# Service difficulty reports: N709PS, cancelled Apr 3, 2025

A list on [N709PS, cancelled Apr 3, 2025](https://openairdocs.org/deregistered/N709PS-2025-04-03.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 · 150 reports

- [SDR VNAA20250116075](https://openairdocs.org/sdr/VNAA20250116075.md): Angle · corroded · Jan 16, 2025 · N709PS · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > FS 280.00 J ANGLE CORRODED LBL 9 TO RBL 9 INCLUDING BOTH WALL CLIPS. REMOVED AND REPLACED IAW CRJ 700 SRMS 51-40-11-001-001-A01, 51-42-06-001-001-A01, AND 51-42-21-001-001-A01. BLENDED WALL CLIPS IAW CRJ 700 SRM 51-21-06-001-001-A01, WITHIN LIMITS IAW CRJ 70
- [SDR VNAA20250116074](https://openairdocs.org/sdr/VNAA20250116074.md): Plate · corroded · Jan 16, 2025 · N709PS · Cndair CL6002C10 · Fuselage Main, Structure
  > MULTIPLE AREAS OF CORROSION R/H SILL PLATE F.S. 280 -333 RBL 34 CORRECTIVE ACTION: REMOVED AND REPLACED R/H SILL PLATE P/N SH670-32172-5 AT FS 280-333 RBL 34 IAW CRJ 700 SRM 51-42-13-001-001-A01
- [SDR VNAA20250116073](https://openairdocs.org/sdr/VNAA20250116073.md): Tie Down · corroded · Jan 16, 2025 · N709PS · Cndair CL6002C10 · Fuselage, Equipment Attach Fittings
  > RIGHT INBD FWD GALLEY TIE DOWN CORRODED JUST AFT OF F.S.280 APPROX RBL 14. REMOVED CORRODED TIE DOWN. LOCATED AND REPLACED WITH NEW SERVICEABLE R/H INBD FWD GALLEY TIE DOWN P/N (SH670-32149-3) JUST AFT OF F.S.280 APPROX RBL 14 IAW CRJ-700 SRM 51-42-21-001-00
- [SDR VNAA20250116072](https://openairdocs.org/sdr/VNAA20250116072.md): Angle · corroded · Jan 16, 2025 · N709PS · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > FS 280.00 J ANGLE CORRODED LBL 9 TO RBL 9 INCLUDING BOTH WALL CLIPS. REMOVED AND REPLACED IAW CRJ 700 SRMS 51-40-11-001-001-A01, 51-42-06-001-001-A01, AND 51-42-21-001-001-A01. BLENDED WALL CLIPS IAW CRJ 700 SRM 51-21-06-001-001-A01, WITHIN LIMITS IAW CRJ 70
- [SDR VNAA20250116071](https://openairdocs.org/sdr/VNAA20250116071.md): Torque Box · damaged · Jan 16, 2025 · N709PS · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > 3 EA TOOLING MARKS ON AFT BOTTOM SIDE OF L/H TORQUE BOX BELOW LOOKING UP F.S.295 APPOX LBL12. REMOVED AND REPLACED IAW CRJ 700 SRMS 51-40-11-001-001-A01 AND 51-42-13-001-001-A01.
- [SDR VNAA20250116070](https://openairdocs.org/sdr/VNAA20250116070.md): Stringer · corroded · Jan 16, 2025 · N709PS · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > STR 25R CORRODED F.S. 280 -333. REMOVED AND REPLACED IAW CRJ 700 SRMS 51-40-11-001-001-A01, 51-42-06-001-001-A01, AND 51-42-21-001-001-A01.
- [SDR VNAA20250116069](https://openairdocs.org/sdr/VNAA20250116069.md): Support Angle · corroded · Jan 16, 2025 · N709PS · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > FS 632-655 WING-TO-FUSELAGE FAIRING SUPPORT STRUCTURE FLANGE IS CORRODED. CORRECTIVE ACTION: REMOVED AND REPLACED IAW CRJ 700 SRMS 51-40-11-001-001-A01 AND 51-42-06-001-001-A01.
