# Service difficulty reports: N8855A

A list on [N8855A](https://openairdocs.org/aircraft/N8855A.md).

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

- [SDR REXA2014121401193](https://openairdocs.org/sdr/REXA2014121401193.md): Light · inoperative · Dec 14, 2014 · N8855A · Cndair CL6002B19 · Emergency Lighting
  > AFT EMER LIGHT ON RT SIDE OF FUSELAGE INOPERATIVE. RELAMPED EMER LIGHT AT AFT RT FUSELAGE IAW AMM 33-51-21. OPERATIONS CHECKED GOOD.
- [SDR REXA2014110301109](https://openairdocs.org/sdr/REXA2014110301109.md): Life Vest · damaged · Nov 3, 2014 · N8855A · Cndair CL6002B19 · Life Jacket
  > INFANT LIFE VEST DAMAGED. R & R INFANT LIFE VEST IAW AMM 25-61-03. OK FOR SERVICE.
- [SDR REXA2014102401073](https://openairdocs.org/sdr/REXA2014102401073.md): Fire Bottle · low pressure · Oct 24, 2014 · N8855A · Cndair CL6002B19 · Fire Bottle, Portable
  > FLIGHT ATTENDANT FWD GALLEY FIRE EXTINGUISHER LOW. R & R FLIGHT ATTENDANT FWD FIRE EXTINGUISHER IAW AMM 26-23-01. OK FOR SERVICE.
- [SDR REXA2014090100853](https://openairdocs.org/sdr/REXA2014090100853.md): Cover · unknown · Sep 1, 2014 · N8855A · Cndair CL6002B19 · Emergency Lighting
  > EMERGENCY LIGHT STRIP COVER NEAR ROW 1 - 2 IS CABIN. INSTALLED EMER FLOOR LIGHT STRIP IAW AMM 33-51-01. ALL CHECKED GOOD, ACFT OK FOR SERVICE.
- [SDR REXA2014070600676](https://openairdocs.org/sdr/REXA2014070600676.md): Light · inoperative · Jul 7, 2014 · N8855A · Cndair CL6002B19 · Emergency Lighting
  > FLIGHT DECK EMER LIGHT MID CABIN NACK SIDE OUT. RELAMPED FLIGHT & EMER LIGHT AT MID CABIN SIGN IAW AMM 33-51-14 OK FOR SERVICE.
- [SDR REXA2014062400634](https://openairdocs.org/sdr/REXA2014062400634.md): Container · torn · Jun 26, 2014 · N8855A · Cndair CL6002B19 · Life Jacket
  > ONE INFANT LIFE VEST BAG TORN. R & R LIFE VEST IAW PA 25-096A.
- [SDR REXA2014062200626](https://openairdocs.org/sdr/REXA2014062200626.md): Connector · unsecure · Jun 22, 2014 · N8855A · Cndair CL6002B19 · Light System Wiring
  > CABIN FLOOR EMER LIGHTING NOT ILLUMINATING AFT OF THE OVERWING EMERGENCY EXIT. SECURED EMER LIGHTING CONNECTOR AT AFT END IAW AMM 33-51-01. LIGHT OPERATIONS CHECKED GOOD OK FOR SERVICE.
- [SDR REXA2014061200585](https://openairdocs.org/sdr/REXA2014061200585.md): Light · damaged · Jun 12, 2014 · N8855A · Cndair CL6002B19 · Emergency Lighting
  > FOUND EMER LIGHT STRIP ORANGE OVERLAY DAMAGED. REPLACED OVERLAY IAW AMM 33-51-01. ACFT OK FOR SERVICE.
- [SDR REXA2013090101721](https://openairdocs.org/sdr/REXA2013090101721.md): G Switch · failed · Sep 1, 2013 · N8855A · Cndair CL6002B19 · Emergency Locator Beacon
  > ELT FAILED G-SWITCH TEST. R & R ELT IAW AMM 25-61-01. OPS CHECKED GOOD.
