# Service difficulty reports: N257PS, cancelled Dec 9, 2025

A list on [N257PS, cancelled Dec 9, 2025](https://openairdocs.org/deregistered/N257PS-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 · 61 reports

- [SDR VNAA202003119995](https://openairdocs.org/sdr/VNAA202003119995.md): Door Sill · corroded · Mar 11, 2020 · N257PS · Bombdr CL6002D15 · Fuselage Miscellaneous Structure
  > AFT CARGO DOOR FLOOR SILL CORRODED IN MULTIPLE LOCAITONS FROM FS 574 - 621 UNDER FLOORBOARD 281LLF. 03/02/20 (ROSEM) M/A: 1. N/A. C/A: 1. FOUND AFT CARGO DORO FLOOR SILL TO BE OUT OF LIMITS IAW CRJ 200 53-0-00 SRM. MTC 03/03/20 M/A: 2. REMOVED THE AFT CARGO DO
- [SDR VNAA202003119994](https://openairdocs.org/sdr/VNAA202003119994.md): Door Sill · corroded · Mar 11, 2020 · N257PS · Bombdr CL6002D15 · Fuselage Miscellaneous Structure
  > LH PRESSURE FLOOR SILL HAS 3 AREAS OF CORROSION FS449-FS473. 02/20/20 (AS) M/A: 1. N/A C/A: 1. REMOVED CORROSION @ L/H PRESSURE FLOOR SILL BETWEEN FS 409+129 AND FS 559, PRESSURE FLOOR ANGLE 409+128-559 IAW REO 601R-53-41-666, REV.C DATED 2012-11-06. 2/20/20 M
- [SDR VNAA202003119993](https://openairdocs.org/sdr/VNAA202003119993.md): Door Sill · corroded · Mar 11, 2020 · N257PS · Bombdr CL6002D15 · Fuselage Miscellaneous Structure
  > RH PRESSURE FLOOR SILL HAS 9 AREAS OF CORROSION BETWEEN FS428 AND FS530. 02/20/20 (AS) M/A: 1. N/A C/A: 1. REMOVED CORROSION @ R/H PRESSURE FLOOR SILL AND FLOOR ANGLE IAW REO 601R-53-41-666, REV.C DATED 2012-11-06. 2/20/20 M/A: 2. REPAIR AREAS REQUIRE NDT TO
- [SDR VNAA202003119992](https://openairdocs.org/sdr/VNAA202003119992.md): Bulkhead · cracked · Mar 11, 2020 · N257PS · Bombdr CL6002D15 · Fuselage Main, Bulkhead
  > FOUND REAR PRESSURE BUCKHEAD HAS INDICATIONS NOTED AT BLOO WL112-110 5090 FSH AND LBL18 WL141-142.510090FSH BOTH AREAS FAILED NOT INSPECTIONS. 2/17/20 (TK) M/A: 1. REMOVE AFT CARGO DOOR PULLEY BRACKET IAW CRJ200 SRM 51-42-06. 2/20/20 C/A: 1. REINSTALLED AFT CA
- [SDR VNAA202003119991](https://openairdocs.org/sdr/VNAA202003119991.md): Skin · corroded · Mar 11, 2020 · N257PS · Bombdr CL6002D15 · Fuselage Main, Plate/Skin
  > CORROSION FOUND ON OUTER SKIN UNDER FWD WATER DRAIN MAST. 2/15/20 (PCC) M/A: 1. CORROSION FOUND TO BE OUT OF LIMITS IAW CRJ200 SRM 53-00-31. 2/15/20 C/A: 1. REMOVED CORROSION IAW CRJ200 SRM 51-21-06. 2/15/20 M/A: 2. UT INSPECTION REQUIRED TO DETERMINE REMAININ
- [SDR VNAA2019110761102](https://openairdocs.org/sdr/VNAA2019110761102.md): Warning Message · false activation · Nov 6, 2019 · N257PS · Cndair CL6002B19 · Fire Detection
  > APU FIRE RED WARNING MESSAGE IN FLIGHT. DEFERRED APU. PER FIM VISABLY INSPECTED APU FIRE LOOP NO DEFECTS NOTED PERFORMED OPS CHECK OF APU FIRE-DETECTION SYSTEM IAW CRJ 200 AMM OPS CHECK GOOD AT THIS TIME. THIS CLEARS MEL.
