JASC 5310
Service difficulty reports · 38,479
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 ASAA2026052966880Skate Angle · crackedCENTER WING AFT SPAR VAPOR BARRIER SKATE ANGLE SHOWS SIGNS OF BEING CRACKED AT BS.661.95 RBL+9. GROUNDED - YES. ACCOMPLISHED REAR SPAR VAPOR BARRIER ATTACH ANGLE REPAIR IAW SRM 57-10-10-2R-5 REPAIR 5.SDR MASA20260608152Crossbeam · corrodedDURING HEAVY CHECK INSPECTIONS OF THE INTERNAL FUSELAGE CFI FLOOR STRUCTURE, FWD FUSE CROSS BEAM FR 17 SMALL SPOTS OF CORROSION ON UPPER FLANDGE BETWEEN RBL 15 AND RBL 33 REPAIRED IAW SRM 53-00-10, REP 03. SEE AWS AND NDT REPORT TWO 47519-4 FOR DETAILS "NO CRASDR AALA202606037046Crossbeam · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN PASSENGER CABIN FLOOR SUPPORT BREAK ASSEMBLY PANEL AT STA 540 AND LBL 2. REPLACED BREAK ASSEMBLY PANEL PER SRM 51-10-02.SDR DALA2026060103311Door Sill · corrodedLEVEL 2 CORROSION, AFT PASSENGER CABIN, LH DOOR LOWER CUT OUT SILL BEAM AREA CENTER ANGLE WITH CORROSION. REPLACED (SHAPE) CENTER ANGLE P/N: D5348004820203 AT AFT PASSENGER CABIN L/H DOOR LOWER CUT OUT SILL BEAM IAW A320 SRM 51 -72-11-911-001 REV 157.00 DATEDSDR DALA2026053103299Stop Fitting · damagedEXISTING REPAIR FR68, INNER CAP & FR FLANGE, STRG 22 RH AT LEVEL DOOR STOP FITTING 1. CONTACT DELTA LIAISON ENGINEERING FOR ALTERNATE INSPECTION INSTRUCTIONS THAT MAY BE REQUIRED TO COMPLETE WORK CARD 5311-0124 4-02B DUE TO PREVIOUS REPAIR IN THE INSPECTION ARSDR DALA2026053103290Door Sill · corrodedLEVEL 2 CORROSION, AFT PASSENGER CABIN, AFT R/H DOOR CUTOUT AT Y-1235MM FR68 SILL BEAM WITH CORROSION. FOUND DURING PROCESS WITH ORNRC 200- 278. PERFORMED REPAIR AFT PASSENGER CABIN AFT RH DOOR CUT OUT SILL BEAM BETWEEN FR 67 +335MM AND FR 68 +35MM I/A/W A32SDR HNAA2026070300570Door Sill · corrodedCARGO DOOR CUTOUT LOWER SILL CORRODED ON FORWARD END. R & R CARGO DOOR CUTOUT LOWER SILL IAW SRM 51-40-02.SDR AALA202606283815Door Sill · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT RIGHT PASSENGER / CREW DOOR CUT OUT LOWER SILL AT FR 66 AND S23R. REPLACED LOWER SILL PER SRM 51-42-11.SDR MASA20260608157Beam · corrodedDURING HEAVY CHECK INSPECTIONS OF R1 DOOR CUT-OUT LOWER BEAM ON SLIDE FITTING FWD HOUSING EDGE CORROSION REMOVED BY BLENDING !AW SRM 51-10-03, BLENDED AREA FOUND WITH IN LIMITS IAW SRM 53-10-11 AD 02, DUI WITH 10X MAG GLASS C/OUT, "NO FAULT FOUND" BLENDED AREASDR MASA20260608156Beam · corrodedDURING HEAVY CHECK INSPECTIONS OF L1 DOOR CUT-OUT LOWER BEAM ON SLIDE FITTING FWD HOUSING EDGE CORROSION REMOVED BY BLENDING IAW SRM 51-10-03, BLENDED AREA FOUND WITH IN LIMITS IAW SRM 53-10-11 AD 02, DUI WITH 10X MAG GLASS C/OUT, NO FAULT FOUND, BLENDED ARESDR MASA20260608151Crossbeam · corrodedDURING HEAVY CHECK INSPECTIONS OF CFI WET AREA, FWD FUS CROSS BEAM, FR 14, RBL 18, SPOT OF CORROSION ON UPPER FLANGE EDGE REMOVED BY BLENDING IAW SRM 51 10 03, FOUND TO BE WITH IN LIMITS IAW SRM IAW 53 SRM 10 10, 51 23 AD02. 