JASC 5313

Service difficulty reports · 36,313

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 2003UALA00749Stringer · dentedFUSELAGE STRINGER S-20L DENTED AT BS 1690 LAP. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR.Oct 6, 2003 · N576UA · Boeing 757222SDR 2003UALA00748Stringer · dentedSTRINGER DENTED AT STATION 1600, STRINGER 19L. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR.Oct 6, 2003 · N576UA · Boeing 757222SDR SIMA200328201Stringer · chafedABI - DURING AN IMBV INSPECTION, FOUND STRINGER 19R WAS FOUND CHAFED BELOW SRM LIMITS. BLENDED THE CHAFED AREA AND PERFORMED NDT INSPECTION. FABRICATED A REINFORCEMENT ANGLE AND TWO SHIMS. REPAIR DONE IAW EMB REPAIR STATEMENT IC2003-145/3093A. (M)Oct 5, 2003 · N722AE · Emb EMB135LRSDR AUS20031160Stringer · cracked(AUS) STRINGER CRACKED AT RIVET HOLE LOCATED FORWARD OF FRAME 328. CRACK LENGTH APPROXIMATELY 0.0254MM (0.1IN). FOUND DURING EDDY CURRENT INSPECTION.Oct 3, 2003 · Boeing 737476SDR 2003FA0001023Rib · corrodedDURING INSPECTION REQUIRED BY AD 2002-26-02 USING METHOD 1 AND METHOD 3, CORROSION WAS DISCOVERED IN THE VICINITY OF THE PILOT'S SIDE INBOARD RIB P/N 415-13017L. THIS CORROSION CANNOT BE SEEN USING THE WING REMOVAL METHOD OF INSPECTION. HOWEVER USING THE INSPOct 3, 2003 · N2273H · Univar 415DSDR 2003FA0001021Rib · corrodedDURING INSPECTION REQUIRED BY AD 2002-26-02 USING METHOD 1 AND METHOD 3, CORROSION WAS DISCOVERED IN THE VICINITY OF THE PILOT'S SIDE INBOARD RIB P/N 415-13017L THIS CORROSION CANNOT BE SEEN USING THE WING REMOVAL METHOD OF INSPECTION. HOWEVER USING THE INSPECOct 3, 2003 · N10743 · Univar 415CSDR ABXA030379Longeron · crackedRT MAIN LANDING GEAR WHEEL WELL LONGERON 24 AT STA. 875 TO 900 TRIPLER SHOWED EVIDENCE OF CRACK. REPAIRED AREA IAW DC-8 SRM 51-1-20D, 53-2-2, AND REA D853-48-35MR.Oct 2, 2003 · N853AX · Doug DC861SDR UPS03841406Longeron · corrodedINSPECTION TYPE: C3, LONGERON 35L CORRODED AT STA 280-300 FWD PIT. REMOVED CORR IAW DC8 SRM 51-1-8, OUT OF LIMITS IAW DC8 SRM 53-2-0. CUT OUT DAMAGE L-ANGLE IAW DC8 SRM 53-2-2. RECEIVED LONG SECT, LOCATED, DRILLED & TRIMMED LONG SECTION & -31 SPLICES IAW DOct 1, 2003 · N813UP · Doug DC873FSDR EIA2003118Stringer · corrodedAFT CARGO COMPT. BS 1790 TO 1800 STR. 51R STRINGER HAS LIGHT SURFACE CORROSION. REMOVED CORROSION FOUND OUT OF LIMITS IAW B747 SRM 53--10-01 PG2-3. REMOVED AND REPLACED DAMAGED STRINGER FROM STA. 1740-1810 AND REPAIRED IAW B747 SRM 53-10-03 FIG 8 PGS. 33-40, Sep 30, 2003 · N482EV · Boeing 747212BSDR AMTA200301254Stringer · dentedMAIN CABIN STRINGER DENTED. REPAIRED STRINGER IAW MFG ER 03-3629 AND SRM 53-00-03, FIG. 201.