- [SDR VNAA2019071811101](https://openairdocs.org/sdr/VNAA2019071811101.md): Battery · discharged · Jul 18, 2019 · N257PS · Cndair CL6002B19 · Emergency Lighting
  > EMERGENCY LIGHTS WON'T STAY ON. R&R ALL 4 EMERGENCY POWER SUPPLY BATTERIES IAW CRJ 200 AMM 33-51-04-000/400-801. OPS CHECK GOOD AT THIS TIME. S/N 169577, 121949, 103966, 126070
- [SDR VNAA2019060911101](https://openairdocs.org/sdr/VNAA2019060911101.md): Inverter · failed · Jun 9, 2019 · N257PS · Cndair CL6002B19 · Emergency Lighting
  > LH LOWER EMERGENCY EXIT LIGHT WILL NOT ILLUMINATE. REMOVED AND REPLACED LH FLOOR LEVEL FLOOD EXIT SIGN IAW CRJ 200 AMM 33-51-10-000/400-801 REMOVED AND REPLACED #2 INVERTER IAW CRJ 200 AMM 33-51-07-000/400-801 OPS CHECK GOOD
- [SDR VNAA2018102211102](https://openairdocs.org/sdr/VNAA2018102211102.md): Exhaust Valve · malfunctioned · Oct 22, 2018 · N257PS · Cndair CL6002B19 · Air Distribution System
  > DURING CLIMB CREW RECEIVED AN OVERBOARD COOL AMBER MSG. AFTER RUNNING THE QRH THE MSG STILL PERSISTED. CREW DECIDED TO CONTINUE TO CLT PRESSURIZED AND DECLARED AN EMERGENCY INTO CLT. MAINTENANCE DEFERRED OVERBOARD EXHAUST VALVE AND INBOARD EXHAUST VALVE.
- [SDR VNAA2018011499912](https://openairdocs.org/sdr/VNAA2018011499912.md): Trunnion · cracked · Jan 14, 2018 · N257PS · Cndair CL6002B19 · Wing, Landing Gear Attach Fittings
  > ONE INDICATION NOTED IN FASTENER HOLE OTBD OF MLG CUT OUT ON RT SIDE 5TH HOLE GOING FWD FROM AFT HOLE IN STEEL STRAP ON O/B AFT SIDE OF HOLE.550 INCH UP FROM LOWER SURFACE OF STEEL STRAP EXTENDING UP.100 INCH. PERFORMED EDDY CURRENT INSPECTION AT THE RT MLG
- [SDR VNAA2018011499911](https://openairdocs.org/sdr/VNAA2018011499911.md): Trunnion · cracked · Jan 14, 2018 · N257PS · Cndair CL6002B19 · Wing, Landing Gear Attach Fittings
  > ONE INDICATION NOTED IN FASTENER HOLE O/B OF MLG CUT OUT ON LT SIDE FIRST HOLE AFT OF STEEL STRAP. ON AFT SIDE OF HOLE.300 INCH UP FROM LOWER SURFACE OF PLANK EXTENDING UP.100 INCH. REPAIRED THE TRUINNION IAW REO 601R-57-21-2704 REV.