04, DVI WITH 10X 23 05, MAG C/OUSDR DALA2026053103295Window Frame · cracked*DTE* DURING M2 AND WHILE INSPECTING PER EM 5311-01236-01 CRACK INDICATIONS FOUND IN LH LATERAL WINDOW FRAME UPPER JUNCTION FASTENER HOLE #1 AND HOLE #3. *DTE* PER SECTION DTE OF 633473-14, THE REPAIR OF SECTION I IS LIMITED TO 20,700 FC FROM SECTION I (18MAYSDR DALA2026053103285Window Frame · crackedCRACK INDICATION FOUND IN OPEN FASTENER HOLE LOCATED ON FRAME 4 LATERA L WINDOW UPPER JUNCTION RT SIDE. CRACK DEPTH: 0.078 INCH, CRACK DIRECTION: 3 O`CLOCK VIEW LOOKING FWD. REPAIR MUST BE ACCOMPLISHED PRIOR TO FURTHER FLIGHT. A.A 5311 -01236-02. COMPLIED WISDR DALA2026052903266Box Beam · corrodedCORROSION ON BOXBEAM FROM STA 1660 TO STA 1680 RBL 54 AT PASSENGER CABIN FLOOR. CORROSION LEVEL 2. BOXBEAM FROM STA 1660 TO STA 1680 RBL 54 AT PASSENGER CABIN FLOOR WAS REPLACED PER B757-300 SRM 51-40-02-0G PAR 7 D. (1617683) AIRCRAFT WAS GROUNDEDSDR DALA2026052803240Window Frame · crackedAIRCRAFT 3236, CRACK INDICATION FOUND (1 EA) ON RH CONTINUITY FITTING OF THE WINDSHIE LD LOWE R ATTACHMENT AREA, L= 0.118 INCH APPROX. (AD 2020-17-03 WORK CARD 5311-01226-01.) CORRECTIVE ACTION: PERFORMED REPAIR INSTRUCTIONS ON WINDSHIELD CENTER POST; LH AND RSDR DALA2026052803239Window Frame · crackedAIRCRAFT 3236, CRACK INDICATION FOUND ON LH CONTINUITY FITTING OF THE WINDSHIELD LOWE R ATTACHMENT AREA, L=0.118 INCH APPROX. (AD 2020-17-03 WORK CARD 53 11-01226-01.) CORRECTIVE ACTION: PERFORMED REPAIR INSTRUCTIONS ON WINDSHIELD CENTER POST; LH AND RH FRONT SDR DALA2026052803238Window Frame · crackedAIRCRAFT 3236, CRACK INDICATION FOUND ON LH CONTINUITY FITTING OF THE WINDSHIELD LOWE R ATTACHMENT AREA, L= 0.118 INCH APPROX. (AD 2020-17-03 WORK CARD 53 11-01226-01.) CORRECTIVE ACTION: PERFORMED REPAIR INSTRUCTIONS ON WINDSHIELD CENTER POST; LH AND RH FRONTSDR DALA2026052803230Window Frame · crackedAIRCRAFT 3236, DURING M2 CHECK AT AEM (SAL), WHILE EXECUTION OF HFEC INSPECTION OF THE WINDSHIELD CENTRAL NODE CONTINUITY FITTINGS AND WINDSHIELD FRAMES ON LH AND RH SIDES AS PER JOB CARD 5311-01226-01 (IN ORDER TO COMPLY WITH FAA AD 2020-17-03 AND SB A320-53-SDR SWAA2026062307127Pressure Deck · crackedCRACK INDICATION FOUND ON HORIZONTAL PRESSURE DECK WEB AT LBL 31 BETWEEN BS 663 TO BS 675 IN THE MAIN WHEEL WELL. PERFORMED A PERMANENT REPAIR LOC ON HORIZONTAL PRESSURE DECK WEB