# Service difficulty reports: N325PQ

A list on [N325PQ](https://openairdocs.org/aircraft/N325PQ.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 2 · 81 reports

- [SDR REXA2025100700904](https://openairdocs.org/sdr/REXA2025100700904.md): Lamp · inoperative · Oct 2, 2025 · N325PQ · Cndair CL6002D24 · Emergency Lighting
  > #8 EXTERNAL EMERGENCY LIGHT INOP REMOVED AND REPLACED #8 EXTERNAL EMERGENCY LIGHT LAMP IN REF TO AM 33-51-15. OPS CHECK GOOD AT THIS TIME.
- [SDR REXA2024100700856](https://openairdocs.org/sdr/REXA2024100700856.md): Door Frame · cracked · Oct 4, 2024 · N325PQ · Cndair CL6002D24 · Fuselage Main, Structure
  > L/H AFT OVER WING EMERGENCY EXIT DOOR (SN SB1485) CRACKED AT BASE OF UPPER AFT SWITCH TARGET. REPAIRED L/H AFT OVER WING EMERGENCY EXIT DOOR IAW ENDEAVOR EA CRJ952-17346 REV. IR DATED 9/25/2024.
- [SDR REXA2024100700855](https://openairdocs.org/sdr/REXA2024100700855.md): Door Frame · cracked · Oct 4, 2024 · N325PQ · Cndair CL6002D24 · Fuselage Main, Structure
  > L/H FWD OVER WING EMERGENCY EXIT DOOR (SN SB1487) CRACKED AT BASE OF UPPER AFT SWITCH TARGET. REPAIRED L/H FWD OVER WING EMERGENCY. EXIT DOOR IAW ENDEAVOR EA CRJ952-17345 REV. IR DATED 9/25/2024
- [SDR REXA2024100700854](https://openairdocs.org/sdr/REXA2024100700854.md): Skin · chafed · Sep 28, 2024 · N325PQ · Cndair CL6002D24 · Fuselage Main, Plate/Skin
  > THE OUTER LOWER SKIN IS CHAFED BETWEEN FS 897 AND FS 913 STGR 27. UPON FURTHER INVESTIGATION DAMAGE WAS FOUND TO BE ON AN EXISTING DOUBLER AT F.S. 897 - F.S. 913 INSTALLED TO ENDEAVOR EA CRJ953-11279 REV IR. DAMAGE WAS FOUND TO BE OUT OF LIMITS PER ENGINEERIN
- [SDR REXA2024100400840](https://openairdocs.org/sdr/REXA2024100400840.md): Door Frame · cracked · Sep 28, 2024 · N325PQ · Cndair CL6002D24 · Fuselage Main, Structure
  > R/H AFT OVERWING EMER. EXIT DOOR (SN SB1488) CRACKED AT BASE OF UPPER AFT SWITCH TARGET. REPAIRED RH AFT EMERGENCY EXIT DOOR TOP EDGE MEMBER IAW ENDEAVOR AIR EA CRJ952-17347 REV. IR DATED 9/25/2024.
- [SDR REXA2024100400839](https://openairdocs.org/sdr/REXA2024100400839.md): Door Frame · cracked · Sep 28, 2024 · N325PQ · Cndair CL6002D24 · Fuselage Main, Structure
  > R/H FWD OVERWING EMER. EXIT DOOR (SN SB1486) CRACKED AT BASE OF UPPER AFT SWITCH TARGET. REPAIRED RH FWD EMERGENCY EXIT DOOR TOP EDGE MEMBER IAW ENDEAVOR AIR EA CRJ952-17348 REV. IR DATED 9/25/2024.
