JASC 5413

Service difficulty reports · 220

Reports filed under 5413 · Nacelle/Pylon, 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 = '5413'
  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 FOTR23141NR29847Stringer · corrodedFWD CARGO BAY AT BS 500G, STRINGER 28L HAS CORROSION. REPAIRED ON WO 23141.Oct 1, 2013 · N263VT · Boeing 7374Q8SDR SWAA2013061917421Longeron · crackedNR 1 ENGINE APRON LONGERON AT AFT COWL ATTACH POINT CRACKED. REPAIRED LONGERON IAW SRM.Jun 14, 2013 · N974AT · Boeing 717200SDR DALA13027340129Stringer · corrodedFWD CARGO COMPARTMENT BS 446, S33L, STRINGER CORRODED. FOUND OUT OF LIMITS SRM 53-00-03, FIG 101, REV 92 AND REPAIR CARRIED OUT IAW SRM 53-00-03, FIG 201.Jun 3, 2013 · N129DL · Boeing 767332SDR VGCA20130523001Longeron · crackedNACELLE, RT LOWER INBD LONGERON CRACKED.May 23, 2013 · N141FL · Cvac 580SDR SWAA2013052216378Longeron · crackedNR 1 ENG PYLON/APRON CRACKED ON UPPER LONGERON AT AFT HINGE CUT OUT. REPAIRED PYLON IAW T/R.May 3, 2013 · N964AT · Boeing 717200SDR SWAA2012112009672Longeron · crackedCRACK LOCATED ON NR1 ENGINE PYLON APRON AT UPPER AFT COWL HINGE CUT OUT. STOP DRILLED 2 CRACKS IN UPPER LONGERON OF NR 1 ENGINE PYLON AT AFT CUT OUT, FABRICATED AND INSTALLED REPAIR Z ANGLE IAW B-717 SRM 51-41-05 51-41-01, 51-41-04.Nov 14, 2012 · N946AT · Boeing 717200SDR UALA2012071303790Firewall · wornNR 1 ENGINE PYLON FIREWALL OTBD SIDE FAN COWL SUPPORT BEAM INSTALLATION WEB WORN. COMPLETED REPAIR OF NR 1 ENGINE PYLON FIREWALL OTBD SIDE AT PPS 125 IAW EA 57-54- 001 AND ECRA 5450-01966.Jul 11, 2012 · N550UA · Boeing 757222SDR LR7A2012040500356Longeron · corrodedDURING SCHEDULED C-10 CHECK, FOUND NR 3 QEC RT LOWER LONGERON CORROSION AT INNER LOWER FLANGE AT FS 473. REPAIRED BY REPLACEMENT IAW SMP583 51-70 & 54-20, PAGES 2 THROUGH 4.Apr 5, 2012 · N404LC · Lkheed 382GSDR DALA1217696304Stringer · crackedNR 3 PYLON INBOARD SIDE STRINGER AT NACELLE STA 346.402 FOUND CRACKED AT AROUND FASTENER HOLE AREA. ENTERED AND DEFERRED FOR SDR REPORTING. REPAIRED PER PRI 501588-14.Mar 22, 2012 · N664US · Boeing 747451SDR FXGA201202251213Attach Angle · crackedNR 4 NACELLE INBD ATTACH ANGLE CRACKED. R & R CRACKED ANGLE.Feb 25, 2012 · N151 · Doug DC6BSDR CA120214006Longeron · cracked(CAN) WHILE CONDUCTING A CORROSION INSPECTION, CRACKS WERE FOUND ON THE NR 1 NACELLE OTBD LONGERON CHANNEL, PN 75410103-105 AND LONGERON ANGLE, PN 75410104-103 AND NR 4 NACELLE INBD LONGERON CHANNEL, PN 75410119-106 AND LONGERON ANGLE, PN 75410120-104. THE CFeb 13, 2012 · Dhav DHC7102SDR ERAA201200011Stringer · crackedTWO CRACKS ON LT NACELLE SKIN STRINGERS UNDER EXHAUST FINGERNAIL.Feb 8, 2012 · N881EA · Dhav DHC8106SDR HNAA2012011600481Stringer · corrodedSTRINGER 31 RT AT STA X336 IS CORRODED. BLENDED MINOR SURFACE CORROSION IAW SRM 51-20-11. ALODINED AND PRIMED AREA IAW AMM 51-25-03.Jan 16, 2012 · N908HA · Dhav DHC8102SDR FDEA201111295073Longeron · crackedPANEL 485AL, TOP ATTACH ANGLE ON LT SIDE, 8TH HOLE FWD HAS