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 SWAA2026101953037Crossbeam · crackedPASSENGER CABIN FLOOR CROSSBEAM CRACKED, TOP PLATE ONLY, AT BS 540, RBL 27, WL 208. REMOVED AND REPLACED THE CROSSBEAM IAW SRM 51-40-02-0G-0, 51-40-05-0G-0, AND DWG 143A0060, REV B.SDR IPXA2026100500255Door Frame · chafedAPU COMPARTMENT ACCESS DOOR 315 AL FRAME ASSY LOWER FLANGE HAS A CHAFING APPROX AT BS 1885.2, STGR 17L AREA. REMOVAL AND INSTALLATION ACCOMPLISHED. FRAME IAW DWG 148N6663 AND IPC 52-48-05-01.SDR IPXA2026093099320Doubler · corrodedLEFT FUSELAGE SECTION 48 INTERIOR STRUCTURE RIB HAS EVIDENCE OF CORROSION ON LOWER AREA APPROX AT BS 1992.8,SDR SWAA2026092145520Strap · crackedCRACK FOUND ON THE RT AFT FASTENER HOLE OF BS 639 STUB BEAM STRAP. REPLACED THE DAMAGED STUB BEAM STRAPS IAW SRM 51-40-02-0G-0, DWG 144A5901, SH 36, REV -, DWG 110A0170, REV B, DWG 111A6504, REV B, DWG 144A1715, REV A, DWG 144A1705, REV -, SHEET DL, REV PSDR VNAA2026091125Intercostal · corrodedPAX DOOR MID DD2 INTERCOSTAL FOUND TO BE CORRODED REQUIRES REPLACEMENT. REPLACED PAX DOOR DD2 MID INTERCOSTAL IAW SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01, AND 51-42-21-001-001-A01.SDR VNAA2026091117Post · corrodedBS 280 BULKHEAD DOOR POST AND ATTACHING FLOOR ANGLE ARE CORRODED AT LBL 11. REPAIRED BS 280 BULKHEAD DOOR POST IAW SRM 53-11-10-201-006-A01.SDR VNAA2026091116Post · corrodedFS 280 BULKHEAD DOOR POST AND ATTACHING FLOOR ANGLE ARE CORRODED AT RBL 11. REPAIRED BS 280 BULKHEAD DOOR POST IAW SRM 53-11-10-201-006-A01.SDR UIEA2026083100831Pan · damagedWASTE SERVICE PAN FOUND TWO FASTENER HOLES WITHOUT BLANK OUT, AFTER DEACTIVATION. TWO RIVETS INSTALLED IAW DWG 146T3244, DL, & 146T3244, PL. NO FURTHER DEFECTS NOTED.SDR HNAA2026101601001Support · crackedBAGGAGE DOOR SUPPORT MECHANISM CRACKED AT BTW FR67-68 AT STR5R. RAR SUPPORT IAW SRM 51-40-02SDR HNAA2026101500981Support · crackedCARGO DOOR SUPPORT MECHANISM SUPPORT CRACKED AT BTW FR61-62. RAR SUPPORT IAW SRM 51-40-02SDR HNAA2026101300976Beam · crackedCARGO DOOR ENTRY, LWR BEAM FWD FITTING CRACKED AT FR65. RAR FITTING IAW SRM 51-40-02SDR HNAA2026100700953Beam · mechanic errorMISDRLLED HOLE ON COCKPIT ON LH OVERHEAD BEAM. REPAIRED IAW ETD 2026-145-015636 B AND EO 1-53-26-0463SDR HNAA2026100500948Beam · corrodedCARGO DOOR LWR BEAM CORRODED. R & R LWR BEAM IAW SRM 51-40-02SDR AALA202610294951Reinforcement · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON LOWER FUSELAGE STATIC PORT REINFORCEMENT BETWEEN FR 23 AND FR 24 BETWEEN S31L AND S32L - MAINTENANCE REPLACED REINFORCEMENT PER EA 379706SDR IPXA2026100251860Crossbeam · corrodedAFT CARGO COMPT. FR 