# Service difficulty reports: N8492C

A list on [N8492C](https://openairdocs.org/aircraft/N8492C.md).

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

- [SDR REXA2014010100102](https://openairdocs.org/sdr/REXA2014010100102.md): Container · torn · Jan 1, 2014 · N8492C · Cndair CL6002B19 · Life Jacket
  > CAPTAIN`S LIFE VEST BAG TORN. R & R CAPTAIN`S LIFE VEST IAW AMM 25-61-03.
- [SDR REXA2013111802260](https://openairdocs.org/sdr/REXA2013111802260.md): Connector · broken · Nov 18, 2013 · N8492C · Cndair CL6002B19 · Light System Wiring
  > EMERGENCY LIGHT STRIP FWD FLOOR CONNECTOR AT PANEL 231ALF IS BROKE OFF. REPLACED EMERGENCY LIGHT STRIP FWD FLOOR CONNECTOR AT PANEL 231ALF IAW CRJ 200 ESPM 20-17-31. IAW TO WORK ORDER 54183/2000/0098 FOR OPERATIONS CHECK.
- [SDR REXA2013111001172](https://openairdocs.org/sdr/REXA2013111001172.md): Lug · corroded · Nov 8, 2013 · N8492C · Cndair CL6002B19 · Wing, Attach Fittings
  > RIGHT INBD FLAP, INBD HINGE BOX ON WING INBD LUG, SHOWS SIGNS OF CORROSION COMMON TO THE BUSHING. REPAIRED IAW REO 601R-57-21-2027.
- [SDR REXA2013111001171](https://openairdocs.org/sdr/REXA2013111001171.md): Lug · corroded · Nov 8, 2013 · N8492C · Cndair CL6002B19 · Wing, Attach Fittings
  > LEFT INBD FLAP, INBD HINGE BOX ON WING INBD LUG SHOWS SIGNS OF CORROSION COMMON TO THE BUSHING. REPAIRED IAW REO 601R-57-21-2027.
- [SDR REXA2013103001169](https://openairdocs.org/sdr/REXA2013103001169.md): Bulkhead · chafed · Oct 28, 2013 · N8492C · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > AFT PRESSURE BULKHEAD AT FS 621, WL 110.5, LBL 42.7 CHAFED. REPAIRED IAW REOS 601R-53-61-2155, 601R-53-61-1230, AND 601R-53-61-5069.
- [SDR REXA201310280168](https://openairdocs.org/sdr/REXA201310280168.md): Access Panel · corroded · Oct 26, 2013 · N8492C · Cndair CL6002B19 · Wing, Plate/Skin
  > CENTER WING LOWER FUEL ACCESS PANEL 510BB GASKET MATING SURFACE WORN AROUND PERIMETER AND CORRODED IN THE NON-CRITICAL REGION 0.5" X 0.125" X 0.002" DEEP. REPAIRED IAW BOMBARDIER REO 601R-57-21-030.
- [SDR REXA2013102801167](https://openairdocs.org/sdr/REXA2013102801167.md): Bulkhead · damaged · Oct 25, 2013 · N8492C · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FORWARD FACE OF FS 621 BULKHEAD HAS FOUR SCREW MARKS. FOUND TO BE WITHIN LIMITS OF REO 601R-53-61-2155.
- [SDR REXA201306271217](https://openairdocs.org/sdr/REXA201306271217.md): Flap System · failed · Jun 27, 2013 · N8492C · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLAPS FAILED AT 17 DEGREES ON LANDING AT RETRACTION.
- [SDR REXA2013040200711](https://openairdocs.org/sdr/REXA2013040200711.md): Seal · broken · Apr 2, 2013 · N8492C · Cndair CL6002B19 · Emergency Equipment
  > FLIGHT ATTENDENT REPORT SEAL ON EMK BROKEN. VERIFIED SEAL ON EMK BAG ARE INTACT. CLOSED AND LOCKED COMPARTMENT INSTALLED SEAL.
- [SDR REXA2013022600427](https://openairdocs.org/sdr/REXA2013022600427.md): Life Vest · unserviceable · Feb 26, 2013 · N8492C · Cndair CL6002B19 · Life Jacket
  > FIRST OFFICER'S LIFE VEST HAS HOLE IN BAG. REMOVED AND REPLACED FIRST OFFICER'S LIFE VEST IAW AMM 25-61-03.
