# Service difficulty reports: N215PS, cancelled Dec 9, 2025

A list on [N215PS, cancelled Dec 9, 2025](https://openairdocs.org/deregistered/N215PS-2025-12-09.md).

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

Page 1 of 2 · 67 reports

- [SDR VNAA2020022311101](https://openairdocs.org/sdr/VNAA2020022311101.md): Inverter · failed · Feb 23, 2020 · N215PS · Cndair CL6002B19 · Emergency Lighting
  > R&R #2 EMERGENCY LIGHT INVERTER IAW CRJ 200 AMM 33-51-07-000/400-801 OPS CHECK GOOD AT THIS TIME.
- [SDR VNAA2020021399908](https://openairdocs.org/sdr/VNAA2020021399908.md): Intercostal · cracked · Feb 13, 2020 · N215PS · Bombdr CL6002D15 · Fuselage Miscellaneous Structure
  > LH UPPER INTERCOSTAL FROM FS 621 TO FS 625, BL 45, STR 14L, WL 97.5 IS CRACKED APPROX 0.5" LONG. R.CHEUVRONT 1/12/20 (PCC) M/A: 1. REMOVED INTERCOSTAL IAW CRJ 200 SRM 51-42-21. INSTALLED INTERCOSTAL IAW CRJ 200 SRM 51-42-21 AND 51-25-16.
- [SDR VNAA2020021399907](https://openairdocs.org/sdr/VNAA2020021399907.md): Bulkhead Web · cracked · Feb 13, 2020 · N215PS · Bombdr CL6002D15 · Fuselage Main, Bulkhead
  > 5 EA AREAS OF CRACK INDICATIONS NOTED ON FS 621 RPB WEB IN THE HEEL LINE AREA OF VERT POST. 1ST AREA AT RBL 9 WL 127 - 132.5 50% FSH, SECOND AREA AT RBL 9 WL 110 - WL 115 60% FSH, THIRD AREA AT LBL 18 WL 127.25 - WL 135 50% FSH, 4TH LBL 18 WL 100.5 - WL 105 60
- [SDR VNAA2020021399906](https://openairdocs.org/sdr/VNAA2020021399906.md): Post · cracked · Feb 13, 2020 · N215PS · Bombdr CL6002D15 · Fuselage Main, Structure
  > ONE CRACK ON LH WINDISHIELD SIDE POST LOWER AFT ATTACH FITTING IN RADIUS 0.150" LONG. MARKED ON A/C IN RED SHARPIE. REMOVED DAMAGED LH WINDSHIELD SIDE POST LOWER AFT ATTACH FITTING IAW CRJ 200 SRM 51-42-21. INSTALLED NEW SERVICEABLE LH WINDSHIELD SIDE POST L
- [SDR VNAA2020021399905](https://openairdocs.org/sdr/VNAA2020021399905.md): Post · cracked · Feb 13, 2020 · N215PS · Bombdr CL6002D15 · Fuselage Main, Structure
  > ONE CRACK INDICATION NOTED ON LH WINDSHIELD SIDE POST AT LOWER C/B FASTENER APPROX 1.500" LONG BY 100% FSH. FAILED NDT INSP. MARKED ON A/C WIHT SHARPIE. B.FLEEMAN 01/14/20 (ROSEM) M/A: 1. REMOVED L/H SIDE POST TRAP IAW CRJ-200 AMM 56-12-01-000-801-PSA J.BARTLE
- [SDR VNAA2020021399904](https://openairdocs.org/sdr/VNAA2020021399904.md): Strap · corroded · Feb 13, 2020 · N215PS · Bombdr CL6002D15 · Fuselage Main, Floor Beam
  > FS 559 FLOOR SUPPORT STRAP CORRODED BETWEEN LBL 45 AND LBL 27. REMOVED SUPPORT STRAP BETWEEN LBL 45 AND LBL 27 IAW CRJ 200 SRM 51-42-06. LOCATED AND DRILLED NEW SUPPORT STRAP BETWEEN LBL 45 AND LBL 27 FS 559 IAW CRJ 200 SRM TR 51-42, 51-42-06.
