# Service difficulty reports: N220PS, cancelled Dec 8, 2025

A list on [N220PS, cancelled Dec 8, 2025](https://openairdocs.org/deregistered/N220PS-2025-12-08.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 · 70 reports

- [SDR VNAA2019110111101](https://openairdocs.org/sdr/VNAA2019110111101.md): Battery · discharged · Nov 1, 2019 · N220PS · Cndair CL6002B19 · Emergency Equipment
  > FA FLASHLIGHT INOP. MX R&R FA FLASHLIGHT BATTERY IAW CRJ200 VCMM 25-60-07. OPS CHECK GOOD
- [SDR VNAA2019080611101](https://openairdocs.org/sdr/VNAA2019080611101.md): Inverter · failed · Aug 6, 2019 · N220PS · Cndair CL6002B19 · Emergency Lighting
  > LH OVERWING EMERGENCY EXIT LIGHT WILL NOT TEST. R/R #2 EMERGENCY LIGHT INVERTER, IAW CRJ200 AMM 33-51-07-000/400-801. OPS CHECK GOOD
- [SDR VNAA2019040411102](https://openairdocs.org/sdr/VNAA2019040411102.md): Sign · inoperative · Apr 4, 2019 · N220PS · Cndair CL6002B19 · Emergency Lighting
  > L/H EMERGENCY EXIT FLOOR LEVEL EMERGENCY LIGHT WILL NOT ILLUMINATE. REMOVED AND REPLACED LIGHTED FLOOR-LEVEL EXIT SIGN OPS CHECK GOOD AT THIS TIME
- [SDR VNAA2019032911101](https://openairdocs.org/sdr/VNAA2019032911101.md): Light · inoperative · Mar 29, 2019 · N220PS · Cndair CL6002B19 · Emergency Lighting
  > SUPPLEMENTAL INFORMATION:RH AFT EXTERIOR EMERGENCY LIGHT WILL NOT ILLUMINATE. R&R R/H AFT EXTERIOR EMERGENCY LIGHT IAW CRJ200 AMM 33-51-21-000/400-801. OPS CHECK GOOD AT THIS TIME.
- [SDR VNAA2018032099911](https://openairdocs.org/sdr/VNAA2018032099911.md): Seat Track · corroded · Mar 20, 2018 · N220PS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > SIDE SEAT RAIL SECTION FROM FS 409.00 PLUS 112 TO FS 455.00 ON LT SIDE IS CORRODED. INSTALLED REPLACEMENT LT SIDE SEAT RAIL P/N 601R38312-119S BETWEEN FS 409.00+112 TO 455.00 IAW AMM 53-00-11-400-802.
- [SDR VNAA2018032099910](https://openairdocs.org/sdr/VNAA2018032099910.md): Seat Track · corroded · Mar 20, 2018 · N220PS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > SIDE SEAT RAIL SECTION FROM FS 409.00 PLUS 16 TO FS 409.00 PLUS 112 ON RT SIDE IS CORRODED. INSTALLED REPLACEMENT RT SIDE SEAR RAIL P/N 6DIR38312-29 BETWEEN FS 409 AND 16 TO 409 AND 112 IAW AMM 53-01-11-400-802.
- [SDR VNAA2018032099909](https://openairdocs.org/sdr/VNAA2018032099909.md): Seat Track · corroded · Mar 20, 2018 · N220PS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > FLOOR SEAT RAIL SECTION AT RBL 9.0 FROM FS 364 TO FS 396.00 IS CORRODED. INSTALLED NEW SERVICEABLE FLOOR SEAT RAIL IAW AMM 53-01-11-400-802, 53-01-11-000-802.
- [SDR VNAA2018032099908](https://openairdocs.org/sdr/VNAA2018032099908.md): Seat Track · corroded · Mar 20, 2018 · N220PS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > FLOOR SEAT RAIL SECTION AT LBL 9.0 FROM FS 364 TO FS 396.00 IS CORRODED. INSTALLED NEW SERVICEABLE SEAT RAIL IAW AMM 53-01-11-400-802, 53-01-11-000-802.
- [SDR VNAA2018032099907](https://openairdocs.org/sdr/VNAA2018032099907.md): Strap · corroded · Mar 20, 2018 · N220PS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > STRAP AT FS 349 STR 3L IS CORRODED. REMOVED CORROSION IAW EA 43-2018-042.
