# Service difficulty reports: N8515F

A list on [N8515F](https://openairdocs.org/aircraft/N8515F.md).

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

- [SDR REXA2013071401353](https://openairdocs.org/sdr/REXA2013071401353.md): Container · torn · Jul 14, 2013 · N8515F · Cndair CL6002B19 · Life Jacket
  > F/O LIFE VEST BAG TORN. R & R F/O LIFE VEST IAW AMM 25-61-03.
- [SDR REXA2013060301052](https://openairdocs.org/sdr/REXA2013060301052.md): Sensing Element · faulty · Jun 3, 2013 · N8515F · Cndair CL6002B19 · Pneumatic Indicating System
  > ANTI-ICE DUCT WARNING MESSAGE CAME ON ABOVE 20,000 FT, IN CLIMB AT 1046-1047Z. FDR EVENT. SYNOPTIC SHOWED LT FUSELAGE DUCT RED. EVENTUALY COOLED AND WENT OUT AFTER WING & LR 14TH CLOSED. R & R LT FUSELAGE BLEED AIR DUCT SENSING ELEMENT IAW AMM 36-21-04. OP
- [SDR REXA2013050900878](https://openairdocs.org/sdr/REXA2013050900878.md): Light · inoperative · May 9, 2013 · N8515F · Cndair CL6002B19 · Emergency Lighting
  > NR 1 CEILING EMERGENCY FLOODLIGHT INOPERABLE.
- [SDR REXA2013042900647](https://openairdocs.org/sdr/REXA2013042900647.md): Floor Support · corroded · Apr 26, 2013 · N8515F · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > SERVICE DOOR FORWARD FLOOR SUPPORT BRACKET/SILL IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED IAW SRM 51-42-06.
- [SDR REXA2013041200743](https://openairdocs.org/sdr/REXA2013041200743.md): Light · inoperative · Apr 12, 2013 · N8515F · Cndair CL6002B19 · Emergency Lighting
  > NR 1 CAPTAIN`S EXTERIOR EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT IAW AMM-33-51-21. OPS CHECKED GOOD. OK FOR SERVICE.
- [SDR REXA2013040600728](https://openairdocs.org/sdr/REXA2013040600728.md): Bpsu · failed · Apr 6, 2013 · N8515F · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLIGHT 3629, CREW REPORTED FLAPS FAILED MESSAGE IN FLIGHT ON EXTENSION, POSITION AT TIME OF FAILURE 36 DEGREES AT 160KTS, APPROXIMATELY 1 HOUR INTO FLIGHT, AND OAT 7*C. FLIGHT CONTINUED TO DESTINATION. PULLED CODES AND COMPLETED FLAP EVENT SHEET ENTER CODE.
- [SDR REXA2013012700199](https://openairdocs.org/sdr/REXA2013012700199.md): Engine · fire · Jan 27, 2013 · N8515F · Cndair CL6002B19 · Engine (Turbine/Turboprop)
  > ON FLIGHT 3629 (CLT TO MEM) STARTED ENGINE NR 2 SECOND. DURING START WE GOT THE "HOT" ICON AND STOPPED START. AIRCRAFT BEHIND US INDICATED THAT FLAMES WERE COMING OUT OF RIGHT ENGINE. (ITT REACH AT 550 DEG). NO ITT EXCEEDANCE HISTORY RECORDED IN MDC. PERF
- [SDR REXA2012101401399](https://openairdocs.org/sdr/REXA2012101401399.md): Battery · discharged · Oct 14, 2012 · N8515F · Cndair CL6002B19 · Emergency Equipment
  > FORWARD FLIGHT ATTENDANT FLASHLIGHT RED LIGHT ISN'T BLINKING. REMOVED AND REPLACED FLIGHT ATTENDANT FLASHLIGHT BATTERY IAW AMM 25-61-02.
