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 VNAA2026083137Seat Track · corrodedRIGHT SIDE SEAT TRACK HAD CORROSION BTWN BS 613 AND 629. REPLACED THE SEAT TRACK IAW AMM 53-00-49-0400-801-A03.Aug 31, 2026 · N705PS · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA2026083136Seat Track · corrodedRIGHT SIDE SEAT TRACK BS 669 TO 708 HAD MULTIPLE AREAS OF CORROSION AND MULTIPLE RUSTED FASTENERS. REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801-A03, & 53-00-49-400-801-A03.Aug 31, 2026 · N705PS · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA2026083135Seat Track · corrodedRIGHT SEAT TRACK, BTWN BS 708 & 761 HAD MULTIPLE AREAS OF CORROSION AND RUSTED FASTENERS. REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801-A03, & 53-00-49-400-801-A03.Aug 31, 2026 · N705PS · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA2026083134Seat Track · corrodedRIGHT SEAT TRACK, BS 785 - 863 HAS MULTIPLE AREAS OF CORROSION. INSTALLED A NEW SEAT TRACK FROM BS 785 - 863 IAW AMM 53-00-49-400-801(CONFIGA03).Aug 31, 2026 · N705PS · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA2026083133Seat Track · corrodedRIGHT SIDE SEAT TRACK FROM BS 863 TO 969 HAS MULTI AREAS OF CORROSION. REPLACED RT SIDE SEAT TRACK IAW AMM 53-00-49-400-801-A03.Aug 31, 2026 · N705PS · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA2026083132Seat Track · corrodedLEFT SIDE SEAT TRACK BETWEEN BS 863 AND 969 HAS MULTI AREAS OF CORROSION. INSTALLED NEW LT SIDE SEAT TRACK IAW AMM 53-00-49-000-801-A03 AND 53-00-49-400-801-A03.Aug 31, 2026 · N705PS · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA2026083131Seat Track · corrodedLEFT SIDE SEAT TRACK BETWEEN BS 708 AND 761 HAD MULTIPLE AREAS OF CORROSION. REPLACED LT SIDE SEAT TRACK IAW AMM 53-00-49-000-801-A03 AND 53-00-49-400-801-A03.Aug 31, 2026 · N705PS · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA2026083130Seat Track · gougedLEFT SIDE SEAT TRACK HAD GOUGE DAMAGE AT BS 708. REPLACED LT SIDE SEAT TRACK IAW AMM 53-00-49-400-801-A03.Aug 31, 2026 · N705PS · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA2026083129Seat Track · corrodedLEFT SIDE SEAT TRACK HAS CORROSION BETWEEN BS 409 AND 421. REPLACED LT SIDE SEAT TRACK IAW AMM 53-00-49-400-801-A03.Aug 31, 2026 · N705PS · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA2026083138Rib · crackedL/H WHEEL WELL BATT RIB IS CRACKED. REMOVED AND INSTALLED NEW SERVICEABLE LT SIDE WHEEL WELL BATT RIB LOCATED AT WS 24 IAW SRM 51-42-21-001-001-A01.Aug 31, 2026 · N705PS · Cndair CL6002C10 · Fuselage Main, BulkheadSDR VNAA2026083128Seat Track · corrodedLBL 9 SEAT TRACK CORRODED BETWEEN BS 501 AND 565. REPLACED LBL 9 SEAT TRACK IAW AMM 53-00-49-400-801-A03.Aug 31, 2026 · N705PS · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA2026083127Seat Track · corrodedRBL 9 SEAT TRACK CORRODED BETWEEN BS 501 AND 565. REPLACED THE SEAT TRACK IAW AMM 53-00-49-400-801-A03.Aug 31, 2026 · N705PS · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA2026083126Seat Track · corrodedLBL 9 SEAT TRACK CORRODED BETWEEN BS 565 AND 693. INSTALLED A NEW SEAT TRACK IAW AMM 53-00-49-400-801-A03.Aug 31, 2026 · N705PS · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA2026083125Seat Track · corrodedRBL 9 SEAT TRACK IS CORRODED BETWEEN BS 565 AND 693. INSTALLED A NEW SEAT TRACK IAW AMM 53-00-49-400-801-A03.Aug 