# Service difficulty reports: N725PS

A list on [N725PS](https://openairdocs.org/aircraft/N725PS.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 · 122 reports

- [SDR VNAA2025090511101](https://openairdocs.org/sdr/VNAA2025090511101.md): Power Unit · overheated · Sep 4, 2025 · N725PS · Cndair CL6002C10 · Passenger Compartment Lighting
  > BURNING SMELL ABEAM WARDROBE / T/S PER FIM 21-22-00-810-806-A01 AND CEILING LIGHT POWER UNIT/DIMMER AT SEAT ROW 1A FOUND OVERHEATED, REMOVED AND REPLACED POWER UNIT/DIMMER IAW AMM 33-21-03-000/400-801-A01. PERFORMED OPERATIONAL TEST OF PAX COMPARTMENT LIGHT I
- [SDR VNAA2025060211101](https://openairdocs.org/sdr/VNAA2025060211101.md): Control Panel · faulted · Jun 1, 2025 · N725PS · Cndair CL6002C10 · Air Intake Anti/De-Ice System
  > L COWL A/ICE CAUTION. / REMOVED AND REPLACED ANTI-ICE CONTROL PANEL IAW CRJ 700 AMM 30-12-10-000/400-801. L CAIV OPS TEST GOOD; WINDSHIELD HEAT STATUS MESSAGE AND L PITOT HEAT/STATIC HEAT/AOA STATUS MESSAGES APPEARED. REMOVED AND RERACKED DCU 1 IAW CRJ 700 AMM
- [SDR VNAA202407120043](https://openairdocs.org/sdr/VNAA202407120043.md): Floorbeam · corroded · Jul 10, 2024 · N725PS · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > HN147962 DISCREPANCY: RBL 9.00 FLOOR BEAM IS CORRODED AT F.S. 1031.00. CORRECTIVE ACTION: REPAIRED DAMAGE I.A.W. BOMBARDIER CRJ700 SRM REPAIR 53-41-201-001-A01 AND MHIRJ REO 670-53-61-2254 REV.--, DATED 2024-04-05
- [SDR VNAA202407120042](https://openairdocs.org/sdr/VNAA202407120042.md): Floor Support · corroded · Jul 10, 2024 · N725PS · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > HN00147959 DISCREPANCY: LBL 9 FLOOR BEAM IS CORRODED BETWEEN F.S. 1051.30 TO F.S. 1069.85. CORRECTIVE ACTION: REMOVED DAMAGED FLOOR BEAM LBL9 FROM FACTORY SPLICE TO MARKED CUT LINE. IAW CRJ-700 SRM 53-00-41-201-001-A01. FABRICATED REPAIR PARTS AND SPLICE PLATE
- [SDR VNAA202407120041](https://openairdocs.org/sdr/VNAA202407120041.md): Floorbeam · corroded · Jul 10, 2024 · N725PS · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > HN00147598 DISCREPANCY: LBL 27 FLOOR BEAM IS CORRODED AT F.S. 1031. CORRECTIVE ACTION: REPAIRED/REPLACED CORRODED SECTIONS OF FLOOR BEAM AT LBL 27 IAW CRJ 700 SRM 53-00-41-201-001-A01 AND REO 670-53-61-2254 REV -- DATED 2024-04-05.
