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 UPS05443827Stringer · corrodedBS 1560 TO 1580 AFT LT WINDOW FORGING REMOVED FOUND STR CORROSION. CORROSION BLEND OUT 0.040 INCH BY 1" BY 5" EXCEED SRM LIMIT. NEW STRINGER SEGMENT AND SPLICE ANGLE INSTALLED AS PER RS R-53-61-35239 AND ENGINEERING FILE NUMBER : 747-53-20222.Jan 13, 2005 · N675UP · Boeing 747123FSDR UPS05443826Stringer · crackedBS 1438 TO 1460 AFT RT WINDOW FORGING REMOVED FOUND STR CORROSION CRACKED. CORROSION BLEND OUT 0.100" BY 1" BY 5" EXCEED SRM LIMIT. NEW STRINGER SEGMENT, REPAIR STRAP AND SPICE ANGLE INSTALLED AS PER RS R-53-41-35248 AND ENGINEERING FILE NUMBER : 747-53-2022Jan 13, 2005 · N675UP · Boeing 747123FSDR UPS05443825Stringer · crackedBS 1220 TO 1240 AFT RT WINDOW FORGING REMOVED FOUND STR CORROSION CRACKED. CORROSION BLEND OUT 0.080" BY 1" BY 5" EXCEED SRM LIMIT. NEW STRINGER SEGMENT, SPLICE ANGLE AND REPAIR STRAP INSTALLED AS PER RS R-53-41-35245 AND ENGINEERING FILE NUMBER : 747-53-202Jan 13, 2005 · N675UP · Boeing 747123FSDR UPS05443815Stringer · crackedBS 1020 TO 1040 AFT RT WINDOW FORGING REMOVED FOUND STR CORROSION CRACKED. CORROSION BLEND OUT 0.100 BY 1 BY 10 INCHES EXCEED SRM LIMIT. ALL REPAIR PARTS AND NEW STRINGER SEGMENT INSTALLED AS PER RS R-53-41-35252 AND ENGINEERING FILE NUMBER : 747-53-20221.Jan 13, 2005 · N675UP · Boeing 747123FSDR UPS05443814Stringer · corrodedBS 1080 TO BS 1100 AFT RT WINDOW FORGING REMOVED FOUND STR CORROSION CRACKED. CORROSION BLEND OUT 0.100" BY 1" BY 5" EXCEED SRM LIMIT. ALL REPAIR PARTS AND NEW STRINGER SEGMENT INSTALLED AS PER RS R-53-41-35252 AND ENGINEERING FILE NUMBER : 747-53-20221.Jan 13, 2005 · N675UP · Boeing 747123FSDR UPS05443804Stringer · corrodedINSPECTION TYPE:C M/D BS 1580 TO BS 1600 AFT RT WINDOW FORGING REMOVED FOUND STRINGER CORROSION CRACKED. CORROSION BLEND OUT 0.100 X 1 X 10 EXCEED SRM LIMIT. STRINGER SEGMENT AND SPLICE ANGLE REWORKED REFER COMPONENT WORK PROCESS CARD SEQUENCE NR HE70480-1, Jan 13, 2005 · N675UP · Boeing 747123SDR UPS05443803Stringer · corrodedINSPECTION TYPE:C BS 1560 TO BS 1580 AFT RT WINDOW FORGING REMOVED FOUND STRINGER CORROSION CRACKED. CORROSION BLEND OUT 0.060 X 1 X 7 INCH, EXCEED SRM LIMIT. FLAP PEEN CARRIED OUT AS PER SRM 51-10-07 AND SOPM 20-10-03, STRINGER SEGMENT AND SPLICE ANGLE REWOJan 13, 2005 · N675UP · Boeing 747123SDR USAA050202Stringer · crackedPIT - FOUND STRINGER CRACKED .25 INCH, STATION 907 STRINGER 4R. DOUBLER INSTALLED PER SRM 53-00-03 FIG 201. (M)Jan 12, 2005 · N436US · Boeing 7374B7SDR 05FDEA00082Stringer · corrodedBS 640, RBL 15 WL 154 CORROSION ON STRINGER. REPAIRED PER SRM 53-10-3Jan 12, 2005 · N235FE · Boeing 727200SDR 05FDEA00085Longeron · dentedMAIN DECK, LONGERON 18L AT STA Y= 535 FOUND WITH DENT. FOUND MOUNTING FASTENER LOOSE LONGERON 18L AT STA Y= 535 - LOOSE FASTENERS REMOVED AND REPLACED PER SRM 51-31-01 VOLUME IJan 12, 2005 · N605FE · Doug MD11SDR GTIA050034Stringer · crackedAFT ACCESSORY COMPARTMENT STATION 1418 STRINGER 2R CRACKED. CUT AND REMOVED CRACKED STRINGER 2R STATION 1418, LOCATED AND DRILLED NEW STRINGER AND REPAIR SPLICE. TREATED, PRIMED AND INSTALLED. (M)Jan 11, 2005 · N800NK · Doug DC982SDR 05FDEA00075Stringer · corrodedBS 720F, STR 23R STRINGER CORROSION (C53-111-01). *S/D* CORROSION 100 PERCENT IN MATERIAL REMOVED AND REPLACED STRINGER PER SRM 53-10-2 & 51-30-2.Jan 11, 2005 · N235FE · Boeing 727200SDR 05FDEA00071Stringer · corrodedBS 720E PLUS 12 - BS, STR 23R CORROSION. CORROSION 100 PERCENT IN MATERIAL REMOVED AND REPLACED STRINGER PER SRM 53-10-2 AND 51-10-2.Jan 11, 2005 · N235FE · Boeing 727200SDR 05FDEA00068Stringer · corrodedBS 720D PLUS 18, STR 23R STRINGER CORROSION. REMOVED & FABRICATED NEW STRINGER AND 2 HAT CHANNELS SRM 53-10-2, 51-30-2.Jan 11, 2005 · N235FE · Boeing 727200SDR 05FDEA00072Stringer · corrodedBS 675, STR 27R CORROSION ON STRINGER. *S/D* REPAIRED PER SRM 53-10-3.Jan 11, 2005 · N235FE · Boeing 727200SDR 2005UALA00047Stringer · crackedSTATION 482 STRINGER 16R IS CRACKED. INSTALLED SPLICED REPAIR.Jan 10, 2005 · N905UA · Boeing 737522SDR 2005F00029Stringer · corrodedIG CORROSION ON SRTINGER 27L AT STATION 950 LBL5 )LEVEL2)Jan 10, 2005 · N233TM · Boeing 737282SDR 2005F00028Stringer · corrodedSTRINGER 23L AT STA 950 BL 10L HAS IG CORROSION(LEV. 2)Jan 10, 2005 · N233TM · Boeing 737282SDR SIMA200501904Stringer · chafedDURING AN IMBV MAINTENANCE FOUND A PREVIOUS REPAIR ON STRINGER 19R AT JUNCTION 5 BETWEEN FRAMES 52 AND 53 WAS FOUND CHAFED. REMOVED THE EXISTING DAMAGED REPAIR ANGLE AND SHIMS. FABRICATED A REPAIR ANGLE AND 2 SHIMS. REPAIR DONE IAW SRM. (SW21200502482) (K)Jan 9, 2005 · N735TS · Emb EMB135LRSDR UPS05843835Longeron · crackedLONGERON 36 HAS 1 INCH CRACK ON RT UPPER FLANGE IN RADIUS BETWEEN F/S 1260-1280. REMOVED AND REPLACED DAMAGED LONGERON SECTION IAW DWG 5750322 AND SRM 51-1-20D FROM F/S 1260-1360 L36.Jan 8, 2005 · N701UP · Doug DC871FSDR UPS05443812Stringer · crackedBS 1482 - 1485, STR 13R, STRINGER END FOUND CRACK. STRINGER REPAIRED PER RS 53-41-35250 AND ENGINEERING FILE NUMBER 747-53-20214.Jan 8, 2005 · N675UP · Boeing 747123SDR UPS05443808Stringer · crackedBS 1480 - 1485, S6L, STRINGER END FOUND CRACKED. STRINGER REPAIRED PER RS R53-41-35249 AND ENGINEERING FILE NUMBER 747-53-20215.Jan 8, 2005 · N675UP · Boeing 747123FSDR UPS05443773Stringer · crackedINSPECTION TYPE:C - BS 736 - 738, S23R STRINGER END FOUND CRACK. M/D BS 736 TO BS 738 S-23R STRINGER END REPAIRED AS PER RS 53-61-35230 AND ENGINEERING FILE NUMBER 747-53-20204.Jan 8, 2005 · N675UP · Boeing 747123SDR UPS05443720Stringer · crackedINSPECTION TYPE:C M/D - STR END BS 739 S-8L CRACKED. CRACKED STRINGER REPAIRED PER RS 53-21-35238 AND ENGINEERING FILE NUMBER 747-53-20206.Jan 8, 2005 · N675UP · Boeing 747123SDR UPS05443666Stringer · crackedINSPECTION TYPE:C - STRINGER END BS 990 S-7L CRACKED. STRINGER REPAIRED PER