- [SDR VNAA20250116068](https://openairdocs.org/sdr/VNAA20250116068.md): Splice · corroded · Jan 16, 2025 · N709PS · Cndair CL6002C10 · Fuselage Main, Structure
  > DISCREPANCY: FS 629 STGR 19L -27 ON WING-TO-FUSELAGE FAIRING SUPPORT STRUCTURE FLANGES FWD AND AFT HAVE MULTIPLE AREAS OF CORROSION AROUND THE FASTENER HOLES CORRECTIVE ACTION: INSTALLED NEW SERVICEABLE SPLICE JOINT PLATE P/N SH670-39054-3 WITH SOLID RIVETS IA
- [SDR VNAA20250116067](https://openairdocs.org/sdr/VNAA20250116067.md): Seat Track · corroded · Jan 16, 2025 · N709PS · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > R/H I/B SEAT TRACK @ FS 538 HAS SOME GOUGING AND MINOR CORROSION WHICH REQUIRES EVALUATION. CORRECTIVE ACTION: REMOVED RBL 9 SEAT TRACK BETWEEN FS485 AND FS581 IAW CRJ-700 SRM 53-00-49-000-801-A03. FABRICATED NEW SEAT TRACK P/N SH690-33407-1 @ RBL 9 SEAT TRACK
- [SDR VNAA20250116066](https://openairdocs.org/sdr/VNAA20250116066.md): Frame · corroded · Jan 16, 2025 · N709PS · Cndair CL6002C10 · Fuselage Main, Frame
  > FRAME AT FS 661 BOTTOM CL AFT END OF FWD CARGO COMPARTMENT IS CORRODED COMPLETELY THROUGH TO THE SHEAR TIE ON THE FRONT SIDE WITH A HOLE APPROXIMATELY 1". CORRECTIVE ACTION: CUT AWAY DAMAGED PORTION OF FRAME AND INSTALLED REPAIR PARTS IAW MHIRJ REO 670-53-31-9
- [SDR VNAA20250116065](https://openairdocs.org/sdr/VNAA20250116065.md): Beam · chafed · Jan 16, 2025 · N709PS · Cndair CL6002C10 · Wing Miscellaneous Structure
  > FOUND R/H FLAP VANE ACTUATOR AT FLS 140.40 TO HAVE MULTIPLE SPOTS OF CHAFE DAMAGE ALONG BEAM OUTER TUBE. CORRECTIVE ACTION: REPAIRED FLAP VANE ACTUATOR IAW MHIRJ REO 670-57-52-257 REV A DATED 2024-08-20.
- [SDR VNAA20250116064](https://openairdocs.org/sdr/VNAA20250116064.md): Beam · chafed · Jan 16, 2025 · N709PS · Cndair CL6002C10 · Wing Miscellaneous Structure
  > FOUND R/H FLAP VANE ACTUATOR AT FLS 102.90 TO HAVE MULTIPLE SPOTS OF CHAFE DAMAGE ALONG BEAM OUTER TUBE. CORRECTIVE ACTION: REPAIRED FLAP VANE ACTUATOR IAW MHIRJ REO 670-57-52-257 REV A DATED 2024-08-20.
- [SDR VNAA20250116063](https://openairdocs.org/sdr/VNAA20250116063.md): Beam · chafed · Jan 16, 2025 · N709PS · Cndair CL6002C10 · Wing Miscellaneous Structure
  > FOUND R/H FLAP VANE ACTUATOR AT LWS 65.50 TO HAVE MULTIPLE SPOTS OF CHAFE DAMAGE ALONG BEAM OUTER TUBE. CORRECTIVE ACTION: REPAIRED FLAP VANE ACTUATOR IAW MHIRJ REO 670-57-52-257 REV A DATED 2024-08-20.
- [SDR VNAA20250116062](https://openairdocs.org/sdr/VNAA20250116062.md): Beam · chafed · Jan 16, 2025 · N709PS · Cndair CL6002C10 · Wing Miscellaneous Structure
  > FOUND L/H FLAP VANE ACTUATOR AT LWS 140.40 TO HAVE MULTIPLE SPOTS OF CHAFE DAMAGE ALONG BEAM OUTER TUBE. CORRECTIVE ACTION: REPAIRED FLAP VANE ACTUATOR IAW MHIRJ REO 670-57-52-257 REV A DATED 2024-08-20.
- [SDR VNAA20250116061](https://openairdocs.org/sdr/VNAA20250116061.md): Beam · chafed · Jan 16, 2025 · N709PS · Cndair CL6002C10 · Wing Miscellaneous Structure
  > FOUND L/H FLAP VANE ACTUATOR AT LWS 65.50 TO HAVE MULTIPLE SPOTS OF CHAFE DAMAGE ALONG BEAM OUTER TUBE. CORRECTIVE ACTION: REPAIRED FLAP VANE ACTUATOR IAW MHIRJ REO 670-57-52-257 REVA DATED 2024-08-20.