- [SDR VNAA202407120040](https://openairdocs.org/sdr/VNAA202407120040.md): Skin · chafed · Jul 10, 2024 · N725PS · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > HN00147837 DISCREPANCY: FUSELAGE OUTER SKIN IS CHAFED UNDER AFT LAV. RINSE/FILL PORT. CORRECTIVE ACTION: FOUND AN EXTERNAL REINFORCING DOUBLER AROUND CANNON PLUG PL118J1 TO BE CHAFED. NOT THE EXTERNAL SKIN. COMPLIED WITH REMAINING STEPS OF REO 670-53-51-281 RE
- [SDR VNAA202407120039](https://openairdocs.org/sdr/VNAA202407120039.md): Floorbeam · corroded · Jul 10, 2024 · N725PS · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > HN00147488 DISCREPANCY: FS 280 FWD FLOOR SUPPORT ANGLE IS CORRODED AT LBL 9. CORRECTIVE ACTION: REMOVED J-ANGLE @ FS 280 IAW CRJ700 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01. INSTALLED NEW SERVICEABLE J-ANGLE PN/ CC670-34095-1SB - ASSY, ANGLE IAW CRJ70
- [SDR VNAA202407120038](https://openairdocs.org/sdr/VNAA202407120038.md): Door Frame · cracked · Jul 10, 2024 · N725PS · Cndair CL6002C10 · Fuselage Main, Structure
  > HN147025 DISCREPANCY: LH OVERWING EMERGENCY EXIT DOOR TOP EDGE MEMBER IS CRACKED AT THE BASE OF THE AFT ALIGNMENT FITTING. CORRECTIVE ACTION: COMPLIED WITH MHIRJ REO 670-52-21-096 REV-- DATED 2024-04-01
- [SDR VNAA202407120037](https://openairdocs.org/sdr/VNAA202407120037.md): Bracket · cracked · Jul 10, 2024 · N725PS · Cndair CL6002C10 · Fuselage Main, Structure
  > HN146956 DISCREPANCY: GALLEY SERVICE DOOR UPPER STABILIZER BRACKET IS CRACKED. CORRECTIVE ACTION: REMOVED AND REPLACED STABILIZER-BAR BRACKET IAW CRJ-700 AMM 52-41-27-400-801-A01 AND SRM 51-40-11-001-001-A01
- [SDR VNAA202407120036](https://openairdocs.org/sdr/VNAA202407120036.md): Pressure Panel · chafed · Jul 10, 2024 · N725PS · Cndair CL6002C10 · Fuselage Main, Structure
  > HN146636 DISCREPANCY: LOW PRESSURE BLEED PANEL PLATE HAS 4 CHAFED LOCATIONS IN THE SKIN AROUND THE BLEED ASSY CUTOUT. CORRECTIVE ACTION: REMOVED AND REPLACED LP BLEED PANEL PLATE IAW CRJ-700 SRM 51-42-06-001-001-A01, 51-42-22-001-001-A01, AND REO 670-53-61-225
- [SDR VNAA202407120035](https://openairdocs.org/sdr/VNAA202407120035.md): Window Post · cracked · Jul 10, 2024 · N725PS · Cndair CL6002C10 · Fuselage Main, Structure
  > HN146514 DISCREPANCY: FOUND WINDSHIELD POST CRACKED ON CAPTAIN SIDE BETWEEN WINDOW AND WINDSHIELD. CORRECTIVE ACTION: REMOVED AND REPLACED PILOT SIDE WINDSHIELD POST IAW CRJ-700 SRM 51-42-21-001-001-A01 AND 51-40-11-001-001-A01
- [SDR VNAA202407120034](https://openairdocs.org/sdr/VNAA202407120034.md): Seat Track · corroded · Jul 10, 2024 · N725PS · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > E HN154922 DISCREPANCY: RBL 27 SEAT RAIL IS CORRODED BETWEEN FS 1033 AND FS 1061 CORRECTIVE ACTION: REMOVED AND REPLACED RBL 27 SEAT RAIL IAW CRJ-700 SRM 53-00-49-201-002-A01 AND AMM 53-00-49-400-802-A03
- [SDR VNAA202407120033](https://openairdocs.org/sdr/VNAA202407120033.md): Seat Track · corroded · Jul 10, 2024 · N725PS · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > HN154920 DISCREPANCY: RBL 27 SEAT RAIL IS CORRODED BETWEEN FS 977 AND FS 1005 CORRECTIVE ACTION: REMOVED AND REPLACED RBL 27 SEAT RAIL IAW CRJ-700 SRM 53-00-49-201-002-A01 AND AMM 53-00-49-400-802-A03
- [SDR VNAA202407120032](https://openairdocs.org/sdr/VNAA202407120032.md): Seat Track · corroded · Jul 10, 2024 · N725PS · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > HN154917 DISCREPANCY: RBL 9 SEAT RAIL IS CORRODED BETWEEN FS 1033 AND FS 1061 CORRECTIVE ACTION: REMOVED AND REPLACED RBL 9 SEAT RAIL IAW CRJ-700 SRM 53-00-49-201-002-A01 AND AMM 53-00-49-400-802-A03
- [SDR VNAA202407120031](https://openairdocs.org/sdr/VNAA202407120031.md): Seat Track · corroded · Jul 10, 2024 · N725PS · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > HN154916 DISCREPANCY: FOUND SEAT RAIL AT RBL 9.00, FS 977-1005 TO BE CORRODED. CORRECTIVE ACTION: REMOVED AND REPLACED RBL 9 SEAT RAIL IAW CRJ-700 SRM 53-00-49-201-002-A01 AND AMM 53-00-49-400-802-A03.
