N207PS

Service difficulty reports · 160

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 = 'N207PS' 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 SWIA202163709None · corrodedFS 605 FRAME IS CORRODED IN ARES FROM STR 24L AND 23R ON BOTH UPPER AND LOWER FLANGES (C-CHECK RO 1/5/2022) INSTALLED NEW FRAME SECTION PN: 601R36026-27 AT F.S 605 BETWEEN STGR 20L & 20R IAW CRJ 200 SRM 51-42-06. COMPLETED TASK CARD 51-900-1003-SKY ANDOct 24, 2021 · N207PS · Cndair CL6002B19 · Fuselage Main, FrameSDR SWIA202163708None · corrodedBEAM I/B FLANGES AT LBL9 FROM FS 484.00 TO FS 559.00 HAVE MULTIPLE AREAS OF CORROSION. (C-CHECK RO 1/5/2022) REPAIRED BEAM I/B FLANGES AT LBL9 FROM FS 484.00 TO FS 559.00 IAW MHIRJ REO 601R-53-41-2987 REV -- DATED 2021-12-06. COMPLIED WITH SKYCARD 51-Oct 24, 2021 · N207PS · Cndair CL6002B19 · Fuselage Main, FrameSDR SWIA202163707None · corrodedBEAM I/B AND O/B FLANGES AT RBL9 FROM FS 439.00 TO FS 559.00 HAVE MULTIPLE AREAS OF CORROSION. (C-CHECK RO 1/5/2022) REPAIRED BEAM I/B AND O/B FLANGES AT RBL9 FROM FS 439.00 TO FS 559.00 IAW MHIRJ REO 601R-53-41-2985 REV -- DATED 2021-11-29. COMPLIEOct 24, 2021 · N207PS · Cndair CL6002B19 · Fuselage Main, FrameSDR SWIA202163706None · corrodedRBL 9 CABIN FLOOR BEAM IB AND OB FLANGES HAVE AREAS OF CORROSION BETWEEN FS 559+48 TO FS 559+99 (C-CHECK RO 1/5/2022) REMOVED AND REPLACED FLOORBEAM CAP AT RBL 9 BETWEEN FS 559+48 TO FS 559+99 IAW MHIRJ REO 601R-53-51-610 REV -- DATED 2021-11-16 , CRJ Oct 24, 2021 · N207PS · Cndair CL6002B19 · Fuselage Internal Mounting StructureSDR SWIA202163705None · chafedRH WING LWR AFT SKIN IS CHAFED FROM CONTACT WITH MLG FARING AT RBL 45 (C-CHECK RO 1/5/2022) REPAIRED RH WING LWR AFT SKIN IS CHAFED FROM CONTACT WITH MLG FARING AT RBL 45 IAW BOMBARDIER REO 601R-57-21-880 REV D DATED 2017/03/06 AND SKY CARD 51-900-1003Oct 19, 2021 · N207PS · Cndair CL6002B19 · Fuselage Main, FrameSDR SWIA202163746Nut · corrodedRH WING FLIGHT SPOILER AND SPOILERON ACTUATORS LOWER MOUNT BOLT NUTS AND WASHERS ARE CORRODED (C-CHECK RO 1/5/2022) REMOVED AND REPLACED RH FLIGHT SPOILER AND SPOILERON OB + IB ACTUATOR LOWER MOUNT BOLT NUTS AND WASHERS IAW CRJ-200 AMM 27-62-01-000/400Oct 17, 2021 · N207PS · Cndair CL6002B19 · Wing StructureSDR SWIA202163745Bolt · rustedRH WING FLIGHT SPOILER # 1, # 2, #3, AND #4 HINGE MOUNT BOLTS NUTS ARE RUSTED (C-CHECK RO 1/5/2022) REMOVED AND REPLACED RH WING FLIGHT SPOILER #1, #2, #3, AND #4 HINGE MOUNT BOLT NUTS WITH SERVICABLE HARDWARE IAW CRJ 200 AMM 27-64-05-000/400-801Oct 17, 2021 · N207PS · Cndair CL6002B19 · Wing StructureSDR SWIA202163744None · rustedRH WING SPOILERON IB AND OB HINGE POINT BOLT NUTS AND KEEPER BOLTS ARE RUSTED (C-CHECK RO 1/5/2022) REMOVED AND REPLACED ALL RH SPOILERON HINGE BOLT HARDWARE AND KEEPER HARDWARE IAW CRJ-200 AMM 27-64-01-000/400-801. REF ATTACHED CONTINUATION FOR WORK POct 17, 