# Service difficulty reports: N8516C

A list on [N8516C](https://openairdocs.org/aircraft/N8516C.md).

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

- [SDR REXA2014100701029](https://openairdocs.org/sdr/REXA2014100701029.md): Life Vest · unserviceable · Oct 7, 2014 · N8516C · Cndair CL6002B19 · Life Jacket
  > CAPTAIN & FLIGHT ATTENDANT LIFE VEST HAS HOLE IN BAG. R & R IAW AMM 25-61-03.
- [SDR REXA2014092100891](https://openairdocs.org/sdr/REXA2014092100891.md): Skin · damaged · Sep 18, 2014 · N8516C · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > FOUND THE FUSELAGE SKIN TO BE PREVIOUSLY BLENDED AT FS 662 BETWEEN STRINGER 21L & 22L. THE BLEND MEASURES 1.64 INCHES X 1.32 INCHES X 0.016 INCHES DEEP. REPAIRED IAW EA.
- [SDR REXA2014092000790](https://openairdocs.org/sdr/REXA2014092000790.md): Skin · damaged · Sep 17, 2014 · N8516C · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > FOUND THE FUSELAGE SKIN TO BE PREVIOUSLY BLENDED AT FS 662 BETWEEN STRINGER 21L & 22L. THE BLEND MEASURES 1.64 INCHES X 1.32 INCHES X 0.016 INCHES DEEP. REPAIRED IAW EA.
- [SDR REXA2014071300696](https://openairdocs.org/sdr/REXA2014071300696.md): Smoke Goggles · defective · Jul 13, 2014 · N8516C · Cndair CL6002B19 · Emergency Equipment
  > CAPTAIN & FIRST OFFICERS SMOKE GOGGLES NO ELASTICITY. REPLACED BOTH SMOKE GOGGLES IAW AMM 35-10-00.
- [SDR REXA2014042400399](https://openairdocs.org/sdr/REXA2014042400399.md): Battery · discharged · Apr 24, 2014 · N8516C · Cndair CL6002B19 · Emergency Equipment
  > FIRST OFFICER`S FLASHLIGHT BATTERY DEAD FROM MM 02. R & R FIRST OFFICER`S FLASHLIGHT BATTERY IAW AMM 25-60-00, REMOVED FROM MM02.
- [SDR REXA2014041700381](https://openairdocs.org/sdr/REXA2014041700381.md): Smoke Goggles · worn · Apr 17, 2014 · N8516C · Cndair CL6002B19 · Emergency Equipment
  > CA'S SMOKE GOGGLES WORN OUT. REPLACED CA SMOKE GOGGLES IAW AMM 35-11-15, OK FOR SERVICE.
- [SDR REXA2014030500257](https://openairdocs.org/sdr/REXA2014030500257.md): Unknown · odor · Mar 5, 2014 · N8516C · Cndair CL6002B19 · Air Distribution System
  > CREW REPORTED FUEL SMELL IN AFT CARGO BAY. OPERATIONS CHECK OF PACKS IAW 21-51-10, OPERATIONS CHECKED GOOD. COULD NOT FIND SOURCE OF ODOR OR CAN’T DETERMINE THE SMELL.
- [SDR REXA2014021000013](https://openairdocs.org/sdr/REXA2014021000013.md): Skin · dented · Feb 9, 2014 · N8516C · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > DENT IN THE RT FUSELAGE SKIN BETWEEN FS 559.00 & FS 559+16 AT STRINGER 6R. THE DENT MEASURES.635” X.444” X.010” DEEP. REPAIRED IAW EA CRJ253-02275.
- [SDR REXA2014020400012](https://openairdocs.org/sdr/REXA2014020400012.md): Fitting · cracked · Feb 1, 2014 · N8516C · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LOWER WEB LINTEL FITTING WAS FOUND TO BE CRACK ON AFT PRESS BULKHEAD AT FS 621. REPAIRED IAW REO 601R-53-61-1230.
- [SDR REXA2013112002265](https://openairdocs.org/sdr/REXA2013112002265.md): Battery · discharged · Nov 20, 2013 · N8516C · Cndair CL6002B19 · Emergency Equipment
  > CAPTAIN`S SIDE EMERGENCY FLASHLIGHT NOT BLINKING, SUSPECT DEAD BATTERY. R & R CAPTAIN`S SIDE EMERGENCY FLASHLIGHT BATTERY IAW AMM 25-61-00, OPERATIONS CHECKED GOOD, OK FOR SERVICE.
- [SDR REXA2013111702261](https://openairdocs.org/sdr/REXA2013111702261.md): Seal · broken · Nov 17, 2013 · N8516C · Cndair CL6002B19 · Emergency Equipment
  > CABIN FLIGHT DECK FLASHLIGHT SEAL BROKEN. R & R SEAL IAW CRJ200 AMM 25-61-01, OK FOR SERVICE.