- [SDR REXA2012120701754](https://openairdocs.org/sdr/REXA2012120701754.md): Light · inoperative · Dec 7, 2012 · N8492C · Cndair CL6002B19 · Emergency Lighting
  > FWD OVERHEAD EMERGENCY LIGHT INOP. REPLACED NR 1 CEILING EMERGENCY FLOOD LIGHT BULB AND OPS TEST GOOD IAW AMM 33-51-16. THIS CLEARS THE DM. PLACARD REMOVED.
- [SDR REXA2012102601422](https://openairdocs.org/sdr/REXA2012102601422.md): Wire · broken · Oct 25, 2012 · N8492C · Cndair CL6002B19 · Light System Wiring
  > WARDROBE EMERGENCY LIGHTED "EXIT" SIGN INOP, WIRE BROKEN AT LIGHT. REMOVED & REPLACED EXIT SIGN, FLOOR LEVEL IAW AMM 33-51-10. PERFORMED OPS CHECK IAW AMM 33-51-10. OPS CHECK GOOD. A/C OK FOR SERVICE.
- [SDR REXA2012062600866](https://openairdocs.org/sdr/REXA2012062600866.md): Bulkhead · damaged · Jun 19, 2012 · N8492C · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > A DRILL START WAS NOTED AT FS621 BULKHEAD AT WL113 MEASURING 0.023 INCH DEEP. REPAIRED IAW BOMBARDIER REO 601R-53-61-1230 REV F.
- [SDR REXA2012062000861](https://openairdocs.org/sdr/REXA2012062000861.md): Bulkhead · chafed · Jun 19, 2012 · N8492C · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > AFT PRESSURE BULKHEAD CHAFED JUST ABOVE FLOORBOARD. DAMAGE REMOVED IAW REO 601R-53-61-2155 RESULTING IN 0.001 INCH REMOVED.
- [SDR REXA2012061600857](https://openairdocs.org/sdr/REXA2012061600857.md): Seat Track · corroded · Jun 15, 2012 · N8492C · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > LEFT FLOOR SEAT TRACK AT LBL 9 BETWEEN FS 394 AND 409+128 CORRODED. CORROSION REMOVED IAW SRM 53-31-49.
- [SDR REXA2012061600856](https://openairdocs.org/sdr/REXA2012061600856.md): Seat Track · corroded · Jun 15, 2012 · N8492C · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > LEFT SEAT TRACK AT LBL9 BETWEEN FS 559 AND 559+96 CORRODED. CORROSION REMOVED IAW SRM 53-51-49.
- [SDR REXA2012061600855](https://openairdocs.org/sdr/REXA2012061600855.md): Seat Track · corroded · Jun 15, 2012 · N8492C · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > LEFT FLOOR SEAT TRACK HAS EVIDENCE OF CORROSION. REMOVED CORROSION IAW SRM 53-21-49 FROM FS364 TO 394 AT LBL9.
- [SDR REXA2012070100869](https://openairdocs.org/sdr/REXA2012070100869.md): Skin · chafed · Jun 13, 2012 · N8492C · Cndair CL6002B19 · Ailerons
  > RIGHT AILERON SKIN LEADING EDGE CHAFED TOP AND BOTTOM. REPLACED IAW SRM 51-42-06 AND 51-42-13.
- [SDR REXA2012051300725](https://openairdocs.org/sdr/REXA2012051300725.md): Light · inoperative · May 13, 2012 · N8492C · Cndair CL6002B19 · Emergency Lighting
  > LEFT NR 3 EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED LEFT NR 3 EMERGENCY LIGHT IAW AMM 33-51-21. OPS CHECKED GOOD.
- [SDR REXA2012051300724](https://openairdocs.org/sdr/REXA2012051300724.md): Life Vest · damaged · May 13, 2012 · N8492C · Cndair CL6002B19 · Life Jacket
  > OBSV'S LIFE VEST BAG DAMAGED. REMOVED AND REPLACED OBSV'S LIFE VEST IN ACCORDANCE WITH AMM 25-61-03.
- [SDR REXA2012042500566](https://openairdocs.org/sdr/REXA2012042500566.md): Friction Lock · stuck · Apr 25, 2012 · N8492C · Cndair CL6002B19 · Power Lever
  > THRUST LEVER FRICTION ADJUSTMENT KNOB IS STUCK WILL NOT MOVE EITHER DIRECTION. RELEASED THRUST LEVER FRICTION LOCK FROM BEING OVER TIGHTENED. OPS CHECK NORMAL IAW AMM 76-10-00.
