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 72300207Stringer · corrodedA 8 X 2 INCH AREA OF CORROSION ON STRINGER.Apr 26, 2005 · N723CK · Boeing 7272H3SDR SWAA051244Stringer · crackedDURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE STRINGER CRACKED AT BS 203, RBL 16. REPAIRED STRINGER PER BFG ER.Apr 26, 2005 · N679AA · Boeing 7373A4SDR 72300172Stringer · corrodedSEVERAL AREAS OF CORROSION ON STRINGER.Apr 26, 2005 · N723CK · Boeing 7272H3SDR DHL2005741570Stringer · corrodedSTR 28L CORRODED AT FS 1013. REMOVED CORROSION FOUND TO BE OUT OF LIMITS ON STR 28L AT FS 1013 IAW B727 SRM 51-10-6 AND SRM 53-10-1. CUT OUT DAMAGED AREA AND REPAIRED IAW SRM.Apr 25, 2005 · N741DH · Boeing 7272Q9SDR DHL2005741516Stringer · corrodedSTR 28L CORRODED AT FS STA 1013. REMOVED CORROSION FOUND TO BE OUT OF LIMITS ON STR 28L AT FUSE 1013 IAW B727 SRM 51-10-6 AN 53-10-1. CUT OUT DAMAGED AREA SIZE 12" ON STR 28L AT STA 1013 IAW B727 SRM 53-10-3 FIG 1. FABRICATED STRINGER FROM BAC 1498-132 SIZEApr 25, 2005 · Boeing 7272Q9SDR DHL2005741515Stringer · corrodedSTR 28L CORRODED AT FS STA 1013. REMOVED CORROSION FOUND TO BE OUT OF LIMITS ON STR 28L AT FUSE 1013 IAW B727 SRM 51-10-6 AN 53-10-1. CUT OUT DAMAGED AREA SIZE 12 INCHES ON STR 28L AT STA 1013 IAW B727 SRM 53-10-3 FIG 1. FABRICATED STRINGER FROM BAC 1498-13Apr 25, 2005 · Boeing 7272Q9SDR SIMA200512206Stringer · chafedDURING AN MBV INSPECTION, MAINTENANCE FOUND STRINGER 19L WITH CHAFE DAMAGE BETWEEN FRAMES 52 AND 53. MAINTENANCE REPAIRED STRINGER 19L BETWEEN FRAMES 52 AND 53 IAW SRM DOUBLER REPAIR. AIRCRAFT WAS RETURNED TO SERVICE. (SW21200505710) (K)Apr 25, 2005 · N806AE · Emb EMB135KLSDR SIMA200512205Stringer · chafedDURING AN MBV INSPECTION, MAINTENANCE FOUND STRINGER 19R WITH CHAFE DAMAGE BETWEEN FRAMES 52 AND 53. MAINTENANCE REPAIRED STRINGER 19R BETWEEN FRAMES 52 AND 53 IAW SRM DOUBLER REPAIR. AIRCRAFT WAS RETURNED TO SERVICE. (SW21200505710) (K)Apr 25, 2005 · N806AE · Emb EMB135KLSDR SIMA200512204Stringer · chafedDURING AN MBV INSPECTION, MAINTENANCE FOUND STRINGER 19R WITH CHAFE DAMAGE BETWEEN FRAMES 52 AND 53. MAINTENANCE REPAIRED STRINGER 19R BETWEEN FRAMES 52 AND 53 IAW SRM DOUBLER REPAIR. AIRCRAFT WAS RETURNED TO SERVICE. (SW21200505710) (K)Apr 25, 2005 · N806AE · Emb EMB135KLSDR CALA0500124Stringer · damagedSTRINGER DAMAGED AT S-16L BETWEEN STA 620-640. REPAIRED STRINGER PER SRM 53-00-03.Apr 25, 2005 · N12125 · Boeing 757224SDR DHL2005807509Longeron · crackedAFT FUSELAGE SECTION L-17L CRACK 2.000 AT STA 1766.