- [SDR VNAA2018011499910](https://openairdocs.org/sdr/VNAA2018011499910.md): Bulkhead Web · cracked · Jan 14, 2018 · N257PS · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > REAR PRESSURE BULKHEAD WEB HAS CRACK INDICATIONS, LBL 27.5, WL 130. ONE INCH IN LENGTH. CUT OUT DAMAGE IAW REO 601R-53-61-1541, REV F. PERFORMED AN EDDY CURRENT OF REWORKED AREA IAW REO 601R-53-61-1541, REV F. NO INDICATIONS NOTED. REPAIRED IAW REO 6
- [SDR VNAA2018011499909](https://openairdocs.org/sdr/VNAA2018011499909.md): Bulkhead Web · cracked · Jan 14, 2018 · N257PS · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > REAR PRESSURE BULKHEAD WEB HAS MULTIPLE CRACK INDICATIONS NOTED AT LBL 9.5, WL 109, ONE INCH IN LENGTH. CUT OUT DAMAGE IAW REO 601R-53-61-1285, REV E. PERFORMED EDDY CURRENT OF REWORKED AREAS IAW REO 601R-53-61-1285 REV E, NO INDICATIONS NOTED. REPAIRED
- [SDR VNAA2018011499908](https://openairdocs.org/sdr/VNAA2018011499908.md): Bulkhead Web · cracked · Jan 14, 2018 · N257PS · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > REAR PRESSURE BULKHEAD WEB HAS A CRACK INDICATION NOTED AT LBL 36.20, WL 76, ONE INCH LONG. CUT OUT DAMAGE IAW REO 601R-53-61-1285, REV E, SHEET 13, SECTION 5D. THE CUTOUT IS OUTSIDE OF REO 601R-53-61-1285 REPAIR SCOPE. PERFORMED EDDY CURRENT ON REWORKED
- [SDR VNAA2018011499907](https://openairdocs.org/sdr/VNAA2018011499907.md): Drag Angle · cracked · Jan 14, 2018 · N257PS · Cndair CL6002B19 · Passenger/Crew Doors
  > PAX DOOR AFT DRAG ANGLE CRACKED ADJACENT TO POWER ASSIST PULLEY BRACKET. REPAIRED THE DRAG ANGLE IAW EO 2B19-52-L05444A, PART B, AND REO 601R-52-11-513 REV B.
- [SDR VNAA2018011499906](https://openairdocs.org/sdr/VNAA2018011499906.md): Frame · cracked · Jan 14, 2018 · N257PS · Cndair CL6002B19 · Fuselage Main, Frame
  > FRAME CRACKED AT BS 718, STRINGER 11L. REMOVED AND INSTALLED A NEW FRAME SECTION IAW SRM 51-42-06 & 51-23-16.
- [SDR VNAA2018011499905](https://openairdocs.org/sdr/VNAA2018011499905.md): Frame · cracked · Jan 14, 2018 · N257PS · Cndair CL6002B19 · Fuselage Main, Frame
  > FRAME CRACKED AT BS 718, STRINGER 11R. REMOVED AND REPLACED THE FRAME IAW SRM 51-42-06, AND SRM 51-40-11.
- [SDR VNAA2018011499903](https://openairdocs.org/sdr/VNAA2018011499903.md): Angle · cracked · Jan 14, 2018 · N257PS · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > FLOORBEAM AT BS 484, LBL27 HAS A CRACKED ANGLE. REMOVED AND REPLACED THE ANGLE IAW SRM 51-42-21.
- [SDR VNAA20180114999](https://openairdocs.org/sdr/VNAA20180114999.md): Seat Track · corroded · Jan 14, 2018 · N257PS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON LEFT SEAT TRACK FWD AND AFT OF BS 409 + 128 AT VARIOUS LOCATIONS. REMOVED AND REPLACED THE SEAT TRACK IAW REO 601R-53-00-055, REV C.
- [SDR VNAA2018011499902](https://openairdocs.org/sdr/VNAA2018011499902.md): Seat Track · corroded · Jan 14, 2018 · N257PS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON RT SEAT TRACK FWD AND AFT OF BS 409 + 128 AT VARIOUS LOCATIONS. REMOVED AND REPLACED THE SEAT TRACK IAW REO 601R-53-00-055, REV C.
