JASC 5350
Service difficulty reports · 6,118
Reports filed under 5350 · Aerodynamic Fairings, 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 = '5350' 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 = '5350' 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 IPXA2026060906876Tee Angle · corrodedRH WING TO BODY T-CHORD AT STA 1060 IS CORRODED. INSTALLED NEW T-CHORD IAW SRM B757-200 TASK: 51-40-02SDR IPXA2026052305463Tee Fitting · corrodedRH LOWER W TO B PANEL#198AR STRUCTURAL T-CHORD CORROSION PRESENT INSTALLED T-CHORD LOCATED RBL65 AND BTW STA 1037 TO 1060 WTB. IAW B757-200 SRM 51-40-02. REVIEWEDSDR CALA2026051716305Support Frame · gougedLEFT SIDE FUSELAGE WING-TO-BODY FAIRING SUPPORT AT APPROXIMATELY STA 727 JUST ABOVE FLAP TRACK #4 GOUGED. ACCOMPLISHED REPAIR AT LEFT SIDE FUSELAGE WING-TO-BODY FAIRING SUPPORT FRAME AT STA 727 JUST ABOVE FLAP TRACK #4 AS REQUIRED PER ECRA # 5360-02141, COMPSDR DALA2026051603027Fairing · damagedDIV - DUE TO LOUD POPPING NOISE FROM THE LEFT OVERWING EMERGENCY EXIT DOOR. NO PRESSURIZATION ISSUES REPORTED. UPPER WING TO BODY FAIRING PANEL 191DT WAS FOUND DAMAGED WITH LARGE CHUNKS MISSING, BUT NOT A TOTAL PANEL LOSS. : MAINTENANCE IN PROGRESS. (LP: 86488SDR SWAA2026063001515Former · crackedWING TO BODY FAIRING FORMER IS CRACKED BS 500D BETWEEN STRINGER 19 AND 20 RT. REMOVED DAMAGED FAIRING FORMER AND INSTALLED NEW WING TO BODY FAIRING FORMER AT BS 500D BETWEEN STRINGER 19 AND 20 RT IAW SRM 51-40-02-0G-0, AND DWG 116A3010, REV -.SDR SWAA2026051803016Rib · crackedLEFT WING TO BODY FAIRING SUPPORT RIB CRACKED UNDER PANEL 191FL.<[01] INSTALLED LH WING TO BODY FAIRING SUPPORT RIB; REF SRM 51-40-02.SDR UIEA2026051400317Support Angle · damagedCORRODED ANGLE FWD WING TO BODY FAIRING PANEL SUPPORT BS 977, LBL 3.42. REMOVED DAMAGED ANGLE IAW SRM 51-40-02-0G-0, REV 106. INSTALLED NEW ANGLE IAW SRM 51-40-02-0G-0 REV 106 AND DWG 65B06976, SHEET 2, REV G. JOB COMPLETED AND CONDITION CHECKED NORMAL.SDR SWAA2026061002374Access Panel · damagedELONGATED HOLE ACCESS PANEL 195CR BODY FAIRING AT FUSELAGE EXTERIOR. REPAIRED ACCESS PANEL 195CR BODY FAIRING AT FUSELAGE EXTERIOR IAW B737-700 SRM 51-70-04-2R-9 REPAIR 9.SDR MASA20260529139Strap · corrodedDURING HEAVY CHECK INSPECTIONS ON CFIII, AFT WTB FAIRING ATTACHMENT STRAP FOUND CORROSION BETWEEN STR 28-29 RH REMOVED BY BLEND OUT IAW SRM 51-10-03 AND FOUND WITHIN LIMITS IAW SRM 53-04-02 AD02, SURFACE REPROTECTED IAW SRM 51-23-04, 51-23-05 AND 51-21-06. MATSDR SWAA2026061897998Access Panel · delaminatedDELAMINATED WING TO BODY FAIRING ACCESS PANEL 191CR INTERNAL AREA AT LOWER FUSELAGE. REPAIRED ACCESS PANEL 191CR INTERNAL AREA AT LOWER FUSELAGE IAW SRM 51-70-04-2R-6, REPAIR 6.SDR SWAA2026061097915Access Panel · crackedCRACK ACCESS PANEL 193CL BODY FAIRING AT FUSELAGE EXTERIOR. REPAIRED ACCESS