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PG 1, SRM 53-5-3 FIG 5. REMOVED CRACKED LONGERON IAW SRM 51-1-21 PG 1, SRM 51-1-20D PG 21, SRM 51-3-0 PG 1. FABRICATED NEW LONGERON (EXTRUSION 7075 Apr 24, 2005 · N807DH · Doug DC873FSDR UPS05844506Longeron · corrodedINSPECTION TYPE: C1, SEVERE CORROSION ON FRAME/ANGLE AT FS 380 (LONGERON) LBL 33. REMOVED CORROSION ON LONGERON AND FOUND OUT OF LIMITS IAW DC-8 SRM 51-1-8. INSTALLED LONGERON SPLICE FITTING IAW DC-8 SRM 51-1-20D.Apr 23, 2005 · N880UP · Doug DC873FSDR UPS05844452Longeron · crackedINSPECTION TYPE:C1 LONGERON CRACKED .5 INCH LONG AT STA 1746 L5R. REMOVED AND REPLACED LONGERON SECTION AND INSTALLED SPLICE FITTING IAW DC-8 SRM 53-2-2 FIG 10 AND 51-1-20D.Apr 22, 2005 · N880UP · Doug DC873FSDR 05FDEA01100Stringer · corrodedIN A/C COMPARTMENT STRINGER 44L FROM FRAME 39 TO 47 HAS AREAS OF CORROSION ON STRINGER AND AROUND FASTENERS. REMOVED FASTENERS IAW A310-200 SRM 51-40-21, REMOVED CORROSION IAW A310-200 SRM 51-74-10, FOUND SECTION OUT OF LIMITS IAW A310-200 SRM 53-10-00, CUTOApr 22, 2005 · N402FE · Airbus A310203SDR 05FDEA01096Stringer · corrodedAFT PIT FRAME 67 STR 50L STRINGER HAS 2SQ INCH OF CORROSION. STR 50L FR 67 AFT, SECTION OF STRINGER REMOVED AND REPLACED.Apr 22, 2005 · N402FE · Airbus A310203SDR 05FDEA01095Stringer · corrodedAFT CARGO COMPT, BETWEEN FR59 AND FR60 ON R STGR 54 HAS AREA OF CORROSION. REMOVED FASTENERS IAW A310-200 SRM 51-40-21. REMOVED CORROSION IAW A310-200 SRM 51-74-10. MEASURED MATERIAL LOSS IAW A310-200 SRM 53-17-12. VERIFIED MATERIAL IS WITHIN LIMITS IAW A3Apr 22, 2005 · N402FE · Airbus A310203SDR 05FDEA01093Stringer · corrodedAFT CARGO COMPT, AT FR 54.3 FWD AND AFT SIDE, ON R-STR 48 HAS AREAS OF CORROSION. REMOVED FASTENERS AND STRINGER TIE TO FOM IAW A310 SRM 51-40-21 AND 51-72-10. REMOVED CORROSION IAW A310 SRM 51-74-10. FOUND TO BE WITHIN LIMITS IAW A310 SRM 53-10-00 TABLE 1Apr 22, 2005 · N402FE · Airbus A310203SDR 05FDEA01089Stringer · corrodedBULK CARGO COMPT, JUST FWD OF FR68 ON LT STR 50 HAS 1 EA AREA OF CORROSION. REMOVED AND REPLACED STR 50L.Apr 22, 2005 · N402FE · Airbus A310203SDR 05FDEA01077Stringer · corrodedIN ACM BAY FR 40/41 BETWEEN STR 44L AND STR 45L, SKIN HAS AREAS OF CORROSION. REMOVED CORROSION PER A310 SRM 51-74-10. C/W EA 6-5310-87784. FOUND ALL AREAS TO BE WITHIN LIMITS PER EA 6-5310-87784 AND A310 SRM 53-15-12. INSTALLED FASTENERS PER A310 SRM 51-4Apr 22, 2005 · N402FE · Airbus A310203SDR 05FDEA01074Stringer · corrodedIN ACM BAY STR 46 RT BETWEEN FR 43 TO FR 47 HAS AREAS OF CORROSION. REMOVED