# Service difficulty reports: N8631E

A list on [N8631E](https://openairdocs.org/aircraft/N8631E.md).

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

- [SDR REXA2013021600301](https://openairdocs.org/sdr/REXA2013021600301.md): Control Unit · defective · Feb 16, 2013 · N8631E · Cndair CL6002B19 · Landing Gear Steering System
  > ON FLIGHT 3885 (JFK TO PHL) STEERING INOPERABLE CAUTION MESSAGE ILLUMINATED ON DEPATRURE FROM JFK ONCE THE GEAR WAS RETRACTED. FOLLOWED QRH DID NOT ALTER MESSAGE. STEERING DID NOT RESET AND CREW ADVISED THAT THEY WOULD NEED TOW TO CLEAR RUNWAY ON HIGH SPEED.
- [SDR REXA201201360](https://openairdocs.org/sdr/REXA201201360.md): Warning System · false activation · Sep 22, 2012 · N8631E · Cndair CL6002B19 · Trailing Flap Position Indicating System
  > ON FLIGHT 4015 DURING APPROACH INTO CHS RECEIVED FLAPS FAIL MESSAGE AT 20 DEGREES. NO EMERGENCY WAS DECLARED AND THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. PERFORMED TROUBLESHOOTING PER BOMBARDIER REV 43 IAW AD 2009-06-12 PARAGRAPH (H) (6)(I), AMOC DATED AP
- [SDR REXA0829201201298](https://openairdocs.org/sdr/REXA0829201201298.md): Light · inoperative · Aug 29, 2012 · N8631E · Cndair CL6002B19 · Emergency Lighting
  > CEILING EMERGENCY LIGHT OVER ROW 1 IS INOPERATIVE. REMOVED AND REPLACED CEILING EMERGENCY LIGHT OVER ROW 1 IAW AMM 33-51-16. OPS CHECKED GOOD. AIRCRAFT OK FOR SERVICE.
- [SDR REXA2012071201068](https://openairdocs.org/sdr/REXA2012071201068.md): Trim System · malfunctioned · Jul 12, 2012 · N8631E · Cndair CL6002B19 · Stabilizer Control System
  > STAB TRIM & MACH TRIM DISCONNECTS ON APPROACH, ONLY WHEN FLAPS LOWERED AND CAPTAIN TRIM CONTROL SWITCH USED. COULD NOT DUPLICATE ON GROUND. PERFORMED CONTINUITY, RESISTANCE CHECKS IAW ESPM 20-12-0 AND WM 27-41-00. NO DEFECTS NOTED. REMOVED AND REPLACED MC
- [SDR REXA2012071101062](https://openairdocs.org/sdr/REXA2012071101062.md): Switch · failed · Jul 11, 2012 · N8631E · Cndair CL6002B19 · Stabilizer Control System
  > STAB TRIM MACH TRIM DISENGAGES WHEN TRIM IS USED OR WHEN YOKE IS JOSTLED. REMOVED AND REPLACED CAPTAIN'S STAB TRIM DISENGAGE SWITCH. OPS CHECKED GOOD IAW AMM 27-41-30.
- [SDR REXA2012062600865](https://openairdocs.org/sdr/REXA2012062600865.md): Skin · dented · Jun 25, 2012 · N8631E · Cndair CL6002B19 · Trailing Edge Flaps
  > RIGHT OUTBOARD FLAP LOWER SKIN DENTED BETWEEN FLAP STATION 178.13 AND 226.13. REPAIRED IAW BOMBARDIER REO 601R-57-53-938.
- [SDR REXA2012051300734](https://openairdocs.org/sdr/REXA2012051300734.md): Drag Angle · cracked · May 13, 2012 · N8631E · Cndair CL6002B19 · Passenger/Crew Doors
  > AFT PASSENGER DOOR DRAG ANGLE CRACKED. REPAIRED PASSENGER DOOR DRAG ANGLE IAW REO 601R-52-11-513 REV A.
- [SDR REXA2010427200580](https://openairdocs.org/sdr/REXA2010427200580.md): Light · inoperative · Apr 27, 2012 · N8631E · Cndair CL6002B19 · Emergency Lighting
