# Service difficulty reports: N8580A

A list on [N8580A](https://openairdocs.org/aircraft/N8580A.md).

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

- [SDR REXA2013052200905](https://openairdocs.org/sdr/REXA2013052200905.md): Oxygen Mask · malfunctioned · May 22, 2013 · N8580A · Cndair CL6002B19 · Passenger Oxygen System
  > PASSENGER OXYGEN MASK AT SEAT 12AB FAILED TO DROP DURING FUNCTIONAL CHECK RE-PACKED MASK AND RE-LATCHED DOOR IAW CRJ 200 AMM 35-21-05. COMPLIED WITH OPERATIONAL TEST OF THE PASSENGER OXYGEN SYSTEM 2 TIMES IAW CRJ 200 AMM 35-20-00-00-710-801. NO DEFECTS NOTED
- [SDR REXA2013052100901](https://openairdocs.org/sdr/REXA2013052100901.md): Smoke Goggles · broken · May 21, 2013 · N8580A · Cndair CL6002B19 · Emergency Equipment
  > FIRST OFFICER'S SMOKE GOOGLES BROKEN. REMOVED AND REPLACED FIRST OFFICER'S SMOKE GOOGLES AS REQUIRED PER AMM 25-61-00. ALL CHECKS GOOD. OK FOR SERVICE.
- [SDR REXA2013050900879](https://openairdocs.org/sdr/REXA2013050900879.md): Defibrillator · unserviceable · May 9, 2013 · N8580A · Cndair CL6002B19 · Emergency Equipment
  > AED DEFIB MISSING GREEN SAFETY TAB AND ACCESSORY KIT. REPLACED WITH BREAK AWAY WIRE, CHECKS GOOD.
- [SDR REXA2013050600651](https://openairdocs.org/sdr/REXA2013050600651.md): Structure · corroded · May 3, 2013 · N8580A · Cndair CL6002B19 · Wing Miscellaneous Structure
  > LEFT WING LOWER WING ACCESS HOLES FOR PANELS 510AB AND 540BB CORRODED. REPAIRED IAW BOMBARDIER REO 601R-57-21-1921.
- [SDR REXA2013050600650](https://openairdocs.org/sdr/REXA2013050600650.md): Structure · corroded · May 3, 2013 · N8580A · Cndair CL6002B19 · Wing Miscellaneous Structure
  > RIGHT WING LOWER ACCESS HOLE FOR PANELS 640BB AND 650EB HAVE CORROSION. REPAIRED IAW BOMBARDIER REO 601R-57-21-1919.
- [SDR REXA2013050600649](https://openairdocs.org/sdr/REXA2013050600649.md): Bulkhead · chafed · May 3, 2013 · N8580A · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > MULTIPLE CHAFES DAMAGES TO THE FORWARD FACE OF THE FS 621 PRESSURE BULKHEAD FROM WL 73.5 TO WL 125.5, LBL 36 TO RBL 36. REPAIRED IAW BOMBARDIER REO 601R-53-61-2155 AND REO 601R-53-61-4895.
- [SDR REXA2013032000393](https://openairdocs.org/sdr/REXA2013032000393.md): Skin · damaged · Mar 18, 2013 · N8580A · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > DURING ROUTINE OPERATIONS AT IND MAINTENANCE FOUND THE FUSELAGE SKIN, STRINGER, AND FRAMES DAMAGED FROM FS 379 TO FS 394 AND BETWEEN S-19L AND S-23L. REPAIRED IAW EA CRJ253-01384 AND ASSOCIATED 8110-3.
- [SDR REXA2013021000284](https://openairdocs.org/sdr/REXA2013021000284.md): Cable · broken · Feb 10, 2013 · N8580A · Cndair CL6002B19 · Passenger/Crew Doors
  > ON FLIGHT 3747 (DTW TO YUL) THERE WAS AN INCREDIBLY LOUD NOISE FROM MAIN CABIN DOOR ON DEPARTURE. COMMUNICATIONS WITH FLIGHT ATTENDANT ALMOST IMPOSSIBLE DUE TO NOISE. HAPPENS COMING FROM RIGHT SIDE, WORSE AT HIGHER ALTITUDE/AIRSPEED. THE CREW DECLARED AN EM
- [SDR REXA2012090301313](https://openairdocs.org/sdr/REXA2012090301313.md): Light · inoperative · Sep 3, 2012 · N8580A · Cndair CL6002B19 · Emergency Lighting
  > EMERGENCY FLOOR LIGHTING INOPERATIVE ROW 1 THRU 6. REMOVED AND REPLACED LIGHT, OP CHECKED GOOD IAW AMM 33-51-00.
