JASC 5311
Service difficulty reports · 61,540
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 SWAA2023050320373Frame · crackedCRACK FRAME LOCATED BS747 AND BETWEEN STR8R TO STR9R AT PASSENGER CABIN 2023-208634<[01] REPAIRED FRAME LOCATED BS747 AND BETWEEN STR8R TO STR9R AT PASSENGER CABIN IAW EA EA 1-A53-12114; SEE INDIVIDUAL SIGN OFFS BELOW.;[02] TASK COMPLETED; RII <BR><BR>SEE INDISDR DALA2023032402303Unknown · unknownAIRCRAFT 9513, CRACKS (2EAS) AND ELONGATED HOLES ON LH CUSP WEB BTW STA=656 TO STA=715 AND X=44 TO X=60 AT PAX CABIN. CORRECTIVE ACTION: CUSP WEB BTW STA=656 TO STA=715 AND X=44 TO X=60 AT PAX CABIN WAS FABRICATED PER B717-200 SRM 53-00-55-2R PROCEDURE 4 REPAISDR DALA2023032402298Unknown · unknownSHIP 649 ER/A 593661-14 / SECTION II INSPECTIONS. CORRECTIVE ACTION: REF ER/A 593661-14AD REV B. (2684628)SDR SWAA2023050319987Stub Frame · crackedCRACK STUB FRAME BS 296.5 AT LEVEL STRINGER 17R AT PASSENGER CABIN 2023-208568<[01] ET EQUIPMENT P/N: NORTEC 600D; S/N: 220272712; DUE DATE: 17-DEC-23;[02] TOOL USED EDDY CURRENT EQUIPMENT PN. NORTEC 600D; SN 220272712; DUE DATE 17-DEC-23;[03] TOOL USED: DIGITSDR SWIA202305030032Unknown · crackedFS.280 HAS A CRACKED CLIP ON THE INBD SIDE OF LBL 9 (MARKED) (C-CHECK RO 4/30/2023) REMOVED CRACKED CLIP, FS 280 LBL9 INBD SIDE AND INSTALLED NEW CLIP PER DWG#601R31113 REV AD AND CRJ 200 SRM 51-42-21. SEE CONTINUATION CARD FOR DETAILS. M-337 AND SKYWESDR SWIA202300418322Unknown · dentedLOWER REAR FUSELAGE @ FS1040 STR26R HAS 2 EA DENTS (MARKED WITH RED) (C-CHECK RO 4/17/2023) CUT AWAY DAMAGED AREA OF SKIN, INSTALLED A DOUBLER REPAIR AND COMPLIED WITH ALL STEPS OF REO 690-53-61-1204 REV -- DATED: 2023-04-04. COMPLIED WITH SKYWEST TASK SDR DALA2023032302212Unknown · unknownSHIP 1601 FUSELAGE FRAME END FITTING CRACK AT CABIN RH STA 852. CORRECTIVE ACTION: FUSELAGE FRAME END FITTING CRACK AT CABIN RH STA 852, CRACK LENGTH IS 1.8" . NEW FRAME END FITTING FABRICATED WITH MATERINAL 7050-T7451-4" AND REPLACED THE DAMAGE END FITTING ASSDR DALA2023032302211Unknown · unknownSHIP 1601 FUSELAGE FRAME END FITTING CRACK AT CABIN LH STA 852. CORRECTIVE ACTION: FUSELAGE FRAME END FITTING CRACK AT CABIN LH STA 852, CRACK LENGTH IS 1.7" . NEW FRAME END FITTING FABRICATED WITH MATERINAL 7050-T7451-4" AND REPLACED THE DAMAGE END FITTING ASSDR DALA2023032302246Unknown · unknownSHIP 199 AFT CARGO FRAME UPPER CHORD AT STA 1197+132 , LBL 6.5 TO LBL 20.5 FOUND CORROSION. CORRECTIVE ACTION: DAMAGED AREA REPAIRED PER ERA 606412-14. ()SDR SWAA2023042619264Attach Angle · crackedL/H BS663 UPPER ATTACH ANGLE IS CRACKED ON VAPOR BARRIER LBL8 WL167.68<REMOVED DAMAGED SECTION OF LH BS663 VAPOR BARRIER UPPER ATTACH ANGLE LBL8-LBL20 WL167.68 IAW SRM 57-10-10-2R-5. RECEIVED REPAIR PARTS FOR BS663 LH VAPOR BARRIER UPPER ATTACH ANGLE LBL8-LBL2SDR SWAA2023042619266Attach Angle · crackedR/H BS663 UPPER ATTACH ANGLE IS CRACKED ON VAPOR BARRIER RBL8 WL167.68<REMOVED DAMAGED SECTION OF RH BS663 VAPOR BARRIER UPPER ATTACH ANGLE RBL8-RBL20 WL167.68 IAW SRM 57-10-10-2R-5.RECEIVED REPAIR PARTS FOR BS663 RH VAPOR BARRIER UPPER ATTACH ANGLE RBL8-RBL20SDR DALA2023032302256Unknown · unknown(LOG 2681754) DURING INSPECTION FOUND LH STA 907 FRAME IS CRACKED AT BIN SUPPORT. REPAIRED LH FRAME STA 907 BETWEEN STR 8-9 FOR BIN SUPPORT BRACKET IAW DELTA WORK CARD 2526-01236-03A.SDR DALA2023032302255Unknown · unknown(LOG 2681714) DURING INSPECTION FOUND L/H FRAME STA 727D IS CRACKED AT BIN SUPPORT BRACKET. REPAIRED FRAME STA 727D BETWEEN STR 8-9 FOR BIN SUPPORT BRACKET IAW DELTA WORK CARD 2526-01236-02A.SDR DALA2023032302254Unknown · unknown(LOG 2681513) DURING INSPECTION FOUND R/H FRAME STA 727D IS CRACKED AT I/B FASTENER HOLE FOR BIN SUPPORT BRACKET. REPAIRED RH FRAME STA 727D BETWEEN STR 8-9 FOR BIN SUPPORT BRACKET IAW DELTA WORK CARD 2526-01236-02B.SDR DALA2023032302253Unknown · unknown(LOG 2681490) DURING INSPECTION FOUND RH FRAME STA 827 IS CRACKED AT I/B FASTENER HOLE FOR BIN SUPPORT BRACKET. REPAIRED RH FRAME AT STA 827 BETWEEN STR 8 - 9 FOR BIN SUPPORT BRACKET IAW DELTA WORK CARD 2526-01236-02B.SDR DALA2023032302252Unknown · unknown(LOG 2681477) DURING INSPECTION FOUND RH FRAME STA 867 IS CRACKED AT I/B FASTENER HOLE FOR BIN SUPPORT BRACKET. REPAIRED FRAME AT STA 867 BETWEEN STR 8 & 9 FOR BIN SUPPORT BRACKET IAW DELTA WORK CARD 2526-01236-02B.SDR DALA2023032302251Unknown · unknown(LOG 2681437) DURING INSPECTION FOUND RH FRAME STA 727B IS CRACKED AT I/B HOLE FOR BIN SUPPORT BRACKET. REPAIRED RH FRAME AT STA 727B AT BIN SUPPORT BRACKET IAW DELTA WORK CARD 2526-01236-02B.SDR 2A6D20230321005Angle · crackedDAMAGE WAS FOUND TO THE FRAME 5 (P/N: L533M1088219/L533M1105219) IN THE FORM OF CRACKS. THERE ARE FOUR CRACKS TO BOTH THE L/H AND R/H FRAME NEAR THE UPPER AND LOWER MOST POINTS WHERE THE MEDICAL INTERIOR BEAM ATTACHES. THE LONGEST CRACK MEASURED TO BE APPROXIMSDR 2A6D20230321004Angle · crackedDAMAGE WAS FOUND TO THE FRAME 5 (P/N: