JASC 5313
Service difficulty reports · 36,303
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.
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
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR COEA2020030403819Stringer · corrodedWO 211121 NR 200038 HEAVY CHECK COE/MAJOR REPAIR: STRINGER 10AR HAS LEVEL 2 CORROSION BETWEEN FRAMES 23C-23D. CORRECTIVE ACTION: REPAIRED PER SRM 530000-300-826-A01.SDR REXA2020012870133Stringer Splice · corroded"LATE FINDING: CORROSION ON STRINGER AND SPLICE 21RH IN STA. FS= 333 TO FS= 349 AT MAIN AVIONICS COMPARTMENT. (E/E) (W1) TCI: 53-20-305
""CORROSION LEVEL 2. STRINGER AND SPLICE 21RH IN STA. FS= 333 TO FS= 349 AT MAIN AVIONICS COMPARTMENT WERE REPLACED PSDR C77A2020011700002Stringer · corrodedDURING BASIC CHECK AT EAMS, CORROSION WAS DISCOVERED ON THE CENTER FUSELAGE III STRINGER 21R BETWEEN FR89/FR90 (P/N 170-65257-001) DURING INSPECTION IN THE AREA. REFERENCE ETD2020-170-000573-B FIGURE 1 FOR DETAILS AND LOCATIONS. EAMS REQUESTED REPAIR DISPOSITISDR C77A2020011700001Stringer · corrodedDURING BASIC CHECK AT EAMS, CORROSION WAS DISCOVERED ON THE CENTER FUSELAGE III STRINGER 21L BETWEEN FR87/FR90 (P/N 170-91898-003) DURING INSPECTION IN THE AREA. REFERENCE ETD2020-170-000574-A FIGURE 1 FOR DETAILS AND LOCATIONS. EAMS REQUESTED REPAIR DISPOSITISDR SWIA2020030549069Stringer · corrodedLH STRG 26 HAS CORROSION ON APROX FS 350.00 (C-CHECK) RO 3/3/2020 REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS. C/W REO. NO LEAKS NOTEDSDR SWIA2020030549067Stringer · corrodedCORROSION FOUND ON STRG 20 FROM APROX FS 320.00 TO FS 333.00 ON BEAM. (C-CHECK) RO 3/3/2020 INSTALLED NEW BACK UP SILLS P/N- SH670-31822-1 AND SH670-31823 -1 REF: CRJ-900 S.R.M. NO LEAKS NOTED AT THIS TIMESDR SWIA2020030549003Stringer · corroded*CORROSION DETECTED ON STGR (20L), BETWEEN F.S. 379.00 AND F.S. 394.00 (MARKED). (C-CHECK) RO 3/3/2020 REMOVED STRG. 20 L/H @ FS 385.00 - FS 400.00 PER. REO AND CRJ 900 SRM FABRICATED AND INSTALLED SPLICE REPAIR ANGLE PER REO AND CRJ 900 SRM. NO LEAKS NOTESDR SWIA2020030549001Stringer Splice · corroded* CORROSION DETECTED ON STGR (19R) ON STRINGER "SPLICE" AT F.S. 477.40 JOINT STRAP, AROUND FASTENER BUCKTAILS (MARKED). (C-CHECK) RO 3/3/2020 REPLACED NEW PART (SH670-33264-1) REF. DWG AND CRJ 900 SRM. NO LEAKS NOTED.SDR SWIA2020030549000Stringer · corrodedCORROSION FOUND ON LH STRG 18 AT APROX FS 320.00 AROUND CANNON PLUG BRACKET (C-CHECK) RO 3/3/2020 REPAIREDSTRG 19 LH. REF CRJ-900 REO. NO LEAKS NOTED AT THIS TIMESDR SWIA2020030548999Stringer · corrodedCORROSION FOUND ON LH STRG 21 AT APROX FS 320.00 (C-CHECK) RO 3/3/2020 BLENDED, INSPECTED AND DETERMINED TO BE OUT OF LIMITS, 100% MATERIAL LOSS. REMOVED AND REPLACED AFFECTED STRINGER SECTION