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 ASOA2012071301891Stringer · corrodedAVIONICS COMPARTMENT, STRINGER 26R IS CORRODED BETWEEN FS 333-349. REMOVED CORROSION IAW SRM 51-21-06-001-001-0-A01, OUT OF LIMITS IAW SRM 53-21-03-101-02-A01. REMOVED STRINGER IAW SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01. INSTALLED NEW STRIJun 25, 2012 · N744EV · Cndair CL6002C10SDR ASOA2012071001881Stringer · corrodedSTRINGER 25L IS CORRODED BETWEEN FS 319.00-333.00. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01. PERFORMED UT THICKNESS INSPECTION OF BLEND AREA IAW MAC NDT PROCEDURES UT-3, MIN MATERIAL REMAINING IS .038", ORIGINAL IS .063:, MATERIAL REMOVED IS .025". RJun 25, 2012 · N744EV · Cndair CL6002C10SDR ASOA2012071001880Stringer · corrodedSTRINGER 26L IS CORRODED BETWEEN FS 319.00-333. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01. PERFORMED UT THICKNESS INSPECTION OF BLEND AREA IAW MAC NDT INSPECTION PROCEDURES UT-3, MIN MATERIAL REMAINING IS .052", ORIGINAL IS .063:, MATERIAL REMOVED IS Jun 25, 2012 · N744EV · Cndair CL6002C10SDR ASOA2012071001879Stringer · corrodedSTRINGER 26R IS CORRODED BETWEEN FS 319 - 333. REMOVED CORROSION IAW SM 51-21-06-001-001-0-A01, OUT OF LIMITS IAW SRM 53-21-03-101-02-A01. REMOVED STRINGER IAW SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01. DRILLED EXISTING HOLES IN NEW STRINGER IAW Jun 25, 2012 · N744EV · Cndair CL6002C10SDR ASOA2012071001878Stringer · corrodedSTRINGER 25 RIGHT IS CORRODED BETWEEN FS 319-333. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01. PERFORMED UT THICKNESS INSPECTION OF BLEND AREA IAW MAC NDT INSPECTION PROCEDURE UT-3. MIN MATERIAL REMAINING IS .042", ORIGINAL IS .063:, MATERIAL REMOVED ISJun 25, 2012 · N744EV · Cndair CL6002C10SDR UALA2012062903443Stringer · corrodedSTRINGER 41R AT FR 61-62 HAS CORROSION. REPLACED STRINGER SECTION 41R FR 58-64 PER SRM. MAJOR REPAIR.Jun 25, 2012 · N458UA · Airbus A320232SDR UALA2012062903442Stringer · corrodedSTRINGER 40R AT FR 65-66 HAS CORROSION. REPLACED STRINGER PER SRM. MAJOR REPAIRJun 25, 2012 · N458UA · Airbus A320232SDR UALA2012062903401Stringer · corrodedSTRINGER 41R AT FR 61-62 HAS CORROSION. REPLACED STR SECTION 41R FR 58-64. MAJOR REPAIR.Jun 25, 2012 · N458UA · Airbus A320232SDR UALA2012062903400Stringer · corrodedSTRINGER 40R AT FR 65-66 HAS CORROSION. REPLACED STRINGER PER SRM, MAJOR REPAIRJun 25, 2012 · N458UA · Airbus A320232SDR SWAA2012072006025Stringer · corrodedSTRINGER CORRODED AT BS 952, STR 20R. REPAIRED STRINGER PER SRM.Jun 24, 2012 · N644SW · Boeing 7373H4SDR SWAA2012071705909Stringer · corrodedSTRINGER CORRODED AT BS 540, STR 26R. REPAIRED STRINGER IAW SRM.Jun 24, 2012 · N772SW · Boeing 7377H4SDR QXEA2012062400549Stringer · corrodedSTRINGER 30P HAS CORROSION BETWEEN STA X-39.00 AND X-18.250. REMOVED STRINGER SPLICE IAW SRM 51-42-05-02-01. FOUND SPLICE OUT OF LIMITS. REMOVED CORROSION ON STRINGER IAW SRM 51-21-00-00-02. VERIFIED STRINGER TO BE CRACK