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 SIMA200507507Stringer · chafedDURING INSPECTION, 652 STRINGER 19R WAS FOUND TO BE CHAFED AT AFT FAIRING CUTOUT. BLENDED THE CHAFE AND PERFORMED EDDY CURRENT INSPECTION WITH NO CRACKS NOTED. FABRICATED A DOUBLER AND TWO SHIMS. REPAIR DONE IAW EMB SRM, SRM 145/1142 REV 28, CHAPTER 53-24-0Mar 13, 2005 · N652RS · Emb EMB145LRSDR UPS05444155Stringer · crackedINSPECTION TYPE:C AREA AFT OF BULK CARGO STA 2180 S42R STRINGER END CRACKED, CRACK LENGTH .75 INCH. AFT OF BULK CARGO BS 2160 TO 2180 STR 42R REPAIRED AS PER SRM 53-10-03 FIG 1.Mar 13, 2005 · N682UP · Boeing 747121SDR UPS05444129Stringer · crackedINSPECTION TYPE:C, BS 1278 STR 25R END FOUND CRACKED. CRACK LENGTH .75 INCH. M/DECK BS 2170-2180 STR 25R REPAIRED AS PER SRM 53-10-03 FIG 1.Mar 12, 2005 · N682UP · Boeing 747121SDR AWXA200500403Stringer · corrodedDURING C-05 CHECK EXFOLIATION CORROSION WAS FOUND ON STRINGER 27 LT AT BS 986. MAINTENANCE CUTOUT DAMAGE IN STRINGER 27 LT AT BS 986; FABRICATED A CHANNEL AND 2 EACH REPAIR ANGLES; INSTALLED REPAIR PARTS IAW B737-300 SRM 53-00-03, FIG 201.Mar 11, 2005 · N336AW · Boeing 737375SDR 05FDEA00496Stringer · corrodedBS 585 STR 24 LT IS DENTED AND GOUGED. REPAIRED STR 24 LT, BS 585 PER SRM 53-10-1, SRM 53-10-3 AND MM 51-20-151.Mar 11, 2005 · N481FE · Boeing 727200SDR 05FDEA00488Stringer · corrodedBS 480, STRINGER 26 RT IS CORRODED. REMOVED CORROSION, OUT OF LIMITS PER SRM, REPLACED STR 26 RT AT BS 480 TO BS 510, IAW SRM 53-10-3 AND 51-30-2.Mar 10, 2005 · N481FE · Boeing 727200SDR 0500379954Longeron · corrodedDURING M-CHECK FOUND CORROSION FROM BS 737-756 ON LONGERON 29L. REPAIRED PER EA 99-203145.Mar 8, 2005 · N921RW · Doug DC931SDR ABXA050069Longeron · corrodedLONGERON 30 AT STA 945 WAS CORRODED BEYOND LIMITS. REPLACED LONGERON IAW DC-9 SRM 51-30-5 AND 51-30-2.Mar 8, 2005 · N945AX · Doug DC931SDR 05FDEA00429Stringer · gougedBS 592 STR 25 LT IS GOUGED. REPAIRED IAW SRM 53-10-3Mar 8, 2005 · N481FE · Boeing 727200SDR 05FDEA00428Stringer · dentedBS 592 STR 23 LT IS DENTED. REPAIRED PER SRM 53-10-3Mar 8, 2005 · N481FE · Boeing 727200SDR 05FDEA00406Stringer · corrodedBULKPIT UNDER FLOOR STRINGER 49R 6 INCHES AFT OF FR65 HAS AN AREA OF 0.5 X 0.5 INCH OF CORROSION. REMOVED CORROSION AT BULKPIT UNDER FLOOR FR65 STG 49R IAW A310-200 SRM 51-74-10. CHECKED MATERIAL LOSS FOUND TO BE OUT OF LIMITS IAW A310-200 SRM 53-10-00 FIG 1Mar 7, 2005 · N446FE · Airbus A310222SDR 05FDEA00400Stringer · corrodedBULK PIT UNDER FLOOR