# Service difficulty reports: N87, cancelled Dec 24, 2025

A list on [N87, cancelled Dec 24, 2025](https://openairdocs.org/deregistered/N87-2025-12-24.md).

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

- [SDR RU3A2021052101111](https://openairdocs.org/sdr/RU3A2021052101111.md): Selector Valve · faulted · May 21, 2021 · N87 · Cndair CL6002B16 · Landing Gear Door Retract Section
  > GEAR FAILED TO RETRACT AFTER TAKEOFF. 'I/P WOW' LIGHT ILLUMINATED. REPLACED DOOR SELECTOR VALVE AND WEIGHT ON WHEELS HARNESS ON NOSE LANDING GEAR
- [SDR RU3A20200108001](https://openairdocs.org/sdr/RU3A20200108001.md): Warning Light · activated · Jan 7, 2020 · N87 · Cndair CL6002B16 · Stall Warning System
  > STALL PROTECTION SYSTEM FAIL LIGHTS FLASHING IN FLIGHT.
- [SDR RU3A201912065072](https://openairdocs.org/sdr/RU3A201912065072.md): Wire Harness · damaged · Dec 4, 2019 · N87 · Cndair CL6002B16 · Landing Gear System Wiring
  > R/ OUTBOARD ANTI-SKID FAIL ILLUMINATED AFTER TEST. (AIRBORNE)...TEMP REPAIR #2 MLG HARNESS FOR SFP TO REPAIR STATION. WILL MONITOR
- [SDR RU3A20191030060](https://openairdocs.org/sdr/RU3A20191030060.md): Motor · failed · Oct 30, 2019 · N87 · Cndair CL6002B16 · Trailing Edge Flap Actuator
  > FLAP MOTOR 2 CIRCUIT BREAKER POPPED IN FLIGHT. REPLACING FLAP MOTOR CORRECTED THE DISCREPANCY.
- [SDR RU3A20191030058](https://openairdocs.org/sdr/RU3A20191030058.md): Charger · failed · Oct 30, 2019 · N87 · Cndair CL6002B16 · Battery/Charger System
  > BATTERY CHARGER CIRCUIT BREAKER TRIPPED IN FLIGHT. CORRECTION: REMOVED AND REPLACED AIRCRAFT BATTERY CHARGER.
- [SDR RU3A20190628026](https://openairdocs.org/sdr/RU3A20190628026.md): Skin · cracked · Jun 19, 2019 · N87 · Cndair CL6002B16 · Wing, Plate/Skin
  > CRACKS THE WING SKIN
- [SDR RU3A20181210050](https://openairdocs.org/sdr/RU3A20181210050.md): Control Head · burned · Dec 10, 2018 · N87 · Cndair CL6002B16 · Audio/Video Monitoring
  > DESCENDING THROUGH 5000'MSL CREW NOTICED ACRID SMELL. DONNED OXYGEN MASK AND TURNED AFIS OFF. SMELL SLOWLY DISSIPATED. NO SMOKE WAS VISIBLE. CAUSE WAS FOUND TO BE CVR CONTROL HEAD BURNED INTERNALLY.
- [SDR RU3A2018031200002](https://openairdocs.org/sdr/RU3A2018031200002.md): Crank Assy · cracked · Mar 5, 2018 · N87 · Cndair CL6002B16 · Passenger/Crew Doors
  > PASSENGER DOOR LATCH MECHANISM CRANK CRACKED PART 600-31890-21.
- [SDR RU3A20171205043](https://openairdocs.org/sdr/RU3A20171205043.md): Display · inoperative · Dec 5, 2017 · N87 · Cndair CL6002B16 · Indicating/Recording System
  > AFIS FAILED IN FLIGHT. DISPLAY WENT DEAD, AND ELECTRICAL FUMES WERE PRESENT. MILTOPE(EIFW IN-FLT WKSTATION)
- [SDR RU3A20171012034](https://openairdocs.org/sdr/RU3A20171012034.md): Windshield · cracked · Oct 12, 2017 · N87 · Cndair CL6002B16 · Flight Compartment Windows
  > PILOT SIDE FRONT WINDOW OUTER GLASS HAD A MAJOR CRACK. REMOVED AND REPLACED PILOT'S WINDSHIELD.
