# Service difficulty reports: N824AY

A list on [N824AY](https://openairdocs.org/aircraft/N824AY.md).

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

- [SDR REXA2013061701191](https://openairdocs.org/sdr/REXA2013061701191.md): Pbe · inoperative · Jun 17, 2013 · N824AY · Cndair CL6002B19 · Emergency Equipment
  > CAPTAIN`S PBE BLUE DOT NOT BLUE ANYMORE. R & R CREW MEMBER PBE IN COCKPIT IAW AMM 35-30-00.
- [SDR REXA2013032600410](https://openairdocs.org/sdr/REXA2013032600410.md): Skin · gouged · Mar 25, 2013 · N824AY · Cndair CL6002B19 · Wing, Plate/Skin
  > LEFT WING PLANK ACCESS HOLE FOR PANEL 510AB GOUGED 0.008" DEEP. REPAIRED IAW BOMBARDIER REO 601R-57-21-030.
- [SDR REXA2013032600409](https://openairdocs.org/sdr/REXA2013032600409.md): Skin · gouged · Mar 25, 2013 · N824AY · Cndair CL6002B19 · Wing, Plate/Skin
  > LEFT WING PLANK ACCESS HOLE FOR PANEL 540BB GOUGED 0.003" DEEP. REPAIRED IAW BOMBARDIER REO 601R-57-21-030.
- [SDR REXA2013032600408](https://openairdocs.org/sdr/REXA2013032600408.md): Skin · damaged · Mar 25, 2013 · N824AY · Cndair CL6002B19 · Wing, Plate/Skin
  > LEFT WING PLANK ACCESS HOLE FOR PANEL 550HB CHAFED AND GOUGED 0.002" DEEP. REPAIRED IAW BOMBARDIER REO 601R-57-21-030.
- [SDR REXA2013032500404](https://openairdocs.org/sdr/REXA2013032500404.md): Skin · chafed · Mar 24, 2013 · N824AY · Cndair CL6002B19 · Trailing Edge Flaps
  > RIGHT INBOARD FLAP TRAILING EDGE SKIN CHAFED NEAR CENTER. REPAIRED IAW SRM 57-52-00.
- [SDR REXA2013032500403](https://openairdocs.org/sdr/REXA2013032500403.md): Rib · cracked · Mar 22, 2013 · N824AY · Cndair CL6002B19 · Wing, Rib/Bulkhead
  > RIGHT MLG BATT RIB CRACKED. REPAIRED IAW BOMBARDIER REO 601R-57-51-046.
- [SDR REXA2013032200397](https://openairdocs.org/sdr/REXA2013032200397.md): Bulkhead · unknown · Mar 20, 2013 · N824AY · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FS 280 BULKHEAD WEB FOUND RIGHT OF RBL 9 AND LBL 9 AND UPPER AFT FLOOR ANGLE AT LBL 9. REPAIRED IAW BOMBARDIER REO 601R-53-11-136/601R-53-11-171.
- [SDR REXA2013032200396](https://openairdocs.org/sdr/REXA2013032200396.md): Seat Track · gouged · Mar 20, 2013 · N824AY · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > GOUGES ON BOTTOM OF SEAT TRACKS AT LBL 9 BETWEEN FS 508 AND FS 519 AND FS 542 - FS 554. REPAIRED IAW SRM 53-41-49.
- [SDR REXA2013032000394](https://openairdocs.org/sdr/REXA2013032000394.md): Bulkhead · damaged · Mar 19, 2013 · N824AY · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > MULTIPLE SCREW MARKS ON FS 621 BULKHEAD. REPAIRED IAW BOMBARDIER REO 601R-53-61-2155.
- [SDR REXA2013032200398](https://openairdocs.org/sdr/REXA2013032200398.md): Skin · chafed · Mar 18, 2013 · N824AY · Cndair CL6002B19 · Elevator, Plate/Skin
  > LEFT ELEVATOR HAS CHAFING ON INBOARD END OF UPPER SKIN CAUSED BY CONTACT WITH SEAL. BLENDED WITHIN LIMITS IAW SRM 55-00-31.
