# Service difficulty reports: N723PS

A list on [N723PS](https://openairdocs.org/aircraft/N723PS.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 · 60 reports

- [SDR VNAA202108091114](https://openairdocs.org/sdr/VNAA202108091114.md): Detector · unserviceable · Aug 7, 2021 · N723PS · Cndair CL6002C10 · Trailing Flap Position Indicating System
  > CREW RECEIVED A FLAPS FAIL CAUTION MESSAGE IN CRUISE, FLAPS INDICATED 0. THEY DECLARED EMERGENCY FOR A FLAPS 0 LANDING AND POSSIBLE BRAKES OVERHEAT AND LANDED WITHOUT FURTHER INCIDENT. FLAPS HALFSPEED S MSG / INTERROGATED MDC AND FOUND B1 CODE: 241338. REMOVED
- [SDR VNAA2020110499922](https://openairdocs.org/sdr/VNAA2020110499922.md): Step · cracked · Nov 4, 2020 · N723PS · Cndair CL6002C10 · Passenger/Crew Doors
  > PASSENGER DOOR AFT STEP SKIN UPPER CORNER IS CRACKED APPROXIMATELY 3/8" IN LENGTH, REPLACED STEP.
- [SDR VNAA2020110499921](https://openairdocs.org/sdr/VNAA2020110499921.md): Step · cracked · Nov 4, 2020 · N723PS · Cndair CL6002C10 · Passenger/Crew Doors
  > PASSENGER DOOR FWD STEP SKIN UPPER CORNER IS CRACKED APPROXIMATELY 3/8" IN LENGTH, REPLACED STEP.
- [SDR VNAA2020110499920](https://openairdocs.org/sdr/VNAA2020110499920.md): Frame · cracked · Nov 4, 2020 · N723PS · Cndair CL6002C10 · Fuselage Main, Frame
  > FRAME AT FS 333.00 IS CRACKED LOCATED BETWEEN STRINGER 1 RT AND STRINGER 2 RT, REPLACED FRAME.
- [SDR VNAA2020110499919](https://openairdocs.org/sdr/VNAA2020110499919.md): Stringer · corroded · Nov 4, 2020 · N723PS · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > STRINGER 26 RT CORRODED BETWEEN FS 953.00 & FS 969.00, REPLACED STRINGER.
- [SDR VNAA2020110499918](https://openairdocs.org/sdr/VNAA2020110499918.md): Stringer · corroded · Nov 4, 2020 · N723PS · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > BELLY STRINGER 26 RT IS CORRODED FROM FS 295.00 TO 315.00.
- [SDR VNAA2020110499917](https://openairdocs.org/sdr/VNAA2020110499917.md): Frame · corroded · Nov 4, 2020 · N723PS · Cndair CL6002C10 · Fuselage Main, Frame
  > BOTTOM OF FRAME FS 565.00 IS CORRODED AND FOUND TO BE OUT OF LIMITS.
- [SDR VNAA2020110499916](https://openairdocs.org/sdr/VNAA2020110499916.md): Frame · corroded · Nov 4, 2020 · N723PS · Cndair CL6002C10 · Fuselage Main, Frame
  > BOTTOM OF FRAME FS 549.00 IS CORRODED AND FOUND TO BE OUT OF LIMITS, REPLACED FRAME.
- [SDR VNAA2020110499915](https://openairdocs.org/sdr/VNAA2020110499915.md): Floor Support · corroded · Nov 4, 2020 · N723PS · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > RT CENTER FLOOR SUPPORT (INTERCOSTAL) BETWEEN FS 349 AND FS 364 IS CORRODED. REPLACED FLOOR SUPPORT.
- [SDR VNAA2020022091101](https://openairdocs.org/sdr/VNAA2020022091101.md): Lens · missing · Feb 19, 2020 · N723PS · Cndair CL6002C10 · Emergency Lighting
  > GALLEY LOWER EMERGENCY LIGHT COVER MISSING. ENTERED ON NEF CLASS 1. REPLACED MISSING LENS ON GALLEY LOWER EMERGENCY LIGHT IAW CRJ 700 AMM. OPS CHECK GOOD. CLEARED NEF.