2021 · N207PS · Cndair CL6002B19 · Wing StructureSDR SWIA202163743Nut · rustedLH IB GROUND SPOILER IB AND OB MOUNT BOLT NUTS ARE RUSTED (C-CHECK RO 1/5/2022) REPLACED RUSTED NUTS ON LH IB GROUND SPOILER IB AND OB BOLTS IAW CRJ 200 AMM 27-65-01-400-801Oct 17, 2021 · N207PS · Cndair CL6002B19 · Wing StructureSDR SWIA202163742Nut · rustedLH OB GROUND SPOILER IB AND OB MOUNT BOLT NUTS ARE RUSTED (C-CHECK RO 1/5/2022) REMOVED AND REPLACED IB AND OB MOUNT BOLT NUTS ON THE LH OUTBOARD GROUND SPOILER WITH NEW SERVICEABLE NUTS IAW CRJ 200 AMM 27-65-01-000/400-801. OPS CHECK GOOD AT THIS TIOct 17, 2021 · N207PS · Cndair CL6002B19 · Wing StructureSDR SWIA202163741Nut · rustedLH WING FLIGHT SPOILER # 1, # 2, #3, AND #4 HINGE MOUNT BOLT NUTS ARE RUSTED (C-CHECK RO 1/5/2022) REPLACED LH FLIGHT SPOILER HINGE BOLT NUTS AT HINGE # 1,2,3 AND 4 IAW CRJ 200 AMM 27-64-05-400-801Oct 17, 2021 · N207PS · Cndair CL6002B19 · Wing StructureSDR SWIA202163740None · rustedLH WING SPOILERON #1, # 2, AND # 4 HINGE MOUNT BOLT NUTS ARE RUSTED AND # 1 AND # 4 HINGE BOLT KEEPER BOLTS ARE ALSO RUSTED (C-CHECK RO 1/5/2022) REMOVED AND REPLACED ALL CORRODED HARDWARE ON LH SPOILERON HINGE POINTS IAW CRJ-200 AMM 27-64-01-000/400-Oct 17, 2021 · N207PS · Cndair CL6002B19 · Wing StructureSDR SWIA202163739None · rustedR/H AILERON BOLT RETAINING PLATES (ALL OF THEM ) ,HAVE THERE BOLTS RUSTED. (C-CHECK RO 1/5/2022) REMOVED CORRODED BOLTS WASHERS AND NUTS FROM AILERON BOLT RETAINING PLATES AND INSTALLED SERVICABLE BOLTS WASHERS AND NUTS ON AILERON BOLT RETAINING PLATESOct 15, 2021 · N207PS · Cndair CL6002B19 · Wing StructureSDR SWIA202163738Nut · rustedR/H AILERON CENTER HINGE ATTACH BOLTS, BOTH NUTS RUSTED (C-CHECK RO 1/5/2022) INSTALLED NEW NUTS ON CENTER HINGE ATTACH BOLTS OF RH AILERON IAW CRJ 200 AMM 27-15-01-400-801 STEPS 3.L.(10)-(15)Oct 15, 2021 · N207PS · Cndair CL6002B19 · Wing StructureSDR SWIA202163704None · brokenRH ENGINE T2 SENSOR LINE OB MOUNT BRACKET IS BROKEN ATTACHED TO NOSE INLET COWL (C-CHECK RO 1/5/2022) REPAIRED RH ENGINE T2 SENSOR LINE OB MOUNT BRACKET ATTACHED TO THE NOSE INLET COWL IAW REO 601R-71-61-3941 REV B DATED5/2/2018 AND SKY CARD 51-900-10Oct 11, 2021 · N207PS · Cndair CL6002B19 · Engine Cowl FlapsSDR SWIA202163703None · nickedCOMPLY WITH SCHEDULED MAINTENANCE CODE: RA65170-601R-53-11-3648 207PS MXCODEID54182-PR - FOUND NICK IN THE MIDDLE OF RH SIDE WINDOW SIDE POST WHERE THE STRAP (I BEAM) MOUNTS ON. COMPLIED WITH TEMPORARY REPAIR PER REO 601R-53-11-3648. PERMANENT REPAIR DUE WITHISep 9, 2021 · N207PS · Cndair CL6002B19 · Fuselage Structure (General)SDR SWIA202163702None · crackedCOMPLY WITH SCHEDULED MAINTENANCE CODE: AD 2019-08-04/02 40000 FC - COMPLY WITH PARAGRAPH (J) OF AD 2019-08-04 BY: (J)(1) DOING A NONDESTRUCTIVE INSPECTION FOR CRACKING OF THE FORWARD FACE OF THE FUSELAGE STATION (FS) 621 PRESSURE BULKHEAD, IN