# Service difficulty reports: N258PS

A list on [N258PS](https://openairdocs.org/aircraft/N258PS.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 VNAA2019061511101](https://openairdocs.org/sdr/VNAA2019061511101.md): Warning Light · false indication · Jun 15, 2019 · N258PS · Cndair CL6002B19 · AC Generator-Alternator
  > WHILE CRUISING AT FL270, RECEIVED GEN 2 OFF CAUTION LIGHT. THE CREW RAN THE QRH AND LIGHT REMAINED. PER QRH, CREW SWITCHED GEN 2 OFF AND STARTED THE APU. SHORTLY THEREAFTER CREW RECEIVED APU OIL TEMP CAUTION. RAN QRH, REQUIRED TO LAND NEAREST SUITABLE. EM
- [SDR VNAA2019032499909](https://openairdocs.org/sdr/VNAA2019032499909.md): Angle · cracked · Mar 24, 2019 · N258PS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FS409+128 VERT POST @ BLO HAS A CRACK INDICATION NOTED ON BOTH LT & RT SIDES IN THE AFT RADIUS @ WL69 (MARKED ON A/C) BOTH FAILED NDT INSP. CORRECTIVE ACTION: DRILLED UP NEW SERVICEABLE ANGLES P/N 601R32208-131/132 IAW SRM 51-40-11 TR51-42.
- [SDR VNAA2019032499908](https://openairdocs.org/sdr/VNAA2019032499908.md): Beam · cracked · Mar 24, 2019 · N258PS · Cndair CL6002B19 · Fuselage Main, Structure
  > UPON REMOVAL OF AFT CARGO FLOOR LANDING PLATE FOUND TRAVERSE BEAM AT FS 589, OUTBOARD OF LBL 27, CRACKED IN RADIUS. CORRECTIVE ACTION: COMPLIED WITH REO 601R-53-61-6908 REV.-- DATED 2019-03-15.
- [SDR VNAA2019032499907](https://openairdocs.org/sdr/VNAA2019032499907.md): Seat Track · corroded · Mar 24, 2019 · N258PS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK SEGMENT BETWEEN FS 364 TO FS 349 AT RBL9 IS CORRODED. CORRECTIVE ACTION: REPLACED SEAT TRACK WITH FABRICATED TRACK PN: N126-2075 IAW REO 601R-53-00-485.
- [SDR VNAA2019032499906](https://openairdocs.org/sdr/VNAA2019032499906.md): Seat Track · corroded · Mar 24, 2019 · N258PS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK SEGMENT BETWEEN FS 364 TO FS 349 AT LBL9 IS CORRODED. CORRECTIVE ACTION: REPLACED SEAT TRACK WITH FABRICATED TRACK PN: N126-2075 IAW REO 601R-53-00-485.
- [SDR VNAA2019032499905](https://openairdocs.org/sdr/VNAA2019032499905.md): Doubler · corroded · Mar 24, 2019 · N258PS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > GALLEY FLOOR MOUNT FITTING IS CORRODED AT RBL 5 AT FS 316. CORRECTIVE ACTION: REPLACED GALLEY FLOOR SUPPORT DOUBLER PN: 601R387781-1 IAW SRM 51-42-06, 51-42-13.
- [SDR VNAA2019032499904](https://openairdocs.org/sdr/VNAA2019032499904.md): Seat Track · corroded · Mar 24, 2019 · N258PS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > LBL 9 SEAT RAIL IS GOUGED/CORRODED IN MULTIPLE LOCATIONS FROM FS 409 TO FS 409 +112. CORRECTIVE ACTION: REPLACED SEAT TRACK WITH FABRICATED TRACK PN: N126-2075 IAW REO 601R-53-00-485.
- [SDR VNAA2019032499903](https://openairdocs.org/sdr/VNAA2019032499903.md): Seat Track · corroded · Mar 24, 2019 · N258PS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
  > RT FLOOR SEAT RAIL IS CORRODED/GOUGED BETWEEN FS 409 TO FS 409+112. CORRECTIVE ACTION: REPLACED SEAT TRACK WITH FABRICATED TRACK PN: N126-2075 IAW REO 601R-53-00-485.
