# Service difficulty reports: N825AY A list on [N825AY](https://openairdocs.org/aircraft/N825AY.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR REXA2013081401586](https://openairdocs.org/sdr/REXA2013081401586.md): Tire · worn · Aug 14, 2013 · N825AY · Cndair CL6002B19 · Tire > NOSE WHEEL STEERING FEELS LIKE IT HAS EXCESSIVE PLAY WHEN STEERING WITH RUDDER PEDALS. WHEN USING TILLER, FROM CENTER THE RESPONSE LAGS THEN FEELS LIKE IT OVER REACTS AND TRIES TO MAKE UP FOR INITAL LAG. PERFORMED CHECK OF NOSE WHEEL STEERING FEEDBACK IAW AMM - [SDR REXA2013040800618](https://openairdocs.org/sdr/REXA2013040800618.md): Bulkhead · cracked · Apr 7, 2013 · N825AY · Cndair CL6002B19 · Fuselage Main, Bulkhead > LEFT FS 621 BULKHEAD WEB AT WL 107 APPROX LINTEL FITTING CRACKED. REPAIRED IAW BOMBARDIER REO 601R-53-61-1230. - [SDR REXA2013040800620](https://openairdocs.org/sdr/REXA2013040800620.md): Bushing · worn · Apr 6, 2013 · N825AY · Cndair CL6002B19 · Trailing Edge Flaps > LEFT WING OUTBOARD FLAP INBOARD HINGE BUSHINGS WORN. REPAIRED IAW BOMBARDIER REO 601R-57-53-001 AND 601R-57-53-002. - [SDR REXA2013040800619](https://openairdocs.org/sdr/REXA2013040800619.md): Bushing · worn · Apr 6, 2013 · N825AY · Cndair CL6002B19 · Trailing Edge Flaps > LEFT WING OUTBOARD FLAP OUTBOARD HINGE BUSHINGS WORN. REPAIRED IAW BOMBARDIER REO 601R-57-53-001 AND 601R-57-53-002. - [SDR REXA2013040800621](https://openairdocs.org/sdr/REXA2013040800621.md): Structure · corroded · Apr 5, 2013 · N825AY · Cndair CL6002B19 · Fuselage Miscellaneous Structure > LBL 27 OUTBOARD FLOOR LANDING HAS CORROSION BETWEEN FS 574 AND FS 621 IN THE AFT CARGO BAY AT SEVERAL SPOTS. REPAIRED IAW BOMBARDIER REO 601R-53-61-3778. - [SDR REXA2013040600612](https://openairdocs.org/sdr/REXA2013040600612.md): Skin · chafed · Apr 3, 2013 · N825AY · Cndair CL6002B19 · Trailing Edge Flaps > LEFT WING INBOARD FLAP VANE INBOARD UPPER SKIN CHAFED. REPAIRED IAW SRM 51-42-13. - [SDR REXA2013040600611](https://openairdocs.org/sdr/REXA2013040600611.md): Hinge · gouged · Apr 3, 2013 · N825AY · Cndair CL6002B19 · Passenger/Crew Doors > PASSENGER DOOR HINGE DOOR SIDE GOUGED. REPAIRED IAW BOMBARDIER REO 601R-52-11-1347. - [SDR REXA2013020100211](https://openairdocs.org/sdr/REXA2013020100211.md): Drive Unit · failed · Feb 1, 2013 · N825AY · Cndair CL6002B19 · Trailing Edge Flap Control System > FLIGHT 3637. FLAPS FAILED CAUTION MESSAGE ON APPROACH. FAILED AT FLAPS ZERO. PERFORMED TROUBLESHOOTING PER FIM REV 44 IAW AM 2009-06-12 PARAGRAPH (H)(6)(I), PER AMOC DATED DECEMBER 07,2012 AND PA AD27-052J. REPLACED ALL ACTUATORS AND FLEX DRIVES. - [SDR REXA2013012100186](https://openairdocs.org/sdr/REXA2013012100186.md): Flex Drive · malfunctioned · Jan 23, 2013 · N825AY · Cndair CL6002B19 · Trailing Edge Flap Actuator > ON FLIGHT 