- [SDR REXA2013060101061](https://openairdocs.org/sdr/REXA2013060101061.md): Stall Warning · false activation · Jun 1, 2013 · N8855A · Cndair CL6002B19 · Stall Warning System
  > STALL FAIL MASTER CAUTION ON CLIMB OUT, MESSAGE PERSISTED FOR DURATION OF FLIGHT IAW MOC PERFORMED FIM PROCEDURE PIT TEST MESSAGE CLEARED. OK FOR SERVICE.
- [SDR REXA2013052400910](https://openairdocs.org/sdr/REXA2013052400910.md): Throttle Cable · stuck · May 24, 2013 · N8855A · Cndair CL6002B19 · Power Lever
  > LEFT ENGINE THROTTLE CABLE STUCK AT 72% N1 IN AIR QRH COMPLETE, ENGINE SHUT DOWN IN THE FLIGHT FOR 2-15 MINUTES.
- [SDR REXA2013021000286](https://openairdocs.org/sdr/REXA2013021000286.md): Flashlight · inoperative · Feb 10, 2013 · N8855A · Cndair CL6002B19 · Emergency Equipment
  > CAPTAIN'S EMERGENCY FLASHLIGHT INOPERABLE. REPLACED FLASHLIGHT, OPS CHECK GOOD.
- [SDR REXA2012052200761](https://openairdocs.org/sdr/REXA2012052200761.md): Life Vest · unserviceable · May 22, 2012 · N8855A · Cndair CL6002B19 · Life Jacket
  > CAPTAIN`S LIFE VEST BAG TORN. REMOVED AND REPLACED CAPTAIN`S LIFE VEST IAW AMM 25-61-03.
- [SDR REXA2012051500737](https://openairdocs.org/sdr/REXA2012051500737.md): Detector · defective · May 15, 2012 · N8855A · Cndair CL6002B19 · Trailing Flap Position Indicating System
  > FLAP FAIL ON RETRACTION. PERFORMED TROUBLESHOOTING PER BOMBARDIER FIM REV 39 IAW AD2009-06-12 PARAGRAPH (H),(6),(1).AMOC DATED MARCH 27-2009,TR #27-012 D PER AMOC DATED DECEMBER 18,2009 AND PAAD27-052G, REMOVED AND REPLACED SKEW DETECTION UNIT IAW AMM 27-51-0
- [SDR REXA2012050900699](https://openairdocs.org/sdr/REXA2012050900699.md): Wire · damaged · May 9, 2012 · N8855A · Cndair CL6002B19 · Light System Wiring
  > ZONE NR 1 EMERGENCY LIGHTS INOP. PLACARD INSTALLED. REPAIRED DAMAGED WIRE LY73C22 IAW ESPM 20-11-00, SYSTEM OPC GOOD THIS CLEARS DM #63214, PLACARD REMOVED.
- [SDR REXA2012050900698](https://openairdocs.org/sdr/REXA2012050900698.md): Charger · defective · May 9, 2012 · N8855A · Cndair CL6002B19 · Emergency Lighting
  > NR 1 EMERGENCY BATT CHARGER ASSY FUSES ARE BAD. REMOVED AND REPLACED NR 1 EMERGENCY BATT CHARGER ASSY, SYSTEM OPC GOOD IAW CRJ200 AMM 33-51-00. A/C OK FOR SERVICE.
- [SDR REXA2012050700697](https://openairdocs.org/sdr/REXA2012050700697.md): Wire · damaged · May 7, 2012 · N8855A · Cndair CL6002B19 · Light System Wiring
  > LT & RT FWD EXTERNAL EMERG LIGHTS INOP. REPAIRED DAMAGED WIRE LY73C22 IAW ESPM 20-11-00, SYSTEM OPC GOOD THIS CLEARS DM #63328, PLACARD REMOVED.
