N827AY

Service difficulty reports · 27

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 = 'N827AY' 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.

SDR REXA2013012700078Bulkhead · crackedBULKHEAD WEB IS CRACKED AT FS 280, LBL 9, WL 70. REPAIRED IAW BOMBARDIER REO 601R-53-11-171.Jan 26, 2013 · N827AY · Cndair CL6002B19 · Fuselage Main, BulkheadSDR REXA2013012700077Bulkhead · crackedBULKHEAD WEB IS CRACKED AT FS 280, RBL 9, WL 70. REPAIRED IAW BOMBARDIER REO 601R-53-11-171.Jan 26, 2013 · N827AY · Cndair CL6002B19 · Fuselage Main, BulkheadSDR REXA2013012700081Skin · chafedFUEL PANEL 510AB LANDING ON LEFT WING LOWER SKIN IS CHAFED AND PITTED AT WS 12.245. REPAIRED IAW BOMBARDIER REO 601R-57-21-030.Jan 24, 2013 · N827AY · Cndair CL6002B19 · Wing, Plate/SkinSDR REXA2013012700080Skin · chafedFUEL PANEL 640BB LANDING ON RIGHT WING LOWER SKIN IS CHAFED AND PITTED AT WS 54.897. REPAIRED IAW BOMBARDIER REO 601R-57-21-030.Jan 24, 2013 · N827AY · Cndair CL6002B19 · Wing, Plate/SkinSDR REXA2013012700079Skin · chafedFUEL PANEL 540BB LANDING ON LEFT WING LOWER SKIN IS CHAFED AND PITTED AT WS 54.897. REPAIRED IAW BOMBARDIER REO 601R-57-21-030.Jan 24, 2013 · N827AY · Cndair CL6002B19 · Wing, Plate/SkinSDR REXA2013011100134Light · damagedEMERGENCY EXIT LIGHT BY MCD IS DAMAGED AND LOOSE FROM ITS MOUNTING. REMOVED AND REPLACED EMERGENCY EXIT FLOOD LIGHT IAW AMM 33-51-19. OK FOR SERVICE.Jan 11, 2013 · N827AY · Cndair CL6002B19 · Emergency LightingSDR REXA2012103001435Life Vest · unserviceableCAPTAIN & FIRST OFFICER'S LIFE VEST BAG TORN. REMOVED AND REPLACED CAPTAIN & FIRST OFFICER'S LIFE VESTS IAW AMM 25-61-03.Oct 30, 2012 · N827AY · Cndair CL6002B19 · Life JacketSDR REXA2012072401186Container · tornONE INFANT LIFE VEST BAG TORN. REMOVED AND REPLACED ONE INFANT LIFE VEST IAW PA 25-096A.Jul 24, 2012 · N827AY · Cndair CL6002B19 · Life JacketSDR REXA201200021Control Quadrant · defectiveON LANDING ALL SPLR'S DEPLOYED AS NORMAL, HOWEVER ONE FULL TR THEY SPLR'S ALL RETRACTED AND THE DEPLOYED AGAIN ONCE THE TR WENT TO IDLE. REMOVED AND REPLACED THROTTLE QUADRANT IAW AMM 76-11-00 OPS CHECKS GOOD. AND FUNCTIONAL CHECK OF SPOILER GROUND LIFT DUMDec 30, 2011 · N827AY · Cndair CL6002B19 · Power LeverSDR REXA201100211Bulkhead · chafedINTERNAL CARGO COMPARTMENT AT FS 621 PRESSURE BULKHEAD AT WL 103.5 BETWEEN LBL 27 AND RBL 36, SKIN IS CHAFED AT NINE LOCATIONS APPROX 1.00"L X 0.100"W X 0.005"D. REPAIRED IAW BOMBARDIER REO 601R-53-61-2155.Apr 2, 2011 · N827AY · Cndair CL6002B19 · Fuselage Main, BulkheadSDR REXA201100210Bulkhead · chafedINTERNAL CARGO COMPARTMENT AT FS 621 PRESSURE BULKHEAD AT WL 86.75 ON RBL 27, SKIN IS CHAFED APPROX 1.00"L X 0.100"W X 0.005"D. REPAIRED IAW BOMBARDIER REO 601R-53-61-2155.Apr 2, 2011 · N827AY · Cndair CL6002B19 · Fuselage Main, BulkheadSDR REXA201100199Rivet · damagedINTERNAL CARGO COMPARTMENT AT FS 621 PRESSURE BULKHEAD AT WL 86.5 BETWEEN RBL 18 AND RBL 36 HAS TWO DAMAGED RIVETS. RIVETS REMOVED AND REPLACED IAW SRM 51-42-06.Apr 2, 2011 · N827AY · Cndair CL6002B19 · Fuselage Main, BulkheadSDR REXA201100198Bulkhead · damagedINTERNAL CARGO COMPARTMENT AT FS 621 PRESSURE BULKHEAD AT WL 94.5 ON LBL 9 HAS BROKEN ISOLATOR NUT PLATE. REPAIRED IAW SRM 51-42-06.Apr 2, 2011 · N827AY · Cndair CL6002B19 · Fuselage Main, BulkheadSDR REXA201100197Bulkhead · damagedINTERNAL CARGO COMPARTMENT AT FS 621 PRESSURE BULKHEAD AT WL 86.5 BETWEEN LBL 9 AND LBL 36 HAS FOUR DAMAGED RIVETS. RIVETS