- [SDR VNAA2019050311101](https://openairdocs.org/sdr/VNAA2019050311101.md): Proximity Sensor · out of rig · May 3, 2019 · N723PS · Cndair CL6002C10 · Landing Gear Position and Warning
  > AFTER TAKEOFF FROM LEX THE CREW RECEIVED A GEAR DISAGREE WARNING MESSAGE. THEY RAN THE QRH WHICH INSTRUCTED THEM TO LAND AT THE NEAREST SUITABLE AIRPORT. THEY RETURNED THE AIRCRAFT TO LEX WHERE ATC DECLARED AN EMERGENCY FOR THEM AND THE FLIGHT LANDED WITHOUT
- [SDR VNAA2019040499902](https://openairdocs.org/sdr/VNAA2019040499902.md): Crossbeam · corroded · Apr 4, 2019 · N723PS · Cndair CL6002C10 · Fuselage Main, Structure
  > F.S. 280 CROSSBEAM HAS CORROSION ON TOP OF CROSSBEAM AT RBL 9 & LBL 9. CORRECTIVE ACTION: REPAIRED THE F.S. 280 IAW BBD SERVICE BULLETIN 670BA-53-041 REV F (REINFORCEMENT OF THE FS 280 SEMI-PRESSURE BULKHEAD).
- [SDR VNAA2019040499901](https://openairdocs.org/sdr/VNAA2019040499901.md): Bulkhead Web · corroded · Apr 4, 2019 · N723PS · Cndair CL6002C10 · Fuselage Main, Bulkhead
  > LEFT & RIGHT HAND F.S. 280 BULKHEAD WEBS CORRODED. CORRECTIVE ACTION: REPAIRED THE F.S. 280 LH/RH BULKHEAD WEBS IAW BBD REO 670-53-11-594 REV A.
- [SDR VNAA2018042741101](https://openairdocs.org/sdr/VNAA2018042741101.md): Light · odor · Apr 24, 2018 · N723PS · Cndair CL6002C10 · Flight Compartment Lighting
  > BURNING ODOR COMING FROM THE CAPTAIN`S YOKE CHART HOLDER LIGHT ASSY. THE ASSEMBLY WAS REMOVED AND REPLACED. OPS CHECK GOOD
- [SDR VNAA2018012511104](https://openairdocs.org/sdr/VNAA2018012511104.md): A/C Pack · odor · Jan 25, 2018 · N723PS · Cndair CL6002C10 · Cabin Cooling System
  > RETURNED TO THE GATE IN ORD DUE TO LT PACK FAIL MSG AND SMOKE IN THE COCKPIT. MX INSPECTED AND VERIFIED NO SMOKE IN COCKPIT WITH LT PACK SELECTED OFF. DEFERRED LT PACK.
- [SDR VNAA2016101600017](https://openairdocs.org/sdr/VNAA2016101600017.md): Crossbeam · cracked · Oct 16, 2016 · N723PS · Cndair CL6002C10 · Fuselage Main, Structure
  > LEFT BS 280 CROSSBEAM IS CRACKED AT LBL 9. MAINTENANCE REPAIRED THE CROSSBEAM IAW REO.
- [SDR VNAA2016101400047](https://openairdocs.org/sdr/VNAA2016101400047.md): Crossbeam · cracked · Oct 14, 2016 · N723PS · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > LEFT HAND FS 280 CROSSBEAM CRACKED AT LBL9. MAINTENANCE REPAIRED THE CROSSBEAM AND PERFORMED CHECKS IAW THE AMM. THE AIRCRAFT WAS RELEASED FOR SERVICE.
- [SDR VNAA2016012900027](https://openairdocs.org/sdr/VNAA2016012900027.md): Skin · damaged · Jan 29, 2016 · N723PS · Cndair CL6002C10 · Fuselage Main, Structure
  > BIRD STRIKE DAMAGE ON CANOPY SKIN, PN CC670-33136-5 FROM BS 241.6 - 247, BL 0 - LBL 11-16. CANOPY SKIN R & R.
