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 COEA2011083030816Stringer · dentedHEAVY CK COE / MAJOR REPAIR: STRINGER 7AL HAS A DENT BETWEEN FRAME 23D - 24. REPAIRED BY INSTALLING STRINGER SPLICE PER SRM AT STRINGER 7AL, 48 INCHES FWD OF FR 25 (23C-23D) TO FR25.Aug 30, 2011 · N816FX · Aerosp ATR72212SDR SWAA116176Stringer · corrodedDURING SCHEDULED 24Y CHECK, FOUND STRINGER CORRODED AT BS 500A, STR 26L. REPAIRED STRINGER IAW SRM.Aug 29, 2011 · N669SW · Boeing 7373A4SDR SWAA116132Stringer · crackedDURING SCHEDULED 24Y CHECK, FOUND FWD CARGO COMPARTMENT STRINGER CRACKED AT BS 440, STR 28R. REPAIRED STRINGER IAW SRM.Aug 29, 2011 · N669SW · Boeing 7373A4SDR SWAA116114Stringer Splice · corrodedDURING SCHEDULED 16Y CHECK, FOUND STRINGER SPLICE CORRODED AT BS 907, STR 22R. REMOVED AND REPLACED SPLICE IAW SRM AND DWG.Aug 29, 2011 · N622SW · Boeing 7373H4SDR C2XA11SH123Stringer · crackedSHV - DURING C-CHECK STRINGER 2L WAS FOUND TO BE CRACKED AT FRAME 75. MAINTENANCE REMOVED THE CRACKED SEGMENT AND PERFORMED A STRINGER SPLICE REPAIR IAW EC5310-01563. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Aug 29, 2011 · N14959 · Emb EMB145LRSDR FDEA201108293545Longeron · corrodedLONGERON 16L BS 1199-1219 CORRODED. CORROSION EXCEEDED SRM LIMITS IAW SRM 53-00-00 REV 47, FIG 205. LONGERON REMOVED IAW SRM 51-31-01, REV 47. NEW LONGERON FABRICATED IAW DWG AEA7063, REV G AND INSTALLED SRM 51-31-01, REV 47. REPAIR CLASSIFIED AS MAJOR Aug 29, 2011 · N643FE · Doug MD11FSDR FDEA201108293544Longeron · corrodedLONGERON 16L BS 1179-1199 CORRODED. CORROSION REMOVED IAW SRM 51-21-01, REV 47. ORGINAL THICKNESS = 0.125"; MATERIAL REMOVED = 0.065"; MATERIAL REMAINED = 0.060 INCH, FOUND EXEEDED LIMIT IAW SRM 53-00-00, REV 47, FIG 205. NEW LONGERON FABRICATED IAW DWG AAug 29, 2011 · N643FE · Doug MD11FSDR FDEA201108293543Longeron · corrodedLONGERON 16L, BS 1179-1199 CORROSION EXCEEDED SRM LIMITS. NEW LONGERON FABRICATED IAW DWG AEA7065, REV B AND INSTALLED IAW SRM 51-31-01, REV 47. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.Aug 29, 2011 · N643FE · Doug MD11FSDR COMA2011082950063Doubler · crackedON STRINGER STR 3, 2.5 INCHES AFT FROM FS 280 BULKHEAD THERE IS A VERTICAL CRACK ON STRINGER DOUBLER. REMOVED AND INSTALLED A SERVICEABLE STRINGER 3 DOUBLER AT FS 280.00 AND FS 295.00 IAW SRM SOLID RIVETS 51-42-06, HI LITES 51-42-20 AND EO DRW 601R31522 AND MAug 29, 2011 · N969CA · Cndair CL6002B19SDR SWIA201129953Stringer · corrodedSTRINGER 18L HAS CORROSION BELOW FORWARD PASSENGER DOOR ACTUATOR. (C-CHECK) REPAIRED STRINGER 18L.Aug 28, 2011 · N296SW · Emb EMB120ERSDR FDEA201108283536Stringer · corrodedSTRINGER 30 IS CORRODED BETWEEN BS 950- 950A. CUT OUT DAMAGED AREA OF STRINGER SECTION. FABRICATED REPAIR, LOCATED AND DRILLED, TREATED AND PRIMED. INSTALLED REPAIR IAW EA 7-5310-152442.Aug 28, 2011 · N236FE · Boeing 727247SDR USAA2011090100023Stringer · crackedQ5 CHECK - CRACK ON STRINGER AT BS 1011, S7L. REPLACED STRINGER AT BS 1011, S7L IAW BOEING DRAWING 65-52988 & SRM 51-10-02.Aug 26, 2011 · N425US · Boeing 