JASC 5310
Service difficulty reports · 38,519
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 2026FA0000079Window Frame · corrodedRIGHT WINDOW FRAME BETWEEN BS 500 AND 520, CORRODED,SDR 2026FA0000076Failsafe · crackedBS 955, S22L, LT FAIL SAFE STRAP ,SB 767-53A0100, A CRACK WAS FOUND ON THE LOWER HOLE OF THE LT FAIL SAFE STRAP.SDR 2026FA0000075Failsafe · crackedSEC 45 BS 955 S22R, RIGHT FAIL SAFE STRAP, SB 767-53A0100, CRACK FOUND ON THE LOWER HOLE OF THE RIGHT FAIL SAFE STRAP.SDR AALA202602098710Crossbeam · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN CROSSBEAM AT BS 537.5, LBL 1. REPLACED CROSSBEAM PER AARD 51-00-05-1.SDR AALA202602092104Crossbeam · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN CROSSBEAM AT BS 537.5, RBL 1. REPLACED THE CROSSBEAM PER AARD 51-00-05-1.SDR DALA2026020600876Intercostal · crackedUPPER FUSELAGE, FORWARD ENTRY AREA, DOOR STOP FITTING 7 ON FR 16 RT SIDE, HOLE 1 & 3, WITH CRACK INDICATION AT INTERCOSTAL LAYER. REPLACED THE INTERCOSTAL IAW SRM 51-72-11-911-001, REV 155, AND DRAWING D5312300, ISSUE E, SHEET 01. FITTING P/N: D53114236201SDR AALA202602055605Rail · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CARGO COMPARTMENT AFT BULKHEAD LOWER LOBE RAIL ASSEMBLY AT BS 500I, FROM LBL 25 TO RBL 25. REPLACED RAIL ASSEMBLY PER AARD 51-00-05-1.SDR FDEA202602030116Seat Track · corrodedMAIN CARGO SEAT TRACK BS 1320 TO 1540 LBL 45.50 WITH MULTIPLE CORROSION. REMOVED SEAT TRACK SECTION MAIN CABIN STA 1320 TO 1540 LBL 45.50 TRIMMED, LOCATED AND DRILLED SEAT TRACK SECTION IAW B757 SRM 51-40-05-0G AND BOEING DWG 146N5130 REV C INSTALLED SEATSDR SWAA2026030966766Crossbeam · crackedCRACKED FLOOR STRUCTURE LOCATED BS 540, BL 0 - LBL 24. REPLACED FLOOR STRUCTURE IAW SRM 51-10-02, ITEM 9, & DWG 143A0060, SHEET 64, REV-.SDR CALA2026030914402Structure · corrodedR2 DOOR CUTOUT AREA, INNER CHORD HAS CORROSION ON UPPER SURFACE BETEWEEN BS 947 TO 986.5 APPROX. RBL-56. REMOVED AND REPLACED INNER CHORD AT R2 DOOR CUTOUT AREA BETWEEN BS947 TO 986.5 RBL56 PART NUMBER 147A8540Y3D PO NO. 1140348.18 IAW B737-900 SRM 51-40-02 ASDR SWAA2026021167393Drain Valve · crackedLOWER FUSELAGE SKIN HAD THREE BILGE DRAIN VALVES CRACKED BS 420, 500A & 500G. R & R THE THREE BILGE DRAIN VALVES IAW AMM 53-31-03-000-801 AND AMM 53-31-03-400-801. ACCOMPLISHED CABIN PRESSURE LEAK TEST IAW TASK CARD 821-PRD-01-01 (TTG8Q00MBMAW). NO LEAKS SDR DALA2026020600875Door Frame · crackedWORK CARD 5311-01229-02, UPPER FUSELAGE, FORWARD ENTRY AREA, DOOR STOP