JASC 5310
Service difficulty reports · 38,528
Reports filed under 5310 · Fuselage Main, Structure, 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 = '5310' 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 = '5310' 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 DALA2025020600944Failsafe · cracked(LOG 0797913) DURING INSPECTIONS FOR CRACKING OF THE FS663 PICKLE FORK FITTINGS PER AD 2021-09-06 (EM 5300-01157-02B), DAL MAINTENANCE IN CVG FOUND A CRACK ON THE FAILSAFE STRAP (P/N: 144A2412-4) COMMON TO THE RH FS663 PICKLE FORK FITTING. REPLACED FITTING PERSDR AALA202504146733Window Post · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION FOUND ON LOWER RADIUS OF WINDSHIELD CENTER POST LOWER ATTACHMENT AREA INTERNAL SIDE RH. CRACK L= 0.150 INCH. MAINTENANCE ACCOMPLISHED TIME LIMITED REPAIR ON WINDSHIELD CENTER POST LOWER ATTACHMENT AREA LH/RH SIDE SDR AALA202504143602Window Post · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION FOUND ON UPPER RADIUS OF WINDSHIELD CENTER POST LOWER ATTACHMENT AREA INTERNAL SIDE LH. L: 0.190 INCH. MAINTENANCE ACCOMPLISHED TIME LIMITED REPAIR O N WINDSHIELD CENTER POST LOWER ATTACHMENT AREA LH/RH SIDES (MIRSDR AALA202504142089Fitting · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION FOUND ON CONTINUITY FITTING OF WINDSHIELD LOWER ATTACHMENT AREA SIDE LH. CRACK L: 0.200 IN. MAINTENANCE REPLACED CONTINUITY FITTING LH LOC ON WINDSHIELD CENTER POST LOWER ATTACHMENT INTERNAL AREA IAW EA 361898, RESDR CALA2025021000321Beam · damaged(SUPPORT TASK) R/H LONGITUDINAL BEAM HAS SCREW STRIKE DAMAGE AT FR70 AND -Y464.8 TRANSCRIBED FROM HAECO GSO NR 9282045 REMOVED AND REPLACED LONGITUDINAL BEAM LOCATED BETWEEN FR68 TO FR70 AT -Y464.8 PER A320 SRM 51-42-11/001 AND AIRBUS DWG D53472040, ISSUE ASDR CALA2025021000319Beam · corroded(SUPPORT TASK) AFT MAIN CABIN, BETWEEN FR68 AND FR70, Y160.5, LONGITUDINAL BEAM, HAS CORROSION. REMOVED AND REPLACED LONGITUDINAL BEAM BETWEEN FR68 TO FR70 AT Y160.5 PER A320 SRM 51-42-11/001 AND AIRBUS DWG D53472040 ISSUE A.SDR DALA2025020600932Vortex Gen · damaged(LOG 0797479) WHILE ACCOMPLISHING REMOVAL OF VORTEX GENERATOR STRAP TO REPLACE ONE OF THE GENERATORS, IT WAS FOUND DAMAGE UNDER THE STRAP MADE BY 3 ADDITIONAL HOLES NOT FROM OEM INSTALL. ACCOMPLISHED REPAIR IAW ERA 623748-14 REV ORIGINAL.SDR AALA202502064702Fitting · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN CENTER WING BOX FORWARD SPAR UPPER SHEAR FITTING AT BS 540 AND LBL 54.60. REPLACED SHEAR FITTING PER AARD 57-14-00-1 REPAIR 1. THIS ACCOMPLISHES BOEING SB-737-57-1309.SDR AALA202502067569Fitting · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN