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 XN0A1296Stringer · corrodedDURING CPCP INSPECTION FOUND STR 25R CORRODED FROM FS 1150 TO FS 1183. REMOVED DAMAGED SECTION OF STRINGER, INSTALLED STR MATERIAL P/N BAC1498-145 PER B727 SRM 51-30-2 AND STRINGER REPAIR PER B727 SRM 53-10-3.Jan 30, 2006 · N79754 · Boeing 727227SDR XN0A1197Stringer · corrodedDURING CPCP INSPECTION FOUND STR 30 CORRODED FROM FS 1150 TO FS 1183. REMOVED CORRODED SECTION OF STRINGER FROM FS 1150 TO FS 1183 AND REPAIRED SAME PER B727 SRM 53-10-3.Jan 30, 2006 · N79754 · Boeing 727227SDR SWAA060358Stringer · corrodedDURING SCHEDULED D CHECK, FOUND FUSELAGE STRINGER CORRODED AT BS 892, STR 24L. REPAIRED STRINGER PER SRM.Jan 30, 2006 · N678AA · Boeing 7373A4SDR C1HA200682013Stringer · corrodedAFT LWR COMPARTMENT STRINGER 30 SPLICE AREA SECTION BETWEEN BS 1030 THRU BS 1050 CORROSION SPOTS BETWEEN STRINGER & FUSELAGE SKIN. REMOVED AND REPLACED STRINGER, MATERIAL USED BAC1498-145, DIM 17 INCHES IN LENGTH IAW 727 SRM 53-10-3 FIG 1. NO CORROSION NOTEDJan 30, 2006 · N682CA · Boeing 7272S7SDR C1HA200682012Stringer · corrodedAFT LWR COMPARTMENT STRINGER 30 SPLICE AREA SECTION BETWEEN BS 1010 THRU BS 1030 SPOT OF CORROSION BETWEEN STRINGER & FUSELAGE SKIN. REMOVED AND REPLACED DAMAGED STRINGER, MATERIAL USED BAC1498-145, DIM 18 INCHES IN LENGTH IAW 727 SRM 53-10-3 FIG 1. NO CORROJan 30, 2006 · N682CA · Boeing 7272S7SDR C1HA200682011Stringer · corrodedAFT PIT STRINGER 29R CORRODED AT BS 1075. REMOVED AND REPLACED DAMAGED STRINGER SECTION MATERIAL USED BAC1498-147, DIM 18.375 INCH LENGTH IAW 727 SRM 53-10-2 FIG 9 & 53-10-3 FIG 1.Jan 30, 2006 · N682CA · Boeing 7272S7SDR SWAA060347Splice · crackedDURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE STRINGER SPLICE CRACKED AT BS 360, STR 15L. REMOVED AND REPLACED STRINGER SPLICE PER SRM.Jan 29, 2006 · N351SW · Boeing 7373H4SDR SWAA060346Stringer · crackedDURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE STRINGER CRACKED AT BS 807, STR 14R. REPAIRED STRINGER PER SRM.Jan 29, 2006 · N351SW · Boeing 7373H4SDR IXXA06SMN057SLongeron · crackedDURING ROUTINE C CHECK INSPECTION, 'FWD ACCY COMPT- L-34R CRACKED BETWEEN STA 208.000 - STA 270.000. REMOVED CRACKED L-34R IAW DC-8 SRM 51-1-21. CLEANED, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8B. INSTALLED NEW LONGERON WITH RIVETS + HILOKS IAW DC-8 SRM Jan 26, 2006 · N722CX · Doug DC872SDR 06FDEA0374Stringer · corrodedAFT CARGO COMPARTMENT, CORROSION ON STR. 30 BS 1166 TO BS 1183 BL 0. REPAIRED STR 30 BS 1140 - 1183 IAW SRM 53-10-3, 51-10-2 AND 51-30-2.Jan 25, 2006 · N191FE · Boeing 727100SDR ACE012406Stringer · corrodedFOUND CORROSION ON STRINGER 15 LH AT FUSELAGE STATION 210. THE REPAIR REQUIRED DER. ENGINEERING ASSISTANCE DUE NO OEM DOCUMENT COVERING THE REQUIRED REPAIR.Jan 24, 2006 · N111AX · Beech 1900CSDR SWAA060314Stringer · crackedDURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE STRINGER CRACKED AT BS 380, STR 