SRM 53-10-03 FIG 2.Jan 8, 2005 · N675UP · Boeing 747123SDR UPS05443665Stringer · crackedINSPECTION TYPE:C - STRINGER END BS 990 S-9L CRACKED. STRINGER REPAIRED PER SRM 53-10-03 FIG 2.Jan 8, 2005 · N675UP · Boeing 747123SDR UPS05443660Stringer · crackedINSPECTION TYPE:C U/D - BS 680, S9R, STRINGER END FOUND CRACK. STRINGER REPAIRED PER SRM 53-10-03 FIG 2.Jan 8, 2005 · N675UP · Boeing 747123SDR UPS05443657Stringer · crackedINSPECTION TYPE:C U/D - BS 620, S9R, STRINGER END FOUND CRACK. STRINGER REPAIR PER SRM 53-10-03 FIG 2.Jan 8, 2005 · N675UP · Boeing 747123SDR UPS05443656Stringer · crackedINSPECTION TYPE:C U/D - BS 560, S9R, STRINGER END FOUND CRACK. STRINGER REPAIR PER SRM 53-10-03 FIG 2.Jan 8, 2005 · N675UP · Boeing 747123SDR UPS05443655Stringer · crackedINSPECTION TYPE:C - BS 640, S9R, STRINGER END FOUND CRACK. STRINGER REPAIR PER SRM 53-10-03 FIG 2.Jan 8, 2005 · N675UP · Boeing 747123SDR UPS05443652Stringer · crackedINSPECTION TYPE:C - BS 736 - 738, S8R, STRINGER END FOUND CRACK. STRINGER REPAIRED PER SRM 53-10-03 FIG 2.Jan 8, 2005 · N675UP · Boeing 747123SDR UPS05843836Longeron · crackedMAIN CABIN LONGERON CRACKED AT STA 1760 L15L. REMOVED DAMAGED SECTION OF LONGERON AND FABRICATED SPLICE AND LONGERON SECTION INSTALLED IAW SRM'S 53-2-2 FIG10, 51-1-21, 53-2-0,51-1-20D AND DC8-53B-OO9-39.Jan 7, 2005 · N701UP · Doug DC871FSDR UPS05443824Stringer · crackedSTR END BS 1476 S-6L CRACKED. CRACKED STRINGER REPAIRED PER RS R53-41-35242 AND ENGINEERING FILE NUMBER : 747-53-20217.Jan 7, 2005 · N675UP · Boeing 747123FSDR UPS05443817Stringer · crackedSTR END BS 1003 S-3L CRACKED. STRINGER REPAIRED PER RS R-53-41-35231 AND ENGINEERING FILE NUMBER 747-53-20216.Jan 7, 2005 · N675UP · Boeing 747123FSDR UPS05443811Stringer · crackedSTR END BS 1485 S-8L CRACKED. STRINGER REPAIRED PER RS 53-1-35249 AND ENGINEERING FILE NUMBER 747-53-20215.Jan 7, 2005 · N675UP · Boeing 747123FSDR UPS05443810Stringer · crackedBS 1480 - 1500 S8R STRINGER END FOUND CRACKED. STRINGER REPAIRED AS PER HX RS R-53-41-35249 AND ENGINEERING FILE NUMBER: 747-53-20215.Jan 7, 2005 · N675UP · Boeing 747123FSDR UPS05443809Stringer · crackedBS 1460 - 1480 S8R STRINGER END FOUND CRACKED. STRINGER REPAIRED PER RS R53-41-35249 AND ENGINEERING FILE NUMBER 747-53-20215.Jan 7, 2005 · N675UP · Boeing 747123FSDR UPS05443767Stringer · crackedINSPECTION TYPE:C M/D - BS 742 - 744 STR 23R, STRINGER END FOUND CRACK. M/D BS 742 TO BS 744 S-23R STRINGER END REPAIRED AS PER RS : 53-61-35230 AND ENGINEERING FILE NUMBER 747-53-20204.Jan 7, 2005 · N675UP · Boeing 747123SDR UPS05443713Stringer · crackedINSPECTION TYPE:C - BS 1000 TO 1020 S10R STRINGER END FOUND CRACKED. M/D BS 1000 TO BS 1030 STR 10R STRINGER REPAIR CARRIED OUT IAW SRM 53-10-03 FIG 4.Jan 7, 2005 · N675UP · Boeing 747123SDR SIMA200501206Stringer · damagedDURING AN INSPECTION THE HOLDING STRINGER AT FRAME 50 AND STRINGER 13L WAS FOUND TO HAVE ONE DAMAGED HI-LOCK