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 SWAA2026012659858Crossbeam · crackedCABIN CROSSBEAM IS CRACKED. LOCATED BELOW FLOORBOARD 231UF, BS 540 FROM BL 0 - RBL 24. REPLACED CROSSBEAM IAW SRM 51-40-02.SDR SWAA2026011359676Post · corrodedPASSENGER CABIN FWD LAV AFT INBD LOWER POST HAS EVIDENCE OF CORROSION. REMOVED FWD FLIGHT ATTENDANT SEAT TO FOM IAW AMM 25-25-12. FWD FLIGHT ATTENDANT SEAT INSTALLED IAW TASK CARD 725-41-01. REMOVED AND REPLACED THE FWD LAV ASSY IAW TASK 725-41-01.SDR DALA2026011200289Deck Plate · out of limitsREFERENCE TO NRC 437 WIP 9, (UT) MEASUREMENT THICKNESS WAS ACCOMPLISHED ON WEB SURFACE (DECK PLATE ) BTW STA 1716 AND RBL 35 AT W4, IT'S OUT OF LIMITS PER B757-200 SRM 53-60-51-1A PROCEDURE 2 ALLOWABLE DAMAGE 2. PAR. 2. C. TABLE 101. DETAIL III . TABLE 102. SSDR EE4Y2026090123724Door Frame · crackedDURING THE ACCOMPLISHMENT OF ALLEGIANT TASK A32X-E5316-0002 RELATED TO AD 2022-02-11 / SB53-1330/SB53-1339, IT WAS FOUND AT FR16/20 LH DOOR STOP FITTING FASTENER HOLES AREA WITH CRACK INDICATION AND FR16 RH DOOR STOP FITTING FASTENER HOLE AREA WITH CRACK INDICSDR EE4Y2026090123723Fitting · crackedDURING THE ALLEGIANT TASK A32X-53-210-003 INSTRUCTIONS RELATED TO AD 2020-17-03 / SB A320-53-1331 LT CONTINUITY FITTING WITH CRACK WAS FOUND. THIS CONDITION WAS REPORTED TO AIB AND THE PART WAS REPLACED IAW AIB MESSAGE 81706551/003 AND PER SB 53-1331.SDR REXA2026052700689Door Sill · crackedINITIAL INSPECTION: CRACK ON AFT RH DOOR LANDING FS 188.0 (LATCH CUT OUT OF ACCESS DOOR 212AR) AT FWD EQUIPMENT COMPARTMENT. DOOR LANDING (LATCH CUT OUT OF ACCESS DOOR 212AR) AT FWD EQUIPMENT COMPARTMENT WAS REPLACED PER EA CRJ953-21314 REV. IR AND CRJ-900 SRSDR IPXA2026020313618Support Beam · damagedMAIN CARGO COMPARTMENT DOOR SUPPORT STRUCTURE, BETWEEN FR 27-28 HAS (1EA) HOLE DRILLED NEXT TO HI-LOCK.SDR IPXA2026012314576Tee Fitting · corrodedRIGHT RAM AIR EXHAUST, BTWN BS 1040 AND 1060, OTBD T-FITTING CORRODED. INSTALLED NEW T-CHORD/ INTERCOSTAL I.A.W. B757-200 SRM 51-40-02-0G-0SDR CALA2026011412954Shear Fitting · crackedSHEAR FITTING AT BS 540 AND LBL 6.14 IS CRACKED. REMOVED AND REPLACED THE SHEAR FITTING IAW SRM 51-40-02 AND DWG 111A2000 REV ORIGINAL.SDR CALA2026011412952Shear Fitting · crackedSHEAR FITTING AT BS 540, RBL 15.04 CRACKED. R & R THE SHEAR FITTING IAW SRM 51-40-02, & DWG 111A2000, REV ORIGINAL.SDR JJBA20260113024Door