- [SDR VNAA2020021399903](https://openairdocs.org/sdr/VNAA2020021399903.md): Strap · corroded · Feb 13, 2020 · N215PS · Bombdr CL6002D15 · Fuselage Main, Floor Beam
  > FS 559 FLOOR SUPPORT STREP CORRODED BETWEEN RBL 27 AND RBL 45. REMOVED FLOOR SUPPORT STRAP BETWEEN RBL 27 AND RBL 45 IAW SRM 51-42-06. LOCATED AND DRILLED NEW SUPPORT STRAP BETWEEN RBL 27 AND RBL 45 IAW CRJ 200 SRM TR 51-42. INSTALLED NEW SUPPORT STRAP BET
- [SDR VNAA2020021399902](https://openairdocs.org/sdr/VNAA2020021399902.md): Frame · corroded · Feb 13, 2020 · N215PS · Bombdr CL6002D15 · Fuselage Main, Frame
  > DEEP CORROSION ON LH FS 513 FRAME AFT FREE FLANGE JUST ABOVE FLOOR IN 1" AREA AT CORNER OF PART. MARKED WITH TAPE. BLOCKED OUT CORROSION ON FRAME, BLEND OUT IS.075" DEEP EVALUATED DAMAGE AND FOUND TO BE OUT OF ALLOWABLE LIMITS IAW CRJ200 SRM 53-00-00 FIG 10
- [SDR VNAA2020021399901](https://openairdocs.org/sdr/VNAA2020021399901.md): Attach Angle · cracked · Feb 13, 2020 · N215PS · Bombdr CL6002D15 · Passenger/Crew Doors
  > PAX DOOR MOTOR BOTTOM ATTACH ANGLE CRACKED. DISPLACED POWER ASSIST MOTOR FOR ACCESS. CANON PLUG WAS NOT DISCONNECTED. REINSTALLED PAX DOOR MOTOR ASSIST IAW CRJ200 AMM 52-11-08-400-802. REFER TO JOB: 27880105, OP:35 FOR COMPLETION OF INSTALL AND OPERATIONAL
- [SDR VNAA2019123081103](https://openairdocs.org/sdr/VNAA2019123081103.md): Contact · dirty · Dec 28, 2019 · N215PS · Cndair CL6002B19 · Emergency Lighting
  > LOWER EMERGENCY EXIT LIGHT INOPERATIVE ON THE L/H SIDE BY THE EMERGENCY DOOR. REMOVED EMERGENCY LIGHT, CLEANED CONTACTS, AND REINSTALLED EMERGENCY LIGHT IAW AMM. OPS CHECKED GOOD.
- [SDR VNAA2019120541101](https://openairdocs.org/sdr/VNAA2019120541101.md): Warning Message · false activation · Dec 4, 2019 · N215PS · Cndair CL6002B19 · Airfoil Anti/De-ice System
  > FLIGHT 5663 DCA/CLE DIVERTED TO CMH DUE TO MAINTENANCE. IN FLIGHT WHILE ON DESCENT INTO CLE ANTI-ICE CAUTION MESSAGE ALERT. CREW RAN QRH AND CAUTION MESSAGE EXTINGUISHED IN FLIGHT. / CREW DECIDED TO CONTINUE DIVERSION AFTER CAUTION MESSAGE EXTINGUISHED. C/W OP
- [SDR VNAA2019042641101](https://openairdocs.org/sdr/VNAA2019042641101.md): Computer · failed · Apr 24, 2019 · N215PS · Cndair CL6002B19 · Fuel Quantity Indicator
  > EMERGENCY DECLARED DUE TO LT AND TOTAL FUEL READOUT DASHED OUT DURING CRUISE. CAPTAIN CONTINUED FLT AND LANDED SAFELY. READOUTS REMAINED DASHED OUT FOR THE REST OF THE FLIGHT AFTER THE EMERGENCY WAS DECLARED.