HOLE. REMOVED DAMAGED HOLDING STRINGER. INSTALLED NEW FASTENER IAW SRM. (SW21200502478) (K)Jan 7, 2005 · N654AE · Emb EMB145LRSDR UPS05443692Longeron · crackedINSPECTION TYPE :C, STR BS 1120 S-7L CRACKED, M/D BS 1120 STR 7L STRINGER. REPAIRED CARRIED OUT IAW SRM 53-10-03 FIG 4.Jan 7, 2005 · N675UP · Boeing 747123FSDR UPS05843854Longeron · crackedINSPECTION TYPE: C3, LONGERON 35L CRACKED STA 1260-1280. REMOVED 2 CLIPS & 1 INTERCOSTAL AT STA 1270. REMOVED SPLICE FITTING AT STA 1350. REMOVED SPLICE FITTING AT STA 1270. REMOVED AND REPLACED LONGERON SECTION FROM 1270-1350. REINSTALLED ALL FOM PARTS. Jan 6, 2005 · N868UP · Doug DC873FSDR DHL2004809517Longeron · crackedAFT FUSELAGE L-17R CRACKED 3.000, STA 1766.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PG 1, SRM 53-5-3 FIG 5 SHEET 1. REMOVED DAMAGED LONGERON IAW SRM 51-1-20D PG 21. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. APPLIED PRC SEALANT TO Jan 6, 2005 · N809DH · Doug DC873FSDR UPS05443813Stringer · crackedBS 1476 - 1478 STR 13R STRINGER END FOUND CRACK. STRINGER REPAIRED PER RS 53-41-35250 AND ENGINEERING FILE NUMBER 747-53-20214.Jan 6, 2005 · N675UP · Boeing 747123SDR UPS05843755Longeron · crackedINSPECTION TYPE:C3 LONGERON 34L CRACKED AT STA 1260-1280. REMOVED SPLICE AT STA 1270 L34L. REMOVED L34L FROM SPLICE AT STA 1350 TO STA 1270. FAB & INSTALL REPLACEMENT LONGERON SECTION FROM 3758593-1 BETWEEN STA 1270-1350 AND SPLICE FITTING AT STA 1270 REF SJan 6, 2005 · N868UP · Doug DC873FSDR UPS05843736Longeron · crackedINSPECTION TYPE:C3, LONGERON 34R CRACKED STA 1260-1280. REMOVED SPLICE FITTINGS AT STA 270 & 1350. OPENED BELLY SKIN FROM L31 LT TO L31 RT TO FOM FROM STA 1300-1350. CLEANED, TREATED, PRIMED AREA. REMOVED AND REPLACED LONGERON 34R FROM STA 1270-1350. REINJan 6, 2005 · N868UP · Doug DC873FSDR UPS05443722Stringer · crackedINSPECTION TYPE:C - STR END BS 1484 S-17L CRACKED. CRACKED STRINGER REPAIRED PER RS 53-41-35227 AND ENGINEERING FILE NUMBER 747-53-20203.Jan 6, 2005 · N675UP · Boeing 747123SDR UPS05443721Stringer · crackedINSPECTION TYPE:C M/D - STR END BS 1476 S-15L CRACKED. CRACKED STRINGER REPAIRED PER RS 53-41-35226 AND ENGINEERING FILE NUMBER 747-53-20202.Jan 6, 2005 · N675UP · Boeing 747123SDR UPS05843759Longeron · crackedINSPECTION TYPE:C3 LONGERON 15R CRACKED UNDER SHEAR TIE AT STA 1754. REMOVED END FITTING AND CLIP TO FOM. REMOVED DAMAGED SECTION OF L15R FROM APPROX STA 1745-1766. FAB REPLACEMENT LONGERON SECTION FROM S1616757, SPLICE STRAPS FROM SHT7075T6-.080, SPLICE FIJan 5, 2005 · N868UP · Doug DC873FSDR UPS05843757Longeron · crackedINSPECTION TYPE:C3 LONGERON 14R CRACKED UNDER CLIP AT STA 1756. REMOVED DAMAGE SECTION OF L14R FROM APPROX STA 1745-1766. REMOVED SHEAR TIE, END FITTING TO FOM. FAB REPLACEMENT LONGERON SECTION FROM S1616757, 2 SPLICE STRAPS FROM SHT7075T6-.080, AND 1 SPLICJan 5, 2005 · N868UP · Doug DC873F
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