  > EXTERIOR EMERGENCY LIGHT AT SERVICE DOOR INOPERATIVE. REMOVED AND REPLACED RT FWD, AFT EXTERNAL EMERGENCY LIGHTS, OPS CHECKED GOOD IAW AMM 33-51-21.
- [SDR REXA2012042700579](https://openairdocs.org/sdr/REXA2012042700579.md): Proximity Switch · out of rig · Apr 27, 2012 · N8631E · Cndair CL6002B19 · Landing Gear Position and Warning
  > UPON GEAR RETRACTION HAD A NOSE GEAR DISAGREE MESSAGE. INTERROGATED PSEU & FOUND 2 EVENTS FAULTS ON S23 (PS14GA) INSPECTED & MEASURED PRO SWITCH PS14GA AND FOUND TO BE OUT OF LIMITS. RERIGGED PROX SWITCH PS14GA IAW AMM32-61-05. OPS CHECK GOOD. PERFORMED GE
- [SDR REXA2012022000266](https://openairdocs.org/sdr/REXA2012022000266.md): Battery · inoperative · Feb 20, 2012 · N8631E · Cndair CL6002B19 · Emergency Equipment
  > FLIGHT ATTENDANT FLASHLIGHT INOPERATIVE. REMOVED AND REPLACED FA FLASHLIGHT BATTERY IAW AMM 25-61-04, OPS CHECKED GOOD.
- [SDR REXA201200015](https://openairdocs.org/sdr/REXA201200015.md): Beam · damaged · Jan 24, 2012 · N8631E · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RIGHT BEAM IN NLG WHEEL WELL AT FS 202.75 HAS 1.5" OF MISSING MATERIAL FROM FREE FLANGE AND A CRACK MEASURING.5" PROPAGATING FROM THE TOP OF THE MISSING MATERIAL AND INTO THE BEND RADIUS. REPAIRED IAW BOMBARDIER REO 601R-53-11-2272.
- [SDR REXA201200104](https://openairdocs.org/sdr/REXA201200104.md): Warning System · false activation · Jan 8, 2012 · N8631E · Cndair CL6002B19 · Pitot/Static Anti-Ice System
  > AIR RETURN FOR L AOA HEAT CAUTION MSG IN FLIGHT (1500 FT AGL DEPARTING) RAN QRH-MSG PERSISTED. RESET CB IAW AMM 30-31-15. OPS CHECKED GOOD MESSAGE CLEARED.
- [SDR REXA201100509](https://openairdocs.org/sdr/REXA201100509.md): Ecu · malfunctioned · Aug 4, 2011 · N8631E · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLAPS STUCK AT 20 DEGREES AFTER TAKEOFF. AIR RETURN & CREW DECLARED AN EMERGENCY. REMOVED AND REPLACED FECU IAW AMM 27-50-00, OPS CHECK GOOD.
- [SDR REXA201100508](https://openairdocs.org/sdr/REXA201100508.md): Flap · failed · Aug 4, 2011 · N8631E · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLAP FAILED AT ZERO, PLACED ON MEL 27-50-00.
- [SDR REX2008F00045](https://openairdocs.org/sdr/REX2008F00045.md): Bpsu · malfunctioned · Aug 22, 2008 · N8631E · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLAP FAIL MESSAGE IN CRUISE. FLAP ELECTRONIC CONTROL UNIT (FECU) INTERROGATED FAULT CODES LOGGED 1. RT BPSU (BRAKE POSITION SENSING UNIT) 2. FECU 3. WIRING RT BPSU. 12 1B AND 12 2B. R&R THE RT BPSU PER BOMBARDIER AMM OPS CHECK PERFORMED ALONG WITH A FUNCTI
- [SDR REX2008F00040](https://openairdocs.org/sdr/REX2008F00040.md): Bpsu · malfunctioned · Aug 15, 2008 · N8631E · Cndair CL6002B19 · Trailing Edge Flap Control System
  > RECEIVED "FLAP FAIL" MESSAGE IN CRUISE. QRH FOLLOWED. EMERGENCY DECLARED FOLLOWED BY UNEVENTFUL LANDING. REMOVED AND REPLACED RT WING BRAKE POSITION SENSING UNIT (BPSU) IAW BOMBARDIER AMM, OPERATIONALLY CHECK FLAPS. (S)