- [SDR REXA2024093000747](https://openairdocs.org/sdr/REXA2024093000747.md): Floorbeam · corroded · Sep 28, 2024 · N325PQ · Cndair CL6002D24 · Fuselage Main, Floor Beam
  > L/H FS280 CROSSBEAM CORRODED. REMOVED LH CROSSBEAM @ FS 280 IAW CRJ 900 SRM 51-42-06-001-001-A01, 51-42-13-001-001-A01, 51-42-21-001-001-A01, 51-42-22-001-001-A01. LOCATED AND DRILLED SERVICEABLE LH FS 280 CROSSBEAM IAW CRJ 900 SRM 51-40-11-001-001-A01. INSTA
- [SDR REXA2024093000745](https://openairdocs.org/sdr/REXA2024093000745.md): Floorbeam · corroded · Sep 28, 2024 · N325PQ · Cndair CL6002D24 · Fuselage Main, Floor Beam
  > FS280 CROSS BEAM CORRODED AROUND FASTENERS AT RBL9. REMOVED FS 280 RH CROSSBEAM (PN# CC670-34010-970) IAW CRJ900 SRM 51-42-06-001-001-A01, 51-42-13-001-001-A01, AND 51-42-21-001-001-A01. LOCATED AND DRILLED NEW SERVICEABLE FS 280 RH CROSSBEAM (PN# CC670-34094J
- [SDR REXA2024100300828](https://openairdocs.org/sdr/REXA2024100300828.md): Floorbeam · cracked · Sep 18, 2024 · N325PQ · Cndair CL6002D24 · Fuselage Main, Floor Beam
  > R/H COCKPIT FLOOR BEAM RBL 12.50 FOUND TO BE CRACKED ON LWR OB SIDE @ FS 280. REPAIRED R/H COCKPIT FLOOR BEAM RBL 12.50 OB SIDE @ FS 280 IAW MHIRJ REO 690-53-11-1852 REV DATED 2024-09-19.
- [SDR REXA2024100100752](https://openairdocs.org/sdr/REXA2024100100752.md): Handle · cracked · Sep 16, 2024 · N325PQ · Cndair CL6002D24 · Electrical/Electronic Compartment Doors
  > MAIN AVIONICS COMPARTMENT DOOR HANDLE FAILED NDT AND REQUIRES REPAIR/REPLACEMENT. REMOVED HANDLE HOUSING FROM AVI. BAY DOOR IAW CRJ 900 SRM 51-42-21-001-001-A01. INSTALLED SERVICEABLE HANDLE HOUSING (P/N: H3445-5, S/N: 1311) ON AVI. BAY DOOR IAW CRJ 900 SRM 5
- [SDR REXA2024093000741](https://openairdocs.org/sdr/REXA2024093000741.md): Floorbeam · corroded · Sep 16, 2024 · N325PQ · Cndair CL6002D24 · Fuselage Main, Floor Beam
  > "FLOOR PANEL SUPPORT ANGEL (""J"") CORRODED AT FS280 BETWEEN RBL9 AND LBL9. REMOVED AND INSTALLED NEW SERVICEABLE J ANGLE (PN# CC670-34095-1SB) IAW CRJ900 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01."
- [SDR REXA2021041600240](https://openairdocs.org/sdr/REXA2021041600240.md): Stringer · corroded · Apr 12, 2021 · N325PQ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > FOUND STRINGER 21R AFT OF FS 333 TO BE CORRODED. REMOVED, LOCATED, DRILLED AND INSTALLED A NEW SERVICEABLE STRINGER P/N SH670-31383-1S IAW CRJ 900 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01 AND 51-40-11-001-001-A01.
- [SDR REXA2021041500221](https://openairdocs.org/sdr/REXA2021041500221.md): Support · corroded · Apr 10, 2021 · N325PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > RIGHT SIDE JACK FITTING SUPPORT INTERCOSTAL IS CORRODED ON LOWER FLANGE BETWEEN FS 280 TO FS 265. REMOVED AND REPLACED RH SIDE JACK FITTING SUPPORT INTERCOSTAL IAW EA CRJ 953-11379 REV IR DATED 3-25-21.
- [SDR REXA2021041600218](https://openairdocs.org/sdr/REXA2021041600218.md): Frame · corroded · Apr 10, 2021 · N325PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > FS 349.00 LOWER FRAME SECTOR STGR 24RH - 27LH CORRODED. REMOVED FRAME AT FS 349 IAW CRJ 900 SRM 51-42-06-001-001-A01 AND INSTALLED IAW SRM 51-42-06-001-001-A01 AND SRM 51-40-11-001-001-A01.
