# Service difficulty reports: N213PS, cancelled Dec 9, 2025

A list on [N213PS, cancelled Dec 9, 2025](https://openairdocs.org/deregistered/N213PS-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 · 81 reports

- [SDR VNAA2020022061102](https://openairdocs.org/sdr/VNAA2020022061102.md): Centering Unit · out of limits · Feb 16, 2020 · N213PS · Cndair CL6002B19 · Landing Gear Steering System
  > EMERGENCY DECLARED GOING INTO CLT DUE TO A NOSEWHEEL STEERING AND WOW CAUTION MESSAGE ON TAKEOFF OUT OF DCA. DECIDED TO DIVERT TO CLT DUE TO THE CAPABILITIES OF A GEAR SWING AND PAX COVERAGE. FLIGHT LANDED IN CLT AND TRUCKS WERE ROLLED AND AFTER A RESET THE CA
- [SDR VNAA2020020611102](https://openairdocs.org/sdr/VNAA2020020611102.md): Warning Message · false activation · Feb 6, 2020 · N213PS · Cndair CL6002B19 · Brake Anti-Skid Section
  > A/SKID INBD CAUTION MESSAGE ON TAKEOFF ROLL.SYSTEM RESET DID NOT CLEAR MESSAGE. PERFORMED ANTISKID-CONTROL UNIT SYSTEM BITE TEST IAW CRJ 200 AMM. OPS CHECK GOOD.
- [SDR VNAA2019111399904](https://openairdocs.org/sdr/VNAA2019111399904.md): Bracket · separated · Nov 13, 2019 · N213PS · Bombdr CL6002D15 · Passenger/Crew Doors
  > WHILE PERFORMING T.O. 52-579-001-18 FOUND PAX DOOR PULLEY HINGE BRACKET AND INNER SKIN IS SEPARATED WHILE OPENING AND CLOSING. REMOVED PULLEY BRACKET IAW CRJ 200 SRM 51-42-22. INSTALLED PULLEY BRACKET IAW CRJ 200 SRM 51-42-22. COMPLIED WITH BOMBARDIER REO 60
- [SDR VNAA2019111399902](https://openairdocs.org/sdr/VNAA2019111399902.md): Seat Track · corroded · Nov 13, 2019 · N213PS · Bombdr CL6002D15 · Fuselage, Seat/Cargo Attach Fittings
  > RH CABIN AFT CABIN SIDE SEAT TRACK IS CORRODED FROM FS554 TO FS559.00+77 AS MARKED. REMOVED DADO PANEL 272ELW FOR ACCESS IAW CRJ200 AMM 25-26-02-000-802. INSTALLED DADO PANEL 272ELW PER CRJ200 AMM 25-26-02-400-801. OK TO CLOSE. REMOVED SIDEWALL PANELS 272BLW
- [SDR VNAA2019111399901](https://openairdocs.org/sdr/VNAA2019111399901.md): Support Frame · cracked · Nov 13, 2019 · N213PS · Bombdr CL6002D15 · Fuselage Main, Structure
  > LH LOWER WINDSHIELD SUPPORT FRAME IS CRACKED. REMOVED L/H LOWER WINDSHIELD SUPPORT FRAME IAW CRJ200 SRM 51-42-06. LOCATED AND DRILLED L/H LOWER WINDSHIELD SUPPORT FRAME IAW CRJ200 SRM 51-40-11 TR 51-42. L/H LOWER WINDSHIELD SUPPORT FRAME REQUIRES INSTALLATION.
- [SDR VNAA2019111399903](https://openairdocs.org/sdr/VNAA2019111399903.md): Rib · cracked · Oct 30, 2019 · N213PS · Bombdr CL6002D15 · Horizontal Stabilizer, Spar/Rib
  > LH END RIB ON HORZ STAB CRACKED AT BL 6:00. REMOVED LH END RIB ON HORIZONTAL STAB AT BL 6.00 IAW CRJ 200 SRM 55-11-12. INSTALLED LH END RIB ON H STAB AT BL6 IAW CRJ 200 SRM 51-42-06. CW BOMBARDIER 2EO#601R-55-12-670 REV--P2 DATED 2019-10-28. FINAL REO REQUIR
- [SDR VNAA2019090311103](https://openairdocs.org/sdr/VNAA2019090311103.md): Light · inoperative · Sep 3, 2019 · N213PS · Cndair CL6002B19 · Emergency Lighting
  > EMERGENCY FLOOD LIGHT IN FRONT OF LAV INOP. REMOVED/REPLACED EMERGENCY FLOOD LIGHT NUMBER 4, IAW AMM 33-51-16-000/400-801. OP-CHECKS GOOD.