- [SDR RU3A20170210003](https://openairdocs.org/sdr/RU3A20170210003.md): Connector · dirty · Feb 10, 2017 · N87 · Cndair CL6013A · Ice/Rain Protection System Wiring
  > RIGHT ENGINE COWL ANTI-ICE FAIL LIGHT ILLUMINATED DURING FLIGHT, PROBLEM WAS CORRECTED AFTER CLEANING OF ELECTRICAL CONNECTORS.
- [SDR RU3A20151021022](https://openairdocs.org/sdr/RU3A20151021022.md): Anti-Ice System · defective · Sep 29, 2015 · N87 · Cndair CL6002B16 · Windshield/Door Rain/Ice Removal
  > PILOT LT SIDE WINDSHIELD HEAT FAIL. REPEAT FAILURE.
- [SDR RU3A20150811017](https://openairdocs.org/sdr/RU3A20150811017.md): Fms · malfunctioned · Aug 11, 2015 · N87 · Cndair CL600* · Flight Management Computing Hardware System
  > WAAS 1 & WAAS 2 FAILED IN CRUISE FLIGHT. MULTIPLE NAV SYS FAILURES, FD, CDU, FMS 1 & 2 FLAGS ON MFD BOTH SIDE NAV INDICATIONS FAILED. RE-SEATING & RE-LOADING THE FMS DATABASES CORRECTED THE ISSUE.
- [SDR RU3A20140519019](https://openairdocs.org/sdr/RU3A20140519019.md): Hydraulic Line · loose · May 19, 2014 · N87 · Cndair CL6002B16 · Hydraulic System, Auxiliary
  > SUPPLEMENTAL INFORMATION: CORRECT ATA CODE(C) TO 2910, CORRECT HOW DISCOVERED (E) TO V-VISUAL. CORRECTIVE ACTION: FOUND LOOSE B NUT ON HYDRAULIC TUBE ASSY P/N: 601-75238-43 AFT CONNECTION. INSPECTED B-NUT, RE-TORQUED B NUT FITTING. LEAK CHECK SATISFACTORY
- [SDR RU3A20130502006](https://openairdocs.org/sdr/RU3A20130502006.md): Window · cracked · May 1, 2013 · N87 · Cndair CL6002B16 · Flight Compartment Windows
  > DURING FLIGHT, CREW HEARD LOUD POP. INITIAL INSPECTION DISCOVERED LEFT PILOT SIDE WINDOW WITH LARGE CRACK AND SIGNIFICANT GAP IN OUTER PANE WITH ASSOCIATED "FAIL" LIGHT ON WINDSHIELD HEAT.
- [SDR RU3A1203](https://openairdocs.org/sdr/RU3A1203.md): Thrust Reverser · malfunctioned · Feb 15, 2012 · N87 · Cndair CL6002B16 · Engine Thrust Reverser
  > AT FL150, GOT RIGHT T/R UNLOCK LIGHT. CREW PRESSED T/R EMERGENCY STOW AND COMPLIED WITH CHECKLISTS. DECLARED EMERGENCY AND DIVERTED TO NEAREST AIRPORT WITH ADEQUATE RUNWAY LENGTH.
- [SDR RU3A1119](https://openairdocs.org/sdr/RU3A1119.md): Bulkhead · buckled · Sep 16, 2011 · N87 · Cndair CL6002B16 · Fuselage Main, Bulkhead
  > BULKHEAD AND AIRCRAFT SKIN AT FORWARD FUSELAGE STATION 235 IS CRACKED AND BUCKLED.