L533M1088219/L533M1105219) IN THE FORM OF CRACKS. THERE ARE FOUR CRACKS TO BOTH THE L/H AND R/H FRAME NEAR THE UPPER AND LOWER MOST POINTS WHERE THE MEDICAL INTERIOR BEAM ATTACHES. THE LONGEST CRACK MEASURED TO BE APPROXIMSDR 2A6D20230321003Frame · crackedDAMAGE WAS FOUND TO THE FRAME 5 (P/N: L533M1088219/L533M1105219) IN THE FORM OF CRACKS. THERE ARE FOUR CRACKS TO BOTH THE L/H AND R/H FRAME NEAR THE UPPER AND LOWER MOST POINTS WHERE THE MEDICAL INTERIOR BEAM ATTACHES. THE LONGEST CRACK MEASURED TO BE APPROXIMSDR 2A6D20230321002Frame · crackedDAMAGE WAS FOUND TO THE FRAME 5 (P/N: L533M1088219/L533M1105219) IN THE FORM OF CRACKS. THERE ARE FOUR CRACKS TO BOTH THE L/H AND R/H FRAME NEAR THE UPPER AND LOWER MOST POINTS WHERE THE MEDICAL INTERIOR BEAM ATTACHES. THE LONGEST CRACK MEASURED TO BE APPROXIMSDR 2A6D20230321001Keel Fitting · corrodedDAMAGE WAS NOTED TO THE R/H KEEL BEAM CAP (P/N: L533M1010203) IN THE FORM OF 2 EA SPOTS OF CORROSION LOCATED BENEATH THE EDGE OF THE COCKPIT FLOOR. THE CORROSION AT LOCATION 1 MEASURED AT APPROXIMATELY 1.0” X 0.50” AND 0.020” DEEP. CORROSION AT LOCATION 2 MEASSDR SWAA2023050318817Pressure Deck · crackedCRACK INDICATION FOUND ON HORIZONTAL PRESSURE DECK LBL 35 AT MAIN WHEEL WELL COMPARTMENT. CRACK LENGTH: 0.312 INCH. 2023-208334<[01] TOOL USED EDDY CURRENT EQUIPMENT P/N NORTEC 600D; S/N 60009161631 DUE DATE 31/JAN/24;[02] EDDY CURRENT EQUIPMENT P/N: NORTEC500SDR SWAA2023041918995Frame · crackedCRACK FRAME ON BS 312 AND STR5L TO STR6L FWD GALLEY AND LAV 2023-191894<[01] TRIMMING OUT INNER FLANGE UPPER CHORD FRAME BS 312 AT LBL 33 BETWEEN S-5L AND S-6L IAW EA# M-22-153-01244 [TTG8Q00K10P4] SEE INDIVIDUAL SIGN OFF BELOW.;[02] TRIMMING OUT INNER FLANGE SDR DALA2023032302245Unknown · unknownSHIP 199 HFEC FOUND 01 EA CRACK ABOUT 3MM LONG AT LH-BS 903.5 FRAME INNER CHORD TRANSITION RADIUS,THE REPAIR W/C 5311- 01195-09E MUST BE ACCOMPLISHED PRIOR TO FURTHER FLIGHT. CORRECTIVE ACTION: ACCOMPLISHED THE REPAIR FOR THE CRACK INNER CHORD AT LH STA 903.5 SDR DALA2023032302241Unknown · unknownSHIP 199 HFEC FOUND 01 EA CRACK ABOUT 3MM LONG AT RH-BS 859.5 FRAME INNER CHORD TRANSITION RADIUS,THE REPAIR W/C:5311- 01195-09B MUST BE ACCOMPLISHED PRIOR TO FURTHER FLIGHT. CORRECTIVE ACTION: ACCOMPLISHED THE REPAIR FOR THE CRACK INNER CHORD AT RH BS 859.5 FSDR DALA2023032202163Unknown · unknownSHIP 5647 COMPLY WITH ERA 607015-14AD REV. ORIGINAL. CORRECTIVE ACTION: COMPLIED WITH ERA 607015-14AD REV. ORIGINAL. (2679804)SDR