- [SDR REXA2012091201332](https://openairdocs.org/sdr/REXA2012091201332.md): Selector Valve · malfunctioned · Sep 12, 2012 · N8515F · Cndair CL6002B19 · Landing Gear Selector
  > AFTER TAKEOFF FROM CLE ON FLIGHT 4166 THE NLG WOULD NOT RETRACT ALONG WITH A GEAR DISAGREE WARNING. CREW CYCLED THE GEAR, NO HELP. THE AIRCRAFT THEN DIVERTED TO DTW AND SWAPPED TO ANOTHER AIRCRAFT. REMOVED AND REPLACED NLG SELECTOR VALVE IAW CRJ200AMM 33-22
- [SDR REXA2012072901207](https://openairdocs.org/sdr/REXA2012072901207.md): Selector Valve · malfunctioned · Jul 29, 2012 · N8515F · Cndair CL6002B19 · Landing Gear Retraction/Extension System
  > FLIGHT 4049, DIVERTED DUE TO MAIN LANDING GEAR WOULD NOT RETRACT AND CYCLED ON ATTEMPT. CREW DID NOT DECLARE EMERGENCY AND LANDED SAFELY. COMPLIED WITH PA 50-018G SCENARIO NR 1. REMOVED AND REPLACED MLG SELECTOR VALVE IAW AMM 32-32-10. OPS AND LEAK CHECKE
- [SDR REXA2012052900798](https://openairdocs.org/sdr/REXA2012052900798.md): Pump · leaking · May 29, 2012 · N8515F · Cndair CL6002B19 · Hydraulic Pump (Electric/Engine), Main
  > HYDRAULIC SYSTEM PUMP 3B LEAKING AND FOLLOWED WITH LOW CAUTION MESSAGE. MANUALLY EXTENDED GEAR FOR LANDING. EMERGENCY DECLARED. ALL OPS CHECK GOOD. REMOVED AND REPLACED HYDRAULIC SYSTEM NR 3B. OP CHECK LEAK CHECKED GOOD IAW AMM 29-12-00. OK FOR SERVICE
- [SDR REXA2012040900480](https://openairdocs.org/sdr/REXA2012040900480.md): Light · inoperative · Apr 9, 2012 · N8515F · Cndair CL6002B19 · Emergency Lighting
  > CEILING OVERHEAD EMERGENCY LIGHT 2ND FROM FRONT INOPERATIVE. REMOVED AND REPLACED CEILING LEVEL EMERGENCY FLOOD LIGHTS IAW AMM 33-51-21. OP'S CHECKED GOOD.
- [SDR REXA2012032700411](https://openairdocs.org/sdr/REXA2012032700411.md): Flap · failed · Mar 27, 2012 · N8515F · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLAPS FAIL AT 20. PERFORMED TROUBLESHOOTING PER BOMBARDIER FIM REV 39 IAW AD 2009-06-12 PARAGRAPH (H)(6)(I) AMOC DATED MARCH 27, 2009 AND TR 27-012 PER AMOC DATED DECEMBER 18,2009. LRU LOG "FLAP LEVER FAULT" AND FAULT CODES 19 C1, 19 C2, 25 BC, 33 BC, NO FUR
- [SDR REXA201101012](https://openairdocs.org/sdr/REXA201101012.md): Battery · weak · Dec 24, 2011 · N8515F · Cndair CL6002B19 · Emergency Equipment
  > CAPT'S / FO'S EMERGENCY FLASHLIGHT BATTERY WEAK. REMOVED AND REPLACED CAPT'S / FO'S EMERGENCY FLASHLIGHT BATTERIES, OPS CHECK GOOD IAW AMM 25-61-00.
- [SDR REXA201100952](https://openairdocs.org/sdr/REXA201100952.md): Unknown · odor · Dec 9, 2011 · N8515F · Cndair CL6002B19 · APU Engine Fuel and Control
  > FUEL SMELL FROM APU WHEN STARTED. OPS CHECK APU IAW CRJ AMM 49-10-00, NO SMELL OF FUEL PRESENT AT THIS TIME.
- [SDR REXA201100718](https://openairdocs.org/sdr/REXA201100718.md): Beam · cracked · Nov 27, 2011 · N8515F · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FS 280 TRANSVERSE BEAM CRACKED. REPAIRED IAW BOMBARDIER REO 601R-53-11-926 REV B AND BOMBARDIER SERVICE CORPORATION STANDARD REPAIR 601R-53-0110.