Sill · damagedUPON REMOVAL OF SERVICE DOOR FWD SILL ASSEMBLY, FOUND ELONGATED HOLES IN UNDER LYING STRUCTURE. REMOVED AND REPLACED UNDERLYING STRUCTURE BENEATH SERVICE FOOR FWD SILL ASSEMBLY.SDR DALA2026010900221Channel · damagedFORWARD SIDE OF FRAME 61 TOOLING DAMAGE IN CHANNEL @ P'3. REPAIRED TOOLING DAMAGE PER ERA 631298-14 REV. ORIG. (1392442)SDR DALA2026010900212Deck Plate · damagedIN REFERENCE TO NRC 437 WIP 7, (UT) MEASUREMENT THICKNESS WAS ACCOMPLISHED ON WEB SURFACE (DECK PLATE) BTW STA 1681.8 AND RBL 47 AT W4, THEREFORE IT'S OUT OF LIMITS PER B757-200 SRM 53-60-51-1A PROCEDURE 2 ALLOWABLE DAMAGE 2. PAR. 2. C. TABLE 101. DETAIL III. SDR JJBA20260108009Plate · corrodedRIGHT SILL PLATE FR 53-59 HAS CORROSION. REMOVED AND REPLACED 1EA RH SILL FR 53-59 RBL 16SDR SWIA2026010775795Window Frame · crackedWINDSHIELD CENTER POST PILOTS SIDE LWR CLIP CRACKED AS MARKED (C-CHECK RO 04/17/2026)REMOVED AND INSTALLED NEW WINDSHIELD CENTER POST PILOT SIDE LOWER CLIP PN: 601R33237-1S - FITTING IAW CRJ-200 SRM 51-42-21-00 & BOMBARDIER INC. DWG# 601R33007 REV. -U. COMPLISDR IPXA2026020297816Adapter · corrodedCLS ADAPTER WITH CORROSION AT FR54.3 Y/0 L/H SIDE. DOT 06648-04. ACCOMPLISHED PERMANENT REPAIR IN ACCORDANCE WITH EO-96231-REQ1 AND VT-MAE EA 300-5316-27-A4266 REV.-.SDR IPXA2026020297850Adapter · corrodedMAJOR REPAIR, CLS ADAPTER CORRODED AT FR 55 Y/0 LT SIDE. ACCOMPLISHED EA 300-5316-27-A4270, PRELIMINARY 1, STEP 13. INSTALLED THE CLS ADAPTER IAW SRM 51-40-21. ACCOMPLISHED PERMANENT REPAIR IAW EO-96237-REQ1 & VT-MAE EA 300-5316-27-A4270, REV-.SDR IPXA2026020298010Adapter · corrodedMAJOR REPAIR, CLS ADAPTER WITH CORROSION AT FR 61 Y/0 LT SIDE. ACCOMPLISHED EA 300-5317-27-A4265, REV -, PRELIMINARY 1, STEP 13. INSTALLED THE CLS ADAPTER IAW SRM 51-40-21. ACCOMPLISHED PERMANENT REPAIR IAW EO-96228-REQ 1 & VT-MAE EA 300-5317-27-A4265, REVSDR IPXA2026020298032Adapter · corrodedMAJOR REPAIR. CLS ADAPTER WITH CORROSION AT FR 62 Y/0 LT SIDE. PERFORMED EA 300-5317-27-A4265 REV -, PRELIMINARY 1, STEP 16. ACCOMPLISHED PERMANENT REPAIR IAW EO-96228-REQ1 & VT-MAE EA 300-5317-27-A4265 REV -.SDR IPXA2026020297886Adapter · corrodedMAJOR REPAIR, CLS ADAPTER WITH CORROSION AT FR54.2 Y/0 LT SIDE. ACCOMPLISHED EA 300-5316-27-A4266, PRELIMINARY 1, STEP 14. APPLIED CORROSION PREVENTIVE COMPOUND ON AFFECTED AREA IAW SRM 51-23-20 AND EO-2780-REQ001. ACCOMPLISHED PERMANENT