15L. REMOVED AND REPLACED STRINGER SECTION PER SRM.Jan 24, 2006 · N351SW · Boeing 7373H4SDR 06FDEA0319Stringer · crackedSTA 720B PLUS 3 STR 15R CRACKED ON END. REMOVED DAMAGE AND INSTALLED REPAIR PARTS PER SRM 53-10-3.Jan 23, 2006 · N492FE · Boeing 727200SDR 06FDEA0318Stringer · crackedSTA 720B PLUS 3, STR 15L CRACKED ON END. REMOVED DAMAGE AND INSTALLED REPAIR PARTS PER SRM 53-10-3Jan 23, 2006 · N492FE · Boeing 727200SDR USAA06099Stringer · crackedSTA 686, S9L AFT END OF STRINGER CRACKED. REMOVED & REPLACED STRINGER CHORD PER SRM 51-40-02, 51-20-01, 51-10-02, DEFECT SIZE: 1.5 INCH.Jan 20, 2006 · N600AU · Boeing 757225SDR AWXA200600393Stringer · corrodedMCN - MAJOR REPAIR - DURING C24 CHECK DISCOVERED LEVEL 2 CORROSION ON STR 25R AT BS 960 TO BS 1020. MAINTENANCE FOUND CORROSION TO BE OUT OF LIMITS IAW BOEING 737-300 SRM 53-00-03-1A1 FIG 101. MAINTENANCE REMOVED DAMAGED STRINGER SECTION IAW BOEING 737-300 SJan 18, 2006 · N328AW · Boeing 7373B7SDR AWXA200600403Stringer · crackedMCN - DURING C19 CHECK DISCOVERED RT STR 18A WEB CRACKED, 1.1 INCHES. MAINTENANCE CUT OUT AND REMOVED DAMAGE FROM RT STR 18A WEB IAW AMERICA WEST AIRLINES ENGINEERING REPAIR NR 03-5361-06043-RC1. FABRICATED FILLER, RADIUS FILLER AND RECEIVED REPAIR GUSSET IAJan 17, 2006 · N166AW · Boeing 73733ASDR AWXA200600402Stringer · crackedMCN - DURING C19 CHECK DISCOVERED LT STR 18A WEB CRACKED, .9375 INCHES, JUST FORWARD OF BS 727 BULKHEAD. MAINTENANCE CUT OUT AND REMOVED DAMAGE FROM LT STR 18A WEB IAW AMERICA WEST AIRLINES ENGINEERING REPAIR NR 03-5361-06043-RC2. FABRICATED FILLER, RADIUS FJan 17, 2006 · N166AW · Boeing 73733ASDR 2006UALA00083Stringer · crackedFUSELAGE STR 22R CRACKED STA 847, 6 INCHES AFT OF PIT DOOR CUTOUT. *S/D* FABRICATED AND INSTALLED STR REPAIR REF SRM 53-00-03 REPAIR 1.Jan 17, 2006 · N325UA · Boeing 737322SDR ASAA0680002Longeron · corrodedC-CHECK, LONGERON CORRODED. REPLACED DAMAGED SECTION WITH SPLICES. (K)Jan 15, 2006 · N969AS · Doug DC983SDR USAA060019Stringer · corrodedFOUND STA 1470 RBL 2, 7 AND LBL 16,7,11. CUT OUT DAMAGE SECTIONS OF STRINGER, FAB'D AND INSTALLED REPAIR ANGLES PER SRM 53-00-53, 51-70-11 AND EA, DEFECT SIZE: .250 CIRCUMFERENCE AROUND FASTENER HOLE (6 PLACES) BY .051 DEPT.Jan 13, 2006 · N629AU · Boeing 7572B7SDR USAA0619Stringer · corrodedSTA 1470 RBL 2, 7 & LBL 16, 7, 11 CORRODED. CUT OUT DAMAGE SECTIONS OF STRINGER, FAB'D & INSTALLED REPAIR ANGLES PER SRM 53-00-53, 51-70-11 & EA, DEFECT SIZE: .250 CIRCUMFERENCE AROUND FASTENER HOLE (6 PLACES) X .051 DEPT.Jan 13, 2006 · N629AU · Boeing 7572B7SDR ABXA060062Longeron · crackedFOUND LONGERON 4 FEET AT STA 200 CRACKED. REMOVED AND REPLACED LONGERON 4 LEFT, STA 160.230 IAW DC9 SRM 51-30-2 AND 51-30-5.Jan 12, 2006 · N908AX · Doug DC931SDR 06FDEA0161Stringer · corrodedCORROSION ON STR 3 RT, BS 720C-720D. REPAIRED STR 3 RIGHT, BS 720C-720D PER SRM 53-10-3 FIG 3.Jan 12, 2006 · N485FE · Boeing 727200SDR 06FDEA0160Stringer · corrodedCORROSION