(K)Sep 29, 2003 · N519AT · Boeing 75723NSDR AAL2004F00001Longeron · crackedCRACK ON LONGERON 46 AT STA 700. CRACKED IN SECTION NEXT TO LOWER ATTACH FASTENER. SPLICED IN NEW SECTION OF LONGERON FROM STA 180 TO STA 235.Sep 28, 2003 · N484AA · Doug DC982SDR SIMA200327902Stringer · chafedABI - DURING AN MBV INSPECTION, FOUND STRINGER 19R WAS FOUND CHAFED BELOW SRM LIMITS BETWEEN FRAMES 52 AND 53. BLENDED THE CHAFED AREA AND PERFORMED AN EDDY CURRENT INSPECTION WITH NO DEFECTS NOTED. FABRICATED A REPAIR ANGLE AND SHIMS FOR REPAIR. REPAIR DONESep 27, 2003 · N823AE · Emb EMB135KLSDR SIMA200327906Stringer · chafedABI - DURING AN MBV INSPECTION, FOUND STRINGER 19L WAS FOUND CHAFED BELOW SRM LIMITS BETWEEN FRAMES 52 AND 53. BLENDED THE CHAFED AREA AND PERFORMED AN EDDY CURRENT INSPECTION WITH NO DEFECTS NOTED. FABRICATED A REPAIR ANGLE AND SHIMS FOR REPAIR. REPAIR DONESep 27, 2003 · N823AE · Emb EMB135KLSDR 2004F00063Stringer · corrodedAT C-CHECK, FOUND AFT CABIN FUSELAGE STRINGER FLOOR LEVER UPPER SURFACE CORRODED BETWEEN FRAMES 68-69 AT STATION 3280. REMOVED AND REPLACED STRINGER 21L BETWEEN FRAMES 68 AND 69 STATION 3280. (M)Sep 26, 2003 · N951LF · Airbus A320233SDR 03FDEA01648Stringer · corrodedCORROSION ON STRINGER AT BS 720F 18, STR 27R. CUT OUT DAMAGED STR B/S 720F 9 FABRICATED AND INSTALLED STR 27R. REPAIRED IAW SRM 53-10-3 FIG 1.Sep 26, 2003 · N469FE · Boeing 727200SDR UPS03841432Longeron · corrodedINSPECTION TYPE: C3, LONGERON 6R STA 12 HAS CORROSION ON FLANGE. REMOVED CORR OUT OF LIMITS IAW DC8 SRM 51-1-8 & 53-2-0. MAT ID PO 409830 .2 7075-T6.050 IAW REO G09499 PG 4. FABBED REPAIR DOUBLER IAW REO G0949 9, ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSep 25, 2003 · N813UP · Doug DC873FSDR MWEA030393Longeron · crackedWHILE REPLACING DOME NUTS FOR FUSELAGE FILET PANEL, FOUND SUSPECT CRACK ON AFT END OF LONGERON 26 RT FRAME STATION 604. FABRICATED AND INSTALLED FITTING.Sep 25, 2003 · N209ME · Doug DC932SDR A6WA200360043Stringer · corrodedFOUND STRINGER 33 RIGHT BETWEEN FRAME 34 AND 35 CORRODED BEYOND LIMITS OF SRM 53-00-00-101 AVMAX NON-ROUTINE 2289 FOR REPAIR. REPAIRED STRINGER IAW BAE SRM 53-00-12 FIG 207. (M)Sep 24, 2003 · N606AW · Bac 146200ASDR A6WA200360042Stringer · corrodedFOUND STRINGER 33 LEFT BETWEEN FRAME 34 AND 35 CORRODED BEYOND LIMITS OF SRM 53-00-00-101. REV AVMAX NON-ROUTINE 1204 FOR REPAIR. REPAIRED STRINGER IAW SRM 53-00-12 FIG 207. (M)Sep 24, 2003 · N606AW · Bac 146200ASDR UPS03841388Longeron · corrodedINSPECTION