- [SDR VNAA2017121399908](https://openairdocs.org/sdr/VNAA2017121399908.md): Bulkhead Web · cracked · Dec 13, 2017 · N215PS · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FOUND REAR PRESSURE BULKHEAD WEB HAS MULTIPLE INDICATIONS NOTED AT LBL 27.50 WL83; BL0 WL114; RBL 18 WL 113; RBL 27.5 WL 87; RBL 27.5 WL 132; BL 0 WL 132. C/A: PERFORMED 621 BLKHD REPAIR IAW REO 601R-53-61-6352 REV -- WITH REF REO 601R-53-61-1240 REV D
- [SDR VNAA2017121399907](https://openairdocs.org/sdr/VNAA2017121399907.md): Frame · corroded · Dec 13, 2017 · N215PS · Cndair CL6002B19 · Fuselage Main, Frame
  > FRAME FS 605, LOWER SECTOR, 27-26L FWD FLANGE IS CORRODED. C/A: INSTALLED FRAME SECTOR @ FS 605 IAW CRJ 200 SRM 51-42-06 AND 51-42-21.
- [SDR VNAA2017121399906](https://openairdocs.org/sdr/VNAA2017121399906.md): Strap · corroded · Dec 13, 2017 · N215PS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RIGHT FLOORBEAM STRAP AT FS 559 BETWEEN RBL 27 AND RBL 43 IS CORRODED.C/A: INSTALLED NEW SERVICEABLE STRAP IAW CRJ 200 SRM 51-42-06 & 51-42-15.
- [SDR VNAA2017121399905](https://openairdocs.org/sdr/VNAA2017121399905.md): Strap · corroded · Dec 13, 2017 · N215PS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LEFT FLOORBEAM STRAP AT FS 559 BETWEEN LBL 27 AND LBL 43 IS CORRODED. C/A: LOCATED, DRILLED AND INSTALLED LEFT FLOOR SUPPORT STRAP AT FS 559 BETWEEN LBL 27 AND LBL 43 IAW CRJ 200 SRM 51-40-11 AND 51-42-06.
- [SDR VNAA2017121399904](https://openairdocs.org/sdr/VNAA2017121399904.md): Frame · cracked · Dec 13, 2017 · N215PS · Cndair CL6002B19 · Fuselage Main, Frame
  > FUSELAGE FS 333.0 FRAME IS CRACKED BETWEEN STGR0 AND STGR 1L. C/A: REMOVED AND REPLACED CRACKED FRAME SECTOR BETWEEN STGR 0 AND STGR 1L @ FUSELAGE FS 333.0 IAW BOMBARDIER CRJ 200 SRM REF 51-42-06.
- [SDR VNAA2017121399903](https://openairdocs.org/sdr/VNAA2017121399903.md): Frame · cracked · Dec 13, 2017 · N215PS · Cndair CL6002B19 · Fuselage Main, Frame
  > FUSELAGE FS 718 FRAME IS CRACKED AT STGR 11R. C/A: INSTALLED NEW PART F.S 718 P/N 600-36030-24 IAW CRJ200 SRM 51-42-06, 51-42-21, AND 51-41-00.
- [SDR VNAA2017121399902](https://openairdocs.org/sdr/VNAA2017121399902.md): Frame · corroded · Dec 13, 2017 · N215PS · Cndair CL6002B19 · Passenger/Crew Doors
  > PASSENGER DOOR INTERNAL FRAME CORRODED. LOCATED AT CENTER-LINE JUST BELOW PASSENGER DOOR HANDLE HOUSING. C/A: INSTALLED NEW FRAME IAW CRJ200 SRM 51-42-06 AND 51-42-21 AND 51-77-00.
- [SDR VNAA2017121399901](https://openairdocs.org/sdr/VNAA2017121399901.md): Vane Cap · chafed · Dec 13, 2017 · N215PS · Cndair CL6002B19 · Trailing Edge Flaps
  > RH INBD FLAP VANE SKIN IS CHAFED AT TWO LOCATIONS (MIDDLE AND INBD). C/A: INSTALLED SERVICEABLE LEADING EDGE. P/N 601R14303-52S & -54S IAW CRJ 200 SRM 51-40-11, 51-42-13.
