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 JJBA20251120082Sill Drain · corrodedRH MOP SILL AT FR 30, STR 16R, HAS CORROSION. REMOVED AND REPLACED RH FLOOR SILL AT FR 25 - FR 31.SDR SWAA2025111829041Pressure Web · crackedCRACK INDICATION FOUND (2EA) ON HORIZONTAL PRESSURE WEB AT LBL 31 BETWEEN STA 663 TO STA 675 IN MAIN WHEEL WELL. CRACK LENGTHS: 0.250 IN. & 0.187 IN. PERFORMED A PERMANENT REPAIR ON HORIZONTAL PRESSURE WEB IAW SRM 53-40-51-2R-2, REPAIR 2, AND EA 25-153-03006SDR SWAA2025111829040Pressure Web · crackedCRACK INDICATION FOUND ON HORIZONTAL PRESSURE DECK WEB AT RBL 41 BETWEEN STA 663 TO STA 675 IN THE MAIN WHEEL WELL CRACK LENGTH: 0.312 IN. PERFORMED PERMANENT REPAIR ON THE PRESSURE WEB IAW SRM 53-40-51-2R-2, REPAIR 2.SDR CALA2025102910704Deck Plate · corrodedAFT DECK PLATE HAS SEVERAL CORROSION SPOTS BETWEEN STA 1680 AND STA 1700 ROM BL 0 TO ABOUT 52". OUT OF LIMITS.SDR YENA2025102801072Door Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 68 LH SIDE IN OPEN FASTENER HOLE UPPER INBO ARD AT DOOR STOP FITTING 6 POSITION, CRACK DIRECTION IS 3 OCLOCK, CRACK DEPTH IS 0.095 INCH, AT AFT GALLEY AREA (1 EA); EVALUATED DIAMETER HOLES D1 TO D4 AND FOUNDSDR YENA2025102801071Door Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON FRAME SEGMENTS 1 AT DOOR / EMERGENCY EXIT / OVERWING EMERGENCY EXIT HATCH (AFT RH SIDE ZONE 844) CRACK LENGTH= 0.2 55 INCHES; REMOVED AND REPLACED FRAME SEGMENTS ON EMERGENCY EXIT DOOR DOOR 844 FOLLOWING INSTSDR YENA2025102801070Door Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON FRAME SEGMENTS 1 AT DOOR / EMERGENCY EXIT / OVERWING EMERGENCY EXIT HATCH (AFT RH SIDE ZONE 843) CRACK LENGTH= 0.2 95 INCHES; REF AEROMAN WO# 2025-262/1 NR# 2025-608615 REMOVED AND REPLACED FRAME SEGMENTS ON SDR YENA2025102801069Door Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON FRAME SEGMENTS 1 AT DOOR / EMERGENCY EXIT / OVERWING EMERGENCY EXIT HATCH (AFT LH SIDE ZONE 834) CRACK LENGTH= 0.2 75 INCHES; REF AEROMAN WO@ 2025-262/1 NR# 2025-608616 REMOVED AND REPLACED FRAME SEGMENTS ON SDR YENA2025102801068Door Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON FRAME SEGMENTS 1 AT DOOR / EMERGENCY EXIT / OVERWING EMERGENCY EXIT HATCH (AFT LH SIDE ZONE 833) CRACK LENGTH= 0.3 05 INCHES; REF AEROMAN WO 2025-262/1 NR# 2025-608617 REMOVED AND REPLACED FRAME SEGMENTS ON ESDR YENA2025102801066Door Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 68 RH SIDE IN OPEN FASTENER HOLE LOWER INBOA RD AT DOOR STOP FITTING 1 POSITION, CRACK DIRECTION IS 6 OCLOCK, CRACK DEPTH IS 0.115 INCH, AT AFT GALLEY AREA (1 EA); REF AEROMAN WO# 2025-262/1 NR2025-608762 PERSDR CALA2025102810664Crease Beam · damagedELONGATED HOLE ON CABIN R/H CREASE BEAM JUST AFT OF STA 1040.SDR SWAA2025120428642Pressure Deck · crackedCRACK INDICATION ON THE HORIZONTAL PRESSURE DECK WEB, RBL 41, BS 663. CRACK LENGTH: 0.187 INCH. PERFORMED A PERMANENT REPAIR ON THE HORIZONTAL PRESSURE DECK, BS 663 - 675, RBL 30 - 60 IAW SRM 53-40-51-2R-2, REPAIR 2.SDR DALA2025102907932Frame · corrodedWING TO BODY FAIRING FRAME 48, BOTH LEFT AND RIGHT FRAMES SHOW SIGNS OF CORROSION AND ELONGATED FASTENER HOLES. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 053-0001:5352-01038-09 /001 00626. REMOVED AND REPLACED FRAME REF A220 ASRP 53-82-55. (LP# 1272016)SDR IXXA20251026003Beam · crackedINNER CHORD AT STA 903.5 RBL89 CRACKEDSDR AALA202601052229Window Frame · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION FOUND ON WINDSHIELD CENTER POST UPPER TENSION BOLT POSITION LH, CRACK LENGTH 0.127 INCH APPROX AND CRACK DIRECTION 1 C LOCK LOOKING INBOARD. MAINTENANCE ACCOMPLISHED TIME LIMITED REPAIR LOCATED ON CENTER WINDSHIESDR AALA202601059245Window Frame · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION FOUND ON WINDSHIELD CENTER POST UPPER TENSION BOLT POSITION LH, CRACK LENGTH 0.127 INCH APPROX AND CRACK DIRECTION 1 C LOCK LOOKING INBOARD. MAINTENANCE ACCOMPLISHED TIME LIMITED REPAIR LOCATED ON CENTER WINDSHIESDR SWIA202512121025Post · corrodedAVIONICS BAY LEFT FLOOR POST AT LBL12 AND FS280.00 THERE IS SIGNS OF CORROSION WHERE THE POST CONNECTS TO FRAME 280. PERFORMED REPAIR AT LT FLOOR POST AT LBL 12 AND FS280.00 IAW SRM 53-00-00, 53-11-43, 51-42-06, 51-42-21, 51-42-10, 51-24-21, 51-40-11, 51-21-1SDR SWAA2025120128162Pressure Deck · crackedCRACK INDICATION ON THE HORIZONTAL PRESSURE DECK WEB, LBL 40, BS 663. PERFORMED A PERMANENT REPAIR ON HORIZONTAL PRESSURE DECK WEB IAW SRM 53-40-51-2R-2, REPAIR 2.SDR SWAA2025111728485Pressure Deck · crackedSUSPECTED OF CRACK AT HORIZONTAL PRESSURE DECK WEB BS 663, LBL 31, REMOVED AND REPAIRED HORIZONTAL PRESSURE DECK BS 663 - 675, LBL 25 - LBL 60 IAW SRM 53-40-51-2R-2, REPAIR 2.SDR AALA202511039050Door Frame · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION ON FRAME 16 , HOLE 4, AT LEVEL OF DOOR STOP 7, RH SIDE AT FWD GALLEY AREA. MAINTENANCE ACCOMPLISHED TIME LIMITED REPAIR LOC. ON FRAME16 RH SIDE IAW EA 367452.SDR JJBA20251120081Sill Drain · corroded"LH MOP SILL AT FR 26, STR 16L, HAS CORROSION. LH MOP SILL AT FR 24 HAS CORROSION AT FWD END. REMOVED AND REPLACED LH MOP SILL AT FR26SDR SWI2025F01538Beam · corrodedAFT WET AREA L/H BEAM AT FR 87/88 HAS CORROSION (C-CHECK RO 11/18/2025)REMOVED AND REPLACED L/H BEAM AFT WET AREA FR 86/89. REF EMB SRM 51-40-08. NO CHANGE TO WEIGHT AND BALANCE. SEE CONTINUATION CARD FOR WORK ACCOMPLISHED.SDR SWI2025F01537Beam · corrodedAFT WET AREA R/H BEAM AT FR 87/88 HAS CORROSION (C-CHECK RO 11/18/2025)REMOVED AND REPLACED AFT WET AREA R/H BEAM AT FR 87/88. REF EMB SRM 51-40-08. NO CHANGE TO WEIGHT AND BALANCE. SEE CONTINUATION CARD FOR WORK ACCOMPLISHED.SDR SWI2025F01536Beam · corrodedAFT SERVICE DOOR FWD AND AFT EVACUATION SLIDE FITTING CUTOUT HAS CORROSION. REMOVED AND REPLACED AFT SERVICE DOOR LOWER THRESHOLD BEAM IAW SRM 51-40-08. REPLACED WITH NEW OEM PART.SDR SWIA2025111900024Crossbeam · corrodedFRAME 87 CROSS BEAM CORRODED IN MULTIPLE AREAS. PERFORMED CUTOUT, FILLER, DOUBLER REPAIR ON FRAME 87 CROSS BEAM REF ETD2025-170-931088 AND SRM 53-00-10/REPAIR03P. NO CHANGE TO WEIGHT AND BALANCE.SDR ASAA2025102462314Crease Beam · corrodedAT PASSENGER CABIN FLOOR STRUCTURE RT CREASE