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 REXA2022100200811Stringer · corrodedSTRINGER 24R HEAVILY CORRODED ON ATTACHED FLANGE BETWEEN FS 333 TO 349. REMOVED AFT STGR 24R SECTION FROM FS 333 TO FS 385.50 FOR REPLACEMENT, IAW CRJ700 SRM 51-42-06-001-001-A01 & 51-42-21-001-001-A01. INSTALLED NEW SERVICEABLE STRINGER 24R SEGMENT, MADE FROMSDR FDEA202310011680Stringer · crackedUPPER AUXILIARY TANK - STRINGER 47 AT STATION XCW -17 FOUND CRACK DURING PERFORMING W/C 57.20.01.3. UPPER AUXILIARY TANK - STRINGER 47 AT STATION XCW -17 REPAIR CARRIED OUT AS PER MD-11 SRM 57-10-03-2R REPAIR 1 FIGURE 201. REPAIR CLASSIFIED AS MAJOR AS PERSDR FDEA202310011679Stringer · crackedUPPER AUXILIARY TANK - STRINGER 47 AT STATION XCW 17 FOUND CRACK DURING PERFORMING W/C 57.20.01.3. UPPER AUXILIARY TANK - STRINGER 47 AT STATION XCW 17 REPAIR CARRIED OUT AS PER MD-11 SRM 57-10-03-2R REPAIR 1 FIGURE 201. REPAIR CLASSIFIED AS MAJOR AS PER GSDR FDEA202310011678Stringer · crackedUPPER AUXILIARY TANK - STRINGER 47 AT STATION XCW 46.5 FOUND CRACK DURING PERFORMING W/C 57.20.01.3. UPPER AUXILIARY TANK - STRINGER 47 AT STATION XCW 46.5 REPAIR CARRIED OUT AS PER MD-11 SRM 57-10-03-2R REPAIR 1 FIGURE 201. REPAIR CLASSIFIED AS MAJOR AS PSDR VNAA202309300001Longeron · damagedMEL (MEL FAILURE) DRILLED THROUGH THE RADIUS ON THE UPPER LONGERON BETWEEN FS 645.00 - FS 661.00 STR18LSDR AALA202311083684Stringer · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON STRINGER IN BULK CARGO COMPARTMENT LOCATED AT FR 67 AND STR 44. REPAIRED STRINGER PER SRM 53-41-13-300-004.SDR DALA2023100308086Unknown · unknownCRACK ON CAP STA Y=1022RH LONGERON 7RH (INNER STRUCTURE) AT CPAX. SUMMARY OF NRC 00386: CAP STA Y=1022RH LONGERON 7RH INNER STRUCTURE WAS REPAIRED PER ER/A 611872-14 REV ORIGINAL SECTION I PERMANENT REPAIR. ASSOCIATED ER/A 14-611872 ADDED FOR AC 9520. (LP #299SDR REXA2024110601436Stringer · corrodedSTRINGER 26R CORRODED AROUND 4 FASTENERS BETWEEN FS 265.00 TO FS 280.00 REPAIRED STGR 26R P/N CC670-33150-2 IAW MHIRJ EO CL-600-2D24-53-L07599 REV. IR DATED 10-17-2023.SDR SWAA2023110105384Stringer · crackedCRACK STRINGER 26L LOCATED BS 540 FWD CARGO COMPARTMENT 2023-614914<[01] TOOL USED UT EQUIPMENT P/N: 45MG; S/N: 221860711; CAL DUE DATE: 07-NOV-23;[02] TOOL USED: EDDY CURRENT FLAW DETECTOR; P/N: NORTEC 600D; S/N: 220273012; DUE DATE: 17-DEC-23;[03] TOOLS USEDSDR SWAA2023110105386Stringer · crackedCRACK STRINGER 25L LOCATED BS 540 AT FWD CARGO COMPARTMENT 2023-614915<[01] TOOL USED UT EQUIPMENT P/N: 45MG; S/N: 221860711; CAL