# Service difficulty reports: N829AY

A list on [N829AY](https://openairdocs.org/aircraft/N829AY.md).

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

- [SDR REXA2013030600547](https://openairdocs.org/sdr/REXA2013030600547.md): Battery Pack · inoperative · Mar 6, 2013 · N829AY · Cndair CL6002B19 · Emergency Lighting
  > FORWARD OVERHEAD CEILING EMERGENCY FLOOD LIGHT IS INOPERATIVE. REMOVED AND REPLACED BATTERY PACK IAW AMM 33-51-04.
- [SDR REXA2013022700371](https://openairdocs.org/sdr/REXA2013022700371.md): Vane · chafed · Feb 26, 2013 · N829AY · Cndair CL6002B19 · Trailing Edge Flaps
  > RIGHT INBOARD FLAP VANE LEADING EDGE HAS CHAFE DAMAGE IN 3 AREAS, FLAP STA137.012 AND 108.135 WERE WITHIN LIMTS OF BOMBARDIER REO 601R-57-52-004. DAMAGE AT FLAP STA 60.005 OUT OF LIMITS AND REPLACED.
- [SDR REXA2013022700374](https://openairdocs.org/sdr/REXA2013022700374.md): Bulkhead · gouged · Feb 25, 2013 · N829AY · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > AFT PRESSURE BULKHEAD AT FS 621 FOUND TO BE GOUGED IN 10 AREAS FROM WL 88.43 TO WL 102.43, BETWEEN LBL 18 AND RBL 36.2 UP TO 0.005" DEEP. REPAIRED IAW BOMBARDIER REO 601R-53-61-4818.
- [SDR REXA2013022700373](https://openairdocs.org/sdr/REXA2013022700373.md): Structure · corroded · Feb 25, 2013 · N829AY · Cndair CL6002B19 · Wing Miscellaneous Structure
  > WING PANEL ACCESS HOLE FOR PANEL 540BB AT WS 54.897 (HOLE 1) WAS FOUND CORRODED 0.003" DEEP. REPAIRED IAW BOMBARDIER REO 601R-57-21-030J.
- [SDR REXA2013022700372](https://openairdocs.org/sdr/REXA2013022700372.md): Structure · corroded · Feb 25, 2013 · N829AY · Cndair CL6002B19 · Wing Miscellaneous Structure
  > WING PANEL ACCESS HOLE FOR PANEL 650FB AT WS 274.319 (HOLE 14) WAS FOUND CORRODED 0.002" DEEP. REPAIRED IAW BOMBARDIER REO 601R-57-21-030J.
- [SDR REXA2013022700370](https://openairdocs.org/sdr/REXA2013022700370.md): Flap · dented · Feb 25, 2013 · N829AY · Cndair CL6002B19 · Trailing Edge Flaps
  > LEFT INBOARD FLAP INADVERTANTLY DROPPED DURING MAINTENANCE OPERATIONS AND DENTED IN SEVERL LOCATIONS. REPAIRED IAW SRM 57-52-00 REPAIR 3.
- [SDR REXA2013022700369](https://openairdocs.org/sdr/REXA2013022700369.md): Intercostal · cracked · Feb 25, 2013 · N829AY · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > INTERCOSTAL AT FS 484 IS CRACKED AT RBL 27 AND RBL 36. REPAIRED IAW BOMBARDIER REO 601R-53-41-059B.
- [SDR REXA2013022500342](https://openairdocs.org/sdr/REXA2013022500342.md): Fitting · cracked · Feb 25, 2013 · N829AY · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FS 280 CLIP CRACKED AT RBL 9. REPAIRED IAW BOMBARDIER REO 601R-53-11-136/601R-53-11-171.
- [SDR REXA2013022500341](https://openairdocs.org/sdr/REXA2013022500341.md): Fitting · cracked · Feb 25, 2013 · N829AY · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FS 280 CLIP CRACKED AT LBL 9. REPAIRED IAW BOMBARDIER REO 601R-53-11-136/601R-53-11-171.
- [SDR REXA2013022500340](https://openairdocs.org/sdr/REXA2013022500340.md): Angle · cracked · Feb 24, 2013 · N829AY · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FOUND UPPER AFT FLOOR ANGLE 2 EACH CRACKED AND FOUND LOWER FLOOR WEB 2 EACH CRACKS AT FS 280 LBL 9 AND RBL 9. REPAIRED IAW BOMBARDIER REO 601R-53-11-136/601R-53-11-171.
- [SDR REXA2013022500339](https://openairdocs.org/sdr/REXA2013022500339.md): Frame · corroded · Feb 24, 2013 · N829AY · Cndair CL6002B19 · Fuselage Main, Frame
  > FRAME AT FS 605 HAS CORROSION BETWEEN S-26L AND S-27. REPLACED IAW SRM 51-42-06 AND 51-42-21.
- [SDR REXA2013022500338](https://openairdocs.org/sdr/REXA2013022500338.md): Intercostal · cracked · Feb 24, 2013 · N829AY · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > INTERCOSTAL AT FS 484 IS CRACKED AT RBL 27 AND RBL 36. REPAIRED IAW BOMBARDIER REO 601R-53-41-059.
