N160SY
Service difficulty reports · 16
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 = 'N160SY' 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 = 'N160SY' 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 SWIA2026030475414Spring · brokenON APPROACH, RECEIVED MLG LEVER DISAGREE MESSAGE, & RT MAIN WAS NOT INDICATING DOWN. RAN QRH & MESSAGE CLEARED & GEAR OPS NORMAL ON SECOND APPROACH. (FLIGHT 5574) INTERROGATED CMC, FOUND FAULT CODES 32612208PSS & 32611213PSS. RT MLG R2 DOWNLOCK SPRING BROKESDR SWIA202405150001Skin · chafedRH SLAT PANEL #3 NOSE SKIN HAS CHAFES IN TWO SPOTS AS MARKED. (C-CHECK RO 5/14/2024) BLENDED OUT THE CHAFES ON RH WING #3 SLAT LEADING EDGE NOSE SKIN. BLEND DIMENSIONS AS FOLLOWS; D= .010", L= 1.747", W= 1.498", NOMINAL THICKNESS= .087", MAXIMUM ALLOWABLE SDR SWIA2024051500430Rib · damagedDURING COMPLETION OF SB170-57-0073 REV. 1 FOUND ELONGATED MOUNT HOLE FOR UPPER IB RIB 42 CONNECTION IN R/H WING OB SPAR 1 P/N 170-31107-052 (C-CHECK RO 5/14/2024) REPAIRED ELONGATED HOLE ON UPPER IB RIB 42 CONNECTION ON RH WING OB SPAR 1 PN: 170-31107-052 SDR SWIA2024051500426Skin · scratchedRH WING #3 SLAT INBOARD END UPPER SKIN HAS TWO SCRATCHES. (C-CHECK RO 5/14/2024) DAMAGE ACCEPTED AS PERMANENTLY ALLOOWABLE WITH NO ADDITIONAL REPAIR REQUIRED PER ETD2024-170-012219 THE REWORKED AREAS MUST BE DETAILED VISUAL INSPECTED EVERY 24 MONTHS FOR CSDR SWIA2024051500425Seat Track · gougedGOUGES ON L/H SIDEWALL SEAT TRACK BETWEEN FR 21-23 IN 2 LOCATIONS AS MARKED. (C-CHECK RO 5/14/2024) REMOVED AND REPLACED LH SIDEWALL SEAT TRACK BETWEEN FR 21-23 REF SRM 51-40-08. RESTORED SURFACE PROTECTION REF SRM 51-23-06 (310857) AND APPLIED CIC PROTECTSDR SWI202405150409Seat Track · corrodedRH INBD SEAT TRACK FR 43-59 GOUGED AND CORRODED AS MARKED: FR 43, 43-45, 46, 47, 48, 49, 50, 56, 57 AND 58 (C-CHECK RO 5/14/2024) REMOVED AND REPLACED RH INBD SEAT TRACK FR 43-59 REF SRM 51-40-08 REPLACED WITH NEW OEM PART, NO WEIGHT AND BALANCE ADJUSTMENTSDR SWI2024F00407Seat Track · corrodedLH IB SEAT TRACK HAS MULTIPLE LOCATIONS WHERE CORROSION IS PRESENT AS MARKED FR 74- FR 84 (C-CHECK RO 5/14/2024) REMOVED AND REPLACED LH IB SEAT TRACK FR 74- FR 84. REF EMB SRM 51-40-08. THIS REPAIR DOES NOT CHANGE WEIGHT AND BALANCE. SEE CONTINUATION CARDSDR SWI20240515000406Seat Track · corrodedLH OB SEAT TRACK HAS MULTIPLE LOCATIONS WHERE CORROSION IS PRESENT AS MARKED FR 74- FR 84 (C-CHECK RO 5/14/2024) REMOVED AND REPLACED LH OB SEAT TRACK FR 74- FR 84, REF SRM 51-40-08. REPLACED WITH NEW OEM PART, NO WEIGHT AND BALANCE ADJUSTMENT REQUIRED.SDR SWIA2024051500424Seat Track · corrodedRH IB SEAT TRACK HAS MULTIPLE LOCATIONS WHERE CORROSION IS PRESENT AS MARKED FR 74- FR 84 (C-CHECK RO 5/14/2024) REMOVED AND REPLACED RH IB SEAT TRACK FR 74-84 REF SRM 51-40-08. RESTORED SURFACE PROTOCTION REF SRM 51-23-06 PO 313198 AND CPM 51-25-00 PO 314SDR SWIA2024051500421Floorbeam · corrodedCORROSION, AFT WET AREA, ON LH LONGITUDINAL FLOOR BEAM AT FRAME 87 WHERE THE BEAM PASSES BETWEEN THE LH AND CENTER SHEAR PANELS. (C-CHECK RO 5/14/2024) REMOVED AND REPLACED A FT WET AREA, ON LH LONGITUDINAL FLOOR BEAM AT FRAME 87, REF SRM 51-40-08. RESTORESDR SWI2023F00476Unknown · warning messageSHORTLY AFTER TAKEOFF, WITH ECS OFF AND APU ON, BLEED 2 OVERPRESS CAUTION MESSAGE APPEARED. COMPLETED ASSOCIATED QRH AND THE MESSAGE EXTINGUISHED. THE MESSAGE DID NOT RETURN, NORMAL OPERATION THEREAFTER. (FLIGHT 4746 FILED CLOSED)INTERROGATED CMC AND FOUND BLESDR SWIA202158734Floorbeam · corrodedAFT WET AREA-FLOOR CROSSBEAM FR 84 HAS CORROSION/ LIGHT SCORE MARK ON UPPER FLANGE 12" OTBD OF RH SEAT TRACK (C-CHECK RO 6/11/2021) INSTALLED NEW L ANGLE REPAIR AT FR84 REF ETD 2021-170-017514 SRM53-00-10 REPAIR 03. REFER TO ATTACHMENTS FOR WORK PERFOSDR SWIA202158733Seat Track · corrodedFWD WET AREA- RH FLOOR SEAT TRACK (Y= 10.7") HAS CORROSION ON FLOOR FLANGE AT FR 17 (C-CHECK RO 6/11/2021) BLENDED OUT CORROSION REF SRM 51-10-03. LENGTH: 1.237" / WIDTH: .494" / DEPTH: .024" / ORIGINAL THICKNESS: .080' / REMAINING MATERIAL: .056" / ASSSDR SWIA202158732Floorbeam · damagedFWD WET AREA- FRAME 17 FLOOR CROSS BEAM UPPER FLANGE HAS SCORE MARK EXTENDING BETWEEN LH FLOOR SEAT TRACK (Y= -10.7") AND RH FLOOR SEAT TRACK (Y= 10.7") (C-CHECK RO 6/11/2021) BLENDED OUT DAMAGE REF SRM 51-10-03. LENGTH: 21.500" / WIDTH: .900" / DEPTH: SDR SWIA202158735Door Frame · corrodedFWD CARGO DOOR FRAME, CORROSION AROUND NUT PLATES IN SEAL REST SURFACE, AS MARKED. (C-CHECK RO 6/11/2021) REMOVED AND REPLACED FWD CARGO DOOR FRAME NUTPLATES AS MARKED. REF. SRM 51-75-16.SDR SWIA201845097Sensor · dirtyRETURN TO FIELD. LANDING GEAR WOULD NOT RETRACT. LG WOW SYS FAIL CAUTION MSG. (FLT#5261) FO: 09/27/2018 CLOSED CLEANED BOTH WOW SENSORS IAW AMM. PERFORMED MULTIPLE GEAR SWINGS IAW AMM. OPS CHECK GOOD.
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