737401SDR FDEA201108263522Stringer · corrodedSTRINGER 30 CORRODED BETWEEN BS 1030 TO 1050. CUT OUT DAMAGE AREA ON STRINGER 30 IAW SRM 53-10-3 FIG 1. FABRICATED NEW STRINGER SECTION AND SPLICE IAW SRM 53-10-3 FIG 1. INSTALLED ALL REPAIR PART IAW SRM 53-10-3 FIG 1.Aug 26, 2011 · N236FE · Boeing 727247SDR FDEA201108263523Stringer · corrodedSTRINGER 28L IS CORRODED ON FWD SIDE OF FRAME AT BS 950B. CUT OUT DAMAGE, FABRICATED REPAIR PARTS, AND INSTALLED IAW SRM 51-30-2 REV 103.Aug 26, 2011 · N236FE · Boeing 727247SDR QXEA2011083000767Stringer · corrodedSTRINGER 30S IS CORRODED, FRAME 1.00 TO 19.4. REMOVED CORROSION IAW SRM 51-21-00-00-01 AND RD 8/4-53-3888, MINIMUM REMAINING THICKNESS .057", CONFIRMED CRACK FREE REF NTM 51-00-02-250-801 AND 51-00-01-250-801. MATERIAL LOSS FOUND TO BE WITHIN LIMITS IAW RD 8Aug 26, 2011 · N5300 · Dhav DH82ASDR ALGAR8291153069Longeron · crackedDURING 50 HR, LT UPPER AFT LONGERON CRACKED AT STA 204.92. INSPECTED AND REPLACED LT UPPER AFT LONGERON PN 206-031-314-237, C/W ASB 407-11-95 PART III, INSTALLATION OF 3 EXTERNAL STRAP DOUBLERS, PART V, TERMINATING ACTION TO RECURRING INSPECTION.Aug 26, 2011 · N436AL · Bell 407SDR KCSA111201Stringer · corrodedBS 2164, STR 49L HAS CORROSION.Aug 26, 2011 · N701CK · Boeing 747259BSDR KCSA111199Stringer · crackedBS 2231 STRINGER 16R HAS A CRACK IN FWD (AND AFT) CHORD OF FRAME.Aug 26, 2011 · N701CK · Boeing 747236BSDR FDEA201108263512Longeron · corrodedCENTER CARGO COMPARTMENT STA 5-83 TO STA 5-93, RT LONGERON NR33R CORRODED. LONGERON REMOVED IAW SRM 51-21-01, REV 47. ORIGINAL MATERIAL THICKNESS= 0.060"; MATERIAL REMOVED = 0.040"; MATERIAL REMAINED = 0.030" - FOUND EXCEEDED LIMITS IAW SRM 53-00-00 REV 47, Aug 26, 2011 · N643FE · Doug MD11FSDR A6WA201140791Stringer · chafedLT STRINGER NEX TO LT OIL REPLENISH TUBE CHAFED. REPAIRED LT STRINGER 12 NEXT TO LT OIL REPLENISH TUBE BY INCORPORATING SRM STRINGER. REPAIR CHAPTER 53-00-03, FIG 202, SHEET G.Aug 25, 2011 · N408AW · Cndair CL6002B19SDR UIEA2011082500470Stringer · crackedBS 988, STRINGER 16L CRACKED.Aug 25, 2011 · N523MC · Boeing 7472D7BSDR QXEA2011082600754Stringer Splice · corrodedSTRINGER 24S SPLICE AT FR 116.0 HAS CORRODED FASTENERS AND POSSIBLE CORROSION. BLENDED OUT CORROSION IAW SRM 51-21-00-00-01. MINIMUM REMAINING THICKNESS .051", CONFIRMED CRACK FREE REF NTM 51-00-01-250-801 AND 51-00-02-250-801. MATERIAL LOSS FOUND TO BE WITAug 25, 2011 · N427QX · Bombdr DHC8402SDR FDEA201108253477Longeron · corrodedCORROSION ON LONGERON 12R AT BS 1239-1299. CORROSION REMOVED IAW SRM 51-21-01, REV 47. ORIGINAL THICKNESS = 0.173 INCH; MATERIAL REMOVED = 0.055 IN; MATERIAL REMAINED = 0.118 IN AND FOUND EXCEEDED LIMITS SRM 53-22-00, REV 47, FIG 205. LONGERON SECTION REMOVAug 25, 2011 · N643FE · Doug MD11FSDR JR2R2011082500357Stringer · corrodedSTRINGER 26R BETWEEN FS 280 AND 333 CORRODED.Aug 25, 2011 · N909FJ · Cndair CL6002D24SDR QXEA2011082600757Stringer · corrodedSTRINGER 31S CORRODED FR 604.5 TO 624.5. BLENDED OUT CORROSION IAW SRM 51-21-00-00-01 AND RD 8/4-53-3877. MINIMUM REMAINING