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 DALA2025050703543Failsafe · corroded(LOG 7129800) WHILE WORKING AMDS CARD 5300-01157-02A CRACK INDICATION FOUND IN THE FAILSAFE STRAP AT FRAME STA 663.75. COMPLIED WITH E/RA 625780-14AD REV. ORIG. PRI REV 0. REPAIR INSTRUCTIONAL STEPS ENSURED ALL E/RA 625780-14AD REV ORIG. PRI REV 0, REPAIR INSTSDR DALA2025050703542Failsafe · corroded(LOG 6887799) WHILE WORKING AMDS CARD 5300-01157-02A A CRACK WAS FOUND IN THE FAILSAFE STRAP AT FRAME STA 663.75. COMPLIED WITH E/RA 625780-14AD REV ORIG. PRI REV 0, REPAIR INSTRUCTIONAL STEPS. ENSURED ALL E/RA 625780-14AD REV. ORIG. PRI REV 0, REPAIR INSTRUCTSDR DXTA2025050403348Door Frame · damagedFUSELAGE DOOR FRAME: WHEN OPENING THE MAIN CABIN DOOR THERE WAS A POPOING NOISE AND THE DOOR WAS EXTREMELY DIFFICULT TO OPEN. CORRECTIVE ACTION: BEGAN TROUBLESHOOTING. POWERED UP AIRCRAFT AND PERFORMED OPS CHECKS OF MED MULTIPLE TIMES WITH NO DEFECTS. GAINED ASDR SWIA202507150503Vertical Beam · damagedDURING INSPECTION OF THE 409+128 VERTICAL POSTS A INDICATION WAS NOTED AT 409+128 RBL18 VERTICAL POST INBD. CHANNEL AT WL69 IN THE RADIUS APPROX .400" IN LENGTH AND 100% FULL SCREEN HEIGHT FAILING NDT. (C-CHECK RO 07/15/2025)REPLACED FS 409+128 RBL 18 POSTS ISDR SWAA2025052266808Web · corrodedCORROSION WEB LOC ON STR28L AND BS 360 AT EQUIPMENT ELECTRONIC COMP 2025-296188 <[01]. REPLACED REPAIR WEB LOC. BS 351 TO BS 360; PLATE LOC BS 360;ANGLE LOC BS 351 ON STR 28L AT EQUIPMENT ELECTRONIC COMPARTMENT IAW B737-700 SRM 51-40-02 AND DWG 141A8511 SHEET SDR FDEA202505030731Crossbeam · crackedMDCC CROSSBEAM AT FR24, Y-450 - Y-953 CRACKED. COMPLIED WITH EA 6-5310-T0383330 P1 TO REPAIR MDCC CRACKED CROSSBEAM AT FR24, Y-450 - Y-953. EA TITLE: FUSELAGE - MAINFRAME - CRACK ON FR24 CROSSBEAM, BETWEEN -Y450 AND -Y953. THIS IS CATEGORY A REPAIR. MAJOR SDR DALA2025050703549Fitting · damaged(LOG 0946239) COMPLY WITH ER/A 625781-14AD REV. ORIG. FUSELAGE / STRINGERS / S-14L AND S-14R, FS 663.75 / SPLICES FOR ACCESS TO PICKLE FORK FITTING. COMPLIED WITH E/RA 625781-14AD REV. ORIG. PRI REV. "0", REPAIR INSTRUCTIONAL STEPS. ENSURED ALL E/RA 625781-14ASDR CALA2025050704523Window Frame · damagedACCOMPLISH PERMANENT REPAIR AT LEFT WINDOW FRAME POST PER ECRA 5611-01327 REF AAR N/R 9961722 ACCOMPLISHED REPAIR AT FLIGHT DECK LEFT WINDOW POST PER ECRA: 5310-08574. ACCOMPLISHED REPAIR AT FLIGHT DECK LEFT WINDOW POST PER ECRA: 5310-08574.REF AAR NR996172SDR DALA2025050603501Fitting · damaged(LOG 0946907) COMPLY WITH E/RA 625945-14AD REV. ORIG. PRI REV. "0","1","2", 3" REPAIR INSTRUCTIONAL STEPS. ENSURE ALL 625945-14AD REV. ORIG. PRI REV. "0","1","2",3" REPAIR