- [SDR VNAA2016010100002](https://openairdocs.org/sdr/VNAA2016010100002.md): Warning Message · false activation · Jan 1, 2016 · N723PS · Cndair CL6002C10 · Door Warning System
  > CREW REPORTED AFT CARGO DOOR CAUTION MESSAGE IN FLIGHT. CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE PERFORMED OPS CHECK OF AFT CARGO DOOR IAW AMM. NO DEFECTS NOTED. ACFT RELEASED FOR SERVICE.
- [SDR VNAA2015050800010](https://openairdocs.org/sdr/VNAA2015050800010.md): Striker · corroded · May 8, 2015 · N723PS · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > SERVICE DOOR LOWER SEAL STRIKER CORRODED AROUND MULTIPLE FASTENER HOLES. REPLACED SERVICE DOOR LOWER SEAL STRIKER, PN SH670-31412-7 IAW SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01.
- [SDR VNAA2015050800009](https://openairdocs.org/sdr/VNAA2015050800009.md): Door Sill · corroded · May 8, 2015 · N723PS · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > SERVICE DOOR SILL CORRODED AROUND FWD FITTING. INSTALLED A NEW SERVICABLE SERVICE DOOR SILL IAW SRM 51-42-06-001-001-A01 AND 51-40-11-001-001-A01.
- [SDR VNAA2015050800008](https://openairdocs.org/sdr/VNAA2015050800008.md): Floor Support · corroded · May 8, 2015 · N723PS · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > FLOOR SUPPORT JUST AFT OF BS 280 IS CORRODED. INSTALLED A NEW SERVICABLE FLOOR SUPPORT IAW SRM 51-42-06-001-001-A01, 51-42-21-001-A01 AND 51-42-13-001-A01.
- [SDR VNAA2015050800007](https://openairdocs.org/sdr/VNAA2015050800007.md): Bulkhead Web · corroded · May 8, 2015 · N723PS · Cndair CL6002C10 · Fuselage Main, Bulkhead
  > FS 280 LT AND RT BULKHEAD WEBS ARE CORRODED. REPAIRED THE BULKHEAD IAW REO 670-53-11-594, DATED 2011/04/27.
- [SDR VNAA2015050800005](https://openairdocs.org/sdr/VNAA2015050800005.md): Floorbeam · cracked · May 8, 2015 · N723PS · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > BS 280 LT SIDE OF CROSSBEAM IS CRACKED AT LBL 12.0. REPAIRED CROSSBEAM IAW SRM 53-11-41-205-003-A01.
- [SDR VNAA2015050800006](https://openairdocs.org/sdr/VNAA2015050800006.md): Floorbeam · corroded · May 8, 2015 · N723PS · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > FS 280.00 CROSSBEAM RT SECTION HAS AREAS OF CORROSION ALONG UPPER SURFACE. REPLACE RT CROSSBEAM IAW SRM 53-11-41-201-003-A01.
- [SDR VNAA2015050800004](https://openairdocs.org/sdr/VNAA2015050800004.md): Bulkhead Web · corroded · May 8, 2015 · N723PS · Cndair CL6002C10 · Fuselage Main, Bulkhead
  > FS 280 LT AND RT LOWER BULKHEAD WEBS HAVE CORROSION. COMPLIED WITH REPAIR TO LT AND RT LOWER BULKHEAD AT FS 280, REO 670-53-11-594.
- [SDR VNAA2015050800003](https://openairdocs.org/sdr/VNAA2015050800003.md): Floorbeam · corroded · May 8, 2015 · N723PS · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > BS 280, LBL 12 ANGLE HAS CORROSION. R & R IAW SRM 51-42-06-001-001-A01, 51-42-13-001-001-A01 AND 51-40-11-001-001-A01.
- [SDR VNAA2015050800002](https://openairdocs.org/sdr/VNAA2015050800002.md): Floorbeam · corroded · May 8, 2015 · N723PS · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > BS 280.FORWARD ANGLE HAS CORROSION. R & R ANGLE IAW SRM 51-42-06-001-A01 AND 51-040-11-001-001-A01.