- [SDR VNAA2018011499901](https://openairdocs.org/sdr/VNAA2018011499901.md): Angle · cracked · Jan 14, 2018 · N257PS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > AFT EQUIPMENT BAY LEFT BS 621 - 625 OBLIQUE ANGLE CRACKED. REMOVED AND REPLACED THE OBLIQUE ANGLE IAW SRM 51-42-21.
- [SDR VNAA2017070911101](https://openairdocs.org/sdr/VNAA2017070911101.md): Connector · dirty · Jul 9, 2017 · N257PS · Cndair CL6002B19 · Fire Protection System Wiring
  > CREW RECEIVED A CARGO BOTTLE LOW CAUTION MESSAGE AT FLIGHT LEVEL 290. DECLARED AN EMERGENCY AND DIVERTED. LANDED WITH OUT INCIDENT. FOUND NO EVIDENCE OF FIRE OR SMOKE. MAINTENANCE CLEANED THE CONNECTOR PLUGS ON THE FIRE BOTTLES AND PREFORMED AN OPS CHECK OF
- [SDR VNAA2016081800020](https://openairdocs.org/sdr/VNAA2016081800020.md): Control Lever · faulty · Aug 18, 2016 · N257PS · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLAPS FAILED DURING APPROACH AT 30 DEGREES AND 160 KNOTS. LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, REMOVED AND REPLACED THE FLAP CONTROL LEVER AND PREFORMED CHECKS IAW THE AMM. THE AIRCRAFT WAS RELEASED FOR SERVICE.
- [SDR VNAA2016081100009](https://openairdocs.org/sdr/VNAA2016081100009.md): Inverter · inoperative · Aug 11, 2016 · N257PS · Cndair CL6002B19 · Emergency Lighting
  > EMERGENCY FLOOR TRACK LIGHTING OUT AFTER ROW 5 TO THE BACK SIDEWALL. MAINTENANCE R & R THE NR 3 INVERTER IAW AMM AND THE NR 4 POWER SUPPLY BATTERY FOR THE EMERGENCY LIGHTS IAW AMM, OPS CHECK GOOD.
- [SDR VNAA2016081100008](https://openairdocs.org/sdr/VNAA2016081100008.md): Inverter · inoperative · Aug 11, 2016 · N257PS · Cndair CL6002B19 · Emergency Lighting
  > RIGHT LOWER FLOODLIGHT INOPERATIVE. MAINTENANCE R & R THE NR 3 INVERTER IAW AMM, OPS CHECK GOOD.
- [SDR VNAA2016060400005](https://openairdocs.org/sdr/VNAA2016060400005.md): Controller · inoperative · Jun 4, 2016 · N257PS · Cndair CL6002B19 · Windshield/Door Rain/Ice Removal
  > CAPTAIN SIDE WINDSHIELD SHATTERED IN FLIGHT. THE CREW DECLARED AN EMERGENCY, DIVERTED TO NEAREST FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, R & R THE LT WINDSHIELD AND WINDSHIELD TEMP CONTROLLER. MAINTENANCE PERFORMED CHECKS IAW THE AMM AND T
- [SDR VNAA2016060400004](https://openairdocs.org/sdr/VNAA2016060400004.md): Windshield · cracked · Jun 4, 2016 · N257PS · Cndair CL6002B19 · Flight Compartment Windows
  > CAPTAIN SIDE WINDSHIELD SHATTERED IN FLIGHT. THE CREW DECLARED AN EMERGENCY, DIVERTED TO NEAREST FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, R & R THE LT WINDSHIELD AND WINDSHIELD TEMP CONTROLLER. MAINTENANCE PERFORMED CHECKS IAW THE AMM AND T
- [SDR VNAA2016041600017](https://openairdocs.org/sdr/VNAA2016041600017.md): A/C Pack · malfunctioned · Apr 16, 2016 · N257PS · Cndair CL6002B19 · Cabin Cooling System
  > DURING CLIMBOUT, THE CREW RECEIVED A RT PACK FAULT AND RT PACK HIGH PRESSURE WHEN COMPLYING WITH MEL PROCEDURES FOR THE LT PACK. MAINTENANCE INTEROGATED AND FOUND NO RELATED FAULTS FOR THE RT PACK AND COULD NOT DUPLICATE THE ISSSUE. MAINTENANCE PERFORMED CHEC
- [SDR VNAA2016030300003](https://openairdocs.org/sdr/VNAA2016030300003.md): Plate · corroded · Mar 3, 2016 · N257PS · Cndair CL6002B19 · Fuselage Main, Structure
  > PASSENGER DOOR FWD ANCHOR FITTING SERRATED PLATE CORRODED. R & R PASSENGER DOOR FWD ANCHOR FITTING SERRATED PLATE, PN 600-38061-11 IAW AMM 52-11-17-400-804.