4049 (MLI TO DTW) RECEIVED FLAPS FAIL MESSAGE AT 0 DEGREES ON APPROACH INTO DTW. PERFORMED TROUBLESHOOTING PER BOMBARDIER FIM REV 44 IAW AD 2009-06-12 PARAGRAPH(H)(6)(I). AMOC DATED DECEMBER 7,2012 AND PA AD27-052J. PERFORMED FREEZE CHECK OF ALL F - [SDR REXA201201250](https://openairdocs.org/sdr/REXA201201250.md): Battery · inoperative · Aug 10, 2012 · N825AY · Cndair CL6002B19 · Emergency Equipment > MAINTENANCE FOUND THAT FIRST OFFICERS EMERGENCY FLASHLIGHT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED FIRST OFFICERS EMERGENCY FLASHLIGHT BATTERY. OPS CHECK GOOD IAW AMM 25-61-01. - [SDR REXA2012080501234](https://openairdocs.org/sdr/REXA2012080501234.md): A/C Pack · smoke · Aug 5, 2012 · N825AY · Cndair CL6002B19 · Cabin Cooling System > FLIGHT 3711, TOILET SMOKE CAUTION MESSAGE ON DEPARTURE. SLIGHT ODOR OF SMOKE IN CABIN. AIR RETURNED & EMERGENCY DECLARED. REMOVED AND REPLACED COALESCER SOCKS IAW AMM 21-51-13. PERFORMED SMOKED AND FUMES WORK SCOPE. FOUND SMOKE COMING FROM RIGHT PACK BIN - [SDR REXA2012080401222](https://openairdocs.org/sdr/REXA2012080401222.md): Apu · malfunctioned · Aug 4, 2012 · N825AY · Cndair CL6002B19 · APU Core Engine > FLIGHT 3727. CREW REPORTED POSSIBLE SMOKE IN CABIN. OBSERVED FLUID LEAKING OUT OF AFT EQUIPMENT BAY. PERFORMED SMOKE AND FUMES CHECK PER WORK SCOPE IN THE CABIN AND FLIGHT DECK. VERIFIED FUMES ORIGINATED FROM MALFUNCTIONING APU. CLEANED ECS DUCTING AND - [SDR REXA2012080301223](https://openairdocs.org/sdr/REXA2012080301223.md): Unknown · unknown · Aug 3, 2012 · N825AY · Cndair CL6002B19 · Engine Thrust Reverser > RIGHT THRUST REVERSER WOULD NOT DEPLOY ON LANDING. TROUBLESHOT RIGHT HAND THRUST REVERSER VERIFIED RIG OF STOW, THROTTLE LOCKOUT AND DEPLOY SWITCHES IAW AMM 78-37-01. PERFORMED OPS CHECK OF THRUST REVERSER IAW AMM 71-00-00. OPS CHECKED GOOD. - [SDR REXA2012062701024](https://openairdocs.org/sdr/REXA2012062701024.md): Pdu · malfunctioned · Jun 27, 2012 · N825AY · Cndair CL6002B19 · Engine Thrust Reverser > RIGHT THRUST REVERSER DID NOT FULLY DEPLOY AND WILL NOT STOW. CHECKED RIGGING OF STOW, DEPLOY AND THROTTLE LOCKOUT SWITCHES IAW AMM 78-37-01. ALL GOOD. INSPECTED THRUST REVERSER PDU, PDU WILL NOT MANUALLY OPERATE. REMOVED AND REPLACED PDU IAW 78-32-03. VE - [SDR REXA2012040200459](https://openairdocs.org/sdr/REXA2012040200459.md): Bulb · inoperative · Apr 2, 2012 · N825AY · Cndair CL6002B19 · Emergency Lighting > LEFT MIDDLE EMERGENCY OVERWING BULB INOPERATIVE. REMOVED AND REPLACED EXTERIOR EMERGENCY LIGHT BULB IAW AMM 33-51-21. OPS CHECKED GOOD. - [SDR REXA201200108](https://openairdocs.org/sdr/REXA201200108.md): Tape · dislodged · Jan 10, 2012 · N825AY · Cndair CL6002B19 · Smoke Detection > UNSCHEDULED LANDING FOR MOMENTARY LAV SMOKE INDICATION IN LAV. REMOVED OLD SPEED TAPE, THAT