INSTRUCTIONAL STEPS ARE COMPLETED AND MATCH FINAL - FUSELAGE / STA. 663.75 / R/H FITTINGSDR CALA2025050504461Window Frame · crackedRH COCKPIT, SLIDING WINDOW , FWD LATCH AREA , MILLED RISER, UNDE R LATCH CRACKED. ACCOMPLISHED REPAIR PER HAECO REO-L25450 REV 1R WITH NO DEVIATIONS. INTERIM REPAIR PERFORMED PER PART 1 OF ECRA 5311-03359 TO RH FR4 VERTICAL STIFFENER.SDR AALA202507088577Fitting · crackedAIRCRAFT IN BASE MAINTENANCE: FLIGHT DECK CENTER WINDSHIELD FRAMING LEFT HAND CONTINUITY FITTING CRACKED AT FR 4 AND Y0. REPLACED CONTINUITY FITTING PER EA 365054 .SDR AALA202507086944Fitting · crackedAIRCRAFT IN BASE MAINTENANCE: FLIGHT DECK CENTER WINDSHIELD FRAMING RIGHT HAND CONTINUITY FITTING CRACKED AT FR 4 AND Y0. REPLACED CONTINUITY FITTING PER EO 5319Y017-002.SDR AALA202506090627Door Frame · crackedAIRCRAFT IN BASE MAINTENANCE: AIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION WAS FOUND AT FR20 RH IN UPPER I/B HOLE DOOR STOP 7 . CRACK DEPTH : 0.100 INCHES. MAINTENANCE REPLACED INTERCOSTAL FITTING LOC. BTW FR20 TO FR21 RH AT LEVEL DOOR STOP FITTING 7 IAW A31SDR SWI2025F00676Beam · corrodedLH BEAM HAS CORROSION FRAME 87. REMOVED AND REPLACED LH BEAM BETWEEN FR86 - FR89. REF EMB SRM 51-40-08.. REPLACED BEAM WITH O.E.M PART AND DOES NOT EFFECT WEIGHT AND BALANCE.SDR SWI2025F00675Beam · corrodedRH IB BEAM HAS CORROSION FRAME 85-87. REMOVED AND REPLACED RH IB BEAM BETWEEN FR86 - FR89. REF EMB SRM 51-40-08. FACTORY REPLACEMENT PART NO CHANGE TO AIRCRAT WEIGHT AND BALANCE.SDR DALA2025050603504Failsafe · corroded(LOG 0945475) DUE TO CRACKS IN THE FAILSAFE STRAPS FUSELAGE / FS663.75 BULKHEAD / RH PICKLE FORK FITTING / FITTING REPLACEMENT. REPAIR PER ERA 625779-14AD.SDR AALA202505054759Structure · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON LAVATORY L4F-1L LOWER BASE EXTRUSION AT BS 1670, FROM LBL 39.5 TO LBL 102.5. REPAIRED LAVATORY LOWER BASE EXTRUSION PER EA 363691.SDR DALA2025050303397Post · damagedSHIP 3142 SECONDARY FINDING ELONGATED HOLE VERTICAL POST INTERNAL STRUCTURE AT LEVEL FR60 RH SIDE IN AFT CARGO COMPARTMENT. REPLACED VERTICAL POST INTERNAL STRUCTURE AT LEVEL FR60 RH SIDE IN AFT CARGO COMPARTMENT AS PER A319 SRM 51-42-11, A319 SRM51-72 -11 ASDR SWI2025F01226Cam · wornPASSENGER DOOR EXTERNAL SURROUND STRUCTURE FORWARD FS310 CAM FITTING WORN (C-CHECK RO 09/07/2025) REMOVED AND INSTALLED NEW PAX DOOR EXTERNAL SURROUND STRUCTURE FWD CAM FITTING @FS310 REF CRJ700 SRM 51-42-21-001-001-A01, DRAWING SH670-31810 REV -AE. SEE CONTSDR SWI2025F01225Stop Fitting · deformedPASSENGER DOOR EXTERNAL SURROUND STRUCTURE, FORWARD UPPER CORNER, DROP DOWN DOOR STOP ASSY DEFORMED FROM STOP BOLT (C-CHECK RO 