- [SDR VNAA2014071100005](https://openairdocs.org/sdr/VNAA2014071100005.md): Seal · dislodged · Jul 11, 2014 · N723PS · Cndair CL6002C10 · Passenger/Crew Doors
  > CREW REPORTED MAIN CABIN DOOR DEVELOPED A LEAK IN UPPER RT CORNER WHILE CLIMBING THROUGH FL270. CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND FOUND SEAL DISLODGED FROM CHANNEL. MAINTENANCE REINSTALLED, CLEANED AND LUBED SEAL
- [SDR VNAA2014042900021](https://openairdocs.org/sdr/VNAA2014042900021.md): Sensor · out of adjust · Apr 29, 2014 · N723PS · Cndair CL6002C10 · Landing Gear Position and Warning
  > CREW REPORTED GEAR DISAGREE MESSAGE ON TAKEOFF. NOSEWHEEL WOULD NOT RETRACT. CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, ADJUSTED NLG UPLOCK SENSOR AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.
- [SDR VNAA2014032900025](https://openairdocs.org/sdr/VNAA2014032900025.md): Angle · corroded · Mar 29, 2014 · N723PS · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > DURING SCHEDULED MAINTENANCE, CORROSION WAS FOUND ON J ANGLE, BS 280. REPLACED IAW AMM. ACFT WAS RELEASED FOR SERVICE.
- [SDR VNAA2014032900024](https://openairdocs.org/sdr/VNAA2014032900024.md): Stringer · cracked · Mar 29, 2014 · N723PS · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > DURING SCHEDULED MAINTENANCE, BS 202, STRINGER 3L WAS CRACKED. REPAIRED IAW AMM. ACFT WAS RELEASED FOR SERVICE.
- [SDR VNAA2014032900023](https://openairdocs.org/sdr/VNAA2014032900023.md): Stiffener · cracked · Mar 29, 2014 · N723PS · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > DURING SCHEDULED MAINTENANCE, BS 202.75 STIFFNER AT RT AND LT BUTTLINE 30 WAS CRACKED. REPAIRED IAW AMM. ACFT WAS RELEASED FOR SERVICE.
- [SDR VNAA2014020400001](https://openairdocs.org/sdr/VNAA2014020400001.md): Engine · contaminated · Feb 4, 2014 · N723PS · Cndair CL6002C10 · Engine (Turbine/Turboprop)
  > AT ROTATION, CREW REPORTED SMOKE LAVATORY WARNING MESSAGE WITH FUMES AND HAZE. CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED ACFT AND FOUND SMOKE AND ODOR COMING FROM PACK DUCTS IN CABIN DUE TO ENGINE WASHES PERFORMED DURING OVERN
- [SDR VNAA201310200009](https://openairdocs.org/sdr/VNAA201310200009.md): Control Unit · failed · Oct 20, 2013 · N723PS · Cndair CL6002C10 · Landing Gear Steering System
  > CREW REPORTED A NOSE WHEEL STEERING CAUTION MESSAGE IN FLIGHT. ACFT LANDED WITHOUT INCIDENT. MX TROUBLESHOT, REMOVED, REPLACED, AND OPS CHECKED THE NOSE WHEEL STEERING ELECTRONIC CONTROL UNIT USING AMM. ACFT WAS RELEASED FOR SERVICE.
- [SDR VNAA2013022700016](https://openairdocs.org/sdr/VNAA2013022700016.md): Sensor · out of adjust · Feb 27, 2013 · N723PS · Cndair CL6002C10 · Landing Gear Position and Warning
  > CREW REPORTED GEAR DISAGREE MESSAGE WHEN RETRACTING GEAR IN FLIGHT. CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, ADJUSTED NOSE LANDING GEAR SENSOR AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT RELEASED FOR
- [SDR VNAA2012022800011](https://openairdocs.org/sdr/VNAA2012022800011.md): Light · inoperative · Feb 22, 2012 · N723PS · Cndair CL6002C10 · Emergency Lighting
  > CREW REPORTED CEILING LEVEL EMERGENCY FLOOD LIGHT ADJACENT TO ROW 13 WOULD NOT ILLUMINATE. MAINTENANCE INSPECTED, RELAMPED EMERGENCY FLOOD LIGHT AT ROW 13 AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT RELEASED FOR SERVICE.
