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 SWIA202266849None · corrodedLH INTERCOSTAL FS 310 TO 319 STGR 21 HAS CORROSION (C-CHECK RO 11/10/2022) REPLACED STR 21L INTERCOSTAL FS310.00 TO FS333.00 REF. CRJ 200 SRM 51-42-06 AND CRJ 200 SRM 51-42-21 AND DWG 601R31527 REV AM". COMPLIED WITH 51-900-1003-SKYSDR SWIA202266799None · corrodedLH INTERCOSTAL FS 333 TO 349 STGR 21 HAS CORROSION (C-CHECK RO 11/10/2022) REMOVED AND REPLACED LH INTERCOSTAL FS 333 TO 349 STGR 21 P/N: 691R31527-19 REF DWG. 601R31527 REV. AM, CRJ-200 SRM 51-21-16, SRM 51-42-06 AND SRM 51-42-21. COMPLIED WITH 51-900SDR FDEA202209022144Longeron · corrodedREFERENCE SNRM NUMBER N01369, AFTER ADDITIONAL REMOVAL FOUND LONGERON NUMBER 49 LEFT CORRODED BETWEEN STATION 535 TO STATION 575. STATION 535 TO STATION 575 LONGERON NUMBER 49 LEFT CORROSION REMOVED AND FOUND EXCEEDED LIMIT AS PER SRM 53-00-00-2R FIGURE 20SDR FDEA202209022143Longeron Splice · crackedAFT CARGO - RIGHT HAND TUNNEL STATION 1863.125 - STATION 1871 LONGERON 38 RIGHT SPLICE FOUND CRACKED AFT CARGO - RIGHT HAND TUNNEL STATION 1863.125 - STATION 1871 LONGERON 38 RIGHT CRACKED SPLICE REMOVED AND REPLACED WITH FABRICATED MACHINED SPLICE AS PER SDR DALA2022090205921None · none(LOG 2390458) DURING INSPECTION FOUND CORROSION ON RH SIDE PLATE-SUPPORT ZEE AT RBL 21.00 AND BTWN STA 727/STA 767 OF AFT CARGO COMPARTMENT. RH SIDE PLATE-SUPPORT ZEE AT RBL 21.00 AND BTWN STA 727/STA 767 OF AFT CARGO COMPARTMENT WAS REPLACED PER B737-900ER SRSDR 2022FA0000489Landing Gear · crackedSTRINGER CLIP CRACKED STA 460, S-25LSDR R61A2022083100533Stringer · corrodedWHILE IN HEAVY CHECK - STGR 21R INTERNAL SIDE HAS CORROSION AS MARKED FR 83-84. REMOVED DAMAGED SECTION STGR 21R
FR81/86 AND REPAIRED WITH FILLER SECTION AND SPLICES BETWEEN FR81 AND FR 86 REF. ETD2022-170-025869.SDR R61A2022083100532Stringer · corrodedWHILE IN HEAVY CHECK - STGR 20R INTERNAL SIDE HAS CORROSION AS MARKED FR 83-84. REMOVED AND REPLACED STRINGER 20R FROM FRAME 80 TO FRAME 89 REF SRM 51-40-02.SDR R61A2022083100531Stringer · corrodedWHILE IN HEAVY CHECK - STGR 19R INTERNAL SIDE HAS CORROSION AS MARKED FR 83-84. REMOVED DAMAGED SECTION OF STRINGER 19R FR 83/84. INSTALLED. REPAIR FILLER SECTION AND SPLICES FR 83/84 REF ETD2022-170-025853SDR R61A2022083100530Stringer · corrodedWHILE IN HEAVY CHECK - STGR 19L INTERNAL SIDE HAS CORROSION AS MARKED FR 83-84. PERFORMED STRINGER SPLICE REPAIR ON STRINGER