BEAM FROM STA.747 THRU STA.887 HAS CORROSION IN MULTIPLE SPOTS (SOME IS MARKED). GROUNDED - YES. REMOVED DAMAGE, FOUND TO BE OUT OF LIMITS IAW SRM 53-60-13-1A-1, REPAIRED DAMAGE IAW EA 900ER-53EA-29536W: 1.5 O: 0.5SDR AALA202511171585Fitting · crackedAIRCRAFT IN BASE MAINTENANCE: CRACKED LEFT HAND MAIN LANDING GEAR DOOR ACTUATOR FITTING, FORWARD POSITION ON THE KEEL BEAM BETWEEN FR 42 AND FR 43, BETWEEN S41L AND S42L. REPLACED FITTING PER EA 368510.SDR AALA202510318069Window Frame · crackedAIRCRAFT IN BASE MAINTENANCE: CRACKED FLIGHT DECK CENTER WINDSHIELD FRAMING AT THE LEFT HAND WINDSHIELD FRAME CENTER POST AREA, FR 2 AND Y0. REPAIRED WINDSHIELD FRAME PER EA 367511.SDR AALA202510310728Window Frame · crackedAIRCRAFT IN BASE MAINTENANCE: CRACKED FLIGHT DECK CENTER WINDSHIELD FRAMING AT THE RIGHT HAND WINDSHIELD FRAME CENTER POST AREA, FR 2 AND Y0. REPAIRED WINDSHIELD FRAME PER EA 367511.SDR CALA2025102810675Window Frame · crackedON THE R3 WINDOW FRAME E-F CRACK REPAIR, ACCOMPLISH INSPECTION REQUIREMENTS PER PART 2 OF EC/RA 5311-03408 ON OR BEFORE 24 OCT 2027. WHILE PERFORMING EA 5310-08195 OP 002 ON R3 WINDOW FRAME, CRACK FOUND ON 3RD LOWER HOLE, REPAIR OF WINDOW FRAME ACCOMPLISHED PSDR DALA2025102407787Stub Beam · corrodedCORROSION ON CENTER WING TANK UPPER SKIN AT B STA 1000 LBL 57 UNDER A STUB BEAM. COMPLIED WITH ER/A 629550-14 PRI REV 1 AT STA 1000 LBL 57 ON CENTER WING TANK UNDER STUB BEAM. (1268463)SDR DALA2025102407785Stub Beam · corrodedCORROSION ON CENTER WING TANK UPPER SKIN B STA 1000 RBL 57 UNDER A STUB BEAM. COMPLIED WITH ER/A 629549-14 PRI RFV 1 FOR CENTER WING TANK UPPER SKIN OF STA 1000 RBL 57 UNDER STUB BEAM. (1268460)SDR DALA2025102407784Stub Beam · corrodedCORROSION AROUND A FASTENER HEAD ON THE CENTER WING TANK UPPER SKIN AT BS 960 RBL 57 UNDER A STUB BEAM. COMPLIED WITH ER/A 629549-14 PRI REV 1 ON CENTER WING TANK UPPER SKIN AT STA 960 RBL 57 UNDER A STUB BEAM. (1268458)SDR AALA202512301941Window Frame · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION FOUND ON WINDSHIELD CENTER POST LOWER ATTACHMENT AREA INTERNAL SIDE LOWER RADIUS LH. CRACK L= 0.100 INCH. MAINTENANCE PERFORMED TIME LIMITED REPAIR LOC ON WINDSHIELD CENTER POST LOWER ATTACHMENT AREA INTERNAL SIDSDR AALA202512300198Window Frame · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION FOUND ON WINDSHIELD CENTER POST LOWER ATTACHMENT AREA INTERNAL SIDE UPPER RADIUS RH. CRACK L= 0.110 INCH. MAINTENANCE PERFORMED TIME LIMITED REPAIR LOC WINDSHIELD CENTER POST LOWER ATTACHMENT AREA INTERNAL SIDE UPSDR AALA202512309193Window Frame · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION FOUND ON WINDSHIELD CENTER POST LOWER ATTACHMENT AREA INTERNAL SIDE LOWER RADIUS RH. CRACK L= 0.235 INCH. MAINTENANCE PERFORMED TIME LIMITED REPAIR ON WINDSHIELD CENTER POST LOWER ATTACHMENT AREA INTERNAL SIDE LOSDR REXA2025121201032Striker · corrodedCORROSION ON LOWER SILL OF GALLEY SERVICE DOOR (LOWER SURROUND STRUCTURE AREA) LOWER SILL OF GALLEY SERVICE DOOR (LOWER SURROUND STRUCTURE AREA) WAS REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01SDR