FITTING NR 7 ON FR 16 LT SIDE, HOLES 1 & 3, CRACK INDICATION AT INTERCOSTAL LAYER. REPLACED THE INTERCOSTAL D5311423620091 IAW SRM 51-72-11-911-001, REV 155. AND DWG D5312300, ISSUE E, SHSDR AALA202602058840Gusset · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN FORWARD CARGO COMPARTMENT AFT BULKHEAD GUSSET AT BS 500I, S24L. REPLACED GUSSET PER AARD 51-00-05-1.SDR YENA2026020400141Window Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON WINDSHIELD CENTER OPOST LOWER ATTACHMENT, VERTICAL FLANGE AREA RH SIDE. CRACK LENGTH 0.196 INCHES APPROX; REF AEROMAN NR 2025-682430 WO 2025 413/1 ERFORMED REPAIR TO CRACKS AFFECTING THE WINDSHIELD FRAME CENTSDR YENA2026020400136Fitting · crackedDURING HEAVY MAINTENANCE: CRACK ON CONTINUITY FITTING LH AT COCKPIT; REF AEROMAN NR 2025-682704 WO 2025 413/1 PERFORMED REPAIR TO CRACKS AFFECTING THE WINDSHIELD FRAME CENTER POST LOWER NODE AREA R/H VERTICAL FLANGE AND CONTINUITY FITTINGS ASPER AEROMAN EA# 53SDR YENA2026020400135Structure · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND IN OPEN HOLE ZONE 1, POSITION 4 OF VERTICAL STRINGER RADIUS IN CENTER FUSELAGE ON FR 36, CRACK DEPTH 0.129 INCH CRACK DIRECTION 3 AND 4 O'CLOCK VIEW LOOKING AFT; REF AEROMAN NR 2025-682309 WO 2025 413/1 PERFORMESDR YENA2026020400117Doubler · corrodedDURING HEAVY MAINTENANCE: FUSELAGE / NOSE FWD FUSELAGE / NLG COMPARTMENT REINFORCEMENT DOUBLER AT FR16-17 AND Y+250 / CORROSION - PERMANENT REPAIR; REFERENCES: /1/ AEM EA 53-0089-25 REV 0 (COVER AND PARTS 1 - 5) /2/ AIRBUS RDAF 81702470/003/2025#A /3/ REPAIR ISDR YENA2026020400114Pressure Deck · crackedDURING HEAVY MAINTENANCE: FUSELAGE / CENTER FUSELAGE / PRESSURE DECK PANEL / FR36 RHS / ATTACHMENT HOLES / CRACKS – TIME LIMITED REPAIR; REFERENCES: /1/ AEROMAN EA 53-0085-25 REV. 0 (COVER + PARTS 1-8) /2/ AIRBUS DOSSIER 81696490 /3/ AIRBUS RDAF 81696490/003/2SDR YENA2026020400113Window Frame · crackedDURING HEAVY MAINTENANCE: FUSELAGE / NOSE FWD FUSELAGE / WINDSHIELD FRAME / CTR POST LOWER NODE AREA VERTICAL FLANGE RHS & CONT. FITTING LHS / CRACKS - PERMANENT REPAIR; REFERENCES: /1/ AEROMAN EA 53-0081-25 (COVER + PARTS 1-5) /2/ AIRBUS DOSSIER 81689336 /3/ SDR SWIA2026020176127Post · failed inspFS409+128 BL0 VERTICAL POST RH & LH SIDES HAVE INDICATIONS: LH IS 60% FSH .3? LONG, AND RH IS 50% FSH .3? LONG IN THE AFT RADIUS OF POST @ WL69. FAILED NDT INSPECTION. INSTALLED NEW SERVICEABLE BL0 VERTICAL POST LH AND RH ANGLES AND LH/RH STIFFENERS AT FS 40SDR JJBA20260220071Support · corrodedCORROSION OF THE RH SILL AT FRAMES 44. REMOVED CORROSION AND REPAIRED THE RH SILL AT FRAME 44.SDR DALA2026020600852Window Frame · crackedCRACK INDICATION ON FRAME 2 WINDSHIELD CENTER POST LOWER NODE RH SIDE POCKET INTERNAL AREA, FROM UPPER TENSION BOLT, CRACK DIRECTION IS 10 O CLOCK, CRACK LENGTH IS 0.115 INCH, AD 2020-17- 03 / WORKCARD 5311-01226 -01. REQUESTING REPAIR DISPOSITION. REPAIR MUSTSDR DALA2026020600851Window Frame · crackedCRACK INDICATION ON FRAME 2 WINDSHIELD CENTER POST LOWER NODE LH SIDE POCKET INTERNAL AREA, FROM UPPER TENSION BOLT, CRACK DIRECTION IS 2 O CLOCK, CRACK LENGTH IS 0.095 INCH, AD 2020-17- 03 / WORKCARD 5311-01226 -01. REQUESTING REPAIR DISPOSITION. REPAIR MUST SDR DALA2026020200746Window Frame · crackedCRACK INDICATION ON FRAME 2 WINDSHIELD CENTER POST LOWER NODE RH SIDE POCKET INTERNAL AREA, AT LOWER INBOARD RADIUS, CRACK DIRECTION IS HORIZONTAL, CRACK LENGTH IS 0.375 INCH, AD 2020- 17-03 / WORKCARD 5311-0122 6-01. COMPLIED WITH ER/A 631326-14AD REV. ORIGISDR DALA2026020200745Fitting · not reportedPERFORM ER/A 596680-14AD CONTINUITY FITTINGS LT & RT SIDE REPLACEMENT. COMPLIED WITH ER/A 596680-14AD REV A. MATCHES WITH ALL STEPS ON PRI 596680-14AD REV 0, PRI 596680-14AD REV 1, PRI 596680-14AD REV2 AND PRI 596680-14AD REV 3. STEPS RELATED TO ITEMS OF ER/ASDR AALA202602011242Door Sill · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON L1 ENTRY LOWER SILL INNER CHORD BETWEEN BS 294.50 AND BS 312.0. REPLACED INNER CHORD PER AARD 51-00-05-1 AND EA 366791.SDR SIMA20260131001Reinforcement · not reportedSTD-REQ EJ-53MA-078 OPS PTA DUE - FORWARD PASSENGER AND SERVICE DOORS CUTOUT STRUCTURE REINFORCEMENT. TRANSFERRED FROM NRWC 770-ABI-02962 ITEM 1" (MAJOR ALTERATION) EO EJ-53MA-078 OPS PTA - FORWARD PASSENGER AND SERVICE DOORS CUTOUT STRUCTURE REINFORCEMENT C/SDR SIMA20260131003Reinforcement · not reportedSTD-REQ EJ-53MA-078 OPS PTB DUE - FORWARD PASSENGER AND SERVICE DOORS CUTOUT STRUCTURE REINFORCEMENT. TRANSFERRED FROM NRWC 770-ABI-02961 ITEM 1"(MAJOR ALTERATION) EO EJ-53MA-078 OPS PTB - FORWARD PASSENGER AND SERVICE DOORS CUTOUT STRUCTURE REINFORCEMENT X/WSDR SWAA2026030566536Sill Drain · corrodedCORRODED LOWER SILL DRAIN, BS 440 - 492.4, RBL 21, WL 156. REPLACED THE SILL DRAIN AND FASTENERS IAW SRM 51-40-02, AND DWG 143A8330, SHEET 30, REV -.SDR REXA2026022300060Crossbeam · corrodedLEFT BS 280 CROSSBEAM CORRODED ON UPPER FLANGE BETWEEN BL 0 - LBL 11. REMOVED CORROSION ON THE CROSSBEAM IAW SRM 51-21-06-001-001-A01, DEEP