- [SDR REXA2013022200236](https://openairdocs.org/sdr/REXA2013022200236.md): Intercostal · cracked · Feb 19, 2013 · N829AY · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > INTERCOSTAL AT FS 484 IS CRACKED AT LBL 27 AND LBL 36. REPAIRED IAW BOMBARDIER REO 601R-53-41-059B.
- [SDR REXA2013010600112](https://openairdocs.org/sdr/REXA2013010600112.md): Life Vest · unserviceable · Jan 6, 2013 · N829AY · Cndair CL6002B19 · Life Jacket
  > INFANT LIFE VEST BAG TORN. REMOVED AND REPAIRED INFANT LIFE VEST IAW AMM 25-61-03.
- [SDR REXA2012121001757](https://openairdocs.org/sdr/REXA2012121001757.md): Unknown · malfunctioned · Dec 10, 2012 · N829AY · Cndair CL6002B19 · Landing Gear Brake System
  > ON LEFT BRAKE ONE BTMS SAYS 00 THE OTHER FOR THE LEFT BRAKE SAYS 05 DISCONNECTED AND RE-ATTACHED LEFT O/B BRAKE LINE QUICK DISCONNECT IAW AMM 32-43-26. LEFT O/B BRAKE CHECKS NORMAL. OK FOR SERVICE.
- [SDR REXA2012120701752](https://openairdocs.org/sdr/REXA2012120701752.md): Cover · unknown · Dec 7, 2012 · N829AY · Cndair CL6002B19 · Passenger Compartment Lighting
  > F/A NO SMOKING/FASTEN SEAT BELT SIGN IN GALLY NEEDS COVER REPLACED. 2LA007353-50. OPS CHECK OK. REMOVED AND REPLACED F/A GALLEY NO SMOKING LIGHT IAW CRJ200 AMM 33-24-00. THIS CLOSES OUT DM 76112.
- [SDR REXA2012112101695](https://openairdocs.org/sdr/REXA2012112101695.md): Life Vest · unserviceable · Nov 21, 2012 · N829AY · Cndair CL6002B19 · Life Jacket
  > ONE INFANT LIFE VEST HAS HOLE IN BAG. REMOVED AND REPLACED INFANT LIFE VEST IAW AMM 25-61-03.
- [SDR REXA2012110201549](https://openairdocs.org/sdr/REXA2012110201549.md): Light · inoperative · Nov 2, 2012 · N829AY · Cndair CL6002B19 · Emergency Lighting
  > MID AFT CABIN OVERHEAD EMERGENCY LIGHT INOPERABLE. REMOVED AND REPLACED BULB IAW AMM 33-21-01. OP CHECKS GOOD DM 74146 CLOSED.
- [SDR REXA2012081601264](https://openairdocs.org/sdr/REXA2012081601264.md): Bulb · inoperative · Aug 16, 2012 · N829AY · Cndair CL6002B19 · Emergency Lighting
  > RIGHT EMERGENCY OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED RIGHT OVERWING EMERGENCY LIGHT BULB NR 3 IAW AMM 33-51-21. OPS CHECKED GOOD.
- [SDR REXA2012021000216](https://openairdocs.org/sdr/REXA2012021000216.md): Pseu · malfunctioned · Feb 10, 2012 · N829AY · Cndair CL6002B19 · Landing Gear Position and Warning
  > AIR RETURN FOR PROX SYS FAULT STATUS IN FLIGHT IN CLIMBOUT THRU 10000. FOUND PSEU CODE A06 - NVRAM. REMOVED AND REPLACED PSEU & OP CHECK GOOD IAW AMM 32-61-01. OK FOR SVC.
- [SDR REXA201100429](https://openairdocs.org/sdr/REXA201100429.md): Bpsu · malfunctioned · Jun 26, 2011 · N829AY · Cndair CL6002B19 · Trailing Edge Flap Control System
  > CREW DECLARED EMERGENCY DUE TO FLAPS FAILED AT ZERO EN ROUTE. REMOVED AND REPLACED LT BPSU IAW AMM 27-51-10. FLAPS OP CHECK NORMAL IAW AMM 27-54-00. OK FOR SERVICE. PART EFFECTIVELY VERIFIED.
- [SDR REXA201100428](https://openairdocs.org/sdr/REXA201100428.md): Bpsu · malfunctioned · Jun 26, 2011 · N829AY · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLAPS FAIL AT 18 DEG OUTBOUND OF ROC. A/C DID AIR RETURN AND DECLARED AN EMERGENCY. REMOVED AND REPLACED BPSU IAW AMM 27-51-10.
- [SDR REXA201100427](https://openairdocs.org/sdr/REXA201100427.md): Flap · malfunctioned · Jun 25, 2011 · N829AY · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLAPS FAIL AT 0 ON CLIMBOUT DTW CREW DECLARED AN EMERGENCY ON APPROACH TO BUF RESET AND PLACED ON DI FOR 10 CYC.
