# Service difficulty reports: N202PS, cancelled Oct 27, 2023

A list on [N202PS, cancelled Oct 27, 2023](https://openairdocs.org/deregistered/N202PS-2023-10-27.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 · 85 reports

- [SDR VNAA2019100231105](https://openairdocs.org/sdr/VNAA2019100231105.md): Acm · malfunctioned · Sep 30, 2019 · N202PS · Cndair CL6002B19 · Cabin Cooling System
  > THE AIRCRAFT WAS SINGLE-PACK ONLY WHEN IT LEFT DCA. DURING CLIMB AT FL230, THE FUNCTIONING LH PACK OVER-PRESSURED AND AUTOMATICALLY SHUTOFF. THE CREW INITIATED AN EMERGENCY DESCENT TO FL100. THEY CREW WAS ABLE TO RESET THE PACK ONCE REACHING THAT ALTITUDE AND
- [SDR VNAA2019092711102](https://openairdocs.org/sdr/VNAA2019092711102.md): Light · inoperative · Sep 27, 2019 · N202PS · Cndair CL6002B19 · Emergency Lighting
  > SUPPLEMENTAL INFORMATION RH SIDE #4 EMERGENCY LIGHT ABOVE THE WING INOP RELAMPED RH SIDE #4 EMERGENCY LIGHT OPS CHECK GOOD.
- [SDR VNAA2019090811101](https://openairdocs.org/sdr/VNAA2019090811101.md): Computer · failed · Sep 8, 2019 · N202PS · Cndair CL6002B19 · Fuel Indicating System
  > ON APPROACH TO DCA CREW RECEIVED FUEL IMBALANCE MESSAGES FOLLOWED QRH SAID NEEDED TO LAND WITH 20 DEGREES FLAPS, CREW DIVERTED TO IAD FOR THE LONGER RWY AND SAFETY. AN EMERGENCY WAS NOT DECLARED PAX WHERE NOTIFIED OF THE DIVERSION. DEFERRED FUEL QUANTITY INDIC
- [SDR VNAA2019070211103](https://openairdocs.org/sdr/VNAA2019070211103.md): Bpsu · failed · Jul 2, 2019 · N202PS · Cndair CL6002B19 · Trailing Edge Flap Control System
  > FLAPS FAIL IN FLIGHT. R&R LT FLAP BPSU OPS CHECK GOOD.
- [SDR VNAA2019010611101](https://openairdocs.org/sdr/VNAA2019010611101.md): Windshield · cracked · Jan 6, 2019 · N202PS · Cndair CL6002B19 · Flight Compartment Windows
  > ON DECENT THE CAPTAINS WINDSHIELD CRACKED IN FLIGHT. THE CREW DONNED THEIR OXYGEN MASKS AND DECLARED AN EMERGENCY. THE AIRCRAFT LANDED WITHOUT FURTHUR INCIDENTS. MAINTENANCE REPLACED THE WINDSHIELD AND IS BACK IN SERVICE.
- [SDR VNAA2018121899908](https://openairdocs.org/sdr/VNAA2018121899908.md): Frame · corroded · Dec 18, 2018 · N202PS · Cndair CL6002B19 · Fuselage Main, Frame
  > F.S. 364 FRAME CORRODED AT STINGER 23R. C/A: SPLICE REPAIRED FS 264 FRAME IAW BBD REO 601R-53-21-3055
- [SDR VNAA2018031211101](https://openairdocs.org/sdr/VNAA2018031211101.md): Warning Message · false activation · Mar 12, 2018 · N202PS · Cndair CL6002B19 · Stall Warning System
  > THE AIRCRAFT RECEIVED A STALL FAIL 1 MESSAGE AT 5000 FEET. DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. MAINTENANCE COMPLIED WITH A SYS RESET OF STALL COMPUTER, MESSAGE CLEARED.
- [SDR VNAA2017092199911](https://openairdocs.org/sdr/VNAA2017092199911.md): Stiffener · cracked · Sep 18, 2017 · N202PS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LOWER STIFFENER ON AFT SIDE OF THE BS 621 BULKHEAD, LBL 36 FOUND CRACKED. REMOVED AND REPLACED THE STIFFENER IAW SRM 51-40-11, AND 51-42-06.