- [SDR REXA2013100801765](https://openairdocs.org/sdr/REXA2013100801765.md): Light · unknown · Oct 8, 2013 · N8516C · Cndair CL6002B19 · Emergency Lighting
  > EMERGENCY LIGHTS IN CABIN ARE INOPERATIVE., PERFORMED OP CHECK OF EMERGENCY LIGHT IAW AMM 33-51-01. ALL EMERGENCY LIGHT OPERATE NORMALLY WITH COCKPIT AND F/A PANEL SWITCHES. THIS CLEARS DI 17501.
- [SDR REXA2013100701764](https://openairdocs.org/sdr/REXA2013100701764.md): Bulb · inoperative · Oct 7, 2013 · N8516C · Cndair CL6002B19 · Emergency Lighting
  > ONE OVER-WING EXTERIOR EMERGENCY LIGHT INOPERATIVE ON EACH SIDE OF THE FUSELAGE. R & R SHORTED BULB IAW AMM 33-51-14. OPS CHECKED GOOD.
- [SDR REXA2012123001829](https://openairdocs.org/sdr/REXA2012123001829.md): Battery · discharged · Dec 30, 2012 · N8516C · Cndair CL6002B19 · Emergency Equipment
  > FLIGHT ATTENDANT FLASHLIGHT FAILED TEST. REMOVED AND REPLACED FLIGHT ATTENDANT FLASHLIGHT BATTERY IAW AMM 25-61-02. OPC GOOD. OK FOR SERVICE.
- [SDR REXA2012122201814](https://openairdocs.org/sdr/REXA2012122201814.md): Torque Link · disconnected · Dec 22, 2012 · N8516C · Cndair CL6002B19 · Nose/Tail Landing Gear Strut/Axle
  > ON FLIGHT 3887 FROM PIT TO MEM RECEIVED GEAR DISAGREE WITH NOSE DOOR OPEN AND WOW INPUT MESSAGE. THE GEAR THEN SHOWED DOWN 3 GREEN WITH WOW INPUT CAUTION MESSAGE STILL PRESENT AND WOW OUTPUT FAIL STATUS. AIRCRAFT PERFORMED AIR RETURN TO PIT. FOUND THE GEAR
- [SDR REXA2012120201722](https://openairdocs.org/sdr/REXA2012120201722.md): Torque Link · unsecure · Dec 2, 2012 · N8516C · Cndair CL6002B19 · Nose/Tail Landing Gear Strut/Axle
  > ON FLIGHT 4223 RECEIVED GEAR DISAGREE MESSAGE 6 SECONDS AFTER TAKEOFF OUT OF PVD AND GEAR SELECTED UP. MAIN GEAR SHOWED UP AND LOCKED AND NOSE GEAR SHOWED DOWN. THE CREW OPERATED THE MANUAL RELEASE SYSTEM AND THE NOSE SHOWED LOCKED DOWN. AIRCRAFT PERFORMED
- [SDR REXA2012120101728](https://openairdocs.org/sdr/REXA2012120101728.md): Hinge · worn · Dec 1, 2012 · N8516C · Cndair CL6002B19 · Fuselage, Door Hinge
  > IN HEAVY CHECK, PAX DOOR HINGE IS WORN (AIRCRAFT SIDE). REMOVED AND REPLACED PAX DOOR HINGE (AIRCRAFT SIDE) IAW CRJ 200 SRM 53-21-23.
- [SDR REXA2012120101727](https://openairdocs.org/sdr/REXA2012120101727.md): Hinge · worn · Dec 1, 2012 · N8516C · Cndair CL6002B19 · Passenger/Crew Doors
  > IN HEAVY CHECK, PAX DOOR HINGE IS WORN (DOOR SIDE). REMOVED AND REPLACED DOOR SIDE HINGE ON PASSENGER DOOR IAW CRJ 200 SRM 52-10-31.
- [SDR REXA2012120201538](https://openairdocs.org/sdr/REXA2012120201538.md): Seat Track · gouged · Nov 30, 2012 · N8516C · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > RIGHT NR 3 FLOOR SEAT TRACK GOUGED. REPAIRED AIW SRM 53-21-49.
- [SDR REXA2012120201537](https://openairdocs.org/sdr/REXA2012120201537.md): Seat Track · corroded · Nov 30, 2012 · N8516C · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > LEFT NR 2 SIDE SEAT TRACK IS CORRODED. REPLACED IAW AMM 53-01-11.