REPAIR IAW EO-9623SDR IPXA2026020297834Adapter · corrodedMAJOR REPAIR. CLS ADAPTER WITH CORROSION AT FR57.1 Y/0 RT SIDE. .ACCOMPLISHED EA 300-5316-27-A4266, REV -, PRELIMINARY 1, STEP 13. INSTALLED CLS ADAPTER IAW SRM 51-40-21. ACCOMPLISHED PERMANENT REPAIR IAW EO-96231-REQ1 AND VT-MAE EA 300-5316-27-A4266.SDR IPXA2026020297968Adapter · corrodedMAJOR REPAIR, CLS ADAPTER WITH CORROSION AT FR 32 Y/0 L/H SIDE. DOT 06648-08. REMOVED ADAPTER CLS ON FR63 BTW -Y1959 & -Y2462 IAW A300-600 SRM 51-40-21. INSTALLED CLS ADAPTER FR63 -Y1959 -Y2462 IAW A300-600 SRM 51-40-21.SDR IPXA2026020297958Adapter · corrodedMAJOR REPAIR, CLS ADAPTER WITH CORROSION AT FR 32 Y/0 RT SIDE. ACCOMPLISHED EA 300-5314-27 A4264, PRELIMINARY 1, STEP 13, INSTALLED CLS ADAPTER IAW DRAWING B53774150 AT FR 32 YO RT IAW SRM 51-40-21. ACCOMPLISH PERMANENT REPAIR IAW EO-96227-REQ1 AND VT-MAE SDR IPXA2026020297922Adapter · corrodedMAJOR REPAIR, CLS ADAPTER WITH CORROSION AT FR 34 Y/0 R/H SIDE. ACCOMPLISHED E.A 300-5314-27 A4264 PRELIMINARY 1 STEP 13 INSTALL CLS ADAPTER IAW DRAWING B53774150 AT FR34 YO RT LOCATIONS IAW SRM 51-40-21. ACCOMPLISHED PERMANENT REPAIR IAW EO-96227-REQ1 ASDR IPXA2026020298123Adapter · corrodedMAJOR REPAIR, CLS ADAPTER WITH CORROSION AT FR 33 Y/0 R/H SIDE. ACCOMPLISHED E.A 300-5314-27 A4264 PRELIMINARY 1 STEP 13 INSTALL CLS ADAPTER PER DRAWING B53774150 AT FR33 YO RH LOCATINS IAW SRM 51-40-21. ACCOMPLISHED PERMANENT REPAIR IAW EO-96227-REQ1 ANDSDR IPXA2026020298006Adapter · corrodedMAJOR REPAIR. CLS ADAPTER WITH CORROSION AT FR 28 Y/0 L/H SIDE. ACCOMPLISHED EA#300-5314-27-A4264 PRELIMINARY 1 STEP 9 RESTORE SURFACE AND PAINT SCHEME ACCORDING TO SRM 51-23-10 AND 51-75-10. ACCOMPLISHED PERMANENT REPAIR IAW EO-96227-REQ1 AND VT-MAE EA 3SDR IPXA2026020297992Adapter · corrodedMAJOR REPAIR. CLS ADAPTER WITH CORROSION AT FR 28 Y/0 R/H SIDE. ACCOMPLISHED E.A 300-5314-27 A4264 PRELIMINARY 1 STEP 13 INSTALL CLS ADAPTER PER AIRBUS DRAWING B53774150 AT FR 28 YO RH LOCATINS IAW SRM 51-40-21. ACCOMPLISHED PERMANENT REPAIR IAW EO-96227SDR IPXA2026020297812Adapter · corrodedMAJOR REPAIR. CLS ADAPTER WITH CORROSION AT FR57.1 Y/0 L/H SIDE. DOT 06648-02. ACCOMPLISHED E.A. 300-5316-27-A4266 REV -, PRELIMINARY 1, STEP 13. INSTALLED CLS ADAPTER IAW A300-600 SRM 51-40-21. ACCOMPLISHED PERMANENT REPAIR IAW EO-96231-REQ1 AND VT-MAE EA 3SDR SWAA2026020659197Crossbeam · crackedCRACK ON