- [SDR REXA201100404](https://openairdocs.org/sdr/REXA201100404.md): Flap · failed · Jun 20, 2011 · N829AY · Cndair CL6002B19 · Trailing Edge Flap Control System
  > CREW REPORTED FLAPS FAILED AT ZERO AFTER CLIMBOUT CONTINUED ON TO DTW LANDED WITHOUT INCIDENT. PERFORMED TROUBLESHOOTING PER BOMBARDIER FCM REV 39 IAW AD 2009-06-12 PARAGRAPH (H) (6) (I), AMOC DATED MARCH 27, 2009, TR 27-012 PER AMOL DATED DECEMBER 18, 2009 A
- [SDR REXA201100386](https://openairdocs.org/sdr/REXA201100386.md): Flap · malfunctioned · Jun 13, 2011 · N829AY · Cndair CL6002B19 · Trailing Edge Flap Control System
  > CREW REPORTED FLAPS FAIL CAUTION WITH FLAPS RETRACTED TO '0' AIRSPEED 200/250. DEFERRED FLAP SYSTEM IAW MEL 27-50-00 DM-45378.
- [SDR REXA201100248](https://openairdocs.org/sdr/REXA201100248.md): Bulkhead · chafed · Apr 20, 2011 · N829AY · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FWD FACE OF FS 621 BULKHEAD CHAFED IN 9 EACH PLACES NO DEEPER THAN 0.003 INCHES. REPAIRED IAW BOMBARDIER REO 601R-53-61-2155 AND 601R-53-61-4042.
- [SDR REXA201100218](https://openairdocs.org/sdr/REXA201100218.md): Yoke · scratched · Apr 11, 2011 · N829AY · Cndair CL6002B19 · Engine Mount Section
  > RIGHT FORWARD ENGINE MOUNT YOKE HAS FOUR SCRATCHES AT TOP FORWARD LUG ON FORWARD FACE. TWO SCRATCHES MEASURE.156 INCH LONG AND UP TO 0.025 INCH DEEP. TWO SCRATCHES MEASURE 0.375 INCH LONG AND UP TO 0.007 INCH DEEP. REPAIRED IAW BOMBARDIER REO 601R-71-21-04
- [SDR REXA201100183](https://openairdocs.org/sdr/REXA201100183.md): Panel · open · Mar 11, 2011 · N829AY · Cndair CL6002B19 · Aircraft Structures
  > LOUD NOISE COMING FROM THE NOSE OF THE A/C FOLLOWED BY A STALL FAIL MSG DURING INITIAL CLIMBOUT. FOUND PANEL 212BR OPEN. PERFORMED OPS CHECK ON STALL PROTECTION SYSTEM IAW 27-35-00.
- [SDR REXA201100123](https://openairdocs.org/sdr/REXA201100123.md): Web · canning · Feb 14, 2011 · N829AY · Cndair CL6002B19 · Passenger/Crew Doors
  > DAMAGE WAS FOUND ON THE AFT SIDE PANEL WEB OF THE MAIN PASSENGER DOOR STAIRS (P/N 601R31701-01, S/N 8029) NEAR THE TOP OF THE 2ND STEP (AT FS 349). THE DAMAGE IS OIL CANNING WITH A DENT PROTRUDING OUTWARD. ONLY THE WEB IS DAMAGED NO INTERNAL STRUCTURE IS AFF
- [SDR REXA201100109](https://openairdocs.org/sdr/REXA201100109.md): Skin · cracked · Feb 12, 2011 · N829AY · Cndair CL6002B19 · Spoilers
  > A DENT WAS FOUND ON THE UPPER SURFACE OF THE RIGHT WING OUTBOARD GROUND SPOILER (P/N 600-10502-56, S/N 3971165). THE DENT MEASURES 0.625 X 0.625 X 0.011 DEEP; IT IS 2.8 FROM THE OUTBOARD EDGE AND 2.0 FROM THE LEADING EDGE. REPAIRED IAW STS ENGINEERING EA 09-
- [SDR REXA201000041](https://openairdocs.org/sdr/REXA201000041.md): Warning System · malfunctioned · Apr 5, 2010 · N829AY · Cndair CL6002B19 · Central Warning
  > GEN 2 OFF CAUTION SVC NR 2 IDG IAW AMM 12-13-24. OPC GOOD THIS CLEARS DM 19630. OK FOR SERVICE.
- [SDR REXA200600046](https://openairdocs.org/sdr/REXA200600046.md): Flap · failed · Apr 7, 2006 · N829AY · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLAPS FAILED AT 30 DEGREES ON APPROACH. APPROACH ABORTED QRH FOLLOWED UNEVENTFUL LANDING. SYSTEM RESET AND PLACED ON 72 HOUR WATCH PER AD 98-20-01.
- [SDR REX200500137](https://openairdocs.org/sdr/REX200500137.md): Flap System · malfunctioned · Nov 15, 2005 · N829AY · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLAPS FAIL AT GATE. SYSTEM RESET AND PLACED ON 72 HOUR WATCH PER AD98-20-01.

## 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 = 'N829AY' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N829AY/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.