# Service difficulty reports: N8560F

A list on [N8560F](https://openairdocs.org/aircraft/N8560F.md).

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

- [SDR REXA2014071600703](https://openairdocs.org/sdr/REXA2014071600703.md): Life Vest · unserviceable · Jul 16, 2014 · N8560F · Cndair CL6002B19 · Life Jacket
  > CAPTAINS LIFE VEST HAS A HOLE IN BAG. R & R CAPTAINS LIFE VEST IAW AMM 25-61-03.
- [SDR REXA2014071200686](https://openairdocs.org/sdr/REXA2014071200686.md): Landing Gear · multiple fail · Jul 12, 2014 · N8560F · Cndair CL6002B19 · Landing Gear Retraction/Extension System
  > GEAR WAS SELECTED UP, FOLLOWED BY NOSE DOOR OPEN MASTER WARNING, GEAR DISAGREE WARNING, STEERING INOPERATIVE, WOW INPUT CAUTION & ADVISORY. PERFORMED QRH, GEAR WAS CYCLED & EMERGENCY HANDLE PULLED, WOULD NOT STOW, GEAR LOCKED DOWN WITH 3 GREEN INDICATIONS.
- [SDR REXA2014062600635](https://openairdocs.org/sdr/REXA2014062600635.md): Life Vest · unserviceable · Jun 26, 2014 · N8560F · Cndair CL6002B19 · Life Jacket
  > FIRST OFFICER'S LIFE VEST HAS HOLE IN BAG. R & R FIRST OFFICER`S LIFE VEST IAW AMM 25-61-03.
- [SDR REXA2014021000191](https://openairdocs.org/sdr/REXA2014021000191.md): Bolt · dirty · Feb 10, 2014 · N8560F · Cndair CL6002B19 · Passenger/Crew Doors
  > MAIN CABIN DOOR BINDS & IS DIFFICULT TO OPEN. CLEANED & LUBED PAX DOOR SHOOT BOLTS. OPERATIONS CHECKED GOOD IAW AMM 52-11-00.
- [SDR REXA2014012900150](https://openairdocs.org/sdr/REXA2014012900150.md): Flashlight · inoperative · Jan 29, 2014 · N8560F · Cndair CL6002B19 · Emergency Equipment
  > FLIGHT ATTENDANT`S FLASHLIGHT INOPERATIVE. R & R FWD FLIGHT ATTENDANT`S FLASHLIGHT IAW CRJ200 AMM 25-61-02. OPERATIONS CHECKED GOOD, ACFT FOR SERVICE.
- [SDR REXA2013072601387](https://openairdocs.org/sdr/REXA2013072601387.md): Smoke Goggles · failed · Jul 26, 2013 · N8560F · Cndair CL6002B19 · Emergency Equipment
  > JUMP SEAT SMOKE GOGGLES ELASTIC BAND HAS NO ELASTIC LEFT AND IS FULLY STRETCHED. WON`T FIT EVEN IN TIGHTEST POSTION. REPLACED JUMP SEAT'S SMOKE GOGGLES IAW AMM 25-61-00.
- [SDR REXA2013040700732](https://openairdocs.org/sdr/REXA2013040700732.md): Life Vest · unserviceable · Apr 7, 2013 · N8560F · Cndair CL6002B19 · Life Jacket
  > FLIGHT ATTENDANT LIFE VEST HAS HOLE IN BAG. REMOVED AND REPLACED FLIGHT ATTENDANT LIFE VEST IAW AMM 25-61-03.
- [SDR REXA2013031900578](https://openairdocs.org/sdr/REXA2013031900578.md): Connector · loose · Mar 19, 2013 · N8560F · Cndair CL6002B19 · Landing Gear System Wiring
  > ON FLIGHT 4043 (YYZ TO JFK) AFTER TAKEOFF "STEERING INOPERABLE" CAUTION MESSAGE FOLLOWED BY "WOW INPUT" CAUTION. NOSE WHEEL STEERING WOULD NOT RE-ENGAGE WITH QRH. MESSAGES PERSISTED EN ROUTE UNTIL GEAR WAS LOWERED ON APROACH INTO JFK. AFTER LANDING, NOSE WH
- [SDR REXA2013031300390](https://openairdocs.org/sdr/REXA2013031300390.md): Structure · damaged · Mar 9, 2013 · N8560F · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > STRUCTURAL DAMAGE SUSTAINED DURING GEAR SWING AT LEFT MAIN LANDING GEAR UPLOCK WITH DOOR UNATTACHED. REPAIRED IAW REO 601R-53-41-1668.