- [SDR VNAA2019032499902](https://openairdocs.org/sdr/VNAA2019032499902.md): Angle · cracked · Mar 24, 2019 · N258PS · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > RT MLG WHEEL WELL HYDRAULIC FUSE MOUNTING ANGLE IS CRACKED. CORRECTIVE ACTION: REMOVED AND REPLACED MOUNTING ANGLE IAW SRM 51-42-06.
- [SDR VNAA2019032499901](https://openairdocs.org/sdr/VNAA2019032499901.md): Angle · cracked · Mar 24, 2019 · N258PS · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > LT MLG WHEEL WELL HYDRAULIC FUSE MOUNTING ANGLE IS CRACKED. CORRECTIVE ACTION: REMOVED AND REPLACED MOUNTING ANGLE IAW SRM 51-42-06.
- [SDR VNAA2017052500011](https://openairdocs.org/sdr/VNAA2017052500011.md): Motor · inoperative · May 25, 2017 · N258PS · Cndair CL6002B19 · Passenger/Crew Doors
  > PASSENGER DOOR ASSIST MOTOR INOPERATIVE; REMOVED AND REPLACED PASSENGER DOOR ASSIST MOTOR.
- [SDR VNAA2017052300010](https://openairdocs.org/sdr/VNAA2017052300010.md): Anchor Fitting · cracked · May 23, 2017 · N258PS · Cndair CL6002B19 · Passenger/Crew Doors
  > PASSENGER DOOR CABLE SWIVEL RUBBING AGAINST THE HANDRAIL SUPPORT BRACKETS; REMOVED AND REPLACED PASSENGER DOOR’S FORWARD ANCHOR FITTING.
- [SDR VNAA2017032400016](https://openairdocs.org/sdr/VNAA2017032400016.md): Bulkhead · corroded · Mar 24, 2017 · N258PS · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > MAINTENANCE PERFORMED A MAJOR REPAIR TO THE REAR PRESSURE BULKHEAD WEB AT FS 621.00 WL 73.00 LBL 9.50.
- [SDR VNAA2017031300006](https://openairdocs.org/sdr/VNAA2017031300006.md): Cup · corroded · Mar 13, 2017 · N258PS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FORWARD AND AFT PASSENGER HANDRAIL CUPS ARE CORRODED. REMOVED AND REPLACED FORWARD AND AFT CUPS.
- [SDR VNAA2016100600010](https://openairdocs.org/sdr/VNAA2016100600010.md): Wire Harness · damaged · Oct 6, 2016 · N258PS · Cndair CL6002B19 · Door System Wiring
  > PASSENGER DOOR, SERVICE DOOR, AND CARGO DOOR MESSAGES DURING CLIMBOUT. THE CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. FOUND DAMAGE TO WIRES ON AFT CARGO DOOR WIRING HARNESS. MAINTENANCE REMOVED AND REPLACED AFT CARGO DOOR HARNESS AND PERFORMED CHECKS
- [SDR VNAA2016091900025](https://openairdocs.org/sdr/VNAA2016091900025.md): Control Lever · faulty · Sep 19, 2016 · N258PS · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLAPS FAIL AT 30 DEGREES DURING APPROACH. THE CREW DECLARED AN EMERGENCY, CONTINUED TO DESTINATION AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, REMOVED AND REPLACED THE FLAP CONTROL LEVER AND PERFORMED CHECKS IAW THE AMM. THE AIRCRAFT WAS RELEASED FOR
- [SDR VNAA2016090800003](https://openairdocs.org/sdr/VNAA2016090800003.md): Selector Valve · faulty · Sep 8, 2016 · N258PS · Cndair CL6002B19 · Landing Gear Retraction/Extension System
  > GEAR DISAGREE, ANTI-SKID, AND PARKING BREAK SHUT OFF VALVE MESSAGES AFTER TAKE OFF. THE CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT AND REMOVED AND REPLACED THE MAIN LANDING GEAR SELECTOR VALVE. PERFORMED CHECKS IAW THE AMM. T
- [SDR VNAA2016030600011](https://openairdocs.org/sdr/VNAA2016030600011.md): Selector Valve · inoperative · Mar 6, 2016 · N258PS · Cndair CL6002B19 · Landing Gear Retraction/Extension System