- [SDR VNAA202407120030](https://openairdocs.org/sdr/VNAA202407120030.md): Seat Track · corroded · Jul 10, 2024 · N725PS · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > HN154914 DISCREPANCY: LBL 9 SEAT RAIL IS CORRODED BETWEEN FS 1033 AND FS 1061 CORRECTIVE ACTION: REMOVED AND REPLACED LBL 9 SEAT RAIL IAW CRJ-700 SRM 53-00-49-201-002-A01 AND AMM 53-00-49-400-802-A03
- [SDR VNAA202407120029](https://openairdocs.org/sdr/VNAA202407120029.md): Seat Track · corroded · Jul 10, 2024 · N725PS · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > HN154912 DISCREPANCY: FOUND SEAT RAIL @LBL 9 F.S 988-1005 HAS CORROSION. CORRECTIVE ACTION: REMOVED AND REPLACED SEAT RAIL P/N BA670-45074-3 @ LBL 9 F.S 988-1005 IAW CRJ 700 AMM 53-00-49-400-802 CONFIG A03
- [SDR VNAA202407120028](https://openairdocs.org/sdr/VNAA202407120028.md): Seat Track · corroded · Jul 10, 2024 · N725PS · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > HN154910 DISCREPANCY: LBL 27 SEAT RAIL IS CORRODED BETWEEN FS 1033 AND FS 1061. CORRECTIVE ACTION: REMOVED AND REPLACED LBL 27 SEAT RAIL IAW CRJ-700 SRM 53-00-49-201-002-A01 AND AMM 53-00-49-400-802-A03
- [SDR VNAA202407120027](https://openairdocs.org/sdr/VNAA202407120027.md): Seat Track · corroded · Jul 10, 2024 · N725PS · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > HN154909 DISCREPANCY: LBL 27 SEAT RAIL IS CORRODED BETWEEN FS 977 AND FS 1005. CORRECTIVE ACTION: REMOVED AND REPLACED LBL 27 SEAT RAIL IAW CRJ-700 SRM 53-00-49-201-002-A01 AND AMM 53-00-49-400-802-A03
- [SDR VNAA202407120026](https://openairdocs.org/sdr/VNAA202407120026.md): Bracket · cracked · Jul 10, 2024 · N725PS · Cndair CL6002C10 · Passenger/Crew Doors
  > HN153304 DISCREPANCY: PAX DOOR BRACKET AT FWD CAM LATCH ASSY. FOUND TO BE CRACKED. CORRECTIVE ACTION: REMOVED BROKEN BRACKET. INSTALLED NEW SERVICEABLE PAX DOOR BRACKET AT FWD CAM LATCH ASSY IAW CRJ700 SRM 51-41-02-001-001-A01 AND CRJ700 AMM 52-70-04-400-806 (
- [SDR VNAA202407120025](https://openairdocs.org/sdr/VNAA202407120025.md): Trunnion · corroded · Jul 10, 2024 · N725PS · Cndair CL6002C10 · Wing, Attach Fittings
  > HN150978 DISCREPANCY: FOUND CORROSION ON L/H INBD FLAP VANE ACTUATOR FWD TRUNNION BODY (FLS24.00) CORRECTIVE ACTION: RECEIVED NEW SERVICEABLE FLAP VANE ACTUATOR TRUNNION BODY P/N 601R14261-1.