CROSSBEAM, BS 540, BTW RBL 24.75 TO RBL 45.5, WL 208.1. REPLACED CROSSBEAM IAW SRM 51-40-02, AND DWG 143A5240, SHEET 13, REV-. CRACK LENTH: 0.581'SDR IPXA2026013096567Tee Fitting · corrodedTEE FITTING AT BS 1147, RBL 65 SHOWS SIGNS OF LIGHT CORROSION. REMOVED THE DAMAGED TEE FITTING IAW SRM 51-40-02. INSTALLED NEW TEE FITTING P/N: UP-149N7222-69 BETWEEN BS 1147 RBL 65 IAW SRM 51-40-02-OG.SDR IPXA2026013096671Tee Fitting · corrodedTEE FITTING, BS 1037 - 1060, LBL 37, HAD EXFOLIATING CORROSION. REMOVED FLOOR PANEL 198CR AT EXHAUST AREA BTWN BS 1037 TO 1060, RBL 65 TO FACILITATE THE EVALUATION IAW SRM 51-40-02-0G. INSTALLED A NEW TEE FITTING IAW SRM 51-40-02.SDR IPXA2026011997722Adapter · corrodedCLS ADAPTER CORRODED AT FR36 RT, UNDER FLOOR PANEL 242KF. REMOVED THE CLS ADAPTER AT FR36 IAW SRM 51-40-21. INSTALLED A NEW CLS ADAPTER IAW SRM 51-40-21.SDR CALA2026011212870Fitting · crackedLEFT & RIGHT WINDSHIELD CONTINUITY FITTINGS CRACKED. REMOVED & REPLACED LT & RT WINDSHIELD CONTINUITY FITTINGS ON EA 5310-07675 004.SDR AALA202601099056Door Frame · bentAIRCRAFT WAS NOT GROUNDED: LAVATORY-D DOOR FRAME IS BENT AND LOOSE AND MAKES DOOR DIFFICULT TO OPEN. **SUPPLEMENTAL REPORT FOR (AALA202601089056) SUBMITTED 1/8/2026 BY DFW: RESECURE THE LOOSE DOOR FRAME AND RAIL. PER CMM 25-40-64. DOOR OPERATIONAL CHECK GOOD**SDR CALA2026010912827Floor Skin · wornFLIGHT DECK FLOOR SKIN PANEL WEAR MARKS STA 259 LBL11 TO RBL 10. INSTALLED REPAIR AT FLIGHT DECK FLOOR IAW SRM 53-10-51-2R-2 AND SRM 51-40-02-0G-0.SDR CALA2026010812818Panel · delaminatedPANEL 192AT DELAMINATION LOWER SURFACE EXPOSED DAMAGE DIMENSIONS ARE 3 INCHES LONG BY 1.5 INCHES WIDE. PIC INCLUDED. APPLIED TAPE PER SRM 51-75-12-911002 INSPECT TAPE EACH FLIGHT PERMANENT REPAIR WITHIN 30 DAYS ADD EMP:U116706 INFO: PAINT PEELING OFF. NO DAMGESDR AALA202601089056Door Frame · bentAIRCRAFT WAS NOT GROUNDED: LAVATORY-D DOOR FRAME IS BENT AND LOOSE AND MAKES DOOR DIFFICULT TO OPEN. (OPEN).SDR AALA202601080074Threshold · unsecureAIRCRAFT WAS NOT GROUNDED: LAVATORY-D DOOR IS HARD TO OPEN. SERCURED THRESHOLD, OPERATIONAL CHECK GOOD.SDR SWAA2026020659007Crossbeam · crackedCRACKED CROSSBEAM, BS 540, BTW BL 0 TO LBL 24.75, WL 208.1. REPLACED CROSSBEAM IAW SRM 51-40-02, AND DWG 143A0060, SHEET 46, REV-.SDR AALA202602051624Fitting · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT RIGHT PASSENGER / CREW DOOR CUTOUT