HAD BECOME DISLOGED, REAPPLIED SPEED TAPE IAW PA 21-009. OK FOR SERVICE. - [SDR REXA201100997](https://openairdocs.org/sdr/REXA201100997.md): Ring · missing · Dec 20, 2011 · N825AY · Cndair CL6002B19 · Emergency Equipment > FLIGHT DECK DOOR LOWER ESCAPE RING PIN MISSING PULL RING. INSTALLED FLIGHT DECK DOOR PIN RING IAW AMM 20-00-00. - [SDR REXA201100806](https://openairdocs.org/sdr/REXA201100806.md): Knob · sticks · Nov 6, 2011 · N825AY · Cndair CL6002B19 · Rudder Tab Control System > RUDDER TRIM STICKS AND RUNS FULL DEFLECTION LEFT. CLEARED RUDDER TRIM KNOB. OPS CHECK GOOD IAW AMM 27-20-00. - [SDR REXA201100276](https://openairdocs.org/sdr/REXA201100276.md): Shaft · scored · May 12, 2011 · N825AY · Cndair CL6002B19 · Engine Mount Section > RT ENGINE THRUST SHAFT SCORED APPROXIMATELY 0.002 INCH ON THREADED END AROUND ENTIRE SURFACE. REPAIRED IAW BOMBARDIER CMM CMM 71-22-05. - [SDR REXA201100275](https://openairdocs.org/sdr/REXA201100275.md): Rib · chafed · May 12, 2011 · N825AY · Cndair CL6002B19 · Nacelle/Pylon, Frame/Spar/Rib > RT ENGINE PYLON OUTBOARD RIB P/N 601-37010-2 PRODUCTION RISER HAS CHAFE, OR FRETTING, DAMAGE AROUND THE DIAMETER ON RISER 0.0625 INCH LONG BY 0.002 INCH DEEP BEING THE WORST. - [SDR REXA201100274](https://openairdocs.org/sdr/REXA201100274.md): Bulkhead · damaged · May 11, 2011 · N825AY · Cndair CL6002B19 · Fuselage Main, Bulkhead > FS 621 BULKHEAD FORWARD FACE HAS 5 EACH TOOLING MARKS AT THE FOLLOWING LOCATION 1.5 INCH INBOARD OF LBL 9, 18, 27, AND 36. DAMAGE IS APPROXIMATELY.25" LONG X.25 WIDE X 0.004" DEEP AT WORST LOCATION. REPAIRED IAW BOMBARDIER REO 601R-53-61-2155. - [SDR REXA201100273](https://openairdocs.org/sdr/REXA201100273.md): Bulkhead · damaged · May 11, 2011 · N825AY · Cndair CL6002B19 · Fuselage Main, Bulkhead > FS 621 FORWARD FACE HAS 2 EACH TOOLING MARKS LOCATED APPROXIMATELY 2 INCHES ABOVE FLOOR AND 5 INCHES OUTBOARD OF RBL 18 AND 5 INCHES OUTBOARD OF RBL 36. DAMAGE IS APPROXIMATELY.25" LONG X.25" WIDE X 0.005" DEEP AT WORST LOCATION. REPAIRED IAW BOMBARDIER RE - [SDR REXA201100272](https://openairdocs.org/sdr/REXA201100272.md): Bulkhead · damaged · May 11, 2011 · N825AY · Cndair CL6002B19 · Fuselage Main, Bulkhead > FS 621 BULKHEAD FORWARD FACE HAS TOOLING MARKS APPROXIMATELY 0.250" WIDE X 0.250" WIDE X 0.007" DEEP AT WORST LOCATION AT THE FOLLOWING LOCATIONS 30" ABOVE FLOOR 1.5" INBOARD OF RBL 9, 18, 27, AND 36. REPAIRED IAW BOMBARDIER REO 601R-53-61-2155. - [SDR REXA201100268](https://openairdocs.org/sdr/REXA201100268.md): Rib · corroded · May 7, 2011 · N825AY · Cndair CL6002B19 · Nacelle/Pylon, Frame/Spar/Rib > LT PYLON OUTBOARD RIB P/N 601-37010-1 PRODUCTION RISER HAS FRETTING DAMAGE APPROXIMATELY 50 PERCENT AROUND CIRCUMFERENCE OR RISER 0.125 INCH WIDE BY 0.002 INCH DEEP AT DEEPEST AREA. REPAIRED