- [SDR VNAA2018032099906](https://openairdocs.org/sdr/VNAA2018032099906.md): Frame · cracked · Mar 20, 2018 · N220PS · Cndair CL6002B19 · Fuselage Main, Frame
  > CRACK AT FS 333 FRAME TOOLING HOLE BETWEEN STR 1L AND STR 0. LOCATED AND DRILLED SERVICEABLE FRAME PN 601R32004-41 IAW SRM 51-40-11. INSTALLED NEW FRAME AT FS 333 IAW SRM 51-42-06 AND 51-42-21. PN 601R32004-41.
- [SDR VNAA2018032099905](https://openairdocs.org/sdr/VNAA2018032099905.md): Bulkhead · cracked · Mar 20, 2018 · N220PS · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > CRACKS ON THE FS 621 AFT PRESSURE BULKHEAD AND ATTACHING STRUCTURE AT LBL27.5/WL131-133, LBL18/WL74-75.5 AND WL130.5-133.5, LBL9.5/WL75-77, BL0/WL127.5-132, RBL18/WL74-75.5 AND RBL27.5/WL109-110.5. REPAIRED DAMAGED AREAS ON 621 BULKHEAD AND ATTACHING STRUCTURE
- [SDR VNAA2018032099904](https://openairdocs.org/sdr/VNAA2018032099904.md): Strap · corroded · Mar 20, 2018 · N220PS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RT SIDE FLOOR STRAP AT FS 559, LBL36 TO WALL IS CORRODED. REMOVED FLOOR STRAP AT FS 559 RBL 36 TO WALL IAW SRM 51-42-06-01. INSTALLED FLOOR STRAP AT FS 559 RBL 36 P/N 601R31025-29 IAW SRM 51-42-06.
- [SDR VNAA2018032099903](https://openairdocs.org/sdr/VNAA2018032099903.md): Skin · chafed · Mar 20, 2018 · N220PS · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > EXTERIOR SKIN JUST AFT OF APU EXHAUST CUTOUT HAS 3 AREAS OF DAMAGE THAT ARE MARKED WITH RED MARKER. RECEIVED ENGINEERING ORDERS AND REPAIRED DAMAGED AREA IAW EA 25-2018-058
- [SDR VNAA2018032099902](https://openairdocs.org/sdr/VNAA2018032099902.md): Frame · cracked · Mar 20, 2018 · N220PS · Cndair CL6002B19 · Fuselage Main, Frame
  > RT FS 718 FRAME IS CRACKED AT STR 11. LOCATED AND DRILLED LT FS 718 FRAME SECTOR IAW SRM 51-40-11.
- [SDR VNAA2018032099901](https://openairdocs.org/sdr/VNAA2018032099901.md): Frame · cracked · Mar 20, 2018 · N220PS · Cndair CL6002B19 · Fuselage Main, Frame
  > LT FS 718 FRAME IS CRACKED AT STR 11. LOCATED AND DRILLED LT FS 718 FRAME SECTOR IAW SRM 51-40-11.
- [SDR VNAA2017080711101](https://openairdocs.org/sdr/VNAA2017080711101.md): Transducer · faulted · Aug 7, 2017 · N220PS · Cndair CL6002B19 · Brake Anti-Skid Section
  > DURING TAKEOFF AT 90 KNOTS, THE CREW RECEIVED AN INBOARD ANTI-SKID CAUTION MESSAGE AND ABORTED TAKEOFF AND RETURNED TO THE GATE. MAINTENANCE REPLACED THE RIGHT HAND INBOARD WHEEL SPEED TRANSDUCER AND CANNON PLUG AND REPAIRED WIRING TO LEFT HAND INBOARD WHEEL S
- [SDR VNAA2017080511102](https://openairdocs.org/sdr/VNAA2017080511102.md): Warning Light · false activation · Aug 5, 2017 · N220PS · Cndair CL6002B19 · Extinguishing System
  > WHILE IN CRUISE THE CREW RECEIVED A CARGO FIRE BOTTLE LOW AMBER CAUTION MESSAGE. THE AIRCRAFT RETURNED TO FIELD. THE FIRE BOTTLE WAS FOUND TO BE WITHIN LIMITS AND THE AIRCRAFT RETURNED TO SERVICE.