- [SDR VNAA2017072611101](https://openairdocs.org/sdr/VNAA2017072611101.md): Carbon Seal · leaking · Jul 26, 2017 · N215PS · Cndair CL6002B19 · Engine Oil Pressure
  > ON FLIGHT LEVEL 270, THE AIRCRAFT LOST THE RIGHT ENGINE OIL PRESSURE. THEY DECENDED TO FLIGHT LEVEL 170 WHERE THEY CONTINUED TO LOSE OIL PRESSURE, AND SHUT DOWN THE RIGHT ENGINE AND DIVERTED. THE CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. MAINTEN
- [SDR VNAA2016121200023](https://openairdocs.org/sdr/VNAA2016121200023.md): Wire Harness · faulty · Dec 12, 2016 · N215PS · Cndair CL6002B19 · Light System Wiring
  > EMERGENCY FLOOR LIGHTS ON ROW 1 THROUGH 5 INOPERATIVE. REMOVED AND REPLACED WIRING HARNESS.
- [SDR VNAA2016062800032](https://openairdocs.org/sdr/VNAA2016062800032.md): Control Unit · faulty · Jun 28, 2016 · N215PS · Cndair CL6002B19 · Stabilizer Actuator
  > HORIZONTAL STABILIZER TRIM CONTOL UNIT FLAGGING MOTOR NR 1 DURING CLIMBOUT. THE CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, R & R THE STAB TRIM MOTOR CONTROL UNIT AND PERFORMED CHECKS IAW THE AMM. THE ACFT WAS RELEASE FOR SE
- [SDR VNAA2016020700013](https://openairdocs.org/sdr/VNAA2016020700013.md): Bottle · low pressure · Feb 7, 2016 · N215PS · Cndair CL6002B19 · Crew Oxygen System
  > CREW REPORTED OXYGEN LOW PRESSURE CAUTION MESSAGE IN FLIGHT. CREW DIVERTED AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED, SERVICED CREW OXYGEN SYS AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.
- [SDR VNAA2015020500002](https://openairdocs.org/sdr/VNAA2015020500002.md): Proximity Sensor · contaminated · Feb 5, 2015 · N215PS · Cndair CL6002B19 · Landing Gear Position and Warning
  > CREW REPORTED STEERING INOPERATIVE AND WEIGHT ON WHEELS, INPUT CAUTION MESSAGES JUST AFTER ROTATION. MESSAGE CLEARED WHEN GEAR WAS SELECTED DOWN. CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT AND FOUND NLG WOW SENSOR HAD FAULTE
- [SDR VNAA2014102800018](https://openairdocs.org/sdr/VNAA2014102800018.md): Element · out of position · Oct 28, 2014 · N215PS · Cndair CL6002B19 · Overheat Detection
  > CREW REPORTED RIGHT FOURTEENTH DUCT MESSAGE IN FLIGHT. CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND FOUND RT FOURTEENTH PYLON LOOP RUBBING AIRFRAME IN 2 PLACES AND UNCLAMPED IN ONE. MAINTENANCE CLAMPED AND REPOSITIONED LOOP A
- [SDR VNAA2014102800017](https://openairdocs.org/sdr/VNAA2014102800017.md): Reservoir · leaking · Oct 28, 2014 · N215PS · Cndair CL6002B19 · Hydraulic Reservoir, Main
  > CREW REPORTED LOSS OF FLUID FROM HYDRAULIC SYSTEM NR 2 WITH QUANTITY AT ZERO PERCENT. CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED, R & R NR 2 HYD RESERVOIR AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.