- [SDR VNAA2016030200002](https://openairdocs.org/sdr/VNAA2016030200002.md): Angle · corroded · Mar 2, 2016 · N257PS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > PAX DOOR UPPER SILL ANGLE CORRODED BETWEEN BS 310 AND 349. REPAIRED PAX DOOR UPPER SILL ANGLE, PN 601R31527-221 IAW SRM 51-42-10, 51-42-21, AND 51-42-06.
- [SDR VNAA2016030200001](https://openairdocs.org/sdr/VNAA2016030200001.md): Floor Support · corroded · Mar 2, 2016 · N257PS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RIGHT PRESSURE FLOOR SILL STRAP CORRODED BEYOND LIMITS AT FS 513.00. R & R RT PRESSURE SILL STRAP IAW SRM 51-42-16, 51-42-22, AND 51-77-00.
- [SDR VNAA2016021400017](https://openairdocs.org/sdr/VNAA2016021400017.md): Connector · damaged · Feb 14, 2016 · N257PS · Cndair CL6002B19 · Light System Wiring
  > CREW REPORTED BACK HALF OF FLOOR TRACK EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE TROUBLESHOT, REPAIRED AFT CONNECTOR ON EMERGENCY LIGHT STRIP AND PERFORMED CHECKS IAW AMM. THE ACFT WAS RELEASED FOR SERVICE.
- [SDR VNAA2015111100004](https://openairdocs.org/sdr/VNAA2015111100004.md): Wire · disconnected · Nov 11, 2015 · N257PS · Cndair CL6002B19 · Light System Wiring
  > CREW REPORTED FLOOR EMERGENCY LIGHTS HAD A DISCONNECTED WIRE AND AFT HALF OF LIGHTS BEYOND ROW NINE INOPERATIVE. MAINTENANCE INSPECTED, SPLICED IN WIRE SPLICE CONNECTORS ON ROW 13 EMERGENCY FLOOR LIGHTS AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE
- [SDR VNAA2015050700001](https://openairdocs.org/sdr/VNAA2015050700001.md): Sensor · failed · May 7, 2015 · N257PS · Cndair CL6002B19 · Detection System
  > CREW REPORTED ANTI-ICE DUCT WARNING MESSAGE DURING CLIMB. CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, R & R FUSELAGE SENSING ELEMENT AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.
- [SDR VNAA2014102800016](https://openairdocs.org/sdr/VNAA2014102800016.md): Light · broken · Oct 28, 2014 · N257PS · Cndair CL6002B19 · Emergency Lighting
  > CREW REPORTED ENTRY LIGHT BROKEN. MAINTENANCE INSPECTED, R & R ENTRY FLOOR EMERGENCY FLOODLIGHT AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.