ON STR 4 RT AT BS 720C PLUS 10. REPAIRED STRINGER 4 RIGHT AT BS 720C PLUS 10 PER SRM 53-10-3 FIG 3.Jan 12, 2006 · N485FE · Boeing 727200SDR 06FDEA0165Longeron · crackedCENTER CARGO COMPARTMENT RIGHT HAND TUNNEL STATION 5-123 LONGERON 33R FOUND CRACKED. CENTER CARGO COMPARTMENT RIGHT HAND TUNNEL STATION 5-123 LONGERON 33R REPAIRED AS PER SRM 53-10-00 FIGURE 1 VOLUME I. THIS REPAIR IS CLASSIFIED AS MAJOR REPAIR AS PEJan 12, 2006 · N607FE · Doug MD11SDR 06FDEA0164Stringer · corrodedCORROSION ON STRINGER 4 RT BS 620-700. CORROSION OUT OF LIMITS, STRINGER SECTION BS 660 - 720E TO BE REPLACED ON CARD N00343.Jan 12, 2006 · N488FE · Boeing 727200SDR 06FDEA0163Stringer · corrodedCORROSION ON STRINGER 2 LT BS 640-700. CORROSION OUT OF LIMITS, STRINGER SECTION TO BE REPLACED ON CARD N00346.Jan 12, 2006 · N488FE · Boeing 727200SDR 06FDEA0162Stringer · corrodedCORROSION ON STRINGER 3 RT BS 620-700.Jan 12, 2006 · N488FE · Boeing 727200SDR 06FDEA0143Longeron · corrodedFUSELAGE: CTR SECTION R3 DOOR EXTERIOR STA 1189-1301, LONGERON 27-28 FOUND STRINGER CORRODED & CRACKED DURING SCUFF PLATE OPEN-UP. REPAIR CARRIED OUT AS PER FEDEX EA 1-5310-90725.Jan 11, 2006 · N607FE · Doug MD11SDR 06FDEA0142Longeron · corrodedFUSELAGE CTR SECTION L3 DOOR EXTERIOR STA 1189-1301, LONGERON 27-28 FOUND STRINGER CORRODED & CRACKED DURING SCUFF PLATE OPEN-UP. REPAIRED AS PER FEDEX EA 1-5310-90717.Jan 11, 2006 · N607FE · Doug MD11SDR DHL2006763511Stringer · corrodedS/O 284007 N/R 032080 - CORROSION ON S-28L IN AFT PIT OUTBD SIDE BETWEEN BS 970 - 990. CUT OUT CORRODED SECTION. FABRICATED AND INSTALLED STRINGER REPAIRS 5.5" X 3.6" FROM 7075-T6 .040 AND 25-1/4" X 11-1/4" FROM BAC1498-131 AT BS 950F + 9.25" - 984.5 S-28L IAJan 10, 2006 · N763AT · Boeing 727264SDR DHL2006763504Stringer · corrodedS/O 284007 N/R 031818 - FWD CARGO S-27R AT BS 560 HAS EXFOLIATION CORROSION. CUT OUT CORRODED SECTION BS 568 - 547.2 S-27R. FABRICATED AND INSTALLED REPAIRS 3.150" X .090" X .800" FROM 7075-T6 .090, 20.800" X 3.00" X 1.250" FROM BAC1498-131 AND 1.650" X .825"Jan 10, 2006 · N763AT · Boeing 727264SDR USAA0512Angle · crackedBETWEEN STA 927 AND 947.5 AT BL 0 CRACK. INSTALLED NEW ANGLE IAW SRM 51-40-02, DEFECT SIZE: 1 INCH CRACK.Jan 10, 2006 · N784AU · Boeing 7374B7SDR 06FDEA0131Stringer · damagedAFT CARGO COMPARTMENT HOLE IN STR 23 LT B/S 965. REPAIRED AFT CARGO COMPARTMENT STR 23L AT BS 965, HOLE IN TOP OF STR IAW SRM 53-10-3.Jan 9, 2006 · N191FE · Boeing 72722SDR 06FDEA0101Stringer · misdrilledFOUND MCD STRINGER 4L AT STA 450 HAS TOOLING MARKS AND 2 DRILLED MARKS ON OUTBD SIDE OF STRINGER, AFTER BLENDING AND FOUND OUT OF LIMITS PER SRM 5310-01, FIG 1, REMOVED AND REPLACED ALL DAMAGE PARTS IAW SRM 51-30-3.Jan 9, 2006 · N498FE · Boeing 727200SDR MWEA060003Longeron · crackedLONGERON 17 RIGHT IS CRACKED AT STATION 408 WHERE IT ATTACHES TO THE FRAME AT THE LOWER POSITION. FABRICATED AND INSTALLED DOUBLER.Jan 9, 2006 · N808ME · Doug DC982SDR