19L BETWEEN FR 82/83 TO FR 86/87. REF EMB ETD2022-170-025842.SDR ASAA2022083040114Stringer · corrodedSTGR 23L SECTION BETWEEN 312-344 CORRODED SEVERAL AREAS. GROUNDED - YES. REMOVED AND REPLACED STR-23L BETWEEN STA 270 TO STA 360 IAW B737-700 SRM 51-40-02-0G-0W=.90 O=.09 R=.00 L=4.0" D=.090.SDR IPXA2022092086458Stringer · corrodedINSPECTION TYPE:SEG1, STR 28R HAS CORROSION ON THE BOTTOM SURFACE OF STRINGER APPROX. 6 INCHES LONG. LOCATED AT THE FACTORY SPLICE FWD OF STA 1460.ACCOMPLISHED REPAIR PER SRM 53-00-03-2R-1 DETAIL IV AND RCD 284546.SDR LR7A2022083003195Longeron · crackedDURING SCHEDULED B-1 CHECK UNDER JOB CARD HB5305, FOUND THE LONGERON ABOVE THE CREW DOOR CRACKED AT FS212, LBL65, WL195. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. NR# 1000806177. / PSE# 53-30-12, AD 2012-06-09SDR FDEA202208292096Longeron · crackedREFERENCE SPECIAL/NONROUTINE MAINTENANCE FORM N00314, TO INSPECT STATION 595 BULKHEAD FOUND FUSELAGE NO.1 AIRCON BAY AFT BULKHEAD STATION 595 APPROXIMATE LONGERON NO.42 SUSPECTED CRACK. FUSELAGE STATION 595 BULKHEAD NO.1 AIRCON BAY CRACKED AT DOUBLER AND SDR R61A2022092000557Stringer · corrodedDURING HEAVY MAINTENANCE CHECK FOUND CENTER FUSELAGE III, STRG 28R CORRODED BETWEEN FR88 AND FR89. CARRIED OUT REPAIR TO STR 28R FROM FR86 TO FR90 IAW EMBRAER 170/175 SRM 53-23-03 REPAIR 06.SDR YENA2022083000835Stringer · corrodedDURING HEAVY MAINTENANCE: CORROSION STRINGER 43L LOCATED BTW FRAME 56 AND FRAME 57 IN AFT CARGO COMPARTMENT (CPCP RELATED MPD TASK 534107-01); REMOVED AND REPLACEDSTRINGER 43L AND FASTENERS LOCATED BTW FRAME 54AND FRAME 60 IN AFT CARGO COMPARTMENT AS PER A320SDR DALA2022082905776Unknown · unknown(LOG 2381094) DURING INSPECTION FOUND CORROSION ON RH SHIELD AT RBL 21.00 AND BTWN STA 767/STA 787 OF AFT CARGO COMPARTMENT. RH SHIELD AT RBL 21.00 AND BETWEEN STA 767/STA 787 OF AFT CARGO COMPARTMENT WAS FABRICATED PER DWG 146A8127-12 REV: A AND INSTALLED PERSDR CALA2022082402154Stringer · corrodedCORROSION FOUND ON STRINGER 26 RIGHT . DIRECTLY AFT OF FRAME 70. CORROSION LOCATION IS FRAME 67-STRINGER 27 PER SRM ENGINEERING UPDATE, IT IS STRG 26R 53-41-13-50-A. REMOVED STRINGER 26 RIGHT . DIRECTLY AFT OF FRAME 70.AND ASSOCIATED FASTNER FWD OF F.S 70 STR SDR SWAA2022091244999Stringer · crackedCRACK STRINGER 23L LOCATED BS 540 AT FWD CARGO COMPARTMENT 2022-447706 / [01] TOOL USED EDDY CURRENT EQUIPMENT PN: NORTEC 600D; SN:60009161631; DUE DATE: 03-DEC-22;[02] TOOL USED: TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 112031023; DUE DATE: 01-FEB-23SDR CALA2022082402168Stringer · corroded(SUPPORT TASK) AFT CARGO FR56 TO FR58 STRINGER 37R CORRODED.(REP LACE P/N: D5347552623000) REMOVED AND REPLACED STRINGER IAW SRM 51-42-11, DWG D53475580. E MP# V935774 WORK ACCOMPLISHED AT ST ENGINEERING AEROSPACE OF MOB ILE AT BFM ON NR# 34925.SDR SWIA202266565None · corrodedFOUND PAX DOOR INTERCOSTAL DD6 AFT SIDE TO BE CORRODED. (C-CHECK RO 9/28/2022) REMOVED AND REPLACED PA.X DOOR INTERCOSTAL DD6 IAW CRJ200 SRM 51-42-06. FORM 337 AND MAJOR REPAIR TASK CARD 51-900-1003-SKY COMPLETED AND ATTACHED. NO WEIGHT CHANGE. SEE CSDR