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 JR2R20250711803Shear Tie · corrodedSHEAR TIE CORRODED AT FR88 BETWEEN STR26R AND STR27R. REPLACEDSDR DALA2026031101697Door Frame · corrodedFWD SERVICE DOOR CUTOUT FASTENER HOLES FOR TRIM NUT PLATES AT FR17 AND FR20 SHOW OXIDATION. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0568:5321-2013/003 00338 REPAIRED IAW PRI 627026-14 REV 0, PRI 627026-14 REV 1, PRI 627026-14 REV 2, PRI 627026-14 REV 3, SDR DALA2026031101696Door Frame · corrodedFWD PAX DOOR FRAME 19 HAS MULTIPLE FASTENER HOLES WITH CORROSION. REPAIRED IAW PRI 627025-14 REV 0, PRI 627025-14 REV 1, PRI 627025-14 REV 2, PRI 627025-14 REV 3, AND ER/A 627025-14 REV ORIGINAL SECTION 1. (LP# 1074103)SDR DALA2026031101695Door Frame · corrodedFWD PAX DOOR FRAME 22 HAS MULTIPLE FASTENER HOLES WITH CORROSION. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0567:5321-2009/003 00324 REPAIRED IAW PRI 627025-14 REV 0, PRI 627025-14 REV 1, PRI 627025-14 REV 2, PRI 627025-14 REV 3, AND ER/A 627025-14 REV ORISDR SWAA2025081289830Stub Frame · crackedCRACK FOUND ON STUB FRAME BS 294.5 +8.5'; ABOVE SEAL DEPRESSOR, BETWEEN S8R AND S9R; LENGTH 1.4'. REMOVED OLD FWD SERVICE DOOR STUB FRAME BS 294 +8.5' IAW SRM 51-40-02-0G-0 AND INSTALLED NEW FWD SERVICE DOOR STUB FRAME IAW SRM 51-40-02-0G-0 AND DWG 141A8370 SDR SWIA2025073000010Pressure Deck · out of positionPRESSURE FLOOR LOWER SIDE, AFT OF THE THE REAR SPAR AT RBL 27 DOUBLER CONTACTING THE REAR SPAR. REMOVED AND INSTALLED NEW PRESSURE FLOOR LOWER SIDE, AFT OF THE THE REAR SPAR AT RBL 27 DOUBLER. REF SRM 51-42-06-001-001-A01 AND DWG SH670-35820 REV-R. COMPLIED WSDR CALA2025072106743Window Frame · crackedFOUND CRACK AT THE LT SIDE NUMBER 3 WINDOW FRAME POST HOLE NO 2 3 AND 4 (HOLE NR 2 REPAIR PER EA5310-08195 REVISION B OPS 003) ( REF. AAR NR 1000043040) REPAIRED THE LH WINDOW #3 FRAME PART#141A8800-23 IAW EO#250203, REV P1, IR, ECRA 5310-08625. REPAIRED THE LSDR CALA2025072106742Window Frame · crackedFOUND DAMAGE CRACK AT THE RH SIDE NUMBER 3 WINDOW FRAME POST AT HOLE NO 4 DIRECTION 9 O'CLOCK, REF EA 5310-08195 REVISION B OPS 004 (REF. AAR NR 1000043039) REPAIRED THE RH WINDOW #3 FRAME 141A8800-24 IAW EO#250204, REV P1, IR, ECRA 5310-08626 ESFR HAS BEEN CRSDR JJBA20250716051Bracket · corrodedCARGO DOOR CUT-OUT STRUCTURE, LH FR 65 AT FLOOR LEVEL BRACKET FOUND CORRODED. ON CARGO DOOR CUT-OUT STRUCTURE, LH FR 65 AT FLOOR LEVEL BRACKET REMOVED AND INSTALLEDSDR DALA2025071405257Pressure Deck · cracked(LOG 1073967) A.A.5714-01004-01: CRACK WAS FOUND OF 0.8IN OF LENGTH APPROX ON LH PRESSURE DECK WEB AT STA 663 BTW LBL 40 AND 45 AT WING BOX. CRACK ON LH PRESSURE DECK