FREE REF NTM 51-00-06-910-801 PT 1.Jun 24, 2012 · N404QX · Bombdr DHC8402SDR QXEA2012062400548Stringer · corrodedSTRINGER 31P HAS CORROSION BETWEEN STA X39.00 AND X -18.250. REMOVED CORROSION IAW SRM 51-21-00-00-02. MIN REMAINING THICKNESS .075' CONFIRMED AREA CRACK FREE REF NTM 51-00-04-910-801 AND 51-00-06-910-801 PT 1. FOUND TO BE IN LIMITS IAW RD 8/4-53-4576.Jun 24, 2012 · N404QX · Bombdr DHC8402SDR DALA1238640934Longeron · crackedDURING HMV, A CRACKED LONGERON WAS FOUND LONGERON 12 LT AT INTERSECTION WITH FRAME 1437. LONGERON WAS REMOVED FROM BS 1437 TO 1448 AND SPLICED IN NEW LONGERON IAW SRM 53-02 FIG 18.Jun 24, 2012 · N934DL · Doug MD88SDR DALA1238630934Longeron · crackedDURING HMV, A CRACK WAS FOUND ON LONGERON 4 LT AT INTERSECTION WITH FRAME BS 1437. REMOVED LONGERON FROM BS 1432 TO 1448 AND SLICED IN NEW LONGERON IAW SRM 53-02 FIG 18.Jun 24, 2012 · N934DL · Doug MD88SDR IPXA12M74267Longeron Fitting · corrodedINSPECTION TYPE: 4C, LONGERON 26R FITTING BETWEEN FS 1199-1219 IS CORRODED AND CRACKED AT AFT END. REPAIRED LONGERON 26R AT BS 1199-1219, REF EA 011-5310-01-A4017 I/R AND EO MD11-5310-47768-A, 8110-3.Jun 23, 2012 · N288UP · Doug MD11FSDR SWAA2012070905645Stringer · corrodedSTRINGER CORRODED AT BS 910, STR 27L. REPAIRED STRINGER IAW SRM.Jun 23, 2012 · N644SW · Boeing 7373H4SDR AALA20120623010Longeron · crackedLONGERON 3 LEFT CRACKED AT FRAME 160. INSTALLED NEW LONGERON 3 LEFT AND PRE-EXISTING SPLICE DOUBLER FROM STATIONS 148 TO 178 PER SRM 53-02-00 FIGURE 18 AND E.A. MD80-53-024548.Jun 23, 2012 · N485AA · Doug DC982SDR MASA2012062534936Stringer · corrodedSTRINGER 25R BETWEEN FS 310.00 AND FS 349.00 HAS SEVERAL AREAS OF CORROSION. INSTALLED STRINGER IAW SRM 51-42-06-001-001-A01.Jun 23, 2012 · N509MJ · Cndair CL6002C10SDR MASA2012062534935Stringer · corrodedSTRINGER 26R BETWEEN FS 333.00 AND FS 364.00 HAS SEVERAL AREAS OF CORROSION, FS 333.00-364.00.Jun 23, 2012 · N509MJ · Cndair CL6002C10SDR MASA2012062234925Stringer · corrodedSTRINGER 26R IS CORRODED FROM FS 333.00 TO 364.00. INSTALLED AVIONICS FLOOR PANEL IAW AMM 53-00-47-400-801. INSTALLED NEW SERVICEABLE FWD SUPPORT ANGLE IAW SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01.Jun 21, 2012 · N509MJ · Cndair CL6002C10SDR MASA2012062234924Stringer · corrodedSTRINGER 26R BETWEEN FS 280.00 AND 333.00 HAS SEVERAL AREAS OF CORROSION. INSTALLED AVIONICS FLOOR PANEL 181ALF IAW AMM 53-00-47-400-801. INSTALLED NEW SERVICEABLE FWD SUPPORT ANGLE IAW SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01.Jun 21, 2012 · N509MJ · Cndair CL6002C10SDR SWAA2012070905637Stringer · corrodedSTRINGER CORRODED AT BS 773, RBL 8. REPAIRED STRINGER IAW EA.Jun 20, 2012 · N772SW · Boeing 7377H4SDR IPXA2M74226Longeron Splice · crackedINSPECTION TYPE: 4C, CENTER CARGO BAY LONGERON 38R SPLICE FITTING CRACKED AT FS 1531/5-11 6. FABRICATED AND REPLACED SPLICE FITTING AT STA 1531/5-116 AND L38R REF SRM 51-33-01, PARA 9, PG 45, SRM 51-33-01 PARA 8, PG 30 AND DWG A5A7114.Jun 