BETWEEN FS 334 AND FS 358 AND ADDED A STRINGER SPLICE AT APPROSDR SWIA2020030548998Stringer · corrodedFFOUND CORRODED AREAS ON LH STRG 19 FROM APROX FS 340.00 TO FS 360.00 (C-CHECK) RO 3/3/2020 DISCREPENCY SHOULD STATE L/H STR 20. REPAIRED L/H STR 20 BETWEEN FS 340.00 AND 360.00 REF REO AND CRJ 900 SRM.SDR ASAA2020030232315Stringer · corrodedCORROSION AT, AFT PIT, R/H FRAME C51, STRINGER 38 LATE FIND GROUNDED - YES. REMOVED CORROSION AND CHECKED THE LIMITS. ORIGINAL THICKNESS IS .095, REMAINING IS .083, .012 WAS REMOVED. FOUND TO BE OUT OF LIMITS REF A320 SRM 51-73-11 AND AIRBUS DWG E53470525 ISSDR SWIA2020021848657Stringer · corroded* STR 27 HAS CORROSION ON ATTACHMENT FLANGE FORWARD OF FS 533 FRAME (MARKED). (C-CHECK) RO 2/14/2020 BLENDED CORROSION ON ATTACHMENT FLANGE FWD OF FS533 FRAME, WITHIN LIMITS REF. REO FOR STR 27 LEAK CHECK GOOD.SDR FDEA202001160143Stringer · crackedCENTER UPPER AUXILIARY FUEL TANK STRINGER 46 FOUND CRACK FROM XCW 42.5 TO XCW 52.3. CENTER UPPER AUXILIARY FUEL TANK STRINGER 46 FROM XCW 42.5 TO XCW 52.3 CARRIED OUT REPAIR IAW EA # 1-5710-T0352202 PART 1 TITLE :" WINGS - BASIC WING STRUCTURE - CENTER SDR FDEA202001160148Stringer · crackedCENTER UPPER AUXILIARY FUEL TANK STRINGER 47 FOUND CRACK FROM XCW -14.2 TO XCW - 23 CENTER UPPER AUXILIARY FUEL TANK CRACKED STRINGER 47 FROM XCW -14.2 TO XCW -23 CARRIED OUT REPAIR AS PER SRM 57-10-03-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PESDR FDEA202001160147Stringer · crackedCENTER UPPER AUXILIARY FUEL TANK STRINGER 47 FOUND CRACK FROM XCW 14 TO XCW 23.8 CENTER UPPER AUXILIARY FUEL TANK CRACKED STRINGER 47 FROM XCW 14 TO XCW 23.8 CARRIED OUT REPAIR AS PER SRM 57-10-03-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM SDR FDEA202001160146Stringer · crackedCENTER UPPER AUXILIARY FUEL TANK STRINGER 47 FOUND CRACK FROM XCW 37.5 TO XCW 52 CENTER UPPER AUXILIARY FUEL TANK CRACKED STRINGER 47 FROM XCW 37.5 TO XCW 52 CARRIED OUR REPAIR AS PER SRM 57-10-03-2R FIGURE 201 REPAIR 1 . REPAIR CLASSIFIED AS MAJOR PER GMMSDR FDEA202001160145Stringer · crackedCENTER UPPER AUXILIARY FUEL TANK STRINGER 47 FOUND CRACK FROM XCW -39.4 TO XCW - 52.5. CENTER UPPER AUXILIARY FUEL TANK CRACKED STRINGER 47 FROM XCW -39.4 TO XCW -52.5 CARRIED OUT REPAIR AS PER SRM 57-10-03-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJSDR REXA2020012860077Stringer · corroded"INITIAL INSPECTION. CORROSION ON STRINGERS 26R AND 26L BTW FS 333-364 AT MAIN AVIONICS COMPARTMENT.(TCI 100-09).
"STRINGERS 26R AND 26L BTW FS 333-364 AT MAIN AVIONICS COMPARTMENT WERE REPLACED FOR A NEW ONES PER CRJ900 SRM 51-42-SDR REXA2020012860076Stringer · corroded"INITIAL INSPECTION. CORROSION ON STRINGER SPLICE 25R BTW FS 333 AT MAIN AVIONICS COMPARTMENT.(TCI 100-09).