- [SDR REXA2012033000447](https://openairdocs.org/sdr/REXA2012033000447.md): Cable · loose · Mar 30, 2012 · N8492C · Cndair CL6002B19 · Passenger/Crew Doors
  > MAIN CABIN DOOR WHEEL IS DISCONNECTED FROM DOOR CABLE & IS NOT IN CONTACT WITH THE GROUND. INSTALLED PAX DOOR SUPPORT WHEEL CABLE ONTO PULLEY. OPS CHECKED GOOD IAW AMM 52-11-13.
- [SDR REXA201200179](https://openairdocs.org/sdr/REXA201200179.md): Battery · discharged · Feb 3, 2012 · N8492C · Cndair CL6002B19 · Emergency Equipment
  > F/A'S FLASHLIGHT STRAP IS BROKEN AND DOES NOT BLINK RED. REMOVED AND REPLACED F/A FLASHLIGHT BATTERY AS REQ'D. VERIFIED PART EFFECTIVITY. OK FOR SVC.
- [SDR REXA201100903](https://openairdocs.org/sdr/REXA201100903.md): Light · loose · Dec 5, 2011 · N8492C · Cndair CL6002B19 · Emergency Lighting
  > EMERGENCY FLOOR LIGHTING FROM THE EXIT ROW AFT IS INOPERATIVE. RE-SECURED LOOSE FLOOR LIGHTING. OPS CHECK GOOD, REF AMM 33-51-00.
- [SDR REXA201100777](https://openairdocs.org/sdr/REXA201100777.md): Control Panel · defective · Oct 25, 2011 · N8492C · Cndair CL6002B19 · Rudder Tab Control System
  > RUDDER TRIM INOP, CB IS TRIPPED, RESET PER MOC, TRIPPED AGAIN WHEN TESTING. REMOVED AND REPLACED RUDDER TRIM CONTROL PANEL IAW AMM 27-12-10-04. OP/C GOOD. PART EFFECTIVITY VERIFIED.
- [SDR REXA201100748](https://openairdocs.org/sdr/REXA201100748.md): Bulkhead · chafed · Oct 23, 2011 · N8492C · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FS 621.0 PRESSURE BULKHEAD FWD FACE HAS 4 EACH CHAFES AT LBL 32, LBL 23, LBL 14, AND RBL 41 2 ABOVE FLOOR. REPAIRED IAW BOMBARDIER REOS 601R-53-61-2155 AND 601R-53-61-4238.
- [SDR REXA201100747](https://openairdocs.org/sdr/REXA201100747.md): Bulkhead · chafed · Oct 23, 2011 · N8492C · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FS 621.0 PRESSURE BULKHEAD FWD FACE HAS 5 EACH CHAFES 30 ABOVE FLOOR AT LBL 27, LBL 18, RBL 27, AND RBL 36. MAXIMUM CHAFE DAMAGE IS APPROX.163L X.163W X.002D. REPAIRED IAW BOMBARDIER REO 601R-53-61-2155.
- [SDR REXA201100745](https://openairdocs.org/sdr/REXA201100745.md): Angle · corroded · Oct 19, 2011 · N8492C · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CARGO BAY LBL 27 CAP ANGLE OUTBOARD SIDE CORRODED AROUND NUT PLATE HOLES FS 574-621. REPAIRED IAW SRM 51-40-11, 53-61-43 AND BOMBARDIER REO 601R-53-61-3778.
- [SDR REXA201100742](https://openairdocs.org/sdr/REXA201100742.md): Structure · corroded · Oct 19, 2011 · N8492C · Cndair CL6002B19 · Wing Miscellaneous Structure
  > LT WING FUEL TANK ACCESS HOLE NR 1 AT WS 54.897 HAS MINOR CORROSION AT I/B SIDE APPROX 002 D IN NON-CRITICAL REGION. REPAIRED IAW BOMBARDIER REO 601R-57-21-030 REV H.
- [SDR REXA201100741](https://openairdocs.org/sdr/REXA201100741.md): Structure · damaged · Oct 19, 2011 · N8492C · Cndair CL6002B19 · Wing Miscellaneous Structure
  > LT WING FUEL TANK ACCESS HOLE NR 2 AT WS 12.245 HAS AREAS OF PITTING APPROX.004 D IN CRITICAL AND NON-CRITICAL REGIONS. REPAIRED IAW BOMBARDIER REO 601R-57-21-030 REV H.
- [SDR REXA201100668](https://openairdocs.org/sdr/REXA201100668.md): Structure · chafed · Oct 19, 2011 · N8492C · Cndair CL6002B19 · Wing Miscellaneous Structure
  > RT WING FUEL TANK ACCESS HOLE NR 16 AT WS 303.861 IS CHAFED ON THE I/B END APPROX.002 D IN NON-CRITICAL REGION. REPAIRED IAW BOMBARDIER REO 601R-57-21-030 REV H.