AWXA200600308Stringer · corrodedMCN - DURING C24 CHECK DISCOVERED CORROSION ON STRINGER 26R FROM BS 1006 TO BS 1012. MAINTENANCE REMOVED STRINGER AND FABRICATED REPLACEMENT STRINGER IAW BOEING 737-300 SRM 51-30-01-0G. INSTALLED FABRICATED REPLACEMENT STRINGER AT STR 26R AND FROM BS 1006 TOJan 8, 2006 · N328AW · Boeing 7373B7SDR QXEA200600137Stringer · corrodedPDX: FOUND STR 31R HAS CORROSION AT 2 RIVETS, STA X25. MAINTENANCE REPAIRED IAW Q400 SRM 51-42-05.Jan 8, 2006 · N400QX · Bombdr DHC8402SDR 0601026Stringer · crackedFUSELAGE STRINGER REPAIRED DUE TO CRACK.Jan 6, 2006 · N767TW · Boeing 737230CSDR 0601025Stringer · corrodedFUSELAGE STRINGER REPAIRED DUE TO CORROSION.Jan 6, 2006 · N767TW · Boeing 737230CSDR 0601003Stringer · corrodedSTRINGER SECTION WAS REPAIRED DUE TO CORROSION.Jan 6, 2006 · N767TW · Boeing 737230CSDR UPS06845979Longeron · crackedINSPECTION TYPE:C3 LONGERON 34R CRACKED AT STA 1420. REMOVED LONG 34R IAW SRM 51-1-20D, FABRICATED AND INSTALLED LONG 34R AT STA 1420 IAW DWG 3645937, SRM 51-1-8, AND SRM 51-1-20D.Jan 6, 2006 · N718UP · Doug DC871FSDR IXXA06SMN013SLongeron · crackedDURING ROUTINE C-CHECK INSPECTION, FWD CARGO COMPT L-34L CRACKED BETWEEN STA 600.000 AND STA 620.000. PERFORMED MAJOR REPAIR. REMOVED FASTENERS, REMOVED LONGERON SEGMENT. FABRICATED SPLICES (02 EA) (EXTRUSION BAR 7075 T6 51) FABRICATED NEW LONGERON SEGMENT Jan 5, 2006 · N722CX · Doug DC872SDR IXXA06SMN014SLongeron · crackedDURING ROUTINE C CHECK INSPECTION, FWD CARGO COMPT L-33L CRACKED, STA 600.000 - STA 620.000. REMOVED CORROSION FROM FWD CARGO COMPT INTERNAL SKIN (SAT 570.000 – 580.000, L-29R TO L-29R TO L-26R) IAW DC-8 SRM 51-1-8 PAGES 17-18 (MATERIAL THICKNESS: 0.063”, BLEJan 5, 2006 · N722CX · Doug DC872SDR IXXA06SMN009SLongeron · corrodedDURING ROUTINE C-CHECK INSPECTION, FWD CARGO COMPT - L-36 CORRODED AT STA 286.000. REMOVED LEVEL I CORROSION IAW DC-8 SRM 51-1-8 PAGES 17-18 MEASURED: THICKNESS: 0.120, BLEND OUT: 0.003, REMAINING THICKNESS: 0.117. FOUND WITHIN ALLOWABLE LIMITS IAW DC-8 SRM Jan 5, 2006 · N722CX · Doug DC872SDR UPS06845976Longeron · crackedINSPECTION TYPE:C1 LONG 10L IS CRACKED ON LWR SIDE AT CANTED WEB STA 1720 AT LWR NUT. CUT OUT DAMAGED AREA IAW SRM 53-2-2 FIG 11 FABRICATED AND INSTALLED REPAIR ANGLE AND FILLER AT STA 1720 L10L IAW SRM 53-2-2 FIG 11, SRM 51-1-8 AND SRM 51-1-20D.Jan 5, 2006 · N852UP · Doug DC873FSDR QXEA200600032Stringer · corrodedPDX - CLEAT IS CORRODED ON STRINGER 26R, AFT OF X424.124 SPAR FRAME. REPAIRED IAW DHC-8-200 SRM 51-20-16, SRM 51-40-00 AND SRM 51-40-11.Jan 4, 2006 · N379PH · Dhav DHC8202SDR ABXA060049Longeron · crackedLONGERON 17 RIGHT CRACKED AT FS 1056. REPLACED LONGERON SECTION AS REQUIRED IAW DC9 SRM LONGERON SPLICE REPAIR 53-02.Jan 4, 2006 · N976AX · Doug DC941SDR 06FDEA00019Stringer · dentedDENTED STRINGER AT STA 493, STR 8RT. *S/D* REPAIRED STRINGER PER SRM 53-10-3.Jan 4, 2006 · N191FE · Boeing 727100
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