- [SDR VNAA2011102700028](https://openairdocs.org/sdr/VNAA2011102700028.md): Skin · dented · Oct 27, 2011 · N723PS · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > DURING SCHEDULED MAINTENANCE. A DENT WAS FOUND ON SKIN AT FS 234.0 BETWEEN S26-27L. ACFT INSPECTED AND REPAIRED USING MM. ACFT RELEASED FOR SERVICE.
- [SDR VNAA2011102600022](https://openairdocs.org/sdr/VNAA2011102600022.md): Tire · separated · Oct 20, 2011 · N723PS · Cndair CL6002C10 · Tire
  > ON DEPARTURE FROM CLT, CREW HEARD A WHISTLING NOISE AND SUSPECTED AN ACCESS DOOR HAD BEEN LEFT OPEN. CREW RETURNED TO CLT AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AIRCRAFT AND FOUND TREAD HAD COME OFF LEFT NOSE WHEEL TIRE, DAMAGING NOSE GEAR DOOR.
- [SDR VNAA2011100400027](https://openairdocs.org/sdr/VNAA2011100400027.md): Warning System · false activation · Sep 29, 2011 · N723PS · Cndair CL6002C10 · Drag Control System
  > CREW REPORTED OUTBOARD SPOILERONS AND OUTBOARD FLIGHT SPOILERS CAUTION MESSAGES IN FLIGHT ON APPROACH TO CLT. AIRCRAFT LANDED IN CLT WITHOUT INCIDENT. MAINTENANCE PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUAL. NO DEFECTS NOTED. AIRCRAFT RELEASED FOR S
- [SDR VNAA2011061500014](https://openairdocs.org/sdr/VNAA2011061500014.md): Bleed Air Sys · leaking · Jun 12, 2011 · N723PS · Cndair CL6002C10 · Pneumatic Distribution System
  > CREW REPORTED RED BLEED DUCT WARNING MESSAGE. AIRCRAFT RETURNED AND LANDED AT CLT WITHOUT INCIDENT. MAINTENANCE FOUND BLEED AIR LEAKS AND TIGHTENED THESE CONNECTIONS. MAINTENANCE REMOVED AND REPLACED BLEED DET HARNESS 140P2 TO 142P2. ALL TROUBLESHOOTING AN
- [SDR VNAA2011061500013](https://openairdocs.org/sdr/VNAA2011061500013.md): Isolation Valve · leaking · Jun 12, 2011 · N723PS · Cndair CL6002C10 · Pneumatic Distribution System
  > CREW REPORTED RED BLEED DUCT WARNING MESSAGE AT 11000FT. AIRCRAFT LANDED AT CLT WITHOUT INCIDENT. MAINTENANCE FOUND THE ISOLATION VALVE LEAKING HOT AIR. DURING TROUBLESHOOTING THE ISOLATION VALVE WAS REMOVED. THE SAME ISOLATION VALVE WAS RE-INSTALLED AND L
- [SDR VNAA2011053000026](https://openairdocs.org/sdr/VNAA2011053000026.md): Bulkhead · corroded · May 31, 2011 · N723PS · Cndair CL6002C10 · Fuselage Main, Bulkhead
  > DURING SCHEDULED MAINTENANCE CORROSION WAS FOUND AT FS 280.0. THE FS 280.0 LOWER BULKHEAD WEB WAS INSPECTED, REMOVED AND REPLACED USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.