PANEL 193CL BODY FAIRING AT FUSELAGE EXTERIOR IAW SRM 51-70-04-2R-2 REPAIR 2.SDR IPXA2026052037295Fairing · debonded- DISBOND - PNL , AFT WING TO BODY FAIRING L/H PNL NO : 195PL. I.A.W AMM 53-66-01-404-003 REV.148 INSTALL PNL NO.195PL.SDR VNAA20260512029Structure · corrodedCORROSION ON SETTLEMENT SUPPORT STRUCTURE AT AFT C-CHANNEL ALONG AFT WING-TO-FUSELAGE FAIRING (196DR). SETTLEMENT SUPPORT STRUCTURE (STRAP) WAS REPLACED PER CRJ-700 SRM 51-42-10-001-001-A01.SDR IPXA2026052414678Bracket · corrodedRIGHT WING TO BODY FARING BRACKET FOUND LIGHT CORRISION AT B.S. 906.5 ES-046. INSTALLED 2 EA WTB FAIRING BRACKETS, P/N: 149N7210-70SAAU AND P/N: 149N7210-76SAAU AT RIGHT WING TO BODY FARING AT B.S. 906.5 IAW B757-200PF SRM 51-40-02-0G-0. AND DWG 149N7210.SDR IPXA2026052114678Bracket · corrodedRIGHT WING TO BODY FARING BRACKET FOUND LIGHT CORRISION AT B.S. 906.5 OUT OF LIMITSSDR IPXA2026060195355Tee Angle · corrodedWTB T-CHORD STA 1037 AND LBL10 WITH CORROSION AROUND THE NUTPLATE HOLE(S) INSTALLED T-CHORD IAW B757-200, SRM 51-40-02-0G-0SDR IPXA2026050995487Intercostal · corrodedWTB INTERCOSTAL BTW LBL 19 TO LBL 37 AND STA 1040 WITH CORROSION. INSTALLED NEW INTERCOSTAL 1 EA BTW LBL 19 TO LBL 37 AND STA 1040 IAW B757-200 SRM 51-40-02-0G.SDR IPXA2026052195286Intercostal · corrodedT: WTB INTERCOSTAL STA 1040 AND BTW RBL 45 TO RBL 60 WITH CORROSION. INSTALLED NEW INTERCOSTAL STA 1040 AND BTW RBL 45 TO RBL 60 1 EA IAW B757-200 SRM 51-40-02-0G.SDR IPXA2026051095297Intercostal · corrodedWTB INTERCOSTAL BTW STA 1037 TO 1060 AND RBL 60 WITH CORROSION. INSTALLED NUT PLATES AND NEW INTERCOSTAL IAW B757-200PF, SRM 51-40-02. REVIEWEDSDR IPXA2026050995446Intercostal · corrodedFAULT: WTB INTERCOSTAL BTW STA 1037 TO 1060 AND LBL 19 WITH CORROSION AROUND NUTPLATE HOLE(S). INSTALLED NEW INTERCOSTAL 1 EA BTW STA 1037 TO 1060 AND LBL 19 IAW B757-200 SRM 51-40-02-0G.SDR IPXA2026050995372Intercostal · corrodedWTB INTERCOSTAL BTW STA 1037 TO 1060 AND LBL 5 WITH CORROSION AROUND NUTPLATE HOLE(S). INSTALLATION OF NEW INTERCOSTAL AT BTW STA 1037 TO 1060 AND LBL 5 IAW B757-200 SRM 51-40-02. REVIEWEDSDR SWAA2026061596087Former · crackedWING TO BODY FAIRING FORMER IS CRACKED BS 500D BETWEEN STRINGER 19 AND 20 L/H. REMOVED DAMAGED FAIRING FORMER AND INSTALLED NEW WING TO BODY FAIRING FORMER AT BS 500D BETWEEN STRINGER 19 AND 20 R/L PER SRM 51-40-02-0G-0; AND DWG 116A3010 REV: -.SDR IPXA2026050947995Tee Angle · corrodedWING TO BODY T-CHORD AT STA 1037 RBL 0 - 16 IS CORRODED DOT 95305-02. INSTALLED T-CHORD IAW B757-200, SRM 51-40-02-0G-0.SDR IPXA2026050948140Tee Fitting · damagedWING TO BODY T-CHORD AT PANEL 198KR AT STA 1180 TO 1240 RBL 65 IS CORRODED. INSTALLED NEW T-CHORD AT WING TO BODY T-CHORD AT PANEL 198KR AT STA 1180 TO 1240 RBL 65 IAW B757-200 SRM 51-40-02. REVIEWEDSDR IPXA2026052347942Tee Fitting · corrodedWING TO BODY T-CHORD AT STA 900 RBL 46 TO LBL 27 IS CORRODED AND CHAFED DOT 95305-01. PERFORMED INSTALLATION OF THE T-CHORD 1(EA) AND REPAIR PLATES 8(EA) AT STA 900. PER B757-200 SRM 51-40-02-0G. REVIEWEDSDR SWAA2026052894992Drain Mast · crackedCRACK APU DRAIN MAST ASSY ACCESS PANEL 194FL AT LOWER FUSELAGE. REPLACED APU DRAIN MAST ASSY ACCESS PANEL 194FL AT LOWER FUSELAGE IAW AMM 28-25-07-020-801 AND AMM 28-25-07-420-801.SDR UIEA2026043000276Radome · damagedLEFT LOWER FWD FUSELAGE SKIN HAS LIGHTNING STRIKE JUST AFT OF RADOME. REMOVED AND REPLACED FASTENER ON LH LOWER FUSELAGE SKIN BS 188.5 IAW SRM 53-00-01-2R-9 REPAIR 9. NO FURTHER DEFECTS NOTED.SDR SWAA2026052097324Access Panel · deterioratedDETERIORATED ACCESS PANEL 193AL AT BODY FAIRING LT SIDE. REPAIRED ACCESS PANEL 193AL AT BODY FAIRING IAW SRM 51-70-05-2R-6 REPAIR 6.SDR DALA2026050402800Longeron · crackedWING TO BODY FAIRING LONGERON FOUND CRACKED. REPLACED WTBF LONGERON IAW ASRP 53-82-55 AND A220 ASRP 51- 42-21. (LP# 1570816; AIRCRAFT WAS GROUNDED)SDR REXA2026052900889Hinge · corrodedCORROSION ON HINGE ARMS (2E/A) OF ACCESS DOOR ON BODY FAIRING ACCESS PANEL 196DR HINGES ARMS (2EAS) OF ACCESS DOOR ON BODY FAIRING ACCESS PANEL 196DR WERE REPLACED PER SRM 51-41-02-001-001-A01 AND AMM 20-21-00.SDR REXA2026052900888Hinge · corrodedCORROSION ON HINGE ARMS (2E/A) OF ACCESS DOOR ON BODY FAIRING ACCESS PANEL 196DR HINGES ARMS (2EAS) OF ACCESS DOOR ON BODY FAIRING ACCESS PANEL 196DR WERE REPLACED PER CRJ900 SRM 51-41-02-001-001-A01 AND CRJ900 AMM 20-21-00SDR CALA2026042815766Angle · crackedRT MLG W/W FAIRING STRUCTURE ANGLE CORNER AT STA 1094 CRACKED. NR# 145213 ESFR INFORMATION ENTERED REMOVED AND REPLACED ANGLE CORNER AT RT MLG W/W FAIRING STRUCTURE AT BS 1094 IAW B757-200 SRM 51-40-02-0G-0.SDR VNAA202606060009Channel · crackedCRACK AT INNER STRAP ,AFT C-CHANNEL ALONG AFT WING-TO-FUSELAGE FAIRING 195DL. CRACK AT INNER STRAP ,AFT C-CHANNEL ALONG AFT WING-TO-FUSELAGE FAIRING 195DL WAS REPLACED PER CRJ-900 NIEO 34 REV. 2009-01.SDR CALA2026042815747Support Frame · gougedLEFT-SIDE FUSELAGE WING-TO-BODY FAIRING SUPPORT AT APPROXIMATELY STA727 JUST ABOVE FLAP TRACK #4 HAS A DEEP GOUGE. REPAIRED SUPPORT FRAME LOCATED AT L/H WING TO BODY FAIRING STA 727 AS PER AAR WORK INSTRUCTIONS ESR 33-15106 AND EC/RA 5360-02134.SDR 2026F00086Support · corrodedCORROSION FOUND AROUND AND UNDER NUTPLATES ON LH (P/N 6921340-3) AND RH (P/N 6921340-4) UNDER-FAIRING SUPPORTS FOR PANELS 175BC AND 176BC. MECHANICALLY REMOVED CORROSION LOCATED AROUND AND UNDER NUTPLATES ON LH (P/N 6921340-3) AND RH (P/N 6921340-4) UNDER-FAISDR SWAA2026051992082Tail Cone · debondedTAIL CONE OUTER SKIN IS DISBONDED 4' FWD OF ACCESS PANEL 318BR, FWD LOWER CORNER. REPAIRED DISBOND TO TAILCONE OUTER SKIN 4' FWD OF ACCESS PANEL 318BR LOWER CORNER IAW SRM 51-70-04-2R-2.SDR