TYPE: C1, STATION 565 LONG 33R IS CORRODED BEYOND LIMITS. REMOVED, FABRICATED AND REPLACED LONGERON BETWEEN STATION 450 TO 610 IAW DWG 3750539 SRM 53-2-2 FIG 10.Sep 23, 2003 · N866UP · Doug DC873FSDR USAA030209Stringer · crackedFOUND STRINGER CRACKED 3 INCHES, BS 520 STRINGER 12 RT. INSTALLED DOUBLER PER EA 77007. (M)Sep 22, 2003 · N397US · Boeing 7373B7SDR UPS03841346Longeron · crackedINSPECTION TYPE: C1, STATION 70 LONGERON 36 RT. UPPER FLANGE IS CRACKED REMOVED AND REPLACED LONGERON IAW DWG.3702969,AND SRM. 51-1-21, 51-1-20D.Sep 21, 2003 · N866UP · Doug DC873FSDR SIMA200326807Stringer · chafedABI - DURING AN MBV INSPECTION, FOUND STRINGER 19R WAS FOUND CHAFED BELOW SRM LIMITS. BLENDED THE CHAFED AREA AND PERFORMED NDT INSPECTION. FABRICATED A REPAIR ANGLE AND TWO SHIMS. REPAIR DONE IAW EMB 145 SRM, SRM EMB-145/1142 REV 22, CHAPTERS 53-24-02 AND Sep 20, 2003 · N821AE · Emb EMB135KLSDR SIMA200326805Stringer · chafedABI - DURING A MBV INSPECTION, FOUND STRINGER 19L WAS FOUND CHAFED BELOW SRM LIMITS. BLENDED THE CHAFED AREA AND PERFORMED NDT INSPECTION. FABRICATED REPAIR ANGLE AND TWO SHIMS. REPAIR DONE IAW EMB SRM, SRM 145/1142, REV 22, CHAPTER 53-24-02 AND EMB IC2003-Sep 20, 2003 · N821AE · Emb EMB135KLSDR UPS03841325Longeron · crackedINSPECTION TYPE: C1, STA 1730, LONG 14R CRACKED. REMOVED LONGERON SECTION 14R BETWEEN STA 1720-1766, FABRICATED AND REPLACED LONGERON SECTION IAW SRM 53-2-2 FIG10.Sep 20, 2003 · N866UP · Doug DC873FSDR AWXA200301245Stringer · crackedDURING C-17 CHECK A 1.5 INCH CRACK WAS FOUND ON STRINGER 18A RT HORIZONTAL LEG, AT BS 725. MAINTENANCE CUT OUT CRACKED SECTION OF STRINGER 18A RT AT BS 725 AND PERFORMED HFEC INSPECTION OF CUTOUT TO VERIFY NO CRACKS EXIST; FABRICATED A REPAIR FILLER AND RADIUSep 19, 2003 · N326AW · Boeing 737301SDR SWAA032085Stringer · corrodedDURING SCHEDULED 1/4D CHECK, FOUND STRINGER 26R CORRODED AT BS 1011 TO BS 1015. REPAIRED STRINGER PER SRM.Sep 18, 2003 · Boeing 7372H4SDR 03FDEA01570Stringer · corrodedCORROSION INSIDE STRINGER CHANNEL BS 1090, STR 27 LT. **SD** COMINGSep 18, 2003 · N468FE · Boeing 727200SDR IXXA060526SLongeron · crackedDURING ROUTINE C CHECK, FOUND LONGERON 11 RIGHT CRACKED AT STATION FS 1660. REMOVED CRACKED LONGERON. LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED NEW LONGERON, IAW DC8 SRM 51-1-21, 51-1-8, 51-1-20D, AND DOUGLAS DRAWING 3773512.Sep 16, 2003 · N829BX · Doug DC871FSDR SIMA200326506Stringer · chafedABI - DURING AN IMBV INSPECTION, FOUND STRINGER 19R WAS FOUND TO BE CHAFED BEYOND SRM LIMITS AFT OF FRAME 