JASC 5310
Service difficulty reports · 38,511
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 JR2R20260221298Doubler · corrodedFWD WET AREA, RT BANJO DOUBLER AT RBL40 FR17 IS CORRODED AT FWD END. REPAIRED PER ETD.SDR AALA202602266476Crossbeam · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN PASSENGER CABIN FLOOR STRUCTURE BREAK ASSEMBLY PANEL AT BS 540 AND RBL 24. REPLACED BREAK ASSEMBLY PANEL PER AARD 51-00-05-1.SDR CALA2026022313983Door Frame · corrodedL2 DOOR CUTOUT INNER CHORD WITH SEVERAL CORROSION SPOTS. REMOVED AND REPLACED L2 INNER CHORD IAW SRM 51-40-02-0G-0 AND DWG 147A8501.SDR AALA202602205962Crossbeam · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN PASSENGER CABIN CROSSBEAM AT BS 540, RBL 3. REPLACED CROSSBEAM IAW SRM-51-40-02-0G.SDR AALA202602205083Crossbeam · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN PASSENGER CABIN CROSSBEAM AT BS 540, LBL 3. REPLACED CROSSBEAM IAW SRM-51-40-02-0G.SDR SWAA2026032472502Pressure Deck · crackedCRACK INDICATION FOUND ON THE HORIZONTAL PRESSURE DECK, LBL 31, BS 663 - 675 IN THE MAIN WHEEL WELL. PERFORMED CATEGORY A REPAIR IAW SRM 53-40-51-2R-2, REPAIR 2.SDR SWAA2026031972308Crossbeam · crackedCRACKED CROSSBEAM, BS 540, RBL 24.75 - RBL 45.5. REPLACED THE CROSSBEAM IAW SRM 51-40-02, SRM 51-10-02, STEP 9, & DWG 143A0060, SHEET 36, REV A.SDR IPXA2026031499159Retainer · corrodedMAIN DECK FLOOR AREA STA 1620-1640 LBL 62 ANGLE BAR SURFACE BULGING AND FASTENER HEAD FULL THROUGH SIGN OF CORROSION. INSTALLED NEW ANGLE BAR FASTENER RETAINER AT MAIN DECK FLOOR AREA STA 1620-1640 LBL 62 IAW SRM 51-40-02-0G-0.SDR ASAA2026021964791Transition Panel · corrodedAFT CARGO RH TRANSITION PANEL HAS CORROSION BETWEEN STATIONS 727I TO FWD BULKHEAD. GROUNDED - YES. REMOVED CORROSION BETWEEN 727I - FWD BULKHEAD. ORIG. THICKNESS .040, MAT LOSS AT GREATEST .008, NEW THICKNESS AT LOWEST .032. AREAS OUT OF LIMITS PER B737-900 SRSDR REXA2026030900222Door Sill · corrodedCORROSION ON LOWER SILL ALSO ON SETTLEMENT AREA OF CARGO FLOOR 281JLF AT AFT BAGGAGE BAY DOOR CUT-OUT SURROUND STRUCTURE. DUE TO EXCESSIVE DAMAGE LOWER SILL OF AFT CARGO MUST BE REPLACE PER CRJ900 SRM 51-10-06-001-001-A01, SRM 51-42-21-001-001-A01, SRM 51-42-1SDR AALA202602229151Door Frame · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK VERTICAL FRAME ON EMERGENCY EXIT DOOR 844 IN PASSENGER CABIN (L=0.490 IN) MAINTENANCE REPLACED VERTICAL FRAME AND FASTENER (SEGMENT FRAME LOWER FWD LH) ON EMERGENCY EXIT DOOR 844 IN PASSENGER CABIN IAW A320 SRM 51-42-11-801SDR DALA2026022001232Fitting · crackedAIRCRAFT 3131, FLIGHT DECK, WINDSHIELD FRAMING, LT / RT CONTINUITY FITTING CRACKED. CORRECTIVE ACTION: REPLACED CONTINUITY FITTINGS (LH P/N D53111077202009) (RH P/N D5311107720300) IAW DELTA ERA 631770-14AD REV ORIGINAL DATED 10-FEB-26 AND REPAIR DWG R531-1291SDR IPXA2026032973627Structure · corrodedAFT CARGO- FR 54.2 CEILING STRUCTURE HAS CORROSION, 