A6WA202303208521Skin · dentedEXTERNAL FUSELAGE SKIN IS DENTED AT FS 265 BETWEEN STGR 24L AND 25L. AIRCRAFT REMOVED FROM SERVICE. COMPLIED WITH MHIRJ REO 601R-53-11-3834 REV-- DATED 2023-03-12 REPAIRED FUSELAGE SKIN BETWEEN FS250-FS265 AND STR23L -24LSDR SWAA2023042718657Frame · crackedCRACK ON FRAME BS 312 BTW STR 5L TO STR 6L AT FWD GALLEY AREA 2023-200069<[01] REPAIRED FRAME BS 312 BTW STR 5L TO STR 6L AT FWD GALLEY AREA IAW EA M-22-153-01244 REV 2 BARCODE TTG8Q00JZGGU. SEE INDIVIDUAL SIGN OFF BELOW.;[02] STEP 1 CORRECTED.<BR>REPAIRED FRASDR DALA2023032102128Unknown · unknownSHIP 5647 INSPECT STA 1260, 1280 & 1300 - ERA 607015-14. CORRECTIVE ACTION: REF ERA 607015-14. (2677188)SDR AALA202303285435Frame · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON FRAME LOCATED AT BS 320 AND S23L. REPAIRED FRAME PER SRM 51-40-02-OG AND EA B737-53-021226.SDR SWAA2023050117473Web · crackedCRACK FOUND AT HORIZONTAL PRESSURE DECK WEB STA 663; RBL-42. CRACK LENGTH : 0.265' CRACK FOUND AT HORIONTAL PRESSURE DECK WEB STA 663 RBL-42. CRACK LENGTH : 0.265'<[01] REMOVED AND INSTALLED NEW REPAIR PARTS AT STA 663 RBL 42 ON PREASSURE DECK WEB AND STIFFNERSDR SWAA2023041917566Angle · pulledAFT CARGO R/H TRANSITION ANGLE HAS FASTENER PULLED THROUGH STA 727E AT FRAME.< REMOVED TRANSITION ANGLE PER SRM 51-40-02.;[02] REMOVED RIVET. RIVET WAS PULLED THROUGH DUE TO CORROSION AROUND FASTENER. FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2.;CUT AND RESDR DALA2023031702008Unknown · unknownAIRCRAFT 9513, INITIAL INSPECTION: CRACKED RH CUSP WEB (2 EA) STA. Y= 655 TO Y=674 AT PASSENGER CABIN. CORRECTIVE ACTION: CUSP WEB RH (2 EA) STA. Y= 655 TO Y=674 AT PASSENGER CABIN WERE REPAIRED PER B717-200 SRM 53-00-55-2R PROCEDURE 4. CONFIGURATION 7003 CUSPSDR DALA2023031701993Unknown · unknownSHIP 3235 REPAIR AT FR68 AND S-22LH. CORRECTIVE ACTION: COMPLIED WITH ERA 606234-14AD REV A. (2673863)SDR DALA2023031701992Unknown · unknownSHIP 3235 REPAIR AT FR68 AND S-22LH. CORRECTIVE ACTION: COMPLIED WITH ERA 606234-14. (2673858)SDR DALA2023031701991Unknown · unknownSHIP 3235 REPAIR AT FR68 AND S-22LH. CORRECTIVE ACTION: COMPLIED WITH ERA 606234-14AD REV A. (2673855)SDR DALA2023031701990Unknown · unknownSHIP 3235 REPAIR AT FR68 AND S-22LH. CORRECTIVE ACTION: COMPLIED WITH ERA 606234-14. (2673850)SDR SWAA2023042416638Frame · crackedCRACK ON STA 312 FRAME INNER RADIUS ABOVE L1 DOOR CUT OUT. (MARKED)<[01] VERIFIED APPLICABILITY OF SRM 53-10-15-1A-1 