- [SDR VNAA2016102300027](https://openairdocs.org/sdr/VNAA2016102300027.md): Battery Pack · inoperative · Oct 23, 2016 · N220PS · Cndair CL6002B19 · Emergency Lighting
  > MIDSHIP FORWARD EMERGENCY LIGHT INOPERATIVE. MAINTENANCE INSPECTED, REMOVED AND REPLACED THE NR TWO EMERGENCY LIGHT BATTERY AND PERFORMED CHECKS IAW THE AMM. THE AIRCRAFT WAS RELEASED FOR SERVICE.
- [SDR VNAA2016102300026](https://openairdocs.org/sdr/VNAA2016102300026.md): Skin · dented · Oct 23, 2016 · N220PS · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > DENT BETWEEN BS 295-310, STRINGERS 14-15L. MAINTENANCE PERFORMED A MAJOR REPAIR TO THE SKIN IAW AMM. THE AIRCRAFT WAS RELEASED FOR SERVICE.
- [SDR VNAA2016062900033](https://openairdocs.org/sdr/VNAA2016062900033.md): Sign · unsecure · Jun 29, 2016 · N220PS · Cndair CL6002B19 · Emergency Lighting
  > EMERGENCY EXIT SIGN FELL DOWN. MAINTENANCE INSPECTED, REINSTALLED COVER AND PERFORMED CHECKS IAW THE AMM. THE ACFT WAS RELEASED FOR SERVICE.
- [SDR VNAA2016052600027](https://openairdocs.org/sdr/VNAA2016052600027.md): Shutoff Valve · warning message · May 26, 2016 · N220PS · Cndair CL6002B19 · Landing Gear Brake System
  > PARKING BRAKE SHUTOFF VALVE MESSAGE AFTER RETRACTION COMMAND INBD ANTI-SKID MESSAGE. MAINTENANCE TROUBLESHOT, R & R PARKING BRAKE SHUTOFF VALVE AND PERFORMED CHECKS IAW THE AMM. THE ACFT WAS RELEASED FOR SERVICE.
- [SDR VNAA2016051700015](https://openairdocs.org/sdr/VNAA2016051700015.md): Terminal · damaged · May 17, 2016 · N220PS · Cndair CL6002B19 · Fire Protection System Wiring
  > LEFT JET OVERHEAT FAIL CAUTION MESSAGE IN FLIGHT. THE CREW DECLARED AN EMERGENCY, CONTINUED TO DESTINATION, AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, R & R THE RING TERMINAL OF INBD WIRE AT LOOP A AND PERFORMED CHECKS IAW THE AMM. THE ACFT WAS REL
- [SDR VNAA2016050900016](https://openairdocs.org/sdr/VNAA2016050900016.md): Mount · corroded · May 16, 2016 · N220PS · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > GALLEY AFT MOUNT PLATE ON RT FLOOR SILL CORRODED BETWEEN FS 310-FS 319. REPLACED GALLEY AFT MOUNT PLATE, PN 601R38669-49 IAW SRM 51-40-11, 51-42-06.
- [SDR VNAA2016050900020](https://openairdocs.org/sdr/VNAA2016050900020.md): Cargo Track · corroded · May 9, 2016 · N220PS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > CARGO TRACK AT RBL 9 BETWEEN FS 559+91 - 569 CORRODED. REPLACED THE CARGO TRACK IAW AMM 53-01-11-000/400-802.
- [SDR VNAA2016050900019](https://openairdocs.org/sdr/VNAA2016050900019.md): Cargo Track · corroded · May 9, 2016 · N220PS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > CARGO TRACK AT LBL 9 BETWEEN FS 559+91 - 600 CORRODED. REPLACED THE CARGO TRACK IAW AMM 53-01-11-000/400-802.601R38779-5.
- [SDR VNAA2016050900018](https://openairdocs.org/sdr/VNAA2016050900018.md): Cargo Track · corroded · May 9, 2016 · N220PS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > CARGO TRACK AT LBL 27, BETWEEN FS 559+80 - 567 CORRODED. REPLACED SEAT TRACKS IAW AMM 53-01-11-000/400-802.
- [SDR VNAA2016050900017](https://openairdocs.org/sdr/VNAA2016050900017.md): Cargo Track · corroded · May 9, 2016 · N220PS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > CARGO TRACK AT 27 BETWEEN FS 559+80- 559+96 IS CORRODED. REPLACED SEAT TRACK IAW AMM 53-01-11-000/400-802,
- [SDR VNAA2015051000012](https://openairdocs.org/sdr/VNAA2015051000012.md): Bulkhead Web · cracked · May 10, 2015 · N220PS · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > DURING EDDY CURRENT INSPECTION OF REAR PRESSURE BULKHEAD, FWD CRACK AT BL 0, WL 110.09 OF Z-MEMBER HEEL LINE. C/W REPAIRED IAW REO 601R-53-61-1285D.