- [SDR VNAA2019052811103](https://openairdocs.org/sdr/VNAA2019052811103.md): Battery Pack · discharged · May 28, 2019 · N213PS · Cndair CL6002B19 · Emergency Lighting
  > REMOVED AND REPLACED ALL FOUR EMERGENCY LIGHT BATTERY PACKS IAW CRJ200 AMM 33-51-04-000/400-801. OPS CHECK GOOD AT THIS TIME IAW CRJ200 AMM 33-51-04-740-801. S/N 122912, 76332, 65160, 459376
- [SDR VNAA2018083051101](https://openairdocs.org/sdr/VNAA2018083051101.md): Display · multiple fail · Aug 15, 2018 · N213PS · Cndair CL6002B19 · Navigation System
  > AFTER TAKE OFF, CLIMBING THRU 4000 FT, BOTH FLT DIRECTORS FAILED AND THEN THE FIRST OFFICER'S PFD FAILED. DECLARED EMERGENCY AND RETURNED TO FIELD, LANDED WITHOUT INCIDENT
- [SDR VNAA2017112199913](https://openairdocs.org/sdr/VNAA2017112199913.md): Rib · cracked · Nov 17, 2017 · N213PS · Cndair CL6002B19 · Wing, Rib/Bulkhead
  > LEFT BAT RIB AT WS 48.30 IS CRACKED. PERFORMED PERMANENT REPAIR OF LEFT BATT, RIB IAW REO 601R-57-51-046 REVISION B
- [SDR VNAA2017112199911](https://openairdocs.org/sdr/VNAA2017112199911.md): Trunnion · cracked · Nov 17, 2017 · N213PS · Cndair CL6002B19 · Wing, Landing Gear Attach Fittings
  > A CRACK INDICATION NOTED ON THE LEFT LOWER WING PLANK TRUNNION WHILE PERFORMING SB 601R-57-046. REPLACED THE TRUNNION.
- [SDR VNAA2017112199910](https://openairdocs.org/sdr/VNAA2017112199910.md): Trunnion · cracked · Nov 17, 2017 · N213PS · Cndair CL6002B19 · Wing, Landing Gear Attach Fittings
  > A CRACK INDICATION NOTED AT LEFT LOWER WING PLANK TRUNNION WHILE PERFORMING SB 601R-57-046. REPLACED THE LEFT MLG TRUNNION.
- [SDR VNAA201711219991](https://openairdocs.org/sdr/VNAA201711219991.md): Support Strap · corroded · Nov 17, 2017 · N213PS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FOUND CORROSION ON PRESSURE FLOOR SUPPORT BS 559. INSTALLED PRESSURE FLOOR SUPPORT STRAP IAW SRM 51-42-06, AND SRM 51-42-15.
- [SDR VNAA2017112199909](https://openairdocs.org/sdr/VNAA2017112199909.md): Frame · cracked · Nov 17, 2017 · N213PS · Cndair CL6002B19 · Fuselage Main, Frame
  > FRAME BS 333 IS CRACKED BETWEEN STRINGERS 0 AND 1L. REPLACED THE FRAME.
- [SDR VNAA2017112199908](https://openairdocs.org/sdr/VNAA2017112199908.md): Web · cracked · Nov 17, 2017 · N213PS · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR AFT WEB HAS A CRACK INDICATION NOTED IN THE REPAIR AREA OF DRAG ANGLE. REPAIRED THE WEB IAW EO CL00-2B19-52-L05344.
- [SDR VNAA2017112199907](https://openairdocs.org/sdr/VNAA2017112199907.md): Rib · cracked · Nov 17, 2017 · N213PS · Cndair CL6002B19 · Elevator, Spar/Rib
  > ONE RIBLET WAS FOUND TO BE CRACKED ON RT ELEVATOR. REPLACED THE DAMAGED RIB IAW SRM 51-42-06
- [SDR VNAA2017112199906](https://openairdocs.org/sdr/VNAA2017112199906.md): Angle · cracked · Nov 17, 2017 · N213PS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LOWER ANGLE AT BS 621 IS CRACKED ON CARGO DOOR BEAM. REMOVED & REPLACED THE ANGLE.
