# Service difficulty reports: N826AY

A list on [N826AY](https://openairdocs.org/aircraft/N826AY.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

- [SDR REXA2013030900386](https://openairdocs.org/sdr/REXA2013030900386.md): Skin · chafed · Mar 7, 2013 · N826AY · Cndair CL6002B19 · Wing, Plate/Skin
  > REMOVED CHAFE ON RIGHT WING FUEL CUTOUT PANEL LANDING 640BB, HOLE NR 1, IN THE NON-CRITICAL AREA WITHIN LIMITS IAW BOMBARDIER REO 601R-57-21-030 REV J.
- [SDR REXA2013030900385](https://openairdocs.org/sdr/REXA2013030900385.md): Angle · cracked · Mar 7, 2013 · N826AY · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RIGHT FS 280 BEAM LOWER ANGLE IS CRACKED AT VERTICAL POSTS JUST OUTBOARD OF RBL 9. REPAIRED IAW BOMBARDIER REO 601R-53-11-171.
- [SDR REXA2013030900384](https://openairdocs.org/sdr/REXA2013030900384.md): Angle · cracked · Mar 7, 2013 · N826AY · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RIGHT FLOOR SILL PLATE ANGLE OVERWING BOX CORRODED. REPAIRED IAW BOMBARDIER REO 601R-53-41-666.
- [SDR REXA2013030900383](https://openairdocs.org/sdr/REXA2013030900383.md): Angle · cracked · Mar 7, 2013 · N826AY · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LEFT FLOOR SILL PLATE ANGLE OVERWING BOX CORRODED. REPAIRED IAW BOMBARDIER REO 601R-53-41-666.
- [SDR REXA2013030900382](https://openairdocs.org/sdr/REXA2013030900382.md): Angle · cracked · Mar 7, 2013 · N826AY · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LEFT FS 280 BEAM LOWER ANGLE CRACKED JUST BELOW THE PULLEY BRACKET AND OUTBOARD OF LBL 9. REPAIRED IAW BOMBARDIER REO 601R-53-11-171.
- [SDR REXA2013030900381](https://openairdocs.org/sdr/REXA2013030900381.md): Angle · cracked · Mar 7, 2013 · N826AY · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LEFT FS 280 BEAM UPPER ANGLE IS CRACKED JUST OUTBOARD OF LBL 9. REPAIRED IAW BOMBARDIER REO 601R-53-11-138.
- [SDR REXA2013030900380](https://openairdocs.org/sdr/REXA2013030900380.md): Bulkhead · corroded · Mar 7, 2013 · N826AY · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > AFT CARGO COMPARTMENT FLOORBOARD LANDING CORRODED ON FWD FACE OF THE FS 621 BULKHEAD AT LBL 39. REPAIRED IAW BOMBARDIER REO 601R-53-61-117.
- [SDR REXA2013012300177](https://openairdocs.org/sdr/REXA2013012300177.md): Fuel Control · out of rig · Jan 23, 2013 · N826AY · Cndair CL6002B19 · Fuel Control/Turbine Engines
  > DURING START TO TAKE AIRCRAFT TO THE GATE RECEIVED HOT ICON, NO FUEL APPLIED, FLAMES COMING OUT OF ENGINE AND ENGINE FIRE BOTTLES WERE DISCHARGED. REMOVED AND REPLACED NR 2 FIRE BOTTLE IAW AMM 26-21-10. RIGGED RIGHT FUEL CONTROL IAW AMM 76-10-00. OK FOR SER
- [SDR REXA2013012100171](https://openairdocs.org/sdr/REXA2013012100171.md): Actuator · failed · Jan 21, 2013 · N826AY · Cndair CL6002B19 · Trailing Edge Flap Actuator
  > ON FLIGHT 3867 (BUF TO DTW) RECEIVED FLAPS FAIL AT 20 DEGREES ON APPROACH INTO DTW. PERFORMED TROUBLESHOOTING PER BOMBARDIER FIM REV 44 IAW AD2009-06-12 PARAGRAPH (H)(6)(I), AMOC DATED DECEMBER 07, 2012 AND PA AD27-052J (DOCUMENT WORK PERFORMED) INSPECTED FLA
- [SDR REXA2013011500145](https://openairdocs.org/sdr/REXA2013011500145.md): Light · inoperative · Jan 14, 2013 · N826AY · Cndair CL6002D24 · Emergency Lighting
  > CEILING EMERGENCY FLOOD LIGHT, LIGHT NR 1. RE-LAMP CEILING LEVEL EMERGENCY FLOOD LIGHT IAW 33-51-16.