IAW SRM 53-40-51-2R-2, REPAIR 2.SDR SWAA2026062207276Pressure Deck · crackedCRACK INDICATION ON HORIZONTAL PRESSURE DECK BETWEEN BS 663 TO 675, RBL 42. PERFORMED A PERMANENT REPAIR ON THEHORIZONTAL PRESSURE DECK BTW RBL30 TO RBL60 AND BTW BS 663 - 675 AT PASSENGER CABIN IAW SRM 53-40-51-2R-2, REPAIR 2.SDR IPXA2026060273867Seal Depressor · deformedFOUND MAIN DECK SIDE CARGO DOOR UPPER - AFT SIDE DEPRESSOR SEAL DEFORM AND SCRATCH. INSTALLED THE DEPRESSOR SEAL. IAW AMM I.A.W AMM 20-11-00-910-802 REV.148.TORQUED THE SCREW TO 35 IN-LB. CONDITION CHECK NORMAL.SDR DALA2026053103294Fitting · cracked*DTE* DURING M2 WHILE INSPECTING PER EM 5311-01226-01, THE RHS CONTINUITY FITTING WAS FOUND CRACKED. FURTHER INSPECTION REVEALED HOLES D1 ON RH AND LH SIDES WERE ALSO CRACKED IN FRONT WINDSHIELD LWR CTR NODE AREA. C/A: *DTE* PER SECTION DTE OF 633637-14AD THE SDR DALA2026053103293Fitting · crackedDURING M2 AND WHILE INSPECTING PER EM 5311-01226-01, THE RHS CONTINUITY FITTING WAS FOUND CRACKED. FURTHER INSPECTION REVEALED THAT HOLES D1 ON RH AND LH SIDES WERE ALSO CRACKED IN FRONT WINDSHIELD LWR CTR NODE AREA. PER SECTION II OF 633637-14AD, ACCOMPLISH SDR DALA2026053103292Fitting · crackedDURING M2 AND WHILE INSPECTING PER EM 5311-01226-01, THE RHS CONTINUITY FITTING WAS FOUND CRACKED. FURTHER INSPECTION REVEALE D THAT HOLES D1 ON RH AND LH SIDES WERE ALSO CRACKED IN FRONT WINDSHIELD LWR CTR NODE AREA. PER SECTION II OF 633308-14AD, ACCOMPLISHSDR DALA2026052803235Stop Fitting · scratchedAIRCRAFT 3251, UPPER FUSELAGE PAX CABIN BETWEEN FR15 AND FR16 R/H SIDE AT STOP FITTING #1, INTERCOSTAL WITH SCRATCHES AND TOOL MARK. CORRECTIVE ACTION: ACCOMPLISHED INTERCOSTAL REPLACEMENT AT FR16 RH DOOR STOP #1 IAW ER/A #589110-14AD REV A. (LP 1615986 - AIRCSDR DALA2026052803231Window Frame · brokenDURING THE M2 CHECK (D CHECK) AT COO (SJO), AND WHILE EXECUTING A DELTA TASK CARD INSTRUCTIONS RELATED TO SB A320-53-1331 R01 AND AD 2020-17-03, THE LT CONTINUITY FITTING AND WINDSHIELD FRAMING WITH CRACK WERE FOUND. CORRECTIVE ACTION: PERFORMED WINDSHIELD FRASDR HDNA2026FA0000445Frame · crackedFRAME 5 CRACK FOUND WHILE CONDUCTING A 1000H SCHEDULED INSPECTION. REPAIRED WITH APPROVED DATA FROM THE AIRCRAFT MANUFACTURER.SDR 4VAA202605260040Door Frame · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE LEFT OVERWING EMERGENCY EXIT BOTTOM FRAME. THE FRAME WAS REPLACED IN ACCORDANCE WITH SRM 51-40-21/22.SDR MASA20260608149Doubler · corrodedDURING HEAVY CHECK INSPECTIONS OF INTERNAL FUSELAGE FWD FLOOR STRUCTURE AT CFI, FWD CABIN,CORROSION FOUND ON DOUBLER AT BETWEEN FR 19-FR20 LT AND BETWEEN LBL 19 AND LBL20 REMOVED AND REPLACED IAW