31, 2026 · N705PS · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA2026083124Seat Track · corrodedLBL 9 SEAT TRACK CORRODED BETWEEN BS 693 AND 813. UPON FURTHER EVALUATION FOUND SEAT TRACK AT LBL 9 BETWEEN BS 693 AND 813 TO BE OUT OF ALLOWABLE LIMITS DUE TO MULTIPLE LARGE AREAS OF PITTING CORROSION AROUND FASTENER HOLES IAW SRM 53-41-49-101-001-A01. INSAug 31, 2026 · N705PS · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA2026083123Seat Track · corrodedRBL 9 SEAT TRACK CORRODED BETWEEN BS 693 AND 813. REMOVED AND REPLACED RBL 9 SEAT TRACK IAW AMM 53-00-49-000/400-801-A01.Aug 31, 2026 · N705PS · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA2026083122Slat Track · wornRIGHT SLAT TRACK 1-1 HAS WEAR IN MULTIPLE LOCATIONS ON SIDES TOP AND BOTTOM SURFACES. REPAIRED RH SLAT TRACK 1-1 IAW MHIRJ REO 670-57-42-2542 REV -.Aug 31, 2026 · N705PS · Cndair CL6002C10 · Leading Edge DevicesSDR VNAA2026083121Slat Track · wornRIGHT SLAT TRACK 1-2 HAS WEAR IN MULTIPLE LOCATIONS ON SIDES TOP AND BOTTOM SURFACES. PERFORMED A MAJOR REPAIR TO RH SLAT TRACK 1-2 IAW REO 670-57-42-2532 REV -.Aug 31, 2026 · N705PS · Cndair CL6002C10 · Leading Edge DevicesSDR VNAA2026083120Slat Track · wornHN00321750 DISCREPANCY: RH SLAT TRACK 1-3 HAS WEAR IN MULTIPLE LOCATIONS ON SIDES TOP AND BOTTOM SURFACES. CORRECTIVE ACTION: PERFORMED A MAJOR REPAIR TO RH SLAT TRACK 1-3 IAW MHIRJ REO 670-57-42-2540 REV.-- DATED 2026-07-07.Aug 31, 2026 · N705PS · Cndair CL6002C10 · Leading Edge DevicesSDR VNAA2026083119Slat Track · wornLEFT SLAT TRACK 1-1 HAS WEAR IN MULTIPLE LOCATIONS ON SIDES TOP AND BOTTOM SURFACES.Aug 31, 2026 · N705PS · Cndair CL6002C10 · Leading Edge DevicesSDR VNAA2026083118Slat Track · wornLEFT SLAT TRACK 1-2 HAS WEAR IN MULTIPLE LOCATIONS ON SIDES TOP AND BOTTOM SURFACES. REPAIRED BY BLENDING IAW MHIRJ REO 670-57-42-2531 REV--.Aug 31, 2026 · N705PS · Cndair CL6002C10 · Leading Edge DevicesSDR VNAA2026083117Slat Track · wornLEFT SLAT TRACK 1-3 WORN IN MULTIPLE LOCATIONS ON SIDES TOP AND BOTTOM SURFACES. REPAIRED IAW IAW REO 670-57-42-2543 REV -.Aug 31, 2026 · N705PS · Cndair CL6002C10 · Leading Edge DevicesSDR VNAA2026083139Access Panel · gougedFOUND GOUGING DAMAGE AROUND 1 EACH FASTENER HOLES ON PANEL 422BT. REPAIRED IAW EA 5452-2026-0701 REV--.Aug 31, 2026 · N705PS · Cndair CL6002C10 · Passenger/Crew DoorsSDR VNAA2026083116Post · corrodedRIGHT FLIGHT COMPARTMENT ENTRY POST IS CORRODED AT THE BOTTOM. COMPLIED WITH REPAIR IAW SRM 53-11-10-201-006-A01.Aug 31, 2026 · N705PS · Cndair CL6002C10 · Fuselage Main, StructureSDR VNAA2026083115Post · corrodedLT COCKPIT ENTRY POST IS CORRODED AT THE BOTTOM. REPAIRED LT FLIGHT COMPARTMRENT ENTRY POST IAW REO 670-53-11-2349 REV.--.Aug 31, 2026 · N705PS · Cndair CL6002C10 · Fuselage Main, StructureSDR VNAA2026083114Floorbeam · corrodedFS 280 FWD FLOORBEAM ANGLE CORRODED. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01, FOUND J ANGLE TO BE OUT OF LIMITS DUE TO NO LIMITS GIVEN IN SRM. REMOVED THE J ANGLE AT BS 280 BTWN LBL 12 AND RBL 12 IAW SRM 51-42-06-001-001-A01 & SRM 51-42-21-001-001-A01Aug 31, 2026 · N705PS · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR VNAA2026083113Floorbeam · corrodedBS. 