- [SDR VNAA2017112199905](https://openairdocs.org/sdr/VNAA2017112199905.md): Support Fitting · cracked · Nov 17, 2017 · N213PS · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > SUPPORT FITTINGS FOR INTERCOSTALS ARE CRACKED AT BS 460, RBL 11 AND LBL 11. LOCATED, DRILLED, AND INSTALLED THE NEW SERVICEABLE SUPPORT FITTING IAW SRM 51-40-11.
- [SDR VNAA2017112199904](https://openairdocs.org/sdr/VNAA2017112199904.md): Bulkhead · cracked · Nov 17, 2017 · N213PS · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FOUND REAR PRESSURE BULKHEAD WEB HAS A CRACK INDICATION NOTED AT RBL 9.50, WL 132. APPROX 2 INCHES. REPAIRED THE BS 621 BULKHEAD IAW REO 601R-53-61-1285, REV.E
- [SDR VNAA2017112199903](https://openairdocs.org/sdr/VNAA2017112199903.md): Skin · torn · Nov 17, 2017 · N213PS · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > RIGHT AFT CORNER OF NLG CUT OUT IS CRACKED APPROX.250. REPAIRED THE SKIN AT BS 235 BETWEEN STRINGERS 26L AND 26R IAW REO 601R-53-11-048, REV D, AND REO 601R-53-11-3143, REV -.
- [SDR VNAA2017112199902](https://openairdocs.org/sdr/VNAA2017112199902.md): Skin · torn · Nov 17, 2017 · N213PS · Cndair CL6002B19 · Elevator, Plate/Skin
  > LEFT ELEVATOR FOUND, DOUBLER HAS A ONE INCH TEAR. REPAIRED IAW EO CL600-2B19-55-L05337, REV IR, STEPS 5 & 6. FABRICATED A REPAIR DOUBLER AND TAPERED SHIMS.
- [SDR VNAA2017112199901](https://openairdocs.org/sdr/VNAA2017112199901.md): Stringer · cracked · Nov 17, 2017 · N213PS · Cndair CL6002B19 · Fuselage Main, Longeron/Stringer
  > STRINGER 3L IS CRACKED AT BS 379. REMOVED & REPLACED THE STRINGER IAW SRM 51-42-06, SRM 51-42-21, AND SRM 53-00-03.
- [SDR VNAA2017021400024](https://openairdocs.org/sdr/VNAA2017021400024.md): Bpsu · faulty · Feb 14, 2017 · N213PS · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLAPS FAIL MESSAGE DURING DESCENT. REMOVED AND REPLACED RIGHT BPSU.
- [SDR VNAA2016100200001](https://openairdocs.org/sdr/VNAA2016100200001.md): Trim Switch · inoperative · Oct 2, 2016 · N213PS · Cndair CL6002B19 · Stabilizer Control System
  > CAPTAIN’S TRIM SWITCH INOPERATIVE. RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED CAPTAIN’S PITCH TRIM SWITCH AND PERFORMED CHECKS IAW AMM. THE AIRCRAFT WAS RELEASED FOR SERVICE.
- [SDR VNAA2016091700020](https://openairdocs.org/sdr/VNAA2016091700020.md): Fire Bottle · low pressure · Sep 17, 2016 · N213PS · Cndair CL6002B19 · Extinguishing System
  > AFT CARGO FIRE BOTTLE LOW CAUTION. THE CREW DIVERTED TO NEAREST FIELD AND LANDED WITHOUT INCIDENT. TECHNICIANS REMOVED AND REPLACED THE AFT CARGO FIRE BOTTLE IAW CRJ-200 AMM. OPS CHECK GOOD. AIRCRAFT RELEASED FOR SERVICE.
- [SDR VNAA2016091500017](https://openairdocs.org/sdr/VNAA2016091500017.md): Battery Pack · discharged · Sep 15, 2016 · N213PS · Cndair CL6002B19 · Emergency Lighting
  > EMERGENCY POWER SUPPLY BATTERY PACKS DEAD. MAINTENANCE INSPECTED, REMOVED AND REPLACED THE EMERGENCY POWER SUPPLY BATTERY PACKS AND PERFORMED CHECKS IAW THE AMM. THE AIRCRAFT WAS RELEASED FOR SERVICE.