  > CREW REPORTED RECEIVING A GEAR DISAGREE MESSAGE ON DESCENT. THEY DECLARED AN EMERGENCY, CONTINUED TO DESTINATION AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, R & R THE MLG SELECTOR VALVE AND PERFORMED CHECKS IAW THE AMM. THE ACFT WAS RELEASED FOR S
- [SDR VNAA2016021900023](https://openairdocs.org/sdr/VNAA2016021900023.md): Carbon Seal · leaking · Feb 19, 2016 · N258PS · Cndair CL6002B19 · Engine Collector/Tailpipe/Nozzle
  > CREW REPORTED RECEIVING A RT ENGINE OIL PRESSURE MESSAGE DURING CRUISE AT FL310. THE CREW DECLARED AN EMERGENCY, DIVERTED TO NEAREST FIELD AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE TROUBLESHOT, R & R THE NR 7 CARBON SEAL AND PERFORMED CHECKS IAW THE A
- [SDR VNAA2016021900022](https://openairdocs.org/sdr/VNAA2016021900022.md): Carbon Seal · leaking · Feb 19, 2016 · N258PS · Cndair CL6002B19 · Engine Collector/Tailpipe/Nozzle
  > CREW REPORTED RECEIVING A RT ENGINE OIL PRESSURE MESSAGE DURING CRUISE AT FL310. THE CREW DECLARED AN EMERGENCY, DIVERTED TO NEAREST FIELD AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE TROUBLESHOT, R & R THE NR 6 CARBON SEAL AND PERFORMED CHECKS IAW THE AM
- [SDR VNAA2015082300034](https://openairdocs.org/sdr/VNAA2015082300034.md): Controller · failed · Aug 23, 2015 · N258PS · Cndair CL6002B19 · Windshield/Door Rain/Ice Removal
  > CREW REPORTED CRACK IN LT WINDSHIELD IN FLIGHT AND SUBSEQUENTLY RECEIVED A LT WINDSHIELD HEAT AMBER CAUTION MESSAGE. CREW DIVERTED AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED, R & R CAPTAIN’S WINDSHIELD HEAT CONTROLLER DUE TO ARCING IN WINDSHIELD AND P
- [SDR VNAA2015082300033](https://openairdocs.org/sdr/VNAA2015082300033.md): Windshield · cracked · Aug 23, 2015 · N258PS · Cndair CL6002B19 · Flight Compartment Windows
  > CREW REPORTED CRACK IN LT WINDSHIELD IN FLIGHT AND SUBSEQUENTLY RECEIVED A LT WINDSHIELD HEAT AMBER CAUTION MESSAGE. CREW DIVERTED AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED, R & R CAPTAIN’S WINDSHIELD DUE TO ARCING IN WINDSHIELD AND PERFORMED CHECKS
- [SDR VNAA2015080800013](https://openairdocs.org/sdr/VNAA2015080800013.md): B-Nut · loose · Aug 8, 2015 · N258PS · Cndair CL6002B19 · Turbine Engine Oil System
  > CREW REPORTED RT ENGINE OIL PRESSURE MESSAGE IN FLIGHT AND ELECTED TO DIVERT. PRIOR TO LANDING, OIL PRESSURE CONTINUED TO DROP, SO CREW ELECTED TO SHUTDOWN RT ENGINE. MAINTENANCE INSPECTED AND FOUND OIL LEAK DUE TO LOOSE B-NUT ON B-SUMP SCAVENGE TUBE BELOW PU
- [SDR VNAA2015080100001](https://openairdocs.org/sdr/VNAA2015080100001.md): Wire · broken · Aug 1, 2015 · N258PS · Cndair CL6002B19 · Light System Wiring
  > PRIOR TO FIRST FLIGHT OF THE DAY, CREW REPORTED EMERGENCY LIGHTS NOT WORKING FROM ROW 9 TO 12. MAINTENANCE TROUBLESHOT, REPAIRED CONNECTOR WIRE, REINSTALLED AFT RT FLOOR EMERGENCY LIGHT TRACK ASSY AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.
- [SDR VNAA2015061800014](https://openairdocs.org/sdr/VNAA2015061800014.md): Bulkhead Web · cracked · Jun 18, 2015 · N258PS · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FOUND REAR PRESSURE BULKHEAD WEB THAT SURROUNDS THE LINTAL FITTING HAS INDICATION NOTED, APPROX.300" IN LENGTH, FAILED NDT INSPECTION. REPAIRED REAR PRESSURE BULKHEAD WEB IAW REO 601R-53-61-1230 AND REO 601R-53-61-5490.