ALLOWABLE DAMAGE 1 - FORWARD ENTRY AND AIRSTAIR DOOR SURROUND STRUCTURE;[02] ACCOMPLISHED EVALUATION ON STA312 FRAME INNER RADIUS ABOVE L1 DOORSDR DALA2023031501886Unknown · unknownIN REF NRC 00485 CORROSION ON RH CUSP WEB BTW STA Y=600 TO Y=615 AT PAX CABIN. SUMMARY OF NRC 00640: CORROSION LEVEL 2. CUSP WEB BTW STA Y=600 TO Y=615 AT PAX CABIN WAS REPAIRED PER B717-200 SRM 53-00-55-2R-4 FIGURE 216. (LP #2671432)SDR VNAA202304270007Frame · corrodedCORROSION ON FRAME FS= 310 BETWEEN STRG 24LH TO 25RH AT MAIN AVIONICS COMPARTMENT. (E/E)SDR VNAA202304270006Frame · corrodedCORROSION ON FRAME FS=333 BETWEEN STRG 25LH TO 26RH AT MAIN AVIONICS COMPARTMENT. (E/E)SDR SWAA2023041716214Frame · crackedCRACK FRAME ON BS 947.5 AT LBL 8.1 AFT CARGO COMPARTMENT 2023-185388<[01] REPLACED FRAME LOCATED ON BS947.5 BTW STR23L TO STR23R AT AFT CARGO COMPARTMENT I.A.W. B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02 AND DWG 147A1047 SHEET 107 REV. - AND DWG 147A0040 SHSDR SWAA2023041116511Frame · crackedFORWARD ENTRY DOOR CUTOUT STA 303.9+7' BETWEEN STR 5L-6L FRAME END CRACKED<[01] C/W EA NO: M-22-153-01244;[02] ACCOMPLISHED EA: M-22-153-01244.;[03] VERIFIED ACCOMPLISHMENT OF EA M-22-153-01244SDR SWIA202303280013Unknown · corrodedCORROSION ON AFT WET AREA R/H FLOOR BEAM AT FR87. (C-CHECK RO 3/24/2023) REMOVED AND REPLACED R/H FLOOR BEAM AT FR87. REF EMB 175 SRM 51-40-08. THIS ACTION DOES NOT EFFECT THE AIRCRAFT'S WEIGHT AND BALLANCE. REF CONTINUATION CARD FOR CORRECTIVE ACTION DSDR DALA2023031701967Unknown · unknownSHIP 199 LH BS 852 FRAME END TIE TRANSITION RADIUS FOUND CRACK. CORRECTIVE ACTION: DAMAGED AREA REPAIRED PER RA 606578-14 REV ORIGINAL. (2668013)SDR DALA2023031501902Unknown · unknownSHIP 5642 COMPLY WITH SECTION ONE OF ERA 606783-14AD REV. ORIGINAL. CORRECTIVE ACTION: COMPLIED WITH SECTION ONE OF ERA 606783-14AD REV. ORIGINAL. (2669007)SDR KCSA202303131018Frame · crackedCRACK FOUND ON FRAME SEGMENT AT LOWER FORWARD CORNER OF L5 DOOR CUTOUTSDR DALA2023031401879Unknown · unknownSHIP 5642 VIASAT SYSTEM INSTALLATION ON FS 1260 & FS 1280 FRAMES. CORRECTIVE ACTION: REF ERA 606783-14. (2667469)SDR DALA2023031501885Unknown · unknownNLG WHEEL WELL AFT FRAME FOR GEAR DOOR CUTOUT DAMAGED 2 PLACES. (MARKED) SUMMARY SEE NRC 005-0003:3221-4001/002 00005: REPLACED NLG WHEEL WELL AFT FRAME FOR GEAR DOOR CUT OUT FRAME PER B717 SRM 53-10-15-2. AND DAC DWG 5913421. (LP #2665497)
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