- [SDR VNAA2014041100011](https://openairdocs.org/sdr/VNAA2014041100011.md): Computer · faulted · Apr 11, 2014 · N215PS · Cndair CL6002B19 · Attitude and Direction Data System
  > DURING CRUISE AT FL290 AND WITH APU OFF, CREW REPORTED YAW DAMPER NR 2 AND AUTOPILOT WENT OFF AND EFIS COMPUTER MONITOR MESSAGE AND HDG AND PIT BOXES DISPLAYED. F/O SIDE PRIMARY FLIGHT DISPLAY (PFD) FLICKERED WITH VERTICAL BARS. ATTITUDE INDICATOR CLIMBING, H
- [SDR VNAA2014032900021](https://openairdocs.org/sdr/VNAA2014032900021.md): Feeder Cable · damaged · Mar 29, 2014 · N215PS · Cndair CL6002B19 · Light System Wiring
  > CREW REPORTED FLOOR EMERGENCY LIGHTS WOULD NOT ILLUMINATE PAST ROW 8. MAINTENANCE INSPECTED, R & R EMERGENCY LIGHT CABLE ASSEMBLY IN FRONT OF LAVATORY AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.
- [SDR VNAA2014032300019](https://openairdocs.org/sdr/VNAA2014032300019.md): Cargo Track · corroded · Mar 23, 2014 · N215PS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > DURING SCHEDULED MAINTENANCE, AT THE CARGO COMPARTMENT FLOOR TRACKS AND TIE DOWNS CORROSION WAS FOUND. THE AREA WAS INSPECTED AND TRACKS AND TIEDOWNS REPLACED USING AMM. AIRCRAFT WAS RELEASED FOR SERVICE
- [SDR VNAA2014032300018](https://openairdocs.org/sdr/VNAA2014032300018.md): Sill · corroded · Mar 23, 2014 · N215PS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > DURING SCHEDULED MAINTENANCE, AT THE CARGO DOOR LOWER SILL CORROSION WAS FOUND AROUND FASTENER HOLES. THE AREA WAS INSPECTED AND CARGO DOOR SILL WAS REPLACED USING AMM. AIRCRAFT WAS RELEASED FOR SERVICE.
- [SDR VNAA20130323](https://openairdocs.org/sdr/VNAA20130323.md): Sill · corroded · Mar 23, 2014 · N215PS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > DURING SCHEDULED MAINTENANCE, AT THE CARGO DOOR LOWER SILL CORROSION WAS FOUND AROUND FASTENER HOLES. THE AREA WAS INSPECTED AND CARGO DOOR SILL WAS REPLACED USING AMM. AIRCRAFT WAS RELEASED FOR SERVICE.
- [SDR VNAA2014032300017](https://openairdocs.org/sdr/VNAA2014032300017.md): Skin · cracked · Mar 23, 2014 · N215PS · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > DURING SCHEDULED MAINTENANCE, SKIN AT FS 235 WAS FOUND CRACKED. THE AREA WAS INSPECTED AND REPAIRED USING AMM. AIRCRAFT WAS RELEASED FOR SERVICE.
- [SDR VNAA2014032300016](https://openairdocs.org/sdr/VNAA2014032300016.md): Skin · damaged · Mar 23, 2014 · N215PS · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > DURING SCHEDULED MAINTENANCE, AREA AFT OF NOSE LANDING GEAR DAMAGED, CAUSED BY LIGHTNING STRIKE. THE AREA WAS INSPECTED AND REPAIRED USING AMM. A PERMANENT REPAIR WAS MADE. AIRCRAFT WAS RELEASED FOR SERVICE.
- [SDR VNAA2014032300015](https://openairdocs.org/sdr/VNAA2014032300015.md): Skin · cracked · Mar 23, 2014 · N215PS · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > DURING SCHEDULED MAINTENANCE, THE RT FORWARD CABIN WINDOW SKIN CRACKED. THE AREA WAS INSPECTED AND REPAIRED USING AMM. AIRCRAFT WAS RELEASED FOR SERVICE.