- [SDR REXA2012112701527](https://openairdocs.org/sdr/REXA2012112701527.md): Seat Track · corroded · Nov 25, 2012 · N8516C · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > RIGHT NR 7 SEAT TRACK CORRODED AND GOUGED. REPAIRED IAW AMM 53-01-11.
- [SDR REXA2012112701526](https://openairdocs.org/sdr/REXA2012112701526.md): Seat Track · corroded · Nov 25, 2012 · N8516C · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > RIGHT NR 6 SEAT TRACK CORRODED AND GOUGED. REPAIRED IAW AMM 53-01-11.
- [SDR REXA2012112701525](https://openairdocs.org/sdr/REXA2012112701525.md): Seat Track · corroded · Nov 25, 2012 · N8516C · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > RIGHT NR 4 SEAT TRACK CORRODED AND GOUGED. REPAIRED IAW AMM 53-01-11.
- [SDR REXA2012112701524](https://openairdocs.org/sdr/REXA2012112701524.md): Bulkhead · chafed · Nov 25, 2012 · N8516C · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > AFT PRESSURE BULKHEAD AT FS 621 HAS AREAS OF SCREW CHAFES. REPAIRED IAW BOMBARDIER REO 601R-53-61-2155.
- [SDR REXA2012072901208](https://openairdocs.org/sdr/REXA2012072901208.md): Container · damaged · Jul 29, 2012 · N8516C · Cndair CL6002B19 · Life Jacket
  > OBSERVERS LIFE VEST HAS A HOLE IN THE BAG. REMOVED AND REPLACED OBSERVERS LIFE VEST IAW AMM 25-61-03.
- [SDR REXA2012071601160](https://openairdocs.org/sdr/REXA2012071601160.md): Warning Light · false activation · Jul 16, 2012 · N8516C · Cndair CL6002B19 · Engine Thrust Reverser
  > ON LANDING, USED THRUST REVERSER, STOWED IT, THE LEFT UNLOCK MESSAGE CAME ON. LEFT ENGINE THEN SHUTDOWN WITH THRUST REVERSER LEVER AT IDLE. LEFT INDICATIONS NORMAL EXCEPT REVERSER AND UNLOCK LIGHTS ON. PERFORMED ENGINE RUN IAW AMM 71-00-00 AND OPS CHECKED B
- [SDR REXA2012042900577](https://openairdocs.org/sdr/REXA2012042900577.md): Unknown · malfunctioned · Apr 29, 2012 · N8516C · Cndair CL6002B19 · Engine Thrust Reverser
  > LEFT TR WOULD NOT DEPLOY ON LANDING. LEFT TR CHECKS GOOD IAW AMM 78-30-00.
- [SDR REXA2012032600274](https://openairdocs.org/sdr/REXA2012032600274.md): Seat Track · damaged · Mar 25, 2012 · N8516C · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > LEFT NR 3 SEAT TRACK AT LBL 9 CORRODED AND GOUGED. REPAIRED IAW BOMBARDIER REO 601R-53-00-005.
- [SDR REXA2012032600273](https://openairdocs.org/sdr/REXA2012032600273.md): Seat Track · damaged · Mar 25, 2012 · N8516C · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > LEFT SEAT RAIL AFT OF FS 409+128 GOUGED, NICKED, AND CORRODED. REPAIRED IAW AMM 53-01-11.
- [SDR REXA2012032600272](https://openairdocs.org/sdr/REXA2012032600272.md): Seat Track · damaged · Mar 25, 2012 · N8516C · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > LEFT SIDE NR 2 SEAT TRACK AT LBL 9 CORRODED AND GOUGED. REPAIRED IAW SRM 53-21-49.
- [SDR REXA2012032600271](https://openairdocs.org/sdr/REXA2012032600271.md): Seat Track · corroded · Mar 25, 2012 · N8516C · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > RIGHT SIDE SEAT RAIL FORWARD OF FS 409+128 GOUGED AND CORRODED. REPAIRED IAW SRM 53-21-49.
- [SDR REXA2012030700340](https://openairdocs.org/sdr/REXA2012030700340.md): Battery · discharged · Mar 7, 2012 · N8516C · Cndair CL6002B19 · Emergency Equipment
  > F/A'S FLASHLIGHT INOP. REMOVED AND REPLACED F/A FLASHILGHT BATTERY IAW AMM 25-61-02.
- [SDR REXA201100977](https://openairdocs.org/sdr/REXA201100977.md): Unknown · malfunctioned · Dec 16, 2011 · N8516C · Cndair CL6002B19 · Drag Control System
  > WITH ALL HYDRAULICS ON RECEIVED FLT SPLRS AND SPOILERONS CAUTION MESSAGE. RESET A/C POWER PER AMM 20-00-00. MSG CLEARED.