ACCORDANCE WITHSep 9, 2021 · N207PS · Cndair CL6002B19 · Fuselage Main, BulkheadSDR SWIA202158149Thrust Reverser · unlockedD: RECEIVED L REV UNLOCKED AFTER TAKEOFF. / C: MEL 78-30-1 / CAT: C DUE 05/23/21 / RECEIVED L REV UNLOCKED AFTER TAKEOFF. (FLIGHT 4722 - FILED CLOSED) MAY 13, 2021 STATION: DEN--DEFERRED #1 LH ENG THRUST REVERSER IN REF TO CRJ200 MEL 78-30-1. LH TR DEAMay 13, 2021 · N207PS · Cndair CL6002B19 · Engine Thrust ReverserSDR SWIA202054132Bracket · wornALL FOUR BRACKETS ON THE FORWARD WING TO BODY FAIRING WERE FOUND TO BE WORN BEYOND LIMITS. SEE CP 21704602 FOR INSPECTION TASK CARD. FILED CLOSED. REMOVED THE FOUR FAIRING FITTINGS FOR THE FORWARD FAIRING IN THE MLG BAY, PER THE CRJ 200 AMM AND REPLACED THENov 11, 2020 · N207PS · Cndair CL6002B19 · Aerodynamic FairingsSDR VNAA2020050811101Oil Tank · contaminatedSMOKY HAZE FROM AFT CABIN AFTER TAKEOFF. SMOKE TOILET MSG ILLUMINATED AND EXTINGUISHED BEFORE LANDING. REMOVED EXCESS ENGINE OIL FROM L/H & R/H ENGINE OIL TANKS IAW CRJ200 AMM. C/W OPS CHECK OF L/H & R/H AIR CONDITIONING SYSTEM IAW CRJ200 AMM. CABIN & COCKPIT May 5, 2020 · N207PS · Cndair CL6002B19 · Turbine Engine Oil SystemSDR VNAA2019111871101Transmitter · failedREPEAT FLAPS FAIL IN FLIGHT FROM PHL, UNABLE TO LAND IN MYR DUE TO WIND CONDITIONS AND REPORTED WINDSHEAR. CREW WAS DIVERTED TO CLT. MAINTENANCE REMOVED AND REPLACED FLAP POSITION TRANSMITTER ASSEMBLY AND THE SYSTEM OPS CHECKED GOODNov 17, 2019 · N207PS · Cndair CL6002B19 · Trailing Flap Position Indicating SystemSDR VNAA2019082099910Frame · corrodedDURING COMPLIANCE OF T.O. 53-050-001-17. DRAIN TUBE PATH CHANGE, FOUND CORROSION @ FS333 STR 25L TO STR 25R WHEN REMOVAL OF INSULATION TASK #4 OF T.O. REPAIRED FS333 IAW REO 601R-53-21-3163Aug 20, 2019 · N207PS · Bombdr CL6002D15 · Fuselage Main, FrameSDR VNAA2019082099909Bulkhead Web · crackedFOUND RPB WEB AT RBL 18.00 HAS MULTIPLE INDICATIONS NOTED AT WL136-WL129 7" LONG 60% FSH FAILED NDT INSPECTION. COMPLETED REO 601R-53-61-1285 REV-E DATED 2016-10-31.Aug 20, 2019 · N207PS · Bombdr CL6002D15 · Fuselage Main, BulkheadSDR VNAA2019082099908Fitting · corrodedRH ENGINE THRUST FITTING HAS PITTING CORROSION. INSTALLED NEW THRUST FITTING ON R/H ENGINE IAW CRJ 200 AMM 71-22-01-400-801 STEPS 2.C-3.E.Aug 20, 2019 · N207PS · Bombdr CL6002D15 · Engine (Turbine/Turboprop)SDR VNAA2019082099907Fitting · corrodedLH ENGINE THRUST FITTING IS CORRODED. INSTALLED NEW L/H ENGINE THRUST FITTING IAW CRJ 200 AMM 71-22-01-400-801Aug 20, 2019 · N207PS · Bombdr CL6002D15 · Engine (Turbine/Turboprop)SDR VNAA2019082099906Support Bracket · crackedRHS OVERWING FAIRING SUPPORT BRACKET AT FS476 IS CRACKED. DRILLED NEW BRACKET AND INSTALLED NEW BRACKET IAW CRJ 200 SRM 51-40-11, 51-42-06 AND 51-45-00.Aug 20, 2019 · N207PS · Bombdr CL6002D15 · Fuselage Miscellaneous StructureSDR VNAA2019082099905Floor Support · crackedLH FLOOR BEAM CAP AT LBL 27 IS CORRODED AROUND NUTPLATE HOLES BETWEEN FS 574.00 AND FS 621.00. INSTALLED NEW FLOOR BEAM CAP IAW REO 601R-53-61-7069, REV.