- [SDR REXA2013123000051](https://openairdocs.org/sdr/REXA2013123000051.md): Priority Valve · malfunctioned · Dec 30, 2012 · N826AY · Cndair CL6002B19 · Landing Gear Retraction/Extension System
  > ON FLIGHT 4145 (PVD TO DTW) CREW RECEIVED NOSE GEAR DISAGREE MESSAGE AND THE CREW DECLARED AN EMERGENCY. HYDRAULIC PRESSURE SHOWED NORMAL (2900), NOSE GEAR STAYED DOWN (DID NOT RETRACT). MAIN GEAR RETRACTED NORMALLY. QRH COMPLETE. THE FLIGHT PERFORMED AN A
- [SDR REXA2012050300606](https://openairdocs.org/sdr/REXA2012050300606.md): Bracket · damaged · May 3, 2012 · N826AY · Cndair CL6002B19 · Landing Gear Position and Warning
  > AFTER T/O NOSE GEAR DID NOT RETRACT RECEIVED NOSE DOOR OPEN AND GEAR DISAGREE MASTER WARNING. COMPLIED SCENARIO 1 OF PA -05-018F AND FOUND CENTERING /OLEO EXTENSION PROX SENSOR BRACKET DAMAGED. SEE AML 2167904 DISC NR 2 FOR CORRECTIVE ACTION.
- [SDR REXA2012031300354](https://openairdocs.org/sdr/REXA2012031300354.md): Arm · unsecure · Mar 13, 2012 · N826AY · Cndair CL6002B19 · Fuselage, Equipment Attach Fittings
  > AIR RETURN FOR THE FOLLOWING: AFTER LIFT OFF, HEARD CLUNCKING IN RT NOSE AREA. FOUND RADOME SECURE ARMS UNSECURED AND FREE MOVING RESECURED ARMS IAW AMM 53-81-01.
- [SDR REXA201100884](https://openairdocs.org/sdr/REXA201100884.md): Wire · damaged · Nov 28, 2011 · N826AY · Cndair CL6002B19 · Electrical Power System Wiring
  > IDG 2 CAUTION MSG. EMERGENCY DECLARED. IDG 2 INTERMITTENT BUT MOSTLY ON AFTER FL170. REPAIRED WIRE TO RT IDG OVERTEMP SWITCH IAW ESPM 20-17-10. RECONNECTED RT IDG IAW AMM 24-11-01. OPC GOOD.
- [SDR REXA201100440](https://openairdocs.org/sdr/REXA201100440.md): Uplock · malfunctioned · Jul 4, 2011 · N826AY · Cndair CL6002B19 · Landing Gear Retraction/Extension System
  > GEAR UP DISAGREE WARNING MSG IN FLIGHT, AFTER QRH MSG CLEARED REMOVED AND REPLACED RT MLG UPLOCK IAW AMM 32-32-05. VERIFIED PART EFFECTIVITY & COMPLIED WITH PA 05-018B GEAR DISAGREE EVENT PROCEDURES.
- [SDR REXA201100347](https://openairdocs.org/sdr/REXA201100347.md): Bpsu · malfunctioned · Jun 6, 2011 · N826AY · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLAPS FAILED AT ZERO AFTER TAKEOFF CONTINUED ON, LANDED WITHOUT INCIDENT. /R RT BPSU IAW AMM 27-51-10 OP CHECK GOOD.
- [SDR REXA201100246](https://openairdocs.org/sdr/REXA201100246.md): Skin · dented · Apr 23, 2011 · N826AY · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > EXISTING FUSELAGE REPAIR DOUBLER JUST FORWARD OF FS 640 BETWEEN STRINGERS S-21R AND 23R FOUND DENTED. REPAIRED IAW BOMBARDIER SERVICE CORPORATION 601R-53-21208A AND ASSOCIATED 8110-3 DATED 4/21/11.