DUE DATE: 07-NOV-23;[02] TOOL USED: EDDY CURRENT FLAW DETECTOR; P/N: NORTEC 600D; S/N: 220273012; DUE DATE: 17-DEC-23;[03] TOOLS USDR SWAA2023110105385Stringer · crackedCRACK STRINGER 23R LOCATED BS 540 FWD CARGO COMPARTMENT 2023-614908<[01] TOOL USED UT EQUIPMENT P/N: 45MG; S/N: 221860711; CAL DUE DATE: 07-NOV-23;[02] TOOL USED: EDDY CURRENT FLAW DETECTOR; P/N: NORTEC 600D; S/N: 220273012; DUE DATE: 17-DEC-23;[03] TOOLS USEDSDR SWAA2023110105387Stringer · crackedCRACK STRINGER 23L LOCATED BS 540 FWD CARGO COMPARTMENT 2023-614909<[01] TOOL USED: EDDY CURRENT FLAW DETECTOR; P/N: NORTEC 600D; S/N: 220273012; DUE DATE: 17-DEC-23;[02] TOOLS USED: TEMPERATURE CONTROLLER: P/N P3015GOES00000; S/N 142811020; DUE DATE: 25-JAN-2SDR CALA2023100602946Stringer · corrodedAFT CARGO FR 60-62 R/H STR 42 AND CORRESPONDING SKIN MULTIPLE SPOTS OF FITTINGS (A3NB-53-4-6179). . REMOVED AND REPLACED STRINGER 42RH AT FR 59 TO FR 64 IAW A319 SR M 51-72-11 PAR 2.SDR DALA2023100208058Unknown · unknown(LOG 2991646) AFT BULKHEAD @ STA 1042 STRINGER 18L CLIP HAS CORROSION. REMOVED, FABRICATED AND INSTALLED NEW STRINGER END CLIP IAW DWG 148A3451-25 REV B, BOEING DWG 148A3451 REV -, BOEING DWG 148A0933 REV -, B737 SRM 51-40-05 AND B737 SRM 51-40-02.SDR AALA202309294000Stringer · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT STRINGER BETWEEN FR 65 AND FR 66 AT S31R. REPLACED STRINGER PER SRM 51-42-11.SDR R61A2023092800541Stringer · corrodedWHILE IN HEAVY CHECK - CORROSION ON STRINGER 19L BETWEEN FR 83 AND FR 84. REPAIRED STGR 19L BETWEEN FR 82-90. REF ETD20223-170-022854.SDR R61A2023092800540Stringer · corrodedWHILE IN HEAVY CHECK - CORROSION ON STRINGER 21L BETWEEN FR 88-89. REMOVED AND REPLACED STGR 21L BETWEEN FR88-90. REF ETD2023-170-022855.SDR R61A2023092800539Stringer · corrodedWHILE IN HEAVY CHECK - CORROSION ON STRINGER 19R BETWEEN FR 88-89 BELOW GALLEY HOSE. PERFORMED PERMANENT REPAIR BY CUTOUT AND FILLER SPLICE ON STRINGER 19R BETWEEN FR 88-89 IN ACCORDANCE WITH, REF ETD2023-170-022828.SDR R61A2023092800538Stringer · corrodedWHILE IN HEAVY CHECK - CORROSION ON STRINGER 21L BETWEEN FR 78-79. PERFORMED SPLICE REPAIR TO STGR 21L BETWEEN FR 78-79 REFER ETD2023-170-022835SDR R61A2023092800537Stringer · corrodedWHILE IN HEAVY CHECK - CORROSION ON STRINGER 23L BETWEEN FR 75-76 AND BETWEEN FR84-85. PERFORMED SPLICE REPAIR TO STGR 23L BETWEEN FR75-76 AND FR84-85 IAW ETD2023-170-002836.SDR R61A2023092800536Unknown · gougedWHILE IN HEAVY CHECK - MAIN CABIN STRINGER CHAFFED NEAR FORWARD SERVICE DOOR AT FR 17-18 