-- DATED 2019-07-25. SRM 51-42-21 AND 51-42-22.Aug 20, 2019 · N207PS · Bombdr CL6002D15 · Fuselage Miscellaneous StructureSDR VNAA2019082099904Anchor Fitting · crackedPASSENGER DOOR FWD AND AFT ANCHOR FITTINGS ARE CRACKED. INSTALLED FWD AND AFT PAX DOOR ANCHOR FITTINGS IAW AMM 52-11-17-400-804.Aug 20, 2019 · N207PS · Bombdr CL6002D15 · Fuselage Main, Attach FittingsSDR VNAA2019082099903Angle · crackedRH FS 621.00 TO FS 625.00 ANGLE AT RBL 14 IS CRACKED. LOCATED DRILLED AND INSTALLED NEW SERVICEABLE ANGLE IAW CRJ 200 SRM 51-40-11 AND 51-42-21.Aug 20, 2019 · N207PS · Bombdr CL6002D15 · Fuselage Miscellaneous StructureSDR VNAA2019082099902Seat Track · corrodedR/H FLOOR SEAT TRACK AT RBL 9 HAS CORROSION AT FS559.00+16 AND FS 559.00+48. REMOVED UNSERVICEABLE FLOOR SEAT TRACK AT RBL 9 BETWEEN FS 559+16 AND 559+48 IAW CRJ200 AMM 53-01-11-000-802. INSTALLED NEW SERVICEABLE SEAT TRACK AT FS559+16 TO 559+48, RBL 9 IAW Aug 20, 2019 · N207PS · Bombdr CL6002D15 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA2019082099901Step · corrodedSERVICE DOOR STEP PLATE HAS CORROSION NEEDS REPLACED. RECIEVED NEW SERVICEABLE STEP PLATE LOCATED DRILLED AND INSTALLED SOLID RIVETS AND NUTPLATESAug 20, 2019 · N207PS · Bombdr CL6002D15 · Service DoorsSDR VNAA2018102211101Windshield · crackedDURING CRUISE FLIGHT THE FIRST OFFICER WINDSHIELD CRACKED. THE CREW FOLLOWED THE QUICK REFERENCE HANDBOOK AND DIVERTED AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE WINDSHIELD.Oct 22, 2018 · N207PS · Cndair CL6002B19 · Flight Compartment WindowsSDR VNAA2017120511101Housing · looseIN FLIGHT THE CREW REPORTED THE RIGHT ENGINE OIL PRESSURE WAS FLUCTUATING. THE PULLED BACK THE THROTTLES PER THE QRH, AND REPORTED THE PRESSURE DROPPED TO 20 PSI. UPON LANDING THE FIRE CREW REPORTED OIL DRIPPING FROM THE ENGINE. MX INSP AND FOUND THE FILTER HODec 5, 2017 · N207PS · Cndair CL6002B19 · Turbine Engine Oil SystemSDR VNAA2017100299917Intercostal · crackedBS 621 PRESSURE BULKHEAD, LEFT SIDE STRINGER CLIP 14L BS 621 - 625 ON THE INTERCOSTAL CRACKED. INSTALLED A NEW INTERCOSTAL.Sep 30, 2017 · N207PS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR VNAA2017100299916Seat Track · crackedLEFT SEAT TRACK BS 449.85 TO 499 SEGMENT FOUND CORRODED. REMOVED AND REPLACED THE SEAT TRACK.Sep 30, 2017 · N207PS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA2017100299915Angle · crackedANGLE AT BS 484, RBL 27 FOUND CRACKED. REMOVED AND REPLACED THE ANGLE.Sep 30, 2017 · N207PS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR VNAA2017100299914Seat Track · corrodedRIGHT SEAT TRACK BS 364 TO 559+80 SEGMENT CORRODED. REPLACED THE SEAT TRACK.Sep 30, 2017 · N207PS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA2017100299913Seat