IAW BOMBARDIER REO 601R-54-50-036 REV C. - [SDR REXA201100159](https://openairdocs.org/sdr/REXA201100159.md): Skin Panel · dented · Mar 7, 2011 · N825AY · Cndair CL6002B19 · Fuselage Main, Plate/Skin > THE AIRCRAFT WAS LOWERED ONTO TAIL STAND RESULTING IN SKIN, AND STRINGER DAMAGE BETWEEN FS 755 AND 67.5 PERCENT CANTED FRAME BETWEEN STRINGER 24L AND 23R. DAMAGE REPAIRED IAW EA 253-00002 AND 8110-3 DATED 3/6/11, STRINGERS S-25L TO S23R REPLACED. - [SDR REXA201000332](https://openairdocs.org/sdr/REXA201000332.md): Unknown · malfunctioned · Dec 28, 2010 · N825AY · Cndair CL6002B19 · Landing Gear Steering System > AIRCRAFT PERFORMED AN AIR RETURN BACK TO MEM FOR NLG STEERING INOP MSG IN FLIGHT. AIRCRAFT LANDED SAFELY AND PILOT RE-ENGAGED STEERING AFTER LANDING AND TAXIED TO THE GATE. CREW DID DECLARE AN EMERGENCY. AIRCRAFT IS STILL OUT OF SERVICE IN MEM HANGAR. - [SDR REX2008F00014](https://openairdocs.org/sdr/REX2008F00014.md): Landing Gear · malfunctioned · Jul 10, 2008 · N825AY · Cndair CL6002B19 · Nose/Tail Landing Gear > GEAR DISAGREE MESSAGE (NOSE NOT DOWN AND LOCKED) ON APPROACH, QRH FOLLOWED GEAR LOCKED DOWN EMERGENCY DECLARED WITH UNEVENTFUL LANDING. AFTER LANDING THE F/A REPORTED SMOKE COMING FROM ROW A. TROUBLESHOT SYSTEM IAW MM AND REPLACED THE NLG PRIORITY VALVE. GE - [SDR REXA200700065](https://openairdocs.org/sdr/REXA200700065.md): Switch · malfunctioned · Dec 11, 2007 · N825AY · Cndair CL6002B19 · Emergency Lighting > EMERGENCY LIGHTS WOULD NOT SHUTOFF ON ONE LOCATION. ANOTHER TIME EMERGENCY LIGHTS WOULD NOT TURN ON. - [SDR REXA200600109](https://openairdocs.org/sdr/REXA200600109.md): Flap System · malfunctioned · Dec 1, 2006 · N825AY · Cndair CL6002B19 · Trailing Edge Flap Control System > RECEIVED FLAP FAILURE MESSAGE AT FLIGHT LEVEL 290. QRH FOLLOWED AND ZERO FLAPS LANDING WITHOUT INCIDENT. RESET FLAPS AND PLACED ON 72 HOUR WATCH PER AD 2006-12-21 - [SDR REXA200600098](https://openairdocs.org/sdr/REXA200600098.md): Caution Message · illuminated · Oct 28, 2006 · N825AY · Cndair CL6002B19 · Trailing Flap Position Indicating System > FLAP FAIL CAUTION MESSAGE AT GATE. SYSTEM RESET AND PLACED ON 72 HOUR WATCH PER AD 2006-12-21. - [SDR REX2005F00037](https://openairdocs.org/sdr/REX2005F00037.md): Control System · out of rig · May 18, 2005 · N825AY · Cndair CL6002B19 · Trailing Edge Flap Control System > (REF NR: 05-066) FLAPS FIAL ON TAXI. QRH FOLLOWED, RETURNED TO BLOCKS. FLAP SYSTEM RIGGED IAW AMM. OPS CHECKED GOOD. (K) ## The whole list in SQL Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS: ```sql 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 = 'N825AY' AND registry_match = 'registration' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/aircraft/N825AY/reports --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.