09/07/2025)REMOVED AND INSTALLED NEW PASSENGER DOOR EXTERNAL SURROUND STRUCTURE, FWD UPPER CORNER, DOOR STOP ASSEMBLY WITH P/N: 600-SDR SWI2025F01224Stop Fitting · wornAFT BAGGAGE BAY DOOR SURROUND FORWARD LOWER STOP FITTING WORN (C-CHECK RO 09/07/2025)PERFORMED REPAIR ON AFT BAGGAGE BAY DOOR SURROUND FWD LOWER STOP FITTING PER REO 670-53-61-2516 REV -- DATED 2025-06-20. ALL STEPS COMPLIED WITH SEE CONTINUE CARD FOR DETAILSSDR SWI2025F01222Striker · damagedPASSENGER DOOR EXTERNAL SURROUND STRUCTURE AFT SEAL STRIKER DAMAGED AT FS349 CAM FITTING (C-CHECK RO 09/07/2025)COMPLIED WITH REPAIR OF PASSENGER DOOR EXTERNAL SURROUND STRUCTURE AFT SEAL STRIKER. REF - REO 670-53-22-001 REV -J DATED 2016-11-10 REPAIR (TYPE SDR SWI2025F01218Plate · corrodedTHE FWD CARGO DOOR SURROUND FUSELAGE SIDE AFT JOINT PLATE AT FS581 AND STR 25L IS CORRODED. (C-CHECK RO 09/07/2025)REMOVED CORROSION ON FWD CARGO DOOR SURROUND FUSELAGE SIDE, AFT JOINT PLATE AT FS588.00 AND STR 25LH, PER REF.CRJ/700 SRM.51-21-06-001-001-A01,SDR SWI2025F01217Strap · corrodedTHE INTERNAL PAX DOOR SURROUND FUSELAGE SIDE STRAP PLATE AT FS349 IS CORRODED. (C-CHECK RO 09/07/2025) BLENDED CORROSION (2 EA) ON INTERNAL PAX DOOR SURROUND FUSELAGE SIDE STRAP PLATE AT FS349. AND THEN COMPLIED WITH REO 670-53-21-2642, REV: -- DATED: 2025-0SDR SWIA2025082500501Door Frame · damagedLAND 27 ON THE FUSELAGE SIDE HAS FURTHER DAMAGE FROM FURTHER PIN MIGRATION. (C-CHECK RO 8/21/2025) REMOVED AND EVALD DAMAGE ON THE PAX DOOR LAND 27 ON FUSELAGE SIDE. FOUND TO BE WITHIN LIMITS REF DWG SH670-31875 REV. G AND CRJ 900 SRM 52-11-01-201-007-ASDR AALA202507250185Structure · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION FOUND ON CENTER WING BOX FR36 FRONT VERTICAL STRINGER #2 ZONE 1. CRACK DIRECTION AT 12 AND 1 O'CLOCK LOOKING AFT. D: 0.090 INCH. MAINTENANCE PERFORMED PERMANENT REPAIR ON CENTER WING BOX UPPER BEAM #2 +Y765 IAW EASDR SWAA2025052266285Web · crackedCRACK INDICATION ON HORIZONTAL PRESSURE DECK WEB LBL 31 STA 663 AT PASSENGER CABIN (1E/A). CRACK LENGTH APPROX. 0.600 INCHES. 2025-296071<[01]. TOOL USED IN STEP 6: ET EQUIPMENT; P/N: NORTEC 600D; S/N: 200053402 DUE DATE: 16-SEP-25; [02] TOOL USED IN STEP 7: ESDR IPXA2025051455228Window Frame · crackedRH FRONT UPPER WINDOW FRAME SECTION CRACK INDICATION NOTED IN FWD I/B HOLE AT 3 O' CLOCK AT UPPER ENTABLATURE LAYER. ROTO PERFORMED ON HOLE. HOLE IS FREE OF DEFECTS AT .218". INSPECTION DONE IAW NTM 51-10-01 T96526 T98461.SDR HYIA20250506001Door Frame · corrodedDURING MAINTENANCE, CORROSION DAMAGE WAS NOTED UNDERNEATH THE STRIKER PLATE FOR THE UPPER CLAMSHELL DOOR PIN ENGAGEMENT HOLE LOCATED ON THE MAIN CABIN DOOR POST. (F.S. 