- [SDR VNAA2014071800016](https://openairdocs.org/sdr/VNAA2014071800016.md): Skin · dented · Jul 18, 2014 · N220PS · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > DURING SCHEDULED MAINTENANCE, FOUND FUSELAGE SKIN AT BS 635 DENTED. REPAIRED IAW AMM. ACFT WAS RELEASED FOR SERVICE.
- [SDR VNAA2014071800015](https://openairdocs.org/sdr/VNAA2014071800015.md): Stiffener · cracked · Jul 18, 2014 · N220PS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > DURING SCHEDULED MAINTENANCE, BS 409.00 + 128 VERTICAL POST AT AFT FLANGE RADIUS FOUND CRACKED. THE AREA WAS INSPECTED AND REPAIRED USING AMM. ACFT WAS RELEASED FOR SERVICE.
- [SDR VNAA2014040600005](https://openairdocs.org/sdr/VNAA2014040600005.md): Unknown · unknown · Apr 6, 2014 · N220PS · Cndair CL6002B19 · Standard Practices/Structures
  > CREW REPORTED ABNORMAL BUMP, NOISE, & VIBRATION AFTER TAKEOFF. DECLARED AN EMERGENCY, LANDED SAFELY AT DESTINATION AIRPORT AND REPORTED LANDING NORMAL. MAINTENANCE PERFORMED GENERAL VISUAL INSPECTION OF FLAPS, SPOILERS, LANDING GEAR AND COMPONENTS, WHEELS, TI
- [SDR VNAA2014021200011](https://openairdocs.org/sdr/VNAA2014021200011.md): Pump · leaking · Feb 12, 2014 · N220PS · Cndair CL6002B19 · Hydraulic Pump (Electric/Engine), Main
  > CREW REPORTED HYD SYSTEM NR 1 PRESSURE LOW AND QUANTITY READING ZERO DURING FLIGHT. DIVERTED AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND FOUND LEAK ON HYD EDP NR 1 AND HYD NR 1 PRESSURE MANIFOLD LINE. R & R NR 1 EDP, R & R NR 1 HYDRAULIC PRESSURE M
- [SDR VNAA2013121200006](https://openairdocs.org/sdr/VNAA2013121200006.md): Light · inoperative · Dec 12, 2013 · N220PS · Cndair CL6002B19 · Emergency Lighting
  > CREW REPORTED AN APPROXIMATE 6 INCH SECTION OF FLOOR LEVEL EMERGENCY LIGHTS NOT WORKING. MAINTENANCE INSPECTED, R & R FORWARD SECTION OF EMERGENCY FLOOR LIGHT STRIP AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.
- [SDR VNAA2013093000012](https://openairdocs.org/sdr/VNAA2013093000012.md): Connector · disconnected · Sep 30, 2013 · N220PS · Cndair CL6002B19 · Light System Wiring
  > CREW REPORTED FLOOR EMERGENCY LIGHTS INOPERATIVE ROW 9 AND BACK. MX INSPECTED, ATTACHED CONNECTOR TO FLOOR LIGHT STRIP AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.
- [SDR VNAA2013022800019](https://openairdocs.org/sdr/VNAA2013022800019.md): Windshield · cracked · Feb 28, 2013 · N220PS · Cndair CL6002B19 · Flight Compartment Windows
  > CREW REPORTED THE CAPTAINS WINDSHIELD CRACKED DURING CRUISE. CREW DIVERTED AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, REMOVED, REPLACED, AND OPERATIONAL CHECKED THE CAPTAINS WINDSHIELD USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED FO
- [SDR VNAA2013022300013](https://openairdocs.org/sdr/VNAA2013022300013.md): Rvdt · failed · Feb 23, 2013 · N220PS · Cndair CL6002B19 · Landing Gear Steering System
  > CREW REPORTED AIRCRAFT PULLED TO RIGHT SIDE DURING TAKEOFF ROLL. CREW ABORTED TAKEOFF AND RETURNED TO GATE. MAINTENANCE TROUBLESHOT, REMOVED AND REPLACED RIGHT STEERING FEEDBACK RVDT (ROTARY VARIABLE DIFFERENTIAL TRANSFORMER), AND PERFORMED CHECKS USING AIRC
- [SDR VNAA2012120800007](https://openairdocs.org/sdr/VNAA2012120800007.md): Light · inoperative · Dec 8, 2012 · N220PS · Cndair CL6002B19 · Emergency Lighting
  > CREW REPORTED CABIN IN-FLOOR EMERGENCY LIGHTS INOPERATIVE AND NOT SECURE AT ROWS 1-3. MAINTENANCE INSPECTED, REMOVED AND REPLACED FORWARD EMERGENCY FLOOR LIGHT STRIP AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT RELEASED FOR SERVICE.