- [SDR REXA2021041600244](https://openairdocs.org/sdr/REXA2021041600244.md): Frame · damaged · Apr 9, 2021 · N325PQ · Cndair CL6002D24 · Fuselage Main, Frame
  > DURING INSTALLATION OF NEW FS 310 FRAME THE SECTOR @ STR 19R-28R HAS ONE FASTENER WITH LOW ED. REPAIRED IAW ENDEAVOR EA CRJ 953-11361 REV A.
- [SDR REXA2021041600243](https://openairdocs.org/sdr/REXA2021041600243.md): Stringer Splice · corroded · Apr 9, 2021 · N325PQ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > FOUND STRINGER 23R PLUS SPLICE ANGLE FROM FS 280 TO 333 TO BE CORRODED. REMOVED AND REPLACED STR 23R IAW AND SPLICE CRJ 900 SRM 51-42-06-001- 001-A01, 51-42-21-001-001-A01, 51-40-11-001-001-A01, AND 51-42-06-001-001-A01, 51-40-11-001-001-A01.
- [SDR REXA2021041600242](https://openairdocs.org/sdr/REXA2021041600242.md): Stringer · corroded · Apr 9, 2021 · N325PQ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > FOUND STRINGER 23R PLUS SPLICE ANGLE FROM FS 280 TO 333 TO BE CORRODED. REMOVED AND REPLACED STR 23R IAW AND SPLICE CRJ 900 SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01, 51-40-11-001-001-A01, AND 51-42-06-001-001-A01, 51-40-11-001-001-A01.
- [SDR REXA2021041600235](https://openairdocs.org/sdr/REXA2021041600235.md): Stringer · corroded · Apr 8, 2021 · N325PQ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > FOUND STRINGER 21 R/H FROM FS 333 TO 379 PLUS SPLICE ANGLE TO BE CORRODED. REMOVED,LOCATED,DRILLED, AND INSTALLED STRINGER 21 RH PLUS STRINGER SPLICE ANGLE BETWEEN FS 333 TO 379 IAW CRJ 900 SRM 51-42-06-0
- [SDR REXA2021041600234](https://openairdocs.org/sdr/REXA2021041600234.md): Stringer · corroded · Apr 8, 2021 · N325PQ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > FOUND STRINGER 21 R/H FROM FS 333 TO 379 PLUS SPLICE ANGLE TO BE CORRODED. REMOVED,LOCATED,DRILLED, AND INSTALLED STRINGER 21 RH PLUS STRINGER SPLICE ANGLE BETWEEN FS 333 TO 379 IAW CRJ 900 SRM 51-42-06-001-001-A01 P/N SH670-31197-1 AND SH670-31636-1.
- [SDR REXA2021041600229](https://openairdocs.org/sdr/REXA2021041600229.md): Frame · corroded · Apr 8, 2021 · N325PQ · Cndair CL6002D24 · Fuselage Main, Frame
  > BS 310 FRAME CORRODED BETWEEN STRINGER 19R AND 18R. REMOVED AND REPLACED 310 FRAME IAW CRJ 900 SRM 51-42-06-001-001-A01 51-42-21-001-001-A01, 51-42-06-001-001-A01 AND CRJ 900 SRM 51-42-21-001-001-A01.
- [SDR REXA2021041600224](https://openairdocs.org/sdr/REXA2021041600224.md): Channel · corroded · Apr 8, 2021 · N325PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION FS 290.00 BELOW WL 72.50@ ANTENNA @ CANNON PLUG AND SURROUNDING AREA. REFERENCE JOB:81532511 OP:522 FOR REPLACEMENT OF TCAS ANTENNA REPLACED P/N SH670-32364-5 IAW SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01.