STG 54L 10 IN AFT OF FR 67 IS AN AREA 5 X 2 OF CORROSION EXTENDING UNDER FASTENERS. REMOVED CORROSION FOUND OUT OF LIMITS, REPAIRED IAW 53-10-14.Mar 7, 2005 · N446FE · Airbus A310222SDR 05FDEA00399Stringer · corrodedBULK PIT UNDER FLOOR STG 49R FR 64 FWD 4 IN TO AFT 4 IN 1 IN I/B AND O/B OF STG HAS CORROSION EXTENDING UNDER FRAME REF N00781. REMOVED CORRODED AREA OUT OF LIMITS, REPAIRED STG IAW SRM 53-10-14.Mar 7, 2005 · N446FE · Airbus A310222SDR SIMA200507508Stringer · chafedABI - DURING INSPECTION OF AIRCRAFT, STRINGER 19R WAS FOUND CHAFED. BLENDED THE CHAFED AREA AND PERFORMED NDT INSPECTION. FABRICATED REPAIR ANGLE AND TWO SHIMS. REPAIR DONE IAW EMB REPAIR STATEMENT IC2005-145/1147 PARA 8 DATED MARCH 3, 2005. (M)Mar 6, 2005 · N655AE · Emb EMB145LRSDR 05FDEA00388Stringer · corrodedBULK PIT UNDER FLOOR STG 50R FROM 10 INCHES AFT OF FR 64 TO FR 65, 1 INCH INBOARD OF STG TO 2 INCHES OUTBOARD OF STG HAS CORROSION EXTENDING ON AND UNDER BRACKETS AND STG SPLICE. REMOVED CORROSION IAW A310-200 SRM 51-74-10. AREA OUT OF LIMITS IAW A310-200 SRMar 6, 2005 · N446FE · Airbus A310222SDR 05FDEA00386Stringer · corrodedBULK PIT UNDER FLOOR FR 65 STG 54R HAS A 5 X 2 INCH AREA OF CORROSION ON SPLICE EXTENDING UNDER FASTENERS. REMOVED SPLICE ANGLE IAW A310-200 SRM 51-40-21. REMOVED CORROSION IAW A310-200 SRM 51-74-10. AREA OUT OF LIMITS IAW A310-200 SRM 53-10-00. REPLACED DMar 6, 2005 · N446FE · Airbus A310222SDR QXEA200500482Stringer · corrodedYYC - FUSELAGE INTERIOR STRINGER AT FS 280 TO FS 333 STRINGER 25R HAS SEVERAL SPOTS OF CORROSION ALONG RIVET ROW. REPAIRED IAW CRJ700 SRM 53-21-03-101-002-AA1, SRM 51-42-06-001-001-A01, AND SRM 51-42-21-001-001-A01.Mar 5, 2005 · N605QX · Cndair CL6002C10SDR AWXA200500401Stringer Clip · crackedDURING C-16 CHECK A .375 INCH CRACK WAS FOUND IN STRINGER TIE CLIP ON FWD SIDE OF BS 727A, STR 27 LT. MAINTENANCE REMOVED CRACKED STRINGER TIE CLIP AT BS 727A, STR 27 LT; FABRICATED A NEW REPLACEMENT STRINGER TIE CLIP PER DWG 69-35350; INSTALLED REPAIR PART IMar 3, 2005 · N305AW · Boeing 7373G7SDR MASA200500175Stringer · chafedIN C-CHECK, STRINGER 19 RT IS CHAFED OUT OF LIMITS AND HAS BEEN REPAIRED IAW SRM 53-24-02.Mar 3, 2005 · N850MJ · Emb EMB145LRSDR SWAA050659Stringer · corrodedDURING SCHEDULED C4 CHECK, FOUND CORROSION ON FUSELAGE STRINGER AT BS 344, STR 28R. REMOVED AND REPLACED STRINGER SECTION PER SRM.Mar 3, 2005 · N695SW · Boeing 7373Q8SDR 05FDEA00337Stringer · tool damageTOOLING DAMAGE AT BS 1010 STRINGER 7L IN STRINGER CLIP