- [SDR REXA201100667](https://openairdocs.org/sdr/REXA201100667.md): Floor Support · cracked · Oct 18, 2011 · N8492C · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FS 280 FLOOR SUPPORT WEB CRACKED O/B OF LBL 9, AND LBL AND RBL 9 FLOORBEAM CLIPS ARE CRACKED (I/B AND O/B), AND AFT J-ANGLE HAS AREAS OF CORROSION AROUND NUT PLATE. REPAIRED IAW BOMBARDIER REO 601R-53-11-926 REV B.
- [SDR REXA201100666](https://openairdocs.org/sdr/REXA201100666.md): Skin · gouged · Oct 16, 2011 · N8492C · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > RT SIDE EXTERNAL FUSELAGE HAS A LIGHT GOUGE BETWEEN FS 559.00+112 AND FS 574.00, BETWEEN STRINGERS 20 AND 21. REPAIRED IAW SRM 53-00-31 REPAIR 8.
- [SDR REXA201000256](https://openairdocs.org/sdr/REXA201000256.md): Skin · damaged · Nov 11, 2010 · N8492C · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > DURING OVERNIGHT MAINTENANCE IN LEXINGTON, KEY (LAX), THE GROUND POWER UNIT (GPU) ACCESS DOOR LANDING WAS FOUND DEFORMED AND DAMAGED IN THE UPPER FORWARD CORNER. DAMAGE TO THE POWER PLUG RECEPTACLE IS LIMITED TO ONE PLUG PRONG THAT APPEARS TO BE SLIGHTLY OUT
- [SDR REXA200700035](https://openairdocs.org/sdr/REXA200700035.md): Flap System · unknown · Feb 4, 2007 · N8492C · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLAPS FAIL ON APPROACH. LANDING UNEVENTFUL. COMPLIED WITH AD 2006-12-21, RESET AND MONITORING FOR 72 HOURS.
- [SDR REXA20060026](https://openairdocs.org/sdr/REXA20060026.md): Flap System · malfunctioned · Feb 26, 2006 · N8492C · Cndair CL6002B19 · Trailing Edge Flap Control System
  > DURING CLIMBOUT UPON SELECTION OF FLAPS UP RECEIVED FLAPS FAIL CAUTION MESSAGE. FOLLOWED QRH, DECLARED EMERGENCY RETURNED TO RIC WITH UNEVENTFUL LANDING. RESET FLAPS AND PLACED SYSTEM ON 72 HOUR WATCH PER AD 98-20-01.
- [SDR REXA200600007](https://openairdocs.org/sdr/REXA200600007.md): Flap · malfunctioned · Feb 5, 2006 · N8492C · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLAP FAIL AT 45 DEGREES ON APPROACH. RESET SYSTEM AND PLACED ON 72 HOUR WATCH PER AD 98-20-01.
- [SDR 05105](https://openairdocs.org/sdr/05105.md): Dcu · failed · Aug 27, 2005 · N8492C · Cndair CL6002B19 · Central Computers
  > ON ROTATION ICE CAUTION FOLLOWED BY MASTER CAUTION LEFT ENGINE FIRE FOLLOWED BY ASSORTED OTHER MESSAGES. DECLARED EMERGENCY AND LANDED. UPON INVESTIGATION FOUND DCU'S BAD. REMOVED AND REPLACED DCU 1 AND DCU2 IAW AMM 31-41-00. PERFORMED OPS CHECK GOOD.
- [SDR REXA01011](https://openairdocs.org/sdr/REXA01011.md): Hose · ruptured · Jul 17, 2001 · N8492C · Cndair CL6002B19 · Oxygen System
  > OBSERVER SEAT POSITION OXYGEN MASK SUPPLY HOSE RUPTURED AND SEPARATED FROM FITTING. REMOVED AND REPLACED HOSE. THIS WAS FOUND WHILE INVESTIGATING A DEPLETED CREW OXYGEN SYSTEM. (M)
- [SDR REXA01008](https://openairdocs.org/sdr/REXA01008.md): Bpsu · failed · Jun 11, 2001 · N8492C · Cndair CL6002B19 · Flight Control System
  > FLAP FAILURE MESSAGE AND FLAPS STUCK AT 20 DEGREES. INTERROGATED FECU (FLAP ELECTRONIC CONTROL UNIT) FOUND LEFT BPSU (BRAKE POSITION SENSING UNIT) FAILURE MESSAGE. REMOVED AND REPLACED LEFT FLAP BPSU. (M)

## 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 = 'N8492C' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N8492C/reports

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