- [SDR VNAA202407120024](https://openairdocs.org/sdr/VNAA202407120024.md): Trunnion · corroded · Jul 10, 2024 · N725PS · Cndair CL6002C10 · Wing, Attach Fittings
  > HN150977 DISCREPANCY: FOUND CORROSION ON LH I/B FLAP VANE ACTUATOR FWD TRUNNION BODY. (FLS65.50) CORRECTIVE ACTION: RECEIVED SERVICEABLE TRUNNION BODY (P/N: 601R14261-1),
- [SDR VNAA202407120023](https://openairdocs.org/sdr/VNAA202407120023.md): Trunnion · corroded · Jul 10, 2024 · N725PS · Cndair CL6002C10 · Wing, Attach Fittings
  > HN150974 DISCREPANCY: FOUND CORROSION ON R/H INBD FLAP VANE ACTUATOR FWD TRUNNION BODY (FLS24.00) CORRECTIVE ACTION: RECEIVED NEW SERVICEABLE FLAP VANE ACTUATOR TRUNNION BODY P/N 601R14261-1.
- [SDR VNAA202407120022](https://openairdocs.org/sdr/VNAA202407120022.md): Trunnion · corroded · Jul 10, 2024 · N725PS · Cndair CL6002C10 · Wing, Attach Fittings
  > HN150973 DISCREPANCY: FOUND CORROSION ON R/H INBD FLAP VANE ACTUATOR FWD TRUNNION BODY (FLS65.50) CORRECTIVE ACTION: RECEIVED NEW SERVICEABLE FLAP VANE ACTUATOR TRUNNION BODY P/N 601R14261-1. REFERENCE HR393982 FOR INSTALLATION. CERTS ATTACHED
- [SDR VNAA202407120021](https://openairdocs.org/sdr/VNAA202407120021.md): Trunnion · corroded · Jul 10, 2024 · N725PS · Cndair CL6002C10 · Wing, Attach Fittings
  > HN150971 DISCREPANCY: FOUND CORROSION ON R/H INBD FLAP VANE ACTUATOR FWD TRUNNION BODY (FLS102.90) CORRECTIVE ACTION: RECEIVED NEW SERVICEABLE FLAP VANE ACTUATOR TRUNNION BODY P/N 601R14261-1. REFERENCE HR393982 FOR INSTALLATION. CERTS ATTACHED
- [SDR VNAA202407120020](https://openairdocs.org/sdr/VNAA202407120020.md): Trunnion · corroded · Jul 10, 2024 · N725PS · Cndair CL6002C10 · Wing, Attach Fittings
  > HN150970 DISCREPANCY: FOUND CORROSION ON R/H INBD FLAP VANE ACTUATOR FWD TRUNNION BODY (FLS140.40) CORRECTIVE ACTION: RECEIVED NEW SERVICEABLE FLAP VANE ACTUATOR TRUNNION BODY P/N 601R14261-1.
- [SDR VNAA202407120019](https://openairdocs.org/sdr/VNAA202407120019.md): Cradle · corroded · Jul 10, 2024 · N725PS · Cndair CL6002C10 · Trailing Edge Flap Actuator
  > HN150969 DISCREPANCY: FOUND CORROSION ON THE R/H INBOARD FLAP VANE ACTUATOR CRADLE ASSY. (FLS24.00) CORRECTIVE ACTION: RECEIVED NEW SERVICEABLE CRADLE ASSY P/N CC670-14301 BN 30917.
- [SDR VNAA202407120018](https://openairdocs.org/sdr/VNAA202407120018.md): Cradle · corroded · Jul 10, 2024 · N725PS · Cndair CL6002C10 · Trailing Edge Flap Actuator
  > FOUND CORROSION ON R/H INBD FLAP VANE ACTUATOR CRADLE ASSY (FLS 140.40) CORRECTIVE ACTION: RECEIVED NEW SERVICEABLE CRADLE ASSY P/N CC670-14301-9 BN 309137
- [SDR VNAA202407120017](https://openairdocs.org/sdr/VNAA202407120017.md): Cradle · corroded · Jul 10, 2024 · N725PS · Cndair CL6002C10 · Trailing Edge Flap Actuator
  > HN150967 DISCREPANCY: FOUND CORROSION ON THE L/H INBOARD FLAP VANE ACTUATOR CRADLE ASSY. (FLS140.00) CORRECTIVE ACTION: RECEIVED NEW SERVICEABLE CRADLE ASSY P/N CC670-14301-9 BN 309137.