- [SDR VNAA2017092199910](https://openairdocs.org/sdr/VNAA2017092199910.md): Door Frame · corroded · Sep 18, 2017 · N202PS · Cndair CL6002B19 · Fuselage Main, Structure
  > PASSENGER DOOR UPPER FRAME AT BS 333 IS CRACKED AT THE STANDOFF. REMOVED & REPLACED THE UPPER DOOR FRAME,
- [SDR VNAA2017092199909](https://openairdocs.org/sdr/VNAA2017092199909.md): Frame · corroded · Sep 18, 2017 · N202PS · Cndair CL6002B19 · Fuselage Main, Frame
  > FUSELAGE FRAME AT BS 605 IS CORRODED FROM STRINGERS 24L TO 24R. INSTALLED A NEW FRAME.
- [SDR VNAA2017092199908](https://openairdocs.org/sdr/VNAA2017092199908.md): Floor Support · corroded · Sep 18, 2017 · N202PS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LEFT FLOOR SUPPORT IS CORRODED FROM BS 574 TO 621. REPAIRED IAW REO 601R-53-00-526.
- [SDR VNAA2017092199907](https://openairdocs.org/sdr/VNAA2017092199907.md): Floor Support · corroded · Sep 18, 2017 · N202PS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RIGHT FLOOR SUPPORT CORRODED FROM BS 559+96 TO 595. REPAIRED THE FLOOR SUPPORT IAW REO 601R-53-00-526.
- [SDR VNAA2017092199906](https://openairdocs.org/sdr/VNAA2017092199906.md): Floor Support · corroded · Sep 18, 2017 · N202PS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > LEFT FLOOR SUPPORT IS CORRODED AT BS 473.15 AND 559. COMPLIED WITH REO 601R-53-41-666.
- [SDR VNAA2017092199905](https://openairdocs.org/sdr/VNAA2017092199905.md): Floor Support · corroded · Sep 18, 2017 · N202PS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RIGHT SIDE FLOOR SUPPORT CORRODED AT BS 499 AND 513. COMPLIED WITH REO 601R-53-41-666.
- [SDR VNAA2017092199904](https://openairdocs.org/sdr/VNAA2017092199904.md): Floorbeam · cracked · Sep 18, 2017 · N202PS · Cndair CL6002B19 · Fuselage Main, Floor Beam
  > FS 280.00 FLOORBEAM CRACKED AT RBL 9. REPAIRED IAW REO 601R-53-11-171 REV D.
- [SDR VNAA2017092199903](https://openairdocs.org/sdr/VNAA2017092199903.md): Door Sill · corroded · Sep 18, 2017 · N202PS · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RT FLOOR SILL DOUBLER AT FS 319.70 IS CORRODED ON I/B CORNER RBL 36. REMOVED AND REPLACED W/NEW SERVICEABLE P/N 601R38669-49 IAW SRM 51-42-06, 51-40-11 AND 51-42-15.
- [SDR VNAA2017092199902](https://openairdocs.org/sdr/VNAA2017092199902.md): Bulkhead · cracked · Sep 18, 2017 · N202PS · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FS 621 REAR PRESSURE BULKHEAD WEB CRACKED AT LBL 18.0 / WL 132, LBL 27.50 / WL 112, BL 0.0 / WL 112, BL 0.0 / WL 134, RBL 9.50 / WL103, RBL 9.50 / WL110, RBL 9.50 / WL127, RBL 18.00 / WL110, RBL 27.50 / WL101 AND RBL 27.50 / WL111. REPAIRED CRACKS IN REAR PRES
- [SDR VNAA2017010900006](https://openairdocs.org/sdr/VNAA2017010900006.md): Beam · leaking · Jan 9, 2017 · N202PS · Cndair CL6002B19 · Fuselage Main, Structure
  > LOUD HIGH PRESSURE HISS EMINATING FROM FRONT LEFT SIDE OF COCKPIT. RESEALED LEFT WINDSHIELD I-BEAM.
- [SDR VNAA2016092400027](https://openairdocs.org/sdr/VNAA2016092400027.md): Light · peeling · Sep 24, 2016 · N202PS · Cndair CL6002B19 · Emergency Lighting
  > EMERGENCY LIGHT STRIP AT ROW 1D PEELING UP. MAINTENANCE INSPECTED, R & R THE LIGHT STRIP COVER AT ROW 1D AND PERFORMED CHECKS IAW THE AMM. THE ACFT WAS RELEASED FOR SERVICE.