"CORROSION ON STRINGER 25R BTW FS 280-333 AT MAIN AVIONICS COMPARTMENT WAS REPLACED FOR A NEW ONES PER CRJ900 SRM 5SDR REXA2020012816075Stringer · corroded"INITIAL INSPECTION. CORROSION ON STRINGER 25R BTW FS 280-333 AT MAIN AVIONICS COMPARTMENT.(TCI 100-09)."STRINGER 25R BTW FS 280-333 AT MAIN AVIONICS COMPARTMENT WAS REPLACED FOR A NEW ONES PER CRJ900 SRM 51-42-06-001-001-A01 AND SRM 51-42-20-001-001-A01 COSDR P5CA2020012200013Stringer · crackedBS 1702-1725 STRINGER 29L CRACKED. STRINGER REPAIRED IAW RI-53-80-13880 REV. ASDR ASAA2020022852292Stringer · corrodedAFT CARGO, STR.43 L/H HAS AREA OF CORROSION FROM FR. 56 TO FR.57 GROUNDED - YES. REMOVED CORROSION AND CHECKED THE LIMITS. ORIGINAL THICKNESS IS .110, .078 WAS REMOVED, REMAINING THICKNESS IS .032 FOUND TO BE OUT OF LIMITS REF A320 SRM 51-73-11. REPAIRED STR 4SDR FDEA2020011650136Longeron · crackedNOSE LANDING GEAR Ï¿½ WHILE CARRING OUT RIGHT HAND TRUNNION FITTING REPAIR FOUND LONGERON 49 RIGHT HAND CRACK AT STATION Y=595. NOSE LANDING GEAR RIGHT HAND TRUNNION FITTING AREA CRACK LONGERON 49 RIGHT HAND STATION Y=595. REMOVED AND REPLACED AS PER MD-11SDR FDEA2020011650135Longeron · crackedNOSE LANDING GEAR Ï¿½ WHILE CARRING OUT LEFT HAND TRUNNION FITTING REPAIR FOUND LONGERON 49 LEFT HAND CRACK AT STATION Y=595. NOSE LANDING GEAR LEFT HAND TRUNNION FITTING AREA CRACK LONGERON 49 LEFT HAND STATION Y=595 REMOVED AND REPLACED AS PER MD-11 SRM SDR IPXA2020013105588Longeron · crackedINSPECTION TYPE:2CMAIN CABIN LONGERON 15 L/H T ANGLE IS CRACKED ATS TA. 1219.REMOVED, FABRICATED AND FREPLACED T ANGLE IAW DWG. AEA7588 AND SRM 51-31-01. (MINOIR)SDR REXA2020012850092Stringer · corroded"AWR, HIDDEN DAMAGE [DURING PERFORMING OF NRC 00274]: CORROSION ON STGR 20R BTW FS310-319.70 WAS FOUND. (FUS).
""STRINGER 20RH BTW FS280 TO FS333 WAS REPLACED FOR A NEW ONE PER CRJ-900 SRM 51-42-20-001-001-A01 AND CRJ-900 SRM 51SDR REXA2020012850067Stringer Splice · corroded"AWR. IN REF EO R25120 AFTER INSULATION REMOVAL, CORROSION WAS FOUND ON STRIGER SPLICE R21, R22, R23- FS 333 AT MAIN AVIONICS COMPARTMENT.(TCI 100-09).