WEB AT STA 663 BTW LBL 40 AND 45 AT WING BOX REA WAS REPAIRED PER B737-800 SRM 57-10-10-2R-3 SDR DALA2025071405256Pressure Deck · cracked(LOG 1073925) CRACK WAS FOUND OF 0.8 IN OF LENGTH APPROX ON LH PRESSURE DECK WEB AT STA 663 BTW LBL 40 AND 45 AT WING BOX. CRACK ON LH PRESSURE DECK WEB AT STA 663 BTW LBL 40 AND 45 AT WING BOX REA WAS REPAIRED PER B737-800 SRM 57-10-10-2R-3 REPAIR 3.SDR DALA2025071105243Crossbeam · crackedSHIP 3130 CRACK INDICATION FOUND IN HOLE H2 AT CROSSBEAM SPLICING FR16 RH, CRACK DIRECTION 11 O CLOCK VIEW LOOKING FORWARD. CORRECTIVE ACTION: COMPLIED WITH ER/A 626895-14AD. (1075195).SDR DALA2025071105242Crossbeam · crackedSHIP 3130 CRACK INDICATION FOUND IN HOLE H3 AT CROSSBEAM SPLICING FR16 RH, CRACK DIRECTION 11 O CLOCK VIEW LOOKING FORWARD. CORRECTIVE ACTION: COMPLIED WITH ER/A 626895-14AD. (1075180).SDR ABXA20250710154Beam · corrodedDURING 763CK'S C4 CHECK IN OSC, KALITTA MAINTENANCE CORROSION FOUND NOSE WHEEL WELL BEAM STA: 266.5 RIGHT HAND E&E BAY TUNNEL REPAIRED DAMAGED BEAM IAW B767-300 SRM 51-70-12.SDR R61A2025070500300Beam · corrodedDURING HEAVY CHECK AFT PASSENGER DOOR CUT OUT LOWER BEAM FOUND CORRODED BETWEEN FR 85-87. REPLACED BEAM IAW SRM 51-42-01SDR R61A2025070500299Seal Rest · corrodedDURING HEAVY CHECK AFT PASSENGER DOOR CUT OUT LOWER BEAM SUPPORT SEAL REST FOUND CORRODED. REPLACED SEAL REST IAW SRM 51-41-01SDR SWIA202511030709Door Sill · corrodedPAX DOOR LOWER SILL CORRODED IN MULTIPLE SPOTS (MARKED). (C-CHECK RO 11/01/2025)REMOVED AND INSTALLED NEW KICKPLATE ANGLE IAW CRJ 900 SRM 51-42-06-001-001-A01 AND CRJ 900 SRM 51-42-21-001-001-A01 AND DWG SH670-31810 REV. AE AND COMPLIED WITH TASK CARD 51-900SDR AALA202510213980Door Frame · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION ON FRAME 16 RH FROM THE THIRD FASTENER HOLE 6 FROM UPPER TO LOWER) OF AFT ROW AND 7 DOORSTOP FITTING LEVEL AT FWD GALLEY AREA L= 0.098IN. MAINTENANCE PERFORMED TIME LIMITED REPAIR (PARTIAL FRAME REPLACEMENT) ON FRSDR CALA2025072907030Web · damagedFLIGHT COMPARTMENT FLOOR STRUCTURE BETWEEN BS 250-260 LBL 17 TO RBL3 HAS DENT AT MULTIPLE PLACES. REMOVED 2 EACH DAMAGED AREAS BETWEEN STA 250 TO 260 LBL2 AND LBL13 IAW SRM 53-10-51-2R-2, REPAIR 2 SECTION 41 FLOOR WEB FIG 203. INSTALLED REPAIR DOUBLER BETWEEN SDR JR2R20250709784Beam · corrodedFWD WET AREA, CORROSION ON RBL 10 BEAM AT FRAME 17. OUT OF LIMITS. REPLACEDSDR DALA2026031101704Door Sill · corrodedDOOR LOWER SILL HAS CORROSION AS MARKED AT FASTENER HOLES. REMOVED CORROSION, AFFECTED AREA OF FWD CARGO DOOR LWR SILL FOUND OUT OF LIMITS IAW A220 ASRP J51-21-06, J53-21-25. RESTORED FINISH AND ACCOMPLISHED ALL WORK IAW DELTA ERA 627232-14 