# Service difficulty reports: N708PS A list on [N708PS](https://openairdocs.org/aircraft/N708PS.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 3 · 108 reports - [SDR VNAA2024101400014](https://openairdocs.org/sdr/VNAA2024101400014.md): Bracket · dented · Oct 14, 2024 · N708PS · Cndair CL6002C10 · Fuselage, Equipment Attach Fittings > INBD FWD MAIN MOUNTING BRACKET ON GALLEY 1 IS CORRODED. COMPLETE: REMOVED AND REPLACED IB FWD GALLEY 1 MOUNT FITTING PER C&D CMM# A668001 25-33-66 PG. 3013 PAR. 2.P.(25),(26) AND PG. 7001 PAR. 2.-A.(3),(4) - [SDR VNAA2024100300013](https://openairdocs.org/sdr/VNAA2024100300013.md): Skin · dented · Oct 14, 2024 · N708PS · Cndair CL6002C10 · Fuselage Main, Plate/Skin > FS893.00 - FS909.00 STRG 5RH - 7RH, 2 EA, EXTERIOR SKIN DENTS. COMPLIED WITH ALL STEPS OF REO 670-53--51-308 REV -- DATED 2024-09-24. AND COMPLIED WITH ALL STEPS OF REO 670-53-51-309 REV --, DATED 2024-10-02. - [SDR VNAA202410140014](https://openairdocs.org/sdr/VNAA202410140014.md): Mount · corroded · Oct 14, 2024 · N708PS · Cndair CL6002C10 · Fuselage, Equipment Attach Fittings > INBD FWD MAIN MOUNTING BRACKET ON GALLEY 1 IS CORRODED. REMOVED AND REPLACED IB FWD GALLEY 1 MOUNT FITTING PER C&D CMM# A668001 25-33-66 PG. 3013 PAR. 2.P.(25),(26) AND PG. 7001 PAR. 2.-A.(3),(4) - [SDR VNAA2024100300012](https://openairdocs.org/sdr/VNAA2024100300012.md): Skin · damaged · Oct 3, 2024 · N708PS · Cndair CL6002C10 · Vertical Stabilizer, Plate/Skin > NDT NOTED DAMAGE AT LH MOST O/B FACE OF TRIM ACTUATOR FITTING ON VERT. STABILIZER NEAR THE FWD AND AFT FASTENERS. BLENDED OUT DAMAGES AT LH MOST O/B FACE OF TRIM ACTUATOR FITTING ON VERT. STABILIZER NEAR THE FWD AND AFT FASTENERS. FOUND WITHIN LIMITS. REF. - [SDR VNAA2024100300011](https://openairdocs.org/sdr/VNAA2024100300011.md): Skin · cracked · Oct 3, 2024 · N708PS · Cndair CL6002C10 · Vertical Stabilizer, Plate/Skin > RH VERTICAL STAB TO FUSELAGE AFT DRAG ANGLE POSSIBLE CRACK. INSTALLED -6 ANGLE DOUBLER AND -8 ANGLE FILLER ON R/H VERTICAL TO FUSELAGE ATTACHMENT AFT DRAG ANGLE REPAIR REF CRJ 700 SRM 55-31-00-201-001-A0. - [SDR VNAA2024100300010](https://openairdocs.org/sdr/VNAA2024100300010.md): Skin · corroded · Oct 3, 2024 · N708PS · Cndair CL6002C10 · Fuselage Main, Plate/Skin > CORROSION NOTED AROUND WATER DRAIN HOLES EXTERNAL SKIN AT APPROX. FS946.00 BETWEEN STRG26L-STRG26R. BLENDED CORROSION ON EXTERNAL SKIN AROUND WATER DRAIN HOLES AT FS946.00 BETWEEN STGR 26L - 26R REF CRJ700 SRM 51-21-06-001-001-A01 AND FOUND ACCEPTABLE TO ENGIN - [SDR VNAA202410030009](https://openairdocs.org/sdr/VNAA202410030009.md): Skin · corroded · Oct 3, 2024 · N708PS · Cndair CL6002C10 · Fuselage Main, Plate/Skin > CORROSION NOTED ON EXTERNAL SKIN AROUND DOME NUT SCREW HOLE FOR R/H196DR BODY FAIRING BETWEEN FS923-FS939. REPAIRED AREA AND COMPLIED WITH ALL STEPS