# Service difficulty reports: N705PS A list on [N705PS](https://openairdocs.org/aircraft/N705PS.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 4 · 180 reports - [SDR VNAA2026083137](https://openairdocs.org/sdr/VNAA2026083137.md): Seat Track · corroded · Aug 31, 2026 · N705PS · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings > RIGHT SIDE SEAT TRACK HAD CORROSION BTWN BS 613 AND 629. REPLACED THE SEAT TRACK IAW AMM 53-00-49-0400-801-A03. - [SDR VNAA2026083136](https://openairdocs.org/sdr/VNAA2026083136.md): Seat Track · corroded · Aug 31, 2026 · N705PS · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings > RIGHT 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. - [SDR VNAA2026083135](https://openairdocs.org/sdr/VNAA2026083135.md): Seat Track · corroded · Aug 31, 2026 · N705PS · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings > RIGHT 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. - [SDR VNAA2026083134](https://openairdocs.org/sdr/VNAA2026083134.md): Seat Track · corroded · Aug 31, 2026 · N705PS · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings > RIGHT 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). - [SDR VNAA2026083133](https://openairdocs.org/sdr/VNAA2026083133.md): Seat Track · corroded · Aug 31, 2026 · N705PS · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings > RIGHT 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. - [SDR VNAA2026083132](https://openairdocs.org/sdr/VNAA2026083132.md): Seat Track · corroded · Aug 31, 2026 · N705PS · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings > LEFT 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. - [SDR VNAA2026083131](https://openairdocs.org/sdr/VNAA2026083131.md): Seat Track · corroded · Aug 31, 2026 · N705PS · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings > LEFT 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. - [SDR VNAA2026083130](https://openairdocs.org/sdr/VNAA2026083130.md): Seat Track · gouged · Aug 31, 2026 · N705PS · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings > LEFT SIDE SEAT TRACK HAD GOUGE DAMAGE AT BS 708. REPLACED LT SIDE SEAT TRACK IAW AMM 53-00-49-400-801-A03. - [SDR VNAA2026083129](https://openairdocs.org/sdr/VNAA2026083129.md): Seat Track · corroded · Aug 31, 2026 · N705PS · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings > LEFT SIDE SEAT TRACK HAS CORROSION BETWEEN BS 409 AND 421. REPLACED LT SIDE SEAT TRACK IAW AMM 53-00-49-400-801-A03. - [SDR VNAA2026083138](https://openairdocs.org/sdr/VNAA2026083138.md): Rib · cracked · Aug 31, 2026 · N705PS · Cndair CL6002C10 · Fuselage Main, Bulkhead > L/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. - [SDR VNAA2026083128](https://openairdocs.org/sdr/VNAA2026083128.md): Seat Track · corroded · Aug 31, 2026 · N705PS · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings > LBL 9 SEAT TRACK CORRODED BETWEEN BS 501 AND 565. REPLACED LBL 9 SEAT TRACK IAW AMM 53-00-49-400-801-A03. - [SDR VNAA2026083127](https://openairdocs.org/sdr/VNAA2026083127.md): Seat Track · corroded · Aug 31, 2026 · N705PS · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings > RBL 9 SEAT TRACK CORRODED BETWEEN BS 501 AND 565. REPLACED THE SEAT TRACK IAW AMM 53-00-49-400-801-A03. - [SDR VNAA2026083126](https://openairdocs.org/sdr/VNAA2026083126.md): Seat Track · corroded · Aug 31, 2026 · N705PS · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings > LBL 9 SEAT TRACK CORRODED BETWEEN BS 565 AND 693. INSTALLED A NEW SEAT TRACK IAW AMM 53-00-49-400-801-A03. - [SDR VNAA2026083125](https://openairdocs.org/sdr/VNAA2026083125.md): Seat Track · corroded · Aug 31, 2026 · N705PS · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings > RBL 9 SEAT TRACK IS CORRODED BETWEEN BS 565 AND 693. INSTALLED A NEW SEAT TRACK IAW AMM 53-00-49-400-801-A03. - [SDR VNAA2026083124](https://openairdocs.org/sdr/VNAA2026083124.md): Seat Track · corroded · Aug 31, 2026 · N705PS · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings > LBL 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. INS - [SDR VNAA2026083123](https://openairdocs.org/sdr/VNAA2026083123.md): Seat Track · corroded · Aug 31, 2026 · N705PS · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings > RBL 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. - [SDR VNAA2026083122](https://openairdocs.org/sdr/VNAA2026083122.md): Slat Track · worn · Aug 31, 2026 · N705PS · Cndair CL6002C10 · Leading Edge Devices > RIGHT 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 -. - [SDR VNAA2026083121](https://openairdocs.org/sdr/VNAA2026083121.md): Slat Track · worn · Aug 31, 2026 · N705PS · Cndair CL6002C10 · Leading Edge Devices > RIGHT 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 -. - [SDR VNAA2026083120](https://openairdocs.org/sdr/VNAA2026083120.md): Slat Track · worn · Aug 31, 2026 · N705PS · Cndair CL6002C10 · Leading Edge Devices > HN00321750 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. - [SDR VNAA2026083119](https://openairdocs.org/sdr/VNAA2026083119.md): Slat Track · worn · Aug 31, 2026 · N705PS · Cndair CL6002C10 · Leading Edge Devices > LEFT SLAT TRACK 1-1 HAS WEAR IN MULTIPLE LOCATIONS ON SIDES TOP AND BOTTOM SURFACES. - [SDR VNAA2026083118](https://openairdocs.org/sdr/VNAA2026083118.md): Slat Track · worn · Aug 31, 2026 · N705PS · Cndair CL6002C10 · Leading Edge Devices > LEFT 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--. - [SDR VNAA2026083117](https://openairdocs.org/sdr/VNAA2026083117.md): Slat Track · worn · Aug 31, 2026 · N705PS · Cndair CL6002C10 · Leading Edge Devices > LEFT SLAT TRACK 1-3 WORN IN MULTIPLE LOCATIONS ON SIDES TOP AND BOTTOM SURFACES. REPAIRED IAW IAW REO 670-57-42-2543 REV -. - [SDR VNAA2026083139](https://openairdocs.org/sdr/VNAA2026083139.md): Access Panel · gouged · Aug 31, 2026 · N705PS · Cndair CL6002C10 · Passenger/Crew Doors > FOUND GOUGING DAMAGE AROUND 1 EACH FASTENER HOLES ON PANEL 422BT. REPAIRED IAW EA 5452-2026-0701 REV--. - [SDR VNAA2026083116](https://openairdocs.org/sdr/VNAA2026083116.md): Post · corroded · Aug 31, 2026 · N705PS · Cndair CL6002C10 · Fuselage Main, Structure > RIGHT FLIGHT COMPARTMENT ENTRY POST IS CORRODED AT THE BOTTOM. COMPLIED WITH REPAIR IAW SRM 53-11-10-201-006-A01. - [SDR VNAA2026083115](https://openairdocs.org/sdr/VNAA2026083115.md): Post · corroded · Aug 31, 2026 · N705PS · Cndair CL6002C10 · Fuselage Main, Structure > LT COCKPIT ENTRY POST IS CORRODED AT THE BOTTOM. REPAIRED LT FLIGHT COMPARTMRENT ENTRY POST IAW REO 670-53-11-2349 REV.--. - [SDR VNAA2026083114](https://openairdocs.org/sdr/VNAA2026083114.md): Floorbeam · corroded · Aug 31, 2026 · N705PS · Cndair CL6002C10 · Fuselage Main, Floor Beam > FS 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-A01 - [SDR VNAA2026083113](https://openairdocs.org/sdr/VNAA2026083113.md): Floorbeam · corroded · Aug 31, 2026 · N705PS · Cndair CL6002C10 · Fuselage Main, Floor Beam > BS. 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. - [SDR VNAA2026083112](https://openairdocs.org/sdr/VNAA2026083112.md): Floor Support · corroded · Aug 31, 2026 · N705PS · Cndair CL6002C10 · Fuselage Miscellaneous Structure > EVIDENCE 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. - [SDR VNAA2026083111](https://openairdocs.org/sdr/VNAA2026083111.md): Crossbeam · damaged · Aug 31, 2026 · N705PS · Cndair CL6002C10 · Fuselage Main, Structure > ELONGATED HOLE IN THE CROSSBEAM AT BS 549, RBL 27. REPAIRED THE CROSSBEAM IAW REO 670-53--31-1226, REV-. - [SDR VNAA2026083110](https://openairdocs.org/sdr/VNAA2026083110.md): Floorbeam · corroded · Aug 31, 2026 · N705PS · Cndair CL6002C10 · Fuselage Main, Floor Beam > FLOORBEAM 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 - [SDR VNAA2026083109](https://openairdocs.org/sdr/VNAA2026083109.md): Floor Support · corroded · Aug 31, 2026 · N705PS · Cndair CL6002C10 · Fuselage Miscellaneous Structure > RIGHT 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 SH670-32172-5 - [SDR VNAA2026083140](https://openairdocs.org/sdr/VNAA2026083140.md): Skin · corroded · Aug 31, 2026 · N705PS · Cndair CL6002C10 · Passenger/Crew Doors > PAX DOOR INNER SKIN FOUND TO BE CORRODED IN MULTIPLE LOCATIONS. REPLACED THE PAX DOOR INNER SKIN. - [SDR VNAA2026083141](https://openairdocs.org/sdr/VNAA2026083141.md): Web · cracked · Aug 31, 2026 · N705PS · Cndair CL6002C10 · Passenger/Crew Doors > PAX 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. - [SDR