- [SDR VNAA20250116060](https://openairdocs.org/sdr/VNAA20250116060.md): Beam · chafed · Jan 16, 2025 · N709PS · Cndair CL6002C10 · Wing Miscellaneous Structure
  > FOUND L/H FLAP VANE ACTUATOR AT LWS 102.90 TO HAVE MULTIPLE SPOTS OF CHAFE DAMAGE ALONG BEAM OUTER TUBE. CORRECTIVE ACTION: REPAIRED FLAP VANE ACTUATOR IAW MHIRJ REO 670-57-52-257 REV A DATED 2024-08-20.
- [SDR VNAA20250116059](https://openairdocs.org/sdr/VNAA20250116059.md): Beam · chafed · Jan 16, 2025 · N709PS · Cndair CL6002C10 · Wing Miscellaneous Structure
  > FOUND L/H FLAP VANE ACTUATOR AT FLS 24.00 TO HAVE MULTIPLE SPOTS OF CHAFE DAMAGE ALONG BEAM OUTER TUBE CORRECTIVE ACTION: REPAIRED FLAP VANE ACTUATOR IAW MHIRJ REO 670-57-52-257 REVA DATED 2024-08-20.
- [SDR VNAA20250116057](https://openairdocs.org/sdr/VNAA20250116057.md): Channel · damaged · Jan 16, 2025 · N709PS · Cndair CL6002C10 · Rudder Structure
  > PILOT RUDDER FEEL UNIT CHANNEL CC670-94223 REQUIRES REMOVAL DUE TO DOUBLE DRILLED HOLE. CORRECTIVE ACTION: REMOVED PILOT RUDDER FEEL UNIT LWR CHANNEL CC670-94223 IAW CRJ 700 AMM 27-21-05-000-801-A01 FABRICATED RUDDER PEDAL SUPPORT CHANNEL PN: CC670-94223-3 IAW
- [SDR VNAA20250116056](https://openairdocs.org/sdr/VNAA20250116056.md): Angle · cracked · Jan 16, 2025 · N709PS · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR INNER ANGLE ON VENT FLAP COVER FOUND CRACKED AND REQUIRES REPLACEMENT. CORRECTIVE ACTION: REMOVED CRACKED INNER ANGLE IAW CRJ 700 SRM 51-42-06-001-001-A01. LOCATED AND DRILLED NEW INNER ANGLE IAW CRJ 700 SRM 51-40-11-001-001-A01. INSTALLED NEW SERVICE
- [SDR VNAA20250116055](https://openairdocs.org/sdr/VNAA20250116055.md): Step · cracked · Jan 16, 2025 · N709PS · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR TOP STEP PANEL CRACKED REQUIRES REPLACEMENT CORRECTIVE ACTION: LOCATED AND DRILLED NEW SERVICEABLE PAX DOOR TOP STEP PANEL P/N:601R317075-3 IAW CRJ700 SRM 51-40-11-001-001-A01. REFERENCE JOB CARD HN00189258 FOR REMOVAL AND INSTALL
- [SDR VNAA20250116054](https://openairdocs.org/sdr/VNAA20250116054.md): Seat Track · cracked · Jan 16, 2025 · N709PS · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > R/H I/B SEAT TRACK @ FS 538 HAS SOME GOUGING AND MINOR CORROSION WHICH REQUIRES EVALUATION. REMOVED RBL 9 SEAT TRACK BETWEEN FS485 AND FS581 IAW CRJ-700 SRM 53-00-49-000-801-A03. FABRICATED NEW SEAT TRACK P/N SH690-33407-1 @ RBL 9 SEAT TRACK BETWEEN FS485 AND
- [SDR VNAA20250116053](https://openairdocs.org/sdr/VNAA20250116053.md): Drag Angle · cracked · Jan 16, 2025 · N709PS · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR AFT DRAG ANGLE FOUND WITH CRACK AT UPPER END. CORRECTIVE ACTION: LOCATE, DRILL, AND INSTALLED NEW SERVICEABLE DRAG ANGEL P# 601R31772-5S IAW CRJ 700 SRM 51-40-11-001-001-A01 AND 51-42-06-001-001-A01.