THICKNESS .081", CONFIRMED CRACK FREE REF NTM 51-00-01-250-801 AND 51-00-02-250-801. TREATED, PRIMED IAW RD 8/4-53-3877.Aug 24, 2011 · N427QX · Bombdr DHC8402SDR QXEA2011082600756Stringer · corrodedSTRINGER 26S CORRODED FR 156 TO 176. BLENDED CORROSION IAW SRM 51-21-00-00-01. MINIMUM REMAINING THICKNESS .062", CONFIRMED CRACK FREE REF NTM 51-00-01-250-801 AND 51-00-02-250-801. MATERIAL LOSS FOUND TO BE WITHIN LIMITS IAW RD 8/4-53-3879. ALODINED, PRIMAug 24, 2011 · N427QX · Bombdr DHC8402SDR QXEA2011082600755Stringer · corrodedSTRINGER 26S CORRODED FR 136 TO 156. BLENDED OUT CORROSION IAW SRM 51-21-00-00-01. MINIMUM REMAINING THICKNESS .066", CONFIRMED CRACK FREE REF NTM 51-00-01-250-801 AND 51-00-02-250-801. MATERIAL LOSS FOUND TO BE WITHIN LIMITS IAW RD 8/4-53-3879. ALODINED, Aug 24, 2011 · N427QX · Bombdr DHC8402SDR EIAA2011206Stringer · crackedREMOVE AND REPLACE REPAIR ON S37R BETWEEN BS 421 & 430. EXISTING REPAIR REMOVED AND NEW REPAIR INSTALLED PER B747 SRM 53-10-03 FIGURE 3.Aug 24, 2011 · N486EV · Boeing 747212BSDR EIAA2011204Stringer · crackedREMOVE AND REPLACE REPAIR ON S38L BETWEEN BS 480 TO 500. EXISTING REPAIR REMOVED AND NEW REPAIR INSTALLED PER B747 SRM 53-10-03 FIGURE 3.Aug 24, 2011 · N486EV · Boeing 747212BSDR EIAA2011203Stringer · crackedREMOVE AND REPLACE REPAIR ON S37L BETWEEN BS 460 & 480. EXISTING REPAIR REMOVED AND NEW REPAIR INSTALLED PER B747 SRM 53-10-03 FIGURE 3.Aug 24, 2011 · N486EV · Boeing 747212BSDR SWAA116034Stringer · crackedDURING SCHEDULED SPV CHECK, FOUND STRINGER CRACKED AT BS 787, STR 1. REPAIRED STRINGER IAW EA.Aug 24, 2011 · N632SW · Boeing 7373H4SDR SWAA116021Stringer · corrodedDURING SCHEDULED 26Y CHECK, FOUND STRINGER CORRODED BETWEEN BS 480 TO BS 500, STR 28R. REPAIRED STRINGER IAW SRM.Aug 24, 2011 · N316SW · Boeing 7373H4SDR FDEA201108233418ALongeron · corrodedCABIN RT FUSELAGE LONGERON 16R STA 1159 TO STA 1179 FOUND WITH CORROSION. CORROSION REMOVED IAW SRM 51-21-01 REV 47 AND FOUND CRACKED. NEW LONGERON FABRICATED IAW DWG AEA0220, REV R. CRACKED LONGERON R & R IAW SRM 51-31-01, REV 47. REPAIR CLASSIFIED AS MAAug 23, 2011 · N662FE · Airbus A300F4605RSDR FDEA201108233425Stringer · corrodedSTRINGER 22R IS CORRODED BTWN BS 1183 -1166 WITH EXFOLIATION UNDER POWERED OUTFLOW VALVE. CUT OUT DAMAGED STRINGER IAW SRM 53-10-3 FIG 1. FABRICATED REPAIR PARTS IAW SRM 53-10-3 FIG 1 AND INSTALLED IAW SRM 51-30-2.Aug 23, 2011 · N236FE · Boeing 727233SDR EIAA2011202Stringer · crackedSTRINGER CRACKED AT BS 220 S0. CRACKED STRINGER REMOVED AND REPLACED WITH NEW STRINGER PER B747 SRM 51-30-02.Aug 23, 2011 · N486EV · Boeing 747212BSDR SWAA115962Stringer · crackedDURING SCHEDULED SPV CHECK, FOUND CREASE BEAM I/B CHORD STRINGER CRACKED AT BS 617, STR 17R. REPAIRED STRINGER PER SRM.Aug 23, 2011 · N676SW · Boeing 7373A4SDR SWAA115955Stringer · corrodedDURING SCHEDULED 26Y CHECK, FOUND STRINGER CORRODED BETWEEN BS 500B TO BS 500C, STR 27L. REMOVED AND REPLACED STRINGER IAW SRM AND DWG.Aug 23, 2011 · N316SW · Boeing 7373H4SDR FDEA201108233422Longeron · corrodedLONGERON 