SWAA2022092744364Stringer · crackedCRACK STRINGER 7L AND BS294.5 AT PASSENGER CABIN 2022-441287 / [01] TOOL USED: TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 112031023; DUE DATE: 01-FEB-23; TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 112820025; DUE DATE: 01-FEB-23;[02] TOOL USED: ETSDR SWAA2022092777339Stringer · crackedCRACK STRINGER 15L AND BS294.5 AT PASSENGER CABIN 2022-441290 / [01] TOOL USED: ET EQUIPMENT P/N: NORTEC 600D; S/N: 60009161631; CAL DUE DATE: 03-DEC-22;[02] PERFORMED REPAIR ON STRINGER 15L AND BS294.5 AT PASSENGER CABIN IAW B737-700 SRM 53-00-03-2R-1 REPAIR SDR SWAA2022092744365Stringer · crackedCRACK STRINGER 16L AND BS294.5 AT PASSENGER CABIN 2022-441292 / [01] TOOL USED: ET EQUIPMENT P/N: NORTEC 600D; S/N: 60009161631; CAL DUE DATE: 03-DEC-22;[02] PERFORMED REPAIR ON STRINGER 16L LOCATED BS 294.5 AT PASSENGER CABIN IAW B737-700 SRM 53-00-03-2R-1; RSDR SWAA2022092744355Tie Clip · crackedCRACK TIE CLIP LOCATED BS277 AND STR10R AT PASSENGER CABIN 2022-441286 / [01] REPLACED TIE CLIP LOCATED BS277 AND STR10R AT PASSENGER CABIN IAW B737-700 SRM 51-10-02 ITEM 9 AND DWG 141A1110 SHEET 18 REV -. SEE INDIVIDUAL SIGN OFFS BELOW;[02] CERTIFIED RII WORKSDR AALA202209228580Stringer · damagedAIRCRAFT IN BASE MAINTENANCE: STRINGER SPLICE PART NUMBER 69-78188-31 REQUIRES FABRICATION FOR STRINGER REPAIR. FABRICATED 2EA SECTIONS OF PART NUMBER 69-78188-31 PER BAC DRAWING NUMBER 69-78188 REVISION C.SDR AALA202209212621Stringer · damagedAIRCRAFT IN BASE MAINTENANCE: STRINGER SPLICE PART NUMBER 69-78188-30 REQUIRES FABRICATION FOR STRINGER REPAIR. FABRICATED 2EA, SECTIONS OF PART NUMBER 69-78188-30 PER DRAWING NUMBER 69-78188, REVISION C.SDR DALA2022082405716None · none(LOG 2374341) DURING INSPECTION FOUND CORROSION SEVERAL PLACES ON SIDE PLATE LH SIDE UPPER AND LOWER FACE BTW STA= 500I TO 500D AT FWD CARGO COMPARTMENT C-1. SIDE PLATE LH SIDE BTW STA= 500I TO 500A AT FWD CARGO COMPARTMENT WAS REPAIRED PER B737-800 SRM 53-00-SDR SWIA202266564None · corrodedAVI DOOR INTERCOSTAL FROM F.S. 349.00 TO F.S. 364.00 BETWEEN STGR 27R AND STGR 26R IS CORRODED (C-CHECK RO 9/28/2022) INSTALLED NEW SERVICEABLE INTERCOSTAL IAW CRJ 200 SRM 51-42-06 & CRJ 200 SRM 51-42-21.COMPLETED SKY CARD 51-900-1003-SKY AND COMPLETED SDR DALA2022081905653None · noneAIRCRAFT 176, AFT CGO STRUCTURE SHEAR TIE CORROSION AT STA 1219 S38L-S39L REF TO CPCP 53-558-00. CORRECTIVE ACTION: THE CORROSION REMOVED AND THE REWORKED AREA MEASURED. THE ORIGINAL THICKNESS T=0.063". THE REMAINING THICKNESS IS 0.051". THE DEPTH OF CLEANUP ISDR DALA2022081905652None · noneAIRCRAFT 176, AFT CGO STRUCTURE SHEAR TIE CORROSION AT STA 1197+88 S36R-S37R REF TO CPCP 53-558-00. CORRECTIVE ACTION: THE CORROSION REMOVED AND THE REWORKED AREA MEASURED. THE