- [SDR REXA2013031300389](https://openairdocs.org/sdr/REXA2013031300389.md): Structure · damaged · Mar 9, 2013 · N8560F · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > STRUCTURAL DAMAGE SUSTAINED DURING GEAR SWING AT RIGHT MAIN LANDING GEAR UPLOCK WITH DOOR UNATTACHED. REPAIRED IAW REO 601R-53-41-1669.
- [SDR REXA2012111601685](https://openairdocs.org/sdr/REXA2012111601685.md): Unknown · malfunctioned · Nov 16, 2012 · N8560F · Cndair CL6002B19 · Cabin Pressure Control System
  > PERFORMED AN AIR RETURN TO JFK ON FLIGHT 4105 FOR CABIN ALTITUDE WARNING MESSAGE AFTER TAKEOFF DUE TO DEPRESSURIZATION AND MASKS DEPLOYING. REMOVED AND REPLACED THE 25 OXYGEN GENERATORS, OXYGEN MASK WERE STOWED, ALL CHECKS GOOD. COMPLIED WITH SERVICE CHECK O
- [SDR REXA2012102901436](https://openairdocs.org/sdr/REXA2012102901436.md): Charger · inoperative · Oct 29, 2012 · N8560F · Cndair CL6002B19 · Emergency Lighting
  > CHECK FOUND EXIT EMERGENCY LIGHT DSLF INOPERABLE. REPLACED CHARGER ASSEMBLY PS2LF IAW CRJ-200 AMM 33-51-05. OPS CHECK GOOD.
- [SDR REXA2012081901278](https://openairdocs.org/sdr/REXA2012081901278.md): Lamp · inoperative · Aug 19, 2012 · N8560F · Cndair CL6002B19 · Emergency Lighting
  > AFT CEILING EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP, OPS CHECKED GOOD.
- [SDR REXA2012081901279](https://openairdocs.org/sdr/REXA2012081901279.md): Oil System · low pressure · Aug 19, 2012 · N8560F · Cndair CL6002B19 · Engine Oil Pressure
  > ON FLIGHT 3952, THE CREW PERFORMED A RIGHT ENGINE SHUTDOWN DUE TO LOW ENGINE OIL PRESSURE (5PSI) AFTER TAKEOFF FROM FNT. CREW DECLARED AN EMERGENCY AND THE AIRCRAFT LANDED SAFELY. REMOVED AND REPLACED RIGHT ENGINE IAW AMM 71-00-00 AND CHECKLIST PROVIDED. AL
- [SDR REXA201201278](https://openairdocs.org/sdr/REXA201201278.md): Light · inoperative · Aug 19, 2012 · N8560F · Cndair CL6002B19 · Emergency Lighting
  > AFT CEILING EMERGENCY LIGHT INOPERATIVE. OPEN
- [SDR REXA2012052600781](https://openairdocs.org/sdr/REXA2012052600781.md): Light · inoperative · May 26, 2012 · N8560F · Cndair CL6002B19 · Emergency Lighting
  > FWD OVERHEAD EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED FWD OVERHEAD EMERGENCY LIGHT IAW AMM 33-51-21. OPS CHECKED GOOD.
- [SDR REXA2012050900716](https://openairdocs.org/sdr/REXA2012050900716.md): Duct · leaking · May 9, 2012 · N8560F · Cndair CL6002B19 · Air Distribution System
  > FLIGHT ATTENDANT REPORTED CABIN HOT AND THEN SMOKE ODOR, CREW HAD NO WARNINGS, ECS PAGE SHOWED RIGHT PACK DUCT TEMP REACHED 59 DEG C, TURN OFF. SWAPPED COMPRESSOR INLET DUCT FROM LEFT SIDE PER MOD IAW AMM 21-51-10. OPS CHECK LEAK CHECKED GOOD.
- [SDR REXA2012042900578](https://openairdocs.org/sdr/REXA2012042900578.md): Light · inoperative · Apr 29, 2012 · N8560F · Cndair CL6002B19 · Emergency Lighting
  > FORWARD OVERHEAD EMERGENCY LIGHT INOP. REMOVED AND REPLACED FORWARD OVERHEAD EMERGENCY LIGHT IAW AMM 33-50-00.
- [SDR REXA2012042300565](https://openairdocs.org/sdr/REXA2012042300565.md): Transmitter · faulty · Apr 23, 2012 · N8560F · Cndair CL6002B19 · Trailing Flap Position Indicating System
  > SPLIT FLAP CONDITION. SELECTED FLAPS 8: LT FLAP DEPLOYED TO 8 DEG, RT FLAP DEPLOYED TO 2 DEG. RT FLAP POSITION SENSOR RIG CHECKS GOOD. BEGINNING OF THE NIGHT THE RT FLAP WAS 6 DEGREES HIGHER ON EACH FLAP DETENT. BEFORE DEFERRING FLAP POSITION SENSOR IT WAS
- [SDR REXA201100830](https://openairdocs.org/sdr/REXA201100830.md): Light · inoperative · Nov 9, 2011 · N8560F · Cndair CL6002B19 · Emergency Lighting
  > ONE EMERGENCY FLOOR LIGHT STRIP INOP AT 8CD. REMOVED AND REPLACED 1 EMERGENCY FLOOR LIGHT STRIP AT 8CD IAW AMM 33-51-01. OPS CHECK GOOD. VERIFIED PART EFFECTIVITY.