- [SDR VNAA20150618](https://openairdocs.org/sdr/VNAA20150618.md): Bulkhead Web · cracked · Jun 18, 2015 · N258PS · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FOUND REAR PRESSURE BULKHEAD WEB THAT SURROUNDS THE LINTAL FITTING HAS INDICATION NOTED. APPROXIMATELY.300" IN LENGTH, FAILED NDT INSPECTION. REPAIRED REAR PRESSURE BULKHEAD WEB IAW REO 601R-53-61-1230 AND REO 601R-53-61-5490.
- [SDR VNAA2015061800013](https://openairdocs.org/sdr/VNAA2015061800013.md): Bulkhead · cracked · Jun 18, 2015 · N258PS · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FS 202.75 BULKHEAD IS CRACKED AROUND THE HOLE FOR THE PARKING BRAKE CABLE. REPAIRED FS 202.75 BULKHEAD AT LBL 23.71 IAW REO AND SRM.
- [SDR VNAA2015061800012](https://openairdocs.org/sdr/VNAA2015061800012.md): Strap · corroded · Jun 15, 2015 · N258PS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > TENSION STRAPS BETWEEN RBL 36 AND RBL 27 AT FS559 HAVE FILIFROM AND PITTING CORROSION. R & R TENSION STRAPS WITH NEW SERVICABLE STRAPS IAW SRM.
- [SDR VNAA2015061800011](https://openairdocs.org/sdr/VNAA2015061800011.md): Strap · corroded · Jun 15, 2015 · N258PS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > TENSION STRAPS BETWEEN LBL 36 AND LBL 27 AT FS559 HAVE FILIFORM AND PITTING CORROSION. R & R TENSION STRAPS WITH NEW SERVICABLE STRAPS IAW SRM.
- [SDR VNAA2015061800015](https://openairdocs.org/sdr/VNAA2015061800015.md): Skin · cracked · Jun 13, 2015 · N258PS · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > EXTERNAL FUSELAGE SKIN AT NLG CUTOUT AFT RT CORNER HAS CRACK APPROXIMATELY 1" LONG. REPAIRED IAW REO.
- [SDR VNAA2015041400019](https://openairdocs.org/sdr/VNAA2015041400019.md): Duct · unknown · Apr 14, 2015 · N258PS · Cndair CL6002B19 · Cabin Cooling System
  > CREW REPORTED NO AIR FLOW FROM ANY VENTS WHEN BLEEDS WERE TRANSFERRED TO ENGINE AFTER TAKEOFF. CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED, R & R PRECOOLER OUTLET DUCT AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.
- [SDR VNAA2015041400018](https://openairdocs.org/sdr/VNAA2015041400018.md): Regulator Valve · failed · Apr 14, 2015 · N258PS · Cndair CL6002B19 · Cabin Cooling System
  > CREW REPORTED NO AIR FLOW FROM ANY VENTS WHEN BLEEDS WERE TRANSFERRED TO ENGINE AFTER TAKEOFF. CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED, R & R LT PACK VALVE AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.
- [SDR VNAA201412290009](https://openairdocs.org/sdr/VNAA201412290009.md): Battery Pack · discharged · Dec 26, 2014 · N258PS · Cndair CL6002B19 · Emergency Lighting
  > CREW REPORTED THAT THE EMERGENCY LIGHTS HAD BEEN LEFT ON ALL NIGHT. FERRIED, WHERE MAINTENANCE R & R EMERGENCY LIGHT BATTERIES AND PERFORMED CHECKS IAW MM. ACFT RELEASED FOR SERVICE.
