N176SY
Service difficulty reports · 24
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. 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 n_number = 'N176SY' AND registry_match = 'registration' 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 n_number = 'N176SY' AND registry_match = 'registration' 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 SWIA20260107230Pump · failedFUEL 1 LO LEVEL WARNING MESSAGE DURING FLIGHT. QRH COMPLIED WITH AND DIVERSION REQUIRED. (FLIGHT 3102) THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 31453918. TROUBLESHOOT FUEL 1 LO LEVEL WARNING MESSAGE IN REFERENCE TO ERJ175 FIM 28-44-00. PERFORMED OPS TESDR SWI2026F00000Warning Message · illuminatedFUEL 1 LO LEVEL WARNING MESSAGE DURING FLIGHT. QRH COMPLIED WITH AND DIVERSION REQUIRED. (FLIGHT 3102) OPEN.SDR SWIA2025122400010Shim · wornFWD PASSENGER DOOR FWD SERRATED SLIDE SHIM IS WORN. REMOVED AND REPLACED FWD PASSENGER DOOR FWD SERRATED SLIDE SHIM. REF EMB 175 AMM 53-10-21.SDR SWI2025F01868Flap Track · wornRIGHT WING FLAP TRACK 1A HAS THICKNESS REDUCTION WEAR OF .87MM MAX ALONG FWD SIDE. REMOVED AND REPLACED RT WING FLAP TRACK 1A IAW AMM 57-54-25.SDR SWIA2025122300004Flap Track · wornLEFT WING FLAP TRACK 1A HAS THICKNESS REDUCTION WEAR OF .25MM MAX ALONG FWD SIDE. REMOVED AND REPLACED LH WING FLAP TRACK 1A REF AMM 57-54-25.SDR SWIA20230619002Unknown · warning messageON TAKE OFF I CALLED FOR GEAR UP-WE RECEIVED A CAUTION MESSAGE. MESSAGE WAS ONLY VISIBLE FOR A FEW SECONDS THEN IT CLEARED. THE GEAR HANDLE WAS LOCKED IN THE DOWN POSITION AND PUSHED THE DN LOCK REL BUTTON-GEAR RETRACTED WITH NO ISSUES. IT OCCURRED DURING A CRSDR SWIA20230217None · corrodedFWD FUSELAGE HAS LIGHTNING STRIKE ABOVE STGR 19R AFT OF FR 04 AS MARKED (C-CHECK RO 3/6/2023) REPAIRED DAMAGE AT STGR 19R AFT OF FR 04, BY DRILLING HOLE AND INSTALLING REPAIR FASTENER AND WASHER. REF EMB ETD2023-170-004756 REV.A NO WEIGHT INCREASE DUE TSDR SWIA20230216None · corrodedCORROSION/GOUGING FOUND AT RH IB SEAT TRACK FROM FR 75 TO 85 ALONG ENTIRE LENGTH. (C-CHECK RO 3/6/2023) REMOVED AND REPLACED RH IB SEAT TRACK FR 75-85 REF SRM 51-40-08. RESTORED SURFACE PROTECTION REF SRM 51-23-06 PO# 291216 AND APPLIED CIC REF CPM 51-2SDR SWIA20230215None · gougedFORWARD FUSELAGE R/H INBOARD SEAT TRACK HAS GOUGE BETWEEN FRAMES 21-22. (C-CHECK RO 3/6/2023) REMOVED AND REPLACED FORWARD FUSELAGE R/H INBOARD SEAT TRACK BETWEEN FRAMES 20-23. REF: SRM 51-40-08. SEAT TRACK REPLACED WITH FACTORY PART, NO CHANGE TO WEIGHSDR SWIA2023020014None · crackedCRACKED FR 12 COCKPIT FLOOR STRUCTURE CENTER CONNECTOR SUPPORT ANGLE. (C-CHECK RO 3/6/2023) REMOVED AND REPLACED CENTER CONNECTOR SUPPORT ANGLE AT FR 12 COCKPIT FLOOR. REF SRM 51-40-08 PO#279119 PO#291158SDR SWIA2023020013None · gougedRH LATERAL SEAT TRACK HAS GOUGES AS MARKED FR59-73. (C-CHECK RO 3/6/2023) REMOVED AND REPLACED RH LATERAL SEAT TRACK LOCATED AT FR59-73 REF EMB SRM 51-40-08. SEE CONTINUATION CARD FOR WORK PERFORMED. SEAT TRACK REPLACED WITH FACTORY PART, NO CHANGE TO WSDR SWIA20230213None · corrodedCORROSION AS MARKED ON 7 AREAS AS MARKED ON THE RH FLOOR BEAM SEAT TRACK FRAMES 23 THROUGH 34. (C-CHECK RO 3/6/2023) REMOVED AND REPLACED RH FLOOR BEAM