- [SDR VNAA2025F00005](https://openairdocs.org/sdr/VNAA2025F00005.md): Stringer · corroded · Jan 16, 2025 · N709PS · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > STR 26R @ FS. 333 + 6 FOUND TO HAVE PITTING/CORROSION ON ATTACH FLANGE. CORRECTIVE ACTION: REMOVED CORRODED STRINGER AND INSTALLED A NEW STGR26R BETWEEN FS 333 AND FS 364 (PN- SH670-31372-4S) IAW CRJ700 SRM 51-42-06-001-001-A01 AND SRM 51-21-06-001-001-A0
- [SDR VNAA20250116052](https://openairdocs.org/sdr/VNAA20250116052.md): Drag Angle · cracked · Jan 16, 2025 · N709PS · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR FWD STAIR WEB DRAG ANGLE FOUND CRACKED. CORRECTIVE ACTION: REMOVED AND REPLACED IAW CRJ 700 SRMS 51-40-11-001-001-A01 AND 51-42-06-001-001-A01.
- [SDR VNAA20250116051](https://openairdocs.org/sdr/VNAA20250116051.md): Drag Angle · cracked · Jan 16, 2025 · N709PS · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR FWD STAIR WEB DRAG ANGLE FOUND CRACKED. CORRECTIVE ACTION: REMOVED AND REPLACED IAW CRJ 700 SRMS 51-40-11-001-001-A01 AND 51-42-06-001-001-A01.
- [SDR VNAA20250116049](https://openairdocs.org/sdr/VNAA20250116049.md): Cover · cracked · Jan 16, 2025 · N709PS · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR AFT CORNER COVER FOUND CRACKED UPON REMOVAL. REQUIRES REPLACEMENT. REMOVED AND REPLACED IAW CRJ 700 SRMS 51-40-11-001-001-A01 AND 51-42-13-001-001-A01.
- [SDR VNAA20250116048](https://openairdocs.org/sdr/VNAA20250116048.md): Cleat · corroded · Jan 16, 2025 · N709PS · Cndair CL6002C10 · Fuselage Main, Attach Fittings
  > CLEAT LOCATED AT STR19L ON FWD SIDE OF FS1047 IS CORRODED. CORRECTIVE ACTION: REMOVED AND REPLACED IAW CRJ 700 SRMS 51-40-11-001-001-A01 AND 51-42-021-001-001-A01.
- [SDR VNAA20250116047](https://openairdocs.org/sdr/VNAA20250116047.md): Window Post · cracked · Jan 16, 2025 · N709PS · Cndair CL6002C10 · Fuselage Main, Structure
  > LH WINDSHIELD SIDE POST P/N 601R33223 IS CRACKED APPROX. 6" FROM TOP AND 2" LONG AT 100% FSH FAILING NDT. REPAIRED BY CUTTING OUT DAMAGED PORTION AND SPLICING IN NEW REPAIR PARTS IAW MHIRJ REO 670-53-21-2465 REV-- DATED 10-21-24
- [SDR VNAA20250116046](https://openairdocs.org/sdr/VNAA20250116046.md): Retainer · corroded · Jan 16, 2025 · N709PS · Cndair CL6002C10 · Fuselage Main, Structure
  > MAIN AVIONICS DOOR L/H FWD SEAL RETAINER IS CORRODED. CORRECTIVE ACTION: REMOVED AND REPLACED IAW CRJ 700 SRMS 51-40-11-001-001-A01 AND 51-42-06-001-001-A01.
- [SDR VNAA20250116045](https://openairdocs.org/sdr/VNAA20250116045.md): Support · corroded · Jan 16, 2025 · N709PS · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > FS 909 RBL 2- RBL 22 WING TO FUSELAGE SUPPORT STRUCTURE FLANGE FAYING SURFACE (BOTTOM) IS CORRODED ALONG LENGTH. REMOVED AND REPLACED IAW CRJ 700 SRMS 51-40-11-001-001-A01, 51-42-06-001-001-A01, AND 51-42-10-001-001-A01.
- [SDR VNAA20250116044](https://openairdocs.org/sdr/VNAA20250116044.md): Support · corroded · Jan 16, 2025 · N709PS · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > FS 909 RBL 2- RBL 22 WING TO FUSELAGE SUPPORT STRUCTURE FLANGE FAYING SURFACE (BOTTOM) IS CORRODED ALONG LENGTH. REMOVED AND REPLACED IAW CRJ 700 SRMS 51-40-11-001-001-A01, 51-42-06-001-001-A01, AND 51-42-10-001-001-A01.