CENTER WING BOX FORWARD SPAR UPPER SHEAR FITTING AT BS 540 AND LBL 40.87. REPLACED SHEAR FITTING PER AARD 57-14-00-1 REPAIR 1. THIS ACCOMPLISHES BOEING SB-737-57-1309.SDR AALA202502062463Fitting · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN CENTER WING BOX FORWARD SPAR UPPER SHEAR FITTING AT BS 540 AND LBL 32.40. REPLACED SHEAR FITTING PER AARD 57-14-00-1 REPAIR 1. THIS ACCOMPLISHES BOEING SB-737-57-1309.SDR AALA202502062315Fitting · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN CENTER WING BOX FORWARD SPAR UPPER SHEAR FITTING AT BS 540 AND LBL 15.04. REPLACED SHEAR FITTING PER AARD 57-14-00-1 REPAIR 1. THIS ACCOMPLISHES BOEING SB-737-57-1309.SDR AALA202502060464Fitting · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN CENTER WING BOX FORWARD SPAR UPPER SHEAR FITTING AT BS 540 AND LBL 6.14. REPLACED SHEAR FITTING PER AARD 57-14-00-1 REPAIR 1. THIS ACCOMPLISHES BOEING SB-737-57-1309.SDR AALA202502068521Fitting · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN CENTER WING BOX FORWARD SPAR UPPER SHEAR FITTING AT BS 540 AND RBL 6.14. REPLACED SHEAR FITTING PER AARD 57-14-00-1 REPAIR 1. THIS ACCOMPLISHES BOEING SB-737-57-1309.SDR AALA202502066189Fitting · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN CENTER WING BOX FORWARD SPAR UPPER SHEAR FITTING AT BS 540 AND RBL 15.04. REPLACED SHEAR FITTING PER AARD 57-14-00-1 REPAIR 1. THIS ACCOMPLISHES BOEING SB-737-57-1309.SDR AALA202502067067Fitting · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN CENTER WING BOX FORWARD SPAR UPPER SHEAR FITTING AT BS 540 AND RBL 32.40. REPLACED SHEAR FITTING PER AARD 57-14-00-1 REPAIR 1. THIS ACCOMPLISHES BOEING SB-737-57-1309.SDR AALA202502068223Fitting · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN CENTER WING BOX FORWARD SPAR UPPER SHEAR FITTING AT BS 540 AND RBL 40.87. REPLACED SHEAR FITTING PER AARD 57-14-00-1 REPAIR 1. THIS ACCOMPLISHES BOEING SB-737-57-1309.SDR AALA202502064310Fitting · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN CENTER WING BOX FORWARD SPAR UPPER SHEAR FITTING AT BS 540 AND RBL 54.60. REPLACED SHEAR FITTING PER AARD 57-14-00-1 REPAIR 1. THIS ACCOMPLISHES BOEING SB-737-57-1309.SDR 9WGA2025020534401Pressure Deck · corrodedEVIDENCE OF CORROSION STA 1240 ON THE RH CANTED PRESSURE DECK AREA ON THE OUTBOARD WALL. REMOVED CORROSION AT STA 1240 R/H CANTED PRESSURE DECK O/B WALL IAW B747-400 SRM 51-17-02-06-0, ALODINED, PRIMED AND TOP COATED IAW B747-400 SRM 51-20-01-06-0, PRIMED, AMSDR DALA2025020500881Door Frame · corrodedCORROSION ON AFT CARGO DOOR JAMB AT AFT CARGO BIN. SUMMARY OF NRC 00064: CORROSION LEVEL 2. THE AFT CARGO DOOR