- [SDR REXA201100122](https://openairdocs.org/sdr/REXA201100122.md): Fastener · missing · Feb 14, 2011 · N826AY · Cndair CL6002B19 · Exterior Lighting
  > ONE OF THE STUD NUT FASTENERS (P/N CA2023-5) FOR THE RT WING LANDING RECOGNITION LIGHT WAS FOUND MISSING. TEMPORARY REPAIR IAW STS ENGINEERING EA 09-2011-040. REPEAT INSPECT EVERY 150 FH. WITHIN 500 FLIGHT HOURS, ACCOMPLISH A PERMANENT REPAIR TO THE DAMAGED
- [SDR REXA201100089](https://openairdocs.org/sdr/REXA201100089.md): Door Seal · leaking · Feb 7, 2011 · N826AY · Cndair CL6002B19 · Passenger/Crew Doors
  > FLT 3837 YOW-DTW DIVERTED TO YYZ HAD LOUD DOOR SQUEAL FOLLOWED BY LOSS OF PRESSURIZATION APPROX 45 MIN INTO THE FIGHT. EMERGENCY DESCENT TO 1000 FT. EMERGENCY DECLARED AND DIVERTED TO YYZ. A/C LANDED SAFELY IN YYZ. INSPECTED AND CLEANED DOOR SEAL AND DOOR
- [SDR REXA201000328](https://openairdocs.org/sdr/REXA201000328.md): Unknown · unknown · Dec 25, 2010 · N826AY · Cndair CL6002B19 · Cabin Pressure Control System
  > EN ROUTE AT FL290 FROM KBHM TO KDTW THE FLIGHT CREW DETECTED THE SOUND OF A HIGH PITCHED RUSHING AIR SOUND. CABIN ALTITUDE INDICATED A 1000-1300 FPM CLIMB. THE FLIGHT CREW DONNED O2 MASKS, DECLARED AN EMERGENCY AND BEGAN AN EMERGENCY DESCENT. ON DESCENT ARO
- [SDR REXA201000149](https://openairdocs.org/sdr/REXA201000149.md): Doubler · dented · Sep 17, 2010 · N826AY · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > DENT 2"L X 1.9"W X.075" DEEP, ON DOUBLER INSTALLED BETWEEN FS 640-625 AND STR 21R-23R PER PREVIOUS REO 601R-53-61-3563. FLY-ON FOR 1650 FH PER REO 601R-53-61-3823 TO NEXT C CHECK WHEN A PERMANENT REPAIR WILL BE PERFORMED.
- [SDR REXA200900077](https://openairdocs.org/sdr/REXA200900077.md): Acm · failed · Jul 13, 2009 · N826AY · Cndair CL6002B19 · Cabin Cooling System
  > ON TAXI, ODOR OF SMOKE NOTICED IN CABIN, RETURNED TO BLOCK. AIRCRAFT INSPECTED AND DETERMINED TO BE A FAILED RIGHT AIR CYCLE MACHINE (ACM). DEFERRED PER MEL RETURNED TO SERVICE.
- [SDR REX2009F00016](https://openairdocs.org/sdr/REX2009F00016.md): Smoke Detector · false indication · Jan 18, 2009 · N826AY · Cndair CL6002B19 · Smoke Detection
  > AFTER TAKE OFF RECEIVED LAVATORY SMOKE MSG WITH NO ACTUAL VISUAL SMOKE OR FUMES. TROUBLESHOT LAVATORY SMOKE DETECTION SYSTEM AND DETERMINED TO BE A FALSE SMOKE INDICATION. SYSTEM DEFERRED UNDER MEL 26-16-01.
- [SDR REXA200500131](https://openairdocs.org/sdr/REXA200500131.md): Actuator · failed · Oct 7, 2005 · N826AY · Cndair CL6002B19 · Trailing Edge Flap Actuator
  > FLAPS FAIL ON APPROACH WHEN SELECTED TO 30. FOLLOWED QRH, LANDED WITHOUT INCIDENT. REMOVED AND REPLACED LEFT INBOARD FLAP ACTUATORS POSITION 1 AND 2 P/N 852D100-19.
- [SDR REX2005F00042](https://openairdocs.org/sdr/REX2005F00042.md): Fcu · failed · May 6, 2005 · N826AY · Cndair CL6002B19 · Trailing Edge Flap Control System
  > (REF NR: 05-061) FLAPS FAIL AT ZERO ON CLIMB-OUT. QRH FOLLOWED, EMERGENCY DECLARED RETURNED TO DEPARTURE WITH UNEVENTFUL LANDING. REMOVED AND REPLACED FLAP ELECTRONIC CONTROL UNIT. (FECU) (K)
- [SDR REX2005F00043](https://openairdocs.org/sdr/REX2005F00043.md): Bpsu · failed · May 5, 2005 · N826AY · Cndair CL6002B19 · Trailing Edge Flap Control System
  > (REF NR: 05-060) FLAP FAIL MESSAGE UPON POWER UP. REMOVED AND REPLACED RT BRAKE POSITION SENSING UNIT (BPSU). (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 = 'N826AY' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N826AY/reports

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