N708PS

Service difficulty reports · 108

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 = 'N708PS' 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 VNAA2024101400014Bracket · dentedINBD 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)Oct 14, 2024 · N708PS · Cndair CL6002C10 · Fuselage, Equipment Attach FittingsSDR VNAA2024100300013Skin · dentedFS893.00 - 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.Oct 14, 2024 · N708PS · Cndair CL6002C10 · Fuselage Main, Plate/SkinSDR VNAA202410140014Mount · corrodedINBD 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)Oct 14, 2024 · N708PS · Cndair CL6002C10 · Fuselage, Equipment Attach FittingsSDR VNAA2024100300012Skin · damagedNDT 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. Oct 3, 2024 · N708PS · Cndair CL6002C10 · Vertical Stabilizer, Plate/SkinSDR VNAA2024100300011Skin · crackedRH 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.Oct 3, 2024 · N708PS · Cndair CL6002C10 · Vertical Stabilizer, Plate/SkinSDR VNAA2024100300010Skin · corrodedCORROSION 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 ENGINOct 3, 2024 · N708PS · Cndair CL6002C10 · Fuselage Main, Plate/SkinSDR VNAA202410030009Skin · corrodedCORROSION 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-- DATEOct 3, 2024 · N708PS · Cndair CL6002C10 · Fuselage Main, Plate/SkinSDR VNAA202410030008Skin · scratchedSCRATCHES 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:Oct 3, 2024 · N708PS · Cndair CL6002C10 · Fuselage Main, Plate/SkinSDR VNAA202410080007Skin · damagedFORWARD 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 ACCEPTAOct 2, 2024 · N708PS · Cndair CL6002C10 · Fuselage Main, Plate/SkinSDR VNAA202410020006Access Door · damagedFORWARD 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 2024-09-13Oct 2, 2024 · N708PS · Cndair CL6002C10 · Cargo/Baggage DoorsSDR VNAA202410020005Window Sill · damagedFORWARD 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 Oct 2, 2024 · N708PS · Cndair CL6002C10 · Fuselage Main, StructureSDR VNAA202410020004Window Sill · damagedDESCREPANCY - 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.Oct 2, 2024 · N708PS · Cndair CL6002C10 · Fuselage Main, StructureSDR VNAA202410020003Window Sill · damagedPILOT 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.Oct 2, 2024 · N708PS · Cndair CL6002C10 · Fuselage Main, StructureSDR VNAA202409270002Web · crackedTWO 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 INSTASep 27, 2024 · N708PS · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR VNAA202409270001Duct · gougedRIGHT 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 RSep 27, 2024 · N708PS · Cndair CL6002C10 · Engine (Turbine/Turboprop)SDR VNAA202206161111A/C Pack · odorRT 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 SYSTJun 13, 2022 · N708PS · Cndair CL6002C10 · Cabin Cooling SystemSDR VNAA2021112301111Packing · damagedDEPARTING 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 SAFENov 19, 2021 · N708PS · Cndair CL6002C10 · Nose/Tail Landing Gear Strut/AxleSDR VNAA2021010499918Skin · canningRUDDER SKIN IS OIL CANNING ON LOWER RT CORNER AROUND CUTOUT.Jan 4, 2021 · N708PS · Cndair CL6002C10 · Rudder, Plate/SkinSDR VNAA2021010499917Stringer · corrodedSTR 21 RT HAS AREA OF CORROSION BETWEEN FR AT FS 364.00 AND FR AT FS 379.00.Jan 4, 2021 · N708PS · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR VNAA2021010499916Skin · damagedEXT FUSELAGE SKIN HAS AREAS OF DAMAGE BETWEEN FS 969.00 AND FS 985.00 AND STR 26 LT TO 26 RT.Jan 4, 2021 · N708PS · Cndair CL6002C10 · Fuselage Main, Plate/SkinSDR VNAA2021010499915Stringer · corrodedSTR 27 IS CORRODED BETWEEN FR AT FS 310.00 AND FR AT FS 319.70.Jan 4, 2021 · N708PS · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR VNAA2021010499914Door Sill · corrodedAFT CARGO DOOR SILL IS CORRODED.Jan 4, 2021 · N708PS · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR VNAA2021010499913Door · corrodedPASSENGER DOOR REMOVED FOR NUMEROUS AREAS OF CORROSION ON THE INNER SKIN AND STRUCTURE.Jan 4, 2021 · N708PS · Cndair CL6002C10 · Passenger/Crew DoorsSDR VNAA2021010499912Frame · crackedFRAME AT FS 333.00 BETWEEN STRINGER 1RT AND STRINGER 2RT IS CRACKED.Jan 4, 2021 · N708PS · Cndair CL6002C10 · Fuselage Main, FrameSDR VNAA2021010499911Drag Angle · crackedRT LOWER VERTICAL STAB TO FUSELAGE ATTACHMENT ANGLE BRACKET. HAS EVIDENCE OF A CRACK 1 1/2" LONG ON THE REPAIR DOUBLER.Jan 4, 2021 · N708PS · Cndair CL6002C10 · Fuselage, Stabilizer Attach FittingsSDR VNAA2021010499910Drag Angle · crackedLT LOWER VERTICAL STAB TO FUSELAGE ATTACHMENT ANGLE BRACKET. HAS EVIDENCE OF A CRACK AFT