JAMB AT AFT CARGO BIN WAS REPAIRED PER B717-200 SRM 53-20-15-2R PROCEDURE 7 REPAIR 7. (LP #0796316)SDR IXXA20250205002Failsafe · corrodedFAILSAFE STRAP FOUND TO BE CORRODED 2 ADDITIONAL SPOTS AFTER REMOVAL OF BALLMAT SUPPORTSDR IXXA20250205001Panel · crackedFOUND WHILE CLEANING PDU 5L IN FLC, BILGE PANEL SURROUNDING CRACKED AND CORRODINGSDR CALA2025021000323Pressure Deck · dentedFLIGHT DECK FLOOR SKIN PANEL DENTS AT LBL 11 STA 259 AND STA 277 REF AAR N/R 9933688 ACCOMPLISHED FLIGHT DECK FLOOR WEB REPAIR AT LBL 11 STA 259 - STA 277 AS PER SRM 53-10-51-2R-2. WORK ACCOMPLISHED BY V928495 ACCOMPLISHED FLIGHT DECK FLOOR WEB REPAIR AT LBLSDR UIEA2025020300115Support Fitting · corrodedUPON RH BLG RETRACT ACTUATOR REMOVED, FOUND SUPPORT FITTING O/B LEG CORROSION.(<P>WORK ACCOMPLISHED IAW EN 1005-25 REV 0. NO FURTHER DEFECTS NOTED.</P>)SDR AALA202502057333Panel · tornAIRCRAFT WAS NOT GROUNDED: BILGE BARRIER DECOMPRESSION PANEL AT BS 345 LEFT HAND SIDE IS DAMAGED (TEARS). REMOVED AND REPLACED BILGE BARRIER DECOMPRESSION PANEL AT LEFT HAND SIDE AT BS 345. PER AMM 50-11-08. OKAY FOR SERVICE.SDR SWAA2025031092764Door Frame · crackedCRACK INDICATION ON STUB FRAME LOCATED ON BS 296.5 BTW S-8R TO S-9R AT FWD GALLEY DOOR AREA CRACK LENGTH 0.312 IN. APROX.AT PASSENGER CABIN 2025-110503<[01] REPLACED STUD FRAME LOC. ON BS 296.5 BTW S-8R TO S-9R AT FWD GALLEY DOOR AREA I.A.W B737-700 SRM 51-40-SDR SWAA2025031092771Stub Frame · crackedCRACK FRAME STUB LOCATED ON BS 294.5 AT LEVEL STR 17R AT PASSENGER CABIN 2025-110507<[01] EQUIPMENT P/N PHASEC 3D; S/N 800YBRK; DUE DATE 16-JUL-25 WAS USED ON STEP 4;[02] EQUIPMENT P/N PHASEC 3D; S/N 800YBRK; DUE DATE 16-JUL-25 WAS USED ON STEP 6;[03] REPAIREDSDR DALA2025020500900Failsafe · cracked(LOG 0794263) DURING INSPECTIONS FOR CRACKING OF THE FS663 PICKLE FORK FITTINGS PER AD 2021-09-06 (EM 5300-01157-02B), DAL MAINTENANCE IN CVG FOUND A CRACK ON THE FAILSAFE STRAP (P/N: 144A2412-4) COMMON TO THE RH FS663 PICKLE FORK FITTING. MAINTENANCE REPAIREDSDR DALA2025020500899Failsafe · cracked(LOG 0794037) DURING INSPECTIONS FOR CRACKING OF THE FS663 PICKLE FORK FITTINGS PER AD 2021-09-06 (EM 5300-01157-02B), DAL MAINTENANCE IN CVG FOUND A CRACK ON THE FAILSAFE STRAP (P/N: 144A2412-4) COMMON TO THE RH FS663 PICKLE FORK FITTING.SDR CALA2025020500293Window Frame · corrodedFWD CARGO DOOR CUTOUT AFT SHIELD UPPER SURFACE CORROSION REF AAR N/R 9937318 REMOVED AND REPLACED NEW SHIELD FROM STA 492 TO STA500A PER REF SRM 51-40-02-0G-0 AND DWG 143A8126.SDR CALA2025020500295Door Frame · corrodedPASSENGER CABIN R/H INNER CORD HAS SURFACE CORROSION AT STA 322. (DOT-241-003) REF AAR N/R 9936843 REMOVED