JASC 5311
Service difficulty reports · 61,537
Reports filed under 5311 · Fuselage Main, Frame, 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 = '5311' 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 = '5311' 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 SWAA2025040700756Stub Frame · crackedCRACK STUB FRAME LOCATED STA 294.5 AT LEVEL STR 17R AT FWD GALLEY AREA 2025-167697<[01] REPLACED STUB FRAME; SERATE PLATE (2 EA) AND LOWER REVEAL CORNER LOCATED BS 294.5 TO BS 296 BETWEEN STR14 R TO STR 17 R FWD GALLEY AREA B737-700 SRM 51-40-02 AND DWG 141A83SDR SWAA2025040214212Stub Frame · crackedCRACK STUB FRAME LOCATED STA 294.5 AT LEVEL STR 17R AT FWD GALLEY AREA 2025-167697 <[01]. REPLACED STUB FRAME; SERATE PLATE (2 EA) AND LOWER REVEAL CORNER LOCATED BS 294.5 TO BS 296 BETWEEN STR14 R TO STR 17 R FWD GALLEY AREA B737-700 SRM 51-40-02 AND DWG 141ASDR AC2A202502289202Support Frame · elongatedDURING OUR INSPECTION, WE DISCOVERED WORKING HYLOC FASTENERS AT THE FS 345.6 FRAME AND THE BL -16.5 TRANSMISSION MOUNT INTERCOSTAL FITTING. WHEN WE GRABBED THE COLLAR WITH PLIERS, WE NOTICED THAT THE FASTENER SHOWING THE MOST SIGNS OF WEAR HAS SLIGHT MOVEMENT.SDR AC2A202502289201Frame · corrodedUPON INSPECTION OF THE L/H SPONSON UPPER CENTRAL ATTACHMENT POINT (FS 361) WE HAD EVIDENCE OF LOOSE HARDWARE. UPON REMOVAL OF HARDWARE, WE FOUND THE BOLTS CORRODED AND CORROSION WITHIN THE BUSHING OF THE HOLE. THERE IS NO EVIDENCE OF FRETTING OR MUD WHERE THE SDR SWAA2025040700235Stub Frame · crackedCRACK INDICATION ON STUB FRAME LOCATED ON BS 294.5 BETWEEN STR-8 TO STR-9 IN FORWARD GALLEY DOOR RH SIDE; CRACK LENGTH 1.272 INCHES APPROX. 2025-167597<[01] REPLACED STUB FRAME LOC. ON BS 294.5 BTW S-7R TO S-9R AT FWD GALLEY DOOR AREA IAW B737-700 SRM 51-40-02SDR SWAA2025040214194Stub Frame · crackedCRACK INDICATION ON STUB FRAME LOCATED ON BS 294.5 BETWEEN STR-8 TO STR-9 IN FORWARD GALLEY DOOR RH SIDE; CRACK LENGTH 1.272 INCHES APPROX. 2025-167597 <[01]. REPLACED STUB FRAME LOC. ON BS 294.5 BTW S-7R TO S-9R AT FWD GALLEY DOOR AREA IAW B737-700 SRM 51-40SDR AALA202506266998Frame · crackedAIRCRAFT IN BASE MAINTENANCE: CRACKED FRAME AT FR 16 RIGHT AND DOOR STOP #7. REPAIRED FRAME PER EA EA 362981SDR SWIA2025041813Frame · corrodedCORROSION ON FORWARD SIDE OF FS700 BETWEEN STGR24L AND STGR23L AS MARKED (C-CHECK RO 04/17/2025)REMOVED AND REPLACED SECTION FRAME P/N: 600-36029-9, ON FORWARD SIDE OF FS700 BETWEEN STGR24L AND STGR23L, REF. DRW 600-36029, REV. D AND CRJ-200 SRM 51-42-06, RESDR SWIA20250418225Frame · corrodedFS589.0 