- [SDR REXA201100719](https://openairdocs.org/sdr/REXA201100719.md): Sill · corroded · Nov 25, 2011 · N8515F · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > PRESSURE FLOOR SILL AT FS 449 LBL 36 IS CORRODED. REPAIRED IAW BOMBARDIER REO 601R-53-41-666.
- [SDR REXA201100850](https://openairdocs.org/sdr/REXA201100850.md): Unknown · malfunctioned · Nov 18, 2011 · N8515F · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLAPS FAIL RESET FLAPS PER PA AD2. TROUBLESHOT FLAPS IAW FIM CHPT 27-50-00. NO DEFECTS NOTED. PERFORMED AMM TASKS 27-54-00-710-801, 27-51-05-740-801, 27-54-00-720-801, AND 27-51-15-710-802.
- [SDR REXA201100435](https://openairdocs.org/sdr/REXA201100435.md): Engine · overspeed · Jun 30, 2011 · N8515F · Cndair CL6002B19 · Engine (Turbine/Turboprop)
  > RT ENGINE N2 OVER SPEED PEAKED TO 99.5 AT 101F OAT. PER GE MANUAL 72-00-00 INSPECTION MUST BE PERFORMED WITHIN 10 FC OPENED DI-46424 IAW GE MANUAL FOR COMPLIANCE.
- [SDR REXA201000282](https://openairdocs.org/sdr/REXA201000282.md): Skin · damaged · Nov 29, 2010 · N8515F · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > DENT DAMAGE WITH SCRATCHES FROM IMPACT WITH GROUND SERVICE EQUIPMENT REPORTED ON RT WING CENTER LIE BETWEEN WS199.00 AND 220.00. DAMAGES CONSIST OF THE FOLLOWING: DENT TO LIE SKIN: APPROX 1O.O"L X 6.0"W X 0.50" DEEP MAX SCRATCHES TO LIE SKIN: 3-0FF, 3.0", 5.0"
- [SDR REXA201000259](https://openairdocs.org/sdr/REXA201000259.md): Anti-Ice Valve · failed · Nov 15, 2010 · N8515F · Cndair CL6002B19 · Air Intake Anti/De-Ice System
  > (L) COWL ANTI-ICE CAUTION IN ICE IN CLIMB RAN QRH, LEFT ICE STILL SHOWING MESSAGE. REMOVED AND REPLACED LT COWL ANTI-ICE VALVE IAW AMM 30-22-01. OP CHECKS GOOD, OK FOR SERVICE.
- [SDR REXA201000258](https://openairdocs.org/sdr/REXA201000258.md): Bulkhead · cracked · Nov 10, 2010 · N8515F · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > CRACKED FS 559.00 BULKHEAD WEB REQUIRES REPAIR. REPAIRED FS 559.00 BULKHEAD WEB IAW BOMBARDIER REO 601R-53-41-260 REV E AND BOMBARDIER REO 601R-53-41-609 REV B, DEVIATION C.