REV. ORIGINAL. (LP#SDR DALA2026031101703Door Sill · corrodedDOOR LOWER SILL HAS CORROSION AS MARKED AT FASTENER HOLES. REMOVED CORROSION, AFFECTED AREA ON AFT CARGO DOOR LOWER SILL FOUND OUT OF LIMITS IAW A220 ASRP J51-21-06, J53-61-25. RESTORED FINISH, ACCOMPLISHED ALL WORK IAW DELTA ERA 627233-14 REV.. ORIGINAL. ASSOSDR DALA2025070905181Door Frame · crackedSHIP 3130 CRACK INDICATION FOUND ON HOLE 3 OF THE DOOR STOP FITTING 7 AT FRAME 1 6 RH SIDE. REPLACED INTERCOSTAL FITTING (1 E/A) LOC. AT LEVEL DOOR STOP #7 ON FR16 RH IN FWD GALLEY AREA AS PER A319 SRM 51-42-11, A319 SRM51-72-11.SDR CALA2025070906383Crease Beam · corrodedMAIN CABIN CREASE BEAM INNER CHORD UPPER SURFACE HAS CORROSION AT STA 294, RBL 53. REMOVED CORROSION IAW SRM 51-10-02. FOUND TO BE OUT OF LIMITS PER ECRA 5321-01330 REV H. ORIGINAL MAT .094, REMOVED .017, REMAINING .077. INSTALLED NEW CREASE BEAM IAW SRM 51-SDR SCNA20250728277Pressure Deck · crackedCRACK ON PRESSURE DECK WEB AT STA 663 & RBL 42, MLG WHEEL WELL.. CRACK ON PRESSURE DECK WEB AT STA 663 & RBL 42, MLG WHEEL WELL WAS REPAIRED UNDER NRC 00265SDR DALA2025071105227Window Frame · cracked(LOG 1069452) CRACK OF 0.220IN LENGTH WAS FOUND ON NO. 1 LH WINDOW FRAME INNER CORNER RADIUS. NO. 1 LH WINDOW FRAME WAS REPAIRED PER ERA 619132-14ADTR REV. A SECTION I: PERMANENT REPAIR.SDR CALA2025070906376Blanking Plate · missingPDA 2 CREW LOG PAGE# 5470969, LEFT MAIN LANDING GEAR PURPLE BLANKING PLUG MISSING. LEFT MLG MISSING BLANKING PLUG. PERFORMED INTERIM REPAIR PER PART 1 OF ECRA 3211-01346 TO LT MLG BLANKING PLUG. ISSUE DIP TO ACCOMPLISH DAILY INSP IAW PART 2 & PERMANENT REPAIRSDR SCNA20250728282Frame · crackedWO 88395 NR00160, 00251: INITIAL INSPECTION: CRACK ON FRAME STA 312 & S-6L AT PASSENGER CABIN RESOLUTION: CRACK ON FRAME STA 312 & S-6L AT PASSENGER CABIN WAS REPAIRED PER B737-800 SRM 53-10-07-2R-1 REPAIR 1SDR CALA2025070706273Fitting · crackedWINDSHIELD LOWER NODE AREA, LEFT CONTINUITY FITTING CRACKED AT HORIZONTAL FLANGE, AFT EDGE. REMOVED/REPLACED LH AND RH CONTINUITY FITTINGS AS DIRECTED BY EA 5310-07675 AND IAW A319 SRM 51-42-14/001 AND AIRBUS REPAIR DRAW INGS R5311-2919 AND R 53113426.SDR SCNA20250707242Nut · missingFOUR OVER WING EMERGENCY EXIT DOOR, STOPS ARE MISSING DOOR STOP NUTS (16 EA).SDR FDEA202507061123Repair · no discrepancyEXISTING REPAIR ON MAIN DECK CROSSBEAM AT FR60 BETWEEN Y450 AND Y953 REQUIRES EVALUATION FOR CONFORMITY. THE EXISTING REPAIR ON MAIN DECK CROSSBEAM AT FR60 BETWEEN Y450 AND Y953 WAS EVALUATED AND FOUND IN CONFORMITY WITH A300-600F SRM53-10-15-201 FIG211. ESDR AALA202512022292Door Frame · crackedAIRCRAFT IN BASE MAINTENANCE: CRACKED FRAME FASTENER