REMOVED AND REPLACED IAW SRM 51-42-06.Apr 2, 2011 · N827AY · Cndair CL6002B19 · Fuselage Main, BulkheadSDR REXA201100196Skin · dentedTWO DENTS WERE FOUND PROTRUDING FROM THE FUSELAGE SKIN FWD OF ESC BAY DOOR AT FS 672 BETWEEN STRINGERS 26L AND 27. REPAIR DENTS IAW SRM 53-00-31 FIG 103 ALLOWABLE DAMAGE AND SRM 51-12-00 PAGE 21 REPAIR OF SMALL HOLES PAGE 22 FIG 7.Apr 2, 2011 · N827AY · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR REXA201000078Warning Light · false activationAT CRUISE ALTITUDE, ENROUTE, THE R REV UNLOCK MESSAGE ILLUMINATED. THE FLIGHT CREW COMPLETED THE QRH AND DETERMINED THAT THE THRUST REVERSER WAS NOT ACTUALLY DEPLOYED. FLIGHT CREW ELECTED TO PERFORM AN AIR RETURN. AN OTHERWISE NORMAL APPROACH AND LANDING WEMay 13, 2010 · N827AY · Cndair CL6002B19 · Engine Thrust ReverserSDR REX2008F00016Switch · inoperativeSTAB TRIM RUN AWAY. CAPTAIN`S SWITCH NOT FUNCTIONING. MAINTENANCE FOUND NO STAB TRIM RUN AWAY. THE CAPTAIN`S SWITCH WAS NOT CONTROLLING THE TRIM. SWITCH WAS REPLACED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. (K)Jul 11, 2008 · N827AY · Cndair CL6002B19 · Elevator Tab Control SystemSDR REXA200600114Warning Message · illuminatedRECEIVED FLAPS FAIL MESSAGE. SYSTEM RESET AND PLACED ON 72 HOUR WATCH PER AD 2006-12-21Dec 6, 2006 · N827AY · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR REXA200600112Flap System · malfunctionedRECEIVED FLAPS FAIL MESSAGE DECLARED EMERGENCY QRH FOLLOWED WITH UNEVENTFUL LANDING. SYSTEM RESET AND PLACED ON 72 HOUR WATCH PER AD 2006-12-21.Dec 3, 2006 · N827AY · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR REXA200600106Flap System · malfunctionedRECEIVED "FLAPS FAIL" MESSAGE ON DESCENT DIVERTED TO COS FOR FLAPS AND BAD WEATHER IN DEN. SYSTEM RESET AND PLACED ON 72 HOUR WATCH PER AD 2006-12-21Nov 28, 2006 · N827AY · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR REXA200500124Bpsu · failedFLAPS FAIL AT ZERO ON CLIMBOUT.Sep 24, 2005 · N827AY · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR REXA200500123Flap System · failedEMERGENCY DELCARED WHEN FLAPS FAILED AT 20 DEGREES ON APPROACH. LANDING UNEVENTFUL.Sep 16, 2005 · N827AY · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR REXA300500117Flap System · malfunctionedFLAPS FAILED AT 20 DEGEES ON APPROACH. COMPLIED WITH AD98-20-01. NO DISCREPANCIES NOTED. UNDER 72 HOURS FLAP WATCH.Sep 11, 2005 · N827AY · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR REXA200500117Control System · malfunctionedFLAPS FAILED AT 20 DEGREES ON APPROACH. COMPLIED WITH AD 98-20-01. NO DISCREPANCIES NOTED. UNDER 72 HOURS FLAP WATCH.Sep 11, 2005 · N827AY · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR REX2005F00005Control System · failed( REF NR: 05-102) FLAP FAILURE ENROUTE, AT 0. QRH FOLLOWED UNEVENTFUL LANING. RESET FLAPS AND PLACED ON 72 HOUR WATCH IAW AD 98-20-01. (K)Aug 25, 2005 · N827AY · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR REX2005F00021Warning Light · illuminated(REF NR: 05-082) FLAP FAIL CAUTION MESSAGE. QRH FOLLOWED. RESET FLAPS AND PLACED ON 72 HOUR WATCH IAW AD 98-20-01. (K)Jun 26, 2005 · N827AY · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR REX2005F00022Fcu · failed(REF NR: 05-081) FLAPS FAIL ON CLIMB-OUT. QRH FOLLOWED UNEVENTFUL LANDING. REMOVED AND REPLACED FLAP ELECTRONIC UNIT (FECU). (K)Jun 25, 2005 · N827AY · Cndair CL6002B19 · Trailing Edge Flap Control System
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