LOWER SILL AFT CORNER FITTING AT FR 68 AND S23R. REPLACED CORNER FITTING PER SRM 51-72-11.SDR IPXA2026011271869Angle · corrodedAPU INLET DOOR UPPER ANGLE FROM BS 1787.45 - 1825.00, S3R WAS CORRODED. INSTALLED A NEW UPPER ANGLE IAW SRM 51-40-02-0G-0.SDR IPXA2026011572116Strap · corrodedMAJOR REPAIR. APU INLET DOOR AFT STRAP AT BS 1825.00 FROM S3 - 6R WAS CORROED (EXISTING REPAIR FOUND IN THE AREA) INSTALLED NEW FILLER MIDDLE STRAP IAW SRM 51-40-02-0G-0.SDR FDEA202601060047Crossbeam · crackedMDCC CROSSBEAM AT FR64, BETWEEN -Y1456 AND -Y1959 CRACKED. REPAIRED THE MDCC CRACKED CROSSBEAM ON MDCC AT FR64 BETWEEN -Y1456 AND -Y1959 PER A300-600F SRM 53-10-15-201 FIG.211. THIS IS A CATEGORY "A" REPAIR. MAJOR REPAIR IAW GMM 6-2-100.SDR ASMF20260115006Panel · detachedDURING TAKEOFF ROLL THE OVERHEAD PANEL COMES OFF ITS POSITION RIGHT SIDE. PERFORMED GVI OVERHEAD PANEL INSIDE AND OUTSIDE, ALL NORMAL, PANEL RE-SECURED IAW AMM 33-11-00/201SDR JJBA20260113018Structure · corrodedTOILET WASTE VALVE EXTERNAL SURROUND STRUCTURE HAS DAMAGE. REMOVED AND REPLACED WITH NEW FROM STOCK TOILET WASTE HOUSING CUP.SDR AALA202601109451Shear Plate · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK SHEAR PLATE STR 23 R LOCATED FR69 TO FR70 AT AFT GALLEY AREA (L= 0.217 IN). MAINTENANCE REPLACED SHEAR PLATE STR 23 R LOCATED FR69 TO FR70 AT AFT GALLEY AREA IAW A320 SRM 51-42-11-801 AND DWG D53474180.SDR FDEA202601060007Crease Beam · crackedRH LOBE INTERIOR BETWEEN BS 1720 AND STR 17 HAS CREASE BEAM WITH CRACK 2 INCH APROX. ACCOMPLISHED REPAIR ON ADDITIONAL DAMAGE FOUND: CRACK IN THE HOLE AT AFT PRESSURE BULKHEAD STA 1720 PER FEDEX E.A.#: F-5310-T0385818 P1 WITH TITLE: FUSELAGE - MAINFRAME - SDR DALA2026010600108Deck Plate · damagedIN REFERENCE TO NRC 437 WIP 6, (UT) MEASUREMENT THICKNESS WAS ACCOMPLISHED ON WEB SURFACE (DECK PLATE ) BTW STA 1681.8 AND LBL 25 AT W4, WITH ORIGINAL THICKNESS IS 0.071IN AND MINIMUM REMAINING THICKNESS IS 0.030IN THEREFORE IT'S OUT OF LIMITS PER B757-200 SRMSDR DALA2026010600090Beam · damagedTOOLING DAMAGE ON BEAM AT BRACKET INSTALLED BETWEEN STATIONS 28/29 STATION 953 BOTH HOLES. REPAIRED PER ERA 631298-14 REV ORIG. (1387787)SDR SWIA2026010575791Cleat · crackedSUSPECTED CRACK ON CLEAT AT APPROX FS484, LBL36. INSTALLED NEW REPAIR ANGLE AT APPROX FS484 LBL36 REF REO 601R-53-41-3388 REV--
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