AND STRINGER SPLICE. REPAIRED PER SRM 53-10-2 (DUPLICATE ENTRY TO TRACKING NR 05-0336)Mar 2, 2005 · N481FE · Boeing 727227SDR 05FDEA00336Stringer · tool damageTOOLING DAMAGE AT BS 1010 STRINGER 7L IN STRINGER CLIP AND STRINGER SPLICE. REPAIRED PER SRM 53-10-2.Mar 2, 2005 · N481FE · Boeing 727227SDR 05FDEA00334Stringer · corrodedCORROSION IN STRINGER 26R, AFT OF BS 1148, AFT CARGO BAY.Mar 2, 2005 · N481FE · Boeing 727227SDR SWAA050640Stringer · crackedDURING SCHEDULED D-CHECK, FOUND CRACKED STRINGER AT BS 360, STR 14L. REPAIRED STRINGER PER SRM.Mar 1, 2005 · N663SW · Boeing 7373Q8SDR SWAA050623Stringer Clip · crackedDURING SCHEDULED SPECIAL VISIT, FOUND CRACKED STRINGER CLIP AT STR 9L, BS 400. REMOVED AND REPLACED STRINGER CLIP PER SRM.Feb 28, 2005 · N693SW · Boeing 737317SDR AALA20050217Longeron · crackedAFW - RIGHT HAND UPPER LONGERON WEB AT STRINGER 12 RIGHT JUST FORWARD OF STATION 1809 CRACKED. CUT OUT DAMAGED WEB AT APPROXIMATELY STATION 1798 AND FABRICATED A REPAIR WEB FROM .032 7075T6 CLAD. DOUBLER FROM .040 7075T6 CLAD AND FILLER FROM 0.080 7075T6 ANDFeb 28, 2005 · N357AA · Boeing 767323SDR SWAA050608Stringer · crackedDURING SCHEDULED 1/2D CHECK, FOUND CRACKED STRINGER AT BS 360, STR 15L. REPAIRED STRINGER PER SRM.Feb 27, 2005 · N507SW · Boeing 7375H4SDR IXXA0500144SLongeron · crackedDURING A ROUTINE C-CHECK INSPECTION FOUND RT FUSELAGE TAIL SECTION STRUCTURE LONGERON 17 RT HAS CRACK DAMAGE STA 1770.00. MAJOR REPAIR ACCOMPLISHED REMOVAL OF CRACKED LONGERON. FABRICATED NEW LONGERON, CLEANED, TREATED AND PRIMED AREA. APPLIED SEALANT TO FAFeb 25, 2005 · N821BX · Doug DC871FSDR 72300162Stringer · corroded1.500 INCH BY 3 INCH AREA OF CORROSION ON STRINGER.Feb 25, 2005 · N723CK · Boeing 7272H3SDR SIMA200506106Stringer · gougedABI - DUIRNG A IMBV INSPECTION OF AIRCRAFT, STRINGER 19R WAS FOUND TO BE GOUGED BETWEEN FRAMES 49 AND 50. BLENDED OUT THE GOUGE, PERFORMED EDDY CURRENT INSPECTION WITH NO REJECTABLE INDICATIONS. FABRICATED A REPAIR ANGLE AND TWO SHIMS. REPAIR DONE IAW EMB SFeb 25, 2005 · N801AE · Emb EMB135KLSDR SIMA200506107Stringer · gougedABI - DURING INSPECTION OF AIRCRAFT, STRINGER 19L AS FOUND TO BE GOUGED BETWEEN FRAMES 49 AND 50. BLENDED OUT THE GOUGE. PERFORMED EDDY CURRENT INSPECTION WITH NO REJECTABLE INDICATIONS. FABRICATED A REPAIR ANGLE AND TWO SHIMS. REPAIR DONE IAW EMB SRM, SRMFeb 25, 2005 · N801AE · Emb EMB135KLSDR SWAA050594Stringer · corrodedDURING SCHEDULED SPECIAL VISIT, FOUND CORROSION ON FUSELAGE STRINGER SPLICE BETWEEN