HOLE 4 IN THE DOUBLE JOGGLE AREA AT FR 16 RIGHT AND THE #7 DOOR STOP FITTING. REPAIRED FRAME PER EA 367854.SDR AALA202511282108Door Frame · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION ON FRAME 16 LH SIDE, IN HOLE 4, AT LEVEL DOOR STOP 7, AT FWD GALLEY AREA. (REPLACED PARTIAL FRAME REQUIRED BY EA 367853). MAINTENANCE ACCOMPLISHED TIME LIMITED REPAIR (PARTIAL FRAME 16 REPLACEMENT) LOC. ON FR16 LHSDR NACA2025070500002Stiffener · crackedDURING PERFORM MFEC INSPECTION OF RH SIDE NOSE WHEEL WELL BULKHEAD STIFFENER , ONE CRACK WAS FOUND AT BS287 BETWEEN WL 159 TO WL 185 AS MARKED, IT IS ABOUT 0.8 INCH LONG. CARRIED OUT THE STIFFENER REPAIR AT LEFT SIDE NOSE WW BULKHEAD STA 287 LBL 25 AS PER DRAFSDR NACA2025070500001Stiffener · crackedDURING PERFORM MFEC INSPECTION OF LT SIDE NOSE WHEEL WELL BULKHEAD STIFFENER , ONE CRACK WAS FOUND AT BS 287 BETWEEN WL 159 TO WL 185 AS MARKED, IT IS ABOUT 1 INCH LONG. CARRIED OUT THE STIFFENER REPAIR AT LT SIDE NOSE WW BULKHEAD STA 287 LBL25 AS PER DRAFT EOSDR YENA2025070800707Door Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 16 LH SIDE IN OPEN FASTENER HOLE H1 AT DOOR STOP FITTING 7 POSITION, CRACK DIRECTIONS ARE 6 AND 12 OCLOCK, CRACK D EPTH IS 0.115 INCH APPROX, AT FWD GALLEY AREA (2 EA); REF AEROMAN NR 2025-315768 WO 2025 177/SDR YENA2025070800706Door Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 16 LH SIDE IN OPEN FASTENER HOLE H3 AT DOOR STOP FITTING 7 POSITION, CRACK DIRECTION IS 3OCLOCK, CRACK DEPTH IS 0 .120 INCH APPROX, AT FWD GALLEY AREA (1 EA); REF AEROMAN NR 2025-315769 WO 2025 177/1 PERFORMESDR YENA2025070800705Door Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 16 RH SIDE IN OPEN FASTENER HOLE H1 AT DOOR STOP FITTING 7 POSITION, CRACK DIRECTION IS 7 OCLOCK, CRACK DEPTH IS 0.080 INCH APPROX, AT FWD GALLEY AREA (1 EA); REF AEROMAN NR 2025-315766 WO 2025 177/1 REMOVED SDR YENA2025070800704Door Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 16 RH SIDE IN OPEN FASTENER HOLE H3 AT DOOR STOP FITTING 7 POSITION, CRACK DIRECTIONS ARE 6 AND 9 OCLOCK, CRACK DEPTH IS 0.085 INCH APPROX, AT FWD GALLEY AREA (2 EA); REF AEROMAN NR 2025-315767 WO 177/1 REMOVSDR YENA2025070800703Door Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 16 LH SIDE IN OPEN FASTENER HOLE H2 AT CROS SBEAM SPLICING AREA, CRACK DIRECTION IS 12 OCLOCK, CRACK DEPTH IS 0.11 2 INCH, AT FWD GALLEY AREA (1 EA); PERFORMED PERMANENT REPAIR ON FRAME 16 LH SIDE HOLE H2 AT SDR YENA2025070800691Door Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION ON EMERGENCY EXIT DOOR 833FRAME SEGMENTS(1), LONGEST CRACK LENGTH IS AT AFT FRAME SEGMENT, L=0.63INCH,IN PASSENGER CABIN (8); (RESOLVED ON W/O: 1381843 TASKCARD: NR-00047) REF AEROMAN WO 2025-177/1 NR 2025-315758. ACCSDR YENA2025070800690Door Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION ON EMERGENCY EXIT DOOR 834 FRAME SEGMENTS(1), LONGEST CRACK LENGTH IS AT FRAME SEGMENT, L=0.22INCH, IN PASSENGER CABIN (8EA); (RESOLVED ON W/O: 1381843 TASKCARD: NR-00048) REF AEROMAN WO 2025-177/1 NR 2025-315757. ACCSDR YENA2025070800689Door Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION ON EMERGENCY EXIT DOOR 843 FRAME SEGMENTS(1), LONGEST CRACK LENGTH IS AT AFT FRAME SEGMENT, L=1.33INCH,IN PASSENGER CABIN (11EA); (RESOLVED ON W/O: 1381843 TASKCARD: NR-00049) REF AEROMAN WO 2025-177/1 NR 2025-315759.SDR YENA2025070800688Door Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION ON EMERGENCY EXIT DOOR 844 FRAME SEGMENTS (1), LONGE ST CRACK LENGTH IS AT FWD FRAME SEGMENT, L=1.43 INCH, IN PASSENGER CAB IN (20 EA); ACCOMPLISHED THE REINFORCEMENT OF THE STRUCTURE ON EMERGENCY EXIT DOOR 844 IAW SDR JR2R20250705800Angle · corrodedDRAIN MAST C-CHANNEL ANGLE JUST AFT OF FR87 BETWEEN STR27R AND STR28R.SDR SWIA2025121900703Door Frame · corrodedCOMPLY WITH SCHEDULED MAINTENANCE CODE: RA93189-601R-53-61-8212 MXCODEID77004-PR - FRAME FS574.00 AT CARGO DOOR FWD OPENING HAS CORROSION AT APPROX. WL 75.00. BLENDED CORROSION ON FRAME BS 574 AT CARGO DOOR FWD OPENING AT WL 75 IAW SRM 51-21-06 AND COMPLIED WSDR SWIA202507300003Pressure Deck · out of positionPRESSURE FLOOR AT BL0.0, R/H SIDE AFT BULKED BEAN AT LOWER SPLICE AND PRESSURE FLOOR, EXISTING PILOT HOLE DOESN'T LINE UP WITH THE EXISTING FULL SIZE HOLE OF THE BULK BEAN. SUBMITTED ENGINEERING. RECEIVED AND COMPLIED WITH REPAIR OF EXISTING UNALIGNED PILOT SDR CALA2025072806953Door Frame · corrodedFOUND TWO AREA OF INTER-GRANULAR CORROSION, NEXT TOO THE R1 DOOR(INNER-CHORD) REF AAR N/R 9983208 COMPLETED INSTALLATION OF FASTENERS AT INNER CHORD OF R-1 DOOR REF SRM 51-40-02-0G-0, DWG 141A8310. WORK ACCOMPLISHED BY V935074 AND INS-223. ESFR CREATED AND SUBSDR CALA2025071406496Crease Beam · corrodedMAIN CABIN L-2 DOOR AREA, INNER CHORD CORRODED ON UPPER SURFACE BETWEEN BS 951 AND BS 986 APPROX. LBL-50. REMOVED AND REPLACED L2 DOOR CREASE BEAM IAW B737-900 SRM 51-40-02 AND 51-40-05 AND BAC DWG 147A8540 ESFR COMPLETED CHANGED RII STATUS REMOVED AND REPLSDR CALA2025071406495Door Sill · corrodedR2 DOOR LOWER SILL AREA, INNER CHORD CORRODED ON UPPER SURFACE BETWEEN BS 951 AND BS 986 APPROX RBL-50. REMOVED DAMAGE, FABRICATED REPAIR PARTS, LOCATED, DRILLED, RESTORED COATINGS AND INSTALLED REF SRM 53-70-15-2R-1 AND 51-70-11-2R-0 THIS IS A CAT A REPAIR
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