19, 2012 · N288UP · Doug MD11FSDR REXA2012061900946Stringer · corrodedSTRINGER 27 CORRODED, FS 250 TO 265. REPAIRED STRINGER IAW EO NR R53203.Jun 19, 2012 · N905XJ · Cndair CL6002D24SDR IPXA2574107Stringer · damagedINSPECTION TYPE: C, STRINGER 25R JUST AFT OF BS 680 HAS MINOR DAMAGE ON SIDE OF STRINGER. REPAIRED STRINGER IAW EA 120803 IR AND EO B757-5310-47667-A.Jun 18, 2012 · N422UP · Boeing 75724APFSDR DALA1238019264Stringer · corrodedE/E COMPARTMENT STRINGER 29L STA 160-200 HAS SPOTS OF CORROSION. REPAIRED PER 53-10-01 FIG 7 ON NR 1000/419/1016165.Jun 18, 2012 · N964DN · Doug MD9030SDR DALA1237999264Longeron · corrodedE/E COMPARTMENT L 28 FS 170-180 HAS SPOTS OF CORROSION. REPAIRED PER SRM 53-10-01 FIG 7.Jun 18, 2012 · N964DN · Doug MD9030SDR DALA1237979264Longeron · corrodedE/E COMPARTMENT L30 FROM FS 160 - 200 HAS SPOTS OF CORROSION. REPAIRED LONGERON PER SRM 53-10-01-FIG 7 ON NR 1000 10417 1016163.Jun 18, 2012 · N964DN · Doug MD9030SDR SWAA2012062505188Stringer Splice · crackedSTRINGER SPLICE CHANNEL CRACKED AT BS 360, STR 14L. REMOVED AND REPLACED CHANNEL IAW SRM AND DWG.Jun 16, 2012 · N399WN · Boeing 7373H4SDR MASA2012062534930Stringer · chafedSTRINGER 7L BETWEEN FS 1144.0 AND 1162.0 IS CHAFED .380, .400, .055D. REPAIRED PER EO CL600-2C10-53-LO1309.Jun 16, 2012 · N509MJ · Cndair CL6002C10SDR SWAA2012062205156Stringer · corrodedSTRINGER CORRODED BETWEEN BS 832 TO BS 851, BETWEEN STR 29R TO STR 29L. REPAIRED STRINGER PER SRM AND DWG.Jun 16, 2012 · N954AT · Boeing 717200SDR SWAA2012062205154Stringer · corrodedSTRINGER CORRODED AT BS 832, STR 27R. REPAIRED STRINGER PER SRM AND DWG.Jun 16, 2012 · N954AT · Boeing 717200SDR USAA2012061900019Stringer · corrodedS2 CHECK - LEVEL 2 EXFOLIATION CORROSION ON STRINGER 41R BETWEEN FR34 TO FR35.8. SPLICED IN NEW SECTION OF STRINGER 41R BETWEEN FR34 TO FR35.8 IAW A321 SRM 51-42-11, 51-72-11 & AIRBUS DRAWING D53372500.Jun 16, 2012 · N161UW · Airbus A321211SDR DALA1242730927Longeron · crackedMAIN CABIN LONGERON CRACKED BS 522 L4L. REPLACED LONGERON SECTION BS 521-550 PER SRM 53-02 FIG 18.Jun 15, 2012 · N927DA · Doug MD88SDR SWAA2012070205471Stringer · crackedSTRINGER CRACKED AT BS 400+12, STR 3R. REPAIRED STRINGER IAW REO & EA.Jun 15, 2012 · N601WN · Boeing 7373H4SDR QXEA2012061500495Stringer · corrodedSTRINGER 33 CORRODED FROM X -18.25 TO X -34.1. REMOVED FASTENERS FOM IAW SRM 51-42-05-02-01. REMOVED CORROSION IAW SRM 51-21-00-00-02. CONFIRMED CRACK FREE AREA REF NTM 51-00-04-910-801 AND 51-00-06-910-801. FOUND TO BE WITHIN LIMITS IAW RD 8/4-53-4570. AJun 15, 2012 · N404QX · Bombdr DHC8402SDR QXEA2012061500494Stringer · corrodedSTRINGER 33, CORRODED FROM X-18.25 TO X1. REMOVED 3 RIVETS TO FOM IAW SRM 51-42-05-02-01. REMOVED CORROSION IAW SRM 51-21-00-00-01. CONFIRMED CRACK FREE REF 51-00-04-910-801 AND 51-00-06-910-801 PT 1. FOUND TO BE WITHIN LIMITS IAW RD 8/4-53-4570. ALODINED,Jun 15, 2012 · N404QX · Bombdr DHC8402SDR QXEA2012061500488Stringer · corrodedSTRINGER 28P