- [SDR VNAA2016091500016](https://openairdocs.org/sdr/VNAA2016091500016.md): Battery Pack · discharged · Sep 15, 2016 · N213PS · Cndair CL6002B19 · Emergency Lighting
  > EMERGENCY POWER SUPPLY BATTERY PACKS DEAD. MAINTENANCE INSPECTED, R & R THE EMERGENCY POWER SUPPLY BATTERY PACKS AND PERFORMED CHECKS IAW THE AMM. THE ACFT WAS RELEASED FOR SERVICE.
- [SDR VNAA2016091500015](https://openairdocs.org/sdr/VNAA2016091500015.md): Battery Pack · discharged · Sep 15, 2016 · N213PS · Cndair CL6002B19 · Emergency Lighting
  > EMERGENCY POWER SUPPLY BATTERY PACKS DEAD. MAINTENANCE INSPECTED, R & R THE EMERGENCY POWER SUPPLY BATTERY PACKS AND PERFORMED CHECKS IAW THE AMM. THE ACFT WAS RELEASED FOR SERVICE.
- [SDR VNAA2016091500014](https://openairdocs.org/sdr/VNAA2016091500014.md): Battery · discharged · Sep 15, 2016 · N213PS · Cndair CL6002B19 · Emergency Lighting
  > EMERGENCY POWER SUPPLY BATTERIES DEAD. MAINTENANCE INSPECTED, R & R POWER SUPPLY BATTERIES AND PERFORMED CHECKS IAW THE AMM. THE ACFT WAS RELEASED FOR SERVICE.
- [SDR VNAA2016052900029](https://openairdocs.org/sdr/VNAA2016052900029.md): Terminal Block · broken · May 29, 2016 · N213PS · Cndair CL6002B19 · Fire Protection System Wiring
  > THE FLIGHT CREW RECEIVED A LT JET PIPE OVER HEAT CAUTION MESSAGE. THEY RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, REPAIRED BROKEN TERMINAL LUG ON LT ENGINE JET PIPE, LOOP A AND PERFORMED CHECKS IAW THE AMM. THE ACFT WAS RELEASED
- [SDR VNAA20162900029](https://openairdocs.org/sdr/VNAA20162900029.md): Connector · broken · May 29, 2016 · N213PS · Cndair CL6002B19 · Fire Protection System Wiring
  > THE FLIGHT CREW RECEIVED A LT JET PIPE OVER HEAT CAUTION MESSAGE, THEY RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, REPAIRED BROKEN TERMINAL LUG ON LT ENGINE JET PIPE LOOP A AND PERFORMED CHECKS IAW THE AMM. THE ACFT WAS RELEASED FO
- [SDR VNAA2016051600012](https://openairdocs.org/sdr/VNAA2016051600012.md): Light · disconnected · May 16, 2016 · N213PS · Cndair CL6002B19 · Light System Wiring
  > EMERGENCY FLOOR LIGHT AT ROW 1 INOPERATIVE. MAINTENANCE INSPECTED, RECONNECTED LIGHT AND PERFORMED CHECKS IAW THE AMM. THE ACFT WAS RELEASED FOR SERVICE.
- [SDR VNAA2016013000028](https://openairdocs.org/sdr/VNAA2016013000028.md): Windshield · delaminated · Jan 30, 2016 · N213PS · Cndair CL6002B19 · Flight Compartment Windows
  > CREW REPORTS THAT DURING CLIMBOUT, THE CREW NOTICED THE WINDSHIELD DELAMINATING ON THE CAPTAIN`S SIDE. THE CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND FOUND DELAMINATION WITHIN LIMITS. MAINTENANCE PERFORMED CHECKS IAW AMM.