PITTING IN ONE LOCATIONS WHERE UP TO 100% MATERIAL LOSS WAS FOUND. DUE TO THE EXTENT OF CORROSION, THE CROSSBEAM REQUIRESDR REXA2026022300058Crossbeam · corrodedRIGHT BS 280 CROSSBEAM CORRODED ON UPPER FLANGE BETWEEN BL 0 AND RBL 11. REMOVED SACRIFICIAL STRIP FROM FS 280 LB11 TO RBL11 TO GET ACCESS IAW SRM 51-42-06-001-001-A01. INSTALLED SAME SERVICEABLE SACRIFICIAL STRIP FROM FS 280 LBL 11 TO RBL 11 IAW SRM 51-42-06SDR R61A2026021600040Doubler · corrodedWHILE ON HEAVY CHECK - COCKPIT FLOOR DOUBLER ON CO-PILOTS SIDE BETWEEN FR FR 8-9 CORRODED AT MULTIPLE LOCATIONS.SDR DALA2026020500831Failsafe · corrodedDURING AN H-CHK AT STAG, CORROSION WAS NOTED ON THE FAIL SAFE AT BS 1197+154 BETWEEN S39L AND S39R. ER/A 631843-14 SECT. I REPAIR WAS ACCOMPLISHED. FOLLOW ON ACTION IS REQUIRED FOR DTE. ASSOCIATED ER/A 74-631843 ADDED FOR AC 1801 (1429898)SDR VNAA20260304021Pressure Deck · corrodedAFTER REMOVAL OF BLIND BOLT ON THE PRESSURE SILL DECK STEP 8, CORROSION FOUND AT SEVERAL BOLT HOLES. REPAIRED IAW REO 690-53-41-578. REV A.SDR DALA2026020200786Door Frame · crackedCRACKS FOUND AT THREE FASTENER HOLES, BS 1640 LT FUSELAGE FRAME, OUTER UPPER HOLE PRESENTS A CRACK ON THE FRAME WEB, OUTER ANGLE & HINGE FITTING AT 6 CLOCK; OUTER LOWER HOLE PRESENTS CRACKS ON THE FRAME WEB, OUTER ANGLE & HINGE FITTING AT 3 & 9 O`CLOCK, INNESDR SWIA2026012975720Window Post · dentedWINDSHIELD CENTER POST LOWER LH FITTING IS DENTED. (C-CHECK RO 04/16/2026)REMOVED AND REPLACED WINDSHIELD CENTER POST LH LOWER FITTING IAW SRM 51-42-21 COMPLETED TASK CARD 51-900-1003-SKY.SDR AALA202604144692Frame · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION ON FRAME 68LH SIDE, AT AFT GALLEY AREA, DOOR STOP 1, LOWER INBOARD HOLE, CRACK POSITION 7 OCLOCK VIEW LOOKING AFT, CRACK DEPTH: 0.100 INCHES APROX. MAINTENANCE ACCOMPLISHED TIME LIMITED REPAIR LOC FRAME 68 LH SIDESDR VNAA20260329018Crossbeam · corrodedCORROSION WAS FOUND ON CROSSBEAM WEB FS 349.0 BTW STGR17 LH TO STGR18 LH AT PASSENGER CABIN. CROSSBEAM WEB FS 349.0 BTW STGR17 LH TO STGR18 LH AT PASSENGER CABIN WAS REPAIRED PER REO 690-53-21-2094 REV -.SDR SWIA2026022375299Beam · corrodedCORROSION IN RT BEAM FR.87-88. REMOVED AND REPLACED RT BEAM IAW SRM 51-40-08.SDR SWIA2026022375298Beam · corrodedCORROSION IN LT BEAM FR.87-88. REMOVED AND REPLACED LT BEAM IAW SRM 51-40-08.SDR R61A2026021600043Window Post · damagedWHILE ON HEAVY CHECK - RT DV WINDOW POST HFEC ROTO TEST FOUND RELEVANT INDICATION DUE TO HOLE DAMAGE ON BOTTOM OF