- [SDR VNAA2010051400004](https://openairdocs.org/sdr/VNAA2010051400004.md): Proximity Switch · faulty · May 10, 2010 · N723PS · Cndair CL6002C10 · Door Warning System
  > CREW REPORTED A PASSENGER DOOR MASTER WARNING WITH ASSOCIATED AURAL WARNING AT 600 FEET AGL AFTER TAKEOFF FROM TLH. AIRCRAFT RETURNED TO TLH AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT THE AIRCRAFT, REMOVED AND REPLACED A PASSENGER DOOR PROXIMITY SW
- [SDR VNAA2010042200015](https://openairdocs.org/sdr/VNAA2010042200015.md): Light · inoperative · Apr 16, 2010 · N723PS · Cndair CL6002C10 · Emergency Lighting
  > AT CLT, CREW REPORTED THE OVERHEAD CEILING EMERGENCY LIGHT BY ROW SEVEN (7) TO BE INOPERATIVE. MAINTENANCE TROUBLESHOT, REMOVED AND REPLACED THE OVERHEAD EMERGENCY LIGHT AT SEAT SEVEN (7) AND PERFORMED CHECKS USING THE AIRCRAFT MAINTENANCE MANUAL. AIRCRAFT W
- [SDR VNAA2010021000003](https://openairdocs.org/sdr/VNAA2010021000003.md): Shutoff Valve · failed · Feb 5, 2010 · N723PS · Cndair CL6002C10 · Air Intake Anti/De-Ice System
  > CREW REPORTED A RIGHT ENGINE BLEED AMBER CAS MESSAGE IN ICING CONDITIONS AFTER DEPARTURE FROM CLT. AIRCRAFT RETURNED TO CLT AND LANDED WITHOUT INCIDENT. USING THE AIRCRAFT MAINTENANCE MANUAL, MAINTENANCE TROUBLESHOT THE AIRCRAFT AND REMOVED AND REPLACED THE
- [SDR VNAA2009101400005](https://openairdocs.org/sdr/VNAA2009101400005.md): Anti-Skid Sys · malfunctioned · Oct 13, 2009 · N723PS · Cndair CL6002C10 · Brake Anti-Skid Section
  > CREW REPORTED LT INBOARD BRAKE WAS OVERHEATED. AIRCRAFT RETURNED TO SDF AND LANDED WITHOUT INCIDENT. MAINTENANCE USED AIRCRAFT MAINTENANCE MANUAL TO TROUBLESHOOT. MAINTENANCE REMOVED AND REPLACED THE ANTI SKID UNIT. CHECKS WERE MADE USING THE AIRCRAFT MAIN
- [SDR VNAA0808011](https://openairdocs.org/sdr/VNAA0808011.md): Valve · malfunctioned · Aug 23, 2008 · N723PS · Cndair CL6002C10 · Cabin Pressure Control System
  > CREW REPORTED ACFT WOULD NOT MAINTAIN PRESSURE. CREW ELECTED TO RETURN TO DTW AND LANDED WITHOUT INCIDENT. MX INSPECTED ACFT AND SECURED CLOSED GROUND VALVE. NO OTHER DEFECTS WERE NOTED AND ACFT WAS RELEASED FOR SERVICE.
- [SDR VNAA0807013](https://openairdocs.org/sdr/VNAA0807013.md): Door · open · Jul 22, 2008 · N723PS · Cndair CL6002C10 · Service Doors
  > CREW REPORTED HIGH PITCHED NOISE IN FLIGHT AFTER TAKEOFF. CREW ELECTED TO RETURN TO CLT LANDING WITHOUT INCIDENT. MAINTENANCE INSPECTED AND FOUND THE MAINTENANCE SERVICE DOOR OPEN. MAINTENANCE INSPECTED AND SECURED THE DOOR WITH NO DEFECTS. AIRCRAFT WAS RE
- [SDR VNAA0802018](https://openairdocs.org/sdr/VNAA0802018.md): Door · open · Feb 24, 2008 · N723PS · Cndair CL6002C10 · Fuel Storage
  > CREW REPORTED A LOUD BANGING NOISE IN FLIGHT. CREW ELECTED TO RETURN TO BHM AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND FOUND REFUEL DOOR OPEN AND CAP MISSING. MAINTENANCE FOUND NO EVIDENCE OF ENGINE INGESTION OR OTHER STRUCTURAL DAMAGE. MAINTEN

Next page: https://openairdocs.org/aircraft/N723PS/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 = 'N723PS' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N723PS/reports

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