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 DALA13008089204Stringer · crackedAFT AIRSTAIR AREA SKIN AT BS 1520 CANTED BULKHEAD STRINGER 4R IS CRACKED. REPAIRED STRINGER IAW ER/A 510924-14 REV O.Feb 16, 2013 · N904DA · Doug MD9030SDR DALA13008200939Longeron · corrodedCORROSION ON LONGERON 23L BS 1231 TO 1338. SECTION OF LONGERON WAS REPLACED IAW SRM 53-02, FIG 18.Feb 15, 2013 · N939DL · Doug MD88SDR V0XR20130219J0165Stringer · crackedSTRINGER LINTEL 3L CRACKED AT FS 281. COMPLIED WITH EC/TC SB 670BA-53-040-01 IN ACCORDANCE WITH SERVICE BULLETIN SB 670BA-53-040,REVISION C.Feb 15, 2013 · N717EV · Cndair CL6002C10SDR IPXA13M77225Longeron Splice · crackedINSPECTION TYPE:4C, LONGERON 25R SPLICE FITTING IS CRACKED AT FS 1129/6-0. FABRICATED AND REPLACED LONGERON SPLICE FITTING AT FS 1129/6-0 REF SRM 51-33-01, PAGES 30,31 AND DWG ADA8435.Feb 14, 2013 · N273UP · Doug MD11FSDR DALA13008500939Longeron · corrodedCORROSION ON LONGERON 24L FROM BS 1338 TO 1380 AT AFT ACCESSORY COMPARTMENT. CORROSION WAS REMOVED, FOUND IS OUT OF LIMITS. NEW SECTION OF LONGERON AND SPLICE WAS INSTALLED IAW SRM 53-02- FIG 18. RII COMPLETED.Feb 14, 2013 · N939DL · Doug MD88SDR IPXA13M77393Longeron · crackedINSPECTION TYPE:4C, LONGERON 24L CRACKED AND CORRODED AT BS 1531. REPAIRED LONGERON IAW SRM 52-00-05, REPAIR 1, FIG 202.Feb 13, 2013 · N273UP · Doug MD11FSDR REXA2013021300305Stringer · corroded900-53-140-300, STGR 26R HAS CORROSION BETWEEN FRAMES 349 AND 333, IN THE FWD E & E BAY. REMOVED AND REPLACED STGR FRAMES 349 & 333. IAW CRJ 900 SRM 51-42-06. P/N SH670-31372-4.Feb 13, 2013 · N929XJ · Cndair CL6002D24SDR REXA2013021300304Stringer Splice · corroded900-53-140-300, SPLICE ON STGR 25R HAS CORROSION AT FRAME 333, IN THE FWD E & E BAY. REMOVED AND REPLACED STGR 25R SPLICE IAW CRJ 900 SRM 51-42-06 EO R53277. P/N SH670-32429-3.Feb 13, 2013 · N929XJ · Cndair CL6002D24SDR REXA2013021300050Stringer · corroded900-53-140-300, STGR 26L HAS CORROSION BETWEEN FRAMES 349 AND 333, IN THE FWD E & E BAY. REMOVED & REPLACED STRINGER 26L FRAMES 349 & 333. IAW CRJ 900 SRM 51-42-06 AND EO R53277. P/N SH670-31372-3.Feb 13, 2013 · N929XJ · Cndair CL6002D24SDR DALA13007910990Longeron · corrodedLONGERON 28R 2 INCHES AFT OF FRAME BS 1287 CORRODED. BLENDED CORROSION. FOUND TO BE OUT LIMITS AND A REPAIR CHANNEL WAS INSTALLED IAW SRM 53-02, STEP 13.Feb 12, 2013 · N990DL · Doug MD88SDR DALA13008190939Longeron · corrodedCORROSION ON LONGERON 22L BS 1287. DAMAGED SECTION OF LONGERON WAS REPLACED, TREATED, PAINTED, AND INSTALLED IAW SRM 53-02 FIG 18 AND SRM 51-30-2 AND 51-30-5.Feb 11, 2013 · N939DL · Doug MD88SDR DALA1305833744Stringer · corrodedCORROSION FOUND AT S23L AT BS 305. REPAIRED IAW ERA 510950-14.Feb 9, 2013 · N3744F · Boeing 737832SDR DALA13006940941Longeron · corrodedCORROSION ON LONGERON 25L BS 1280-1309. LONGERON SECTION REPLACED IAW SRM 53-02, FIG 18.Feb 9, 2013 · N941DL · Doug MD88SDR UALA2013021100808Stringer · corrodedCORROSION IN AFT BULK CARGO BAY ON BILGE STRINGER 42L BETWEEN FR 65-66. REPAIRED STRINGER IAW SRM 53-00-13 FIG 201. MAJOR REPAIR.Feb 8, 2013 · N430UA · Airbus A320232SDR QXEA2013020800371Stringer · corrodedSTRINGER 32S HAS CORROSION AND CORRODED RIVETS BETWEEN STA X216 AND X236. REMOVED COMMON RIVETS TO STR 32S FROM STA X216 TO X236 IAW SRM 51-42-05-02-01 AND REMOVED CORROSION IAW SRM 51-21-00-00-02. MIN THICKNESS REMAINING .068", REF NDTM 51-00-04-910-801 PT 1Feb 8, 2013 · N411QX · Bombdr DHC8402SDR USAA2013021500005Stringer · corroded2S CHECK - 5 AREAS OF CORROSION ON STRINGER 41R AT FR35.7. REPAIRED STRINGER 41R AT FR35.7 IAW EA 204179.Feb 8, 2013 · N190UW · Airbus A321211SDR QXEA2013020800343Stringer · corrodedSTRINGER 32S IS CORRODED, STA 156 TO X 176. REMOVED RIVETS IAW SRM 51-42-05-02-01. MINIMUM THICKNESS REMAINING NOTED .068" REF NDTM PART 1, TASK 51-00-04-910-801 AND VERIFIED AFFECTED AREA TO BE CRACK FREE USING HFEC REF NDTM PART 1 TASK 51-00-06-910-801. OFeb 8, 2013 · N411QX · Bombdr DHC8402SDR DALA1303660125Fitting · damagedWHILE ACCOMPLISHING EA 01-499898-03 AD NEW LONGERON FITTING, WAS FOUND WITH SHORT EDGE MARGIN ON INBD FLANGE SIDE OF FITTING FASTENER HOLES. NEW REPLACEMENT LONGERON FITTING (PN 1114020-8) FABRICATED AND INSTALLED IAW PR1 509717-14 REV 0. DATED 19JAN13. REF Feb 8, 2013 · N125DL · Boeing 767332SDR SIMA20130208011Stringer Splice · corrodedDURING MAINTENANCE INSPECTION FOUND SPLICE STRINGER 18R CORRODED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED NEW STRINGER AT 18R BETWEEN FRAMES 14 & 14 IAW SRM 51-40-02. THE AIRCRAFT WAS RETURNED TO SERVICE.Feb 8, 2013 · N600BP · Emb EMB145LRSDR SIMA20130208010Stringer · corrodedDURING MAINTENANCE INSPECTION FOUND STRINGER 18 R IS CORRDED BETWEEN FRAMES 13 & 14. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED NEW STRINGER AT 18R BETWEEN FRAMES 13 & 14 IAW SRM 51-40-02. THE AIRCRAFT WAS RETURNED TO SERVICE.Feb 8, 2013 · N600BP · Emb EMB145LRSDR QXEA2013020700322Stringer · corrodedSTRINGER 24P HAS AREAS OF MISSING PAINT AND CORRODED RIVETS BETWEEN STA X428.500 AND X664. REMOVED CORRODED RIVETS AND STR CLIPS IAW SRM 51-42-05-02-01. REMOVED CORROSION IAW SRM 51-21-00-00-02. MIN THICKNESS NOTED .072, CONFIRMED CRACK FREE REF NTM 51-00-04Feb 7, 2013 · N411QX · Bombdr DHC8402SDR QXEA2013020700320Stringer · corrodedSTRINGER 24P HAS CORROSION BETWEEN STA X413 AND X428.500. REMOVED NECESSARY RIVETS AND END FITTING FOM IAW SRM 51-42-05-02-01 AND 51-40-15-02-01. REMOVED CORROSION IAW SRM 51-21-00-00-02. MIN THICKNESS NOTED .038" REF NTM 51-00-04-910-801 PT 1. REMOVED CLIPS AFeb 7, 2013 · N411QX · Bombdr DHC8402SDR SWAA2013022012891Stringer · crackedSTRINGER S2L CRACKED AT STA 727C DUE TO BULLET DAMAGE. CUT OUT DAMAGED SECTION OF STR 2L STA 727C FABRICATED, ALODINED & PRIMED. INSTALLED REPAIR PARTS, STRINGER SEGMENT BAC 1498-154 18" LONG PO#2301442 SPLICES 4EA .040 7075-0 20" LONG HT TREATED TO T6 COND Feb 7, 2013 · N261AT · Boeing 73776NSDR DALA13006930941Longeron · corrodedCORROISON FOUND ON LONGERON 24L BETWEEN BS 1271-1300, AFT CARGO BAY. LONGERON SECTION BETWEEN BS 1265-1331 WAS REPLACED IAW SRM 53-02, FIG 18.Feb 7, 2013 · N941DL · Doug MD88SDR WVER201302079301Stringer · crackedSTRINGER 3L IS CRACKED ON FWD EDGE JUST AFT OF FS 280.00 BULKHEAD. REPAIRED CRACKED STRINGER IAW BOMBARDIER SERVICE BULLETIN SB670BA-53-040 REV C, DATED SEP 20/2012.Feb 7, 2013 · N930L · Cndair CL6002D24SDR QXEA2013020600335Stringer · corrodedSTRINGER 31S IS CORRODED STA 71.2 TO 94.8. REMOVED RIVETS IAW SRM 51-42-05-02-01 AND REMOVED CORROSION IAW SRM 51-21-00-00-02. VERIFIED MIN REMAINING THICKNESS .048 REF NTM 51-00-04-910-801, PT 1. VERIFIED CRACK FREE REF SRM 51-00-06-910-801 PT 1. ALODINEFeb 6, 2013 · N411QX · Bombdr DHC8402SDR SWAA2013021912746Stringer · crackedSTRINGER 2L CRACKED AT STA 727C. CUT OUT DAMAGED SECTION OF STR 2L STA 727C, FABRICATED AND INSTALLED REPAIR PARTS, STRINGER SEGMENT, SPLICES IAW B737 SRM 53-00-03-2R-3.Feb 6, 2013 · N261AT · Boeing 73776NSDR DALA13006550941Longeron · corrodedCORROSION ON LONG 29R BETWEEN BS 1287-1338. LONGERON WAS REPLACED IAW DWG 596667 AND SRM 51-30-2 AND 51-30-5.Feb 6, 2013 · N941DL · Doug MD88SDR FDEA201302060275Longeron · crackedFOUND THREE CRACKS IN AREA"C" OF INNER FLANGE OF THE LONGERON AT STRINGER 11 B/W, FR75 AND FR75A ON LT SIDE CUT OUT THE CRACK FLANGE AND SPLICE REPAIR IAW SRM53-18-18/201, FIG 205C.Feb 6, 2013 · N719FD · Airbus A300B4622SDR ERAA20130011Stringer · corrodedCORROSION AT FUSELAGE STRINGER 29P BETWEEN X291 AND X312. REMOVED CORROSION AND REPAIRED REF BOMBARDIER SRM.Feb 6, 2013 · N883EA · Dhav DHC8106SDR FDEA201302050266Longeron · corrodedLOWER CENTER CARGO COMPARTMENT BILGE AREA FOUND LONGERON 51R WITH CORROSION AT BS 1701. REPAIRED IAW SRM 53-00-05 FIGURE 201 TYPE REVISION 51 AND EA 1- 5300-163002. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100 REVISION 116.Feb 5, 2013 · N527FE · Doug MD11FSDR QXEA2013020500317Stringer · corrodedSTRINGER 24P HAS AREAS OF MISSING PAINT AND CORRODED RIVETS BETWEEN STA X196 AND X413. REMOVED NECESSARY RIVETS IAW SRM 51-42-05-02-01. CLEANED STR IAW SRM 51-26-00-02-01. CORROSION LIMITS TO RIVETS ONLY NO CORROSION ON STRINGER AREA. PRIMED STRINGER 24P IAFeb 5, 2013 · N411QX · Bombdr DHC8402SDR QXEA2013020500290Stringer · corrodedSTRINGER 31P BS -18.25 X1.00 HAS CORROSION. REMOVED RIVETS TO FOM IAW SRM 51-42-05-02-01 AND BLENDED CORROSION IAW SRM 51-21-00-00-02. MIN REMAINING THICKNESS .062" REF NDTM 51-00-04-910-801 PT 1. HFEC INSPECTED BLENDS, NO CRACKS DETECTED REF NDTM 51-00-06-Feb 5, 2013 · N411QX · Bombdr DHC8402SDR QXEA2013020500285Stringer · corrodedSTRINGER 32P HAS CORROSION BETWEEN STA X236 AND X258.500. REMOVED RIVETS FOM IAW SRM 51-42-05-02-01. REMOVED CORROSION IAW SRM 51-21-00-00-02. MIN THICKNESS NOTED .068", CONFIRMED CRACK FREE REF NTM 51-00-04-910-801 PT 1 AND 51-00-06-910-801 PT 1. ALODINED, PFeb 5, 2013 · N411QX · Bombdr DHC8402SDR QXEA2013010500281Stringer · corrodedSTRINGER 28S, HAS CORROSION STA X-39 TO X-18.25. REMOVED NECESSARY RIVETS IAW SRM 51-42-05-02-01. REMOVED Z-CHANNEL IAW SRM 51-42-05-02-01 AND REMOVED CORROSION IAW SRM 51-21-00-00-02. FOUND OUT OF LIMITS IAW SRM 53-10-33-00-01, MATCH DRILLED NEW Z CHANNEL IAFeb 5, 2013 · N411QX · Bombdr DHC8402SDR DALA13006960941Longeron · corrodedCORROSION ON LONGERON 22L BS 1287 AND 1307 AT AFT CARGO BAY. LONGERON REPAIRED IAW SRM 53-02, FIG. 18.Feb 5, 2013 · N941DL · Doug MD88SDR AALA20130205008Longeron · crackedCRACK IN LONGERON AT STATION 200, LONGERON 7 RIGHT. REMOVED LONGERON SECTION AND INSTALLED NEW LONGERON SECTION AND SPLICE FROM STATIONS 180 TO 230 PER SRM 53-02-00, FIGURE 18.Feb 5, 2013 · N569AA · Doug DC983SDR DALA13006540939Longeron · crackedCRACK ON LONGERON 4R BS 905. DAMAGE LONGERON WAS REPAIR IAW SRM 53-02, FIG 18 AND INSTALLED WITH SRM 51-30-2 AND 51-30-5.Feb 4, 2013 · N939DL · Doug MD88SDR SWAA2013020712359Stringer Splice · crackedMAIN CABIN - PRODUCTION SPLICE AT BS 908 STRINGER 4R IS CRACKED. REMOVED & REPLACED STRINGER SPLICE PER SRM AND DRAWING.Feb 4, 2013 · N606SW · Boeing 7373H4SDR DALA1305443744Stringer · wornFWD CARGO BS 417, STR 26 HOLE WORN INBD FREE FLANGE. REPAIRED STRINGER IAW SRM 53-00-03, REPAIR 1.Feb 2, 2013 · N3744F · Boeing 737832SDR DALA1305253743Stringer · wornFWD CARGO BAY BS 417, S26R HAS A HOLE WORN THROUGH INBD FREE FLANGE. REPAIRED STRINGER IAW SRM 53-00-03, REPAIR 1.Feb 2, 2013 · N3743H · Boeing 737832SDR UALA2013020400640Stringer · corrodedSTRINGER 43R HAS CORROSION AT FR 27. REPLACED FACTORY STRINGER SECTION FROM FRAME 24 TO 27. MAJOR REPAIR.Feb 2, 2013 · N430UA · Airbus A320232SDR