- [SDR REX2008F00036](https://openairdocs.org/sdr/REX2008F00036.md): Bpsu · failed · Aug 15, 2008 · N8631E · Cndair CL6002B19 · Trailing Edge Flap Control System
  > RECEIVED "FLAP FAIL" MESSAGE IN CRUISE, QRH FOLLOWED. EMERGENCY DECLARED FOLLOWED BY UNEVENTFUL LANDING. REMOVED AND REPLACED RIGHT WING BRAKE POSITION SENSING UNIT (BPSU) IAW BOMBARDIER AMM, OPERATIONALLY CHECK FLAPS. (S)
- [SDR REX2008F00042](https://openairdocs.org/sdr/REX2008F00042.md): Flap System · malfunctioned · Aug 14, 2008 · N8631E · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLAP FAILURE MESSAGE IN CRUISE FL330. OVERSPEED WARNING SOUNDING THEN FLAP FAILURE AT ZERO. QRH FOLLOWED, DIVERTED TO IAD, DECLARED EMERGENCY WITH UNEVENTFUL LANDING. TROUBLESHOT PER BOMBARDIER FIM AND AMM. ALL LRUS PASSED. VERIFIED RIGGING OF THE LT AND
- [SDR REX2008F00038](https://openairdocs.org/sdr/REX2008F00038.md): Flap System · malfunctioned · Aug 14, 2008 · N8631E · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLAP FAILURE MESSAGE IN CRUISE FL330. OVERSPEED WARNING SOUNDING THEN FLAP FAILURE AT ZERO. QRH FOLLOWED. DIVERTED TO IAD, DECLARED EMERGENCY WITH UNEVENTFUL LANDING. TROUBLESHOT PER BOMBARDIER FIM AND AMM, ALL LRUS PASSED. VERIFIED RIGGING OF THE LT AND
- [SDR REX2008F00032](https://openairdocs.org/sdr/REX2008F00032.md): Unknown · unknown · Aug 10, 2008 · N8631E · Cndair CL6002B19 · Central Warning
  > AT FL 260 280KTS RECEIVED OVERSPEED CLACKER THEN FLAPS HALF SPEED FOLLOWED BY FLAPS FAIL MESSAGE. QRH FOLLOWED, DECLARED EMERGENCY WITH UNEVENTFUL LANDING. FLAPS RESET PER FIM AND PLACED ON 72 HOUR WATCH AD 2006-12-21. (S)
- [SDR REX2008F00034](https://openairdocs.org/sdr/REX2008F00034.md): Fcu · malfunctioned · Aug 5, 2008 · N8631E · Cndair CL6002B19 · Trailing Edge Flap Control System
  > IN CRUISE RECEIVED SPEED CLACKER FOLLOWED BY FLAP FAIL MESSAGE. QRH FOLLOWED, EMERGENCY DECLARED LAND WITH FLAPS AT ZERO UNEVENTFUL. REMOVED AND REPLACED THE FLAP ELECTRONIC CONTROL UNIT (FECU) PER BOMBARDIER AMM. OPERATIONAL CHECK PERFORMED. (S)
- [SDR REXA08028](https://openairdocs.org/sdr/REXA08028.md): Flap System · malfunctioned · Jul 17, 2008 · N8631E · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLAP FAIL AT ZERO ON APPROACH. QRH FOLLOWED, EMERGENCY DECLARED WITH UNEVENTFUL LANDING. RESET FLAPS AND PLACED ON 72 HOUR WATCH. (S)
- [SDR REX2008F00002](https://openairdocs.org/sdr/REX2008F00002.md): Bpsu · malfunctioned · Jun 28, 2008 · N8631E · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLAP FAIL MESSAGE DURING CRUISE, QRH FOLLOWED, EMERGENCY DECLARED. LANDED WITHOUT INCIDENT. FLAP SYSTEM RESET PER BOMBARDIER FIM AND PLACED ON 72 HOUR WATCH. THE 72 HOUR WATCH PERIOD CLEARED BY REMOVING AND REPLACING THE RT BRAKE POSITION SENSING UNIT (BPSU

## 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 = 'N8631E' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N8631E/reports

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