- [SDR VNAA2016061200018](https://openairdocs.org/sdr/VNAA2016061200018.md): Shutoff Valve · malfunctioned · Jun 12, 2016 · N202PS · Cndair CL6002B19 · Pneumatic Distribution System
  > RIGHT BLEED AIR SHUTOFF VALVE FAILED TO OPEN. THE CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED, AND PERFORMED OPS CHECKS IAW THE AMM. THE ACFT WAS RELEASED FOR SERVICE.
- [SDR VNAA2015102100014](https://openairdocs.org/sdr/VNAA2015102100014.md): Control Panel · failed · Oct 21, 2015 · N202PS · Cndair CL6002B19 · AC Generation System
  > CREW REPORTED AIR DRIVEN GENERATOR INADVERTENTLY DEPLOYED DURING TAKEOFF ROTATION. CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, R & R AIR DRIVEN GENERATOR AUTO DEPLOYMENT CONTROL PANEL AND PERFORMED CHECKS IAW AMM. ACFT RELEA
- [SDR VNAA2015081800030](https://openairdocs.org/sdr/VNAA2015081800030.md): Battery Pack · failed · Aug 18, 2015 · N202PS · Cndair CL6002B19 · Emergency Lighting
  > PRIOR TO FIRST FLIGHT OF THE DAY, CREW REPORTED THE FOLLOWING EMERGENCY LIGHTS INOPERATIVE: FLOOR LEVEL AFT OF ROW 5, LT OVERWING EXIT, TOP, RT OVERWING EXIT, LOWER, AFT 2 LT EXTERIOR OVERWING EXIT LIGHTS AND AFT 2 RT EXTERIOR OVERWING EXIT LIGHTS. MAINTENANCE
- [SDR VNAA2015081800029](https://openairdocs.org/sdr/VNAA2015081800029.md): Battery Pack · failed · Aug 18, 2015 · N202PS · Cndair CL6002B19 · Emergency Lighting
  > PRIOR TO FIRST FLIGHT OF THE DAY, CREW REPORTED THE FOLLOWING EMERGENCY LIGHTS INOPERATIVE: FLOOR LEVEL AFT OF ROW FIVE, LEFT OVERWING EXIT - TOP, RT OVERWING EXIT - LOWER, AFT 2 LT EXTERIOR OVERWING EXIT LIGHTS AND AFT 2 RT EXTERIOR OVERWING EXIT LIGHTS. MAI
- [SDR VNAA2015051000013](https://openairdocs.org/sdr/VNAA2015051000013.md): Engine · fluctuates · May 10, 2015 · N202PS · Cndair CL6002B19 · Engine (Turbine/Turboprop)
  > CREW REPORTED RT ENGINE N1 FLUCTUATING FROM 80.8 TO 93.0 IN CLIMB AT FL190. CREW LANDED AT DESTINATION AIRPORT WITHOUT INCIDENT. MAINTENANCE INSPECTED AND DEFERRED ENGINE SPEED CONTROL SYS IAW MINIMUM EQUIPMENT LIST, MEL. ACFT RELEASED FOR SERVICE.
- [SDR VNAA2014070500004](https://openairdocs.org/sdr/VNAA2014070500004.md): Control Unit · failed · Jul 5, 2014 · N202PS · Cndair CL6002B19 · Trailing Edge Flap Control System
  > CREW REPORTED FLAPS FAIL AMBER MESSAGE AT FLAPS 8 DEGREES AFTER TAKEOFF. FLAPS WOULD NOT RETRACT TO ZERO DEGREES. CREW DECLARED EMERGENCY, RETURNED TO FIELD AND LANDED SAFELY. MAINTENANCE TROUBLESHOT FLAP SYS, R & R FLAP ELECTRONIC CONTROL UNIT, FECU, AND PER
- [SDR VNAA2014062000019](https://openairdocs.org/sdr/VNAA2014062000019.md): Feeder Cable · damaged · Jun 20, 2014 · N202PS · Cndair CL6002B19 · Engine Indicating System Wiring
  > CREW REPORTED LT ENGINE SURGING AT MAXIMUM CLIMB THRUST (MCT) 86.0 TO 91.0 PERCENT N1 AND LT ENGINE FUEL FLOW SURGE 2,300-2,500 AT MCT. NO SURGE BELOW 76 PERCENT N1. CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT LT ENGINE SPEED C
- [SDR VNAA2014050200004](https://openairdocs.org/sdr/VNAA2014050200004.md): Sensor · failed · May 2, 2014 · N202PS · Cndair CL6002B19 · Fuel Controlling System
  > CREW REPORTED LT N1 PLUS OR MINUS 5 PERCENT UNCOMMANDED POWER ADJUSTMENTS DURING FLIGHT, N1, ITT, N2 AND FUEL FLOW ALL UNCOMMANDED MOVEMENT. UNABLE TO SET AND MAINTAIN POWER SETTING AT HIGHER SETTING. NO ISSUES AT IDLE. CREW RETURNED TO FIELD AND LANDED WIT
- [SDR VNAA2014030800008](https://openairdocs.org/sdr/VNAA2014030800008.md): Connector · dirty · Mar 8, 2014 · N202PS · Cndair CL6002B19 · Light System Wiring
  > CREW REPORTED LIGHTS ON WITH EMERGENCY LIGHT SWITCH IN ARM POSITION. MAINTENANCE INSPECTED, CLEANED CONNECTOR AND PERFORMED CHECKS IAW AMM. AIRCRAFT RELEASED FOR SERVICE.