"STRINGER SPLICE R21, R22, R23- FS333 AT MAIN ASDR DALA2020011600324Longeron · damagedLONGERON 24LT DAMAGED AT STA 1295. SPLICED IN NEW SECTION REF MD88 SRM 53-02 FIG 18 SHEET 2. (LP1447541)SDR DALA2020011600323Stringer · corrodedAFT CARGO COMPARTMENT STRINGER 30, BETWEEN STA 948- 954 IS CORRODED. NRC 040-0008:5331-2001/004 00196: CORROSION LEVEL 1, SPLICED NEW SECTION OF LONGERON FROM STA 937-965 REF SRM 53-20-05-2R PROC 1.SDR DALA2020011600322Stringer · corrodedAFT CARGO COMPARTMENT STRINGER 30, STA 986 IS CORRODED. NRC 040-0008:5331-2001/001 00193: CORROSION LEVEL 1, SPLICED NEW SECTION OF LONGERON FROM STA 965-1012 REF SRM 53-20-05-2R PROC 1.SDR SWIA2020031049145Stringer · corroded*R/H STGR 19 HAS CORROSION AROUND FASTENER HOLE BETWEEN FS 437 TO FS 453. MARKED WITH RED GREASE PENCIL. (C-CHECK) RO 3/6/2020 REMOVED AND REPLACED R/H STGR 19 REF CRJ900 SRM AND DWG. PRESSURE LEAK CHECK SATISFACTORY.SDR SWIA2020031049143Stringer · corroded*R/H STGR 19 HAS CORROSION AROUND FASTENER HOLES BETWEEN FS 295 TO FS 310. MARKED WITH RED GREASE PENCIL. (C-CHECK) RO 3/6/2020 REPAIRED R/H STGR 19 FLANGE CORROSION REF REO. COMPLIED WITH PRESSURE CHECK NO LEAKS NOTED. SEE CONTINUATION CARD FOR ADDITIONALSDR SWIA2020031049139Stringer · corroded* STRINGER 19R HAS CORROSION BETWEEN FS 661.00 + 16 AND FS 661.00 + 32. (C-CHECK) RO 3/6/2020 REPAIRED CORROSION DAMAGE ON STRINGER 19R FS661+16-FS661+32 REF. CRJ 900 SRM. / TASK CARD COMPLIED WITH.SDR SWIA2020031049137Stringer Splice · corroded* STRINGER SPLICE AT FS 477.00 STGR 19R HAS CORROSION. (C-CHECK) RO 3/6/2020 REMOVED AND INSTALLED NEW STRINGER SPLICE JOINT ON STGR19R AT FS477.00. REF. CRJ900 SRM AND BOMBARDIER DWG. RESTORED FINISH TO AREA, PRESSURE LEAK CHECK GOOD REF CRJ 900 AMM, SEE SDR SWAA2020021041146Stringer · corrodedSTRUCTURE STRINGER CORRODED BETWEEN BS. 260 TO BS. 360, STR. 23L. / R&R STRINGER IAW SRM AND DWG.SDR IPXA2020013151604Longeron · crackedINSPECTION TYPE:2CMAIN CABIN LONGERON 15 L/H IS CRACKED AT STA. 1341.REMOVED, FABRICATED AND REPLACED T ANGLE IAW DWG. AEA7568-21 AND SRM 51-35-01. (MINOR)SDR AALA202001159022Stringer · crackedAIRCRAFT IN BASE MAINTENANCE: CRACKED STRINGER AT FR 100 AND S28L. REPAIRED STRINGER PER SRM 53-30-03 REPAIR 51P.SDR CALA2020011900148Stringer · cracked(B757-53-3-0556) STRINGER 16R IN MAIN CABIN IS CRACKED AT STA 780+24. REF NR 0084343. FOUND CRACK ON STRINGER 1.0" LONG, REMOVED, LOCATED AND INSTALLE D NEW STRINGER SECTION AT STA 780+24 TO 775 S16R IAW SRM 51-40-02 AND DWG 143N3500. WORK ACCOMPLISHED. NO FURSDR CALA2020011900147Stringer · cracked(B757-53-3-0556) STRINGER 16L IN MAIN CABIN IS CRACKED AT STA 780+24. REF NR 0084341. FOUND CRACK IN STRINGER 1.0" LONG, REMOVED, LOCATED AND INSTALLED NEW STRINGER SECTION AT