- [SDR VNAA202407120016](https://openairdocs.org/sdr/VNAA202407120016.md): Cradle · corroded · Jul 10, 2024 · N725PS · Cndair CL6002C10 · Trailing Edge Flap Actuator
  > HN00150964 DISCREPANCY: FOUND CORROSION ON L/H INBD FLAP VANE ACTUATOR CRADLE ASSY (FLS102.90 CORRECTIVE ACTION: RECEIVED NEW SERVICEABLE CRADLE ASSY P/N CC670-14301-9 BN 309137.
- [SDR VNAA202407120015](https://openairdocs.org/sdr/VNAA202407120015.md): Web · cracked · Jul 10, 2024 · N725PS · Cndair CL6002C10 · Passenger/Crew Doors
  > HN149932 DISCREPANCY: PAX DOOR FWD STAIR WEB FOUND TO BE CRACKED. CORRECTIVE ACTION: REMOVED AND REPLACED PAX DOOR FWD STAIR WEB IAW CRJ-700 SRM 51-42-06-001-001-A01, 51-40-11-001-001-A01, AND 51-42-21-001-001-A01.
- [SDR VNAA202407120014](https://openairdocs.org/sdr/VNAA202407120014.md): Bracket · damaged · Jul 10, 2024 · N725PS · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > HN00149834 DISCREPANCY: FWD INTERCOSTAL DD2 BRACKET FOUND TO HAVE ELONGATED HOLE. CORRECTIVE ACTION: DD2 BRACKET LOCATED AND DRILLED AND INSTALLED IAW CRJ700 51-40-11-001-001-A01 AND 51-42-06-001-001-A01
- [SDR VNAA202407120013](https://openairdocs.org/sdr/VNAA202407120013.md): Intercostal · corroded · Jul 10, 2024 · N725PS · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > HN00149798 DISCREPANCY: FWD INTERCOSTAL DD5 FOUND TO BE CORRODED. CORRECTIVE ACTION: PAX DOOR DD5 NEW SERVICEABLE INTERCOSTAL LOCATED AND DRILLED IAW CRJ700 SRM 51-40-11-001-001-A01. INSTALLED FWD INTERCOSTAL DD5 IAW CRJ700 SRM 51-42-06-001-001-A01.
- [SDR VNAA202407120012](https://openairdocs.org/sdr/VNAA202407120012.md): Mount Fitting · nicked · Jul 10, 2024 · N725PS · Cndair CL6002C10 · Fuselage Main, Attach Fittings
  > HN00149690 DISCREPANCY: FOUND TRIM ACTUATOR FITTING HAS NICKS ON LH I/B LUG FWD AND AFT SIDES AND RH I/B LUG FWD SIDE. CORRECTIVE ACTION: COMPLIED WITH REO 670-55-31-171 REV-- DATED 4-12-24
- [SDR VNAA202407120011](https://openairdocs.org/sdr/VNAA202407120011.md): Floor Support · cracked · Jul 10, 2024 · N725PS · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > HN149314 DISCREPANCY: FOUND LH COCKPIT FLOOR BOARD SUPPORT ANGLE @ LBL 12 ON THE ATTACH FLANGE NEXT TO THE BULKHEAD POST TO BE CRACKED. CORRECTIVE ACTION: REMOVED LH COCKPIT FLOOR BOARD SUPPORT ANGLE @ LBL 12 ON THE ATTACH FLANGE NEXT TO THE BULKHEAD POST IAW
- [SDR VNAA202407120010](https://openairdocs.org/sdr/VNAA202407120010.md): Former · corroded · Jul 10, 2024 · N725PS · Cndair CL6002C10 · Passenger/Crew Doors
  > HN148941 DISCREPANCY: PAX DOOR AFT FORMER FOUND CORRODED. CORRECTIVE ACTION: REMOVED CORRODED FORMER AND INSTALLED PAX DOOR AFT FORMER P/N 601R318034-5 IAW CRJ700 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01
- [SDR VNAA202407120009](https://openairdocs.org/sdr/VNAA202407120009.md): Door Frame · corroded · Jul 10, 2024 · N725PS · Cndair CL6002C10 · Fuselage Main, Structure
