JASC 5313

Service difficulty reports · 36,310

Reports filed under 5313 · Fuselage Main, Longeron/Stringer, 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 jasc_code = '5313'
  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 SWAA051111Splice · corrodedDURING SCHEDULED SPECIAL VISIT, FOUND CORROSION ON STRINGER SPLICE AT BS 362, STR 27L. REMOVED AND REPLACED STRINGER SPLICE PER SRM.Apr 14, 2005 · N657SW · Boeing 7373L9SDR 72300204Stringer · corrodedA 2 X 2 INCH AREA OF CORROSION ON STRINGER.Apr 13, 2005 · N723CK · Boeing 7272H3SDR C1HA200596012Stringer · corrodedFWD ASSY COMP STA 312, STRINGER 27L IS CORRODED UNDER FRAME (C53-111-03-02) STRINGER SPLICE REPAIR IAW SRM 53-10-3 FIG 3.Apr 13, 2005 · N696CA · Boeing 7272J4SDR SWAA051094Stringer · crackedDURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CRACKED AT BS 380, STR 5L. REPAIRED STRINGER PER SRM.Apr 13, 2005 · N313SW · Boeing 7373H4SDR 72300157Stringer · corrodedA 1 X 2 INCH AREA OF CORROSION ON STRINGER.Apr 12, 2005 · N723CK · Boeing 7272H3SDR ASAA0510053Stringer · crackedYXX - NDT CRACK INDICATION AT FASTENER HOLES ON STR 20L, BSTA 460-481. REPAIRED IAW SRM. (K)Apr 11, 2005 · N730AS · Boeing 737290CSDR ASAA0510052Stringer · crackedYXX- NDT CRACK INDICATION AT FASTENER HOLES ON STR 19L, BSTA 460-480. REPAIRED IAW SRM. (K)Apr 11, 2005 · N730AS · Boeing 737290CSDR ASAA0510044Stringer · crackedYXX - STRINGER 20L AT BSTA 390 CRACKED THROUGH FASTENER HOLE. REPAIRED IAW SRM. (K)Apr 11, 2005 · N730AS · Boeing 737290CSDR ASAA0510043Stringer · crackedYXX - NDT CRACK INDICATION AT FASTENER HOLE BSTA 470, STR 22L. REPAIRED IAW SRM. (K)Apr 11, 2005 · N730AS · Boeing 737290CSDR UPS05444402Stringer · crackedBS 1485 LT STR 6L STRINGER END FOUND CRACKED. CRACK LENGTH 0.5 INCH. M/DECK BS 1485 STR 6L REPAIRED AS PER HX RS R-53-41-35294 AND UPS EA ENGINEERING FILE NR 747-53-20244.Apr 11, 2005 · N523UP · Boeing 747283BSDR UPS05444401Stringer · crackedBS 1478-1480 STR 6R STRINGER END FOUND CRACK. CRACK LENGTH 1.5 INCH. M/DECK BS 1478-1480 STR 6R STRINGER END REPAIRED AS PER RS R-53-41-35294 AND UPS EA ENGINEERING FILE NR 747-53-20244.Apr 11, 2005 · N523UP · Boeing 747283BSDR UPS05444393Stringer · crackedBS 1238-1241 STR 7R STRINGER END FOUND CRACK (CRACK LENGTH 1 INCH ). M/DECK BS 1238 STR 7R STR REPAIRED AS PER HX RS R-53-41-35297 AND UPS ENGINEERING FILE NR 747-53-20245.Apr 11, 2005 · N523UP · Boeing 747283BSDR UPS05444337Stringer · crackedINSPECTION TYPE:C M/D BS 1956 STR 10R FOUND CRACKED. ( CRACK LENGTH .375" ) STRINGER REPAIRED AS PER SRM 53-10-03 FIG 4 AT BS 1930-1960 STR 10R AREA.Apr 10, 2005 · N523UP · Boeing 747283BSDR UPS05444342Stringer · crackedINSPECTION TYPE: C, M/D - BS 180 - 200 S-16R STRINGER FWD FOUND CRACKED. (CRACK LENGTH .250"), M/D BS 180-200 S-16R STRINGER REPLACED AS PER SRM 51-10-01 PG 9.Apr 9, 2005 · N523UP · Boeing 747283BSDR