- [SDR VNAA2016010500007](https://openairdocs.org/sdr/VNAA2016010500007.md): Clamp · loose · Jan 5, 2016 · N213PS · Cndair CL6002B19 · Air Intake Anti/De-Ice System
  > ON TAKEOFF AT ABOUT 2,000 FT, CREW RECEIVED LT 14 DUCT WARNING MESSAGE. CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND FOUND CLAMP AT LT ENGINE COWLING ANTI-ICE DUCT INSIDE PYLON LOOSE AND LEAKING. MAINTENANCE REINSTALLED CLAMP
- [SDR VNAA2015123000016](https://openairdocs.org/sdr/VNAA2015123000016.md): Door Sill · corroded · Dec 30, 2015 · N213PS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CARGO DOOR SILL PLATE HAS MINOR CORROSION AT MULTIPLE LOCATIONS AROUND NUTPLATE HOLES. REMOVED CORROSION FROM CARGO DOOR SILL PLATE IAW REO.
- [SDR VNAA2015031700021](https://openairdocs.org/sdr/VNAA2015031700021.md): Seal · leaking · Mar 17, 2015 · N213PS · Cndair CL6002B19 · Nose/Tail Landing Gear
  > CREW REPORTED GEAR DISAGREE ON TAKEOFF. NOSE WHEEL WOULD NOT RETRACT. CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED, FOUND NOSE STRUT SEALS LEAKING, R & R NLG LOWER BEARING SEALS AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SE
- [SDR VNAA2014100300003](https://openairdocs.org/sdr/VNAA2014100300003.md): Sensor · malfunctioned · Oct 3, 2014 · N213PS · Cndair CL6002B19 · APU Oil System
  > CREW REPORTED APU OIL TEMP CAS MESSAGE DURING FLIGHT. CREW DIVERTED AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED, R & R APU OIL TEMPERATURE SENSOR AND PERFORMED CHECKS PER AMM. AIRCRAFT RELEASED FOR SERVICE.
- [SDR VNAA2014100200001](https://openairdocs.org/sdr/VNAA2014100200001.md): Connector · dirty · Oct 2, 2014 · N213PS · Cndair CL6002B19 · APU System Wiring
  > CREW REPORTED APU OIL TEMP CAUTION MESSAGE IN FLIGHT. CREW DIVERTED AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED APU OIL LEVEL. NO SERVICING REQUIRED. MAINTENANCE REMOVED, INSPECTED, CLEANED AND REINSTALLED APU OIL TEMPERATURE BULB ELECTRICAL CONNECTOR
- [SDR VNAA2014063000026](https://openairdocs.org/sdr/VNAA2014063000026.md): Bulkhead Web · cracked · Jun 30, 2014 · N213PS · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > DURING SCHEDULED MAINTENANCE THE BS 280 LOWER BULKHEAD WEB WAS FOUND CRACKED. THE AREA WAS INSPECTED AND REPAIRED IAW AMM. ACFT WAS RELEASED FOR SERVICE.
- [SDR VNAA2014063000002](https://openairdocs.org/sdr/VNAA2014063000002.md): Bulkhead Web · cracked · Jun 30, 2014 · N213PS · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > DURING SCHEDULED MAINTENANCE THE BS 280 LOWER WEB WAS FOUND CRACKED. THE AREA WAS INSPECTED AND REPAIRED USING AMM. ACFT WAS RELEASED FOR SERVICE.
- [SDR VNAA2014063000025](https://openairdocs.org/sdr/VNAA2014063000025.md): Crossbeam · cracked · Jun 30, 2014 · N213PS · Cndair CL6002B19 · Fuselage Main, Structure
  > DURING SCHEDULED MAINTENANCE, THE BS 280 CROSSBEAM WAS FOUND CRACKED OTBD OF RBL 9. THE AREA WAS INSPECTED AND REPAIRED IAW AMM. ACFT WAS RELEASED FOR SERVICE.
- [SDR VNAA2014022300018](https://openairdocs.org/sdr/VNAA2014022300018.md): Connector · loose · Feb 23, 2014 · N213PS · Cndair CL6002B19 · Light System Wiring
  > CREW REPORTED EMERGENCY FLOOR TRACK LIGHTING ONLY HALF ILLUMINATED. MAINTENANCE INSPECTED, SECURED LOOSE AFT EMERGENCY FLOOR TRACK LIGHTING CONNECTOR AND PERFORMED CHECKS IAW AMM. AIRCRAFT RELEASED FOR SERVICE.