OF THE REPAIR DOUBLER APPROXIMATELY 1" LONG.Jan 4, 2021 · N708PS · Cndair CL6002C10 · Vertical StabilizerSDR VNAA202101049999Frame · corrodedFRAME 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.Jan 4, 2021 · N708PS · Cndair CL6002C10 · Fuselage Main, FrameSDR VNAA202101049998Stringer · corrodedCORROSION LOCATION IS STGR 21RT BEWTEEN FS 319.00 AND FS 349.00.Jan 4, 2021 · N708PS · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR VNAA202101049997Frame · corrodedSTGR 25R FROM FS 280.00 TO FS 333.00 REQS REPLACEMENT DUE TO MULTIPLE AREAS OF OUT OF LIMITS CORROSION.Jan 4, 2021 · N708PS · Cndair CL6002C10 · Fuselage Main, FrameSDR VNAA202101049996Frame · corrodedSTGR 26R FROM FS 280.00 TO FS 333.00 REQS REPLACEMENT DUE TO MULTIPLE AREAS OF OUT OF LIMITS CORROSION.Jan 4, 2021 · N708PS · Cndair CL6002C10 · Fuselage Main, FrameSDR VNAA202101049995Frame · corrodedFRAME AT FS 310.00 IS CORRODED BETWEEN STR 25 LT AND STR 25 RT, FWD SIDE OF FRAME.Jan 4, 2021 · N708PS · Cndair CL6002C10 · Fuselage Main, FrameSDR VNAA202101049994Frame · corrodedFRAME AT FS 319.70 IS CORRODED BETWEEN STR 26 LT AND STR 26 RT, FWD SIDE OF FRAME. REPLACED FRAME.Jan 4, 2021 · N708PS · Cndair CL6002C10 · Fuselage Main, FrameSDR VNAA202101049993Intercostal · corrodedRT INTERCOSTAL CORRODED, LOCATED BETWEEN FR AT FS 349.00 AND FR AT FS 364.00 AND BETWEEN STR 27 AND STR 26 RT.Jan 4, 2021 · N708PS · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR VNAA202101049992Intercostal · corrodedLT 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.Jan 4, 2021 · N708PS · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR VNAA202101049991Stringer · corrodedSTR 20 RT IS CORRODED BETWEEN FR AT FS 295.00 TO FR AT FS 319.00, REPLACED STRINGER.Jan 4, 2021 · N708PS · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR VNAA2020090121101Pin · disconnectedDURING 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.Aug 28, 2020 · N708PS · Cndair CL6002C10 · Light System WiringSDR VNAA2020073111102Battery Pack · dischargedEMERGENCY LIGHT BATTERY IS DEAD. CHARGED EMERGENCY BATTERY WITH A/C POWER FOR 6HRS PER VCMM OPS CHECKS GOODJul 30, 2020 · N708PS · Cndair CL6002C10 · Emergency LightingSDR VNAA2020012301101Window Frame · crackedDURING 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.Jan 20, 2020 · N708PS · Cndair CL6002C10 · Fuselage Main, StructureSDR VNAA2019100511101Cover · unsecureRH OVERWING EMERGENCY EXIT COVER PANEL WILL NOT STAY IN PLACE. STUCK HOOK AND LOOP BACK IN PLACE. PROBLEM DID NOT REOCCUR.Oct 5, 2019 · N708PS · Cndair CL6002C10 · Emergency ExitsSDR VNAA2019072511102Battery · dischargedEMERGENCY 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 TIMEJul 25, 2019 · N708PS · Cndair CL6002C10 · Emergency LightingSDR VNAA2019052899906Angle · crackedWHILE 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 51-42May 28, 2019 · N708PS · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR VNAA2019052899905Stiffener · crackedWHILE 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.May 28, 2019 · N708PS · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR VNAA2019052899904Gusset · corrodedGUSSETS 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.May 28, 2019 · N708PS · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR VNAA2019052899903Bulkhead · corrodedFS 280.00 BULKHEAD LOWER WEBS ARE CORRODED AT LBL 12.0. REPLACED LT LOWER WEB IAW REO 670-53-11-594.May 28, 2019 · N708PS · Cndair CL6002C10 · Fuselage Main, BulkheadSDR VNAA2018092941103Windshield · crackedWHILE 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 Sep 24, 2018 · N708PS · Cndair CL6002C10 · Flight Compartment WindowsSDR VNAA2018072411101A/C Pack · failedAIRCRAFT 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 RJul 24, 2018 · N708PS · Cndair CL6002C10 · Cabin Cooling SystemSDR VNAA2017091911101Light · detachedTHE 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.Sep 19, 2017 · N708PS · Cndair CL6002C10 · Emergency LightingSDR VNAA2017030100001Handle · brokenTHE SERVICE DOOR HANDLE WAS BROKEN OFF. REMOVED AND REPLACED GALLEY SERVICE DOOR ASSIST HANDLE.Mar 1, 2017 · N708PS · Cndair CL6002C10 · Service DoorsSDR VNAA2016101900023Floorbeam · crackedRIGHT BS 280 FLOORBEAM CRACKED. MAINTENANCE PERMORMED A MAJOR REPAIR AND PERFORMED CHECKS IAW THE AMM.Oct 19, 2016 · N708PS · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR VNAA2016101900022Floorbeam · corrodedLEFT BS 280 FLOORBEAM CORRODED. MAINTENANCE PERMORMED A MAJOR REPAIR TO THE FLOORBEAM IAW AMM.Oct 19, 2016 · N708PS · Cndair CL6002C10 · Fuselage Main, Floor Beam
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