- [SDR VNAA20250116043](https://openairdocs.org/sdr/VNAA20250116043.md): Support · corroded · Jan 16, 2025 · N709PS · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > FS 939 ON CL WING TO FUSELAGE SUPPORT STRUCTURE FLANGE IS CORRODED AROUND 2 EA. FASTENER HOLES AND REQUIRES EVALUATION. CORRECTIVE ACTION: REMOVED AND REPLACED ANGLE P/N SH670-39189-1 IAW CRJ-700-SRM-51-40-11-001-001-A01 AND 51-42-06-001-001-A01
- [SDR VNAA20250116042](https://openairdocs.org/sdr/VNAA20250116042.md): Support · corroded · Jan 16, 2025 · N709PS · Cndair CL6002C10 · Aerodynamic Fairings
  > FS 879 LBL 10- RBL 28 WING TO FUSELAGE SUPPORT STRUCTURE FLANGE FAYING SURFACE (BOTTOM) IS CORRODED ALONG LENGTH AND REQUIRES EVALUATION CORRECTIVE ACTION: REMOVED CORRODED STRAPS AND INSTALLED (2) STRAPS P/N: (SH670-39333-9) ON FS 879 LBL 10- RBL 28 WING TO F
- [SDR VNAA20250116041](https://openairdocs.org/sdr/VNAA20250116041.md): Frame · cracked · Jan 16, 2025 · N709PS · Cndair CL6002C10 · Fuselage Main, Frame
  > FS 333.00 FRAME IS CRACKED BETWEEN STRINGER 2R AND 3R. REPAIRED BY CUTTING OUT DAMAGED PORTION AND SPLICING IN NEW REPAIR PARTS IAW MHIRJ REO 670-53-21-2465 REV-- DATED 10-21-24
- [SDR VNAA20250116040](https://openairdocs.org/sdr/VNAA20250116040.md): Retainer · corroded · Jan 16, 2025 · N709PS · Cndair CL6002C10 · Electrical/Electronic Compartment Doors
  > MAIN AVIONICS DOOR, R/H SEAL RETAINER IS CORRODED. REMOVED AND REPLACED RETIANER I.A.W. CRJ700 SRM 51-42-06-001-001-A01.
- [SDR VNAA20250116039](https://openairdocs.org/sdr/VNAA20250116039.md): Skin · dented · Jan 16, 2025 · N709PS · Cndair CL6002C10 · Trailing Edge Flaps
  > THE LEFT WING INBOARD FLAP LOWER SKIN IS DENTED 6 X 6 X.035 JUST AFT OF THE MLG TIRES. CORRECTIVE ACTION: REPAIRED IAW CRJ-700 SRM 57-52-01-201-005-A01.
- [SDR VNAA20250116038](https://openairdocs.org/sdr/VNAA20250116038.md): Stringer · corroded · Jan 16, 2025 · N709PS · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > F.S. 406-421 STR 19 CORRODED CORRECTIVE ACTION:STRINGER WAS REPAIRED IAW IAW CRJ700 SRM 53-00-03-201-001-A01
- [SDR VNAA20250116037](https://openairdocs.org/sdr/VNAA20250116037.md): Slat Track · corroded · Jan 16, 2025 · N709PS · Cndair CL6002C10 · Leading Edge Devices
  > FOUND R/H SLAT TRACK 3-1 TO HAVE WEAR DAMAGE IN MULTIPLE LOCATIONS. CORRECTIVE ACTION: REPAIRED R/H SLAT TRACK 3-1 IAW REO 670-57-42-1745 REV-DATED 11-11-2024. SDIR IS BEING TRACKED UNDER RFTS-116974
- [SDR VNAA20250116036](https://openairdocs.org/sdr/VNAA20250116036.md): Floorbeam · corroded · Jan 16, 2025 · N709PS · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > RBL 9 FLOOR BEAM IS CORRODED AT FS 1031 CORRECTIVE ACTION: DAMAGE WAS REPAIRED IAW CRJ700 SRM 53-00-41-201-001-001-A01 AND REO 670-53-61-2395 REV-- DATED 2024-10-24
- [SDR VNAA20250115034](https://openairdocs.org/sdr/VNAA20250115034.md): Door Sill · corroded · Jan 15, 2025 · N709PS · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > UPON REMOVAL OF AFT CARGO DOOR SILL, FOUND THE CENTER INNER CHORD TO BE CORRODED AT NUTPLATE LOCATIONS. DAMAGE WAS REPAIRED BY INSTALLING A SERVICABLE INNER CHORD
- [SDR VNAA20250115033](https://openairdocs.org/sdr/VNAA20250115033.md): Door Sill · corroded · Jan 15, 2025 · N709PS · Cndair CL6002C10 · Cargo/Baggage Doors
  > UPON REMOVAL OF AFT CARGO DOOR SILL, FOUND THE CENTER INNER CHORD TO BE CORRODED AT NUTPLATE LOCATIONS. CORRECTIVE ACTION: DAMAGE WAS REPAIRED BY INSTALLING A SERVICABLE INNER CHORD