REO 670-53-51-306 REV-- DATE - [SDR VNAA202410030008](https://openairdocs.org/sdr/VNAA202410030008.md): Skin · scratched · Oct 3, 2024 · N708PS · Cndair CL6002C10 · Fuselage Main, Plate/Skin > SCRATCHES NOTED ON EXTERNAL SKIN AT APPROX FS847-FS977 BTWN STRG17L-20L, MATING SURFACE FOR L/H BODY FAIRING 196DL AND 195AL. REPAIRED AREA AND COMPLIED WITH ALL STEPS OF REO 670-53-00-748 REV-- DATED: - [SDR VNAA202410080007](https://openairdocs.org/sdr/VNAA202410080007.md): Skin · damaged · Oct 2, 2024 · N708PS · Cndair CL6002C10 · Fuselage Main, Plate/Skin > FORWARD BAGGAGE BAY DOOR SURROUND STRUCTURE INNER SKIN HAS CORROSION AROUND FASTENERS IN MULTIPLE AREAS FS533.00 - 581.00 STGR 26L - 25L. REMOVED CORROSION ON FWD BAGGAGE BAY DOOR SURROUND STRUCTURE, INNER SKIN REF SRM 51-21-06-001-001-A01 AND FOUND ACCEPTA - [SDR VNAA202410020006](https://openairdocs.org/sdr/VNAA202410020006.md): Access Door · damaged · Oct 2, 2024 · N708PS · Cndair CL6002C10 · Cargo/Baggage Doors > FORWARD BAGGAGE BAY DOOR SURROUND STRUCTURE - JOINT PLATE FS581.00 STGR26L - 25L HAS EDGE DAMAGE TO THE FORWARD OUTBOARD CORNER. REPAIRED JOINT PLATE AND MISSED DRILLED HOLE AT FS 581 REF REO 670-53-31-931 REV -- DATED 2024-09-13 - [SDR VNAA202410020005](https://openairdocs.org/sdr/VNAA202410020005.md): Window Sill · damaged · Oct 2, 2024 · N708PS · Cndair CL6002C10 · Fuselage Main, Structure > FORWARD BAGGAGE BAY SURROUND STRUCTURE - BOTH JOINT PLATES HAVE LIGHT CORROSION IN MULTIPLE AREAS, FS533.00 & FS581.00 STGR26L -25L. REMOVED CORROSION ON JOINT PLATE AT FS533 AND BETWEEN STGR 25L AND 26L. REF. SRM 51-21-06-001-001-A01 AND FOUND ACCEPTABLE - [SDR VNAA202410020004](https://openairdocs.org/sdr/VNAA202410020004.md): Window Sill · damaged · Oct 2, 2024 · N708PS · Cndair CL6002C10 · Fuselage Main, Structure > DESCREPANCY - CO-PILOT WINDSHIELD LOWER SILL HAS 2EA AREA OF STRIKE DAMAGE. BLEND OUT CO-PILOT WINDSHIELD LOWER SILL STRIKE DAMAGE REF CRJ 700 SRM 51-12-00-001-001-A01 AND FOUND ACCEPTABLE TO ENGINEERING REF REO 670-53-11-2005 REV -- 2024-08-22. - [SDR VNAA202410020003](https://openairdocs.org/sdr/VNAA202410020003.md): Window Sill · damaged · Oct 2, 2024 · N708PS · Cndair CL6002C10 · Fuselage Main, Structure > PILOT WINDSHIELD LOWER SILL HAS 1EA AREA OF STRIKE DAMAGE. BLENDED OUT PILOT WINDSHIELD LOWER SILL STRIKE DAMAGE REF CRJ 700 SRM 51-12-00-001-001-A01 AND FOUND ACCEPTABLE TO ENGINEERING REF REO 670-53-11-2005 REV --, DATED 2024-08-22. - [SDR VNAA202409270002](https://openairdocs.org/sdr/VNAA202409270002.md): Web · cracked · Sep 27, 2024 · N708PS · Cndair CL6002C10 · Fuselage Miscellaneous Structure > TWO SMALL DENTS WITH CRACKS IN FLIGHT DECK FLOOR WEB BETWEEN CO-PILOT'S INBOARD AND OUTBOARD SEAT RAILS, COMPLIED WITH ALL THE STEPS OF REO 670-53-11-1989 REV-- DATED 2024-07-18. CUT AWAY DAMAGE SECTION OF COCKPIT