- [SDR VNAA2014061400012](https://openairdocs.org/sdr/VNAA2014061400012.md): Access Door · out of adjust · Jun 14, 2014 · N257PS · Cndair CL6002B19 · Fixed Inner Doors
  > CREW REPORTED FORWARD F/A EMERGENCY EQUIPMENT ACCESS, LATCHES AND DOOR, STICKS AND HARD TO OPEN. MAINTENANCE INSPECTED, ADJUSTED EMERGENCY EQUIPMENT ACCESS DOOR AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.
- [SDR VNAA2014052000014](https://openairdocs.org/sdr/VNAA2014052000014.md): Cargo Track · corroded · May 20, 2014 · N257PS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > DURING SCHEDULED MAINTENANCE, CORROSION WAS FOUND ON THE CARGO TRACKS AT BS 559+80, 559.0+96 AND FS 574 - 605. THE AREA WAS INSPECTED AND CARGO FLOOR TRACKS WERE REPLACED USING AMM. ACFT WAS RELEASED FOR SERVICE.
- [SDR VNAA2014052000013](https://openairdocs.org/sdr/VNAA2014052000013.md): Floor Support · corroded · May 20, 2014 · N257PS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > DURING SCHEDULED MAINTENANCE, CORROSION WAS FOUND AROUND CARGO FLOOR SUPPORT FASTENER HOLES. THE AREA WAS INSPECTED AND CARGO FLOOR SUPPORT WAS REPLACED USING AMM. ACFT WAS RELEASED FOR SERVICE.
- [SDR VNAA2014012600017](https://openairdocs.org/sdr/VNAA2014012600017.md): Cover · broken · Jan 26, 2014 · N257PS · Cndair CL6002B19 · Emergency Lighting
  > CREW REPORTED EMERGENCY LIGHT AT ROW 1 INOPERATIVE AND COVER BROKEN. MAINTENANCE INSPECTED, R & R ROW 1 FLOOR-TRACK EMERGENCY LIGHT AND COVER AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.
- [SDR VNAA2013121000005](https://openairdocs.org/sdr/VNAA2013121000005.md): Connector · damaged · Dec 10, 2013 · N257PS · Cndair CL6002B19 · Light System Wiring
  > CREW REPORTED EMERGENCY FLOOR LIGHTING INOPERATIVE FROM ROW 5 TO ROW 9. MAINTENANCE INSPECTED, R & R J391Y CONNECTOR AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.
- [SDR VNAA2013091300006](https://openairdocs.org/sdr/VNAA2013091300006.md): Selector Valve · failed · Sep 13, 2013 · N257PS · Cndair CL6002B19 · Landing Gear Retraction/Extension System
  > CREW REPORTED GEAR DISAGREE RED CAS MESSAGE. MAIN GEAR INDICATED DOWN AND LOCKED AND NOSE GEAR INDICATED UP. STEERING INOPERATIVE AMBER CAS MESSAGE ALSO REPORTED. CREW MANUALLY EXTENDED LANDING GEAR AND LANDED SAFELY. ACFT TOWED TO RAMP. MX TROUBLESHOT, R
- [SDR VNAA2012111200005](https://openairdocs.org/sdr/VNAA2012111200005.md): Controller · failed · Nov 12, 2012 · N257PS · Cndair CL6002B19 · Windshield/Door Rain/Ice Removal
  > CREW REPORTED CAPTAIN’S FRONT WINDOW CRACKED AND ELECTRICAL ARCING NOTICED. CREW RETURNED TO GATE. MAINTENANCE INSPECTED, REMOVED AND REPLACED CAPTAIN’S FRONT WINDOW AND LEFT WINDSHIELD TEMPERATURE CONTROLLER AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE M
- [SDR VNAA2012050700009](https://openairdocs.org/sdr/VNAA2012050700009.md): Light · inoperative · May 7, 2012 · N257PS · Cndair CL6002B19 · Emergency Lighting
  > CREW REPORTED LEFT AFT EXTERIOR DOOR EMERGENCY LIGHT OUT. MAINTENANCE INSPECTED, REMOVED AND REPLACED LEFT AFT EXTERIOR EMERGENCY LIGHT BULB AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUAL. AIRCRAFT RELEASED FOR SERVICE.