FUS STA 780+24 TO 775 S-16L IAW SRM 51-40-02 AND DWG 143N3500. WORK ACCOMPLISHED. NOSDR ASAA2020022832297Stringer · corrodedAFT CARGO, STR.33 L/H HAS CORROSION IN MULTIPLE AREAS FROM FR.57 TO FR.64 GROUNDED - YES. REMOVED CORROSION ON STR 33LH FROMFR.57 TO FR.64 ORIG. THICKNESS .071, REMAINING .043, REMOVED .028 AND FOUND TO BE OUT OF LIMITS PER A320 SRM 51-73-11, REPAIRED STR 33 SDR ASAA2020022832296Stringer · corrodedAFT CARGO, STR. 35 L/H HAS CORROSION IN MULTIPLE AREAS FROM FR.54 TO FR.64 GROUNDED - YES. REMOVED DAMAGE ORIG. THICKNESS .110, REMAINING THICKNESS .080, REMOVED .030 AND IN TRANSITION AREA ORIG. THICKNESS .071, REMAINING THICKNESS .041, REMOVED .030 AND FOUNSDR ASAA2020022832295Stringer · corrodedAFT CARGO, STR 36 L/H HAS CORROSION IN MULTIPLE AREAS FROM FR.53 TO FR.62 GROUNDED - YES. REMOVED CORROSION ON STR 36LH FROM FR.53 TO FR.62 ORIG. THICKNESS .110 REMAINING .082, REMOVED .028 AND ORIG. THICKNESS .071 IN TRANSITION AREA, REMAINING .044, REMOVESDR ASAA2020022832294Stringer · corrodedAFT CARGO, STR 37 L/H HAS CORROSION IN MULTIPLE AREAS FROM FR.55 TO FR.64 GROUNDED - YES. REMOVED CORROSION ON STR 37 L/H FROM FR.55 TO FR.64 ORIG. THICKNESS .110 REMAINING .050, REMOVED .060 AND FOUND TO BE OUT OF LIMITS.PER A320 SRM 51-73-11, REPAIRED STR 3SDR ASAA2020022832293Stringer · corrodedAFT CARGO, STR. 38 L/H HAS CORROSION IN MULTIPLE AREAS FROM FR.56 TO FR61. GROUNDED - YES. REMOVED CORROSION ON STR 38 L/H FROM FR.56 TO FR.61 ORIG THICKNESS .110 REMAINING .034, REMOVED .076 AND FOUND TO BE OUT OF LIMITS PER A320 SRM 51-73-11, REPAIRED STR 38SDR ASAA2020022832291Stringer · corrodedAFT CARCO, STR.34 L/H HAS CORROSION IN MULTIPLE AREAS FROM FR. 53 TO FR.64 GROUNDED - YES. REMOVED CORROSION ON STR 34LH FROM FR.53 TO FR. 64 ORIG. THICKNESS .110, REMAINING THICKNESS .088, REMOVED .022 AND TRANSITION AREA ORIG. THICKNESS .071, REMAINING .048 SDR DALA2020011400241Stringer · corrodedSTRINGER 30 HAS THREE STRINGER FITTING WITH CORROSION BETWEEN FS 898 AND FS 1053. REPLACED STRINGER 30 BUT ONLY ONE SPLICE REQUIRED. INSTALLED STRINGER SPLICE FITTING BETWEEN FS 898-FS1053 IAW SRM 51-40. RII COMPLETE.SDR DALA2020011300238Stringer · corrodedSTRINGER 30 HAS MULTIPLE AREAS OF CORROSION BETWEEN FS 898 AND FS 1053. REPLACED STRINGER #30 IAW SRM 51-40. RII COMPLETE.SDR DALA2020011400240Stringer Splice · corrodedSTRINGER 29L HAS TWO CORRODED SPLICE FITTINGS LOCATED BETWEEN FS898 AND FS1053. REPLACED SPLICE FITTINGS PER SRM 51-41. INSTALLATION COMPLETE. RII COMPLETE.SDR DALA2020011300237Longeron · corrodedSTRINGER "LONGERON" 29L IS CORRODED FROM STA 1002 TO 898. REPLACED LONGERON 29L PER SRM 51-41. INSTALLATION FROM FS 898 TO FS 1053 COMPLETE. RII COMPLETE.
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