HNAA2025120100841Beam · crackedCARGO ENTRY LWR BEAEM CRACKED . R & R LOWER BEAM IAW SRM 51-40-02.SDR SWAA2025112027444Web · corrodedCORRODED WEB BTW BS 927 - 947.5, LBL 3, WL 156.1. WEB CLASSIFIED AS PRIMARY-OTHER IAW SRM 51-00-04. REPLACED THE WEB IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, AND DWG 147A7500; SHEET 38; REV -.SDR JJBA20251120068Sill Drain · corrodedLH MOP SILL FROM FR 19 TO FR 20 HAS CORROSION. LH MOP SILL FROM FR 22 TO FR 23 HAS CORROSION. REMOVED AND REPLACED LH MOP SILL FROM FR18 TO FR23SDR HNAA2025111900754Post · damagedAFT CARGO ENTRY, FR 67 POST AND LWR ANGLE DAMAGED. R & R POST AND ANGLE IAW SRM 51-40-02SDR CALA2025111011073Threshold · corrodedAFT CARGO DOOR SILL PLATE HAS CORRODED NUTPLATES AND STRUCTURE O N UNDERSIDE 5 PLACES. REMOVED AND REPLACED DISCREPENT AFT CARGO THRESHOLD SILL PLATE I AW A319 SRM 51-42-11/001.SDR CALA2025102910700Deck Plate · dentedFLIGHT DECK FLOOR HAS DENTS BETWEEN BS 250 & 260, BEWTEEN LBL-18 & RBL 10. DENT WAS FOUND TO BE OUT OF LIMITS PER SRM 53-10-51-1A-1. W=4.2 DEPTH OF DAMAGE 0.016 ORIG THICK 0.040 REMAIN 0.024. FABRICATED (1 EA -1 WEB) AND (2 EA -2 SPLICE DOUBLER) IAW REO G25SDR FDEA202510232076Skin · corrodedAFT POTABLE WATER SERVICE DOOR PAN POSSIBLE CORROSION STA 1681 TO STA1701 BTW STRINGERS 26R TO STR 29R COMPLIED WITH FEDEX EA F-5330-T0385436 P1 TITLE: FUSELAGE-PLATES AND SKINS-AFT LAV PAN CUT OUT SKIN CORROSION REPAIR. MAJOR REPAIR.SDR SWAA2025120126923Sill Drain · corrodedCORROSION ON UPPER MAN SILL LOCATED BS 440 TO BS 492.5 ABOVE S-19R WL 190 FWD CARGO COMPARTMENT. REPLACED NEW UPPER MAN SILL LOCATED BS 440 TO BS 492.5 ABOVE S-19R WL 190 FWD CARGO COMPARTMENT IAW SRM 51-40-02, SRM 51-10-02, DWG 143A8110, SHEET 20, REV -, ANDSDR SWAA2025112027157Stub Frame · crackedCRACK INDICATION ON STUB FRAME, BETWEEN BS 294.5 - 296.5, BTW S8R TO S9R. LENGTH OF CRACK; 0.312 IN. REPLACED THE STUB FRAME AND FASTENERS IAW SRM 51-40-02, DWG 141A8370, SHEET 9, SHEET 10, REV D.SDR ASAA2025102262378Support Angle · crackedRIGHT A/C BAY AFT BULKHEAD, BS 663 CRACK UPPER INBD SUPPORT ANGLE. GROUNDED - YES. REPAIRED SUPPORT ANGLE ON RT A/C BAY AFT BULKHEAD IAW SRM 57-10-10-2R-5.SDR FXGA202511120001Structure · damagedAIRCRAFT HAD A STATIONARY TAIL STRIKE DAMAGING THE LOWER TAIL CONE AREA AND TAIL TIE DOWN FITTING. AIRCRAFT WAS PARKED ON A SLOPE AND WHEN THE PILOTS EXITED THE AIRCRAFT THE PLANE TILTED BACK AND THE TAIL STRUCK THE GROUND. CAUSED DAMAGE TO LOWER AFT TAIL CONESDR AALA202510312748Fitting · damagedAIRCRAFT IN BASE MAINTENANCE: DUE TO THE MAJOR REPAIR BEING ACCOMPLISHED ON THE FLIGHT DECK CENTER WINDSHIELD FRAMING THE LOWER CONTINUITY FITTING AT FR 1 AND Y0 MUST BE REPLACED PER INSTRUCTIONS OUTLINED IN EA 367511. REPLACED LOWER CONTINUITY FITTING PER EA SDR DALA2025102407782Sill Drain · corrodedCORROSION ON THE CREASE BEAM AKA "MOP SEAL" AKA (THE O/B SUPPORT FOR THE O/B CABIN FLOOR PANEL), ON THE RIGHT SIDE FROM STA.1455 TO STA.1485. CORRECTIVE ACTION: CREASE BEAM HAS BEEN FOUND TO BE OUT OF LIMITS PER SRM 53-60-13- 1A-1 DETAIL VIII. NOMINAL .090 REM
Back to JASC 5310