- [SDR VNAA2011120600001](https://openairdocs.org/sdr/VNAA2011120600001.md): Skin · damaged · Dec 1, 2011 · N220PS · Cndair CL6002B19 · Wing, Plate/Skin
  > AT TYS, CREW REPORTED BIRD STRIKE TO RIGHT WING, ABOUT HALFWAY ON LEADING EDGE. MAINTENANCE PERFORMED BIRD STRIKE INSPECTION, FOUND DAMAGE ON RIGHT WING MIDDLE LEADING EDGE TO BE WITHIN ALLOWABLE LIMITS PER SRM, FILLED DAMAGE AND PERFORMED CHECKS USING AIRCRA
- [SDR VNAA2011062600027](https://openairdocs.org/sdr/VNAA2011062600027.md): Bulkhead · cracked · Jun 25, 2011 · N220PS · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > DURING SCHEDULED MAINTENANCE IT WAS FOUND THE FS 202.0 BULKHEAD HAD A CRACK ADJACENT TO THE HOLE WHERE PARKING BRAKE CABLE PASSES THROUGH. THE AREA WAS INSPECTED AND REPAIRED USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.
- [SDR VNAA2011062600026](https://openairdocs.org/sdr/VNAA2011062600026.md): Bulkhead · cracked · Jun 25, 2011 · N220PS · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > DURING SCHEDULED MAINTENANCE THE FS 559.0 RIGHT BULKHEAD WEB WAS FOUND CRACKED. THE FS 559.0 BULKHEAD WEB WAS INSPECTED AND REPAIRED USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.
- [SDR VNAA2011062600023](https://openairdocs.org/sdr/VNAA2011062600023.md): Floorbeam · cracked · Jun 25, 2011 · N220PS · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > DURING SCHEDULED MAINTENANCE THE FS 280.0 FLOOR TRAVERSE BEAM WAS FOUND CRACKED. THE FS 280.0 FLOOR TRAVERSE BEAM WAS INSPECTED AND REPAIRED USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.
- [SDR VNAA2011051100003](https://openairdocs.org/sdr/VNAA2011051100003.md): Duct · damaged · May 6, 2011 · N220PS · Cndair CL6002B19 · Air Intake Anti/De-Ice System
  > CREW REPORTED 14TH STAGE DUCT RED MESSAGE AFTER TAKEOFF FROM CLT. CREW RETURNED TO CLT AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AIRCRAFT, REMOVED AND REPLACED DAMAGED RIGHT 14TH STAGE PYLON ANTI-ICE DUCTING AND HEAT SENSING ELEMENT AND PERFORMED CH
- [SDR VNAA2011040500001](https://openairdocs.org/sdr/VNAA2011040500001.md): Radome · damaged · Apr 2, 2011 · N220PS · Cndair CL6002B19 · Aerodynamic Fairings
  > CREW REPORTED LIGHTNING STRIKE ON RT SIDE OF THE NOSE AREA. MAINTENANCE INSPECTED AND REPAIRED DAMAGE. THE RADOME WAS ALSO REMOVED AND REPLACED. ALL WORK WAS ACCOMPLISHED USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.