VNAA2026083142](https://openairdocs.org/sdr/VNAA2026083142.md): Web · cracked · Aug 31, 2026 · N705PS · Cndair CL6002C10 · Passenger/Crew Doors > PAX 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. - [SDR VNAA2026083108](https://openairdocs.org/sdr/VNAA2026083108.md): Seat Track · damaged · Aug 31, 2026 · N705PS · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings > FOUND 1 EA OVERSIZED HOLE ON RT SIDE SEAT TRACK AT BS 787. REPAIRED IAW REO 670-53-41-867, REV-. - [SDR VNAA2026083143](https://openairdocs.org/sdr/VNAA2026083143.md): Hinge Arm · corroded · Aug 31, 2026 · N705PS · Cndair CL6002C10 · Fluid Service Doors > AFT 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. - [SDR VNAA2026083107](https://openairdocs.org/sdr/VNAA2026083107.md): Floorbeam · corroded · Aug 31, 2026 · N705PS · Cndair CL6002C10 · Fuselage Main, Floor Beam > WHILE 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: -. - [SDR VNAA2026083106](https://openairdocs.org/sdr/VNAA2026083106.md): Floorbeam · corroded · Aug 31, 2026 · N705PS · Cndair CL6002C10 · Fuselage Main, Floor Beam > WHILE 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-- - [SDR VNAA2026083144](https://openairdocs.org/sdr/VNAA2026083144.md): Skin · damaged · Aug 31, 2026 · N705PS · Cndair CL6002C10 · Fuselage Main, Plate/Skin > LIGHTNING 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-. - [SDR VNAA2026083105](https://openairdocs.org/sdr/VNAA2026083105.md): Hinge · damaged · Aug 31, 2026 · N705PS · Cndair CL6002C10 · Fuselage, Door Hinge > REPLACE 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. - [SDR VNAA2026083145](https://openairdocs.org/sdr/VNAA2026083145.md): Hinge · bent · Aug 31, 2026 · N705PS · Cndair CL6002C10 · Nacelle/Pylon, Main Frame > LEFT 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-. - [SDR VNAA2026083104](https://openairdocs.org/sdr/VNAA2026083104.md): Skin · not reported · Aug 31, 2026 · N705PS · Cndair CL6002C10 · Fuselage Main, Plate/Skin > REPAIR 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. - [SDR VNAA2026083146](https://openairdocs.org/sdr/VNAA2026083146.md): Door · cracked · Aug 31, 2026 · N705PS · Cndair CL6002C10 · Passenger/Crew Doors > PASSENGER 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. - [SDR VNAA2026083103](https://openairdocs.org/sdr/VNAA2026083103.md): Flap · no discrepancy · Aug 31, 2026 · N705PS · Cndair CL6002C10 · Trailing Edge Flaps > C/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 PERFORMED - [SDR VNAA2026083102](https://openairdocs.org/sdr/VNAA2026083102.md): Rib · worn · Aug 31, 2026 · N705PS · Cndair CL6002C10 · Trailing Edge Flaps > PERM 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 SERVI - [SDR VNAA2026083147](https://openairdocs.org/sdr/VNAA2026083147.md): Web · corroded · Aug 31, 2026 · N705PS · Cndair CL6002C10 · Fuselage Main, Bulkhead > BS 280 RT WEB IS CORRODED, LBL 9. REPAIRED BS 280 RIGHT LOWER WEB IAW SRM 53-11-10-201-004-A01. - [SDR VNAA2026083101](https://openairdocs.org/sdr/VNAA2026083101.md): Skin · damaged · Aug 31, 2026 · N705PS · Cndair CL6002C10 · Fuselage Main, Plate/Skin > HR00669946 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. - [SDR VNAA2026020811901](https://openairdocs.org/sdr/VNAA2026020811901.md): Compressor · stalled · Feb 4, 2026 · N705PS · Cndair CL6002C10 · Turbine Engine Compressor Section > COMPRESSOR 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. - [SDR VNAA2026012911501](https://openairdocs.org/sdr/VNAA2026012911501.md): Warning Message · false activation · Jan 26, 2026 · N705PS · Cndair CL6002C10 · Central Warning > NLG STEERING INOPERATIVE IN FLIGHT ILLUMINATED. PERFORMED OPS CHECK IAW AMM 32-51-00-710-801-A01. OPS CHECKED GOOD. - [SDR VNAA2025021011101](https://openairdocs.org/sdr/VNAA2025021011101.md): Dcu · faulted · Feb 6, 2025 · N705PS · Cndair CL6002C10 · Central Computers > DCU 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 C Next page: https://openairdocs.org/aircraft/N705PS/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 = 'N705PS' AND registry_match = 'registration' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/aircraft/N705PS/reports --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.