CORROSION PER A310 SRM 51-74-10. C/W EA 6-5310-87784. FOUND ALL AREAS TO BE WITHIN LIMITS PER A310 SRM 53-10-00 AND EA 6-5310-87784. RESTORED SURFACE PROTECTION PER A310 SRM 51-7Apr 22, 2005 · N402FE · Airbus A310SDR 05FDEA01072Stringer · corrodedAFT CARGO COMPT, BETWEEN FR 54.1 AND FR 54.2 ON STR 56 RT HAS 1 EA AREA OF CORROSION. REMOVED AND REPLACED WITH NEW STRINGER SECTION BETWEEN FRAMES 54.2 AND 54.1 IAW A310 SRM 53-10-14, CUT AND SPLICED FRAME 54.2 IAW A310 SRM 53-10-13 REF EA 6-5320-87234.Apr 22, 2005 · N402FE · Airbus A310203SDR 05FDEA01071Stringer · corrodedAFT CARGO COMPT JUST AFT OF FR 54.3 ON STR 51 RT HAS 1EA AREA OF CORROSION. REMOVED CORROSION FROM AFT OF FR 54.3 RT STG 51 IAW A310-200 SRM. FOUND MATERIAL TO BE WITHIN LIMITS IAW A310-200 SRM 53-10-00 PG 123 ITEM 24. INSTALLED REMOVED PARTS AND FASTENERS Apr 22, 2005 · N402FE · Airbus A310SDR 05FDEA01070Stringer · corrodedAFT CARGO COMPT BETWEEN FR 60 AND FR 61 ON STR 50 RT HAS AREA OF CORROSION. REMOVED FASTENERS AND REMOVED CORROSION FROM STG50 BETWEEN FR60 AND FR61 IAW A310-200 SRM 51-40-21 AND SRM 51-74-10; CHECKED LIMITS AND FOUND MATERIAL THICKNESS TO BE WITHIN LIMITS, TApr 22, 2005 · N402FE · Airbus A310SDR 05FDEA01069Stringer · corrodedIN ACM BAY STR 42R HAS AREAS OF CORROSION BETWEEN FRAME 40/41 TO FRAME 44. REMOVED CORROSION PER A310 SRM 51-74-10. C/W EA 6-5310-87784 AND A310 SRM 53-15-12. RESTORED SURFACE PROTECTION PER A310 SRM 51-75-10.Apr 22, 2005 · N402FE · Airbus A310203SDR 05FDEA01068Stringer · corrodedAFT CARGO COMPT, BETWEEN FR 54.2 AND FR 54.3 ON STR 56 RT HAS 3 AREAS OF CORROSION. REF FEDEX EA 6-5310-88741, REMOVED SHEAR TIE, REMOVED FASTENERS IAW A310-200 SRM 51-40-21. REMOVED CORROSION, CHECK MATERIAL LOSS IAW A310-200 SRM 53-10-00 PG 123 ITEM 24. FApr 22, 2005 · N402FE · Airbus A310SDR 05FDEA01067Stringer · corrodedBULK CARGO COMPT, BETWEEN FR 63 AND FR 64 LT SIDE STR 54 AND STR 55 LT HAS CORROSION AROUND FASTENERS AREA. REMOVED AND REPLACED FASTENERS IAW A310 SRM 51-40-21, REMOVED CORROSION IAW A310-200 SRM 51-74-10, NDT FOR MAT LOSS IAW A310-200 SRM 53-17-12 AND 53Apr 22, 2005 · N402FE · Airbus A310203SDR DHL2005741568Stringer · corrodedSTR 28L AT FUSELAGE STA 545 CORRODED C1 CARGO AREA. REMOVED CORROSION ON STR 28L FUSE STA 545 FOUND TO OUT OF LIMITS IAW B727 SRM 51-10-6 AND 53-10-1 CUT OUT DAMAGED SECTION OF STR 28L DIM 18 INCHES IAW B727 SRM 53-10-3 FIG 1. FABRICATED STRINGER FROM BAC 14Apr 21, 2005 · N741DH · Boeing 7272Q9SDR DHL2005741567Stringer · corrodedSTR 27L AT FUSELAGE STA 490 CORRODED C1 