FORWARD FLANGE HAS MULTIPLE AREAS OF CORROSION BETWEEN STGR19L AND STGR20R (C-CHECK RO 04/17/2025)REPAIRED DAMAGE BY BLENDING AT F.S. 589.00 FRAME BETWEEN STR 19L AND STR 20R REF REO 601R-53-61-8307 REV -- DATED 2025-03-31 COMPLIED WITH SKYWEST TASK SDR IPXA2025040844111Frame · crackedCRACK FOUND ON HOLE "A" ON FR47 LH HORIZONTAL JUNCTION. AREA MARKED IN BLACK. ERIFIED INSTALLATION OF HAREWARE PER EA 300-5710-27-A3809.COMPLIED WITH EA 300-5710-27-A3809 STEP 31. ACCOMPLISH THE REPAIR PER UPS EO-93045-REQ1 AND EA 300-5710-27-A3809 REV. -.SDR IPXA2025032044111Frame · crackedCRACK FOUND ON HOLE "A" ON FR47 LH HORIZONTAL JUNCTION. AREA MARKED IN BLACK. ACCOMPLISH THE REPAIR PER UPS EO-93045-REQ1 AND EA 300-5710-27-A3809 REV. -. CSDR DALA2025030201583Frame · cracked(LOG 0828893) CRACK FRAME BS 827 BTW STR 8R TO STR 9R AT PASSENGER CABIN. COMPLIED WITH ER/A 624011-14AD REV ORIGINAL MATCHES WITH ALL STEPS ON PRI 624011-14 REV 0 AND PRI 624011-14 REV 1, IT HAS BEEN VALIDATED. PERFORMED REPAIR INSTRUCTIONS ON FRAME BS 827 BTSDR DALA2025030201582Frame · cracked(LOG 0828886) CRACK FRAME BS 867 BTW STR 8R TO STR 9R AT PASSENGER CABIN. COMPLIED WITH ER/A 624011-14AD REV ORIGINAL MATCHES WITH ALL STEPS ON PRI 624011-14 REV 0 AND PRI 624011-14 REV 1, IT HAS BEEN VALIDATED. PERFORMED REPAIR INSTRUCTIONS ON FRAME BS 867 BTSDR DALA2025030201581Frame · cracked(LOG 0828867) CRACK FRAME BS 827 BTW STR 8L TO STR 9L AT PASSENGER CABIN. COMPLIED WITH ER/A 624011-14AD REV ORIGINAL MATCHES WITH ALL STEPS ON PRI 624011-14 REV 0 AND PRI 624011-14 REV 1, IT HAS BEENVALIDATED. PERFORMED REPAIR INSTRUCTIONS ON FRAME BS 827 BTWSDR DALA2025030201580Frame · cracked(LOG 0828826) CRACKED FRAME BS 867 BTW STR 8L TO STR 9L AT PASSENGER CABIN. COMPLIED WITH ER/A 624011-14AD REV ORIGINAL MATCHES WITH ALL STEPS ON PRI 624011-14 REV 0 AND PRI 624011-14 REV 1, IT HAS BEEN VALIDATED. PERFORMED REPAIR INSTRUCTIONS ON FRAME BS 867 SDR DALA2025030201578Frame · cracked(LOG 0828755) CRACK FRAME BS 480 BTW STR 8L TO STR 9L AT PASSENGER CABIN. COMPLIED WITH ER/A 624011-14AD REV ORIGINAL MATCHES WITH ALL STEPS ON PRI 624011-14 REV 0 AND PRI 624011-14 REV 1.SDR N6WA2025022504Frame · corrodedCORROSION ON FS333 BETWEEN STRINGERS 27 AND 26R. PERFORMED REPAIR ON FRAME AT FS333 BETWEEN STRINGERS 27 AND 26R IAW GOJET EO C550-53MR-048 AND MHIRJ REO 670-53-21-128.SDR N6WA2025022503Frame · corrodedCORROSION ON FS319 BETWEEN STRINGER 26L TO 26R. PERFORMED REPAIR THE FRAME AT FS319 BETWEEN STRINGERS 26L AND 26R IAW MHIRJ REO670-53-21-1281 AND GOJET EO C550-53MR-048.SDR