54.3 / Y 450 TO Y 1959 CEILING SUPPORT HAS CORROSION. NEW CEILING SUPPORT AFT CARGO COMPT. FR 54.3 / Y 450 TO Y 1959 WAS INSTALLED IAW SRM 51-40-21.SDR IPXA2026100251661Crossbeam · corrodedAFT CARGO COMPT. FRAME 54, Y953 - Y1959. CEILING SUPPORT WAS CORRODED. REMOVAL OF CORROSION FROM CEILING SUPPORT AT FR54 CROSSBEAM Y953 TO Y1959. IAW A300 SRM 51-74-10. FOUND TO BE WITHIN LIMITS IAW A300 SRM 51-73-11.SDR IPXA2026100252048Crossbeam · corrodedAFT CARGO BAY CEILING SUPPORT AT FR 56 - 57.2, BTWN Y 450 - Y953 WAS CORRODED. REMOVAL OF CORROSION FROM CEILING SUPPORT AT FR 56 TO FR 57.2 BETWEEN Y450 TO Y953 IAW A300 SRM 51-74-10.FOUND TO BE NEGLIGIBLE DAMANGE WITHIN LIMITS IAW A300 SRM 51-73-11.SDR IPXA2026100252060Crossbeam · corrodedAFT CARGO BAY, FR 57, Y0 - Y953, CEILING SUPPORT WAS CORRODED. REMOVED CORROSION FROM CEILING AT SUPPORT PANEL FR57, Y0 TO Y953. IAW SRM 51-74-10.ORIGINAL MATERIAL THICKNESS IS .063.MATERIAL LOSS IS .002 REMAINING MATERIAL IS .061 T98828.FOUND TO BE NEGLIGIBLSDR IPXA2026100653507Crossbeam · corrodedAFT CARGO BAY AT FR 62 BTWN Y 0 - Y 1959, CEILING SUPPORT HAS CORROSION. VERIFIED REMOVAL OF CORROSION FROM CEILING AT SUPPORT PANEL FR62, Y0 TO Y1959. IAW SRM 51-74-10.FOUND TO BE NEGLIGIBLE DAMANGE WITHIN LIMITS IAW SRM 51-73-11.SDR ASAA2026090968975Crossbeam · crackedSTA. 540, RBL 45, BRAKE PANEL BROKEN. GROUNDED - YES. REMOVED & REPLACED PANEL BREAK STA 540 RBL22 - RBL45 IAW BOEING 737-800 SRM 51-40-02-0G-0.SDR DALA2026091005066Beam · corrodedLEVEL 2 CORROSION, PAX CABIN, LONGITUDINAL BEAM UPPER FLANGE WITH CORROSION LOC. AT FR 68 Y765. REPLACED LONGITUDINAL P/N D5347219220000 AT Y 765 BTW FR66 TO FR70 I/A/W SRM TASK 51-72-11-911-001 PARAG 2 REV 158.00 DATED 01 -JUN-26. AND REFERENCE A 320 DWGS: DSDR KCSA202609091203Tension Tie · crackedDURING EO 5312-21-02 INSPECTION, A CRACK WAS FOUND IN THE RT 860 TENSION TIE FWD CHANNEL.SDR KCSA202609091200Tension Tie · crackedDURING EO 5312-21-02 INSPECTION, A CRACK WAS FOUND IN THE LT BS 860 TENSION TIE FWD CHANNELSDR KCSA202609091199Tension Tie · crackedDURING EO 5312-21-02 INSPECTION, A CRACK WAS FOUND IN THE LT 840 TENSION TIE FWD CHANNEL.SDR KCSA202609091198Tension Tie · crackedONE HOLE CRACK INDICATION FOUND DURING OPEN HOLE HFEC INSPECTION OF THE LT BS 820 AFT CHANNEL.SDR KCSA202609091197Tension Tie · crackedDURING OPEN HOLE HFEC INSPECTION, CRACK SIGNAL INDICATIONAT LT BS 720 FWD CHANNEL.SDR HNAA2026102901063Door Frame · corrodedSERVICE DOOR CUT-OUT LWR STRUCTURE FROM FR 20 - FR 22 CORRODED AT NUTPLATE HOLE. PERFORMED DOUBLER REPAIR ON SERVICE DOOR CUT-OUT LWR STRUCTURE AT FR 20 NUT PLATE HOLE IAW EMB 145 SRM 