  > HN148697 DISCREPANCY: PAX DOOR FRAME AT FS320.00 FOUND TO BE CORRODED. CORRECTIVE ACTION: REMOVE CORRODED FRAME. LOCATED, DRILLED AND INSTALLED NEW PAX DOOR FRAME. PN# 601R318032-5 IAW CRJ700 SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01 AND 51-42-21-001-001-
- [SDR VNAA202407120008](https://openairdocs.org/sdr/VNAA202407120008.md): Intercostal · corroded · Jul 10, 2024 · N725PS · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > HN00148680 DISCREPANCY: FWD INTERCOSTAL DD2 FOUND TO BE CORRODED. CORRECTIVE ACTION: REMOVED DAMAGED DD2 INTERCOSTAL. LOCATED, DRILLED AND INSTALLED NEW SERVICEABLE FWD INTERCOSTAL DD2 IAW CRJ700 SRM 51-40-11-001-001-A01 AND 51-42-06-001-001-A01
- [SDR VNAA202407120007](https://openairdocs.org/sdr/VNAA202407120007.md): Floorbeam · corroded · Jul 10, 2024 · N725PS · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > HN148582 DISCREPANCY: FS 280 FRAME AFT AVIONICS BAY FLOORBOARD SUPPORT ANGLE IS CORRODED BETWEEN LBL 26 AND RBL 26. CORRECTIVE ACTION: REMOVED UNSERVICEABLE FLOORBOARD SUPPORT ANGLE IAW CRJ700 SRM 51-42-21-001-001-A01. LOCATED AND DRILLED NEW SERVICEABLE ANGLE
- [SDR VNAA202407120006](https://openairdocs.org/sdr/VNAA202407120006.md): Floorbeam · cracked · Jul 10, 2024 · N725PS · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > HN148550 DISCREPANCY: LBL9 FLIGHT COMPARTMENT FLOOR BEAM IS CRACKED ON THE FWD SIDE OF F.S. 280. CORRECTIVE ACTION: REPAIRED FLIGHT COMPARTMENT FLOOR BEAM IAW CRJ 700 SRM 53-11-43-201-003-A01
- [SDR VNAA202407120005](https://openairdocs.org/sdr/VNAA202407120005.md): Skin · corroded · Jul 10, 2024 · N725PS · Cndair CL6002C10 · Passenger/Crew Doors
  > HN148465 DISCREPANCY: PAX DOOR INNER SKIN FOUND CORRODED. CORRECTIVE ACTION: REMOVED PAX DOOR INNER SKIN. SERVICEABLE INNER SKIN LOCATED AND DRILLED IAW CRJ700 SRM 51-40-11-001-001-A01
- [SDR VNAA202407120004](https://openairdocs.org/sdr/VNAA202407120004.md): Intercostal · corroded · Jul 10, 2024 · N725PS · Cndair CL6002C10 · Passenger/Crew Doors
  > HN148463 DISCREPANCY: PAX DOOR INTERCOSTAL DD6 MID FOUND CORRODED INSIDE PAX DOOR. CORRECTIVE ACTION: REMOVED PAX DOOR DD6 MID INTERCOSTAL IAW CRJ700 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01. LOCATED DRILLED AND INSTALLED NEW SERVICEABLE PAX DOOR DD6
- [SDR VNAA202407120003](https://openairdocs.org/sdr/VNAA202407120003.md): Former · corroded · Jul 10, 2024 · N725PS · Cndair CL6002C10 · Passenger/Crew Doors
  > "HN148462 DISCREPANCY: PAX DOOR FWD FORMER FOUND CORRODED. CORRECTIVE ACTION: REMOVED PAX DOOR FWD FORMER IAW CRJ700 SRM 51-42-06-001-001-A01 AND CRJ700 SRM 51-42-21-001-001-A01 INSTALLED PAX DOOR FWD FORMER IAW CRJ700 SRM 51-42-06-001-001-A01 AND CRJ700 S