FDEA202502250291Frame · dentedCABIN - LEFT HAND FRAME AT STATION 1641 LONGERON S 12L FOUND DENT. CABIN - DENT AT LEFT HAND FRAME STATION 1641 LONGERON 12 LEFT, REPAIRED AS PER MD-11 SRM 53-00-07-2R FIGURE 201 REPAIR 2. REPETITIVE INSPECTION REQUIRED - INITIAL AT 14,500 CYCLES AND REPSDR DALA2025022101372Frame · crackedSHIP 5814 A.D. // A.A. CRACK WAS FOUND OF 1.500IN LENGTH ON FRAME WEB STA 1380 BTW STGR 25R TO 26R (BEHIND OF THE GUIDE TRACK FITTING) " CORRECTIVE ACTION: SUMMARY OF NRC 00110: FRAME WEB STA 1380 BTW STGR 25R TO 26R WAS REPAIRED PER ER/A 624067-14AD REV ORIGISDR DALA2025022501460Frame · damaged(LOG 0822495) AFT CARGO BAY FRAME DAMAGED AT STA 727H STR 25L WL 160. REPAIRED AFT CARGO STA 727H L/H FRAME AT STR 25L WL 160 IAW B737 SRM 53-60-07-2R-2.SDR DALA2025022501459Frame · damaged(LOG 0822454) AFT CARGO BAY FRAME DAMAGED AT STA 727E STR 25L WL 160. REPAIRED AFT CARGO L/H FRAME AT STA 727E AT STR 25L WL 160 IAW B737 SRM 53-60-07-2R-2.SDR DALA2025022401391Frame · cracked(LOG 0817471) RIGHT HAND STA 727 FRAME INNER CHORD CRACKING, 737 REPAIR; RII ; SECTION 02 IAW A.A. 5311-01251-02B. ACCOMPLISHING RIGHT HAND STA 727 FRAME INNER CHORD, 737 REPAIR; RII; SECTION 02 IAW A.A. 5311-01251-02B.SDR DALA2025022001344Frame · noneSHIP 5814 DTA MONITOR INSPECTION LOG REF ERA 624067-14 FUSELAGE / FRAME / STA 1380 / WEB AND INNER CHORD, S-25R & S26R / EXISTING FREEZE PLUG REPAIR / INHIBITED INSPECTION. CORRECTIVE ACTION: REF ERA 624067-14. (0817164)SDR DALA2025022001330Frame · unknown(LOG 0817488) ACCOMPLISH LEFT HAND STA 727 FRAME INNER CHORD, 737 REPAIR. ACCOMPLISHING RIGHT HAND STA 727 FRAME INNER CHORD, 737 REPAIR; RII; SECTION 02 IAW A.A. 5311-01251-02A.SDR N6WA2025021808Frame · corrodedCORROSION AT FS533 IN FWD CARGO BAY. REMOVED AND REPLACED FRAME 533 IN THE FWD CARGO IAW CRJ SRM 51-42-06SDR AALA202505025944Frame · crackedAIRCRAFT IN BASE MAINTENANCE: CRACKED FRAME UPPER DOUBLE JOGGLE AREA FASTENER HOLE AT FR 16 AND S10R. REPAIRED FRAME PER EA 362408.SDR REXA2025040300392Frame · corrodedFS 319 FRAME IS CORRODED BETWEEN STRINGERS 26L-26R. CUT AWAY DAMAGED PORTION OF FRAME AND SPLICED IN REPAIR PARTS IAW CRJ 700 SRM 53-00-06-201-006-A01.SDR REXA2025040300388Frame · corrodedF.S. 295 STR 26L-26R CORRODED ON FWD AND AFT SIDE OF FRAME. REPAIRED BY CUTTING AWAY DAMAGED SECTION AND SPLICING IN REPAIR PARTS IAW CRJ700 SRM 53-00-06-201-006-A01.SDR N6WA2025021703Frame · corrodedCORROSION ON FRAME 295.00 BETWEEN STRINGERS 25L AND 25R. PERFORMED FALSE FLANGE REPAIR ON FRAME 295.00 BETWEEN STRINGERS 25L AND 25R IAW GOJET EO