- [SDR REXA2012031900400](https://openairdocs.org/sdr/REXA2012031900400.md): Flap · failed · Mar 19, 2012 · N8855A · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLAPS FAIL ON APPROACH AT 20. PERFORMED TROUBLESHOOTING PER BOMBARDIER FIM REV 39 IAW AD 2009-06-21 PARA H 6 I AMOC DATED MARCH 27, 2009 AND PA AD27-052G FOUND FAULT CODE FLAP LEVER FAULT AND 19C1 AND 19C2 CODES OK FOR RETURN TO SERVICE NO ACTION REQUIRED. A
- [SDR REXA2012031800398](https://openairdocs.org/sdr/REXA2012031800398.md): Lever · failed · Mar 18, 2012 · N8855A · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLAPS FAIL AT 20 DEGREES ON APPROACH. REPLACED FLAP LEVER.
- [SDR REXA2012030100326](https://openairdocs.org/sdr/REXA2012030100326.md): Trim Switch · inoperative · Mar 1, 2012 · N8855A · Cndair CL6002B19 · Stabilizer Control System
  > CAPT STAB TRIM SWITCH INOP F/O SWITCH AND AUTOTRIM WORKED NORMALLY. REMOVED AND REPLACED CAPT SIDE STAB TRIM SWITCH IAW AMM 27-41-05. ALL OPS CHECK GOOD. A/C OK FOR SVC.
- [SDR REXA201200113](https://openairdocs.org/sdr/REXA201200113.md): Transcowl · damaged · Jan 13, 2012 · N8855A · Cndair CL6002B19 · Engine Cowling System
  > RT TRANS COWL HIT BY SNOW PLOW. DAMAGE NOTED TO BE AS: DENT 7 1/2 IN LONG BY 3/8 WIDE WITH A CRACK IN THE OUTER SHELL 6" LONG BY 1/4 " DEEP. OVERALL PAINT SCRATCH 12 1/2 LONG AND 3 1/4 WIDE AT WIDEST POINT. CRACK DID NOT PUNCTURE INNER LINING. REMOVED AND R
- [SDR REXA201100948](https://openairdocs.org/sdr/REXA201100948.md): Angle · cracked · Dec 23, 2011 · N8855A · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FS 559 CAP ANGLE CRACKED AT RBL 18 AND LBL 18. REPAIRED IAW BOMBARDIER REO 601R-53-41-260 AND REO 601R-53-41-609 AS AUTHORIZED BY PA53-025.
- [SDR REXA201100750](https://openairdocs.org/sdr/REXA201100750.md): Bulkhead · cracked · Oct 25, 2011 · N8855A · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > AFT PRESSURE BULKHEAD CRACKED AT FS 621 LEFT SIDE LINTEL FITTING. REPAIRED IAW BOMBARDIER REO 601R-53-61-1230.
- [SDR REXA201100705](https://openairdocs.org/sdr/REXA201100705.md): Trim System · malfunctioned · Oct 12, 2011 · N8855A · Cndair CL6002B19 · Rudder Tab Control System
  > UNCOMMANDED RUDDER TRIM FULL NOSE LEFT. PERFORMED OPERATIONAL TEST OF RUDDER TRIM SYSTEM IAW AMM 27-21-00 NO FAULTS FOUND OK FOR SERVICE.
- [SDR REXA201100688](https://openairdocs.org/sdr/REXA201100688.md): Connector · unsecure · Oct 7, 2011 · N8855A · Cndair CL6002B19 · Light System Wiring
  > EMERGENCY TRACK FLOOR LIGHTING INOP AFT OF THE EMERGENCY EXIT ROW. RE-SECURED EMERGENCY FLOOR LIGHTING CONNECTOR ADJACENT TO LAV DOOR OPC GOOD.
- [SDR REXA201109280628](https://openairdocs.org/sdr/REXA201109280628.md): Connector · disconnected · Sep 28, 2011 · N8855A · Cndair CL6002B19 · Light System Wiring
  > EMERGENCY LIGHTS NOT WORKING. RECONNECTED EMERGENCY LIGHT IAW AMM 33-51-01. OPS CHECKED GOOD. ACFT OK FOR SERVICE.