SEAT TRACK FRAMES 23 THROUGH 34. REF: SRM 51-40-08. SEAT TRACK REPLACED WITH FACTORY PART, NO CHANGE SDR SWIA202265568None · crackedLH GEAR BAY SHOWS SIGNS OF A FRAME 52 CRACK. (FILED CLOSED) REPAIRED THE CRACK ON FRAME 52 IN THE LH WHEEL WELL AREA IN REFERENCE TO SRM 53-22-04/REPAIR 04PSDR SWIA202052900Threshold · corrodedL2 DOOR LOWER THRESHOLD BEAM HAS CORROSION ON EDGES OF FWD AND AFT GIRT BAR FITTING RECESSES. C-CHECK RO 9/29/2020. BLENDED AND REPAIRED L2 DOOR LOWER THRESHOLD BEAM FWD AND AFT GIRT BAR FITTING RECESSES (HOUSING CORNERS), IAW EMB SRM. APPLIED ALODINE, REFSDR SWIA202052899Threshold · corrodedR2 DOOR LOWER THRESHOLD BEAM HAS CORROSION ON EDGES OF FWD AND AFT GIRT BAR FITTING RECESSES. C-CHECK RO 9/29/2020. BLENDED AND REPAIRED R2 DOOR LOWER THRESHOLD BEAM FWD AND AFT GIRT BAR FITTING RECESSES (HOUSING CORNERS), IAW EMB SRM. APPLIED ALODINE, REFSDR SWIA202052897Stop Fitting · wornL2 DOOR, TOP FORWARD AND AFT LOWER DOOR STOPS ON FRAME WORN. C-CHECK RO 9/29/2020. REMOVED AND REPLACED L2 DOOR, TOP FORWARD AND AFT LOWER DOOR STOPS ON FRAME, REF AMM.SDR SWIA202052891Intercostal · corrodedRT FR 88-FR 89 INTERCOSTAL HAS CORROSION, AS MARKED. C-CHECK RO 9/29/2020. REMOVED AND REPLACED RT INTERCOSTAL BEAM AT FR 88-89 WITH NEW PART FROM FACTORY. NO SIGNIFICANT CHANGE TO WEIGHT AND BALANCE, REF EMB 175 SRM.SDR SWIA202052890Firewall · crackedAPU FIREWALL PANEL 351BZ CRACKED, AS MARKED. C-CHECK RO 9/29/2020. PERFORMED PERMANENT REPAIR OF CRACK ON PANEL 351BZ BY TRIMMING OUT THE CRACKED SPT WELDS AND INSTALLING A DOUBLER, REF SRM REPAIR02P REF TABLE 206 FOR REURRENT EXT DET AT 10,000 FC.SDR SWIA202052896Floor Support · corrodedCORROSION FORWARD WET AREA ON FLOOR SUPPORT ON RIGHT SIDE OF FRAME 16 FLOOR BEAM, AS MARKED. C-CHECK RO 9/29/2020. REMOVED AND REPLACED NEW FLOOR SUPPORT BRACKET ON FR 16 RT, REF SRM.SDR SWIA202052895Floor Support · corrodedCORROSION FORWARD WET AREA ON RIGHT FORWARD SILL IN 3 LOCATIONS BETWEEN FRAMES 13 AND 14, AS MARKED. C-CHECK RO 9/29/2020. FOUND RT SILL FR 13-14 TO BE OUT OF LIMITS. REMOVED AND REPLACED RT FORWARD SILL AND APPLIED FINISH, REF EMB SRM. SEE CONTINUATION CASDR SWIA202052894Bracket · crackedCOCKPIT FLOOR SUPPORT BRACKET CRACKED AT FRAME 12 ON PILOTS SIDE, AS MARKED. C-CHECK RO 9/29/2020. LOCATED, DRILLED AND INSTALLLED COCKPIT FLOOR SUPPORT BRACKET AT FRAME 12 ON PILOTS SIDE, REF EMB 175 SRM.SDR SWIA202052893Shear Tie · crackedCOCKPIT FLOOR, AFT END OF THE CONNECTOR FWD FUSELAGE I SUPPORT BETWEEN FRAMES 11 AND 12 HAS A CRACKED SHEAR CLIP, AS MARKED. C-CHECK RO 9/29/2020. REMOVED AND REPLACED SUPPORT ANGLE BETWEEN FR 11 AND 12, REF SRM.SDR SWIA202052892Skin · chafedMID AVIONICS BAY ACCESS DOOR CUTOUT EXTERNAL SKIN HAS 1 CHAFED RIVET HEADS, AS MARKED. C-CHECK RO 9/29/2020. REMOVED AND REPLACED FASTENER (1) AT MID AVIONICS BAY ACCESS DOOR CUTOUT, EXTERNAL SKIN, REF SRM.SDR SWIA2019120246805Unknown · odorSTRONG SMELL OF BURNING OIL AFTER TAKEOFF THROUGH 15,000 FEET. FLIGHT 3329 CLOSED COMPLIED WITH APPLICABLE STEPS IN REFERENCE WITH GE LMM, FAULT ISOLATION 003, NO DEFECTS NOTED. PERFORMED ENGINES RUN IN REFERENCE WITH AMM, NO BURNING OIL SMELL IN COCKPIT AN
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