280 LT FLOORBEAM WEB IS CORRODED AT LBL9. LOCATED, DRILLED, & INSTALLED FLOORBEAM IAW SRM-51-40-11-001-001-A01, 51-42-06-001-001-A01, 51-42-13-001-001-A01, AND 51-42-22-001-001-A01.Aug 31, 2026 · N705PS · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR VNAA2026083112Floor Support · corrodedEVIDENCE OF CORROSION AT APPROX. BS 645 - 661, LBL 9 ON TOP OF FLOOR SUPPORT UNDER THE CENTER FLOOR PANEL. CUT & REPAIRED THE FLOOR SUPPORT IAW SRM 53-00-41-201-001-A01.Aug 31, 2026 · N705PS · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR VNAA2026083111Crossbeam · damagedELONGATED HOLE IN THE CROSSBEAM AT BS 549, RBL 27. REPAIRED THE CROSSBEAM IAW REO 670-53--31-1226, REV-.Aug 31, 2026 · N705PS · Cndair CL6002C10 · Fuselage Main, StructureSDR VNAA2026083110Floorbeam · corrodedFLOORBEAM ANGLE CORRODED ON AFT SIDE OF BS 280, STR 26R TO STR 26L. BLENDED CORROSION ON 3 AREAS OF THE AVI FLOORBEAM ANGLE IAW SRM 51-21-06-001-001-A01. ON FURTHER EVALUATION, FOUND CORROSION TO BE HEAVILY EXFOILIATED AND IS NEAR FULL MATERIAL LOSS AND IS Aug 31, 2026 · N705PS · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR VNAA2026083109Floor Support · corrodedRIGHT FLOOR SUPPORT CORRODED BETWEEN BS 295 TO 319, INSTALLED A NEW RH FLOOR SUPPORT BTWN BS 295 TO 319 IAW SRM 51-23-00-001-001-A01, 51-42-06-001-001-A01, 51-42-13-001-001-A01, AND 51-42-21-001-001-A01 SH670-32172-5Aug 31, 2026 · N705PS · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR VNAA2026083140Skin · corrodedPAX DOOR INNER SKIN FOUND TO BE CORRODED IN MULTIPLE LOCATIONS. REPLACED THE PAX DOOR INNER SKIN.Aug 31, 2026 · N705PS · Cndair CL6002C10 · Passenger/Crew DoorsSDR VNAA2026083141Web · crackedPAX DOOR FWD WEB FOUND TO BE CRACKED. REMOVED THE PAX DOOR FWD WEB, LOCATED AND DRILLED A NEW FWD WEB AND INSTALLED IAW SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01, & 51-42-13-001-001-A01.Aug 31, 2026 · N705PS · Cndair CL6002C10 · Passenger/Crew DoorsSDR VNAA2026083142Web · crackedPAX DOOR AFT WEB FOUND TO BE CRACKED. REMOVED THE PAX DOOR AFT WEB, LOCATED AND DRILLED PAX DOOR AFT WEB AND INSTALLED IAW SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01, & 51-42-13-001-001-A01.Aug 31, 2026 · N705PS · Cndair CL6002C10 · Passenger/Crew DoorsSDR VNAA2026083108Seat Track · damagedFOUND 1 EA OVERSIZED HOLE ON RT SIDE SEAT TRACK AT BS 787. REPAIRED IAW REO 670-53-41-867, REV-.Aug 31, 2026 · N705PS · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA2026083143Hinge Arm · corrodedAFT LAVATORY SERVICE DOOR 196ER OTBD HINGE ARM CORRODED AND OTBD & INBD HINGE BRACKET ASSEMBIES & ATTACHING HARDWARE ARE CORRODED. INSTALLED A NEW LWR SERVICE ARM AND HARDWARE IAW SRM 52-45-01-000-801-A01 AND AMM 20-51-00-400-801-A01.Aug 31, 2026 · N705PS · Cndair CL6002C10 · Fluid Service DoorsSDR VNAA2026083107Floorbeam · corrodedWHILE INSTALLING AV-DEC TAPE FOUND CORROSION AROUND FASTENER HOLE ON FLOORBEAM LOCATED AT BB 333, RBL9 - RBL42. REPAIRED THE FLOORBEAM UPPER FLANGE IAW REO 670-53-21-2943 REV: -.Aug 31, 2026 · N705PS · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR VNAA2026083106Floorbeam · corrodedWHILE INSTALLING AV-DEC TAPE FOUND 3EA SPOTS OF CORROSION ON FLOORBEAM LOCATED AT BS 333 LBL9 - LBL42. REPAIRED FLOORBEAM UPPER FLANGE IAW REO 670-53-21-2943 REV--Aug 31, 2026 · N705PS · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR VNAA2026083144Skin · damagedLIGHTNING STRIKE DAMAGE TO FUSELAGE SKIN AT F.S.503 AND STRINGER 25R. PERFORMED A MAJOR REPAIR TO FUSELAGE SKIN