ORIGINAL THICKNESS T=0.056". THE REMAINING THICKNESS IS 0.030". THE DEPTH OF CLEANUSDR DALA2022081905637Intercostal · corroded(LOG 2371654) DURING INSPECTION FOUND CORROSION ON INTERCOSTAL BTW STA 847-867 BTW S-25L TO S-26L AT AFT CARGO COMPARTMENT. INTERCOSTAL BTW STA 847-867 BTW S-25L TO S-26L AT AFT CARGO COMPARTMENT WAS REPLACED PER DWG 149A8109 REV.B AND B737-800 SRM 51-40-02-0GSDR FDEA202208192006Longeron · corrodedCTR CARGO COMPT STA 1601 LONG 51L HAS EXFOLIATION (LOOK UNDER/MARKED) REPAIRED PER SRM 53-00-05-2RSDR DALA2022081905650None · noneAIRCRAFT 176, AFT CGO STRUCTURE SHEAR TIE CORROSION AT STA 1307 S38L-S39L REF TO CPCP 53-558-00. CORRECTIVE ACTION: THE CORROSION REMOVED AND THE REWORKED AREA MEASURED. THE ORIGINAL THICKNESS T=0.050". THE REMAINING THICKNESS IS 0.030". THE DEPTH OF CLEANUP ISDR DALA2022081905649None · noneAIRCRAFT 176, AFT CGO STRUCTURE SHEAR TIE CORROSION AT STA 1197+132 S37R-S38R REF TO CPCP 53-558-00. CORRECTIVE ACTION: THE CORROSION REMOVED AND THE REWORKED AREA MEASURED. THE ORIGINAL THICKNESS T=0.050". THE REMAINING THICKNESS IS 0.032". THE DEPTH OF CLEANSDR DALA2022081905648None · noneAIRCRAFT 176, AFT CGO STRUCTURE SHEAR TIE CORROSION AT STA 1329 S38L-S39L REF TO CPCP 53-558-00. CORRECTIVE ACTION: THE CORROSION REMOVED AND THE REWORKED AREA MEASURED. THE ORIGINAL THICKNESS T=0.045". THE REMAINING THICKNESS IS 0.023". THE DEPTH OF CLEANUP ISDR DALA2022081905647None · noneAIRCRAFT 176, AFT CGO STRUCTURE SHEAR TIE CORROSION AT STA 1197+66 S37L-S38L REF TO CPCP 53-558-00. CORRECTIVE ACTION: ORROSION REMOVED AND THE REWORKED AREA MEASURED. THE ORIGINAL THICKNESS T=0.050". THE REMAINING THICKNESS IS 0.033". THE DEPTH OF CLEANUP IS SDR DALA2022081905646None · noneAIRCRAFT 176, AFT CGO STRUCTURE SHEAR TIE CORROSION AT STA 1307 S37L-S38L REF TO CPCP 53-558-00. CORRECTIVE ACTION: THE CORROSION REMOVED AND THE REWORKED AREA MEASURED. THE ORIGINAL THICKNESS T=0.040". THE REMAINING THICKNESS IS 0.019". THE DEPTH OF CLEANUP ISDR DALA2022081905645None · noneAIRCRAFT 176, AFT CGO STRUCTURE SHEAR TIE CORROSION AT STA 1175 S35R-S36R REF TO CPCP 53-558-00. CORRECTIVE ACTION: THE CORROSION REMOVED AND THE REWORKED AREA MEASURED. THE ORIGINAL THICKNESS T=0.063". THE REMAINING THICKNESS IS 0.042". THE DEPTH OF CLEANUP ISDR DALA2022081905644None · noneAIRCRAFT 176, AFT CGO STRUCTURE SHEAR TIE CORROSION AT STA 1219 S35R-S36R REF TO CPCP 53-558-00. CORRECTIVE ACTION: THE CORROSION REMOVED AND THE REWORKED AREA MEASURED. THE ORIGINAL THICKNESS T=0.063". THE REMAINING THICKNESS IS 0.052". THE DEPTH OF CLEANUP ISDR DALA2022081905643None · noneAIRCRAFT 173, AFT CGO STRUCTURE SHEAR TIE CORROSION AT STA 1285 S39L-S39R REF TO CPCP 53-558-00. CORRECTIVE ACTION: THE CORROSION REMOVED AND THE REWORKED AREA