52. COMPLETELY REMOVED CHAFED BY BLENDING AREA. PERFORMED AN EDDY CURRENT INSPECTION OF THE BLENDED AREA. NO DEFECTS NOTED. FABRICATED ON REPAIR ANGLESep 16, 2003 · N720AE · Emb EMB135LRSDR C2XA03SH331Stringer · gougedDURING C CHECK STRINGER 19 RIGHT BETWEEN FRAMES 52 AND 53 WAS FOUND TO BE GOUGED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-24-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Sep 14, 2003 · N13992 · Emb EMB145LRSDR C2XA03SH330Stringer · gougedDURING C CHECK STRINGER 19 LEFT BETWEEN FRAMES 52 AND 53 WAS FOUND TO BE GOUGED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 145 SRM 53-24-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Sep 14, 2003 · N13992 · Emb EMB145LRSDR AWXA200301192Stringer · corrodedDURING C-09 CHECK INTERGRANULAR CORROSION WAS FOUND AROUND NUT PLATE HOLES ON FLOOR STRINGER IN AFT CARGO COMPARTMENT BS 1280 TO BS 1360, LBL 18 TO RBL 20. MAINTENANCE CUTOUT CORRODED AREAS OF FLOOR STRINGER BS 1280 TO BS 1360, LBL 18 TO RBL 20; FABRICATED RESep 12, 2003 · N902AW · Boeing 7572S7SDR AWXA200301191Stringer · corrodedDURING C-09 CHECK INTERGRANULAR CORROSION WAS FOUND AROUND NUT PLATE HOLES ON FLOOR STRINGER IN AFT CARGO COMPARTMENT BS 1500 TO BS 1560, LBL 18 TO RBL 18. MAINTENANCE CUTOUT CORRODED AREAS OF FLOOR STRINGER BS 1500 TO BS 1560, LBL 18 TO RBL 18; FABRICATED RESep 12, 2003 · N902AW · Boeing 7572S7SDR UPS03441255Stringer · corrodedINSPECTION TYPE: C, BELOW FLOOR BILGE AREA STRINGER FOUND CORROSION CRACKED AT STA 2020 STRG 46R. CORROSION CRACKED STRINGER TRIMMED OFF IAW SRM 51-10-01 AND PERFORMED STRINGER REPAIRED IAW SRM 53-10-03 FIG 1 AT BTN STA 1980 AND STA 2030 AN AREA PAINT TOUCHSep 12, 2003 · N682UP · Boeing 747121SDR UPS03841413Longeron · crackedINSPECTION TYPE: C3, AFT FUSELAGE INTERIOR L17 LEFT CRACKED BETWEEN FS 1768-1777. REMOVE CRACKED LONGERON IAW UPS DC8 SRM 51-1-20 & 51-1-21. LOCATE NEW LONGERON AND DRILL EXISTING FASTENER HOLES IAW UPS DC8 SRM 51-3-2. INSTALLED NEW LONGERON IAW UPS DC8 SRSep 11, 2003 · N813UP · Doug DC873FSDR UPS03841410Longeron · crackedINSPECTION TYPE: C3, AFT FUSELAGE INTERIOR L17 RIGHT CRACKED BETWEEN FS 1768-1776. REMOVED L-17RT TO FOM, FABBED NEW -35 SPLICE DOUBLER IAW DAC DWG 56493 27, ALODINED AND PRIMED IAW DC8 SRM 51-1-8, LOCATED, DRILLED, DEBURRED, AND INSTALLED NEW LONGERON IAW DSep 11, 2003 · N813UP · Doug DC873FSDR 03FDEA01502Stringer · crackedSTR 15L CRACKED AT 720B 4. REPAIRED IAW SRM 53-10-3 FIG 5Sep 11, 2003 · N221FE · Boeing 727200SDR 03FDEA01501Stringer · crackedN01557 STR CRACKED B/S 720B 15 STR 