- [SDR REXA2012073101220](https://openairdocs.org/sdr/REXA2012073101220.md): Flap System · malfunctioned · Jul 31, 2012 · N8580A · Cndair CL6002B19 · Trailing Edge Flap Control System
  > AIRCRAFT REQUIRED EXTREME RIGHT WING DOWN AILERON TRIM AND NOSE LEFT RUDDER TRIM TO FLY STRAIGHT. ALSO AILERON FEEL IN CONTROLS IS VERY SLOPPY OVER 1 INCH OF LATERAL PLAY AT YOKE. CLEANED INBOARD FLAPS. REMOVED AND REPLACED INBOARD FLAP SEAL INSPECTED FLAPS
- [SDR REXA2012073101209](https://openairdocs.org/sdr/REXA2012073101209.md): Unknown · unknown · Jul 31, 2012 · N8580A · Cndair CL6002B19 · Aileron Control System
  > CREW REPORTED AILERONS FELT SLOPPY, OVER 1 INCH OF LATERAL PLAY AT YOKE. PERFORMED OPS TEST OF AILERON CONTROL SYSTEM NO DEFECTS NOTED. CREW REPORTED SLOP WITH TRIM OUT OF CENTER DETENT, NO DEFECTS NOTED IAW AMM 27-11-00-710-803.
- [SDR REXA2012071401161](https://openairdocs.org/sdr/REXA2012071401161.md): A/C Pack · seized · Jul 14, 2012 · N8580A · Cndair CL6002B19 · Cabin Cooling System
  > ON FINAL, DETECTED GUN POWDER BURNING ODOR. LEFT PACK CONTROLLER IN AUTO AND MANUAL, TEMP CONTINUED TO RISE ABOVE 100. ON ENTERING THE COCKPIT DISCOVERED THAT THE FLIGHT CREW LEFT THE LEFT PACK SWITCH ON THE "ON" POSITION. FURTHER TROUBLESHOOTING REVEALED
- [SDR REXA2012051800750](https://openairdocs.org/sdr/REXA2012051800750.md): Battery · unknown · May 18, 2012 · N8580A · Cndair CL6002B19 · Emergency Lighting
  > NR 2 EMERGENCY LIGHT BATTERY RS. REMOVED AND REPLACED NR 2 EMERGENCY BATTERY IAW AMM 33-51-04-04.
- [SDR REXA2012040100454](https://openairdocs.org/sdr/REXA2012040100454.md): Control Unit · failed · Apr 1, 2012 · N8580A · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLAPS FAIL AT 20 ON FINAL. NO EMERGENCY WAS DECLARED AND AIRCRAFT LANDED SAFELY. REPLACED FECU, OP CK GOOD
- [SDR REXA2012031900394](https://openairdocs.org/sdr/REXA2012031900394.md): Uplock · malfunctioned · Mar 16, 2012 · N8580A · Cndair CL6002B19 · Landing Gear Retraction/Extension System
  > LANDING GEAR DISAGREE ON APPROACH. NOSE GEAR DIDN’T INDICATE DOWN. QRH COMPLETED. REMOVED AND REPLACED NLG UPLOCK ASSY IAW AMM 32-33-05. OP CHECK, LEAK CK GOOD.
- [SDR REXA2012031200355](https://openairdocs.org/sdr/REXA2012031200355.md): Tab · out of adjust · Mar 12, 2012 · N8580A · Cndair CL6002B19 · Passenger/Crew Doors
  > MAIN CABIN DOOR HAS LOUD POPPING NOISE WHEN OPENING AND CLOSING DOOR GETS HUNG UP MOMENTARILY BEFORE OPENING AND CLOSING. MADE DOOR ADJUSTMENTS TO HINGE TABS. OPS CHK NORMAL W/REF TO CRJ AMM 52-11-00. OK FOR SVC.
- [SDR REXA2012030600342](https://openairdocs.org/sdr/REXA2012030600342.md): Battery · discharged · Mar 6, 2012 · N8580A · Cndair CL6002B19 · Emergency Equipment
  > F/A'S FLASHLIGHT INOP. REMOVED AND REPLACED F/A FLASHLIGHT BATTERY IAW AMM 25-61-02.
- [SDR REXA201101030](https://openairdocs.org/sdr/REXA201101030.md): Panel · malfunctioned · Dec 29, 2011 · N8580A · Cndair CL6002B19 · Autopilot System
  > YAW DAMPER 1 IS JAMMED, WILL NOT DISCONNECT. REMOVED AND REPLACED YAW DAMPER PANEL PER AMM 22-22-04. OPS CK GOOD. OK FOR SERVICE.