BETWEEN BS 485 AND 517 AND STR 24R TO STR 26R IAW REO 670-53-31-1216 REV-.Aug 31, 2026 · N705PS · Cndair CL6002C10 · Fuselage Main, Plate/SkinSDR VNAA2026083105Hinge · damagedREPLACE THE PASSENGER DOOR HINGE IAW SRM 53-21-23-201-007-A01. REMOVED AND REPLACED PAX DOOR HINGE IAW SRM 51-25-01-001-001-A01-PSA.Aug 31, 2026 · N705PS · Cndair CL6002C10 · Fuselage, Door HingeSDR VNAA2026083145Hinge · bentLEFT ENGINE COWLING IS UNABLE TO BE OPENED DUE TO A DENTED HINGE LINE THAT WAS BENT UPON ARRIVAL . REPAIRED IAW REO 670-53--31-1226, REV-.Aug 31, 2026 · N705PS · Cndair CL6002C10 · Nacelle/Pylon, Main FrameSDR VNAA2026083104Skin · not reportedREPAIR TO FUSE SKIN BTWN FS501-517, STR15-17R. IAW REO 670-53-31-156. INSPECTION OF REPAIR AT RT FUSELAGE BS 501 & 517, STR 15-17R. PERFORMED PERMANENT REPAIR IAW REO 670-53-31-1221 REV-, & DWG SH670-33162.Aug 31, 2026 · N705PS · Cndair CL6002C10 · Fuselage Main, Plate/SkinSDR VNAA2026083146Door · crackedPASSENGER DOOR AFT BOTTOM CORNER FOUND TO BE CRACKED. REQUIRES REPLACEMENT. REMOVED AND INSTALLED NEW SERVICEABLE PASSENGER DOOR AFT BOTTOM CORNER IAW SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01.Aug 31, 2026 · N705PS · Cndair CL6002C10 · Passenger/Crew DoorsSDR VNAA2026083103Flap · no discrepancyC/W INSPECTION OF REPAIR ON INBOARD FLAP IAW REO670-57-52-009 EVERY 40000 CYCLES (DTA INSPECTION)) C/W INSPECTIONOF REPAIR ON INBOARD FLAP IAW REO 670-57-52-009 EVERY 40000CYCLES (DTA INSPECTION). PERFORMED NDT INSPECTIONS TO PREVIOUS REPAIR AREA AND PERFORMEDAug 31, 2026 · N705PS · Cndair CL6002C10 · Trailing Edge FlapsSDR VNAA2026083102Rib · wornPERM REPAIR - BLENDED WEAR DAMAGE ON OTBD FLAP BUTE DOOR CAM AND RIB FITTING AT FLAP STA 296.073, LT TEMPORARY DISPOSITION:THE SUBJECT CONDITION IS STRUCTURALLY ACCEPTABLE FOR 8000 FLT HOURS FROM TIME OFINCORPORATION OF THIS REO AT REV -. INSTALLED NEW SERVIAug 31, 2026 · N705PS · Cndair CL6002C10 · Trailing Edge FlapsSDR VNAA2026083147Web · corrodedBS 280 RT WEB IS CORRODED, LBL 9. REPAIRED BS 280 RIGHT LOWER WEB IAW SRM 53-11-10-201-004-A01.Aug 31, 2026 · N705PS · Cndair CL6002C10 · Fuselage Main, BulkheadSDR VNAA2026083101Skin · damagedHR00669946 LIGHTNING STRIKE DAMAGE REQUIRES PERMANENT REPAIR BETWEEN FS 319.70 AND 349.00, AND STGR 26L - STGR 26R. CORRECTIVE ACTION: REPAIRED LIGHTNING STRIKE DAMAGE IAW MHIRJ REO 670-53-21-2904 REV-- DATED 2026-06-18.Aug 31, 2026 · N705PS · Cndair CL6002C10 · Fuselage Main, Plate/SkinSDR VNAA2026020811901Compressor · stalledCOMPRESSOR STALL AT ROTATION RT ENGINE. REMOVED & REPLACED RT ENGINE ASSEMBLY IAW AMM 71-00-00-400-801-A02-PSA. OPS & LEAK CHECK GOOD AT THIS TIME.Feb 4, 2026 · N705PS · Cndair CL6002C10 · Turbine Engine Compressor SectionSDR VNAA2026012911501Warning Message · false activationNLG STEERING INOPERATIVE IN FLIGHT ILLUMINATED. PERFORMED OPS CHECK IAW AMM 32-51-00-710-801-A01. OPS CHECKED GOOD.Jan 26, 2026 · N705PS · Cndair CL6002C10 · Central WarningSDR VNAA2025021011101Dcu · faultedDCU 1 SWITCH LIGHT CAME ON WITH NO ASSOCIATED MSG WITH BURNING SMELL IN COCKPIT. THERE WAS NO MEDICAL ATTENTION REPORTED. / PERFORMED FDE INSPECTION FOR ABNORMAL SMELL IN COCKPIT PER CRJ700 FIM FDE 21-22-00-810-806-A01. NO ABNORMAL SMELL NOTED. PERFORMED OPS CFeb 6, 2025 · N705PS · Cndair CL6002C10 · Central Computers
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