CARGO AREA. REMOVED FASTENER & CUT OUT DAMAGED AREA AT STR 27L BS 490 DIM: 16 INCH IAW B727 SRM 53-10-3. REPAIR PARTS FILLER: BAC 1498-113 PO5096102 (16 INCH) & SLICES P/N BAC 1498-132 PO 4496180 10 INCH. LOCATED DRILApr 21, 2005 · N741DH · Boeing 7272Q9SDR DHL2005741524Stringer · corrodedSTR 27R FUSELAGE STA 700 CORRODED. REMOVED CORROSION FOUND TO BE OUT OF LIMITS. CUT OUT DAMAGED SECTION OF STRINGER SIZE 17" IAW B727 SRM 53-10-3 FIG. FABBED STR FROM BAC1498-143 SIZE 17" PO NR 5096198 AND SPLICE FROM BAC1498-132 SIZE 10" PO NR 4246286 IAW Apr 21, 2005 · N741DH · Boeing 7272Q9SDR DHL2005741523Stringer · corrodedSTR 27R CORRODED AT FUSELAGE STA 686. REMOVED CORROSION FOUND TO BE OUT OF LIMITS ON STR 27R AT STA 686 IAW B727 SRM 51-10-6 AND SRM 53-10-1. CUT OUT SECTION OF STR SIZE 10 INCH IAW B727 SRM 53-10-3 FIG 1. FABRICATED STR FROM BAC1498-143 SIZE 10 INCH PO NR Apr 21, 2005 · N741DH · Boeing 7272Q9SDR DHL2005741519Stringer · corrodedSTR 27L CORRODED AT FUSELAGE STA 680. REMOVED EXISTING STR SPLICE AN REMOVED CORROSION MORE THAN 509. OF MAT LOSS AN IS OUT OF LIMITS IAW B727 SRM 51-30-2 FIG 7 AN 53-10-1 FIG 1. LOCATED AN DRILLED FASTENER HOLES IN REPLACEMENT PART BAC 1498-132, PO NR 44961Apr 21, 2005 · N741DH · Boeing 7272Q9SDR DHL2005741517Stringer · corrodedSTRINGER AND FRAME CORRODED AT FUSE STA 720,STR 26R. REMOVED FASTENERS AN STRINGER 19.50 INCH AT STA 720 STR 26R IAW B727 SRM 51-30-2 AN 53-10-3 FIG 1. FABRICATED STRINGER REPLACEMENT PN BAC 1498-144, PO NR 335792 SIZE 19.50 INCH AN 2 SPLICES PN BAC 1498-132 Apr 21, 2005 · N741DH · Boeing 7272Q9SDR UPS05844458Longeron · crackedINSPECTION TYPE:C1 LONGERON CRACKED .5 INCH LONG AT STA 1746 L16L. REMOVED AND REPLACED LONGERON SECTION AND INSTALLED SPLICE FITTING IAW DC-8 SRM 53-2-2 FIG 10.Apr 21, 2005 · N880UP · Doug DC873FSDR UPS05844451Longeron · crackedINSPECTION TYPE:C1 LONGERON CRACKED 1 INCH LONG AT STA 1746 L15L AND STA 1726 L15L. REMOVED AND REPLACED LONGERON SECTION AND INSTALLED SPLICE FITTINGS IAW DC-8 SRM 53-2-2 FIG 10 AND 51-3-2.Apr 21, 2005 · N880UP · Doug DC873FSDR UPS05844450Longeron · crackedINSPECTION TYPE:C1 LONGERON 14R CRACKED .25 INCH LONG AT STA 1757. REMOVED AND REPLACED LONGERON SECTION AND INSTALLED SPLICE FITTING IAW DC-8 SRM 53-2-2 FIG 10 AND 51-1-20D.Apr 21, 2005 · N880UP · Doug DC873FSDR UPS05844449Longeron · crackedINSPECTION TYPE:C1 LONGERON 15R CRACKED 1 INCH LONG AT STA 1757. REMOVED AND REPLACED LONGERON SECTION AND INSTALLED SPLICE FITTING IAW DC-8 SRM 53-2-2 FIG 10 AND 51-1-20D.Apr 21, 2005 · N880UP · Doug DC873FSDR UPS05844448Longeron · crackedINSPECTION TYPE:C1 RIGHT LONGERON 16R CRACKED 2 INCHES LONG AT STA 1756. REMOVED AND REPLACED LONGERON SECTION AND INSTALLED SPLICE FITTING IAW DC-8 SRM 53-2-2 FIG 10 AND 51-1-20D.Apr 21, 2005 · N880UP · Doug DC873FSDR SWAA051181Stringer · crackedDURING SCHEDULED D-CHECK, FOUND FUSELAGE STRINGER CRACKED AT BS 1006, STR 12R. REMOVED AND REPLACED STRINGER SECTION PER SRM.Apr 21, 2005 · N313SW · Boeing 7373H4SDR ASAA0510089Stringer · crackedYXX - FOUND STRINGER 13R AT BS 500A PLUS 15 INCHES CRACKED. CRACK REMOVED AT STRINGER 13R BS 500A PLUS 15 INCHES PER EA 5330-01918. (M)Apr 20, 2005 · N730AS · Boeing 737290CSDR ASAA0510084Stringer · crackedYXX - NDT CRACK INDICATION AT FASTENER HOLE BS 470, STRINGER 22L. REPAIRED AND REMOVED CRACK IAW B737-200 SRM 53-10-3 FIG 1. (M)Apr 20, 2005 · N730AS · Boeing 737290CSDR ASAA0510082Stringer · crackedYXX - NDT CRACK INDICATIONS AT FASTENERS HOLES ON STRINGER 19 LEFT, BS 460-480. CRACK REMOVED IAW B737-200 SRM 53-10-3 FIGURE 1. (M)Apr 20, 2005 · N730AS · Boeing 737290CSDR DHL2005783514Skin · damagedLT FUSELAGE SKIN HAS 2EA CREASES AFT OF BS 1130 ABOVE STR 26L (BELOW PREV REPAIR). REMOVED PREV REPAIR BS 1130 ABOVE STR26L IAW B727 SRM 51-30-2, DAMAGED FOUND TO OUT OF LIMITS IAW B727 SRM. REPAIRED IAW SRM.Apr 19, 2005 · N783DH · Boeing 727227SDR 72300206Stringer · corrodedA 20 X 3 INCH AREA OF CORROSION ON STRINGER.Apr 18, 2005 · N723CK · Boeing 7272H3SDR 72300205Stringer · corrodedA .75 X .5 INCH AREA OF CORROSION ON STRINGER.Apr 18, 2005 · N723CK · Boeing 7272H3SDR 72300179Stringer · corroded1 INCH BY 4 INCH AREA OF CORROSION ON BOTTOM OF STRINGER.Apr 16, 2005 · N723CK · Boeing 7272H3SDR 72300178Stringer · corroded8 INCH BY 3 INCH AREA OF CORROSION ON STRINGER.Apr 16, 2005 · N723CK · Boeing 7272H3SDR ASAA0510071Stringer · corrodedYXX - FOUND CORROSION IN AFT CARGO PIT ON STRINGER 21L AT BS 940. REPAIRED PER B737-200 SRM 53-10-3 FIGURE 1. (M)Apr 14, 2005 · N730AS · Boeing 737290CSDR ABXA050102Longeron · corrodedSKIN BULGING, RIVETS CUPPED AT STA 342, LONGERON 29 RIGHT AND LONGERON 28 RIGHT. REMOVED FASTENERS, EVALUATED. SPLICED LONGERON IAW DC-9 SRM.Apr 14, 2005 · N905AX · Doug DC932FSDR 2005UALA00339Stringer · crackedSTRINGER 16L AT BS 758 IS CRACKED.Apr 14, 2005 · N585UA · Boeing 757222SDR SWAA051113Stringer · corrodedDURING SCHEDULED SPECIAL VISIT, FOUND CORROSION ON STRINGER AT BS 1010, STR 26R. REPAIRED STRINGER PER SRM.Apr 14, 2005 · N657SW · Boeing 7373L9
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