AND REPLACED R/H INNER CHORD FROM STA 259.5-260 AS PER DWG 141A8310.SDR FDEA202502030171Crease Beam · crackedMAIN CABIN STA 1020 RH CREASE BEAM IS CRACKED IN 3 SPOTS AROUND HOLE. CUT / TRIMMED DAMAGE SECTION OF CREASE BEAM INNER CHORD FROM STA 1010 TO ORIGINAL SPLICE AT STA 1040 RBL 64.50 AND INSTALLED REPAIR PARTS BETWEEN STA 1004 TO ORIGINAL SPLICE AT STA 1040SDR AALA202504229055Beam · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION ON OPEN HOLE ZONE 1 POSITION 5 FR36. CRACK DIRECTION IS 12 AND 9 OCLOCK, LENGTH 0.100 INCH). ACCOMPLISHED INTERIM REPAIR ON OPEN HOLE ZONE 1 POSITION 5 FR36 (-Y765) IAW EA361963.SDR REXA2026072701141Strap · corrodedCORROSION ON FRAME STRAP AT FS 319.00 OF THE SERVICE DOOR SURROUND STRUCTURE. CORROSION ON FRAME STRAP AT FS 319.00 OF THE SERVICE DOOR SURROUND STRUCTURE WAS EVALUATED OUT LIMITS PER CRJ-900 SRM 51-10-06-001-001-A01 THEREFORE WAS REPLACED PER CRJ-900 SRM 51-SDR DALA2025020400823Window Frame · crackedSHIP 3136 CRACK INDICATION FOUND AT LH FRONT WINDSHIELD FRAMING (CENTER POST, UPPER RADIUS). CORRECTIVE ACTION: REPAIRED PER ER/A 622029-14. (0791399)SDR DALA2025020300803Retainer · crackedCRACK AROUND DRAIN OF RH SLIDING WINDOW RETAINER AT COCKPIT. SUMMARY OF NRC 00468: CRACK AROUND DRAIN OF RH SLIDING WINDOW RETAINER AT COCKPIT WAS REPAIRED PER PRI 622332-14 REV 1 AND ER/A 622332-14 REV ORIGINAL SECTION I: PERMANENT REPAIR. ASSOCIATED ER/A 14-SDR SWIA202506240131Door Sill · corrodedPASSENGER DOOR LOWER SILL HAS CORROSION FORWARD OF FS349.00 AS MARKED (C-CHECK RO 06/23/2025)INSTALLED NEW SILLL, AFT LOWER CORNER 600-31535-70 FWD OF FS349.00. REF CRJ 200 SRM 51-42-06-00 REV 39 DATE MAR 10/21CRJ 200 SRM51-42-21-00 REV 39 DATE MAR 10/21 DRWGSDR AALA202504021340Fitting · crackedAIRCRAFT IN BASE MAINTENANCE: FLIGHT DECK CENTER WINDSHIELD FRAMING RIGHT HAND CONTINUITY FITTING CRACKED. REPLACED ICONTINUITY FITTING PER EO 5319Y017-002.SDR SWAA2025030691893Stub Frame · crackedCRACK STUB FRAME BS 294.5 AT LEVEL STRINGER 17R PASS CABIN 2025-94239<[01] REPLACED FASTENER (2E/A) LOC. ON INNER CHORD BS 294.5 AT LEVEL STRINGER 17R PASS CABIN IAW B737-700 #DWG: 141A8310 SHEET: 25 REV:- AND SRM 51-40-02.<BR>SEE INDIVIDUAL SIGNS OFF BELOW.;[SDR DALA2025020400808Pressure Deck · corrodedSHIP 6707 RESSURE DECK SHEAR WEB HAS MULTIPLE AREAS OF CORROSION FROM S17L TO S17R @ STA 1681-1720. CORRECTIVE ACTION: REMOVED AND REPLACED PRESSURE DECK FROM STA 1681-1720 STR 14L-STR 17R IAW B757 200 SRM 51-40-02 AND DWG 146N5300 REV C. (0789299)SDR DALA2025020300794Stanchion · cracked(LOG 0788678) WHILE AT SEA, MTC DISCOVERED DAMAGE CONSISTING OF A CRACK RUNNING HORIZONTALLY