- [SDR REXA201000099](https://openairdocs.org/sdr/REXA201000099.md): Warning System · false activation · Aug 1, 2010 · N8515F · Cndair CL6002B19 · Engine Thrust Reverser
  > AFTER REACHING CRUISING ALTITUDE OF FL310 OUT OF KBHM FOR KDTW THE R REV UNLOCKED CAUTION MESSAGE ILLUMINATED. THERE WAS NO BUFFET NOR AIRCRAFT HANDLING ISSUES NOTED. THE CREW PERFORMED THE QRH THEN NOTIFIED BOTH ATC AND COMPANY MOC. THE CAPTAIN DECIDED NOT
- [SDR REXA200900127](https://openairdocs.org/sdr/REXA200900127.md): Smoke Detector · dirty · Nov 21, 2009 · N8515F · Cndair CL6002B19 · Smoke Detection
  > ON FINAL APPROACH INTO KDTW, THE SMOKE CARGO WARNING CAME ON FOR APPROXIMATELY 16 SECONDS. THE FLIGHT CREW PERFORMED THE QRH AND BY THE TIME THE QRH WAS PERFORMED THE MESSAGE CLEARED. THE FLIGHT CREW DECLARED AN EMERGENCY AND REQUESTED CFR ASSISTANCE. AN OT
- [SDR REXA200900118](https://openairdocs.org/sdr/REXA200900118.md): Smoke Detector · malfunctioned · Oct 9, 2009 · N8515F · Cndair CL6002B19 · Smoke Detection
  > DURING CARGO LOADING CREW RECEIVED "CARGO SMOKE" WARNING. AREA WAS INSPECTED WITH NO SMOKE OR FUMES FOUND. DETERMINED TO BE A FALSE WARNING INDICATION. SYSTEM DEFERRED PER MEL 26-15-12. MAINTENANCE INSPECTED AND PERFORMED AMM OPERATIONAL CHECK WITH NO DEFE
- [SDR REXA200800012](https://openairdocs.org/sdr/REXA200800012.md): Landing Gear · malfunctioned · May 5, 2008 · N8515F · Cndair CL6002B19 · Landing Gear Retraction/Extension System
  > ON APPROACH WHEN SELECTING GEAR DOWN NOSE GEAR DID NOT EXTEND. FOLLOWED QRH MANUAL EXTENSION OF GEAR WITH THREE GREENS. DECLARED EMERGENCY AND LANDED WITHOUT INCIDENT. GEAR RETRACTION SYSTEM DEFERRED PER MEL 32-30-01.
- [SDR REXA200500148](https://openairdocs.org/sdr/REXA200500148.md): Flap System · malfunctioned · Dec 6, 2005 · N8515F · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLAPS FAILED AT 0 DEGREES ON APPROACH. LANDING UNEVENTFUL. INSPECTED, RESET AND PERFORMED OPERATIONAL CHECK. PLACED ON 72 HOUR WATCH PER AD 98-20-01.
- [SDR REXA200500139](https://openairdocs.org/sdr/REXA200500139.md): Flap System · failed · Nov 24, 2005 · N8515F · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLAP FAILURE ON APPROACH WHEN SELECTED TO 20. ABORTED APPROACH, FOLLOWED QRH WITH UNEVENTFUL LANDING. RESET SYSTEM AND PLACED FLAPS ON 72 HOUR WATCH PER AD 98-20-01.
- [SDR REXA2005054](https://openairdocs.org/sdr/REXA2005054.md): Apu · smoke · Apr 19, 2005 · N8515F · Cndair CL6002B19 · APU Core Engine
  > SMOKE IN COCKPIT AND CABIN WHEN THE APU WAS STARTED. INVESTIGATED, FOUND APU TO BE THE SOURCE OF THE SMOKE. APU WAS DEFERRED UNTIL IT CAN BE SCHEDULED OFF. (K)
- [SDR REXA04025](https://openairdocs.org/sdr/REXA04025.md): Proximity Sensor · out of position · Oct 29, 2004 · N8515F · Cndair CL6002B19 · Landing Gear Position and Warning
  > ON CLIMB-OUT FROM TAKEOFF, GOT (NOSE DOOR) MESSAGE AND (GEAR DISAGREE) MESSAGE. ORH FOLLOWED, EMERGENCY DECLARED RETURNED TO AIRPORT, UNEVENTFUL LANDING. FOUND PROXIMITY SENSOR ON NOSE GEAR OUT OF POSITION. RIGGED SENSOR IAW AMM, PERFORMED GEAR SWINGS.
- [SDR REXA04015](https://openairdocs.org/sdr/REXA04015.md): Circuit Breaker · tripped · Sep 20, 2004 · N8515F · Cndair CL6002B19 · Trailing Edge Flap Control System
  > ON APPROACH FLAPS FAILED AT 20, QRH FOLLOWED, UNEVENTFUL LANDING. CIRCUIT BREAKER RESET PERFORMED, FLAPS PLACED ON 72 HOURS WATCH PER AD 98-20-01. (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 = 'N8515F' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N8515F/reports

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