- [SDR VNAA2014010500003](https://openairdocs.org/sdr/VNAA2014010500003.md): Controller · failed · Jan 3, 2014 · N215PS · Cndair CL6002B19 · Windshield/Door Rain/Ice Removal
  > CREW REPORTED CAPTAIN’S WINDSHIELD CRACKED AT FL29. DESCENDED, DECLARED AN EMERGENCY AND LANDED AT NEAREST SUITABLE AIRPORT WITHOUT INCIDENT. MAINTENANCE INSPECTED, R & R LT WINDSHIELD, R & R LT WINDSHIELD TEMPERATURE CONTROLLER AND PERFORMED CHECKS IAW AM
- [SDR VNAA2013090800004](https://openairdocs.org/sdr/VNAA2013090800004.md): Relay · failed · Sep 8, 2013 · N215PS · Cndair CL6002B19 · Passenger Compartment Lighting
  > CREW REPORTED ODOR OF BURNING RUBBER NEAR EXIT ROW. LIGHTS OUT ABOVE BINS ON ROW 8 D/F. MX INSPECTED, R & R POWER RELAY AT ROW 8 D/F AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.
- [SDR VNAA2013053100018](https://openairdocs.org/sdr/VNAA2013053100018.md): Fuel Control · failed · May 31, 2013 · N215PS · Cndair CL6002B19 · Fuel Control/Turbine Engines
  > CREW REPORTED RIGHT ENGINE OVERSPEED MASTER WARNING MESSAGE BELOW 80 KNOTS ON TAKEOFF. CREW REJECTED TAKEOFF AND SAFELY RETURNED TO GATE. MAINTENANCE INSPECTED, PERFORMED POWER ASSURANCE RUN AND FOUND RIGHT ENGINE EXCEEDED MAXIMUM PERMITTED N2. MAINTENANCE
- [SDR VNAA2013031100008](https://openairdocs.org/sdr/VNAA2013031100008.md): Controller · failed · Mar 11, 2013 · N215PS · Cndair CL6002B19 · Pitot/Static Anti-Ice System
  > CREW REPORTED RIGHT AOA HEAT, RIGHT PITOT HEAT, RIGHT TAT PROBE HEAT AND RIGHT STATIC HEAT CAS MESSAGES AFTER TAKEOFF. CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, REMOVED AND REPLACED NUMBER TWO (2) AIR DATA SENSOR HEAT CONTRO
- [SDR VNAA2013030600007](https://openairdocs.org/sdr/VNAA2013030600007.md): Engine · malfunctioned · Mar 6, 2013 · N215PS · Cndair CL6002B19 · Engine (Turbine/Turboprop)
  > CREW REPORTED LEFT ENGINE OIL PRESSURE CLIMBED TO APPROXIMATELY 133 PSI ON TAKEOFF ROLL. CREW REJECTED TAKEOFF AND RETURNED TO GATE. MAINTENANCE INSPECTED, REMOVED AND REPLACED LEFT ENGINE AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT RE
- [SDR VNAA2012093000024](https://openairdocs.org/sdr/VNAA2012093000024.md): Bulkhead · cracked · Sep 30, 2012 · N215PS · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > DURING SCHEDULED MAINTENANCE FOUND A CRACK AT THE FS 621 BULKHEAD WEB. THE FS 621 BULKHEAD WEB WAS INSPECTED AND REPAIRED USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.
- [SDR VNAA2012093000023](https://openairdocs.org/sdr/VNAA2012093000023.md): Bulkhead · cracked · Sep 30, 2012 · N215PS · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > DURING SCHEDULED MAINTENANCE A CRACK AT FS 202.0 BULKHEAD WAS FOUND. THE FS 202.0 BULKHEAD WAS INSPECTED AND REPAIRED USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.