STGR 9R. REPLACED FILLER AT FR17-18 STGR 9R IAW ETD2016-170-025213-ASDR REXA2022110800961Stringer · corrodedSTGR 26R IS CORRODED BETWEEN FS 349 AND FS 364 REMOVED AND REPLACED STRG 26R BETWEEN FS 349.00 AND FS 364.00 IAW CRJ900 IAW 51-42-06-001-001-A01,51-40-11-001-001-A01. AND SRM 51-42-21-001-001-A01. P/N INSTALLED IS SH670-31372-4SSDR SWAA2023102305590Stringer · separatedINSPECTION OF BS 727 INNER CHORD AT STRINGER 18A RIGHT SIDE HAS .008 GAP BETWEEN STRINGER AND CHORD AS MEASURED DURING 5311-I-14624-NG STEPS 8 & 9<[01] CORRECTED EXCESSIVE GAP WITH COMPLETION OF EO 5311-E-14625-NG.;[02] CORRECTED EXCESSIVE GAP WITH COMPLETION SDR SWAA2023102305589Stringer · separatedBS 727 INNER CHORD AT STRINGER 18A LEFT SIDE HAS .008 INCH GAP AS MEASURED DURING 5311-I-14576-NG STEP 9<[01] CORRECTED EXCESSIVE GAP WITH COMPLETION OF EO 5311-E-14577-NG.;[02] CORRECTED EXCESSIVE GAP WITH COMPLETION OF EO 5311-E-14577-NG.SDR ASAA2023092546608Stringer · corrodedAFT WET AREA LH SIDE STR 30 AT FR65 TO FR67 HAS CORROSION GROUNDED - YES. NO LIMITS FOUND FOR AREA .ANNEALED MATERIAL DAN50B08 PO 1069688.1 IAW A320 SRM 51-25-00FORMED IAW A320 SRM 51-25-00 AND AIRBUS DWG # D53480505.HEAT TREATED IAW A320 SRM 51-25-00.LOSDR SWI2023F00497Unknown · crackedFOUND CRACK NEAR STRINGER 2LH POSITION ABOVE FLOOR NEAR FS 330 BY THE PASSENGER DOOR (MARKED RED) (C-CHECK RO 11/20/2023) CRACK IS ON FRAME FS 333 BETWEEN STR 1R AND STR 2R. REPAIRED FRAME FS333 BETWEEN STR 1R AND STR 2R CUT OUT CRACK AND INSTALLED REPAIR SDR SWAA2023092604059Stringer · crackedEVIDENCE OF CRACK COMING FROM VERY FWD FASTENER OF STR 16R, BS 993. REMOVED FASTENER WERE SUSPECTED CRACK IS AND 12 FASTENTERS AFT IAW SRM 51-40-02. VERIFIED 13 TOTAL FASTENERS REMOVED. ACCOMPLISHED HFEC INSPECTION OF STRINGER BETWEEN FWD FASTENER HOLE AND FSDR REXA2022100200794Stringer · corrodedSTGR 24L IS CORRODED BETWEEN FS 485 AND FS 517. REMOVED DAMAGE STR24L BETWEEN FS469 THRU FS533 IAW CRJ700 SRM 51-42-06-001-001-A01. AND INSTALLED NEW SERVICEABLE STRINGER 24 L/H WITH P/N SH670-33227-1S BETWEEN FS469 AND FS533 IAW CRJ700 SRM 51-42-06-001-001-ASDR DALA2023092507856Unknown · unknownCORROSION ON LONGERON 30 BTW STA 909 TO STA 912, STA 921 TO STA 922, STA 962 TO STA 968, STA 998 TO STA 1000, LONGERON 29L STA 910 TO STA 912, STA 940 TO STA 950, STA 952 TO STA 955, AND LONGERON 29R STA 924 TO STA 928, STA 1005 TO STA 1006 AT AFT CARGO COMPARSDR P5CA2023083000091Unknown · unknownAPU BATTERY COMPT STA 2598 - STA 2618 STR 42R FOUND CRACK(<P>CRACK STRINGER REPLACED AS PER RI #RI-53-80-16468 REV A. NO FURTHER DEFECTS NOTED</P>)SDR FDEA202309221634Stringer Splice · crackedCOMPLY WITH EO 6-5310-7-5023 A PT2. REPLACED THE CRACKED SPLICE AT THE JUNCTION AT STGR18RH - FR47. TITLE: FUSELAGE - CENTER SECTION - INSPECTION OF STRINGER 18 LH/RH AT FRAME47, AIRBUS SB A300-53-6157 COMPLIED WITH EO 6-5310-7-5023 A PT2. TITLE: FUSELAGE SDR IPXA2023103133051Stringer · corrodedMAJOR REPAIR, AFT CARGO PIT - STRINGER 26 LH BETWEEN STA 1570 AND 1620 IS CORRODED. REPAIRED IAW --1) REMOVE S-26L DAMAGED STRINGER SECTION (P/N: 146N3110-479) BETWEEN STA 1500-1520 (FAULT T3F18E002EKMP) AND STA 1560-1620 (FAULT T3F18E002EKMQ) RESPECTIVELY. 2)SDR IPXA2023100633051Unknown · unknown*** SDR FILED OPEN *** FAULT: AFT CARGO PIT - STRINGER 26 LH BETWEEN STA 1570 AND 1620 IS CORRODED. OK TO INSTALL SPLICE, SPLICE FRAME, WEB, TIE DOWN BRACKET, STRINGER CLIP 5EA, SHEAR TIE (4EA), SHEAR TIE (2EA).SDR IPXA2023100633060Stringer · corroded*** MAJOR REPAIR *** FAULT: AFT CARGO PIT - STRINGER 26 LH AT STA 1510 IS CORRODED. JOB COMPLETESDR FDEA202309211632Longeron · crackedEXISTING REPAIR ON LONGERON 48 LEFT STATION 5-85 FOUND WITH APPROXIMATE 2-INCH CRACK ON THE OUTBOARD REPAIR ANGLE. EXISTING REPAIR AT CENTER CARGO COMPARTMENT ON LONGERON 48 LEFT STATION 5-85 FOUND WITH APPROXIMATE 2-INCH CRACK ON THE OUTBOARD REPAIR ANGLESDR SWAA2023102402660Stringer · crackedAREA AFT OF FWD CARGO BAY HAS A CRACKED STR; STR R25; BS 520+19<[01] REMOVED AND REINSTALLED AND PERFORMED GOOD OPERATIONAL TEST OF RETRACTABLE LANDING LIGHT ASSEMBLY. IAW AMM 33-42-02-960-802.;[02] CERTIFIED ACTION 1.;[03] COMPLETED STEPS 6 AND 10;[04] CERTIFSDR SWAA2023101202736Stringer · crackedCRACKED STRINGER AT AREA AFT OF FCB BS535 S-24R WL162. MARKED<[01] ACCOMPLISHED HFEC SURFACE SCAN OF CUT EDGE IAW 737 NDTM PART 6 CHAPTER 51-00-00 PROCEDURE 23. NO CRACKS NOTED.<BR><BR>EQUIPMENT USED: NORTEC 600 ID: ATS2353 CAL DUE: 01/2024SDR SWAA2023101202735Stringer · crackedCRACKED STRINGER AT AREA AFT OF FCB BS535 S-25R WL155. MARKED<[01] REPAIRED AS PER EA 23-153-02879.;[02] VERIFIED.SDR REXA2022092600773Stringer Splice · corrodedSTGR 25L SPLICE IS CORRODED AT FS 477. REMOVED STRINGER SPLICE AT STGR 25L AND FS 477. IAW CRJ700 SRM 51-42-06-001-001-A01. INSTALLED NEW SPLICE STRINGER AT STGR 25L AND FS 477. IAW CRJ700 SRM 51-42-06-001-001-A01.SDR REXA2022101100851Stringer · corrodedSTGR 25R IS CORRODED BETWEEN FS 310 AND FS 333 REMOVED AND REPLACED STRINGER 25R P/N SH670-31212-2U IAW CRJ-900-SRM-51-42-06-001-001-A01 AND 51-42-21-001-001-A01SDR