# Service difficulty reports: N827AY

A list on [N827AY](https://openairdocs.org/aircraft/N827AY.md).

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

- [SDR REXA2013012700078](https://openairdocs.org/sdr/REXA2013012700078.md): Bulkhead · cracked · Jan 26, 2013 · N827AY · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > BULKHEAD WEB IS CRACKED AT FS 280, LBL 9, WL 70. REPAIRED IAW BOMBARDIER REO 601R-53-11-171.
- [SDR REXA2013012700077](https://openairdocs.org/sdr/REXA2013012700077.md): Bulkhead · cracked · Jan 26, 2013 · N827AY · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > BULKHEAD WEB IS CRACKED AT FS 280, RBL 9, WL 70. REPAIRED IAW BOMBARDIER REO 601R-53-11-171.
- [SDR REXA2013012700081](https://openairdocs.org/sdr/REXA2013012700081.md): Skin · chafed · Jan 24, 2013 · N827AY · Cndair CL6002B19 · Wing, Plate/Skin
  > FUEL PANEL 510AB LANDING ON LEFT WING LOWER SKIN IS CHAFED AND PITTED AT WS 12.245. REPAIRED IAW BOMBARDIER REO 601R-57-21-030.
- [SDR REXA2013012700080](https://openairdocs.org/sdr/REXA2013012700080.md): Skin · chafed · Jan 24, 2013 · N827AY · Cndair CL6002B19 · Wing, Plate/Skin
  > FUEL PANEL 640BB LANDING ON RIGHT WING LOWER SKIN IS CHAFED AND PITTED AT WS 54.897. REPAIRED IAW BOMBARDIER REO 601R-57-21-030.
- [SDR REXA2013012700079](https://openairdocs.org/sdr/REXA2013012700079.md): Skin · chafed · Jan 24, 2013 · N827AY · Cndair CL6002B19 · Wing, Plate/Skin
  > FUEL PANEL 540BB LANDING ON LEFT WING LOWER SKIN IS CHAFED AND PITTED AT WS 54.897. REPAIRED IAW BOMBARDIER REO 601R-57-21-030.
- [SDR REXA2013011100134](https://openairdocs.org/sdr/REXA2013011100134.md): Light · damaged · Jan 11, 2013 · N827AY · Cndair CL6002B19 · Emergency Lighting
  > EMERGENCY 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.
- [SDR REXA2012103001435](https://openairdocs.org/sdr/REXA2012103001435.md): Life Vest · unserviceable · Oct 30, 2012 · N827AY · Cndair CL6002B19 · Life Jacket
  > CAPTAIN & FIRST OFFICER'S LIFE VEST BAG TORN. REMOVED AND REPLACED CAPTAIN & FIRST OFFICER'S LIFE VESTS IAW AMM 25-61-03.
- [SDR REXA2012072401186](https://openairdocs.org/sdr/REXA2012072401186.md): Container · torn · Jul 24, 2012 · N827AY · Cndair CL6002B19 · Life Jacket
  > ONE INFANT LIFE VEST BAG TORN. REMOVED AND REPLACED ONE INFANT LIFE VEST IAW PA 25-096A.
- [SDR REXA201200021](https://openairdocs.org/sdr/REXA201200021.md): Control Quadrant · defective · Dec 30, 2011 · N827AY · Cndair CL6002B19 · Power Lever
  > ON 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 DUM
- [SDR REXA201100211](https://openairdocs.org/sdr/REXA201100211.md): Bulkhead · chafed · Apr 2, 2011 · N827AY · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > INTERNAL 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.
- [SDR REXA201100210](https://openairdocs.org/sdr/REXA201100210.md): Bulkhead · chafed · Apr 2, 2011 · N827AY · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > INTERNAL 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.
- [SDR REXA201100199](https://openairdocs.org/sdr/REXA201100199.md): Rivet · damaged · Apr 2, 2011 · N827AY · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > INTERNAL 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.
- [SDR REXA201100198](https://openairdocs.org/sdr/REXA201100198.md): Bulkhead · damaged · Apr 2, 2011 · N827AY · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > INTERNAL 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.
- [SDR REXA201100197](https://openairdocs.org/sdr/REXA201100197.md): Bulkhead · damaged · Apr 2, 2011 · N827AY · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > INTERNAL 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.