46 PLACES FROM LH TO RH SIDE. REMOVED CORROSION ON CEILING STRUCTURE (03 SECTION) ON FR 54.2FROM LT TO RT SIDE. IAW SRM 51-74-10. INSTALLED NEW CEILING STRUCTURE IAW SRM 51-40-21.SDR WRNA202603190003Door Frame · puncturedDURING INSPECTION OF AFT CARGO DOOR, FOUND FRAME PUNCTURE HOLE AND CRACK ON AFT SECTION OF CARGO DOOR SKIN.SDR WRNA202603190002Spar · corrodedLOWER FUSELAGE AT LH AND RH FWD SPAR OF CENTER TANK AT STA. 987 (APROX), SHOWS CORROSION.SDR QXEA2026031800058Sill Drain · corrodedAFT WET AREA RH MOP SILL IS CORRODED AT FRAME 88-89 RBL 36-40. BLENDED CORROSION AND MATERIAL LOSS WAS 100% AND OUT OF LIMITS. REPLACED THE SILL IAW E175 SRM 51-40-08.SDR DALA2026021901208Box Beam · corrodedCORROSION ON BOX BEAM BTW BS 700 - 720, LBL 62 APPROX ON SETTLEMENT FLOOR PANELS UPPER/LOWER AREA AT PASSENGER CABIN. GUTTER SUPPORT WAS FABRICATED IAW DWG 143N5410 REV A. AND GUTTER SUPPORT BTW BS 700 - 720, LBL 60 APROX AT PASSENGER WAS INSTALLED IAW SRM SDR DALA2026021901201Strap · crackedAIRCRAFT 9585, CRACK ON STRAP BTW UPPER PYLON LH AND Y=1178 AT AFT FUSELAGE AREA. CORRECTIVE ACTION: STRAP BTW UPPER PYLON LH AND Y=1178 AT AFT FUSELAGE AREA WAS REPAIRED PER PRI 631710-14 REV 0 TO REV. 11 AND ER/A 631710-14. (LP 1457499)SDR CALA2026021913913Structure · corrodedSIGNS OF CORROSION FOUND AT INNER CHORD UPPER SURFACE APROX. BS 1459, S17R. SEE N/R 003197679 FOR ALL WORK PERFORMED.SDR 2026F00013Spar · corrodedLOWER FUSELAGE CENTER WING, FRONT SPAR AT STA RBBL 127.50, LOWER PANEL CORROSION.SDR JR2R20260218704Crossbeam · corrodedAFT WET AREA FR 84 CROSSBEAM HAS CORROSION AT APPROX LBL 24. REPAIREDSDR JR2R20260218696Gusset · corrodedAFT WET AREA SPLICE GUSSET AT FR 90 BL 0 CORRODED. REPLACEDSDR JR2R20260218695Sill Drain · corrodedAFT WET AREA LT MOP SILL AT LBL 36 FR 88 - 90 CORRODED. REPLACEDSDR JR2R20260218701Sill Drain · corrodedAFT WET AREA RT MOP SILL AT FR 84, RBL 36 CORRODED. REPLACEDSDR SWIA2026021776587Window Frame · crackedPILOTS SIDE WINDSHIELD SIDE POST LOWER OUT BOARD CLIP CRACKED. REMOVED CRACKED CLIP AND INSTALLED NEW OUTBOARD CLIP AT PILOTS SIDE WINDSHIELD LOWER POST IAW SRM 51-42-21-001-001-A01, AND DWG CC670-33055 REV -F. COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKYSDR SWIA2026021775719Pressure Deck · corrodedLEFT PRESSURE FLOOR SKIN IS CORRODED AT (1EA) LOCATION AT F.S. 529.00. REPAIRED LH PRESSURE FLOOR SKIN AT FS529.00 IAW REO 601R-53-41-666 REV-C DATED 2012-11-06 06 COMPLETED TASK CARD 51-900-1003-SKY .SDR SWIA2026021775717Pressure Deck · corrodedRIGHT PRESSURE FLOOR SKIN IS CORRODED AT (2EA) NUTPLATE LOCATIONS BETWEEN F.S. 499.00 AND F.S .513.00. (C-CHECK RO 04/16/2026)REPAIRED R/H PERESSURE FLOOR SKIN AT 2EA NUTPLATE LOCATIONS BETWEEN FS499.00 AND FS513.00 IAW REO 601R-53-41-666 REV-C DATED 2012-11SDR SWIA2026021775707Pressure Deck · corrodedRIGHT PRESSURE FLOOR SKIN CORRODED AT ONE LOCATION BETWEEN BS 544 - 559. REPAIRED RT PRESSURE FLOOR