- [SDR REXA2012110101444](https://openairdocs.org/sdr/REXA2012110101444.md): Switch · out of adjust · Nov 1, 2012 · N824AY · Cndair CL6002B19 · Landing Gear Position and Warning
  > GEAR DISAGREE ON RETRACTION. GEAR EXTENSION-RETRACTION SYSTEM PLACED ON DEFERRAL. FOUND NLG OLEO STRUT EXTENSION S23 OUT OF LIMITS. RE-ADJUSTED PER AMM 32-61-05. PERFORMED GEAR SWING IN ACCORDANCE WITH AMM 32-30-00. OPS CHECK GOOD. THIS CLEARS DM# 74086
- [SDR REXA2012092801370](https://openairdocs.org/sdr/REXA2012092801370.md): Light · inoperative · Sep 28, 2012 · N824AY · Cndair CL6002B19 · Emergency Lighting
  > LEFT FWD EMERGENCY EXTERIOR LIGHT INOP. REMOVED AND REPLACED LEFT FWD EMERGENCY EXTERIOR LIGHT IAW CRJ 200 AMM 33-51-21.
- [SDR REXA2012082001280](https://openairdocs.org/sdr/REXA2012082001280.md): Relay · failed · Aug 20, 2012 · N824AY · Cndair CL6002B19 · Engine Thrust Reverser
  > RIGHT THRUST REVERSER WILL NOT DEPLOY PAST IDLE, FEELS LIKE LEVER GETS STUCK. REMOVED AND REPLACED RELAY 2K5KE IN JB 3 IAW ESPM 20-22-00. OPS CHECKED GOOD OF RIGHT THRUST REVERSER IAW AMM 78-30-00.
- [SDR REXA2012071901171](https://openairdocs.org/sdr/REXA2012071901171.md): Relay · failed · Jul 19, 2012 · N824AY · Cndair CL6002B19 · Engine Thrust Reverser
  > RIGHT THRUST REVERSER WILL NOT RELEASE FROM IDLE AFTER DEPLOYMENT. REMOVED AND REPLACED RELAY IN JB3 DESIGNATOR 2K6KE IAW AMM/CMM 24-01-03 AND WDM 91-32-03. OPS CHECKS AT LEAST 20 TIMES AND NO DEFECTS WERE NOTED.
- [SDR REXA2012071601165](https://openairdocs.org/sdr/REXA2012071601165.md): Computer · malfunctioned · Jul 16, 2012 · N824AY · Cndair CL6002B19 · Stall Warning System
  > STALL FAIL. PUSHER DOESN'T PUSH TO EITHER SIDE. REMOVED AND REPLACED STALL PROTECT COMPUTER AND OPS CHECKS GOOD IAW AMM 27-35-01. AIRCRAFT OK FOR SERVICE.
- [SDR REXA2012062401019](https://openairdocs.org/sdr/REXA2012062401019.md): Cable · out of rig · Jun 24, 2012 · N824AY · Cndair CL6002B19 · Power Lever
  > THRUST REVERSER WILL NOT DEPLOY. RIGGED THROTTLE GEAR BOX IAW AMM 76-11-17. OP`S CHECKED GOOD AT THIS TIME RIGGED ATR CABLE IAW AMM 78-35-01. OP`S CHECK GOOD.
- [SDR REXA2012060500818](https://openairdocs.org/sdr/REXA2012060500818.md): Throttle · failed · Jun 5, 2012 · N824AY · Cndair CL6002B19 · Power Lever
  > RT THRUST REVERSER HANDLE WILL NOT COME OUT OF IDLE DETENT. REMOVED AND REPLACED THROTTLE QUADRANT IAW AMM 76-11-01. RT THRUST REVERSER OPS CHECKED GOOD.
- [SDR REXA2012052900793](https://openairdocs.org/sdr/REXA2012052900793.md): Unknown · unknown · May 29, 2012 · N824AY · Cndair CL6002B19 · Engine Thrust Reverser
  > RIGHT THRUST REVERSER WILL NOT DEPLOY. PERFORMED OP`S CHECK OF RIGHT THRUST REVERSER IAW AMM 78-30-00. NO DEFECTS NOTED. OK FOR SERVICE.