BS 350 & BS 370, STR 28R. REPAIRED FUSELAGE STRINGER SPLICE PER SRM.Feb 25, 2005 · N657SW · Boeing 7373L9SDR SWAA050593Stringer · corrodedDURING SCHEDULED SPECIAL VISIT, FOUND CORROSION ON FUSELAGE STRINGER SPLICE AT BS 358, STR 27R. REPAIRED FUSELAGE STRINGER SPLICE PER SRM.Feb 25, 2005 · N657SW · Boeing 7373L9SDR EIA2005025Stringer · crackedBETWEEN STA 260-280 STRINGER 41 LT CRACKED AT AFT END. REMOVED AND REPLACED STRINGER STA 260-280 NR 41 LT PER B747 SRM 51-30-02 PG 2-9. FABRICATED NEW STRINGER NR 41 LT STA 260-280 PER B747 SRM 51-20-01 PAGE 11-20.Feb 22, 2005 · N471EV · Boeing 747273CSDR EIA2005016Stringer · crackedBETWEEN STA 300-320 STR 34 RT CRACK AT UPPER SURFACE. REMOVED DAMAGED SECTION BETWEEN STA 280-320 PER B747 SRM 53-10-03 PG 8-10. FABRICATED NEW STRINGER PER B747 SRM 53-10-03 PG 8, 51-30-02, 51-10-02 AND BSOPM 20-41-02 PG 7-9 NDT FOUND NO CRACKS. INSTALLED Feb 22, 2005 · N471EV · Boeing 747273CSDR EIA2005038Stringer · crackedBS 2260 STR 43R INNER CHORD CRACK. DAMAGE REMOVED, REPAIR FABBED AND INSTALLED PER ECRA 478-51-173-1.Feb 22, 2005 · N478EV · Boeing 747SR46SDR QXEA200500322Stringer · corrodedPDX - THERE IS CORROSION ON STRINGER 33 AT APPROXIMATELY STATION X190, JUST BELOW A WIRE BUNDLE. REPAIRED IAW DHC-8-200 SRM 51-40-11, 51-20-16 AND HORIZON AIR EA 2-53-603.Feb 22, 2005 · N363PH · Dhav DHC8202SDR EIA2005007Stringer · crackedSTR 22L CRACKED AT STA 303 UNDERNEATH STRINGER. REPAIRED CRACKED STRINGER AT 22L, STA 303 PER ECRA 471-53-248-2.Feb 21, 2005 · N471EV · Boeing 747273CSDR UPS05844158Longeron · crackedINSPECTION TYPE:C1, COMPT 60 L17R HAS 3 INCH CRACK AND LONGERON END FITTING HAS .5 INCH CRACK 1770. REMOVED AND REPLACED L17R AND END FITTING AT STATION 1770 IAW 51-1-8, 51-1-20D, 53-2-2 AND 51-1-21.Feb 21, 2005 · N805UP · Doug DC873FSDR CALA0500048Stringer · corrodedINSPECTION FOUND STRINGER 27L CORRODED AT RIVET HOLES BETWEEN STA 500 AND 500B. THE CORRODED SECTION OF STRINGER WAS CUT OUT AND A REPAIR WAS INSTALLED IAW SRM 53-00-03, FIGURE 201.Feb 20, 2005 · N17309 · Boeing 7373T0SDR UPS05844115Longeron · crackedINSPECTION TYPE:C1 LONGERON 14R CRACKED UNDER CANTED FRAME AT STA 1756. REMOVED LONG SECTION, END FITTING, CLIP. FAB REPLACEMENT LONG SECTION (S1616757 EXTRUSION), 2 STRAPS (SHT7075T6-.080), SPLICE FITTING ON SVC ORDER 7034949 (S2645716 EXTRUSION). INSTALLEFeb 19, 2005 · N805UP · Doug DC873FSDR UPS05844114Longeron · crackedINSPECTION TYPE:C1 LONGERON 15R CRACKED UNDER CANTED FRAME AT STA 1734 REMOVED LONG FROM 1725-1766, END