SKIN IAW REO 601R-53-41-666, REV-C.SDR SWAA2026032371371Pressure Deck · crackedCRACK INDICATION ON THE HORIZONTAL PRESSURE DECK, LBL 36, BS 663. PERFORMED A CATEGORY B REPAIR, ON HORIZONTAL PRESSURE DECK IAW SRM 53-40-51-2R-2, REPAIR 2, EA 26-153-00558-WIP1, AND EA26-153-00558.SDR SWAA2026032371582Crossbeam · crackedCRACKED CROSSBEAM, BS 540, BTWN RBL 24.75 - RBL 45.5. REPLACED THE CROSSBEAM IAW SRM 51-40-02, SRM 51-10-02, PARAGRAPH 9, & DWG 143A0060, SHEET 46, REV -.SDR SWAA2026031971574Pressure Deck · crackedCRACK INDICATION ON HORIZONTAL PRESSURE DECK WEB LBL 35 STA 663 AT PASSENGER CABIN (1E/A). CRACK LENGTH 0.150 INCH APPROXIMATELY. PERFORMED REPAIR ON HORIZONTAL PRESSURE DECK WEB LBL 30 TO LBL 62 STA 663 TO STA 675 AT PASSENGER CABIN AND FASTENERS IAW B737-7SDR IPXA2026030956993Drain Mast · corrodedRIGHT AFT FUSELAGE RT APU EXHAUST CONE DRAIN MAST BASE EXFOLIATED. REMOVED CORROSION AT RT AFT FUSELAGE AT APU EXHAUST DRAIN MAST BASE IAW SRM 51-10-02-0G-0. INSTALLED DRAIN MAST FROM RT AFT FUSELAGE RH APU EXHAUST CONE IAW IAW AMM 28-25-05-404-162.SDR QXEA2026022400041Beam · corrodedAFT CARGO DOOR CUTOUT LOWER BEAM FORWARD SIDE IS CORRODED. REWORK OUT OF LIMITS. CORROSION LOCAL LEVEL 2. REPAIRED IAW ETD 2026-170-002252.SDR AALA202602223220Window Frame · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK LOCATION FOUND ON WINDSHIELD CENTER POST LOWER ATTACHMENT AREA LOWER RADIUS LH SIDE L=0.590 IN. MAINTENANCE PERFORMED TIME LIMIT REPAIR ON WINDSHIELD CENTER POST LOWER ATTACHMENT AREA LOWER RADIUS LH SIDE ADJACENT AT UPPER TSDR AALA202602228171Window Post · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION FOUND ON WINDSHIELD CENTER POST LOWER ATTACHMENT AREA UPPER RADIUS LH SIDE ADJACENT AT UPPER TENSION BOLT L=0.118 IN. MAINTENANCE PERFORMED TIME LIMIT REPAIR ON WINDSHIELD CENTER POST LOWER ATTACHMENT AREA UPPER RSDR AALA202602223426Window Frame · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION FOUND IN WINDSHIELD CENTER POST LOWER ATTACHMENT AREA UPPER RADIUS RH SIDE ADJACENT AT UPPER TENSION BOLT L= 0.197 IN. MAINTENANCE PERFORMED TIME LIMIT REPAIR ON WINDSHIELD CENTER POST LOWER ATTACHMENT AREA UPPER SDR SWAA2026022071807Door Frame · corrodedCABIN AFT LEFT LAVATORY SHOWS EVIDENCE OF CORROSION AT INBD AFT LAV POST. REMOVED CORROED PORTION OF FRAME ASSY AT AFT LT LAV INBD AFT POST AND REPLACED WITH A SERVICIABLE PART IAW CMM 25-48-25 PAGE 607.03. OPERATED LAV DOOR; OP CHECKED GOOD.SDR DALA2026021801141Box Beam · corrodedCORROSION OUT OF LIMITS. IN REF NRC 423: CORROSION ON BOX BEAM BTW STA 1660-1680 AND LBL 55 AT PASSENGER CABIN IS OUT OF LIMITS PER B757-300 SRM 53-00-51-1A PROCEDURE 1 AD 1. FIG. 101 DETAIL VI SECTION B-B. NEW BOX BEAM WAS REPLACED ON BTW STA 1660- 1680 ANDSDR AALA202602228791Fitting · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION FOUND ON LH CONTINUITY FITTING ON WINDSHIELD LOWER ATTACHMENT AREA L: 0.157 