- [SDR REXA201100685](https://openairdocs.org/sdr/REXA201100685.md): Light · intermittent · Oct 7, 2011 · N8516C · Cndair CL6002B19 · Passenger Compartment Lighting
  > OVERHEAD EMERGENCY LIGHTS OVER ROW 8, FLIGHT ATTENDANT NOTIFICATION LIGHTS INTERMITTENT IN FLIGHT (LOWER LEFT CORNER). COULD NOT DUPLICATE DISCREPANCY. FLT ATT CALL LIGHTS OP TEST OK IAW AMM 33-22-03. OK FOR SERVICE.
- [SDR REXA201100430](https://openairdocs.org/sdr/REXA201100430.md): Switch · out of position · Jun 28, 2011 · N8516C · Cndair CL6002B19 · APU Engine Fuel and Control
  > AFTER CREW DEPLANED, GROUND CREW NOTICED FLAMES IN APU EXHAUST. FIRE CREW NOTIFIED. FLIGHT CREW ALERTED AND RETURNED TO AIRCRAFT. SMALL FLAME WAS OBSERVED IN THE APU EXHAUST WITH EVIDENCE OF FUEL ON THE RAMP BELOW THE APU. PWR FUEL SWITCH FOUND IN ON POSI
- [SDR REXA201100407](https://openairdocs.org/sdr/REXA201100407.md): Shutoff Valve · loose · Jun 23, 2011 · N8516C · Cndair CL6002B19 · APU Engine Fuel and Control
  > CREWS REPORTED FUEL SMELL IN COCKPIT INBOUND "NO"EMERGENCY DECLARED LANDED WITHOUT INCIDENT NSP'D - FOUND APU FUEL FEED S/O VALV OUTLET CONNECTION LOOSE. TIGHTENED AND LEAK CHECKED GOOD IAW AMM 49-30-00.
- [SDR REXA201100141](https://openairdocs.org/sdr/REXA201100141.md): Pump · leaking · Feb 23, 2011 · N8516C · Cndair CL6002B19 · Turbine Engine Oil System
  > FLIGHT DIVERTED DUE TO RIGHT ENGINE LOW OIL PRESSURE INDICATION ENGINE WAS SHUT DOWN IN FLIGHT EMERGENCY WAS DECLARED FOUND RT ENGINE EDP LEAKING. DEFERRED EDP IAW MEL 29-11-01 DM-39183.
- [SDR REXA201000323](https://openairdocs.org/sdr/REXA201000323.md): Bulkhead · cracked · Dec 23, 2010 · N8516C · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > CRACKED FS 559.00 BULKHEAD WEB REQUIRES REPAIR. REPAIRED FS 559.00 BULKHEAD WEB LAW BOMBARDIER REO 601R-53-41-260 REV E AND BOMBARDIER REO 601R-53-41-609 REV B, DEVIATION E.
- [SDR REXA201000077](https://openairdocs.org/sdr/REXA201000077.md): Retainer · corroded · May 15, 2010 · N8516C · Cndair CL6002B19 · Electrical/Electronic Compartment Doors
  > FOUND LEVEL 2 CORROSION ON AVIONICS DOOR, AFT SEAL RETAINERS. REMOVED AND REPLACED TWO AFT AVIONICS DOOR SEAL RETAINERS, P/N CC670-38675-3 AND CC670-38662-5 IAW CRJ200 SRM 51-42-06.
- [SDR REXA200900055](https://openairdocs.org/sdr/REXA200900055.md): Flap System · out of rig · May 25, 2009 · N8516C · Cndair CL6002B19 · Trailing Edge Flap Control System
  > MAY 25, 2009, CREW RECEIVED "FLAP FAILURE" MESSAGE ON CLIMBOUT WHEN SELECTING FLAPS TO UP. MX INSPECTED THE ACFT AND TROUBLESHOT IAW MFG FAULT ISOLATION MANUAL, FLAPS FOUND TO BE OUT OF RIG. FLAPS RIGGED IAW MM WITH OPS CHECKS PERFORMED WITH NO DEFECTS.
- [SDR REXA200600010](https://openairdocs.org/sdr/REXA200600010.md): Proximity Sensor · out of adjust · Feb 10, 2006 · N8516C · Cndair CL6002B19 · Landing Gear Position and Warning
  > ON CLIMBOUT UPON GEAR SELECTED UP RECEIVED GEAR DISAGREE. QRH FOLLOWED RETURNED TO MEMPHIS, UNEVENTFUL LANDING. GEAR SWINGS PERFORMED AND TROUBLESHOT TO AN OUT OF ADJUSTMENT PROX SENSOR. ADJUST PROX SENSOR IAW AMM, OPERATIONAL CHECKS GOOD.

## 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 = 'N8516C' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N8516C/reports

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