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.
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
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
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)SDR 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.SDR 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)SDR 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. SDR 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.SDR 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 ENGINSDR 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-- DATESDR 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:SDR 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 ACCEPTASDR 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 2024-09-13SDR 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 SDR 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.SDR 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.SDR 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 INSTASDR 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 RSDR 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 SYSTSDR 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 SAFESDR VNAA2021010499918Skin · canningRUDDER SKIN IS OIL CANNING ON LOWER RT CORNER AROUND CUTOUT.SDR VNAA2021010499917Stringer · corrodedSTR 21 RT HAS AREA OF CORROSION BETWEEN FR AT FS 364.00 AND FR AT FS 379.00.SDR VNAA2021010499916Skin · damagedEXT FUSELAGE SKIN HAS AREAS OF DAMAGE BETWEEN FS 969.00 AND FS 985.00 AND STR 26 LT TO 26 RT.SDR VNAA2021010499915Stringer · corrodedSTR 27 IS CORRODED BETWEEN FR AT FS 310.00 AND FR AT FS 319.70.SDR VNAA2021010499914Door Sill · corrodedAFT CARGO DOOR SILL IS CORRODED.SDR VNAA2021010499913Door · corrodedPASSENGER DOOR REMOVED FOR NUMEROUS AREAS OF CORROSION ON THE INNER SKIN AND STRUCTURE.SDR VNAA2021010499912Frame · crackedFRAME AT FS 333.00 BETWEEN STRINGER 1RT AND STRINGER 2RT IS CRACKED.SDR VNAA2021010499911Drag Angle · crackedRT LOWER VERTICAL STAB TO FUSELAGE ATTACHMENT ANGLE BRACKET. HAS EVIDENCE OF A CRACK 1 1/2" LONG ON THE REPAIR DOUBLER.SDR VNAA2021010499910Drag Angle · crackedLT LOWER VERTICAL STAB TO FUSELAGE ATTACHMENT ANGLE BRACKET. HAS EVIDENCE OF A CRACK AFT OF THE REPAIR DOUBLER APPROXIMATELY 1" LONG.SDR 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.SDR VNAA202101049998Stringer · corrodedCORROSION LOCATION IS STGR 21RT BEWTEEN FS 319.00 AND FS 349.00.SDR VNAA202101049997Frame · corrodedSTGR 25R FROM FS 280.00 TO FS 333.00 REQS REPLACEMENT DUE TO MULTIPLE AREAS OF OUT OF LIMITS CORROSION.SDR VNAA202101049996Frame · corrodedSTGR 26R FROM FS 280.00 TO FS 333.00 REQS REPLACEMENT DUE TO MULTIPLE AREAS OF OUT OF LIMITS CORROSION.SDR VNAA202101049995Frame · corrodedFRAME AT FS 310.00 IS CORRODED BETWEEN STR 25 LT AND STR 25 RT, FWD SIDE OF FRAME.SDR VNAA202101049994Frame · corrodedFRAME AT FS 319.70 IS CORRODED BETWEEN STR 26 LT AND STR 26 RT, FWD SIDE OF FRAME. REPLACED FRAME.SDR 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.SDR 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.SDR VNAA202101049991Stringer · corrodedSTR 20 RT IS CORRODED BETWEEN FR AT FS 295.00 TO FR AT FS 319.00, REPLACED STRINGER.SDR 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.SDR VNAA2020073111102Battery Pack · dischargedEMERGENCY LIGHT BATTERY IS DEAD. CHARGED EMERGENCY BATTERY WITH A/C POWER FOR 6HRS PER VCMM OPS CHECKS GOODSDR 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.SDR VNAA2019100511101Cover · unsecureRH OVERWING EMERGENCY EXIT COVER PANEL WILL NOT STAY IN PLACE. STUCK HOOK AND LOOP BACK IN PLACE. PROBLEM DID NOT REOCCUR.SDR 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 TIMESDR 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 51-42SDR 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.SDR 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.SDR VNAA2019052899903Bulkhead · corrodedFS 280.00 BULKHEAD LOWER WEBS ARE CORRODED AT LBL 12.0. REPLACED LT LOWER WEB IAW REO 670-53-11-594.SDR 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 SDR 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 RSDR 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.SDR VNAA2017030100001Handle · brokenTHE SERVICE DOOR HANDLE WAS BROKEN OFF. REMOVED AND REPLACED GALLEY SERVICE DOOR ASSIST HANDLE.SDR VNAA2016101900023Floorbeam · crackedRIGHT BS 280 FLOORBEAM CRACKED. MAINTENANCE PERMORMED A MAJOR REPAIR AND PERFORMED CHECKS IAW THE AMM.SDR VNAA2016101900022Floorbeam · corrodedLEFT BS 280 FLOORBEAM CORRODED. MAINTENANCE PERMORMED A MAJOR REPAIR TO THE FLOORBEAM IAW AMM.
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