ACROSS THE INSIDE OF THE VERTICAL STANCHION (C-D POST) COMMON TO WINDOW FRAME (P/N 141A8811-5) OF THE LH NO. 1 FLIGHT DECK WINDOW. THE CRACK EXTENDS INTO THE VERTICAL SDR AALA202504245454Fork · burredAIRCRAFT IN BASE MAINTENANCE: REPLACEMENT FITTING FORK END (BURRED MATERIAL) IS REQUIRED BY EA 361774. MAINTENANCE PERFORMED INTERIM REPAIR ON FITTING FORK-END RH AND LH SIDE ON RACK 80VU LOC BTW FR 23 TO FR 24 AND AT LEVEL STR 32RH /LH LOWER AREA IAW EA 36177SDR AALA202504218492Fitting · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION FOUND ON RH CONTINUITY FITTING OF WINDSHIELD LOWER ATTACHEMENT AREA INTERNAL SIDE, MEASURE OF CRACK IS: L=0.200 INCH. REPLACED CONTINUITY FITTING RH IAW MANUAL TALLY #99 EO# 5319Y017-002. EXACTLY LOCATION IS BTW FSDR AALA202504218730Fork · burredAIRCRAFT IN BASE MAINTENANCE: BURRED MATERIAL LOWER LATERAL FITTING RH SIDE RAC 80VU AFT AVIONIC, MEASURE ENLOGATED HOLE IS W=0.301 INCH.SDR AALA202504072703Fitting · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION FOUND ON LH CONTINUITY FITTING OF WINDSHIELD LOWER ATTACHMENT AREA INTERNAL SIDE, MEASURE OF CRACK IS: L=0.100 INCH. MAINTENANCE REPLACED CONTINUITY FITTING LH IAW MANUAL TALLY #99 EO #5319Y017-002. EXACTLY LOCATSDR SWIA202503060130Door Frame · corrodedPAX DOOR FRAME AT F/S313.56 BETWEEN DD4 AND DD5 INTERCOSTAL CLEAT P/N 600-31902-269 IS EXFOLIATED CORRODED JOB # HN00217522 (C-CHECK RO 3/5/2025) REMOVED AND REPLACED CLEAT AT FRAME F/S313.56 BETWEEN DD4 AND DD5 INTERCOSTAL IAW CRJ 700 SRM 51-42-06-0SDR REXA2025022500217Post · corrodedRBL9 COCKPIT DOOR POST IS CORRODED AT FLOOR LEVEL. REPAIRED RBL9 COCKPIT DOOR POST IAW CRJ700 SRM 53-11-10-201-006-A01 IAW CRJ700 SRM 53-11-10-201-006-A01 REPAIR OPTION A.SDR QXEA2025021800036Seat Track · corrodedLBL 11 SEAT TRACK BETWEEN FRAME 17 AND 20 IS CORRODED. REMOVED AND REPLACED DAMAGED SECTION OF SEAT TRACK IAW SRM 53-10-10-02-01,SDR R61A2025021800095Crossbeam · corroded"FWD WET AREA CROSS FRAME 17 CORRODED BETWEEN SEAT TRACKS AS MARKED. FABRICATED AND INSTALLED DOUBLER AND FILLER FOR REPAIR ON FWD WET AREA CROSS FRAME 17. REF EMB SRM 53-00-10 /REPAIR 03P"SDR FDEA202501300154Floor Skin · dentedMAIN CARGO COMP. AT APROX. STA 360 & RBL33 TO RBL54.75 PANEL 222BFF ABOVE FLOOR SKIN HAS INDENTATION (MARKED) REPAIRED MAIN CARGO COMPT. (MARKED) DENTED AREAS AT STA.360 RBL 33 TO RBL 54.75 PNL# 222BFF MPN: 141T5856-106 TOP SKIN OF FLOORBOARD. IN REF. TO SDR 2A6D20250130001Beam · damagedFASTENER HOLE DAMAGE (ELONGATION) WAS DISCOVERED ON THE LH MAINTENANCE FOOTSTEP BEAM (P/N 350A21124520) IN THE FUSELAGE REAR STRUCTURE.
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