16R STA 1361 TO 1381 FOUND WITH CORROSION. CORROSION REMOVED SRM 51-21-01, REV 47. ORGINAL THICKNESS = 0.100 INCH; MATERIAL REMOVED = 0.050 INCH; MATERIAL REMAINED = 0.050 INCH, FOUND EXEEDED LIMIT IAW SRM 53-00-00 REV 47, FIGURE 205. LONGERON SAug 23, 2011 · N643FE · Doug MD11FSDR FDEA201108233420Longeron · corrodedCABIN RT FUSELAGE INTERCOSTAL AT LONGERON 18R STA 1381 TO STA 1401 FOUND WITH CORROSION. CORROSION REMOVED AS PER SRM 51-21-01 REV 47. ORIGINAL THICKNESS = 0.080 INCH; MATERIAL REMOVED = 0.040 INCH; MATERIAL REMAINED = 0.040 INCH, AND FOUND EXCEEDED LIMITSAug 23, 2011 · N678FE · Airbus A300F4605RSDR FDEA201108233419Longeron · corrodedLONGERON 20R STA 1401 TO STA 1421 FOUND WITH CORROSION. REMOVED IAW SRM 51-21-01, REV 47. ORIGINAL THICKNESS = 0.080 INCH; MATERIAL REMOVED = 0.040 IN; MATERIAL REMAINED = 0.040 IN, AND FOUND EXCEEDED LIMITS IAW SRM 53-00-00, REV 47, FIG 205. NEW LONGERON Aug 23, 2011 · N643FE · Doug MD11FSDR JR2R2011082100354Longeron · corrodedLONGERON AT STRINGER 25R CORRODED BETWEEN FS 364 AND 333.Aug 23, 2011 · N513MJ · Cndair CL6002C10SDR JR2R2011082100353Stringer Splice · corrodedSTRINGER 25R SPLICE CORRODED AT FS 333.Aug 23, 2011 · N513MJ · Cndair CL6002C10SDR JR2R2011082100352Stringer · corrodedSTRINGER 24R AT FS 305 CORRODED.Aug 23, 2011 · N513MJ · Cndair CL6002C10SDR JR2R2011082100351Stringer · corrodedSTRINGER 25R AT FS 305 CORRODED.Aug 23, 2011 · N513MJ · Cndair CL6002C10SDR FDEA201108223396Stringer · corrodedAFT PIT S28L IS CORRODED AT SPLICE AND ON INBD SIDE BETWEEN BS 970 - 990. REMOVED SPLICE AFT PIT STR 28L IAW SRM 51-30-2. FABRICATED NEW SPLICE IAW SRM 53-10-2, FIG 9 AND 53-10-3, FIG 1. INSTALLED NEW SPLICE IAW IAW SRM 51-30-2, REV 103.Aug 22, 2011 · N236FE · Boeing 727247SDR FDEA201108213395Longeron · damagedCENTER CARGO STA 1812 TO 1853, LONGERON 46 RT FOUND WITH SEVERAL FASTENERS DRILLED CLOSE TO RADIUS. REPAIRED AS PER EA 1-5310-150779, PART 1, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100, REV 112.Aug 21, 2011 · N642FE · Doug MD11FSDR FDEA201108213394Stringer · corrodedAFT CARGO BAY STRINGER 30 RT IS CORRODED BETWEEN BS 990-1030. FABRICATED NEW STRINGER SPLICE IAW SRM 53-10-3 FIG 1. & INSTALLED IAW SRM 51-30-2 REV 103.Aug 21, 2011 · N236FE · Boeing 727247SDR QXEA2011082300716Stringer · corrodedSTRINGER 31S HAS CORRODED FASTENERS AND POSSIBLE CORROSION FR 547.0 TO 564.5. REMOVED 12 RIVETS IAW SRM 51-42-05-02-01 AND BLENDED CORROSION IAW SRM 51-21-00-00-01. FOUND WITHIN LIMITS RD 8/4-53-3878. TREATED AND PRIMED IAW SRM 51-21-10-02-01, 51-25-10-02-01Aug 21, 2011 · N427QX · Bombdr DHC8402SDR JR2R2011082100343Stringer · corrodedDURING FINAL BUY OFF FOUND COROSION ON STR 26R FS 897.70. REMOVED AND REPLACED STR 26R FS 897.70 IAW CRJ 900 SRM 51-42-21, 51-42-06.Aug 21, 2011 · N911FJ · Cndair CL6002D24SDR JR2R2011082100342Stringer · corrodedSTR 21R CORRODED FS 333-379. REMOVED AND REPLACED STR 21R FS 333-379 IAW CRJ 900 SRM 51-42-06, 51-42-21.Aug 21, 2011 · N911FJ · Cndair CL6002D24
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