53-21-02-RE ITEM 3 FIG 202.SDR IPXA2026102042390Crossbeam · corrodedFWD CARGO FR 34, BETWEEN -Y140 AND -Y805 CEILING SUPPORT HAS CORROSION. INSPECTED REMOVED CORROSION FROM CEILING SUPPORT AT FR 34, BETWEEN -Y140 AND -Y805. IAW SRM 51-74-10.ORIGINAL MATERIAL THICKNESS IS .063 MATERIAL LOSS IS .003 REMAING MATERIAL IR .060.FOSDR IPXA2026101940470Crossbeam · corrodedAFT CARGO COMPARTMENT, CEALING SUPPORT (Z PROFILE) AT FR57.3 AT CROSSBEAM -Y1959 HAS A SCREW HOLES WITH CORROSION. REMOVED CORROSION FROM CEILING SUPPORT (Z PROFILE) AT FR57.3 AT CROSSBEAM -Y1959. IAW SRM 51-74-10.ORIGINAL MATERIAL THICKNESS IS .063.MATERIAL SDR IPXA2026101941134Crossbeam · corrodedAFT CARGO COMPARTMENT, ANGLE SUPPORT OF SMOKE DETECTOR BOX AT FR62 CROSSBEAM Y0 WITH CORROSION. REMOVED CORROSION FROM CEILING AT SUPPORT PANEL FR62, IAW A300 SRM 51-74-10. ORIGINAL MATERIAL THICKNESS IS .063- MATERIAL LOSS IS .001 REMAINING MATERIAL IS .062 TSDR IPXA2026101840963Crossbeam · crackedAFT CARGO COMPARTMENT FWD BULKHEAD AT FR54 CROSSBEAM Y0 ANGLE SUPORT WITH CRACKED INSTALLED NEW ANGLE SUPPORT, AFT CARGO COMPARTMENT FWD BULKHEAD AT FR54 Y0, IAW SRM 51-40-21.SDR IPXA2026100240470Crossbeam · corrodedAFT CARGO COMPARTMENT, CEALING SUPPORT (Z PROFILE) AT FR57.3 AT CROSSBEAM -Y1959 HAS A SCREW HOLES WITH CORROSION DOT 31-037 VERIFIED CIC APPLIED IAW EO-2780-REQ001<BR>JOB COMPLETE.SDR IPXA2026100242382Crossbeam · corrodedFWD CARGO FR 38.1, BTWN Y805 AND Y1407, CEILING SUPPORT BRACKET WAS CORRODED. REMOVED CORROSION FROM CEILING SUPPORT IAW SRM 51-74-10. APPLIED ALODINE AND PRIMER IAW SRM 51-21-10-001 AND APPLIED PAINT IAW SRM 51-75-10-201. NO FURTHER ACTION REQUIRED.SDR IPXA2026100242390Crossbeam · corrodedFWD CARGO FR 34, BTWN -Y140 AND -Y805, CEILING SUPPORT WAS CORRODED.SDR IPXA2026100242469Crossbeam · corrodedFWD CARGO FR 34, BTWN Y140 - Y805, CEILING SUPPORT WAS CORRODED. INSPECTED REMOVED CORROSION FROM CEILING SUPPORT AT FR 34, BETWEEN Y140 AND Y805. IAW SRM 51-74-10.ORIGINAL MATERIAL THICKNESS IS .063 MATERIAL LOSS IS .003 REMAING MATERIAL IR .060.FOUND TO BESDR IPXA2026100240574Crossbeam · corrodedAFT CARGO COMPARTMENT, CEILING SUPPORT AT FR58 FROM CROSSBEAM -Y450 TO -Y953 HAS A SPOTS WITH CORROSION, PROFILE CROSS T26/1880702 AND LOCATED AND DRILLED PROFILE CROSS IAW SRM 51-40-44-001.SDR CALA2026090919329Window Frame · gougedL1 WINDOW FRAME C-D POST WITH MULTIPLE AREAS OF DAMAGE ALONG WINDOW MATING SURFACE. PERFORMED REPAIR ON NR 1 WINDOW FRAME BTW C-D POST IAW EO 260454 REV.P1, EO 260454 REV. P2, EO 260454 REV.P3, EO 260454 REV, P4, EO 260454 REV. IR AND EC/RA 5610-0157 2.THISSDR JR2R20260908370Sill Drain · chafedRIGHT