C550-53MR-048.SDR REXA2025022100211Frame · corrodedFS 565 IS CORRODED BETWEEN STR 17L AND 18L. REOAIRED PER ENDEAVOR AIR EA# CRJ753-18348.SDR SWI2025F00571Frame · corrodedFS847+16 FRAME ATTACHED FLANGE IS CORRODED BETWEEN STR 26L & 26R (C-CHECK RO 04/26/2025)REPLACED LOWER FRAME SEGMENTWHERE CORRODED AT F.S. 847+16 WITH SPLICE REPAIR OF NEW FRAME SEGMENT BETWEEN STGR 25L-25R, REF CRJ 900 SRM 53-00-06-201-001-A03 AND CRJ 900 SRSDR SWI2025F00581Frame · corrodedCORROSION NOTED ON FRAME 349 BETWEEN STRG25L-26R (MARKED) (C-CHECK RO 04/26/2025)REMOVED AND REPLACED NEW SECTION OF FRAME AT FS 349.00 BETWEEN STGR 25L - 26R REF CRJ900 SRM 51-42-06-001-001-A01, SRM 51-42-21-001-001-A01, DWG# SH690-31350 REV. M, DWG# SH670-3SDR SWIA20250428214Frame · corrodedFS847+32 FRAME ATTACHED FLANGE IS CORRODED BETWEEN STR 26L & 26R (C-CHECK RO 04/26/2025)REPLACED LOWER FRAME SEGMENTWHERE CORRODED AT F.S. 847+16 WITH SPLICE REPAIR OF NEW FRAME SEGMENT BETWEEN STGR 25L-25R, REF CRJ 900 SRM 53-00-06-201-001-A03 AND CRJ 900 SRSDR AALA202504143489Frame · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION FOUND ON FR35 LH SIDE FWD FACE TO PRESSURE BULKHEAD ATTACHMENTS STARTING FROM FASTENER LOCATED LEVEL OF 1 INCH BELOW OF STR 30L. CRACK L= 0.100 INCH. MAINTENANCE PERFORMED TIME LIMITED REPAIR LOC ON FR35 AND STRG SDR DALA2025022401416Frame · damaged(LOG 0820614) AFT CARGO BAY FRAME DAMAGED BETWEEN STA 727B STR 25L - STR 26L WL 160. REPAIRED AFT CARGO STA 727B L/H FRAME BETWEEN STR 25L AND 26L WL 160 IAW B737 SRM 53-60-07-2R-3 ALTERNATIVE 1.SDR UATA2650214255301Frame · puncturedFOUND A SMALL PUNCTURE IN THE AFT SIDE OF THE RH WEB OF FRAME 11, 2 INCHES ABOVE FLOOR LEVEL. REPAIRED PER CASA ENGINEERING DOC 252EA-00020 REV A. SEE 337 DATED 02/10/2025 FOR FURTHER DETAIL. REMOVED DAMAGED MATERIAL. DAMAGED AREA INSPECTED BY HFEC, NO INDICASDR SWI2025F01034Frame · corrodedFRAME F/S 319 IS CORRODED AT STRG 27 (MX 29634776) (C-CHECK RO 07/18/2025)INSTALLED NEW LOWER FRAME SECTION FS319 BETWEEN STR 23R - STR 21L REF CRJ-700 SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01 AND DWG SH670-31630 REV KCOMPLIED WITH SKYWEST TASK CSDR SWI2025F00587Frame · corrodedCORROSION ON FS645 FRAME ATTACHED FLANGE AND WEB BETWEEN STR 26L & 27 (C-CHECK RO 04/26/2025)PERFORMED REPAIR TO CORRDED FRAME AT FS645 BETWEEN STR 26L - 27. PER REO 690-53-31-922 REV -- DATED 2025-03-04. NO LEAKS NOTED. COMPLIED WITH TASK CARD 51-900-1002-SKSDR SWIA20250428213Frame · corrodedCORROSION ON FWD AND AFT SIDES OF FS501FRAME BETWEEN STR 26L AND 27 (C-CHECK RO 04/26/2025)PERFORMED