- [SDR VNAA2011071800020](https://openairdocs.org/sdr/VNAA2011071800020.md): Bpsu · failed · Jul 13, 2011 · N257PS · Cndair CL6002B19 · Trailing Edge Flap Control System
  > CREW REPORTED FLAPS FAILURE DURING APPROACH FLAPS SELECTED FROM 0-08 WHEN FAILURE OCCURED SPEED WAS 190 IAS, ALT 6000 FT. CREW ELECTED TO DIVERT TO CLT WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, REMOVED, REPLACED, AND PERFORMED OPERATIONAL CHECKS USING THE A
- [SDR VNAA2011071800016](https://openairdocs.org/sdr/VNAA2011071800016.md): Computer · failed · Jul 12, 2011 · N257PS · Cndair CL6002B19 · Trailing Edge Flap Control System
  > CREW REPORTED A FLAPS FAIL AT 10,000FT SPEED 250KNTS. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, REMOVED, REPLACED, AND PERFORMED OPERATIONAL CHECKS USING THE AIRCRAFT MAINTENANCE MANUALS ON THE FLAP ELECTRONIC COMPUTER. AIRCRAFT WAS RELEASE
- [SDR VNAA2011071500013](https://openairdocs.org/sdr/VNAA2011071500013.md): Bpsu · failed · Jul 11, 2011 · N257PS · Cndair CL6002B19 · Trailing Edge Flap Control System
  > CREW REPORTED FLAPS FAILURE WHEN FLAPS SELECTED FROM ZERO DEGREES TO EIGHT (8) DEGREES DURING APPROACH TO CLT. AIRCRAFT LANDED IN CLT WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT FLAP SYSTEM, REMOVED AND REPLACED LEFT BPSU (BRAKE AND POSITION SENSOR UNIT) AND P
- [SDR VNAA2011070800005](https://openairdocs.org/sdr/VNAA2011070800005.md): Control Unit · malfunctioned · Jul 2, 2011 · N257PS · Cndair CL6002B19 · Trailing Edge Flap Control System
  > CREW REPORTED FLAPS FAIL AT 20 DEGREES WHEN FLAPS WERE SELECTED TO 30 DEGREES WHILE ON APPROACH TO CLT. AIRCRAFT LANDED IN CLT WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT FLAP SYSTEM, REMOVED AND REPLACED FECU (FLAP ELECTRONIC CONTROL UNIT) AND PERFORMED CHECK
- [SDR VNAA2011031600011](https://openairdocs.org/sdr/VNAA2011031600011.md): Sill · corroded · Mar 16, 2011 · N257PS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > DURING SCHEDULED MAINTENANCE THE LEFT PRESSURE FLOOR SILL HAD CORROSION AROUND NUT PLATES FROM FS 449.85 TO 473.15. REPAIRS WERE ACCOMPLISHED USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RETURNED TO SERVICE.
- [SDR VNAA2011031600013](https://openairdocs.org/sdr/VNAA2011031600013.md): Post · cracked · Mar 16, 2011 · N257PS · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > DURING SCHEDULED MAINTENANCE THE FS 409+128 BULKHEAD VERTICAL POST WAS CRACKED. REPAIRS WERE ACCOMPLISHED USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RETURNED TO SERVICE.
- [SDR VNAA2011061600012](https://openairdocs.org/sdr/VNAA2011061600012.md): Beam · cracked · Mar 16, 2011 · N257PS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > DURING SCHEDULED MAINTENANCE, THE FS 280 TRANSVERSE BEAM WAS CRACKED. REPAIRS WERE ACCOMPLISHED USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RETURNED TO SERVICE.

Next page: https://openairdocs.org/deregistered/N257PS-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 = 'N257PS' AND deregistration_id = 'N257PS-2025-12-09'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N257PS-2025-12-09/reports

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