- [SDR REXA201100809](https://openairdocs.org/sdr/REXA201100809.md): Light · inoperative · Nov 9, 2011 · N8560F · Cndair CL6002B19 · Emergency Lighting
  > ONE EMERGENCY FLOOR LIGHT STRIP INOP AT 6CD. REMOVED AND REPLACED 1 EMERGENCY FLOOR LIGHT STRIP AT 6CD IAW AMM 33-51-01. OPS CHECK GOOD. VERIFIED PART EFFECTIVITY.
- [SDR REXA201100302](https://openairdocs.org/sdr/REXA201100302.md): Bulkhead · cracked · May 14, 2011 · N8560F · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FS 559 BULKHEAD HAS CRACK INDICATION AT LBL 18. REPAIRED IAW BOMBARDIER REO REO 601R-53-41-260 REV E.
- [SDR REXA201100252](https://openairdocs.org/sdr/REXA201100252.md): Isis Unit · contaminated · Apr 24, 2011 · N8560F · Cndair CL6002B19 · Integrated Flight System
  > DIS-328597-2011 ISIS INDICATED 0 KNOTS DURING T/O AT 80 KNOTS T/O ABORTED PERGED STBY ISIS SYSTEM WITH NITROGEN TO REMOVE WATER. PERFORMED OPS CHECK OF ISIS IAW AMM 34-14-01. OPS CHECK GOOD. NO OTHER DEFECTS FOUND.
- [SDR REXA201100144](https://openairdocs.org/sdr/REXA201100144.md): Sill · corroded · Feb 24, 2011 · N8560F · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > PASSENGER DOOR SILL PLATE ANGLE INCURRED LEVEL 2 CORROSION FROM FS 319 TO FS 333. REMOVED AND REPLACED PASSENGER DOOR SILL PLATE ANGLE.
- [SDR 2011F00052](https://openairdocs.org/sdr/2011F00052.md): Cargo Track · corroded · Feb 22, 2011 · N8560F · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > CARGOTRACK AT FS 621 LBL 9 CORRODED. CARGO TRACK REPAIRED IAW SRM 51-41-02.
- [SDR 2011F00051](https://openairdocs.org/sdr/2011F00051.md): Floor Support · corroded · Feb 22, 2011 · N8560F · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FLOORBEAM CAP AT LBL 27 FS 621 TO FS 574 IS CORRODED. REPAIRED IAW SRM 51-42-06, 51-42-11, 51-42-21, 51-42-22, AND REO 601R-53-61-3778.
- [SDR 2011F00049](https://openairdocs.org/sdr/2011F00049.md): Floorbeam · corroded · Feb 22, 2011 · N8560F · Cndair CL6002B19 · Fuselage Main, Structure
  > FS 280, FWD FLOOR SUPPORT FOUND CORRODED.
- [SDR REXA201100136](https://openairdocs.org/sdr/REXA201100136.md): Cargo Track · corroded · Feb 19, 2011 · N8560F · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > CARGO SEAT TRACKS AT FS 621 LBL NINE, FS 559+112 RBL AND LBL NINE, FS 559+96 RBL AND TWENTY-SEVEN ARE CORRODED. CARGO TIE DOWN TRACKS REPAIRED AT LBL 9, FS 621, RBL + LBL 559+112, RBL + LBL 27, FS 559+96 IAW CRJ 200 SRM 51-41-02.
- [SDR REXA201100135](https://openairdocs.org/sdr/REXA201100135.md): Floorbeam · corroded · Feb 19, 2011 · N8560F · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > FLOORBEAM CAP AT LBL 27 FS 621 TO FS 574 IS CORRODED. REPAIRED FLOORBEAM CAP AT LBL 27 FS 621 TO FS 574 IAW CRJ 200 SRM 51-42-06, 51-42-11, 51-42-21, 51-42-22, AND BOMBARDIER REO 601R-53-61-3778.
- [SDR REXA201100134](https://openairdocs.org/sdr/REXA201100134.md): Floor Support · corroded · Feb 19, 2011 · N8560F · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FS 280 FWD FLOOR SUPPORT IS CORRODED. REPAIRED FS 280 FWD FLOOR SUPPORT ANGLE P/N 600-34017-351S IAW CRJ 200 SRM 51-42-06, 51-40-11, 51-21-11, 51-23-00, AND 51-42-21.