FITTING, CLIP AT STA 1752. FAB REPLACEMENT LONG SECTIONS (S1616757 EXTRUSION), 2 SPLICE FITTINGS ON SERVICE ORDER 7034948 (S2645716 EXTRUSION), 4 REPAFeb 19, 2005 · N805UP · Doug DC873FSDR UPS05844112Longeron · crackedINSPECTION TYPE:C1 LONGERON 15L CRACKED NEAR STA 1760. REMOVED LONG FROM STA 1739-1766, SHEAR TIE AT STA 1746, END FITTING AT STA 1766. FABRICATED REPLACEMENT LONG SECTION (S1616756 EXTRUSION), REPAIR SPLICE ON SERVICE ORDER 7034944 (S2645716 EXTRUSION), 2 SFeb 19, 2005 · N805UP · Doug DC873FSDR EIA2005004Stringer · corrodedCORROSION UNDER STR 47 DOUBLER LT SIDE. REMOVED CORROSION PER SRM 51-10-01 BLENDED AREA FOUND TO BE WITHIN LIMITS PER 747 SRM 53-30-02 AND 53-30-01 FIG 1.Feb 19, 2005 · N486EV · Boeing 747212BSDR UPS05844001Longeron · crackedINSPECTION TYPE: C2, LONG 15R CRACKED AT STA 1746. DISASSEMBLED SPLICES AT STA 1726 & 1746. REMOVED SHEAR-TIES, FOUND STA 1746 ASSEMBLED WITHOUT STRAPS UNDER LONGERON. FAB LONG SECTIONS (EXTR S1616 757 & 2 STRAPS SHT7075T6-.080). TREATED, PRIMED, INSTALLEDFeb 19, 2005 · N811UP · Doug DC873FSDR DHL2005781524Stringer · crackedDURING A "C" CHECK, STRINGER 30 AT STA 1175 CRACKED AND EXFOLIATED. REMOVED REINFORCEMENT ANGLE FOR ACCESS IAW B727 SRM 51-30-2 BS 1175 TO 1183 STR 30 EVALUATED STRINGER 30 AT BS 1175 TO 1183. NO CORROSION NOTED. EVALUATED REINFORCEMENT ANGLE FROM BS 1175 TFeb 18, 2005 · N781DH · Boeing 727227SDR USAA050295Stringer · crackedPIT - FOUND STRINGER CRACKED 3 INCHES, BS 1138 S5A LEFT. TRIM OUT DAMAGE AND SPLICE IN NEW SECTION OF STRINGER PER TYPICAL REPAIR 53-80-04. (M)Feb 18, 2005 · N520AU · Boeing 7373B7SDR GTIA050057Longeron · corrodedLONGERON 28R STA 1140 HAS CORROSION AROUND FASTENERS THROUGH SKIN IN AFT PIT. REMOVED FASTENERS THROUGH SKIN AND REMOVED CORROSION. LONGERON 28R AT STA 1140 IS OUT OF LIMITS. LOCATED AND DRILLED FABED LONG SECTION AND SPLICE. TREAT AND PRIMED, INSTALLED LOFeb 17, 2005 · N804NK · Doug DC982SDR UPS05844111Longeron · crackedINSPECTION TYPE:C1 LONG 14L CRACKED NEAR STA 1760. REMOVED LONG SECTION FROM 1746-1766. REMOVED SHEAR TIE AT 1757. FABRICATED REPLACEMENT LONG SECT FROM EXTRUSION S1616757, 2 SPLICE STRAPS (SHT7075-T6 .080), REPAIR SPLICE (S2645716 EXTRUSION) ON SERVICE ORDFeb 15, 2005 · N805UP · Doug DC873FSDR SWAA050399Stringer · corrodedDURING SCHEDULED 1/2D CHECK, FOUND STRINGER 25L AT BS 970, CORRODED. REMOVED AND REPLACED STRINGER SECTION PER SRM.Feb 10, 2005 · N502SW · Boeing 7375H4
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