213.6) THE DEPTH OF THIS CORROSION IN GREATER THAN 25% OF THE THICKNESS OF THE DOOR POST ANDSDR DALA2025050503443Stanchion · cracked(LOG 0942748) DURING OVERNIGHT IN CVG, MTC DISCOVERED DAMAGE CONSISTING OF A CRACK RUNNING HORIZONTALLY ACROSS THE VERTICAL STANCHION (C-D POST) COMMON TO WINDOW FRAME (P/N 141A8811-3) OF THE LH NO. 1 FLIGHT DECK WINDOW. FUSELAGE / NOSE / CAPTAIN WINDSHIELD / SDR DALA2025050503437Fork · cracked(LOG 0943885) DURING INSPECTIONS FOR CRACKING OF THE FS663 PICKLE FORK FITTINGS PER AD 2021-09-06 (EM 5300-01157-02B AND 02A), DAL MAINTENANCE IN ATL FOUND A CRACK ON THE FAILSAFE STRAPS (LH P/N 144A2412-3; RH P/N 144A2412-4) COMMON TO THE LH & RH FS663 PICKLESDR DALA2025050503436Fork · cracked(LOG 0943779) DURING INSPECTIONS FOR CRACKING OF THE FS663 PICKLE FORK FITTINGS PER AD 2021-09-06 (EM 5300-01157-02B AND -02A), DAL MAINTENANCE IN ATL FOUND A CRACK ON THE STRAPS (LH P/N 144A2412-3; RH P/N 144A2412-4) COMMON TO THE LH & RH FS663 PICKLE FORK FISDR CALA2025050504446Fitting · crackedB737-57-4-1262 SHEAR FITTING AT STATION 540 AND RBL 32.40 IS CRACKED. REMOVED AND REPLACED SHEAR FITTING AT STA. 540 RBL 32.40 IAW B737-900 SRM 51-40-02 AND BAC DWG. 111A2000 REV. ORIGINAL.SDR CALA2025050504445Fitting · crackedSHEAR FITTING AT STATION 540 AND RBL 40.87 IS CRACKED. SUPPORT TASK NSA EMX N/R 00094. REMOVED AND REPLACED SHEAR FITTING AT STA. 540 RBL 40.87 IAW B737-900 SRM 51-40-02 AND BAC DWG. 111A2000 REV. ORIGINAL,SDR SWIA202507140430Stop Fitting · chafedALL 4 CARGO DOOR STOP FITTINGS (ROLLER FITTINGS ON DOOR SIDE) ARE CHAFED. HN00239150 (C-CHECK RO 07/11/2025)REPAIRED 4 CARGO DOOR STOP FITTING ON DOOR SIDE IAW MHIRJ REO 601R-52-31-435 REV -- DATE 2025-06-12. COMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKY. SSDR 9WGA2025061354509Rivet · corrodedDURING HEAVY CHECK ZONE 250 STA 1239 RIVETS WITH RUST (CORROSION) AROUND THE WINDOW. REPLACED RIVETS ZONE 250 STA 1239 THE WINDOW IAW MD-11F SRM 51-35-01-06-0. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR REXA2025060900636Beam · chafedWEAR BEAM OF AFT BAGGAGE-BAY CARGO DOOR STRUCTURE (INTERFERENCE WITH AFT BALANCE SPRING CABLE) BEAM OF AFT BAGGAGE-BAY CARGO DOOR STRUCTURE WAS MANUFACTURED PER EA CRJ953-19287 REV. C & EA NO CRJ953-19339 REV. IR AND WERE REPLACED PER CRJ900 SRM 51-42-06-001-0SDR SWAA2025060266007Pressure Deck · crackedCRACK FOUND ON HORIZONTAL PRESSURE DECK AT MID PASSENGER CABIN BS663+2 RBL 41 L: 0.35' MARKED<[01] REMOVED DAMAGE PART OF THE BEADED PRESSURE DECK WEB BS663.75-BS675 RBL38-RBL60 WL 202 AND REPAIRED I.A.W SRM 53-40-51-2R-2 REPAIR 2;[02] UPDATED TABLE MEASUREMENSDR JJBA20250509042Gusset · corrodedCF3 RH GUSSET #5 BTW FR 46-52 FOUND CORRODED. CF3 RH GUSSET #5 BTW FR 46-52 BLENDED OUT OF LIMITS. CF3 RH GUSSET #5 BTW FR 46-52 REPLACEDSDR DALA2025050503445Web · damaged(LOG 0941692) THIS WORK CARD INSTALLS A NEW SHIM BETWEEN THE RIGHT SIDE OF STA 727 FRAME INNER CHORD AND S-18A WEB. AD 2023-06-15 REQUIRES INSPECTING THE STA 727 FRAME INNER CHORD AT STRINGER S-18A FOR EXISTING REPAIRS, INSPECTING THE AREA FOR CRACKING, AND PESDR CALA2025050104386Door Sill · corrodedAFT CARGO ENTRY DOOR SILL HAS CORROSION. MARKED. BLENDED OUT AND SMOOTHED 03 EACH CORRODED AREA, AT AFT CARGO ENTRY DOOR SILL SKIN, WERE FOUND WITHIN LIMIT LIMITS IAW A320 SRM 53-41-49. REMOVED AND PLACED INTERNAL INTERCOSTAL AT FR 53 AND BTW STR 39R/ 41 R IASDR JR2R20250430546Bellcrank · damagedRH MLG BAY, EMERGENCY EXTENSION CABLE CENTER QUADRANT, BELLCRANK, RIG PIN HOLE IS ELONGATED.SDR IXXA20250430002Stiffener · dentedMAIN CABIN LONGITUDINAL STIFFER ABOVE CANTED BULKHEAD AT APPROX STA 1021 HAS 3 EACH DENTS AT APPROX RBL30SDR DALA2025043003326Bracket · unknownSHIP 3407 WIRE BUNDLE BRACKET ON FR 60 BETWEEN STGR 1L/1R IS NOT LOCATED IN THE CORRECT POSITION PER DRAWING. CORRECTIVE ACTION: REPAIRED PER ERA 625466-14 REV C. (0941207)SDR SWI2025F01104Plate · corrodedDURING AUDIT OF 6YR TASK CARD 53-230-500(DETAILED INSPECTION OF THE GALLEY SERVICE DOOR (FORWARD) SURROUND STRUCTURE, ABOVE FLOOR, INTERNAL - FS319.70 TO FS349.00 (EES)) FOUND AFT LOWER JOINT PLATE AT FS 349.00 - WL 72.00 APPEARS TO BE CORRODED. (C-CHECK RSDR SWI2025F01103Plate · corrodedDURING AUDIT OF 6YR TASK CARD 53-230-500(DETAILED INSPECTION OF THE GALLEY SERVICE DOOR (FORWARD) SURROUND STRUCTURE, ABOVE FLOOR, INTERNAL - FS319.70 TO FS349.00 (EES)) FOUND FWD LOWER JOINT PLATE AT FS 319.70 - WL 72.00 APPEARS TO BE CORRODED. (C-CHECK RSDR AALA202507089974Door Sill · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT LEFT PASSENGER / CREW DOOR CUT OUT LOWER SILL BETWEEN FR 67 AND FR 68 AT S23L. REPLACED LOWER SILL PER SRM 51-42-11.SDR AALA202505161486Rail · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CARGO COMPARTMENT AFT BULKHEAD LOWER LOBE RAIL ASSEMBLY AT BS 540 BL 0. REPLACED RAIL ASSEMBLY PER AARD 51-00-05-1.SDR CALA2025050104376Door Frame · dented(SDR)-(B757-06-3-0274) DENT IN L/H APU DOOR FRAME STA 1896. DOT 140-074.REF:124179 SDR/SFR REPORTING REMOVED LONGERON LH SIDE IAW B757-200 SRM 51-40-02-0G-0, RECIEVE D NEW LONGERON PN:UA 148N8201-7 LOCATED AND DRILLED WEB IAW B757 -200 SRM 51-40-05 RESTORED SUSDR IXXA2025042901Crease Beam · corrodedCORROSION ON THE LEFT CREASE BEAM FROM STA. 1600 TO STA 1640, AT CABIN FLOOR LEVEL LBL62
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