- [SDR REXA201000252](https://openairdocs.org/sdr/REXA201000252.md): Hinge Fitting · gouged · Nov 5, 2010 · N8560F · Cndair CL6002B19 · Trailing Edge Flaps
  > DAMAGE WAS FOUND ON THE LEFT WING OUTBOARD FLAP HINGE ARM ASSEMBLY ON THE P/N 601R14611-41 FITTING AT WS-264. DAMAGE TO THE HINGE ARM FITTING CONSISTS OF GOUGING THAT MEASURES 0.75 INCH LONG BY FULL WIDTH OF FITTING WIDE WITH A MAXIMUM DEPTH OF 0.030 INCH. R
- [SDR REXA201000139](https://openairdocs.org/sdr/REXA201000139.md): Warning System · activated · Sep 15, 2010 · N8560F · Cndair CL6002B19 · AC Indicating System
  > ACESS BUS CAUTION MESSAGE. AIRCRAFT STILL IN WORK.
- [SDR REXA201000055](https://openairdocs.org/sdr/REXA201000055.md): Engine · leaking · Apr 24, 2010 · N8560F · Cndair CL6002B19 · Engine (Turbine/Turboprop)
  > AT THE 80 KNOT CALL OUT, ON TAKEOFF ROLL FROM KMEM THE F/O ALERTED THE CAPTAIN TO THE LT ENGINE ITT INDICATION BEING APPROXIMATELY 900 DEGREES AND IN THE RED. THE CAPTAIN ABORTED THE TAKEOFF AND CLEARED THE RUNWAY. THE QRH WAS COMPLETED AND THE CAPTAIN ELECTE
- [SDR REXA2009000031](https://openairdocs.org/sdr/REXA2009000031.md): Coalescer Bag · contaminated · Mar 12, 2009 · N8560F · Cndair CL6002B19 · Humidity Control System
  > AFTER ENGINE START USING GROUND AIR START CABIN BEGIN TO FILL WITH SMOKE. ENGINE SHUTDOWN AND PLANE DEPLANED. MX INSPECTED ACFT, FOUND BOTH LT AND RT ACM (AIR CYCLE MACHINE) WATER SEPARATOR COALESCER BAGS CONTAMINATED WITH OIL, COALESCER BAGS REPLACED, GROUN
- [SDR REXA200600035](https://openairdocs.org/sdr/REXA200600035.md): Flap System · malfunctioned · Mar 11, 2006 · N8560F · Cndair CL6002B19 · Trailing Edge Flap Control System
  > ON APPROACH RECEIVED FLAPS FAIL MESSAGE WHEN SELECTING FLAPS EIGHT DEGREES. QRH PERFORMED, DECLARED EMERGENCY, PERFORMED FLAPS ZERO UNEVETFUL LANDING. MAINT RESET SYSTEM AND PLACED ON 72 HOUR WATCH PER AD 98-20-01.
- [SDR REXA200500156](https://openairdocs.org/sdr/REXA200500156.md): Engine · damaged · Dec 14, 2005 · N8560F · Cndair CL6002B19 · Engine (Turbine/Turboprop)
  > WHEN LEVEL AT FL300 THE RT ENGINE SHUTDOWN. FLIGHT CREW FOLLOWED COMPANY PROCEDURES AND LANDED WITH NO OTHER PROBLEMS. MAINTENANCE FOUND SEVER DAMAGE TO THE ENGINE'S FAN SECTION. THE ENGINE WAS REPLACED AND THE AIRCRAFT RELEASED FOR SERVICE. DAMAGED ENGINE WI
- [SDR REX2005F00013](https://openairdocs.org/sdr/REX2005F00013.md): Sensor · failed · Jul 20, 2005 · N8560F · Cndair CL6002B19 · Trailing Flap Position Indicating System
  > (REF NR 05-090) FLAPS FAIL AT 4 DEGREES ON FINAL. PERFORMED RIGGING OF LT AND RT BRAKE POSITION SENSING UNIT ( BPSL) IAW AMM. (K)
- [SDR REX2002F00002](https://openairdocs.org/sdr/REX2002F00002.md): Proximity Switch · out of adjust · May 22, 2002 · N8560F · Cndair CL6002B19 · Landing Gear Position and Warning
  > (SWITCH) -ON DEPARTURE AFTER GEAR SELECTED UP, CREW RECEIVED A (NOSE DOOR OPEN) MESSAGE AND A GEAR DISAGREE WARNING. CHECKLIST WAS FOLLOWED AND A UNEVENTFUL LANDING WAS MADE. FOUND NOSE LANDING GEAR STRUT CENTERING PROXIMITY SWITCH OUT OF ADJUSTMENT.

## 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 = 'N8560F' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N8560F/reports

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