- [SDR VNAA20250115032](https://openairdocs.org/sdr/VNAA20250115032.md): Door Sill · corroded · Jan 15, 2025 · N709PS · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > UPON REMOVAL OF AFT CARGO DOOR SILL, FOUND THE CENTER INNER CHORD TO BE CORRODED AT NUTPLATE LOCATIONS. CORRECTIVE ACTION: DAMAGE WAS REPAIRED BY INSTALLING A SERVICABLE INNER CHORD
- [SDR VNAA20250115031](https://openairdocs.org/sdr/VNAA20250115031.md): Door Sill · corroded · Jan 15, 2025 · N709PS · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > UPON REMOVAL OF AFT CARGO DOOR SILL, FOUND THE FWD INNER CHORD TO BE CORRODED AT NUTPLATE LOCATIONS. CORRECTIVE ACTION: DAMAGE WAS REPAIRED BY INSTALLING A SERVICABLE INNER CHORD
- [SDR VNAA20250115030](https://openairdocs.org/sdr/VNAA20250115030.md): Seat Track · corroded · Jan 15, 2025 · N709PS · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > DISCREPANCY: LH SIDE SEAT RAIL IS CORRODED BETWEEN FS863 AND FS969.00
- [SDR VNAA20250115029](https://openairdocs.org/sdr/VNAA20250115029.md): Seat Track · corroded · Jan 15, 2025 · N709PS · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > DISCREPANCY: AFT CARGO BAY SEAT TRACK ON LBL27 FROM FS978 TO FS1006 IS CORRODED CORRECTIVE ACTION: REMOVED CORRODED SEAT RAIL AND INSTALLED A SERVICABLE SEAT RAIL IAW CRJ-700 AMM 53-00-49-000/400-801-A03
- [SDR VNAA20250115028](https://openairdocs.org/sdr/VNAA20250115028.md): Seat Track · corroded · Jan 15, 2025 · N709PS · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > CO # 101651424 BARCODE HN00190434 DISCREPANCY: LH SIDE SEAT RAIL IS CORRODED BETWEEN FS863 AND FS969.00
- [SDR VNAA20250115027](https://openairdocs.org/sdr/VNAA20250115027.md): Seat Track · corroded · Jan 15, 2025 · N709PS · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > LH SIDE SEAT RAIL IS CORRODED BETWEEN FS 785.15 AND 863. REMOVED CORRODED SEAT RAIL AND INSTALLED A SERVICABLE SEAT RAIL
- [SDR VNAA20250115026](https://openairdocs.org/sdr/VNAA20250115026.md): Seat Track · corroded · Jan 15, 2025 · N709PS · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > RBL 9 SEAT TRACK IS CORRODED BETWEEN FS 985.00 AND 1015.00. CORRECTIVE ACTION: REMOVED SEAT TRACK ON RBL9 FROM FS985.00 TO FS1015.00 IAW CRJ-700 AMM 53-00-49-000-802 CONFIG A03. SEAT TRACK ON RBL9 FROM FS985.00 TO FS1015.00 WAS FABRICATED IN COMPLIANCE WITH RE
- [SDR VNAA20250115025](https://openairdocs.org/sdr/VNAA20250115025.md): Seat Track · corroded · Jan 15, 2025 · N709PS · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > LBL 9 SEAT TRACK IS CORRODED BETWEEN FS 985.00 AND 1015.00. CORRECTIVE ACTION: REMOVED, FABRICATED, AND REPLACED SEAT TRACK IAW MHIRJ REO 670-53-00-589, REV-C, DATE: 2022-12-19.
- [SDR VNAA20250115024](https://openairdocs.org/sdr/VNAA20250115024.md): Seat Track · corroded · Jan 15, 2025 · N709PS · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > RBL 27 SEAT TRACK IS CORRODED BETWEEN FS 1031.00 AND 1069.75. CORRECTIVE ACTION: REMOVED, FABRICATED, AND REPLACED SEAT TRACK IAW MHIRJ REO 670-53-00-589, REV-C, DATE: 2022-12-19.

Next page: https://openairdocs.org/deregistered/N709PS-2025-04-03/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 = 'N709PS' AND deregistration_id = 'N709PS-2025-04-03'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N709PS-2025-04-03/reports

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