- [SDR VNAA2014021500012](https://openairdocs.org/sdr/VNAA2014021500012.md): Strut · discharged · Feb 15, 2014 · N213PS · Cndair CL6002B19 · Nose/Tail Landing Gear Strut/Axle
  > CREW REPORTED NOSE GEAR DISAGREE AFTER TAKEOFF. NOSE GEAR WOULD NOT RETRACT. RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE SERVICED NLG AND PERFORMED FUNCTIONAL TEST OF LANDING GEAR EXTENSION AND RETRACTION SYSTEM. FUNCTIONAL CHECKED GOOD. AI
- [SDR VNAA2013122600019](https://openairdocs.org/sdr/VNAA2013122600019.md): Control Panel · odor · Dec 26, 2013 · N213PS · Cndair CL6002B19 · Air Distribution System
  > CREW REPORTED A BURNING ODOR IN THE GALLEY. MAINTENANCE TROUBLESHOT, R & R GALLEY CONTOL PANEL USING AMM. AIRCRAFT WAS RELEASED FOR SERVICE.
- [SDR VNAA2013082300014](https://openairdocs.org/sdr/VNAA2013082300014.md): Static Wick · damaged · Aug 23, 2013 · N213PS · Cndair CL6002B19 · Pitot/Static Anti-Ice System
  > CREW REPORTED A LIGHTNING STRIKE TO ACFT. MX TROUBLESHOT, R & R STATIC WICKS AND REPAIRED DAMAGE IAW ACFT MM. CHECKS WERE PERFOMED IAW THE AMM AND ACFT WAS RELEASED FOR SERVICE.
- [SDR VNAA2013010500002](https://openairdocs.org/sdr/VNAA2013010500002.md): Bulkhead · cracked · Jan 5, 2013 · N213PS · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > DURING SCHEDULED MAINTENANCE FOUND FS 202 PRESSURE BULKHEAD AT BRAKE CABLE CUTOUT CRACKED. FS 202 PRESSURE BULKHEAD AT BRAKE CABLE CUTOUT WAS INSPECTED AND REPAIRED USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.
- [SDR VNAA2013010500001](https://openairdocs.org/sdr/VNAA2013010500001.md): Bulkhead · cracked · Jan 5, 2013 · N213PS · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > DURING SCHEDULED MAINTENANCE THE FS 621.00 REAR PRESSURE BULKHEAD WAS FOUND CRACKED. THE FS 621.00 REAR PRESSURE BULKHEAD WAS INSPECTED AND REPAIRED USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.
- [SDR VNAA2012072200014](https://openairdocs.org/sdr/VNAA2012072200014.md): Seal · cut · Jul 22, 2012 · N213PS · Cndair CL6002B19 · Passenger/Crew Doors
  > WHILE CLIMBING THROUGH FL180, CREW REPORTED LOUD SQUEAL BEGAN AROUND PASSENGER DOOR. CREW DIVERTED AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND FOUND CUT IN DOOR SEAL BELOW SUPPORT WHEEL ARM. MAINTENANCE REMOVED AND REPLACED PASSENGER DOOR SEAL AN
- [SDR VNAA2012072000013](https://openairdocs.org/sdr/VNAA2012072000013.md): Door · noisy · Jul 20, 2012 · N213PS · Cndair CL6002B19 · Passenger/Crew Doors
  > AT APPROXIMATELY FL280, CREW REPORTED LOUD HORN-LIKE NOISE HEARD NEAR PASSENGER DOOR. CREW DIVERTED AND LANDED WITHOUT INCIDENT. MAINTENANCE CLEANED AND INSPECTED PASSENGER DOOR SEAL AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUAL. NO LEAKS NOTED. A
- [SDR VNAA2012070500007](https://openairdocs.org/sdr/VNAA2012070500007.md): Light · inoperative · Jul 5, 2012 · N213PS · Cndair CL6002B19 · Emergency Lighting
  > CREW REPORTED AFT CEILING EMERGENCY FLOOD LIGHT DOES NOT ILLUMINATE. MAINTENANCE INSPECTED, REMOVED AND REPLACED MOST AFT CABIN CEILING EMERGENCY FLOOD LIGHT AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUAL. AIRCRAFT RELEASED FOR SERVICE.

Next page: https://openairdocs.org/deregistered/N213PS-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 = 'N213PS' AND deregistration_id = 'N213PS-2025-12-09'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N213PS-2025-12-09/reports

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