING ROTO PROBE ON FWD LOWER HOLE OF INSPECTION AREA THREE IAW WIC E6-5310-7-3328 A PT4, FOUND CRACK IN LONGERON. REPAIRED IAW 6-5310-T0300114, PS P1.SDR FDEA201302250444Fitting · crackedDURING ACCOMPLISHMENT OF EO 6-5310-7-5020 PT 2, FRAME 45, HOLE H22 RT SIDE SHOWS CRACK INDICATION. FRAME 47 RT HOLE 22 COMPLIED WITH MOD TYPE T MOD NR 6-5315 T0300100 REV NR PS P1, STEPS 1, THRU 13.SDR FDEA201302250443Angle · crackedFRAME 46, HOLE H27 SHOWS CRACK INDICATION IN ANGLE FITTING AT 6 O'CLOCK. RT FRAME 46, HOLE H27 COMPLIED WITH MOD TYPE T MOD NR 6-5315-T0300100, REV NO PS P1 STEPS 14 THRU 28.SDR FDEA201302250442Frame · damagedDURING ACCOMPLISHMENT OF EO 6-5310-7-5020, PART 1, FOUND EDGE DISTANCE FOR HOLES H23 AT FR 46 LT TO BE BELOW .472". FRAME 46 LT HOLE H23 COMPLIED WITH MOD TYPE T MOD NR 6-5315-T0300100, REV NO PS P1 STEPS 29 AND 30.SDR FDEA201302220419Ferrule · crackedNR 2 PYLON FERRULE CRACKED AT FWD ATTACH POINT OF PNUEMATIC DUCT. CRACK IS 0.50 LONG. COMPLIED WITH EA 6-5450-T0300088 AND SB 54-2028. R & R FERRULE HALVES AND SPLICES.SDR FDEA201302210405Fitting · crackedNR 2 PYLON FERRULE CRACKED AT FWD OTBD UPPER CORNER AND AT FWD ATTACH POINT OF PNUEMATIC DUCT. CRACK A IS 1' LONG AND CRACK B IS 0.50 LONG. COMPLIED WITH EA 6-5450-T0300088 AD SB 54-2028. R & R FERRULE HALVES AND SPLICES.SDR FDEA201302190373Skin · damagedLEFT ELEVATOR UPPER SURFACE IS PUNCTURED AND DENTED. PUNCTURE (APPROX. 1.5" X .75"X .75") DENT (APPROX. .5" X .4" X .030") DAMAGE IS 8" FWD OF T/E AND 100" INBD OF ELEVATOR TIP REF SNRM N01030. REPAIRED LT ELEVATOR UPPER SURFACE IAW SRM 55-21-11, CONFIG 1, PSDR FDEA201302190371Support Angle · mismanufacturedDURING ACCOMPLISHMENT OF E0 6-5310-7-5020 APT1, FOUND EDGE DISTANCE FOR HOLES H1 AND H 2 AT FR 43 LT TO BE BELOW MINIMUM OF .472". R & R SUPPORT ANGLE AT FR 43 LT IAW SRM 51-72-10. R & R FRAME FOOT AT FR 43 LT IAW SRM 51-72-10.SDR FDEA201302190370Support Angle · crackedWHILE WORKING WC E6-5310-7-5020PT2, FOUND ONE BRACKET CRACKED AT MDCC FR43 BELOW STR 26R. R & R SUPPORT ANGLE IAW SRM 51-72-10. FABRICATED NEW SUPPORT ANGLE ON N00941.
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