N705PS

Service difficulty reports · 180

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 = 'N705PS' 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 VNAA2024041911101Wire Harness · faultedSTEERING INOP INTO KBNA, WAS TOWED TO GATE FROM RUNWAY / MESSAGE CLEARED AND NWS OPS CHECKS GOOD AT THIS TIME IAW CRJ 700 AMM 32-51-00-710-801-A01. NWS REQUIRES MORE T/S PER MANAGEMENT / REMOVED AND REPLACED LH NLG WOFFW, CENTERED AND LVDT PROOXIMITY- SENSOR HApr 16, 2024 · N705PS · Cndair CL6002C10 · Landing Gear System WiringSDR VNAA2024041711103Actuator · unserviceableNOSE WHEELS STEERING INOP CAUTION MSG IN FLIGHT / INTERROGATED MDC AND FOUND B1 CODE 007462. T/S IAW CRJ 700 FIM 32-52-01-810-803-A0. R/R L/H STEERING ACTUATOR IAW CRJ 700 AMM 32-52-01-000/400-801-A01.OPS CHECK GOOD IAW CRJ 700 AMM 32-51-00-710-801-A01, AMM 32Apr 14, 2024 · N705PS · Cndair CL6002C10 · Steering UnitSDR VNAA2024040911104Controller · faultedSTEERING INOP CAUTION MSG IN FLIGHT / INTERROGATED MDC AND FOUND B1 CODES 007467 AND 007462. SHOT WIRES FROM CONNECTORS MT098P1 AND MT099P1 TO A164P1 AND A164P2 IAW CRJ 700 FIM 32-52-01-810-801/803. WIRES READ GOOD. REMOVED AND REPLACED NWS ECU IAW CRJ 700 AMMApr 8, 2024 · N705PS · Cndair CL6002C10 · Landing Gear Steering SystemSDR VNAA202204051111Controller · failedAFTER DEPARTING ERI, THE CREW RECEIVED CAUTION MESSAGES FOR THE L ANTI-ICE SYSTEM AS WELL AS THE L ENGINE BLEED. THEY WERE CLEAR OF ICING AT THE TIME AS STATED TO BE BY THE QRH. ON ARRIVAL INTO CLT, THEY NEEDED A VMC ARRIVAL TO REMAIN OUT OF ICING AND CLT HAD Apr 2, 2022 · N705PS · Cndair CL6002C10 · Pneumatic Distribution SystemSDR VNAA202203269928Skin · gougedFUSELAGE EXTERNAL SKIN IS GOUGED UNDER TCAS DIRECTIONAL ANTENNA.Mar 28, 2022 · N705PS · Cndair CL6002C10 · Fuselage Structure (General)SDR VNAA202203089928Skin · gougedFUSELAGE EXTERNAL SKIN IS GOUGED UNDER TCAS DIRECTIONAL ANTENNA.Mar 28, 2022 · N705PS · Cndair CL6002C10 · Fuselage Structure (General)SDR VNAA202203269922Seat Track · incorrectWHILE REMOVING LH SIDE SEAT TRACKS, 2 HOLES WERE MISDRILLED AT FS 752.00 AND FS 761.00.Mar 26, 2022 · N705PS · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA202203269920Seat Track · incorrectWHILE REMOVING LH SIDE SEAT TRACKS, 2 HOLES WERE MISDRILLED AT FS 752.00 AND FS 761.00.Mar 26, 2022 · N705PS · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA202203269927Floorbeam · corrodedCORROSION FOUND ON FLOOR BEAM FS 517.00TO FS 581.00 AT LBL 9Mar 26, 2022 · N705PS · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR VNAA202203269926Floorbeam · corrodedCORROSION FOUND ON FLOOR BEAM FS 517.00TO FS 581.00 AT LBL 9Mar 26, 2022 · N705PS · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR VNAA202203269925Floorbeam · corrodedCORROSION FOUND ON FLOOR BEAM FS 517.00TO FS 581.00 AT LBL 9Mar 26, 2022 · N705PS · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR VNAA202203269924Floorbeam · corrodedCORROSION FOUND ON FLOOR BEAM FS 517.00TO FS 581.00 AT LBL 9Mar 26, 2022 · N705PS · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR VNAA202203269923Seat Track · mislocatedWHILE REMOVING LH SIDE SEAT TRACKS, 2 HOLES WERE MISDRILLED AT FS 752.00 AND FS 761.00.Mar 26, 2022 · N705PS · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA202203269919Stringer · corrodedSTGR 26R HAS MULTIPLE SPOTS OF CORROSION BETWEEN FS1024 AND FS1040.Mar 26, 2022 · N705PS · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR VNAA202203269918Frame · corrodedFS 1051 FRAME IS CORODED BETWEEN STGR 25L AND 25R.Mar 26, 2022 · N705PS · Cndair CL6002C10 · Fuselage Main, FrameSDR VNAA202203269917Frame · corrodedFS 1031.00 FRAME IS CORRODED BETWEEN STGR 24L AND STGR 24R.Mar 26, 2022 · N705PS · Cndair CL6002C10 · Fuselage Main, FrameSDR VNAA202203269916Pressure Plate · corrodedCORROSION WAS FOUND AFT AREA OF LH FUSELAGE TO PYLON PRESSURE PAN, FS 1069.75 TO FS 1088.20 ON INSIDE OF LOWER PAN.Mar 26, 2022 · N705PS · Cndair CL6002C10 · Nacelle/Pylon StructureSDR VNAA202203269915Wedge · bentRH INBOARD GROUND SPOILER OUTBOARD AFT CORNER IS BENT.Mar 26, 2022 · N705PS · Cndair CL6002C10 · SpoilersSDR VNAA202203269914Stringer · corrodedSTR 21R IS CORRODED FROM FS 349 TO 364.Mar 26, 2022 · N705PS · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR VNAA202203269913Channel · chafedRH ENGINE LOWER FAN COWL FORWARD EDGE HAS TWO CHAFES.Mar 26, 2022 · N705PS · Cndair CL6002C10 · Engine Cowling SystemSDR VNAA202203269912Skin Panel · corrodedFUSELAGE EXTERNAL SKIN UNDER ANTENNA FOOT PRINT BETWEEN FS501 AND FS517 IS CORRODED.Mar 26, 2022 · N705PS · Cndair CL6002C10 · Fuselage Structure (General)SDR VNAA202203269911Skin · corrodedEXTERNAL SKIN WITHIN FOOT PRINT OF ANTENNA AT STGR 27 FROM FS 409.00 TO FS 421.00 HAS CORROSION.Mar 26, 2022 · N705PS · Cndair CL6002C10 · Fuselage Structure (General)SDR VNAA202203269910Floorbeam · corrodedFOUND CORROSION ON FLOORBEAM LBL 9 AT FS 1031.00.Mar 26, 2022 · N705PS · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR VNAA20220326999Cleat · corrodedSTRINGER 21R CORRODED BETWEEN FS 310.00 AND FS 319.70Mar 26, 2022 · N705PS · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR VNAA20220326998Stringer · corrodedSTRINGER 25R CORRODED BETWEEN FS 280.00 AND FS 319.70.Mar 26, 2022 · N705PS · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR VNAA20220326997Stringer · corrodedSTRINGER 19R CORRODED BETWEEN FS295.00 AND FS310.00.Mar 26, 2022 · N705PS · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR VNAA20220326996Stringer · corrodedSTRINGER 26R IS CORRODED FROM FS 280 TO FS 310.Mar 26, 2022 · N705PS · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR VNAA20220326995Angle · corrodedSUPPORT ANGLE CORRODED ON STGR 27 BETWEEN FS 549.00 AND FS 569.00.Mar 26, 2022 · N705PS · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR VNAA20220326994Skin · dentedR/H INBOARD FLAP UPPER SKIN DENTED.Mar 26, 2022 · N705PS · Cndair CL6002C10 · Wing, Control Surface Attach FittingsSDR VNAA20220326993Bulkhead · crackedF.S. 202.75 BULKHEAD AT LBL 13.77 WEB FOUND AN INDICATION BETWEEN 3RD AND 6TH AND 6TH FASTNER FROM THE BOTTOM APPROX 1.75" LONG OVER 100% FSH FAILED NDT.Mar 26, 2022 · N705PS · Cndair CL6002C10 · Fuselage Structure (General)SDR VNAA20220326992Bulkhead · crackedF.S. 202.75 BULKHEAD AT RBL 13.77 WEB FOUND AN INDICATION BETWEEN 3RD AND 6TH AND 6TH FASTNER FROM THE BOTTOM APPROX 1.75" LONG OVER 100% FSH FAILED NDT.Mar 26, 2022 · N705PS · Cndair CL6002C10 · Fuselage Structure (General)SDR VNAA202108201113Hinge Fitting · damagedDURING ROUTINE OPERATIONS AT DAYTON INTERNATIONAL AIRPORT (DAY) FACILITIES IN DAYTON, OH, MAINTENANCE DISCOVERED GOUGE DAMAGE TO THE LH AILERON HINGE FITTING #2 (P/N CC670-18052-11). THE DAMAGE MEASURES 0.360Ï¿½L X 0.122Ï¿½W X 0.030Ï¿½D. THE LH AILERON HINGE FAug 17, 2021 · N705PS · Cndair CL6002C10 · AileronsSDR VNAA202108201112Hinge Fitting · damagedDURING ROUTINE OPERATIONS AT DAYTON INTERNATIONAL AIRPORT (DAY) FACILITIES IN DAYTON, OH, MAINTENANCE DISCOVERED GOUGE DAMAGE TO THE LH AILERON HINGE FITTING (P/N CC670-18054-3). THE DAMAGE MEASURES 0.302Ï¿½L X 0.232Ï¿½W X 0.0245Ï¿½D. THE LH AILERON HINGE FITTAug 17, 2021 · N705PS · Cndair CL6002C10 · AileronsSDR VNAA2021011299929Hinge · out of limitsFOUND PAX DOOR HINGE (FUSELAGE SIDE) TO BE OUT OF LIMITS OF REO 670-53-21-582.Jan 12, 2021 · N705PS · Cndair CL6002C10 · Fuselage, Door HingeSDR VNAA2021011299928Frame · corrodedFRAME AT FS 295.00 CORRODED BETWEEN STGR 26L ON STGR 26R.Jan 12, 2021 · N705PS · Cndair CL6002C10 · Fuselage Main, FrameSDR VNAA2021011299927Bracket · crackedBRACKET AT FS 1015.00 FOUND TO BE CRACKED LT SIDE FUSELAGE UNDERNEATH CARGO DOOR.Jan 12, 2021 · N705PS · Cndair CL6002C10 · Fuselage Main, Attach FittingsSDR VNAA2021011299926Frame · crackedDURING EVALUATION OF CORROSION OF FS 280 CIRCUMFERENTIAL JOINT FROM STR 25L TO 25R, STR 27 WAS FOUND TO BE CRACKED AT FASTENER HOLE, 2ND HOLE AFT FROM FS 280 JOINT.Jan 12, 2021 · N705PS · Cndair CL6002C10 · Fuselage Main, FrameSDR VNAA2021011299925Bracket · crackedUPON INSTALL DISCOVERED L BRACKET AT WS 340.236 ON THE RT AILERON TO BE CRACKED.Jan 12, 2021 · N705PS · Cndair CL6002C10 · AileronsSDR VNAA2021011299924Intercostal · crackedPAX DOOR INTERCOSTAL DD3 IS CORRODED.Jan 12, 2021 · N705PS · Cndair CL6002C10 · Passenger/Crew DoorsSDR VNAA2021011299923Stiffener · crackedSTIFFENING ANGLE FRAME AT FS 265.00 HAS CORROSION BETWEEN STGR 25L AND 27.Jan 12, 2021 · N705PS · Cndair CL6002C10 · Passenger/Crew DoorsSDR VNAA2021011299922Stiffener · corrodedSTIFFENING ANGLE FRAME AT FS 265.00 HAS CORROSION BETWEEN STGR 25L AND 27.Jan 12, 2021 · N705PS · Cndair CL6002C10 · Fuselage Main, StructureSDR VNAA2021011299921Bracket · corrodedAFT WING TO FUSELAGE FAIRING SUPPORT STRUCTURE AT FS 939, ANGLES CORRODED ON FRAME.Jan 12, 2021 · N705PS · Cndair CL6002C10 · Aerodynamic FairingsSDR VNAA2021011299920Seat Track · corrodedSIDE SEAT RAIL FROM FS 437-565 LT FOUND TO BE CORRODED AND GOUGED.Jan 12, 2021 · N705PS · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA2021011299919Seat Track · corrodedSIDE SEAT RAIL FROM FS 879-923 LT FOUND TO BE CORRODED AND GOUGED.Jan 12, 2021 · N705PS · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA2021011299918Seat Track · corrodedSIDE SEAT RAIL FROM FS 485-565 FOUND TO BE CORRODED AND GOUGED.Jan 12, 2021 · N705PS · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA2021011299917Intercostal · corrodedPAX DOOR INTERCOSTAL AT DD6 CORRODED.Jan 12, 2021 · N705PS · Cndair CL6002C10 · Passenger/Crew DoorsSDR VNAA2021011299916Frame · corrodedFRAME AT FS 863 CORRODED BETWEEN STGR 26R AND STGR 26L.Jan 12, 2021 · N705PS · Cndair CL6002C10 · Fuselage Main, FrameSDR VNAA2021011299915Skin · corrodedPAX DOOR INNER SKIN CORRODED IN SEVERAL LOCATIONS AND GOUGED AT ACCESS PNL LOCATION BETWEEN FS 310 AND FS 349.Jan 12, 2021 · N705PS · Cndair CL6002C10 · Passenger/Crew DoorsSDR VNAA2021011299914Frame · corrodedFRAME AT FS 1088.20M CORRODED BETWEEN STGR 27 AND STGR 25R.Jan 12, 2021 · N705PS · Cndair CL6002C10 · Fuselage Main, FrameSDR VNAA2021011299913Angle · corrodedSERVICE DOOR LOWER SILL ANGLE CORRODED.Jan 12, 2021 · N705PS · Cndair CL6002C10 · Fuselage Miscellaneous Structure
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