- [SDR RU3A1109](https://openairdocs.org/sdr/RU3A1109.md): Proximity Switch · faulty · Feb 15, 2011 · N87 · Cndair CL6002B16 · Landing Gear Position and Warning
  > AFTER TAKEOFF THE LANDING GEAR HANDLE WAS MOVED TO THE UP POSITION. BOTH MAIN GEAR RETRACTED BUT THE NOSE GEAR DID NOT RETRACT. THE ONLY INDICATION IN THE COCKPIT WAS ONE GREEN NOSE GEAR DOWN LIGHT. HOLDING WAS COORDINATED WITH ATC. EMERGENCY AND NORMAL CH
- [SDR RU3A1018](https://openairdocs.org/sdr/RU3A1018.md): Unknown · malfunctioned · Jul 23, 2010 · N87 · Cndair CL6002B16 · Autopilot System
  > TWO UNCOMMANDED ABRUPT RIGHT RUDDER INPUTS. AUTOPILOT ON. YAW DAMP ON. AIRCRAFT CLIMBING THROUGH 8000 FEET AT 250 KNOTS. SECOND EVENT 11000 FEET AT 250 KNOTS. NO SERVO MONITOR LIGHT ILLUMINATED. NO INDICATION OF JAM RUDDER. ALL THREE HYDRAULIC SYSTEM PRE
- [SDR RU3A1007](https://openairdocs.org/sdr/RU3A1007.md): Windshield · split · Mar 1, 2010 · N87 · Cndair CL6002B16 · Flight Compartment Windows
  > AFTER APPROXIMATELY 1.0 HOUR OF FLYING IN THE CLIMBOUT TO NEXT WORK, NOTICED WINDSHIELD SPLITTING FROM A SMALL SCRATCH. LEVELED OFF TO 17,000 FEET, RAN CHECKLIST AND GOT CLEARANCE TO RETURN.
- [SDR RU3A004](https://openairdocs.org/sdr/RU3A004.md): Hydraulic Line · chafed · Oct 20, 2008 · N87 · Cndair CL6002B16 · Hydraulic System, Main
  > NUMBER 2 HYDRAULIC SYSTEM LOST PRESSURE ON APPROACH. FOUND PRESSURE HOSE ASSY IN PYLON CHAFED BY HOSE CLAMP WHERE RUBBER LINER WAS ERODED AND THE CLAMP AND HOSE WERE METAL TO METAL. REPLACED HOSE, CLAMP, AND ENGINE DRIVEN HYDRAULIC PUMP. INSPECTED FILTERS,
- [SDR RU3A0710](https://openairdocs.org/sdr/RU3A0710.md): Windshield · cracked · Dec 3, 2007 · N87 · Cndair CL6002B16 · Flight Compartment Windows
  > FLYING AT FL340 1.5 HOURS INTO FLIGHT THE CO-PILOTS WINDSHIELD OUTER PLY CRACKED. COMING INTO THE TERMINAL AREA WITH -3 DEGREE C AND MOISTURE IN THE AIR, RAIN STARTED TO GET INSIDE THE CRACK. ON A 14 MILE ILS FINAL TO RWY 28 AT ABOUT 3000' HEARD A LOUD POP A
- [SDR RU32006F00001](https://openairdocs.org/sdr/RU32006F00001.md): Wing · scratched · Apr 17, 2006 · N87 · Cndair CL6002B16 · Wing, Plate/Skin
  > UPON POST FLT, DISCOVERED STRATCHES ON RT WINGLET. APPARENTLY WHILE POSITIONING OVER GCP AT RKTP, SCRAPED GCP SIGN. NO INDICATION OF CONTACT WHILE AT RTKP. RETURNED TO RKSO WHERE DAMAGE WAS NOTED. PERFORMED TEMP REPAIR REFERENCE REO. (K)
- [SDR RU3A0419](https://openairdocs.org/sdr/RU3A0419.md): Seal · deteriorated · Nov 29, 2004 · N87 · Cndair CL6002B16 · Fuel Storage
  > AFTER TAKEOFF FUEL WAS SEEN STREAMING OUT OF LT OVERWING FUEL CAP DURING CLIMB. REPLACED FUEL CAP.