FASTENER HOLESDR SWAA2026021365575Crossbeam · crackedCRACKED CROSSBEAM, BS 540, RBL 2. REPLACED THE CROSSBEAM & FASTENERS IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, AND DWG 143A0060, SHEET 121, REV B.SDR UIEA2026012800018Torque Box · crackedAFT CARGO BS 1680 RT TORQUE BOX PANEL FOUND CRACKED. AFT CARGO BS 1660-1680, RBL 30" TO RBL 45.5" TORQUE BOX UPPER SKIN WEB REPLACED AND INSTALLED IAW SRM 51-10-02 AND SRM 51-40-2. NO FURTHER DEFECTS NOTED.SDR CALA2026020213489Window Frame · damagedLOUD SQUEALING COMING FROM FO FRONT WINDOW AREA. DEBRIEFED CREW SQUEALING COMING FROM RIGHT SIDE OF FO FRONT WINDOW IMAGE LABOR UPDATE R2 WINDOW LEAKING FROM THREE DIFFERENT ARES, VERIFIED LEAKS. REMOVED R2 WINDOW TO INSPECT PRESSURE SEAL. FOUND SEAL FLAT SDR DALA2026020100737Door Frame · crackedAD RELATED, A.A. 5311-01216-04, AFT PASSENGER/CREW DOOR, FR68 LT, DOOR STOP FITTING NR 1, HOLE NR 4 (DIA. 0.250") HAD A CRACK INDICATION AT FRAME LAYER. EVALUATE & REPAIR IAW SRM 53-41-12. PERFORMED FREEZE PLUG REPAIR AT FR 68 DOOR FRAME STOP FITTING NR 1 HOSDR DALA2026013000729Fitting · corrodedCORROSION CENTER FITTING LOCATED BTW FR 16 TO FR 20 LH SIDE CUT OUT AT FWD GALLEY AREA (SSI 531189). REPLACED CENTER FITTING LOC. BTW FR 16 TO FR 20 LH SIDE CUT OUT AT FWD GALLEY AREA AS PER A320 SRM 51-42-11, A320 SRM 51-72-11 AND DWG D53112109 RELEASE DATE:SDR DALA2026020300803Splice Plate · brokenFOUND SPLICE PLATE BROKEN P/N CO2386047-101 REMOVED DAMAGED SPLICE PLATE. INSTALLED SPLICE PLATE P/N C02386047-101 IAW A220 AMM 53-82. (LP# 1424461)SDR FDEA202601280097Crossbeam · misrepairedEXISTING REPAIR ON MDCC CROSSBEAM LOWER FLANGE AT FR60 BETWEEN -Y1456 AND -Y1959 REQUIRES EVALUATION FOR CONFORMITY THE EXISTING REPAIR ON MDCC CROSSBEAM LOWER FLANGE AT FR60 BETWEEN -Y1456 AND - Y1959. NO RECORD FOUND. REMOVED THE EXISTING REPAIR AND RE-RESDR YENA2026012900084Door Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION ON EMERGENCY EXIT DOOR 843 INSIDE OF INNER FRAME SEGMENT 1 IN PASSENGER CABIN (CRACK L:0.45"); REF AEROMAN WO 2025 415/1 NR 2025-750909; REMOVED AND REPLACED FRAME SEGMENTS ON EMERGENCY EXIT DOOR 843, IAW EC A320-52-1SDR YENA2026012900083Door Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION ON EXIT DOOR 834 INSIDE OF INNER FRAME SEGMENT 1 IN PASSENGER CABIN ( CRACK L= 0.590"); REF AEROMAN WO 2025 415/1 NR 2025-750908; REMOVED AND REPLACED FRAME SEGMENTS ON THE EMERGENCY DOOR 834 IAW A320-52-1144 AND SRM
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