SRM 51-41-02, AND SRM 51-43-04. REV 45, CORROSION LEVEL 2SDR DALA2026052903255Door Frame · corrodedCORROSION AROUND LOWER DOOR JAMB AT AFT CARGO COMPARTMENT. REPAIRED IAW SRM 51-41-02-0G AND SRM 51-41-05-0G AND PER B717-200 SRM 53-20-15. (1614443) (AIRCRAFT GROUNDED)SDR CALA2026052916646Pressure Deck · crackedCRACK FOUND AT BEADED PRESSURE DECK WEB BS 663.75, RBL 41. REPAIRED BEADED PRESSURE DECK WEB IAW SRM 53-40-51-2R-2, PARAGRAPH 4.C.(3)(A), FIGURE 202.SDR 21GA2026052623806Window Frame · crackedWINDOW FRAME AT STATION 944 LH SIDE IS CORRODED AT CENTER OF LOWER EDGE. (MAJOR REPAIR)SDR SWIA2026052576896Door Sill · corrodedAFT BAGGAGE DOOR OPENING SILL BETWEEN BS 574 - 605 WAS CORRODED. REPLACED AFT BAG BAY DOOR SILL IAW REO 601R-53-61-8559, REV--. & GREO 601R-53-61-690, REV D. COMPLETED SKYWEST TASK CARD 51-900-1003-SKY.SDR SWAA2026061506379Crossbeam · crackedCRACKED BRAKE PANEL, BS 540, BTW BL 0 - LBL 24.75. REPLACED THE BRAKE PANEL IAW SRM 51-40-02 AND DWG 143A0060, SHEET 36, REV A.SDR SWAA2026061506380Crossbeam · crackedCRACK BRAKE PANEL LOCATED BS540 BTW BL0 TO RBL 24.75 AT PASSENGER CABIN. REPLACED BRAKE PANEL LOCATED BS540 BTW BL0 TO RBL 24.75 AT PASSENGER CABIN IAW B737-700 SRM 51-40-02 AND DWG 143A0060 SHEET 36 REV A.SDR DALA2026052703204Fitting · damagedBURRED MATERIAL (OVALIZATION) ON LOWER LATERAL FITTING LT SIDE RACK 80VU ADDITIONAL ENGINEERING DOCUMENTATION IS REQUIRED PRIOR TO FURTHER FLIGHT REFER TO AA CARD 2515-01014-02A AD RELEATED. COMPLIED WITH ER/A 633192-14AD REV. ORIGINAL APPROVED DATE 23- MAY-2SDR REXA2026080401425Door Frame · corrodedCORROSION ON ANGLES STA= 847+32 BTW STG 17RH TO 17 LH. CORROSION ON ANGLES BTW STA= 847+32 AND 847+64 AND RBL=18 AND LBL=18. CORROSION ON ANGLE STA= 794 BOTTOM SIDE AND RBL=46 LBL=46 ANGLES STA= 847+32 BTW STG 17RH TO 17 LH, ANGLES, STA= 847+32 ANDSDR REXA2026080401424Door Frame · corrodedCORROSION ON ANGLES BS 847+32 BTW STG 17R TO 17L. CORROSION ON ANGLES BTW BS 847+32 & 847+64 AND RBL 18 LBL 18. CORROSION ON ANGLE BS 794 BOTTOM SIDE AND RBL 46 LBL 46. CORROSION ON ANGLES BS 847+32 BTW S17R TO 17L. CORROSION ON ANGLES BTW BS 847+32 & SDR 2026FA0000444Structure · degradedAPPROXIMATELY 8 SECONDS AFTER DROID RESTOWING AND SHORTLY AFTER CLIMBING FROM DELIVERY ALTITUDE, ONE PROPELLER CONTACTED AN OBJECT AND BRIEFLY SLOWED BEFORE RECOVERING. ABOUT 1.25 SECONDS LATER, THE SAME PROPELLER EXPERIENCED A SECOND IMPACT AND STOPPED COMPLESDR CALA2026052516516Panel · corrodedNLG WHEEL WELL PANEL 114BW HAS SURFACE CORROSION ADJACENT TO ATTACHMENT FASTENER. EVALUATED PANEL ASSY TO BE BEYOND REPAIRABLE LIMITS IAW B737 SRM 53-10-14. RECEIVED REPLACEMENT PANEL