- [SDR 2004F00076](https://openairdocs.org/sdr/2004F00076.md): Sensor · failed · Jan 16, 2004 · N87 · Cndair CL6002B16 · Landing Gear Position and Warning
  > ON FINAL APPROACH GEAR EXTENSION AND ANTI-SKID OUTBOARD FAIL MALFUNCTION OCCURRED. GEAR RECYCLED AND SOME TROUBLESHOOTING WAS UNSUCCESSFUL. IN FLIGHT EMERGENCY WAS DECLARED, EQUIPMENT CALLED OUT, ANTI-SKID TURNED OFF AND UNEVENTFUL LANDING CARRIED OUT. NO DA
- [SDR RU3A03015](https://openairdocs.org/sdr/RU3A03015.md): Tube · cracked · Oct 10, 2003 · N87 · Cndair CL6002B16 · Hydraulic System, Main
  > NR 1 HYDRAULIC SYSETM FAILED IN FLIGHT WITH COMPLETE LOSS OF FLUID WITHING THAT SYSTEM. FOUND HYDRAULIC LINE WITH CRACK AT BEND RADIUS. REPLACED HYDRAULIC LINE. ALSO, REPLACED HYDRAULIC PUMP AND FILTERS DUE OT LOSS OF FLUID. (M)
- [SDR R33A03015](https://openairdocs.org/sdr/R33A03015.md): Line · broken · Oct 10, 2003 · N87 · Cndair CL6002B16 · Hydraulic System, Main
  > NR 1 HYDRAULIC SYSTEM FAILED IN FILGHT WITH COMPLETE LOSS OF FLUID WITHIN THAT SYSTEM. FOUND HYDRAULIC LINE SNAPPED OFF. REPLACED HYDRAULIC LINE. ALSO, REPLACED HYDRAULIC PUMP AND FILTERS DUE TO LOSS OF FLUID. (M)
- [SDR RU32003F00003](https://openairdocs.org/sdr/RU32003F00003.md): Housing · cracked · Apr 30, 2003 · N87 · Cndair CL6002B16 · APU Engine Fuel and Control
  > APU FUEL FILTER HOUSING ATTACHMENT FLANGES CRACKED. THIS IS THE FIFTH FILTER HOUSING THAT HAS CRACKED SINCE 01/30/99, THREE ON N86 AND TWO ON N87. AFTER INVESTIGATION IT WAS CONCLUDED THAT THE FUEL FILTER HOUSING FAILURES ARE THE RESULT OF FUEL CONTROL UNIT
- [SDR 2003F00235](https://openairdocs.org/sdr/2003F00235.md): Windshield · cracked · Mar 26, 2003 · N87 · Cndair CL6002B16 · Flight Compartment Windows
  > DURING CRUISE AT FL330, PILOTS WINDSHIELD, OUTER PLY, POPPED AND THEN CRACKED IMMEDIATELY FROM TOP TO BOTTOM ORIGINATING FROM CENTER. (M)
- [SDR RU3A03003](https://openairdocs.org/sdr/RU3A03003.md): Housing · cracked · Feb 17, 2003 · N87 · Cndair CL6002B16 · APU Engine Fuel and Control
  > APU FUEL FILTER HOUSING ATTACHMENT FLANGES, CRACKED. THIS IS THE 5TH FILTER HOUSING THAT HAS CRACKED SINCE 01/30/99, 3 ON N86, AND 2 ON N87.
- [SDR RU32001F00000](https://openairdocs.org/sdr/RU32001F00000.md): Cover · broken · Jul 3, 2001 · N87 · Cndair CL6002B16 · APU Engine Fuel and Control
  > APU MODEL NUMBER GTCP 36-150RJ. THE LOW PRESSURE FUEL FILTER COVER MOUNTING EAR WAS COMPLETELY BROKEN OFF THE COVER WHERE THE MOUNTING BOLT ATTACHES THE COVER TO THE FUEL CONTROL. APU CONTINUED TO RUN AFTER EAR BROKE OFF.
- [SDR RU3A99007](https://openairdocs.org/sdr/RU3A99007.md): Fuel Cap · dirty · Jun 29, 1999 · N87 · Cndair CL6002B16 · Fuel Storage
  > FUEL OBSERVED STREAMING DOWN THE RIGHT-HAND WING DURING FLIGHT. FUEL WAS LEAKING AT THE RIGHT-HAND OUTBOARD FUEL CAP. AIRCRAFT MADE UNSCHEDULED LANDING. THE LOCKING DEVICE ON THE CAP WAS INSPECTED AND FOUND TO BE FUNCTIONING PROPERLY. FOREIGN MATTER WAS FOU

## 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 = 'N87' AND deregistration_id = 'N87-2025-12-24'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N87-2025-12-24/reports

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