- [SDR REXA2012051400731](https://openairdocs.org/sdr/REXA2012051400731.md): Switch · failed · May 14, 2012 · N824AY · Cndair CL6002B19 · Engine Thrust Reverser
  > RIGHT THRUST REVERSER NOT DEPLOYING, DEFER OUTBOARD IAW MEL 78-30-01 AUT NR 63568. REMOVED AND REPLACED DEPLOY SWITCH IAW AMM 78-37-01. OPS CHECK GOOD, CLEAR DM X63568 PLACARD REMOVED.
- [SDR REXA201100913](https://openairdocs.org/sdr/REXA201100913.md): Line · loose · Dec 7, 2011 · N824AY · Cndair CL6002B19 · Engine Oil Distribution (Airframe Furnished)
  > RIGHT OIL PRESS MASTER WARNING IN CRUISE FLT. CRUISE FLT 330 THE MSG WAS INTERMITTENT AND O2 PRESSURE INDICATION WAS ERRATIC. THE OIL PRESSURE CLIMBED AS WE DESCENDED BUT WASN’T STEADY OR IN A NORMAL RANGE UNTIL ABOUT 22000 FT. RE-SECURED LOOSE LINE ON SCAV
- [SDR REXA201100245](https://openairdocs.org/sdr/REXA201100245.md): Bulkhead · chafed · Apr 25, 2011 · N824AY · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FS 621.00 PRESSURE BULKHEAD HAS SCREW MARKS ON FWD SKIN ABOVE FLOOR AT WL 105.00, LBL 18, LBL 27, RBL 18, RBL 27, AND RBL 36. REPAIRED IAW BOMBARDIER REO 601R-53-61-2155.
- [SDR REXA201100243](https://openairdocs.org/sdr/REXA201100243.md): Skin · dented · Apr 25, 2011 · N824AY · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > AC SKIN DENTED AFT OF FS 280 BETWEEN S-24L AND 25L (LT SIDE AFT AND LEFT OF FWD JACK PAD). REPAIRED IAW BOMBARDIER REO 601R-53-21-1275.
- [SDR REXA201100242](https://openairdocs.org/sdr/REXA201100242.md): Bulkhead · cracked · Apr 25, 2011 · N824AY · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FS 202.75 PRESSURE BULKHEAD IS CRACKED AROUND THE PARKING BRAKE CONTROL CABLE HOLE ON INBOARD SIDE. REPAIRED IAW BOMBARDIER GREO 601R-53-11-563 AND BOMBARDIER SERVICE CORPORATION EO 601R-53-0101A.
- [SDR REXA201100247](https://openairdocs.org/sdr/REXA201100247.md): Skin · scratched · Apr 23, 2011 · N824AY · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN SCRATCHED AND DENTED AT FS 672 BETWEEN S-23R AND S-24R. REPAIRED IAW BOMBARDIER REO 601R-53-52-4048.
- [SDR REXA201100244](https://openairdocs.org/sdr/REXA201100244.md): Skin · dented · Apr 23, 2011 · N824AY · Cndair CL6002B19 · Trailing Edge Flaps
  > LEFT INBD FLAP UPPER SKIN SURFACE IS DENTED AT WS 63.49. REPAIRED IAW BOMBARDIER REO 601R-57-52-1544 AND BOMBARDIER SERVICE CORPORATION EO 601R-57-21207.
- [SDR REXA201100241](https://openairdocs.org/sdr/REXA201100241.md): Rivet · damaged · Apr 19, 2011 · N824AY · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FS 621 PRESSURE BULKHEAD HAS DAMAGED RIVETS AT WL 90, LBL 9, LBL 18, LBL 27, LBL 36, RBL 9, RBL 18, AND RBL 27. REPLACED DAMAGED RIVETS IAW SRM 51-42-06.