15L. REPAIRED IAW SRM 53-10-3 FIG 5.Sep 11, 2003 · N221FE · Boeing 727200SDR 03FDEA01510Stringer · damagedDAMAGED STRINGER BS 647 STR 21R. CUT OUT DAMAGE & REPAIRED PER SRM 51-10-3 FIG 1Sep 11, 2003 · N221FE · Boeing 727200SDR 03FDEA01516Stringer · crackedN01548 CRACKED STRINGER, BS 720B 4 STR 15R. REMOVED DAMAGED PORTION OF STR 15R AT BS 720B 4 IAW SRM 53-10-3 FIG 5. HFEC INSPECTION ON PERPHERY OF CUTOUT NO CRACKS NOTED. FABRICATED ALODINED, PRIMED AND INSTALLED ALL REPAIR PARTS IAW SRM 53-10-3 FIG 5.Sep 11, 2003 · N221FE · Boeing 727200SDR GAIA03092Stringer · crackedDURING B-2 CHECK, FOUND MAIN CABIN STRINGER 15 RT CRACKED AT AFT SIDE OF BS 720B. REF FASI N/R 53135, ACCOMPLISHED STRINGER REPAIR PER B727 SRM 53-10-3 TABLE ONE. (M)Sep 10, 2003 · N6806 · Boeing 727223SDR GAIA03091Stringer · crackedDURING B-2 CHECK FUOND MAIN CABIN STRINGER 15 LT CRACKED FORWARD OF BS 720C. REF FASI N/R 53134 ACCOMPLISHED STRINGER REPAIR PER B727 SRM 53-10-3 TABLE ONE. (M)Sep 10, 2003 · N6806 · Boeing 727223SDR SWAA032032Stringer · crackedDURING SCHEDULED C3 CHECK, FOUND STRINGER CRACKED AT BS 947, STR 24R. REPAIRED STRINGER PER SRM.Sep 10, 2003 · N323SW · Boeing 7373H4SDR UPS03841404Longeron · corrodedINSPECTION TYPE: C3, LONGERON 36 CORRODED AT STA 220-240 FWD PIT. REMOVED CORR IAW DC8 SRM 51-1-8 ORIG .080 INCH, REMOVED .027 INCH, REMAINING .053 INCH OUT OF LIMITS IAW DC8 SRM 53-2-0. CUT OUT DAMAGE IAW DC8 SRM 53-2-2. RECEIVED LONG SECTION, LOCATED, DRSep 9, 2003 · N813UP · Doug DC873FSDR SIMA200326503Stringer · chafedABI - DURING A MBV INSPECTION, FOUND STRINGER 19L WAS FOUND TO BE CHAFED BELOW SRM LIMITS. BLENDED THE CHAFED AREA AND PERFORMED NDT INSPECTION. FABRICATED A REPAIR ANGLE AND TWO SHIMS. REPAIR DONE IAW EMB 145 SRM, SRM EMB 145/1142 REV 22, CHAPTER 53-24-02 Sep 9, 2003 · N820AE · Emb EMB135KLSDR SWAA032008Stringer Clip · crackedDURING SCHEDULED D CHECK, FOUND STRINGER CLIPS CRACKED (3 EA) BS 277 AT STR 15R, BS 807 AT STR 26R AND BS 727B AT STR 18L. REMOVED AND REPLACED STRINGER CLIPS PER SRM.Sep 9, 2003 · N301SW · Boeing 7373H4SDR SWAA032000Stringer · corrodedDURING SCHEDULED D CHECK, FOUND STRINGER CORRODED AT BS 984, STR 25R. REPAIRED STRINGER PER SRM.Sep 8, 2003 · N301SW · Boeing 7373H4SDR SWAA031999Stringer · crackedDURING SCHEDULED D CHECK, FOUND STRINGER CRACKED AT BS 827, STR 20L. REPAIRED STRINGER PER SRM.Sep 8, 2003 · N301SW · Boeing 7373H4SDR C1HA200386001Stringer · corrodedCORROSION ON STRINGER 29 LT AT BS 950B+8.Sep 8, 2003 · N686CA · Boeing 7272S7
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