N723PS

Service difficulty reports · 60

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Query with SQL
duckdb -csv -c "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"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR VNAA202108091114Detector · unserviceableCREW 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. REMOVEDAug 7, 2021 · N723PS · Cndair CL6002C10 · Trailing Flap Position Indicating SystemSDR VNAA2020110499922Step · crackedPASSENGER DOOR AFT STEP SKIN UPPER CORNER IS CRACKED APPROXIMATELY 3/8" IN LENGTH, REPLACED STEP.Nov 4, 2020 · N723PS · Cndair CL6002C10 · Passenger/Crew DoorsSDR VNAA2020110499921Step · crackedPASSENGER DOOR FWD STEP SKIN UPPER CORNER IS CRACKED APPROXIMATELY 3/8" IN LENGTH, REPLACED STEP.Nov 4, 2020 · N723PS · Cndair CL6002C10 · Passenger/Crew DoorsSDR VNAA2020110499920Frame · crackedFRAME AT FS 333.00 IS CRACKED LOCATED BETWEEN STRINGER 1 RT AND STRINGER 2 RT, REPLACED FRAME.Nov 4, 2020 · N723PS · Cndair CL6002C10 · Fuselage Main, FrameSDR VNAA2020110499919Stringer · corrodedSTRINGER 26 RT CORRODED BETWEEN FS 953.00 & FS 969.00, REPLACED STRINGER.Nov 4, 2020 · N723PS · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR VNAA2020110499918Stringer · corrodedBELLY STRINGER 26 RT IS CORRODED FROM FS 295.00 TO 315.00.Nov 4, 2020 · N723PS · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR VNAA2020110499917Frame · corrodedBOTTOM OF FRAME FS 565.00 IS CORRODED AND FOUND TO BE OUT OF LIMITS.Nov 4, 2020 · N723PS · Cndair CL6002C10 · Fuselage Main, FrameSDR VNAA2020110499916Frame · corrodedBOTTOM OF FRAME FS 549.00 IS CORRODED AND FOUND TO BE OUT OF LIMITS, REPLACED FRAME.Nov 4, 2020 · N723PS · Cndair CL6002C10 · Fuselage Main, FrameSDR VNAA2020110499915Floor Support · corrodedRT CENTER FLOOR SUPPORT (INTERCOSTAL) BETWEEN FS 349 AND FS 364 IS CORRODED. REPLACED FLOOR SUPPORT.Nov 4, 2020 · N723PS · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR VNAA2020022091101Lens · missingGALLEY 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.Feb 19, 2020 · N723PS · Cndair CL6002C10 · Emergency LightingSDR VNAA2019050311101Proximity Sensor · out of rigAFTER 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 May 3, 2019 · N723PS · Cndair CL6002C10 · Landing Gear Position and WarningSDR VNAA2019040499902Crossbeam · corrodedF.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).Apr 4, 2019 · N723PS · Cndair CL6002C10 · Fuselage Main, StructureSDR VNAA2019040499901Bulkhead Web · corrodedLEFT & 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.Apr 4, 2019 · N723PS · Cndair CL6002C10 · Fuselage Main, BulkheadSDR VNAA2018042741101Light · odorBURNING ODOR COMING FROM THE CAPTAIN`S YOKE CHART HOLDER LIGHT ASSY. THE ASSEMBLY WAS REMOVED AND REPLACED. OPS CHECK GOODApr 24, 2018 · N723PS · Cndair CL6002C10 · Flight Compartment LightingSDR VNAA2018012511104A/C Pack · odorRETURNED 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.Jan 25, 2018 · N723PS · Cndair CL6002C10 · Cabin Cooling SystemSDR VNAA2016101600017Crossbeam · crackedLEFT BS 280 CROSSBEAM IS CRACKED AT LBL 9. MAINTENANCE REPAIRED THE CROSSBEAM IAW REO.Oct 16, 2016 · N723PS · Cndair CL6002C10 · Fuselage Main, StructureSDR VNAA2016101400047Crossbeam · crackedLEFT HAND FS 280 CROSSBEAM CRACKED AT LBL9. MAINTENANCE REPAIRED THE CROSSBEAM AND PERFORMED CHECKS IAW THE AMM. THE AIRCRAFT WAS RELEASED FOR SERVICE.Oct 14, 2016 · N723PS · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR VNAA2016012900027Skin · damagedBIRD STRIKE DAMAGE ON CANOPY SKIN, PN CC670-33136-5 FROM BS 241.6 - 247, BL 0 - LBL 11-16. CANOPY SKIN R & R.Jan 29, 2016 · N723PS · Cndair CL6002C10 · Fuselage Main, StructureSDR VNAA2016010100002Warning Message · false activationCREW 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.Jan 1, 2016 · N723PS · Cndair CL6002C10 · Door Warning SystemSDR VNAA2015050800010Striker · corrodedSERVICE 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.May 8, 2015 · N723PS · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR VNAA2015050800009Door Sill · corrodedSERVICE 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.May 8, 2015 · N723PS · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR VNAA2015050800008Floor Support · corrodedFLOOR 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.May 8, 2015 · N723PS · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR VNAA2015050800007Bulkhead Web · corrodedFS 280 LT AND RT BULKHEAD WEBS ARE CORRODED. REPAIRED THE BULKHEAD IAW REO 670-53-11-594, DATED 2011/04/27.May 8, 2015 · N723PS · Cndair CL6002C10 · Fuselage Main, BulkheadSDR VNAA2015050800005Floorbeam · crackedBS 280 LT SIDE OF CROSSBEAM IS CRACKED AT LBL 12.0. REPAIRED CROSSBEAM IAW SRM 53-11-41-205-003-A01.May 8, 2015 · N723PS · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR VNAA2015050800006Floorbeam · corrodedFS 280.00 CROSSBEAM RT SECTION HAS AREAS OF CORROSION ALONG UPPER SURFACE. REPLACE RT CROSSBEAM IAW SRM 53-11-41-201-003-A01.May 8, 2015 · N723PS · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR VNAA2015050800004Bulkhead Web · corrodedFS 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.May 8, 2015 · N723PS · Cndair CL6002C10 · Fuselage Main, BulkheadSDR VNAA2015050800003Floorbeam · corrodedBS 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.May 8, 2015 · N723PS · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR VNAA2015050800002Floorbeam · corrodedBS 280.FORWARD ANGLE HAS CORROSION. R & R ANGLE IAW SRM 51-42-06-001-A01 AND 51-040-11-001-001-A01.May 8, 2015 · N723PS · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR VNAA2014071100005Seal · dislodgedCREW 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 Jul 11, 2014 · N723PS · Cndair CL6002C10 · Passenger/Crew DoorsSDR VNAA2014042900021Sensor · out of adjustCREW 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.Apr 29, 2014 · N723PS · Cndair CL6002C10 · Landing Gear Position and WarningSDR VNAA2014032900025Angle · corrodedDURING SCHEDULED MAINTENANCE, CORROSION WAS FOUND ON J ANGLE, BS 280. REPLACED IAW AMM. ACFT WAS RELEASED FOR SERVICE.Mar 29, 2014 · N723PS · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR VNAA2014032900024Stringer · crackedDURING SCHEDULED MAINTENANCE, BS 202, STRINGER 3L WAS CRACKED. REPAIRED IAW AMM. ACFT WAS RELEASED FOR SERVICE.Mar 29, 2014 · N723PS · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR VNAA2014032900023Stiffener · crackedDURING SCHEDULED MAINTENANCE, BS 202.75 STIFFNER AT RT AND LT BUTTLINE 30 WAS CRACKED. REPAIRED IAW AMM. ACFT WAS RELEASED FOR SERVICE.Mar 29, 2014 · N723PS · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR VNAA2014020400001Engine · contaminatedAT 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 OVERNFeb 4, 2014 · N723PS · Cndair CL6002C10 · Engine (Turbine/Turboprop)SDR VNAA201310200009Control Unit · failedCREW 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.Oct 20, 2013 · N723PS · Cndair CL6002C10 · Landing Gear Steering SystemSDR VNAA2013022700016Sensor · out of adjustCREW 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 FORFeb 27, 2013 · N723PS · Cndair CL6002C10 · Landing Gear Position and WarningSDR VNAA2012022800011Light · inoperativeCREW 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.Feb 22, 2012 · N723PS · Cndair CL6002C10 · Emergency LightingSDR VNAA2011102700028Skin · dentedDURING 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.Oct 27, 2011 · N723PS · Cndair CL6002C10 · Fuselage Main, Plate/SkinSDR VNAA2011102600022Tire · separatedON 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. Oct 20, 2011 · N723PS · Cndair CL6002C10 · TireSDR VNAA2011100400027Warning System · false activationCREW 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 SSep 29, 2011 · N723PS · Cndair CL6002C10 · Drag Control SystemSDR VNAA2011061500014Bleed Air Sys · leakingCREW 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 ANJun 12, 2011 · N723PS · Cndair CL6002C10 · Pneumatic Distribution SystemSDR VNAA2011061500013Isolation Valve · leakingCREW 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 LJun 12, 2011 · N723PS · Cndair CL6002C10 · Pneumatic Distribution SystemSDR VNAA2011053000026Bulkhead · corrodedDURING 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.May 31, 2011 · N723PS · Cndair CL6002C10 · Fuselage Main, BulkheadSDR VNAA2010051400004Proximity Switch · faultyCREW 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 SWMay 10, 2010 · N723PS · Cndair CL6002C10 · Door Warning SystemSDR VNAA2010042200015Light · inoperativeAT 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 WApr 16, 2010 · N723PS · Cndair CL6002C10 · Emergency LightingSDR VNAA2010021000003Shutoff Valve · failedCREW 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 Feb 5, 2010 · N723PS · Cndair CL6002C10 · Air Intake Anti/De-Ice SystemSDR VNAA2009101400005Anti-Skid Sys · malfunctionedCREW 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 MAINOct 13, 2009 · N723PS · Cndair CL6002C10 · Brake Anti-Skid SectionSDR VNAA0808011Valve · malfunctionedCREW 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.Aug 23, 2008 · N723PS · Cndair CL6002C10 · Cabin Pressure Control SystemSDR VNAA0807013Door · openCREW 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 REJul 22, 2008 · N723PS · Cndair CL6002C10 · Service DoorsSDR VNAA0802018Door · openCREW 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. MAINTENFeb 24, 2008 · N723PS · Cndair CL6002C10 · Fuel Storage
Back to N723PS