AIPC 32-22-11-02 ITEM 35 FOR EFFECTIVITY. EVALUATED PANEL ASSY TO BE BEYSDR VNAA202608010011Door Frame · corrodedCORROSION ON BULKHEAD DOOR POSTS LOWER SECTION AT FS280.00 (LBL12 & RBL12). BULKHEAD DOOR POSTS LOWER SECTION AT FS280.00 LBL12 & RBL12 WAS EVALUATED FOUND EXCESSIVE DAMAGE PER CRJ 900 SRM 51-10-06-001-001-A01 AND BULKHEAD DOOR POSTS LBL12 & RBL12 WERE REPAISDR CALA2026060116682Door Sill · corrodedCORROSION ON INNER CHORD AT R1 DOOR CUTOUT LOWER SILL. REMOVED AND REPLACED R1 DOOR LOWER SILL INNER CHORD PER SRM 51-40-02-0G-0 AND DWG 141A8310. REMOVED AND REPLACED R1 DOOR LOWER SILL INNER CHORD PER SRM 51-40-02-0G-0 AND DWG 141A8310.SDR DALA2026052703213Window Frame · damagedDURING M2 AND WHILE INSPECTION PER EM 5311-01236-02, CRACK FOUND IN THE UPPER JUNCTION FASTENER HOLE OF FR4 LATERAL WINDOW FRAME, RHS, AT THE INTERFACE WITH RHS FRONT WINDSHIELD FRAME. PER SECTION DTE OF 633157-14AD THE REPAIR OF SECTION I IS LIMITED TO 26,60SDR DALA2026052703203Fitting · cracked*DTE* DURING M2 AND WHILE ACCOMPLISHING EM 5311-01246-01, BOTH LH/RH CONTINUITY FTGS FOUND CRACKED AND ALSO FRONT WINDSHIELD FRAME HOLE D1 CRACKED. C/A: *DTE* PER SECTION DTE OF 633213-14AD, THE REPAIR OF SECTION I IS LIMITED TO 60,000 TOTAL FC (FROM A/C FIRSTSDR UIEA2026040600129Support Frame · cracked1EA FASTENER HOLE CRACK FOUND ON LH SUPPORT FRAME CRACK 4 O'CLOCK APPROX 0.020" IN DEPTH(<P>CRACK FASTENER HOLE REPAIRED AS PER RI-53-80-18195 REV A. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2026040600130Support Frame · cracked1EA FASTENER HOLE CRACK FOUND ON LH SUPPORT FRAME CRACK AT BS 2598 6 O'CLOCK POSITION, APPROX 0.020" IN DEPTH(<P>CRACK FASTENER HOLE REPAIRED AS PER RI-53-80-18195 REV A. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2026041500184Beam · cracked1EA CRACK WAS FOUND ON BEAM RUNNING AFT AT BS260-280 WL 170 LH NOSE WHEEL WELL SIDE PANEL(<P>CRACK BEAM REPLACED AS PER SRM 51-10-02 AND NEW BEAM INSTALLED AS PER SRM 51-40-02. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2026050400290Panel · damagedM/D STA 1720 TO 1780 LH DADO PANEL FOUND DAMAGED(<P>DADO PANEL REPAIRED AS PER RI-25-21-18164 REV A. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2026050400291Panel · damagedM/D STA 1620 TO 1720 LH DADO PANEL FOUND DAMAGED(<P>DADO PANEL REPAIRED AS PER RI-25-21-18163 REV A. NO FURTHER DEFECTS NOTED</P>)SDR DALA2026052603153Structure · damagedDIV- FLIGHT EXPERIENCED BIRD STRIKES ON CLIMB OUT OF CPH AND DIVERTED INTO CDG AFTER WEATHER RADAR FAIL. CDG CONDUCTED BIRD STRIKE INSPECTIONS. MULTIPLE DAMAGE REPAIRS. (8361259) (AIRCRAFT GROUNDED)
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