FLOOR WEB, FABRICATED, LOCATED AND WET INSTA - [SDR VNAA202409270001](https://openairdocs.org/sdr/VNAA202409270001.md): Duct · gouged · Sep 27, 2024 · N708PS · Cndair CL6002C10 · Engine (Turbine/Turboprop) > RIGHT HAND ENGINE LOWER C-DUCT LEADING EDGE CHAFFED AND GOUGED. COMPLETE: COMPLIED WITH ALL THE STEPS OF REO 670-54-23-1272 REV -- DATED 2024-08-27. ENSURED BLEND OUT WAS PERFORMED TO A SMOOTH CONTOUR, ENSURED COMPLETE DAMAGE REMOVAL, ENSURED DID NOT EXCEED R - [SDR VNAA202206161111](https://openairdocs.org/sdr/VNAA202206161111.md): A/C Pack · odor · Jun 13, 2022 · N708PS · Cndair CL6002C10 · Cabin Cooling System > RT PACK OVERHEAT AND BLOWING SMOKE. REMOVED AND REPLACE ACM IAW CRJ 700 AMM 21-51-08-000/400-801-A01. PERFORMED OPS TEST ON RH AIR CONDITION SYSTEM IAW CRJ700 AMM 21-51-00-710-801-A01 OPS TEST GOOD. PERFORMED LEAK TEST OF THE AIR CONDITIONING DISTRIBUTION SYST - [SDR VNAA2021112301111](https://openairdocs.org/sdr/VNAA2021112301111.md): Packing · damaged · Nov 19, 2021 · N708PS · Cndair CL6002C10 · Nose/Tail Landing Gear Strut/Axle > DEPARTING OUT OF KBHM THE CREW RECEIVED A NOSE GEAR DISAGREE MSG. AFTER THE MSG THEY WERE OVER WEIGHT DID A LOW APPROACH WITH TOWER TO MAKE SURE GEAR WAS DOWN. IT WAS CONFIRMED BY THE TOWER THAT THE LANDING GEAR WAS DOWN AND THEY COULD LAND. AFTER LANDING SAFE - [SDR VNAA2021010499918](https://openairdocs.org/sdr/VNAA2021010499918.md): Skin · canning · Jan 4, 2021 · N708PS · Cndair CL6002C10 · Rudder, Plate/Skin > RUDDER SKIN IS OIL CANNING ON LOWER RT CORNER AROUND CUTOUT. - [SDR VNAA2021010499917](https://openairdocs.org/sdr/VNAA2021010499917.md): Stringer · corroded · Jan 4, 2021 · N708PS · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer > STR 21 RT HAS AREA OF CORROSION BETWEEN FR AT FS 364.00 AND FR AT FS 379.00. - [SDR VNAA2021010499916](https://openairdocs.org/sdr/VNAA2021010499916.md): Skin · damaged · Jan 4, 2021 · N708PS · Cndair CL6002C10 · Fuselage Main, Plate/Skin > EXT FUSELAGE SKIN HAS AREAS OF DAMAGE BETWEEN FS 969.00 AND FS 985.00 AND STR 26 LT TO 26 RT. - [SDR VNAA2021010499915](https://openairdocs.org/sdr/VNAA2021010499915.md): Stringer · corroded · Jan 4, 2021 · N708PS · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer > STR 27 IS CORRODED BETWEEN FR AT FS 310.00 AND FR AT FS 319.70. - [SDR VNAA2021010499914](https://openairdocs.org/sdr/VNAA2021010499914.md): Door Sill · corroded · Jan 4, 2021 · N708PS · Cndair CL6002C10 · Fuselage Miscellaneous Structure > AFT CARGO DOOR SILL IS CORRODED. - [SDR VNAA2021010499913](https://openairdocs.org/sdr/VNAA2021010499913.md): Door · corroded · Jan 4, 2021 · N708PS · Cndair CL6002C10 · Passenger/Crew Doors > PASSENGER DOOR REMOVED FOR NUMEROUS AREAS OF CORROSION ON THE INNER SKIN AND STRUCTURE. - [SDR VNAA2021010499912](https://openairdocs.org/sdr/VNAA2021010499912.md): Frame · cracked · Jan 4, 2021 · N708PS · Cndair CL6002C10 · Fuselage Main, Frame > FRAME AT FS 333.00 BETWEEN STRINGER 1RT AND STRINGER 2RT IS CRACKED. - [SDR VNAA2021010499911](https://openairdocs.org/sdr/VNAA2021010499911.md): Drag Angle · cracked · Jan 4, 2021 · N708PS · Cndair CL6002C10 · Fuselage, Stabilizer Attach Fittings > RT LOWER VERTICAL STAB TO FUSELAGE ATTACHMENT ANGLE BRACKET. HAS EVIDENCE OF A CRACK 1 1/2" LONG ON THE REPAIR DOUBLER. - [SDR VNAA2021010499910](https://openairdocs.org/sdr/VNAA2021010499910.md): Drag Angle · cracked · Jan 4, 2021 · N708PS · Cndair CL6002C10 · Vertical Stabilizer > LT LOWER VERTICAL STAB TO FUSELAGE ATTACHMENT ANGLE BRACKET. HAS EVIDENCE OF A CRACK AFT OF THE REPAIR DOUBLER APPROXIMATELY 1" LONG. - [SDR VNAA202101049999](https://openairdocs.org/sdr/VNAA202101049999.md): Frame · corroded · Jan 4, 2021 · N708PS · Cndair CL6002C10 · Fuselage Main, Frame > FRAME AT FS 310.00 FROM STRINGER 25R TO PRODUCTION SPLICE AT 18R REQUIRES REMOVAL AND INSTALLATION TO FACILITATE OTHER MAINTENANCE, REPAIR OF STRINGERS 20R AND 21R. - [SDR VNAA202101049998](https://openairdocs.org/sdr/VNAA202101049998.md): Stringer · corroded · Jan 4, 2021 · N708PS · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer > CORROSION LOCATION IS STGR 21RT BEWTEEN FS 319.00 AND FS 349.00. - [SDR VNAA202101049997](https://openairdocs.org/sdr/VNAA202101049997.md): Frame · corroded · Jan 4, 2021 · N708PS · Cndair CL6002C10 · Fuselage Main, Frame > STGR 25R FROM FS 280.00 TO FS 333.00 REQS REPLACEMENT DUE TO MULTIPLE AREAS OF OUT OF LIMITS CORROSION. - [SDR VNAA202101049996](https://openairdocs.org/sdr/VNAA202101049996.md): Frame · corroded · Jan 4, 2021 · N708PS · Cndair CL6002C10 · Fuselage Main, Frame > STGR 26R FROM FS 280.00 TO FS 333.00 REQS REPLACEMENT DUE TO MULTIPLE AREAS OF OUT OF LIMITS CORROSION. - [SDR VNAA202101049995](https://openairdocs.org/sdr/VNAA202101049995.md): Frame · corroded · Jan 4, 2021 · N708PS · Cndair CL6002C10 · Fuselage Main, Frame > FRAME AT FS 310.00 IS CORRODED BETWEEN STR 25 LT AND STR 25 RT, FWD SIDE OF FRAME. - [SDR VNAA202101049994](https://openairdocs.org/sdr/VNAA202101049994.md): Frame · corroded · Jan 4, 2021 · N708PS · Cndair CL6002C10 · Fuselage Main, Frame > FRAME AT FS 319.70 IS CORRODED BETWEEN STR 26 LT AND STR 26 RT, FWD SIDE OF FRAME. REPLACED FRAME. - [SDR VNAA202101049993](https://openairdocs.org/sdr/VNAA202101049993.md): Intercostal · corroded · Jan 4, 2021 · N708PS · Cndair CL6002C10 · Fuselage Miscellaneous Structure > RT INTERCOSTAL CORRODED, LOCATED BETWEEN FR AT FS 349.00 AND FR AT FS 364.00 AND BETWEEN STR 27 AND STR 26 RT. - [SDR VNAA202101049992](https://openairdocs.org/sdr/VNAA202101049992.md): Intercostal · corroded · Jan 4, 2021 · N708PS · Cndair CL6002C10 · Fuselage Miscellaneous Structure > LT INTERCOSTAL