- [SDR REXA201100621](https://openairdocs.org/sdr/REXA201100621.md): Warning System · false activation · Sep 25, 2011 · N8855A · Cndair CL6002B19 · Stabilizer Position Indicating
  > STAB CH 1 INOP POPPED UP 2 OR 3 TIMES DURING DESCENT. RESET, OPS CHECK GOOD IAW AMM 27-41-15. A/C OK FOR SERVICE.
- [SDR REXA201100388](https://openairdocs.org/sdr/REXA201100388.md): Coalescer Bag · dirty · Jun 16, 2011 · N8855A · Cndair CL6002B19 · Humidity Control System
  > ABORTED TAKEOFF AT 90 KTS FOR SMOKE IN COCKPIT AND CABIN. EMERGENCY DECLARED. AC TAXIED TO THE GATE AND DEPLANED NORMALLY. OUTSTATION MAINT: C/W MINIMUM WORKSCOPE SMOKE/FUMES IN CABIN/FLIGHT DECK. DTW MAINT: REMOVED AND REPLACED LT AND RT COALESCER SOCKS
- [SDR REXA201100179](https://openairdocs.org/sdr/REXA201100179.md): Fitting · elongated · Mar 18, 2011 · N8855A · Cndair CL6002B19 · Elevator Miscellaneous Structure
  > THE RIGHT ELEVATOR NR 2 HINGE ON HORIZONTAL STABILIZER FOUND TO HAVE OVERSIZED BUSHING HOLE (0.5650" D) ON INBOARD LUG. REPAIRED IAW BOMBARDIER SERVICE CORPORATION EO 601R-55-20931 AND 8110-3 DATED MARCH 16, 2011.
- [SDR REXA201100184](https://openairdocs.org/sdr/REXA201100184.md): Fitting · corroded · Mar 15, 2011 · N8855A · Cndair CL6002B19 · Passenger/Crew Doors
  > DISCOVERED CORROSION TO GUSSET CLIPS INSIDE PASSENGER DOOR AT HINGE AREA DURING PERFORMANCE OF AD2010-23-14. REMOVED AND REPLACED GUSSET CLIPS IAW SRM 51-42-06.
- [SDR REXA201100176](https://openairdocs.org/sdr/REXA201100176.md): Sill · corroded · Mar 13, 2011 · N8855A · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CARGO DOOR SILL PLATE CORRODED AT NUT PLATE HOLES FROM FS 511 TO 621. REPAIRED IAW BOMBARDIER GREO 601R-53-61-1574, SRM 51-42-21, 51-42-21.
- [SDR REXA201100175](https://openairdocs.org/sdr/REXA201100175.md): Beam · cracked · Mar 13, 2011 · N8855A · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FS 280 TRANVERSE BEAM IS CRACKED 1.0 INCH IN UPPER AND LOWER RADIUS AT LBL 10. FORWARD "J" ANGLE CORRODED. REPAIRED IAW BOMBARDIER REO 601R-53-11-926 AND BOMBARDIER SERVICE CORPORATION EO 601R-53-0110.
- [SDR REXA201100174](https://openairdocs.org/sdr/REXA201100174.md): Floorbeam · corroded · Mar 13, 2011 · N8855A · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > FLOORBEAM LBL 27 HAS MINOR CORROSION BETWEEN FS 574 AND 621. REPAIRED IAW SRM 51-42-21, 51-42-22, REO 601R53-61-3778.
- [SDR REXA201000004A](https://openairdocs.org/sdr/REXA201000004A.md): Seal · damaged · Jan 10, 2010 · N8855A · Cndair CL6002B19 · Main Landing Gear Strut/Axle/Truck
  > GEAR DISAGREE AND NOSE DOOR WARNING MSG, AND WOW INPUT AND STEERING INOP CAUTION MSG, AND WOW OUTPUT FAIL STATUS MSG WHEN RETRACTING THE GEAR AFTER T/O FROM 12L MSP. COMPLETED QRH RETURNED TO MSP. MTX FOUND DAMAGED NLG BUSHING BACK UP SEAL RESTRICTING STRUT

## 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 = 'N8855A' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N8855A/reports

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