REXA2024103001237Stringer · corrodedSTGR 22L IS CORRODED BETWEEN F.S. 349 TO F.S. 364. REPAIRED STGR 22L BETWEEN F.S. 349 TO F.S. 364 IAW ENDEAVOR AIR EA CRJ953-15538 REV IR DATED 10/05/2023,SDR REXA2024021600196Stringer · corrodedSTGR 26R IS CORRODED BETWEEN F.S. 295 TO F.S. 310. REPLACED AND INSTALLED NEW SERVICEABLE STGR 26R P/N SH670-31634-2S AT FS 280 TO 333 IAW CRJ900 51-42-06-001-001-A01SDR REXA2022111300968Stringer · corrodedSTGR 22R IS CORRODED BETWEEN F.S. 280 TO F.S. 310. LOCATED AND DRILLED STGR 22R P/N SH670-31210-2U FROM FS 280-333 IAW CRJ 900 SRM 51-40-11-001-001-A01. INSTALLED NEW STRINGER 22R, P/N SH670-31210-2U, AT FS 280 TO FS 333 IAW CRJ900 SRM 51-42-06-001-001-A01SDR SWAA2023101602006Stringer · crackedCRACK STRINGER 19R LOC BTW BS500C TO BS500D AT FWD CARGO COMPARTMENT 2023-569785<[01] TOOL USED UT EQUIPMENT P/N: 45MG; S/N: 221860711; CAL DUE DATE: 07-NOV-23;[02] REPAIRED STRINGER 19R LOC BTW BS500C TO BS500D AT FWD CARGO COMPARTMENT SRM 53-00-03-2R-1 REPAISDR DALA2023092207804Unknown · unknownSHIP 177 STRINGER 35RT. IS CORRODED HEAVILY FS 742-764. CORRECTIVE ACTION: REPAIRED FUSELAGE STRINGER REF: B767-300 SRM 53-00 (2976373)SDR DALA2023091907685Unknown · unknownCRACK ON LONGERON 6RH STA Y=1022RH (INNER STRUCTURE) AT CPAX. SUMMARY OF NRC 00385: LONGERON ON 6RH STA Y=1022RH (INNER STRUCTURE) AT CPAX WAS REPAIRED PER B717-200 SRM 53-00-05-2R PROCEDURE 2. (LP #2976393)SDR REXA2024100100755Stringer · corrodedSTRINGER 19 R IS CORRODED BETWEEN F.S. 295 TO F.S. 310. LOCATED AND DRILLED NEW STR19 P/N SH670-31632-1, BETWEEN FS 280 TO FS 319 IAW CRJ-900 SRM 51-40-11-001-001-A01.INSTALLED NEW NEW STR19 P/N SH670-31632-1, BETWEEN FS 280 TO FS 319 IAW CRJ-900 SRM 51-42-06SDR REXA2024100100753Stringer · corrodedSTGR 18R IS CORRODED F.S. 280 TO F.S. 310. LOCATED AND DRILLED NEW STR18R P/N SH670-31631-1 BETWEEN FS 280 AND FS 310, IAW CRJ-900 SRM 51-40-11-001-001-A01. INSTALLED NEW STR18R P/N SH670-31631-1 BETWEEN FS280 TO FS 310 IAW. CRJ-900 SRM 51-42-06-001-001-A01 ANSDR REXA2022120401014Stringer · corrodedSTGR 22R IS CORRODED BETWEEN F.S. 310 TO F.S. 349. LOCATED AND DRILLED STGR 22R P/N SH670-31379-1S FROM FS 333-349 IAW CRJ 900 SRM 51-40-11-001-001-A01. INSTALLED NEW STGR 22R, P/N SH670-31379-1S, FROM FS333-349 IAW CRJ 900 SRM 51-42-06-001-001-A01 AND 51SDR REXA2022110100943Stringer · corrodedSTRINGER 25L CORRODED BETWEEN FS333 - FS364. REPAIRED STGR 25L FROM F.S.333 TO F.S.349 IAW ENDEAVOR AIR EA CRJ953-15452 REV IR DATED 9/15/2023.
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