- [SDR VNAA2014110200001](https://openairdocs.org/sdr/VNAA2014110200001.md): Connector · damaged · Nov 2, 2014 · N258PS · Cndair CL6002B19 · Light System Wiring
  > CREW REPORTED CABIN FLOOR EMERGENCY LIGHTS AT ROW 8 THROUGH 12 WOULD NOT COME ON. MAINTENANCE INSPECTED EMERGENCY FLOOR PATH LIGHTING AND FOUND BROKEN WIRES AT FLOOR CONNECTION. MAINTENANCE INSTALLED NEW CONNECTORS AND PINS ON EMERGENCY LIGHT STRIP AND PERFOR
- [SDR VNAA2013090300002](https://openairdocs.org/sdr/VNAA2013090300002.md): Radar · failed · Sep 3, 2013 · N258PS · Cndair CL6002B19 · Weather Radar System
  > CREW REPORTED WEATHER RADAR STOPPED WORKING AT ALTITUDE AND LOST RETURNS ON CAPTAIN’S AND F/O MFD (MULTIFUNCTION DISPLAY). CREW DIVERTED DUE TO WEATHER AND LANDED WITHOUT INCIDENT. MX INSPECTED, R & R WEATHER RADAR RECEIVER/ TRANSMITTER AND PERFORMED CHECKS
- [SDR VNAA2013071500013](https://openairdocs.org/sdr/VNAA2013071500013.md): B-Nut · loose · Jul 15, 2013 · N258PS · Cndair CL6002B19 · APU Oil System
  > CREW REPORTED A STRONG ODOR OF JET FUEL WHILE OPERATING ON APU BLEED SYS. MX INSPECTED, TIGHTENED B-NUT ON FUEL CONTROL SUPPLY LINE AND PERFORMED CHECKS ON APU USING AMM. NO LEAKS NOTED. ACFT RELEASED FOR SERVICE.
- [SDR VNAA2013062000010](https://openairdocs.org/sdr/VNAA2013062000010.md): Structure · cracked · Jun 20, 2013 · N258PS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > DURING SCHEDULED MAINTENANCE FS 621.0 WAS FOUND CRACKED. THE AREA WAS INSPECTED AND REPAIRED USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.
- [SDR VNAA2012060100001](https://openairdocs.org/sdr/VNAA2012060100001.md): Pump · failed · Jun 1, 2012 · N258PS · Cndair CL6002B19 · Hydraulic Pump (Electric/Engine), Main
  > CREW REPORTED HYDRAULIC SYSTEM TWO (2) AT ZERO PSI AND ZERO PERCENT IN FLIGHT. CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, REMOVED AND REPLACED NUMBER TWO (2) EDP (ENGINE DRIVEN PUMP) AND PERFORMED CHECKS USING AIRCRAFT MAINT
- [SDR VNAA2012052200019](https://openairdocs.org/sdr/VNAA2012052200019.md): Wire · burned · May 22, 2012 · N258PS · Cndair CL6002B19 · Equipment/Furnishings Wiring
  > CREW REPORTED SMELL OF SMOKE IN CABIN ON TAXI OUT. CREW RETURNED TO GATE. MAINTENANCE INSPECTED AND FOUND CAUSE OF BURNING SMELL TO BE BURNT GROUND WIRE ON BOTTOM OF COFFEEMAKER. MAINTENANCE REMOVED AND REPLACED COFFEEMAKER AND PERFORMED CHECKS USING AIRCRA
- [SDR VNAA2012020900002](https://openairdocs.org/sdr/VNAA2012020900002.md): Seal · damaged · Feb 6, 2012 · N258PS · Cndair CL6002B19 · Service Doors
  > CREW REPORTED RUMBLING NOISE COMING FROM SERVICE DOOR IN FLIGHT. NO CHANGES IN AIRCRAFT PRESSURIZATION OBSERVED. CREW DIVERTED AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED, REMOVED AND REPLACED SERVICE DOOR SEAL AND PERFORMED CHECKS USING AIRCRAFT MAI
- [SDR VNAA2011100100004](https://openairdocs.org/sdr/VNAA2011100100004.md): Structure · dented · Oct 2, 2011 · N258PS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > DURING SCHEDULED MAINTENANCE A DENT WAS FOUND TO AIRCRAFT AT FS 682+4 JUST FORWARD OF THE RAM AIR DUCT. THE AREA WAS REPAIRED USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.
- [SDR VNAA2011100100003](https://openairdocs.org/sdr/VNAA2011100100003.md): Structure · corroded · Oct 2, 2011 · N258PS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > DURING SCHEDULED MAINTENANCE CORROSION WAS FOUND AROUND DRAIN HOLES AND FASTENERS UNDER AFT BELLY FAIRING FROM FS 559 TO FS 559+112. THE AREA WAS REPAIRED USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.