- [SDR VNAA2014030200003](https://openairdocs.org/sdr/VNAA2014030200003.md): Skin · cracked · Mar 2, 2014 · N202PS · Cndair CL6002B19 · Cargo/Baggage Doors
  > DURING SCHEDULED MAINTENANCE, THE INTERIOR SKIN OF THE CARGO DOOR WAS FOUND CRACKED FORWARD SIDE OF HANDLE CUTOUT. THE AREA WAS INSPECTED AND REPAIRED USING AMM. AIRCRAFT WAS RELEASED FOR SERVICE.
- [SDR VNAA2014030200002](https://openairdocs.org/sdr/VNAA2014030200002.md): Stringer · cracked · Mar 2, 2014 · N202PS · Cndair CL6002B19 · Fuselage Main, Longeron/Stringer
  > DURING SCHEDULED MAINTENANCE, BS 379.0 AT STRINGER 3L WAS FOUND CRACKED WHERE IT CONNECTS TO THE PASSENGER DOOR UPPER SILL. THE AREA WAS INSPECTED AND REPAIRED USING AMM. AIRCRAFT WAS RELEASED FOR SERVICE.
- [SDR VNAA2014030200001](https://openairdocs.org/sdr/VNAA2014030200001.md): Bulkhead · chafed · Mar 2, 2014 · N202PS · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > DURING SCHEDULED MAINTENANCE, THE BS 621 PRESSURE BULKHEAD WAS FOUND CHAFED AT BL 0.0 AFT FACE ZEE MEMBER. THE AREA WAS INSPECTED AND REPAIRED USING AMM. AIRCRAFT WAS RELEASED FOR SERVICE.
- [SDR VNAA2013092200009](https://openairdocs.org/sdr/VNAA2013092200009.md): Battery Pack · failed · Sep 22, 2013 · N202PS · Cndair CL6002B19 · Emergency Lighting
  > CREW REPORTED EMERGENCY LIGHT STRIP ON RT SIDE, FROM SEAT 2D TO 5D, WILL NOT LIGHT UP. MX INSPECTED, R & R NR 2 EMERGENCY LIGHT BATTERY AND INVERTER AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.
- [SDR VNAA2013072000018](https://openairdocs.org/sdr/VNAA2013072000018.md): Fuel Control · failed · Jul 20, 2013 · N202PS · Cndair CL6002B19 · Fuel Control/Turbine Engines
  > CREW REPORTED RT ENGINE WOULD NOT PRODUCE TAKEOFF THRUST AT TAKEOFF ROLL. ABORTED TAKEOFF AND RETURNED TO GATE. MX TROUBLESHOT, R & R RT ENGINE FUEL CONTROL AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.