AND SPLICE FWD OF STA -18.250 IS CORRODED. BLENDED CORROSION IAW SRM 51-21-00-00-02, 1 RIVET REMOVED FOM IAW SRM 51-42-05-02-01. CONFIRMED AREA CRACK FREE REF NTM 51-00-06-910-801 PT1. FOUND WITHIN LIMITS IAW RD 8/4-53-4571. ALODINED, PRIMED IJun 15, 2012 · N404QX · Bombdr DHC8402SDR QXEA2012061500487Stringer · corrodedSTRINGER 31S IS CORRODED FWD AND AFT OF STA -18.250. REMOVED CORROSION IAW SRM 51-21-00-00-02. BLENDED AREA CONFIRMED CRACK FREE REF NTM 51-00-06-910-801 PT 1. BLENDED AREA FOUND TO BE IN LIMITS IAW RD 8/4-53-4569. ALODINED IAW RD 8/4-53-4569. APPLIED PRIJun 15, 2012 · N404QX · Bombdr DHC8402SDR QXEA2012061500459Stringer · corrodedSTRINGER 29S HAS AREAS OF CORROSION BETWEEN STA 71.200 AND X94.800. REMOVED 30 RIVETS FOM IAW SRM 51-42-05-02-01 BLENDED CORROSION IAW SRM 51-21-00-00-02. PERFORMED HFEC OF BLENDS FOR CRACKS IAW NTM 51-00-06-910-801 PT 1. NO CRACKS NOTED. PERFORMED UT THICJun 15, 2012 · N404QX · Bombdr DHC8402SDR DALA1244240927Longeron · crackedMAIN CABIN LONGERON CRACKED BS 541 L4R. FABRICATED AND INSTALLED NWW LONGERON SECTION BS 531-550 IAW 53-02.Jun 14, 2012 · N927DA · Doug MD88SDR QXEA2012061400463Stringer · corrodedSTRINGER 30S HAS CORROSION BETWEEN STA X1.00 AND X19.400. REMOVED RIVETS FOM IAW SRM 51-42-05-02-01. REMOVED CORROSION IAW SRM 51-21-00-00-02. INSTALLED NEW STRINGER IAW SRM 51-42-05-02-01.Jun 14, 2012 · N404QX · Bombdr DHC8402SDR QXEA2012061400454Stringer · corrodedSTRINGER 32PC HAS CORROSION BETWEEN STA X-39.00 AND X-18.250. REMOVED STRINGER IAW SRM 51-42-05-02-1 AND FOUND TO BE OUT OF LIMITS. MATCH DRILLED NEW STRINGER IAW SRM 51-40-07-02-01. INSTALLED STRINGER IAW SRM 51-42-05-02-01. ALODINED, PRIMED AND PAINTED IJun 14, 2012 · N404QX · Bombdr DHC8402SDR DALA1237469256Longeron · crackedFOUND LONGERON 20L BS 1050 IS CRACKED. TRIMMED OUT DAMAGED AREA, FABRICATED TWO REPAIR ANGLES, SHIM AND INSTALLED REPAIR PARTS AT LONGERON 20 IAW SRM 53-10-01 FIG 9.Jun 14, 2012 · N956DN · Doug MD9030SDR AALA20120613018Longeron · corrodedLONGERON 28 RIGHT CORRODED AFT SIDE OF FRAME STATION 1287. SPLICE IN REPAIR PER SRM 53-02-00, 51-30-05 AND 51-30-02.Jun 13, 2012 · N479AA · Doug DC982SDR DALA1236460934Longeron · crackedDURING HMV, A CRACK WAS FOUND ON LONGERON 4 RT BS 541 OF INTERNAL FUSELAGE STRUCTURE. LONGERON WAS REPAIRED IAW SRM 53-02 FIG 18.Jun 11, 2012 · N934DL · Doug MD88SDR HNAA2012061100821Stringer Fitting · corrodedAREA OF HEAVY CORROSION AT STA X222 AND STR 26S. FOUND STRINGER END CLEAT CORRODED. REMOVED CLEAT. INSTALLED NEW CLEAT IAW DWG 85320983.Jun 11, 2012 · N912HA · Dhav DHC8102SDR UALA2012061103185Stringer · corrodedSTRINGER 43L CORRODED BETWEEN FR 32 AND 33. STRINGER REPLACED FROM FRAME 31 TO FRAME 35 PER SRM 51-42-11.Jun 10, 2012 · N426UA · Airbus A320232SDR DALA1243000635Stringer · gougedFWD CARGO COMPARTMENT STRINGER 21R HAS GOUGE BS 740-760. CW ERA 505287-14 REV ORIGINAL.Jun 9, 2012 · N635DL · Boeing 757232
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