A CRACK APPROX 3" LONG, JUST BELOW IT. R & R LT LONGERON ANGLE ON PANEL 485AL IAW SRM 54-55-51, FIG 205 AND SRM 51-40-21.Nov 29, 2011 · N746FD · Airbus A300F4605RSDR EIAA2011218Stringer · crackedNR 2 PYLON (INTERIOR), PANEL CUTOUT NR 463CL AT NAC STA 180.0, I/B SRTINGER FOUND CRACKED. CRACKED STRINGER REMOVED AND REPLACED PER SRM 51-30-02.Aug 24, 2011 · N486EV · Boeing 747212BSDR IXXA110050SStringer · delaminatedDURING ROUTINE B-CHECK INSPECTION FOUND NR 1 ENGINE LOWER STRINGER DELAMINATED. R & R DAMAGED STRINGER IAW MM 78-10-2.Jul 23, 2011 · N71CX · Doug DC862FSDR S9BA20110005Longeron · crackedRT ENGINE NACELLE OTBD LONGERON CRACKED. FOUND ON ROUTINE INSPECTION, REMOVED AND REPLACED RIGHT NACELLE OTBD LONGERON. FOUND ON ROUTINE INSPECTION.May 28, 2011 · Dhav DHC6300SDR VGCA20110517Longeron · corrodedRIGHT NACELLE STA 8 AND 6 LONGERON HAD SEVERE CORROSION.May 17, 2011 · N191FL · Cvac 580SDR ZZDA2011259Longeron · crackedNR 1 ENGINE APRON LOWER LONGERON AND UPPER FRAME, CRACKED. ACCOMPLISHED LOWER LONGERON AND UPPER FRAME DOUBLER REPAIR PER TRA 17-54-TR00129.Mar 3, 2011 · N970AT · Boeing 717200SDR V0XR20110225001Stringer · cracked(V0XR) STRINGER IN LT NACELLE HAS A CRACK AT AFT END I/B STA YN6, XN 169.9 TO XN 206.0. REPLACED STRINGER IN LT NACELLE I/B AT YN6 FROM XN 169.9 TO XN 206 IAW DHC8-100 SRM 51-10-00, 51-40-11.Feb 25, 2011 · N883EA · Dhav DHC8106SDR VGCA20110203Longeron · corrodedLEFT NACELLE OTBD LONGERON HAD CORROSION.Feb 3, 2011 · N371FL · Cvac STC3405800SDR ZZDA2011034Longeron · crackedFWD OF AFT MOUNT, LEFT PYLON APRON UPPER AND LOWER LONGERON, CRACKED. ACCOMPLISHED LONGERON DOUBLER REPAIR PER EA17-54-02261IR.Jan 11, 2011 · N966AT · Boeing 717200SDR ZZDA2011032Longeron · crackedFWD OF YOKE MOUNT, LEFT PYLON APRON LOWER LONGERON, CRACKED. ACCOMPLISHED LONGERON DOUBLER REPAIR PER EA 17-54-02261IR.Jan 11, 2011 · N966AT · Boeing 717200SDR FDEA201010284181Fitting · corrodedNR1 ENG PYLON RIB 18 FWD SIDE CORRODED ABOVE THE BRG REMOVED NR1 PYLON AFT ATTACH FITTING AT RIB 18 IAW AMM 54-51-75-04. REMOVED CORROSION FROM RIB 18 LUG IAW SRM 51-74-10 , CHECKED FOR LIMITS FOUND OUT OF LIMITS IAW SRM 54-51-71, PAGE 110. INSTALLED NEW FITTOct 28, 2010 · N815FD · Airbus A310324SDR S9BA20100007Longeron · cracked(CLOSED) LT INBD LONGERON CRACKED AT NACELLE STA 47. (THIS WAS FOUND ON AS ROUTINE INSP)Oct 27, 2010 · Dhav DHC6300SDR VGCA20100805Longeron · corrodedLEFT INBD UPPER NACELLE LONGERON HAD EXCESSIVE CORROSION.Aug 5, 2010 · N191FL · Cvac 580SDR S9BA20100004Longeron · crackedRT NACELLE INBD NACELLE LONGERON CRACKED (CRACK IS LESS THEN .2500 INCH NACELLE STA 48) R & R WITH FACTORY NEW PART.Jul 28, 2010 · Dhav DHC6300SDR 2010FA0000431Longeron · crackedNR 3 ENG LT SIDE COWL UPPER LONGERON CRACK. INSTALL REPAIR DOUBLER.Apr 5, 2010 · N708SA · Boeing 7472B5FSDR UIEA201000108Stringer · crackedEO: 4454A096 DURING C-CHECK, A CRACK WAS FOUND IN THE 311U2420-83 PYLON STRINGER TEE AT APPROX NAC STA 300, WL 144.7 ON THE OTBD