- [SDR REXA201100196](https://openairdocs.org/sdr/REXA201100196.md): Skin · dented · Apr 2, 2011 · N827AY · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > TWO 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.
- [SDR REXA201000078](https://openairdocs.org/sdr/REXA201000078.md): Warning Light · false activation · May 13, 2010 · N827AY · Cndair CL6002B19 · Engine Thrust Reverser
  > AT 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 WE
- [SDR REX2008F00016](https://openairdocs.org/sdr/REX2008F00016.md): Switch · inoperative · Jul 11, 2008 · N827AY · Cndair CL6002B19 · Elevator Tab Control System
  > STAB 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)
- [SDR REXA200600114](https://openairdocs.org/sdr/REXA200600114.md): Warning Message · illuminated · Dec 6, 2006 · N827AY · Cndair CL6002B19 · Trailing Edge Flap Control System
  > RECEIVED FLAPS FAIL MESSAGE. SYSTEM RESET AND PLACED ON 72 HOUR WATCH PER AD 2006-12-21
- [SDR REXA200600112](https://openairdocs.org/sdr/REXA200600112.md): Flap System · malfunctioned · Dec 3, 2006 · N827AY · Cndair CL6002B19 · Trailing Edge Flap Control System
  > RECEIVED FLAPS FAIL MESSAGE DECLARED EMERGENCY QRH FOLLOWED WITH UNEVENTFUL LANDING. SYSTEM RESET AND PLACED ON 72 HOUR WATCH PER AD 2006-12-21.
- [SDR REXA200600106](https://openairdocs.org/sdr/REXA200600106.md): Flap System · malfunctioned · Nov 28, 2006 · N827AY · Cndair CL6002B19 · Trailing Edge Flap Control System
  > RECEIVED "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 2006-12-21
- [SDR REXA200500124](https://openairdocs.org/sdr/REXA200500124.md): Bpsu · failed · Sep 24, 2005 · N827AY · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLAPS FAIL AT ZERO ON CLIMBOUT.
- [SDR REXA200500123](https://openairdocs.org/sdr/REXA200500123.md): Flap System · failed · Sep 16, 2005 · N827AY · Cndair CL6002B19 · Trailing Edge Flap Control System
  > EMERGENCY DELCARED WHEN FLAPS FAILED AT 20 DEGREES ON APPROACH. LANDING UNEVENTFUL.
- [SDR REXA300500117](https://openairdocs.org/sdr/REXA300500117.md): Flap System · malfunctioned · Sep 11, 2005 · N827AY · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLAPS FAILED AT 20 DEGEES ON APPROACH. COMPLIED WITH AD98-20-01. NO DISCREPANCIES NOTED. UNDER 72 HOURS FLAP WATCH.
- [SDR REXA200500117](https://openairdocs.org/sdr/REXA200500117.md): Control System · malfunctioned · Sep 11, 2005 · N827AY · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLAPS FAILED AT 20 DEGREES ON APPROACH. COMPLIED WITH AD 98-20-01. NO DISCREPANCIES NOTED. UNDER 72 HOURS FLAP WATCH.
- [SDR REX2005F00005](https://openairdocs.org/sdr/REX2005F00005.md): Control System · failed · Aug 25, 2005 · N827AY · Cndair CL6002B19 · Trailing Edge Flap Control System
  > ( 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)
- [SDR REX2005F00021](https://openairdocs.org/sdr/REX2005F00021.md): Warning Light · illuminated · Jun 26, 2005 · N827AY · Cndair CL6002B19 · Trailing Edge Flap Control System
  > (REF NR: 05-082) FLAP FAIL CAUTION MESSAGE. QRH FOLLOWED. RESET FLAPS AND PLACED ON 72 HOUR WATCH IAW AD 98-20-01. (K)
- [SDR REX2005F00022](https://openairdocs.org/sdr/REX2005F00022.md): Fcu · failed · Jun 25, 2005 · N827AY · Cndair CL6002B19 · Trailing Edge Flap Control System
  > (REF NR: 05-081) FLAPS FAIL ON CLIMB-OUT. QRH FOLLOWED UNEVENTFUL LANDING. REMOVED AND REPLACED FLAP ELECTRONIC UNIT (FECU). (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 = 'N827AY' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N827AY/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.