- [SDR VNAA2012081200005](https://openairdocs.org/sdr/VNAA2012081200005.md): Control Unit · failed · Aug 12, 2012 · N215PS · Cndair CL6002B19 · Landing Gear Steering System
  > CREW REPORTED, STEERING INOP MESSAGE ON GEAR EXTENSION. CREW RESET NOSEWHEEL STEERING IN ACCORDANCE WITH QRH AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE TROUBLESHOT NOSEWHEEL STEERING SYSTEM, REMOVED AND REPLACED NWS (NOSEWHEEL STEERING) ECU (ELECTRONIC
- [SDR VNAA2011110200031](https://openairdocs.org/sdr/VNAA2011110200031.md): Skin · dented · Oct 30, 2011 · N215PS · Cndair CL6002B19 · Wing, Plate/Skin
  > CREW REPORTED BIRD STRIKE ON RIGHT WING LEADING EDGE ON APPROACH TO PHL. AIRCRAFT LANDED IN PHL WITHOUT FURTHER INCIDENT. MAINTENANCE COMPLIED WITH BIRD STRIKE INSPECTION, APPLIED AERODYNAMIC FILLER TO DENT ON RIGHT WING MIDDLE LEADING EDGE AND PERFORMED CHE
- [SDR VNAA2011100600007](https://openairdocs.org/sdr/VNAA2011100600007.md): Skin · damaged · Oct 2, 2011 · N215PS · Cndair CL6002B19 · Wing, Plate/Skin
  > AT GSP, CREW REPORTED BIRD STRIKE ON LEADING EDGE OF LEFT WING. MAINTENANCE INSPECTED AIRCRAFT, REPAIRED DENT ON LEFT WING INBOARD LEADING EDGE (L/E ZONE 1) AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT RELEASED FOR SERVICE.
- [SDR VNAA2011060300023](https://openairdocs.org/sdr/VNAA2011060300023.md): Acm · seized · May 28, 2011 · N215PS · Cndair CL6002B19 · Cabin Cooling System
  > CREW REPORTED STRONG ELECTRICAL SMOKE SMELL IN CABIN AT PHL. GROUND PERSONNEL WITNESSED WHITE SMOKE IN VICINITY OF PACK EXHAUST VENTS. MAINTENANCE INSPECTED, REMOVED AND REPLACED RIGHT PACK ACM AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUALS. AIRCRA
- [SDR VNAA2011060300022](https://openairdocs.org/sdr/VNAA2011060300022.md): Bracket · damaged · May 27, 2011 · N215PS · Cndair CL6002B19 · Landing Gear Position and Warning
  > CREW REPORTED WOW INPUT MESSAGE WITH GEAR IN WELL, THEN STEERING INOP CAS MESSAGE, AFTER TAKEOFF FROM DAY. CREW RETURNED TO DAY AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, REMOVED AND REPLACED SENSOR BRACKET, RIGGED SENSOR AND PERFORMED CHECKS USIN
- [SDR VNAA2011060200020](https://openairdocs.org/sdr/VNAA2011060200020.md): Wire Harness · defective · May 27, 2011 · N215PS · Cndair CL6002B19 · Landing Gear System Wiring
  > CREW REPORTED WOW INPUT AND STEERING INOP AMBER CAS MESSAGES AFTER TAKEOFF FROM DAY. CREW RETURNED TO DAY AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, REMOVED AND REPLACED NR 1 PROXIMITY SENSOR HARNESS ASSEMBLY AND PERFORMED CHECKS USING AIRCRAFT MA
- [SDR VNAA2011021400006](https://openairdocs.org/sdr/VNAA2011021400006.md): Beam · damaged · Feb 14, 2011 · N215PS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > DURING SCHEDULED MAINTENANCE FS 280.0 J-CHANNEL, TRASVERSE BEAM, AND FLOOR SUPPORT CAPS WERE CRACKED AND CORRODED O/B OF RBL6 AND LBL9. REPAIRS WERE MADE USING AIRCRAFT MANUALS AND AIRCRAFT RELEASED FOR SERVICE.
- [SDR VNAA2011021400007](https://openairdocs.org/sdr/VNAA2011021400007.md): Channel · damaged · Feb 14, 2011 · N215PS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > DURING SCHEDULED MAINTENANCE FS 280.0 J-CHANNEL, TRANSVERSE BEAM, AND FLOOR SUPPORT CAPS WERE CRACKED AND CORRODED O/B OF RBL 6 AND LBL 9. REPAIRS WERE MADE USING AIRCRAFT MANUALS AND AIRCRAFT RELEASED FOR SERVICE.

Next page: https://openairdocs.org/deregistered/N215PS-2025-12-09/reports.md?page=2

## 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 = 'N215PS' AND deregistration_id = 'N215PS-2025-12-09'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N215PS-2025-12-09/reports

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