IN. MAINTENANCE REPLACED LH CONTINUITY FITTING OF THE WINDSHIELD CENTER POST LOWER ATTACHMENT INTERNAL AREA IAW EA 370750 AND A319 SRM 51SDR AALA202602224401Fitting · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION FOUND ON RH CONTINUITY FITTING ON WINDSHIELD LOWER ATTACHMENT AREA L: 0.157 IN. MAINTENANCE REPLACED RH CONTINUITY FITTING OF THE WINDSHIELD CENTER POST LOWER ATTACHMENT INTERNAL AREA IAW EA 370750 AND A319 SRM 5SDR DALA2026021901219Structure · damagedUNREPAIRED EXISTING HOLES DIAMETER EQUAL TO OR GREATER THAN MINIMUM STARTING HOLE DIAMETER WAS FOUND. ON HOLES H1: 0.2634 IN , H2: 0.3321IN, H7: 0.2017 IN, H8: 0.2920 IN, HA:0.2027 IN, HB: 0.2620 IN, HC: 0.2030 IN, HD : 0.2631 IN, H9: 0.2032 IN, H10: 0.2631 INSDR AALA202602190322Door Sill · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CARGO COMPARTMENT DOOR CUTOUT LOWER SILL INNER CHORD BETWEEN BS 560 AND BS 571 AT RBL 60. REPLACED CHORD PER SRM 51-40-02-0G.SDR SWAA2026032371181Crossbeam · crackedCRACKED CROSSBEAM, BS 540 BTWN BL 0 - LBL 24.75, WL 208.1. REPLACED THE CROSSBEAM IAW SRM 51-10-02, ITEM 9, & SRM 51-40-02.SDR SWAA2026032371180Crossbeam · crackedCRACKED CROSSBEAM, BS 540 BTWN BL 0 - RBL 24.75, WL 208.1. REPLACED THE CROSSBEAM IAW SRM 51-40-02, & SRM 51-10-02, PARAGRAPH 9.SDR CALA2026030914406Floor Skin · dentedCOCKPIT AFT OF PEDESTAL FLOOR PANEL, SKIN HAS SEVERAL DENTS AND BARE METAL. REPAIRED COCKPIT FLOOR SKIN IAW REO-G25794, REV IR, & EC/RA 5310-08803.SDR CALA2026030914404Pressure Web · crackedREAR SPAR VERTICAL PRESSURE WEB BETWEEN LBL 45.64 AND LBL 40.00 CRACKED. REPAIRED CENER WING REAR SPAR VERTICAL PRESSURE WEB BETWEEN LBL45.64 AND LBL40.SDR DALA2026021901223Door Frame · damagedDURING C-CHK AND WHILE INSPECTING PER EM 5311-01246-01A AT FR16 LHS DOUBLE JOGGLE AREA EXISTING REPAIRSFOUND AT HOLES NR 3, 4, 5, & 6. ELONGATED HOLE NR 5 IN UCD LAYER. PER SECTION DTE OF 567055-14 REV F, THE REPAIR OF SECTION X IS LIMITED TO 6 MONTHS SERVICESDR UIEA2026021600060Door Sill · not reportedFWD LWR CARGO DOOR SURROUND LWR MAIN SILL WEB & OTR CHORD, LATCH SUPPORT FITTING PART 1 TIME LIMITED REPAIR STA 580 REQUIRES EO PART 2 HFEC INSPECTION & EO PART 3 REQUIRES A SECOND TIME LIMITED REPAIR & EO PART 4 PERMANENT REPAIR ALL WITHIN 10 CALENDAR DAYS PESDR AALA202602165783Shoe · damagedAIRCRAFT WAS GROUNDED: AN EMERGENCY WAS NOT DECLARED DUE TO: SUSPECTED TAIL STRIKE ON TAKEOFF. AIRCRAFT AIR DIVERTED TO AND LANDED SAFELY AT JAX. INSPECTION OF TAIL SKID CONFIRMED CONTACT. TAIL DRAG SHOE FOUND WORN AND WITHIN LIMITS PER AMM 32-71-00-900-801. CSDR CALA2026032714856Access Panel · crackedIN NLG WHEEL WELL INSIDE THE ACCESS PANEL 117CL AT THE STA 377.7 CEILING SUPPORT TRACK SIDE LH WHIT CRACK DOT 106-026. REF NRC 136455. FABRICATED NEW PART IAW SRM 53-00-51-2R-12 STEPS 4.0 THRU 4.5. REMOVED FASTENERS AT STRAP IAW SRM 51-40-02-0G, REMOVED AND CU
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