JR2R20260422730Panel · corrodedPANEL 195ML HAS EVIDENCE OF CORROSION AROUND SCREW HOLES. REPAIRED PER ETD.SDR VNAA2026071320001Access Panel · crackedCRACK ON ACCESS PANEL 172CR AT OVER WING FAIRING. ACCESS PANEL 172CR AT OVER WING FAIRING WAS REPAIRED PER REO 679-53-82-430 REV - -, AND STIFFENER WAS REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01.SDR SWAA2026042990731Panel · delaminatedPANEL 191D HAS DELAMINATION DAMAGE ON OUTER SURFACE. PANEL 191D WITH DELAMINATION DAMAGE ON OUTER SURFACE WAS REPAIRED IAW SRM 51-70-05-2R-2.SDR SWAA2026050790230Access Door · corrodedCORROSION ACCESS DOOR 311BL INERNAL DOUBLER AT TAIL CONE 2026-255586<[01] TOOL USED P/N: NORTEC 500D; S/N: N500X1693P030456; CAL DUE: 25-MAY-26.;[02] TOOL USED P/N: 45MG; S/N: 242232211; CAL DUE: 15-DEC-26;[03] ON STEP 7: TOOL USED EDDY CURRENT EQUIPMENT PN: NSDR IPXA2026041735306Support Angle · corrodedRIGHT WING TO BODY AREA HAS A CORRODED SUPPORT ANGLE AT BS 1060, RBL 69. INSTALLED A NEW SUPPORT ANGLE IAW SRM 51-40-02-OG.SDR SWAA2026051189152Channel · crackedCRACK ON CHANNEL OF ACCESS PANEL 443AT. REPLACED CHANNEL LOCATED ON ACCESS PANEL 443AT IAW B737-800 SRM 51-40-02 SRM 51-10-02 ITEM 9SDR IPXA2026090479144Access Panel · corrodedFWD, LT LOWER WTB PANEL LANDING INSIDE ACCESS PANEL 193AL HAS SURFACE CORROSION.SDR IPXA2026090479384Structure · corrodedLEFT AFT WTB FAIRING STRUCTURE LOWER CHORD AT APRROX. BS 1200 - 1220 HAS EXFOLIATION CORROSION.SDR IPXA2026051179384Angle · corrodedLH, AFT WTB FAIRING STRUCTURE LOWER CHORD AT APRROX. STA 1200 TO 1220 HAS EXFOLIATION CORROSION. INSTALLED LWR CHORD AT LH AFT WTB FAIRING STRUCTURE BEAM ASSY BETWEEN STA 1200-1240 AND BL 57.50 IAW B757-200PF SRM 51-40-02-0G-0.SDR IPXA2026051179310Frame · corrodedLH, AFT WTB FAIRING STRUCTURE CHORD AT APRROX. STA 1220 HAS CORROSION. INSTALLED CHORD FRAME AT LH AFT WTB FAIRING STRUCTURE STA 1220, BL 57-50 I.A.W. B757-200PF SRM 51-40-02-0G-0.SDR IPXA2026051179144Fairing · corrodedFWD, LH LOWER WTB PANEL LANDING INSIDE ACCESS PNL 193AL HAS SURFACE CORROSION. STICKER #83-003. ATA 53-30. REMOVED 1EA CORRODED WEB FROM INTERCOSTAL ASSY. INSTALLED (15EA) NEW NUTPLATES ON WEB P/N 149N7125-41SAAU, IAW DWG 149N7125/SAMPLE AND B757-200PF SRM 51SDR IPXA2026051179388Fairing · corrodedLH, AFT WTB FAIRING STRUCTURE FRAME AT APRROX. STA 1200 TO 1220 HAS EXFOLIATION CORROSION. 83-005. ATA 53-30. INSTALLED WEB AND REINSTALLED (1EA) LIGHT SUPPORT BRACKET AT STA 1194 AND BL 57.50, (1EA) LIGHT SUPPORT BRACKET AT STA 1225 AND BL 57.50, (1EA) SUPPORSDR IPXA2026042579388Frame · corrodedLEF AFT WTB FAIRING STRUCTURE FRAME AT APRROX. BS 1200 - 1220 HAD EXFOLIATION CORROSION.SDR IPXA2026042579310Structure · corrodedLEFT AFT WTB FAIRING STRUCTURE CHORD AT APRROX. BS 1220 WAS CORRODED.
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