- [SDR VNAA2011100100002](https://openairdocs.org/sdr/VNAA2011100100002.md): Skin · dented · Oct 2, 2011 · N258PS · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > DURING SCHEDULED MAINTENANCE A DENT WAS FOUND TO AIRCRAFT SKIN BETWEEN FS 654 TO 672. THE AREA WAS REPAIRED USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.
- [SDR VNAA2011100100001](https://openairdocs.org/sdr/VNAA2011100100001.md): Floorbeam · cracked · Oct 2, 2011 · N258PS · 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 VNAA2010051800005](https://openairdocs.org/sdr/VNAA2010051800005.md): Pump · leaking · May 12, 2010 · N258PS · Cndair CL6002B19 · Hydraulic Pump (Electric/Engine), Main
  > CREW REPORTED A HYDRAULIC PUMP 3A AMBER MESSAGE ON APPROACH TO CLT. AIRCRAFT LANDED IN CLT WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT, REMOVED AND REPLACED ELECTRIC MOTOR DRIVEN (HYDRAULIC) PUMP 3A AND PERFORMED CHECKS USING THE AIRCRAFT MAINTENANC
- [SDR VNAA2009051500004](https://openairdocs.org/sdr/VNAA2009051500004.md): Shutoff Valve · failed · May 12, 2009 · N258PS · Cndair CL6002B19 · Cabin Cooling System
  > CREW REPORTED A RT PACK OVERPRESSURE AFTER TAKEOFF. THE PRESSURE NEVER WENT BELOW 60 PSI AND WAS AT 94 PSI WHEN FAILED. CREW ELECTED TO RETURN TO DEPARTURE AND LANDED WITHOUT INCIDENT. MX REMOVED AND REPLACED THE RT PRESSURE REGULATING SHUTOFF VALVE (PRSOV
- [SDR VNAA2009050600002](https://openairdocs.org/sdr/VNAA2009050600002.md): Rivet · damaged · May 4, 2009 · N258PS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > CREW REPORTED A LIGHTNING STRIKE IN CLT. MAINTENANCE INSPECTED AND REPLACED RIVETS, RADOME, AND DRAIN MAST. WORK WAS DONE PER THE AIRCRAFT MAINTENANCE MANUAL AND AIRCRAFT RELEASED FOR SERVICE.
- [SDR VNAA2008120400011](https://openairdocs.org/sdr/VNAA2008120400011.md): Sensing Element · shorted · Nov 30, 2008 · N258PS · Cndair CL6002B19 · Airfoil Anti/De-ice System
  > ON CLIMBOUT FROM PHL CREW RECEIVED AN ANTI ICE WARNING MESSAGE. AIRCRAFT RETURNED TO PHL, LANDING WITHOUT INCIDENT. MAINTENANCE FOUND SENSING ELEMENT A15WK SHORTED TO GROUND. MAINTENANCE REMOVED AND REPLACED ELEMENT AND NO OTHER DEFECTS NOTED. AIRCRAFT WAS
- [SDR VNAA0809007](https://openairdocs.org/sdr/VNAA0809007.md): Radome · delaminated · Sep 15, 2008 · N258PS · Cndair CL6002B19 · Aerodynamic Fairings
  > CREW REPORTED DURING LANDING A BIRD STRIKE TO THE NOSE OF THE ACFT. MX FOUND DELAMINATION ON THE RADOME. THE RADOME WAS R&R. NO OTHER DEFECTS WERE NOTED AND ACFT WAS RELEASED FOR SERVICE.
- [SDR VNAA0802005](https://openairdocs.org/sdr/VNAA0802005.md): Smoke Detector · failed · Feb 11, 2008 · N258PS · Cndair CL6002B19 · Smoke Detection
  > CREW REPORTED A SMOKE TOILET AMBER MESSAGE ON APPROACH. CREW COULD NOT VISUALLY SEE ANY SMOKE AND THE FLIGHT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND MEL'D THE LAV SMOKE DETECTION SYSTEM PER MEL 26-16-01. MAINTENANCE REMOVED AND REPLACED THE LAVAT

Next page: https://openairdocs.org/aircraft/N258PS/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 = 'N258PS' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N258PS/reports

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