- [SDR REXA201100899](https://openairdocs.org/sdr/REXA201100899.md): Unknown · malfunctioned · Dec 3, 2011 · N8580A · Cndair CL6002B19 · Power Lever
  > LARGE DIFFERENCE BETWEEN KNOB AND A HALF WHEN RIGHT T/L BROUGHT TO IDLE WENT TO 150 PPH BEFORE GOING BACK TO 250. PERFORMED HIGH POWER ENGINE RUNS IAW AMM 71-00-00. ALL ENGINE PARAMETERS NORMAL. NO THROTTLE SPLIT NOTED. OK FOR SVC.
- [SDR REXA201100882](https://openairdocs.org/sdr/REXA201100882.md): Pump · inoperative · Nov 28, 2011 · N8580A · Cndair CL6002B19 · Fuel Boost Pump
  > MEL 28-23-01 RT FUEL PUMP INOP. REMOVED AND REPLACED RT BOOST PUMP IAW AMM 28-23-01. OPC GOOD. THIS CLEARS DM 55293. PLACARD REMOVED. "VERIFIED PART EFFECTIVITY."
- [SDR REXA201100536](https://openairdocs.org/sdr/REXA201100536.md): Warning System · activated · Aug 24, 2011 · N8580A · Cndair CL6002B19 · Drag Control System
  > ABORTED TAKEOFF IN LSE DUE TO CONFIG SPOILER WARNING MESSAGE AT APPROX 100 KNOTS AND ALL BRAKES NEVER EXCEEDED 7 ON THE BRAKE TEMPS.
- [SDR REXA201100260](https://openairdocs.org/sdr/REXA201100260.md): Angle · damaged · Apr 19, 2011 · N8580A · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > DAMAGED HOLE IN SPLICE ANGLE AT 3.2 INCH OUTBOARD OF STRINGER 25R AT FS 559. REPAIRED IAW BOMBARDIER REO 601R-53-41-1396.
- [SDR REXA201100189](https://openairdocs.org/sdr/REXA201100189.md): Wire Harness · defective · Mar 21, 2011 · N8580A · Cndair CL6002B19 · Door System Wiring
  > PASSENGER DOOR MASTER WARNING AT 33,000. CREW RAN QRH, MESSAGE CLEARED ON DESCENT, DIVERTED TO OMA. MAINTENANCE FOUND BURNT PIN AT P7MB. REPLACED DOOR HARNESS PER 52-70-04, OPS CHECK GOOD.
- [SDR REXA201000107](https://openairdocs.org/sdr/REXA201000107.md): Sill · corroded · Aug 22, 2010 · N8580A · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LOWER PASSENGER DOOR SILL AND CLEATS CORROSION. REMOVED AND REPLACED LOWER PASSENGER DOOR SILL AND CLEATS.
- [SDR REXA201000009](https://openairdocs.org/sdr/REXA201000009.md): Trim Switch · defective · Jan 14, 2010 · N8580A · Cndair CL6002B19 · Stabilizer Control System
  > STAB TRIM MACH TRIM CAUTION MESSAGES INFLIGHT. REMOVED AND REPLACED STAB TRIM DISENGAGE SWITCH IAW AMM 27-41-30. OPS CHECK GOOD. OK FOR SERVICE.
- [SDR REXA200600082](https://openairdocs.org/sdr/REXA200600082.md): A/C Pack · leaking · Sep 7, 2006 · N8580A · Cndair CL6002B19 · APU System Wiring
  > ON TAXI SMOKE APPEARED IN COCKPIT AND CABIN. LEFT ACM WAS ALREADY DEFERRED UNDER MEL RIGHT PACK DEFERRED BY OUTSTATION. LATER INVESTIGATION SUGGEST APU INTERNAL OIL LEAK. RIGHT PACK DEFER CLEARED AND APU DEFERRED PER MEL.
- [SDR REX2002F00008](https://openairdocs.org/sdr/REX2002F00008.md): Smoke Warning · false activation · May 24, 2002 · N8580A · Cndair CL6002B19 · Smoke Detection
  > AIRCRAFT HAD A LAVATORY SMOKE CAUTION MESSAGE IN FLIGHT. FLIGHT CREW DECLARED AN EMERGENCY AND AN OTHERWISE UNEVENTFUL LANDING WAS MADE. MAINTENANCE PERFORMED A SUCCESSFUL OPERATIONAL CHECK OF THE SMOKE DETECTION SYSTEM IAW APPROVED AMM PROCEDURES.

## 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 = 'N8580A' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N8580A/reports

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