FALSE FLANGE REPAIR TO FS501.00 FRAME SECTOR BETWEEN STR26L AND STR27 REF REO 690-53-31-931 REV -- DATED: 2025-03-18. COMPLIED WITH SKYWEST TASK CARD: 51-900SDR REXA2025031400319Frame · corrodedFRAME SEGMENT AT FS319.70 IS CORRODED BETWEEN STR 20L AND STR 21L. LOCATED AND DRILLED NEW SERVICEABLE FRAME SEGMENT PN: SH670-31891-3S IAW CRJ700 SRM 51-40-11-001-001-A01.INSTALLED NEW SERVICEABLE FRAME SEGMENT PN: SH670-31891-3S IAW CRJ700 SRM 51-42-06-001-0SDR DALA2025021401140Frame · crackedCRACK ON FRAME STA Y=1037, L-17L AND L-17R AT CPAX. SUMMARY OF NRC 00379: FRAME STA Y=1037, L-17L AND L-17R AT CPAX WERE REPAIRED PER B717-200 SRM 53-20-07-2R PROCEDURE 4 REPAIR 4. (LP #0808878)SDR SWAA2025032495545Frame · crackedCRACK ON FRAME BS 259.5 BETWEEN STRINGER 8R AND STRINGER 9R AT PASSENGER CABIN 2025-136683 <[01]. TOOL USED ON STEP 4 EDDY CURRENT EQUIPMENT P/N: NORTEC 600D S:N 60009161631 DUE DATE: 11-MAR-25; [02] REPAIRED FRAME - WEB AT BSTA 259.5 - BTW WL 240 & WL 280 ANSDR SWAA2025032495546Frame · crackedCRACK FRAME BS 259.5 BETWEEN STRINGER 8L TO STRINGER 9L AT PASSENGER CABIN 2025-136687 <[01] .TOOL USED ON STEP 4 ET EQUIPMENT: P/N: NORTEC 600D; S/N: 60007161486; CAL DUE DATE: 06-SEP-25; [02] REPAIRED FRAME - WEB AT BSTA 259.5 - BTW WL 240 & WL 280 AND BTW LSDR 2A6R2025021272504Frame · crackedDURING A 1000 HOUR AIRFRAME INSPECTION, FOUND LEFT & RIGHT SIDES OF THE 5 ALPHA FRAME CRACKED. REPLACING THE FRAME WITH P/N L533M1022966 PER AIRBUS SERVICE BULLETIN EC135-53-031SDR 2A6R2025021272503Frame · chafedDURING A 1000 HOUR AIRFRAME INSPECTION FOUND CHAFING ON THE LEFT AND RIGHT WEBS OF FRAME FOUR. REPAIRED IAW AIR METHODS ENGINEERING AUTHORIZATION 23-5300-EA-5011SDR 2A6R2025021272502Frame · corrodedDURING A 1000 HOUR AIRFRAME INSPECTION FOUND SEVERE CORROSION ON FRAME ONE ALONG THE LOWER FLANGE. REPAIRING IAW AIRBUS RDAS-EC135-53-2025-0282ASDR EE4Y2025021221719Frame · corrodedFWD FUSELAGE AT FR16 RH SIDE LANYARD HOOK HOLES WITH CORROSION, PERFORMED TEMPORARY REPAIR IAW COOPESA EO# COO-EO-2025-21556-R02 DATED 01/27/2025 AND AIRBUS RDAF 80873219/054/2025#A DATED 01/28/2025, UNDER COOPESA JOB: A1Q002 NRI 7-80SDR N6WA2025021202Frame · corrodedCORROSION AT FS349.00 BETWEEN STGR 25L AND STGR 25R. ACCOMPLISH FALSE FLANGE FRAME REPAIR ON FRAME FS349.00 BETWEEN STGR 25L AND STGR 25R IAW EO-C550-53MR-048SDR N6WA2025021201Frame · corrodedCORROSION AT FS310.00 BETWEEN STGR 25L AND 25R. ACCOMPLISH FALSE FLANGE REPAIR ON FRAME FS310.00 BETWEEN STGR 25L AND 25R IAW EO-C550-53MR-048
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