DALA13005893213Stringer · corrodedDURING INSPECTION, FOUND AFT CARGO FRAME 56-57, STR 41L HAS CORROSION. REMOVED CORROSION IAW SRM 51-74-00. CHECKED DAMAGE DIMENSION S L=5.0" W=1.0"D=0.012". NO ESTABLISHED LIMITS IN SRM. REPLACED STRINGER IAW SRM 51-42-11 AND DWG D53470345.Feb 2, 2013 · N313US · Airbus A320211SDR CALA2013020400082Stringer · corrodedFWD CARGO HAS CORROSION AT STA 457 INSIDE S-28L CUT OUT SECTION OF CORROSION. STRINGER 28L, FROM STA 454 TO 460. FABRICATED AND INSTALLED HAT SECTION SPLICE, FILLER AND STRINGER CLIP REF SRM 53-00-03, REPAIR 1.Feb 2, 2013 · N18220 · Boeing 737824SDR QXEA2013020100324Stringer · corrodedSTR 25P, CORRODED BETWEEN STA 1.0 AND 6.7 AND BETWEEN STA 26.7 AND 32.4. FOUND CORROSION DAMAGE TO BE OUT OF LIMITS IAW SRM 53-20-17-00-01. REMOVED STRINGER SECTION IAW SRM 51-40-15-02-01. CONFIRMED STRINGER CUT LINES CRACK FREE REF NTM 51-00-06-910-801 PT Feb 1, 2013 · N411QX · Bombdr DHC8402SDR QXEA2013020100266Stringer · corrodedSTRINGER 30P HAS CORRODED RIVETS STA 49.5 TO X 94.8. REMOVED RIVETS IAW SRM 51-42-05-02-01. INSTALLED RIVETS IAW SRM 51-42-05-02-01. APPLIED PRIMER AND TOP COAT TO RIVETS IAW SRM 51-25-10-02-01 AND 51-25-15-02-01. APPLIED EXTERIOR TOP COAT TO OUTER SKIN IAFeb 1, 2013 · N411QX · Bombdr DHC8402SDR QXEA2013020100265Stringer · corrodedSTRINGER 24P HAS AREAS OF CORROSION AND CORRODED RIVETS STA X 49.5 TO X 196. REMOVED FASTENERS FOM IAW SRM 51-42-05-02-01. CLEANED AND FOUND CORROSION TO BE LIMITED TO FASTENERS ONLY IAW SRM 51-42-05-02-01 AND 51-21-00-00-02. REMOVED STRINGER CLIP FOM IAW SFeb 1, 2013 · N411QX · Bombdr DHC8402SDR QXEA2013020100263Stringer · corrodedSTRINGER 29S IS CORRODED STA X 32.4 TO X 71.2. REMOVED RIVETS FROM STRINGER SECTION IAW SRM 51-42-05-02-01. CLEANED STRINGER IAW SRM 51-26-00-02-01. NO CORROSION NOTED. APPLIED SURFACE PROTECTION TO STRINGER IAW SRM 51-25-10-02-01 AND 51-25-15-02-01. INSTFeb 1, 2013 · N411QX · Bombdr DHC8402SDR QXEA2013020100260Stringer · corrodedSTRINGER 31P HAS CORRODED RIVETS STA X 1.0 TO 19.4. REMOVED 3 CORRODED RIVETS IAW SRM 51-42-05-02-01. INSTALLED RIVETS IAW SRM 51-42-05-02-01. APPLIED ALUMINIZED PAINT IAW SRM 51-25-15-02-01, APPLIED EXTERNAL TOP COAT IAW SRM 51-25-15-02-01.Feb 1, 2013 · N411QX · Bombdr DHC8402SDR QXEA2013020100254Stringer · corrodedSTRINGER 33 IS CORRODED STA X-18.25 TO X1.0. REMOVED RIVETS FROM STRINGER IAW SRM 51-42-05-02-01. REMOVED CORROSION IAW SRM 51-21-00-00-02. FOUND STRINGER 33 AT STA X-18.25 TO X1.0 TO BE OUT OF LIMITS IAW SRM 53-20-03-00-01. CUT OUT DAMAGED STRINGER SEGMENFeb 1, 2013 · N411QX · Bombdr DHC8402
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