MEASURED. THE ORIGINAL THICKNESS T=0.040". THE REMAINING THICKNESS IS 0.021". THE DEPTH OF CLEANUP ISDR DALA2022081905642None · noneAIRCRAFT 176, AFT CGO STRUCTURE SHEAR TIE CORROSION AT STA 1197+110 S37R-S38R REF TO CPCP 53-558-00. CORRECTIVE ACTION: THE CORROSION REMOVED AND THE REWORKED AREA MEASURED. THE ORIGINAL THICKNESS T=0.050". THE REMAINING THICKNESS IS 0.032". THE DEPTH OF CLEANSDR SWAA2022092242808Bear Strap · crackedFORWARD GALLEY DOOR BEAR STRAP HAS A 2 INCH LONG CRACK 3 INCHES BELOW STRINGER 8R / [01] REPAIRED BY 737-700 SRM 53-10-01-2R-6 AND EA M-21-153-03542;[02] UPDATED MEASUREMENT TABLE;[03] VERIFIED MEASUREMENT TABLE COMPLETED.;[04] VERIFIED CORRECTIVE ACTION ITEM SDR SWIA202266559None · corrodedFOUND PAX DOOR INTERCOSTAL DD1 AFT TO BE CORRODED. (C-CHECK RO 9/28/2022) REMOVED AND REPLACED PAX DOOR INTERCOSTAL DD1 IAW CRJ 200 SRM 51-42-06.REFERENCE CONTINUE CARD FOR WORK PERFORMED. COMPLETED MAJOR STRUCTURAL REPAIR CARD 51-900-103-SKY AND COMPSDR SWIA202266558None · corrodedFOUND PAX DOOR INTERCOSTAL DD1A AFT SIDE TO BE CORRODED. (C-CHECK RO 9/28/2022) REMOVED AND REPLACED PAX DOOR INTERCOSTAL DD1A IAW CRJ 200 SRM 51-42-06. REFERENCE CONTINUE CARD FOR WORK PERFORMED. COMPLETED MAJOR STRUCTURAL REPAIR CARD 51-900-103-SKY ASDR SWIA202266557None · corrodedFOUND PAX DOOR INTERCOSTAL DD2 AFT TO BE CORRODED. (C-CHECK RO 9/28/2022) REMOVED AND REPLACED PAX DOOR INTERCOSTAL DD2 IAW CRJ 200 SRM 51-42-06. REFERENCE CONTINUE CARD FOR WORK PERFORMED. COMPLETED MAJOR STRUCTURAL REPAIR CARD 51-900-103-SKY AND COMSDR SWIA202266556None · corrodedFOUND PAX DOOR INTERCOSTAL DD5 AFT TO BE CORRODED. (C-CHECK RO 9/28/2022) REMOVED AND REPLACED PAX DOOR INTERCOSTAL DD5 IAW CRJ 200 SRM 51-42-06 .REFERENCE CONTINUE CARD FOR WORK PERFORMED. COMPLETED MAJOR STRUCTURAL REPAIR CARD 51-900-103-SKY AND COMPSDR SWIA202266553None · corrodedFOUND PAX DOOR INTERCOSTAL DD7 MID TO BE CORRODED. (C-CHECK RO 9/28/2022) REMOVED AND REPLACED PAX DOOR INTERCOSTAL DD7 IAW CRJ 200 SRM 51-42-06.REFERENCE CONTINUE CARD FOR WORK PERFORMED. COMPLETED MAJOR STRUCTURAL REPAIR CARD 51-900-103-SKY AND COMPSDR SWAA2022092943421Stringer · corroded(CORROSION) AT STRINGER 25R TO BULKHEAD CONNECTION AT BS 540. (CORRECTION) TO ORIGINAL DISCREPANCY(CORROSION) AT STRINGER 25R TO BULKHEAD FRAME CONNECTION AT BS 540 / [01] REMOVED CORROSION AT STRINGER 24R BS 540; AS PER B737-7; SRM 51-10-02.[31] INSTALLED STRSDR SWAA2022092802972Stringer · corroded(CORROSION) AT STRINGER 23L TO BULKHEAD FRAME CONNECTION AT BS 540. (CORRECTION TO ORIGINAL DISCREPANCY).(CORROSION) AT STRINGER 23L TO BULKHEAD FRAME CONNECTION AT BS 540. / [01] REMOVED CORROSION AT STRINGER 22L BS 540; AS PER B737-7; SRM 51-10-02.;[21] -FAB
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