- [SDR VNAA2013060300001](https://openairdocs.org/sdr/VNAA2013060300001.md): Position Sensor · failed · Jun 3, 2013 · N202PS · Cndair CL6002B19 · Trailing Flap Position Indicating System
  > CREW REPORTED FLAPS DEGRADED MESSAGE IN FLIGHT AND THAT LEFT FLAP INDICATES ZERO TO 20 DEGREES WITH CONTROLLABILITY ISSUE. AIRCRAFT PITCH REFLECTED MOVEMENT. CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED, REMOVED AND REPLACED LEF
- [SDR VNAA2013020800006](https://openairdocs.org/sdr/VNAA2013020800006.md): Pressure Switch · defective · Feb 8, 2013 · N202PS · Cndair CL6002B19 · Air Intake Anti/De-Ice System
  > CREW REPORTED LEFT COWL ANTI-ICE CAS MESSAGE AFTER TAKEOFF WITH ANTI-ICE SELECTED OFF. CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT USING FIM (FAULT ISOLATION MANUAL), REMOVED AND REPLACED LEFT ENGINE COWL ANTI-ICE PRESSURE SWI
- [SDR VNAA2012103100016](https://openairdocs.org/sdr/VNAA2012103100016.md): Bulkhead · cracked · Oct 31, 2012 · N202PS · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > DURING SCHEDULED MAINTENANCE FOUND FS 202.75 PRESSURE BULKHEAD WEB CRACKED AROUND THE PARKING BRAKE CUTOUT. FS 202.75 PRESSURE BULKHEAD WEB AT THE PARKING BRAKE CUTOUT WAS INSPECTED AND REPAIRED USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED FOR S
- [SDR VNAA2012103100015](https://openairdocs.org/sdr/VNAA2012103100015.md): Bulkhead · cracked · Oct 31, 2012 · N202PS · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > DURING SCHEDULED MAINTENANCE THE REAR PRESSURE BULKHEAD WEB INDICATED CRACKED. THE REAR PRESSURE BULKHEAD WAS INSPECTED AND REPAIRED USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.
- [SDR VNAA2012090500003](https://openairdocs.org/sdr/VNAA2012090500003.md): Trim System · disconnected · Sep 5, 2012 · N202PS · Cndair CL6002B19 · Stabilizer Control System
  > DURING INITIAL CLIMB, CREW REPORTED STAB TRIM DISCONNECTED TWICE AND WAS RESET. AUTOPILOT SELF-CANCELLED AFTER 30 SECONDS OPERATION AND WOULD NOT STAY ON. WHILE ON, YOKE MOVED FRONT AND BACK IN VIBRATING PATTERN IN SMOOTH AIR. LOW FREQUENCY VIBRATION OF TAI
- [SDR VNAA2012082600015](https://openairdocs.org/sdr/VNAA2012082600015.md): Wire Harness · defective · Aug 21, 2012 · N202PS · Cndair CL6002B19 · Landing Gear System Wiring
  > CREW REPORTED THE LANDING GEAR WAS SLOW TO RETRACT. AIRCRAFT RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, REMOVED, AND REPLACED THE NOSE LANDING GEAR HARNESS USING AIRCRAFT MAINTENANCE MANUALS. OPERATIONAL CHECKS WERE ACCOMPLISHED
- [SDR VNAA2012070800008](https://openairdocs.org/sdr/VNAA2012070800008.md): Control Lever · failed · Jul 8, 2012 · N202PS · Cndair CL6002B19 · Trailing Edge Flap Control System
  > CREW REPORTED FLAPS FAIL AT 30 DEGREES WHILE COMING IN TO LAND. CREW LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE TROUBLESHOT FLAP SYSTEM, REMOVED AND REPLACED FLAP CONTROL LEVER AND PERFORMED CHECKS USING FIM. AIRCRAFT RELEASED FOR SERVICE.
- [SDR VNAA2012051400013](https://openairdocs.org/sdr/VNAA2012051400013.md): Computer · malfunctioned · May 14, 2012 · N202PS · Cndair CL6002B19 · Fuel Indicating System
  > CREW REPORTED FUEL CHANNEL 1/2 FAIL CAUTION MESSAGE IN FLIGHT FOR A FEW MINUTES, THEN MESSAGE DISAPPEARED. CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT AIRCRAFT, REMOVED AND REPLACED FUEL QUANTITY GAUGE COMPUTER AND PERFORMED C
- [SDR VNAA2012050400005](https://openairdocs.org/sdr/VNAA2012050400005.md): Light · inoperative · May 4, 2012 · N202PS · Cndair CL6002B19 · Emergency Lighting
  > CREW REPORTED EMERGENCY LIGHT STRIP ON FLOOR AT ROW 5D INOPERATIVE. MAINTENANCE INSPECTED, RE-INSTALLED ROW 5D EMERGENCY FLOOR LIGHT STRIP AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUAL. AIRCRAFT RELEASED FOR SERVICE.