Track · corrodedLEFT SEAT TRACK BS 499 TO 544 SEGMENT IS CORRODED. REPLACED SECTION OF SEAT TRACK.Sep 30, 2017 · N207PS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA2017100299912Seat Track · corrodedLEFT SEAT TRACK SECTION BS 499 TO 544 CORRODED. REPLACED THE SEAT TRACK SECTION.Sep 30, 2017 · N207PS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA2017100299911Seat Track · corrodedLEFT SEAT TRACK BS 409+16 TO 409+112 SEGMENT IS CORRODED. REMOVED AND REPLACED THE SEAT TRACK SECTION.Sep 30, 2017 · N207PS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA2017100299910Frame · crackedFRAME BS 718, STRINGER 11R IS CRACKED. REPLACED FRAME SECTION.Sep 30, 2017 · N207PS · Cndair CL6002B19 · Fuselage Main, FrameSDR VNAA2017100299909Frame · crackedFRAME BS 718, STRINGER 11R IS CRACKED. REPLACED THE FRAME SECTION BETWEEN STRINGERS 6 AND 20R.Sep 30, 2017 · N207PS · Cndair CL6002B19 · Fuselage Main, FrameSDR VNAA2017100299908Fitting · corrodedFLOOR SUPPORT TO FRAME FITTING AT BS 319.7, RBL 42 IS CORRODED. LOCATED, DRILLED AND INSTALLED NEW FLOOR SUPPORT TO FRAME FITTING IAW SRM 51-42-21, AND 51-40-11.Sep 30, 2017 · N207PS · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR VNAA2017100299907Seat Track · corrodedSEAT TRACK AT LBL 9 IS CORRODED FROM BS 399 TO 409+128. REMOVED AND REPLACED THE SEAT TRACK IAW REO 601R-53-00-485, AND AMM 53-01-11-400-802.Sep 30, 2017 · N207PS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA2017100299906Seat Track · corrodedSEAT TRACK AT RBL 9 IS CORRODED FROM BS 364 TO 399. FABRICATED A NEW SEAT TRACKS IAW REO 601R-53-00-485, REV. B.Sep 30, 2017 · N207PS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA2017100299905Seat Track · corrodedSEAT TRACK AT LBL 9 CORRODED FROM BS 409+128 - 559+4. REMOVED AND REPLACED THE SEAT TRACK IAW REO 601R-53-00-485 AND AMM 53-01-11-400-802.Sep 30, 2017 · N207PS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA2017100299904Seat Track · corrodedSEAT TRACK AT RBL 9 IS CORRODED FROM BS 559+4 TO 559+86. REMOVED AND REPLACED THE SEAT TRACK IAW REO 601R-53-00-485, AND AMM 53-01-11-400-802.Sep 30, 2017 · N207PS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA2017100299903Floor Support · corrodedRIGHT FLOOR SUPPORT CORRODED FROM BS 559+80 - 621. INSTALLED A NEW SERVICEABLE FLOOR SUPPORT IAW SRM 51-42-21, AND 51-42-06.Sep 30, 2017 · N207PS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR VNAA2017100299902Channel · crackedFS 621 REAR PRESSURE BULKHEAD, BL 0 ZEE CHANNEL CRACKED. REPAIRED IAW REO 601R-53-61-1285, REV E.Sep 30, 2017 · N207PS · Cndair CL6002B19 · Fuselage Main, BulkheadSDR VNAA2017100299901Bulkhead Web · crackedBS 621 PRESSURE BULKHEAD WEB CRACKED. REPAIRED IAW REO 601R-53-61-1285, REV E.Sep 30, 2017 · N207PS · Cndair CL6002B19 · Fuselage Main, Bulkhead
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