UPS05444340Stringer · crackedINSPECTION TYPE: C, M/D - BS 240-260 STR 11L STRINGER FOUND CRACKED. (CRACK LENGTH .250" ), M/D BS 240-260 STR -11L STRINGER REPLACED AS PER SRM 51-10-01 PG 9.Apr 9, 2005 · N523UP · Boeing 747283BSDR 72300152Stringer · crackedA .5 INCH CRACK COMING FROM HOLE TO OUTER EDGE OF STRINGER FLANGE.Apr 8, 2005 · N723CK · Boeing 7272H3SDR 72300151Stringer · corrodedA 6 X 3 INCH AREA OF CORROSION ON STRINGER.Apr 8, 2005 · N723CK · Boeing 7272H3SDR 72300203Stringer · corrodedA 1 X 2 INCH AREA OF CORROSION ON STRINGER.Apr 7, 2005 · N723CK · Boeing 7272H3SDR 2005UALA00307Stringer · corrodedSTRINGER 22L CORRODED AT STA 700 TO 720. DAMAGE CAUSED BY CORROSION. MAJOR REPAIR ACCOMPLISHED. STRINGER DAMAGE WAS TRIMMED OUT AND A DOUBLER REPAIR WAS INSTALLED.Apr 7, 2005 · N584UA · Boeing 757222SDR UPS05844371Longeron Splice · crackedINSPECTION TYPE: C1, B-PIT LONGERON SPLICE FITTING CRACKED (2) STA 610 L31L. REMOVED, MACHINED AND REPLACED LONGERON SPLICE IAW DWG 3750257, 51-1-20D AND 51-1-21.Apr 7, 2005 · N810UP · Doug DC873FSDR EIA2005100Stringer · crackedFUSELAGE BS 393 STRINGER 44L ONE EACH FASTENER HOLE FOUND CRACKED RUNNING FOWARD LOWER 1/8 INCH APPROX AND 3/16 INCH AFT. STRINGER PLATE REPAIRED PER SB 747-53-2305.Apr 5, 2005 · N485EV · Boeing 747212BSDR EIA2005096Stringer · crackedLEFT BS 1686 AT STRINGER 34L ONE EACH FASTENER HOLE FOUND CRACKED. RUNNING FWD AND AFT 2ND LAYER .0625 INCH APPROX IN LENGTH. THE CRACK TRIMMED OFF AND NDT CONFIRMED CRACK FREE CONDITION. SKIN REPAIRED PER EV EO 53-747-1701-03.Apr 5, 2005 · N485EV · Boeing 747212BSDR ASAA0510039Stringer · corrodedYXX- AFT CARGO PIT BSTA 827, STR 23L SPLICE HAS CORROSION. AFT CARGO PIT BSTA 827, STR 23L REPAIRED IAW SRM. (K)Apr 4, 2005 · N730AS · Boeing 737290CSDR ASAA0510038Stringer · corrodedYXX - AFT CARGO PIT BSTA 827, STR 21L SPLICE HAS CORROSION. AFT CARGO PIT BSTA 827, STR 21L REPAIRED IAW SRM. (K)Apr 4, 2005 · N730AS · Boeing 737290CSDR ASAA0510037Stringer · corrodedYXX- AFT CARGO PIT BSTA 907, STR 21L SPLICE HAS CORROSION. AFT CARGO PIT BSTA 907, STR 21L REAPIRED IAW SRM. (K)Apr 4, 2005 · N730AS · Boeing 737290CSDR ASAA0580201Gusset · corrodedOKC - DURING C-CHECK, FOUND LONGERON GUSSET CORRODED. REPLACED LONGERON GUSSET. (M)Apr 4, 2005 · N950AS · Doug DC983SDR EIA2005088Stringer · crackedAFTER REMOVAL OF SKIN STRINGER BS380 STR38R, FOUND CRACK AT 1EA FASTENER HOLE APPROX 1/8 INCH RUNNING UP AND 3/16 RUNNING DOWN. STRINGER REPAIRED PER SRM 53-10-03 FIG 1.Apr 4, 2005 · N485EV · Boeing 747212BSDR SWAA051001Stringer · corrodedDURING SCHEDULED SPECIAL VISIT, FOUND CORROSION ON FUSELAGE STRINGER BETWEEN BS 967 TO BS 1016, STR 25L. REPAIRED STRINGER PER SRM.Apr 4, 2005 · N657SW · Boeing 7373L9SDR UPS05844311Longeron · crackedINSPECTION TYPE:C1 LONGERON CRACKED 2 INCH LONG, AT STA 480 L20R, UPPER AND LOWER FLANGE. REMOVED