- [SDR VNAA2012041200006](https://openairdocs.org/sdr/VNAA2012041200006.md): Circuit Breaker · tripped · Apr 12, 2012 · N202PS · Cndair CL6002B19 · Door Warning System
  > CREW REPORTED PASSENGER DOOR CAS MESSAGE, SERVICE DOOR MESSAGE AND CARGO DOOR MESSAGE ALL CAME ON AT 15,000 FEET ON CLIMBOUT. CREW RETURNED TO FIELD AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED, RESET A POPPED CIRCUIT BREAKER AND PERFORMED CHEC
- [SDR VNAA2012040800005](https://openairdocs.org/sdr/VNAA2012040800005.md): Light · inoperative · Apr 8, 2012 · N202PS · Cndair CL6002B19 · Emergency Lighting
  > CREW REPORTED FLOOR LEVEL EMERGENCY LIGHTING INOPERATIVE AT SEAT 3D. REMOVED AND REPLACED ROW THREE (3) RIGHT ELECTROLUMINESCENT FLOOR LIGHTING, PERFORMED CHECKS IAW MAINTENANCE MANUAL.
- [SDR VNAA2012011800006](https://openairdocs.org/sdr/VNAA2012011800006.md): B-Nut · loose · Jan 14, 2012 · N202PS · Cndair CL6002B19 · Hydraulic System, Main
  > CREW REPORTED HYD 1 LOW PRESSURE CAS MESSAGE IN FLIGHT EN ROUTE FROM CAK TO PHL. CREW DIVERTED TO PIT AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND TIGHTENED A LOOSE B-NUT ON NUMBER ONE HYDRAULIC SYSTEM PRESSURE MANIFOLD INLET LINE. MAINTENANCE ALS
- [SDR VNAA2011123000016](https://openairdocs.org/sdr/VNAA2011123000016.md): Computer · intermittent · Dec 26, 2011 · N202PS · Cndair CL6002B19 · Fuel Indicating System
  > CREW REPORTED FUEL CHANNEL 1/2 FAIL CAUTION MESSAGE WITH YELLOW DASHED LINES IN ALL FUEL QUANTITY READINGS AFTER DEPARTURE FROM CLT. CREW RETURNED TO CLT AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, REMOVED AND REPLACED FUEL SYSTEM COMPUTER AND PERF
- [SDR VNAA2011120700002](https://openairdocs.org/sdr/VNAA2011120700002.md): Connector · loose · Dec 3, 2011 · N202PS · Cndair CL6002B19 · Light System Wiring
  > AT CLT, CREW REPORTED FLOOR EMERGENCY PATH LIGHTING AT SEAT 5D HAD A LOOSE CONNECTION. MAINTENANCE INSPECTED, SECURED LOOSE CONNECTION AND PERFORMED CHECKS ON EMERGENCY LIGHTS USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT RELEASED FOR SERVICE.
- [SDR VNAA2011112200013](https://openairdocs.org/sdr/VNAA2011112200013.md): Light · disconnected · Nov 16, 2011 · N202PS · Cndair CL6002B19 · Emergency Lighting
  > AT CLT, EMERGENCY FLOOR LIGHT AT ROW 4 NOT ILLUMINATING. MAINTENANCE INSPECTED FLOOR EMERGENCY LIGHTING, FOUND ROW 4 UNPLUGGED AND TRACK COVER LOOSE, REINSTALLED LIGHT STRIP AND COVER AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUAL. AIRCRAFT RELEASED
- [SDR VNAA2011090800002](https://openairdocs.org/sdr/VNAA2011090800002.md): Radome · damaged · Sep 1, 2011 · N202PS · Cndair CL6002B19 · Aerodynamic Fairings
  > CREW REPORTED A LIGHTNING STRIKE IN FLIGHT EN ROUTE FROM CAK TO PHL. AIRCRAFT LANDED IN PHL WITHOUT INCIDENT. MAINTENANCE INSPECTED AIRCRAFT AND REMOVED AND REPLACED RADOME, TAT PROBE, ATC ANTENNA AND STATIC WICKS. DAMAGE (BURN MARKS) WAS REPAIRED ON LEFT A
- [SDR VNAA2011031600010](https://openairdocs.org/sdr/VNAA2011031600010.md): Bulkhead · chafed · Mar 16, 2011 · N202PS · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > DURING SCHEDULED MAINTENANCE CHAFE DAMAGE WAS FOUND ON THE REAR PRESSURE BULKHEAD. THIS WAS FROM THE ISOLATION VALVE. REPAIRS WERE MADE USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RETURNED TO SERVICE.

Next page: https://openairdocs.org/deregistered/N202PS-2023-10-27/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 = 'N202PS' AND deregistration_id = 'N202PS-2023-10-27'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N202PS-2023-10-27/reports

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