SIDE. THE CRACK WAS TRIMMED OUT AND A NEW SECTION OF TEE SPLICED IAW SRM 54-51-02, REPAIR 2 WITH MINOR DEVIATIONS IAW EGAT EI T2010Mar 24, 2010 · N418MC · Boeing 74747UFSDR 22AA201000059Longeron · crackedDURING "C" CHECK, NR 2 ENG RT CORE COWL UPPER LONGERON FOUND WITH CRACK. NON-ROUTINE NR 0202, CRACKED UPPER LONGERON AT NR 2 ENGINE RT CORE COWL AREA REPAIRED IAW 1017-10 WORK INSTRUCTIONS AND FAA APPROVED FROM 8110-3 DATED 12 MARCH 2010.Feb 24, 2010 · N478CT · Doug DC1030FSDR 22AA201000056Longeron · crackedDURING "C" CHECK, NR 2 ENGINE LT CORE COWL UPPER LONGERON FOUND WITH CRACK. NON-ROUTINE NR 0197, CRACK AREA AT NR 2 ENGINE LT CORE COWL UPPER LONGERON AREA REPAIRED IAW EN 1017-10 WORK INSTRUCTIONS AND FAA APPROVED FORM 8110-3 DATED 12 MARCH 2010.Feb 24, 2010 · N478CT · Doug DC1030FSDR 22AA201000055Longeron · crackedDURING "C" CHECK, NR 2 ENGINE LT CORE COWL LOWER LONGERON FOUND WITH CRACK. NON-ROUTINE NR 0196, CRACK AREA AT NR 2 ENGINE LT CORE COWL LOWER LONGERON AREA REPAIRED IAW EN 1017-10 WORK INSTRUCTIONS AND FAA APPROVED FORM 8110-3 DATED 12 MARCH 2010.Feb 24, 2010 · N478CT · Doug DC1030FSDR 22AA201000053Longeron · crackedDURING "C" CHECK, NR 3 ENGINE RT CORE COWL LOWER LONGERON CRACKED AT APPROX AT MID AND AFT FRAME SECTION. NON-ROUTINE NR 0163, CRACK AREA AT MID AND AFT SECTION OF LOWER LONGERON AT NR 3 ENGINE RT CORE COWL AREA REPAIRED IAW EN 1018-10 WORK INSTRUCTIONS AND FFeb 24, 2010 · N478CT · Doug DC1030FSDR 22AA201000052Longeron · crackedDURING "C" CHECK, NR 3 ENGINE LT CORE COWL LOWER LONGERON AFT SECTION FOUND CRACKED. NON-ROUTINE NR 0159, CRACK AREA AT NR 3 ENGINE LT CORE COWL LOWER LONGERON AFT SECTION REPAIRED IAW EN 1018-10 WORK INSTRUCTIONS AND FAA APPROVED FORM 8110-3 DATED 12 MARCH 2Feb 24, 2010 · N478CT · Doug DC1030FSDR 22AA201000051Longeron · crackedDURING "C" CHECK, NR 1 ENG, RT CORE COWL LOWER LONGERON AND STRAP FOUND CRACKED. NON-ROUTINE NR 0125, CRACKED STRAP AND LOWER LONGERON AT NR 1 ENGINE RT CORE COWL AREA REPAIRED IAW EN 1016-10 WORK INSTRUCTIONS AND FAA APPROVED FORM 8110-3 DATED 12 MARCH 2010.Feb 24, 2010 · N478CT · Doug DC1030FSDR 22AA201000050Longeron · crackedDURING "C" CHECK, NR 1 ENG LT CORE COWL LOWER LONGERON FOUND CRACKED. NON-ROUTINE NR 0124, CRACK AREA AT NR 1 ENGINE LT CORE COWL LOWER LONGERON AREA REPAIRED IAW EN 1016-10 WORK INSTRUCTIONS AND FAA APPROVED FORM 8110-3 DATED 12 MARCH 2010.Feb 24, 2010 · N478CT · Doug DC1030FSDR 22AA201000049Longeron · crackedDURING "C" CHECK, NR 1 ENGINE LT CORE COWL UPPER LONGERON FOUND CRACK. NON-ROUTINE NR 0123, CRACK AREA AT NR 1 ENG LT CORE COWL UPPER LONGERON AREA REPAIR IAW EN 1016-10 AND FAA APPROVED FORM 8110-3 DATED 12 MARCH 2010.Feb 24, 2010 · N478CT · Doug DC1030FSDR 2010FA0000363Longeron · worn(KADY) WORN AND BROKEN OF UPPER LONGERON AT NR 2 ENGINE RT SIDE COWL. MINOR REPAIR ACCOMPLISHED BY TRIM OUT THE DAMAGED UPPER LONGERON AND INSTALL REPAIR PARTS.Feb 20, 2010 · N749SA · Boeing 747300SDR 2010FA0000362Longeron · worn(KADY) WORN AND BROKEN OF UPPER LONGERON AT NR 1 ENGINE RT SIDE COWL. MINOR REPAIR ACCOMPLISHED BY TRIM OUT THE DAMAGED UPPER LONGERON AND INSTALL REPAIR PARTS.Feb 20, 2010 · N749SA · Boeing 747300SDR 2010FA0000326Longeron · worn(KADY) WORN AND BROKEN OF UPPER LONGERON AT NR 4 ENGINE SIDE COWL. MONOR REPAIR ACCOMPLISHED BY TRIM OUT THE DAMAGED UPPER LONGERON AND INSTALL REPAIR PARTS.Feb 16, 2010 · N749SA · Boeing 747300SDR SWIA201023711Stringer · crackedSHEET METAL DAMAGE TO DOUBLER AT RIGHT INBOARD MAIN LANDING GEAR FORWARD DOOR. (SERVICE CK) REPLACED CRACKED INBOARD NACELLE STRINGER PER SRM.Feb 14, 2010 · N284YV · Emb EMB120ERSDR 22AA201000047Longeron · crackedDURING "C" CHECK, NR 2 ENG RT CORE COWL LOWER LONGERON AND STRAP FOUND CRACKED. NON-ROUTINE NR 394, CRACKED LONGERON AND STRAP AT NR 2 ENG RT CORE COWL LOWER LONGERON AREA REPAIRED IAW EN 1006-10 WORK INSTRUCTIONS AND FORM 8110-3 DATED 26 FEB 2010.Feb 13, 2010 · N524MD · Doug DC1030FSDR 22AA201000046Longeron · crackedDURING "C" CHECK, NR 2 ENG RT CORE COWL UPPER LONGERON FOUND WITH CRACK AT 02 LOCATIONS. NON-ROUTINE NR 392, CRACKED LONGERON 02 EACH LOCATIONS AT NR 2 ENGINE RT CORE COWL UPPER AREA REPAIRED IAW EN 1006-10 WORK INSTRUCTIONS AND FORM 8110-3 DATED 26 FEB 2010.Feb 13, 2010 · N524MD · Doug DC1030FSDR 22AA201000045Longeron · crackedDURING "C" CHECK, NR 1 ENGINE LT CORE COWL UPPER LONGERON FOUND WITH CRACK. NON-ROUTINE NR 324, CRACKED NR 1 ENG LT CORE COWL UPPER LONGERON AREA REPAIRED IAW EN 1006-10 WORK INSTRUCTIONS AND FORM 8110-3 DATED 26 FEB 2010.Feb 13, 2010 · N524MD · Doug DC1030FSDR 22AA201000044Longeron · crackedDURING "C" CHECK, NR 3 ENGINE LT CORE COWL UPPER LONGERON FOUND WITH CRACK. NON-ROUTINE NR 323, CRACKED LONGERON AT NR 3 ENG LT CORE COWL UPPER AREA REPAIRED IAW EN 1006-10 WORK INSTRUCTIONS AND FORM 8110-3 DATED 26 FEB 2010.Feb 13, 2010 · N524MD · Doug DC1030FSDR 22AA201000043Longeron · crackedDURING "C" CHECK, NR 2 ENGINE LT CORE COWL FOUND UPPER LONGERON WITH CRACK. NON-ROUTINE NR 393, CRACK AREA AT NR 2 ENGINE LT CORE COWL UPPER LONGERON AREA REPAIRED IAW ENGINEERING NOTE (EN) 1006-10 WORK INSTRUCTIONS AND FAA APPROVED FORM 8110-3 DATED 26 FEB 2Feb 13, 2010 · N524MD · Doug DC1030FSDR SWIA200922185Stringer · crackedLEFT NACELLE STRINGER AT FRAME 10 CRACKED. (C CHECK) REPLACED PER SRM.Jul 1, 2009 · N223SW · Emb EMB120ERSDR S9BA20090008Longeron · crackedRT NACELLE OTBD LONGERON CRACKED. REMOVED AND REPLACED RT NACELLE OTBD LONGERON WITH FACTORY NEW PART.Apr 12, 2009 · N888PV · Dhav DHC6300SDR KCSA091010Stringer · crackedNR 2 PYLON O/B STRINGER CRACKED AT FWD ENG MOUNT BULKHEAD CHORD INTERNAL ANGLE ATTACH POINT, LOWER SIDE.Feb 17, 2009 · N746CK · Boeing 747246FSDR S9BA2008027Longeron · crackedLT ENG NACELLE INBOARD LONGERON CRACKED 10.5 INCHES AFT OF THE FWD END. REMOVED AND REPLACED LT ENG INBOARD LONGERON IAW AC 43.13-1B CH 4, RD 6-54-036. (S)Aug 6, 2008 · N533SW · Dhav DHC6300
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