SILL DRAIN HAD CORRODED SPOTS BETWEEN FR 89 - FR 90. REPLACED.SDR SWAA2026100609384Crossbeam · crackedCRACKED SUPPORT BRACKET. BS 540 AT LEVEL LBL 6 AT LT AIR CONDITIONING BAY. REPLACED NEW SUPPORT BRACKET LOCATED BS540 AT LEVEL LBL 6 AT LT AIR CONDITIONING BAY IAW SRM 51-40-02-0G, SRM 51-10-02-0G-0SDR CALA2026092819876Failsafe · crackedBS 663.75 FRAME FITTING AND FAIL SAFE STRAP AT S-18A HAD A VISIBLE CRACK. PERFORMED AN INSPECTION OF RT BS 663.75 REAR SPAR FRAMEASSEMBLY ON AIRCRAFT N14228 IAW PART 2 OF THE LATEST REVISION OF ECRA5340-02286. PART 1 STEP 1 OF ECRA ACCOMPLISHED LP AND WORK CASDR CALA2026090819303Failsafe · corrodedDURING LH FAILSAFE FITTING REPLACEMENT FOUND LH KICK FITTING WITH CORROSION. LH PICKELFORK KICK FITTING WAS REPLACED ON ECRA# 5340-02285 AND EO 260452 STEP 132SDR SWAA2026101434044Crossbeam · crackedCRACKED CROSSBEAM, BS 540, BL 0 - RBL 24.75. REPLACED THE CROSSBEAM IAW SRM 51-40-02, & DWG 143A0060, SHEET 64, REV-.SDR SWAA2026101448469Crossbeam · crackedCRACK CROSSBEAM, BS 540 BTWN BL 0 - LBL 24.75. REPLACED THE CROSSBEAM IAW SRM 51-40-02, & DWG 143A0060, SHEET 64, REV-.SDR JR2R20260906457Seal Rest · corrodedFWD CARGO ENTRY LOWER MIDDLE SEAL REST IS CORRODED. REPLACEDSDR JR2R20260906826Crossbeam · corrodedUPON REMOVAL OF PANEL 221FLF, FOUND FR12 CROSSBEAM CHANNEL BRACKET CORRODED.SDR IPXA2026102006679Deck Plate · corrodedMAIN DECK FROM STA 1681.1 TO 1720 AND LBL 54.9 TO RBL 54.9 DECK PLATE HAS MULTIPLE AREAS WITH CORROSION. 1 DOUBLERS FOR AREA #1 PER B757-200PF SRM 53-60-51-2R-8, AREA #2 PER B757-200PF SRM 53-60-51-2R-5, AREA #3 PER B757-200PF SRM 53-60-51-2R-8 AND AREA #4 PERSDR AALA202610086534Transition Panel · corrodedAIRCRAFT IN BASE MAINTENANCE: FORWARD CARGO, CORROSION ON R/H TRANSITION PANEL BETWEEN STATIONS 500E AND 500F, RBL24 INCHS. INSTALLED NEW R/H TRANSITION PANEL IAW IPC 53-42-11-11 AND AARD 51-00-05-1.SDR SWAA2026100646931Crossbeam · crackedCRACK ON BREAK PANEL LOCATED BS540 BTW BL0 TO RBL24.75 CENTER SECTION AT PASSENGER CABIN. REPLACED BREAK PANEL IAW SRM 51-40-02-0G-0, SRM 51-10-02-0G-0, ITEM 8, AND DWG: 143A0060, SHEET 64, REV-.SDR SWAA2026100643432Crossbeam · crackedCRACKED ON BREAK PANEL LOCATED BS540 BTW BL0 TO LBL24.75 CENTER SECTION AT PASSENGER CABIN. REPLACED BREAK PANEL AND FASTENERS IAW SRM 51-10-02, ITEM 8, SRM 51-40-02, AND DWG 143A0060, SHEET 64, REV-.SDR IPXA2026091406679Deck Plate · corrodedMAIN DECK FROM BS 1681.1 - 1720, LBL 54.9 - RBL 54.9 DECK PLATE HAS MULTIPLE AREAS WITH CORROSION, REQUEST NDT UT THICKNESS. AT REWORKED AREAS IAW SRM 53-60-51-1A-1, PARA 2.C.
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