DAMAGED LONGERON AND INSTALLED LONGERON AND SPLICES FROM FROM STA 460 TO 490 IAW SRM 53-02-02 FIG 11, 53-04-0, 53-04-01 AND 51- 1-8.Apr 2, 2005 · N810UP · Doug DC873FSDR 72300138Stringer · gougedAPPROX .25 X .5 INCH GOUGE IN STRINGER.Apr 2, 2005 · N723CK · Boeing 7272H3SDR ASAA0510036Stringer · corrodedYXX - AFT CARGO PIT BSTA 827-847, STR 27L SPLICE HAS CORROSION. AFT CARGO PIT BSTA 827-847, STR 27L REPAIRED IAW SRM. (K)Apr 1, 2005 · N730AS · Boeing 737290CSDR ASAA0510035Stringer · corrodedYXX - AFT CARGO PIT BSTA 807-847, STR 26L SPLICE HAS CORROSION. AFT CARGO PIT BSTA 807-847, STR 26L REPAIRED IAW SRM. (K)Apr 1, 2005 · N730AS · Boeing 737290CSDR UPS05844369Longeron · crackedINSPECTION TYPE: C1, LONGERON CRACKED .5 INCH LONG AT STA 1746 L14L. CUT OUT DAMAGE AND INSTALLED FILLER AND DOUBLER IAW RM 53-02-02, 51-1-20 AND 51-3-0.Apr 1, 2005 · N810UP · Doug DC873FSDR UPS05844280Longeron · crackedC1 LONGERON CRACKED .25 INCH LONG AT STA 1746 L14R. REPAIRED BY CUTTING OUT DAMAGE AND INSTALLING FILLER AND DOUBLER IAW SRM 53-02-02 FIG 11 AND 51-1-20D AND 51-3-0.Apr 1, 2005 · N810UP · Doug DC873FSDR UPS05844275Longeron · crackedC1 LONGERON .25 INCH LONG CRACKED AT STATION 1726 L15L. REPAIRED LONGERON BY CUTTING OUT DAMAGE. INSTALLING FILLER AND DOUBLER IAW SRM 53-02-02 FIG 11 AND 51-1-20D.Apr 1, 2005 · N810UP · Doug DC873FSDR 05FDEA00721Longeron · crackedMAIN DECK, AT STA 1219 LT FRAME TO FLOORBEAM INTERSECTION AT LONGERON 27 LEFT FOUND CRACKED. MAIN DECK, DISCREPANT LONGERON AT STA 1219 LT L-27 REMOVED AND REPLACED WITH NEW LONGERON: AEA 0435U503. NEW LONGERON LOCATED AND INSTALLED AS PER DRAWING AEA7605. Mar 31, 2005 · N576FE · Doug MD11SDR SIMA200509804Stringer · chafedABI - FOUND STRINGER 19R WAS FOUND CHAFED. BLENDED THE CHAFED AREA AND PERFORMED NDT. FABRICATED A REINFORCEMENT ANGLE AND TWO SHIMS. REPAIR DONE IAW EMB 145 SRM, SRM EMB 145/1142 REV 28 CHAPTER 53-24-02. (M)Mar 31, 2005 · N803AE · Emb EMB135KLSDR SIMA200509805Stringer · chafedFOUND STRINGER 19L WAS FOUND CHAFED. BLENDED THE CHAFED AREA AND PERFORMED NDT. FABRICATED A REINFORCEMENT ANGLE AND TWO SHIMS. REPAIR DONE IAW EMB 145 SRM, SRM EMB 145/1142 REV 28 CHAPTER 53-24-02. (M)Mar 31, 2005 · N803AE · Emb EMB135KLSDR USAA050438Stringer · crackedCLT - Q6 - STRINGER, (.250 INCH CRACK), STRINGER 4L, STATION 908.0906. INSTALLED SPLICE IAW SRM. (K)Mar 31, 2005 · N442US · Boeing 7374B7SDR USAA050437Stringer · crackedCLT - Q6 - STRINGER, (.250 INCH CRACK) STRINGER 4R STA 908.0903. INSTALLED SLICE IAW SRM. (K)Mar 31, 2005 · N442US · Boeing 7374B7SDR 05FDEA00760Stringer · corrodedAFT CARGO COMPT, AFT OF FS 54 ON R-STRINGER 51 HAS AREA OF CORROSION. REMOVED STRINGER END FITTING AT FS 54 ON STRINGER 51R IAW A310-200 SRM 51-74-21. REMOVED CORROSION FROM STRINGER 51 AFT OF FS 54 IAW A310-200 SRM 51-74-10. VERIFIED ALLOWABLE LIMITS AND MMar 31, 2005 · N402FE · Airbus A310SDR 05FDEA00759Stringer · corrodedBULK CARGO COMPT, JUST AFT FS 63 ON R STRINGER 53 1 AREA OF CORROSION. REMOVED DISCREPANT SECTION OF STRINGER AND REPLACED PER A310-200 SRM 51-10-14 IN BULK CARGO COMPARTMENT AFT OF FRAME 63 ON R STRINGER 53.Mar 31, 2005 · N402FE · Airbus A310SDR 05FDEA00758Stringer · corrodedCORROSION ALONG STRINGER 52L BETWEEN FRAMES 60 AND 61, AFT CARGO UNDER FLOOR. REMOVED CORROSION IAW A310-200 SRM 51-74-10. MATERIAL THICKNESS AFTER WENT OUT OF LIMITS IAW A310-200 SRM 51-10-04. CUT AND SPLICED STRINGER 52L AT FRAMES 60 AND 61 IAW A310-200 Mar 31, 2005 · N402FE · Airbus A310SDR 05FDEA00754Stringer · corrodedAREA BEHIND BULK CARGO AT FRAME 72 LEFT SIDE APPROX STR 41L, STRINGER HAS 5 SQ INCHES OF CORROSION. REMOVED CORROSION, AREA OUT OF LIMITS, REMOVED DAMAGED STRINGER SECTION AND REPLACED WITH NEW SECTION PER A310-200 SRM 51-74-10 AND 53-10-14.Mar 31, 2005 · N402FE · Airbus A310SDR 05FDEA00753Stringer · corrodedN00674 AREA BEHIND BULK CARGO AT FRAME 74 LEFT SIDE APPROX FR 49L HAS 7 SQ IN OF CORROSION. REMOVED CORROSION AFT OF FRAME 74 FOUND TO BE OUT OF LIMITS IAW A310-200 SRM 53-10-00 FIG 104, TABLE 102. REMOVED AND REPLACED STRINGER SECTION WITH NEW 48L FS 72-Mar 31, 2005 · N402FE · Airbus A310SDR 05FDEA00752Stringer · corrodedAREA BEHIND BULK CARGO BETWEEN FRAME 75 AND 76 APPROX AREA STR 49L, STRINGER HAS 5 SQ INCHES OF CORROSION. REMOVED CORROSION AFT OF FRAME 75 FOUND TO BE OUT OF LIMITS IAW A310-200 SRM 53-10-00 FIG 104, TABLE 102. REMOVED AND REPLACED STRINGER SECTION WITH NEMar 31, 2005 · N402FE · Airbus A310SDR 05FDEA00751Stringer · corrodedAREA BEHIND BULK CARGO BETWEEN FRAMES 72-74 LEFT SIDE AT STRINGER 48 HAS 15 SQ INCHES OF CORROSION. REMOVED CORROSION FR 72-74 FOUND TO BE OUT OF LIMITS IAW A310-200 SRM 53-10-00 FIG 104. REMOVED AND REPLACED STRINGER SECTION 48L FR 72 TO 78 IAW A310-200 SMar 31, 2005 · N402FE · Airbus A310SDR 05FDEA00748Stringer · corrodedAFT OF BULK CARGO BILGE AREA STGR 53 LT HAS 2 AREAS OF CORROSION BETWEEN FR 70-71. REMOVED REQUIRED FASTENERS AND REMOVED CORROSION IAW A310-200 SRM 51-40-21 AND SRM 51-74-10. MATERIAL LOSS AFTER CORROSION REMOVAL WENT OUT OF LIMITS IAW A310-200 SRM 53-10-00Mar 31, 2005 · N402FE · Airbus A310SDR 05FDEA00747Stringer · corrodedAFT OF BULK CARGO AT BILGE AREA, STRINGER 56 LT HAS NUMEROUS CORROSION ON STRINGER'S. RUNS THROUGH FRAME 70-71 AND FRAME 72, AS MARKED. REMOVED FASTENERS ON STR 56 LT AT FR 70-71 AND 72 IAW A310-200 SRM 51-40-21. REMOVED CORROSION IAW A310-200 SRM 51-74-10Mar 31, 2005 · N402FE · Airbus A310SDR USAA050532Stringer · corrodedBFM - FOUND STRINGER CORRODED 8 INCHES LONG BY 1 INCH WIDE BY .035 INCH DEEP AREA, BS 967, STRINGER 25L. INSTALLED NEW STRINGER SECTION AND REPAIR SPLICE PER SRM 53-00-03. (M)Mar 30, 2005 · N374US · Boeing 7373B7
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