- [SDR REXA201000297](https://openairdocs.org/sdr/REXA201000297.md): Skin · damaged · Dec 11, 2010 · N824AY · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > WHILE BEING REPAINTED IN GLH A DENT WITH A SCRATCH IN THE FUSELAGE SKIN WAS DISCOVERED. THE DENT IS 3.75" X 1.0" X.078" DEEP, THE SCRATCH IS.004 DEEP. THE DAMAGE IS AT FS 654 - FS 672 BETWEEN STR 23R - STR 24R. FERRY FLIGHT FROM GLH TO MEM IAW BOMBARDIER
- [SDR REXA201000175](https://openairdocs.org/sdr/REXA201000175.md): Support Bracket · cracked · Oct 2, 2010 · N824AY · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > TWO CRACKS WERE FOUND IN THE LOWER AFT CORNER OF THE NR 2 HYDRAULIC RETURN SYSTEM SUPPORT BRACKET AT FUSELAGE STATION 718. THE FIRST CRACK IS 0.5 INCH LONG BEFORE IT TURNED AND PROCEEDED FOR AN ADDITION 0.25 INCH (TOTAL LINEAR LENGTH OF 0.75 INCH). A SECOND C
- [SDR REXA201000156](https://openairdocs.org/sdr/REXA201000156.md): Strip · damaged · Sep 22, 2010 · N824AY · Cndair CL6002B19 · Aerodynamic Fairings
  > RADOME LIGHTNING DIVERTER STRIP UPPER RT WITH 13.5 INCH REMAINING STRIP FROM LIE GOING BACK TO THE TIE: 6" THEN 3" THEN 4.5" FOR A TOTAL OF 13.5". FLY ON PER BOMBARDIER REO 601R-53-81-221 FOR 100 FH WITHIN WHICH TIME DAMAGE MUST BE REPAIRED OR RADOME MUST BE
- [SDR REXA200700045](https://openairdocs.org/sdr/REXA200700045.md): Unknown · odor · Mar 4, 2007 · N824AY · Cndair CL6002B19 · Cabin Compressor System
  > ON TAKEOFF GOT SMOKE AND SWEET BURNING ODOR. QRH FOLLOWED RETURNED TO AIRPORT. FOUND TO BE RESIDUAL DE-ICE FLUID IN ECS SYSTEM. ENGINE RUNS PERFORMED OPERATIONAL CHECKED GOOD
- [SDR REXA200600119](https://openairdocs.org/sdr/REXA200600119.md): Acm · smoke · Dec 19, 2006 · N824AY · Cndair CL6002B19 · Cabin Cooling System
  > ON APPROACH, HAD SMOKE/FUMES IN COCKPIT/CABIN WITH SMOKE MESSAGE. LEFT ACM PACK SHUTDOWN. MAINTENANCE DEFERRED LEFT PACK IAW MEL 21-51-11.
- [SDR REXA200600078](https://openairdocs.org/sdr/REXA200600078.md): Bracket · cracked · Jul 31, 2006 · N824AY · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > BRACKET FOUND CRACKED AT (JUST AFT OF) FWD MOST LUG. REMOVED AND REPLACED BRACKET IAW EO (REO) 601R-53-41-432.
- [SDR REXA200600008](https://openairdocs.org/sdr/REXA200600008.md): Trim Switch · dirty · Feb 3, 2006 · N824AY · Cndair CL6002B19 · Stabilizer Control System
  > STAB TRIM DISENGAGED AND WOULD NOT RESET. FOUND TRIM SWITCH STUCK. CLEANED AND LUBRICATED TRIM SWITCH, OPERATIONALLY CHECKS GOOD.
- [SDR REXA200500157](https://openairdocs.org/sdr/REXA200500157.md): Fuel Control · defective · Dec 14, 2005 · N824AY · Cndair CL6002B19 · Fuel Control/Turbine Engines
  > ON DESCENT, THE FLIGHT CREW DISCOVERED THAT THE RT ENGINE WAS UNRESPONSIVE TO THRUST LEVER INPUTS. THE FLIGHT CREW PERFORMED THE QRH AND DECLARED AN EMERGENCY. AN OTHERWISE UNEVENTFUL SINGLE ENGINE APPROACH AND LANDING WAS MADE. MAINTENANCE DISCOVERED THE MAI

## 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 = 'N824AY' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N824AY/reports

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