CORRODED, LOCATED BETWEEN FR AT FS 349.00 AND FR AT FS 364.00 AND BETWEEN STR 27 AND STR 26 LT, REPLACED INTERCOSTAL. - [SDR VNAA202101049991](https://openairdocs.org/sdr/VNAA202101049991.md): Stringer · corroded · Jan 4, 2021 · N708PS · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer > STR 20 RT IS CORRODED BETWEEN FR AT FS 295.00 TO FR AT FS 319.00, REPLACED STRINGER. - [SDR VNAA2020090121101](https://openairdocs.org/sdr/VNAA2020090121101.md): Pin · disconnected · Aug 28, 2020 · N708PS · Cndair CL6002C10 · Light System Wiring > DURING OVERNIGHT MAINTENANCE IT WAS FOUND THE #2 EMERGENCY FLOODLIGHT WAS INOP. MAINTENANCE FOUND THE PINS AT THE LIGHT DISCONNECTED, RESEATED THE PINS AND THE LIGHT OPERATIONS CHECKED GOOD. - [SDR VNAA2020073111102](https://openairdocs.org/sdr/VNAA2020073111102.md): Battery Pack · discharged · Jul 30, 2020 · N708PS · Cndair CL6002C10 · Emergency Lighting > EMERGENCY LIGHT BATTERY IS DEAD. CHARGED EMERGENCY BATTERY WITH A/C POWER FOR 6HRS PER VCMM OPS CHECKS GOOD - [SDR VNAA2020012301101](https://openairdocs.org/sdr/VNAA2020012301101.md): Window Frame · cracked · Jan 20, 2020 · N708PS · Cndair CL6002C10 · Fuselage Main, Structure > DURING REMOVAL OF PILOTS SIDE WINDOW FOUND A CRACK IN THE PRIMARY STRUCTURE OF THE FRAME BETWEEN THE SIDE WINDOW AND WINDSHELD. MX REMOVED AND REPLACED PILOTS SIDE WINDOW POST. - [SDR VNAA2019100511101](https://openairdocs.org/sdr/VNAA2019100511101.md): Cover · unsecure · Oct 5, 2019 · N708PS · Cndair CL6002C10 · Emergency Exits > RH OVERWING EMERGENCY EXIT COVER PANEL WILL NOT STAY IN PLACE. STUCK HOOK AND LOOP BACK IN PLACE. PROBLEM DID NOT REOCCUR. - [SDR VNAA2019072511102](https://openairdocs.org/sdr/VNAA2019072511102.md): Battery · discharged · Jul 25, 2019 · N708PS · Cndair CL6002C10 · Emergency Lighting > EMERGENCY LIGHTS NOT WORKING. REMOVED AND REPLACED #1 AND #2 EMERGENCY POWER SUPPLY UNIT BATTERY P/N AD2013-1A S/N 136305, 79823 OPS CHECK GOOD AT THIS TIME - [SDR VNAA2019052899906](https://openairdocs.org/sdr/VNAA2019052899906.md): Angle · cracked · May 28, 2019 · N708PS · Cndair CL6002C10 · Fuselage Miscellaneous Structure > WHILE WORKING SERVICE BULLETIN FOUND 2EA ANGLES CRACKED AT FS260.00 - FS280.00 LBL9 AND RBL9. REMOVED AND REPLACED CRACKED ANGLES AT FS260-280 LBL9 AND RBL9 WITH NEW ANGLES PART #'S CC670-33199-35 AND CC370-33199-45 IAW SRM 51-40-11-001-001-A01, AND SRM 51-42 - [SDR VNAA2019052899905](https://openairdocs.org/sdr/VNAA2019052899905.md): Stiffener · cracked · May 28, 2019 · N708PS · Cndair CL6002C10 · Fuselage Miscellaneous Structure > WHILE REMOVING L/H INTERCOSTAL, FOUND STIFFNER WAS CRACKED AND NEEDS REPLACED. FS280 LBL 26.00. REMOVED AND REPLACED CRACKED STIFFNER WITH NEW STIFFNER P/N: CC670-34117-1 IAW SRM 51-42-06-001-001-A01. - [SDR VNAA2019052899904](https://openairdocs.org/sdr/VNAA2019052899904.md): Gusset · corroded · May 28, 2019 · N708PS · Cndair CL6002C10 · Fuselage Miscellaneous Structure > GUSSETS AT LBL 9.0 AND RBL 9.0 FS 278.00 ARE CORRODED BEYOND LIMITS. INSTALLED 2EACH GUSSETS AT LBL9 AND RBL9 FS278.00 PART #'S CC670-33467-1 AND CC670-33467-2 IAW SRM 51-42-06-001-001-A01. - [SDR VNAA2019052899903](https://openairdocs.org/sdr/VNAA2019052899903.md): Bulkhead · corroded · May 28, 2019 · N708PS · Cndair CL6002C10 · Fuselage Main, Bulkhead > FS 280.00 BULKHEAD LOWER WEBS ARE CORRODED AT LBL 12.0. REPLACED LT LOWER WEB IAW REO 670-53-11-594. - [SDR VNAA2018092941103](https://openairdocs.org/sdr/VNAA2018092941103.md): Windshield · cracked · Sep 24, 2018 · N708PS · Cndair CL6002C10 · Flight Compartment Windows > WHILE BEING VECTORED TO FINAL THE FIRST OFFICER NOTICED A HAIRLINE CRACK ON HIS WINDSHIELD AND THE CREW DECLARED AN EMERGENCY. THE AIRCRAFT LANDED WITHOUT FURTHUR INCIDENT. THE AIRCRAFT FERRIED TO A MAINTENANCE BASE AND THE FIRST OFFICER WINDSHIELD AND WINDOW - [SDR VNAA2018072411101](https://openairdocs.org/sdr/VNAA2018072411101.md): A/C Pack · failed · Jul 24, 2018 · N708PS · Cndair CL6002C10 · Cabin Cooling System > AIRCRAFT WAS AN ORIGINATOR AND WHILE IT WAS ON THE GATE THE RT PACK FAILED AND THE CABIN FILLED WITH SMOKE. NO PASSENGERS WERE ONBOARD. MAINTENANCE VISUALLY INSPECTED A/C NO EVIDENCE OF FIRE. DEFERRED CABIN TEMP CONTROL SYSTEM AND RT AIRCONDITIONING PACK MX R - [SDR VNAA2017091911101](https://openairdocs.org/sdr/VNAA2017091911101.md): Light · detached · Sep 19, 2017 · N708PS · Cndair CL6002C10 · Emergency Lighting > THE EMERGENCY LIGHT ON THE RIGHT HAND FORWARD BULKHEAD IN FRONT OF THE FIRST CLASS SEATS IS DETACHED FROM THE WALL. FERRIED THE AIRCRAFT TO A MAINTENANCE BASE AND REPLACED THE LIGHT ASSEMBLY. - [SDR VNAA2017030100001](https://openairdocs.org/sdr/VNAA2017030100001.md): Handle · broken · Mar 1, 2017 · N708PS · Cndair CL6002C10 · Service Doors > THE SERVICE DOOR HANDLE WAS BROKEN OFF. REMOVED AND REPLACED GALLEY SERVICE DOOR ASSIST HANDLE. - [SDR VNAA2016101900023](https://openairdocs.org/sdr/VNAA2016101900023.md): Floorbeam · cracked · Oct 19, 2016 · N708PS · Cndair CL6002C10 · Fuselage Main, Floor Beam > RIGHT BS 280 FLOORBEAM CRACKED. MAINTENANCE PERMORMED A MAJOR REPAIR AND PERFORMED CHECKS IAW THE AMM. - [SDR VNAA2016101900022](https://openairdocs.org/sdr/VNAA2016101900022.md): Floorbeam · corroded · Oct 19, 2016 · N708PS · Cndair CL6002C10 · Fuselage Main, Floor Beam > LEFT BS 280 FLOORBEAM CORRODED. MAINTENANCE PERMORMED A MAJOR REPAIR TO THE FLOORBEAM IAW AMM. Next page: https://openairdocs.org/aircraft/N708PS/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 = 'N708PS' AND registry_match = 'registration' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/aircraft/N708PS/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.