- [SDR VNAA2010090100013](https://openairdocs.org/sdr/VNAA2010090100013.md): Windshield · cracked · Aug 28, 2010 · N220PS · Cndair CL6002B19 · Flight Compartment Windows
  > CREW REPORTED THE FIRST OFFICER WINDSHIELD CRACKED IN FLIGHT. CREW DIVERTED TO CLT AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE FIRST OFFICER WINDSHIELD USING AIRCRAFT MAINTENANCE MANUALS. CHECKS WERE MADE USING AIRCRAFT MAINTENANCE M
- [SDR VNAA2010022200008](https://openairdocs.org/sdr/VNAA2010022200008.md): Window · cracked · Feb 19, 2010 · N220PS · Cndair CL6002B19 · Flight Compartment Windows
  > CREW REPORTED THE FIRST OFFICER WINDOW CRACKING. AIRCRAFT DIVERTED TO DAY WHERE MAINTENANCE USING THE AIRCRAFT MANUAL TROUBLESHOT AND REMOVED AND REPLACED THE FIRST OFFICER WINDOW. CHECKS WERE MADE USING THE AIRCRAFT MAINTENANCE MANUALS AND AIRCRAFT WAS RELE
- [SDR VNAA2009100700001](https://openairdocs.org/sdr/VNAA2009100700001.md): Carbon Seal · unknown · Oct 2, 2009 · N220PS · Cndair CL6002B19 · Turbine Engine Oil System
  > CREW REPORTED AT 35,000 A LOW OIL PRESSURE MESSAGE. AIRCRAFT RETURNED TO CLT LANDING WITHOUT INCIDENT. MAINTENANCE INSPECTED AIRCRAFT USING AIRCRAFT MAINTENANCE MANUAL, REMOVED AND REPLACED CARBON SEALS ON ACCESSORY GEARBOX. CHECKS WERE MADE PER THE AIRCRAF
- [SDR VNAA2009090200011](https://openairdocs.org/sdr/VNAA2009090200011.md): Carbon Seal · leaking · Aug 30, 2009 · N220PS · Cndair CL6002B19 · Turbine Engine Oil System
  > CREW REPORTED A LOW OIL PRESS IN FLIGHT. ENGINE WAS SHUTDOWN. AIRCRAFT DIVERTED TO RIC LANDING WITHOUT INCIDENT. MAINTENANCE TROUBLESHOOT PER THE OEM MAINTENANCE MANUAL AND REMOVED AND REPLACED THE IDG ATS & HYD PUMP AGB CARBON SEAL ASSEMBLY. OPERATIONAL
- [SDR VNAA2009030500004](https://openairdocs.org/sdr/VNAA2009030500004.md): Unknown · malfunctioned · Mar 2, 2009 · N220PS · Cndair CL6002B19 · Air Conditioning System
  > CREW REPORTED AFTER TAKEOFF, TRIED TO TRANSFER RIGHT ENG BLEED CONTROL & WERE UNABLE TO GET THE RIGHT PACK TO FUNCTION OFF THE RIGHT ENG BLEED. CREW ELECTED TO RETURN TO DAY BECAUSE OF RESTRICTION OF 10,000 FT (LT PACK DEFERRED). MAINTENANCE INSPECTED ALL DU
- [SDR VNA2008F00008](https://openairdocs.org/sdr/VNA2008F00008.md): Transmitter · failed · Oct 7, 2008 · N220PS · Cndair CL6002B19 · Trailing Flap Position Indicating System
  > CREW REPORTED IN DESCENT AT 290 KTS W/ AUTOPILOT ON, UCA AND FLAP INDICATORS DEPLOYED ON EICAS PAGE. FLAP INDICATOR SHOWED GREEN BAR MOVEMENT AND READOUT MOVED TO 2 DEG. ACFT HAD PITCH OSCILLATIONS OF APPROX 3 DEG NOSE UP AND DOWN. MAINT REMOVED AND REPLACE
- [SDR VNAA2008100900002](https://openairdocs.org/sdr/VNAA2008100900002.md): Transmitter · failed · Oct 7, 2008 · N220PS · Cndair CL6002B19 · Trailing Flap Position Indicating System
  > CREW REPORTED IN DESCENT AT 290KTS W/AUTOPILOT ON, UCA AND FLAP INDICATORS DEPLOYED ON EICAS PAGE. FLAP INDICATOR SHOWED GREEN BAR MOVEMENT AND READOUT MOVED TO 2 DEG. AIRCRAFT HAD PITCH OSCILLATIONS OF APPROX 3 DEG NOSE UP AND DOWN. MAINTENANCE REMOVED AND

Next page: https://openairdocs.org/deregistered/N220PS-2025-12-08/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 = 'N220PS' AND deregistration_id = 'N220PS-2025-12-08'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N220PS-2025-12-08/reports

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