- [SDR VNAA202407120002](https://openairdocs.org/sdr/VNAA202407120002.md): Web · cracked · Jul 10, 2024 · N725PS · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > HN148432 DISCREPANCY: PAX DOOR AFT WEB FOUND CRACKED AND CORRODE. REQUIRES REPLACEMENT. CORRECTIVE ACTION: REMOVED CORRODED/CRACKED WEB. LOCATED AND DRILLED NEW AFT WEB PN 601R317071-11 IAW CRJ700 51-40-11-001-001-A01. REFERENCE TASK CARD HN00148068 FOR INSTAL
- [SDR VNAA202407120001](https://openairdocs.org/sdr/VNAA202407120001.md): Floorbeam · corroded · Jul 10, 2024 · N725PS · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > HN148044 DISCREPANCY: RBL 27 FLOOR BEAM IS CORRODED FROM 1007 TO FS 1024. CORRECTIVE ACTION: REPAIRED RBL 27 FLOOR BEAM IAW CRJ-700 SRM 53-00-41-201-001-A01 AND MHIRJ REO 670-53-61-2254 REV-- DATED 2024-04-05.
- [SDR VNAA202202161112](https://openairdocs.org/sdr/VNAA202202161112.md): Acm · odor · Feb 13, 2022 · N725PS · Cndair CL6002C10 · Cabin Cooling System
  > FLIGHT ATTENDANT REPORTED SEEING LIGHT SMOKE IN AFT CABIN PRIOR TO PUSH. CREW DEPLANED AIRCRAFT FOR INSPECTION. CREW DID NOT NEED MASKS, NO FIRE SUPPRESSION SYSTEMS USED. NO PASSENGER COMPLAINTS OR INJURIES FROM INHALATION. NO EMERGENCY DECLARED. RH PACK BLOWI
- [SDR VNAA202109021113](https://openairdocs.org/sdr/VNAA202109021113.md): Actuator · faulted · Sep 1, 2021 · N725PS · Cndair CL6002C10 · Stabilizer Control System
  > RECIEVED PITCH CONTROL MESSAGE ENROUTE TO SGF, THEY HAD TO LAND FLAPS 20 AND THEY DECLARED AN EMERGENCY. LANDED WITH NO FURTHER ISSUES. REMOVED AND REPLACED LINEAR PITCH-FEEL ACTUATOR (A140) IAW CRJ 700 AMM 27-31-23-000/400-801 A01. OPERATIONAL TEST OF THE PI
- [SDR VNAA2021070199911](https://openairdocs.org/sdr/VNAA2021070199911.md): Stringer · corroded · Jul 1, 2021 · N725PS · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > STGR 21 RH HAS MULTIPLE AREAS OF CORROSION AT FS 364.00 TO FS 394.00 AND ON PIECE JOINT. INSTALLED SERVICEABLE STRINGER AND REPAIR SPLICE IAW CRJ 700 SRM 53-00-03-991-905.
- [SDR VNAA2021070199910](https://openairdocs.org/sdr/VNAA2021070199910.md): Seat Track · corroded · Jul 1, 2021 · N725PS · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > R/H FLOOR SEAT TRACK FROM FS 677 TO FS 830 AT RBL 9 IS CORRODED. INSTALLED NEW SERVICEABLE SEAT TRACK AT FS 677 TO FS 830 AT RBL 9 IAW CRJ 700 AMM 53-00-49-400-801-A03.
- [SDR VNAA202107019999](https://openairdocs.org/sdr/VNAA202107019999.md): Seat Track · corroded · Jul 1, 2021 · N725PS · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > R/H FLOOR SEAT TRACK FROM FS 830 TO 977 AT RBL 9 IS CORRODED. REPLACED CORRODED SEAT TRACK WITH NEW SERVICEABLE SEAT TRACK AT FS 830 TO FS 977 IAW CRJ 700 AMM 53-00-49-400-801-A03.

Next page: https://openairdocs.org/aircraft/N725PS/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 = 'N725PS' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N725PS/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.