- [SDR REXA2021041500107](https://openairdocs.org/sdr/REXA2021041500107.md): Receptacle · cracked · Apr 8, 2021 · N325PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > EXTERNAL A/C POWER RECEPTACLE BOX IS CRACKED. REMOVED AND REPLACED NEW RECEPTICAL BOX IAW CRJ 900 SRM 51-42-06-001-001-A01 LOCATED AND DRILLED PART IAW CRJ 900 SRM 51-40-11-001-001-A01.
- [SDR REXA2021041600217](https://openairdocs.org/sdr/REXA2021041600217.md): Cup · gouged · Apr 5, 2021 · N325PQ · Cndair CL6002D24 · Passenger/Crew Doors
  > PAX DOOR FWD & AFT RETAINING CUPS ARE NICKED GOUGED ON I/B FLANGES. UPON FURTHER INVESTIGATION IT WAS FOUND FWD RETAINING CUP TO HAVE PAINT DAMAGE ONLY,TREATED,PRIMED, AND PAINTED FWD RETAINING CUP IAW CRJ 900 SRM 51-25-00-001-001-A01 ALSO RMEOVED AND REPLACE
- [SDR REXA2021041600219](https://openairdocs.org/sdr/REXA2021041600219.md): Doubler · corroded · Apr 4, 2021 · N325PQ · Cndair CL6002D24 · Fuselage Main, Plate/Skin
  > R/H LOWER ATC ANTENNA DOUBLER IS CORRODED. REMOVED & INSTALLED SERVICEABLE ATC DOUBLER BY LOCATING & DRILLING IAW CRJ 900 SRM 51-40-11-001-001-A01, 51-23-00-001-001-A01, 51-42-06-001- 001-A01 & REMOVED & INSTALLED LOWER ATC ANTENNA IAW ENDEAVOR TS# 001193 I
- [SDR REXA2021041600227](https://openairdocs.org/sdr/REXA2021041600227.md): Intercostal · corroded · Apr 3, 2021 · N325PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > FOUND INTERCOSTAL BETWEEN FS310 AND 364 AT STRG20 TO BE CORRODED BEYOND ALLOWABLE LIMITS. REPLACEMENT REQUIRED. 3EA. REMOVED AND REPLACED INTERCOSTAL BETWEEN FS 310 AND 364 AT STR 19R THREE INTERCOSTALS IAW CRJ 900 SRM 51-40-11-001-001-A01 AND 51-42-06-001-00
- [SDR REXA2021041600216](https://openairdocs.org/sdr/REXA2021041600216.md): Intercostal · corroded · Apr 3, 2021 · N325PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > ALL 4 INTERCOSTALS FWD OF AVIONICS SURROUND FS 364.00 - FS 349.00 STGR 25LH - 25RH CORRODED. REMOVED & REPLACED 4 INTERCOSTALS @ FS 364.00-349.00 STGR 25 LH-25 R/H IAW CRJ 900 SRM 57-42-06-001-001-A01 NO DEFECTS NOTED.
- [SDR REXA2021041600215](https://openairdocs.org/sdr/REXA2021041600215.md): Intercostal · corroded · Apr 3, 2021 · N325PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > ALL 4 INTERCOSTALS FWD OF AVIONICS SURROUND FS 364.00 - FS 349.00 STGR 25LH - 25RH CORRODED. REMOVED & REPLACED 4 INTERCOSTALS @ FS 364.00-349.00 STGR 25 LH-25 R/H IAW CRJ 900 SRM 57-42-06-001-001-A01 NO DEFECTS NOTED.
- [SDR REXA2021041600245](https://openairdocs.org/sdr/REXA2021041600245.md): Support Angle · bent · Apr 1, 2021 · N325PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > L/H LIGHTENING DIVERTER SUPPORT ANGLE BENT. LOCATED, DRILLED AND INSTALLED NEW L/H LIGHTENING DIVERTER SUPPORT ANGLE IAW CRJ 900 SRM 51-40-11-001-001-A01, SRM 51-42-06-001-001-A01 AND 51-42-13-001-001-A01 PN: SH670-33332-5.
- [SDR REXA2021041600230](https://openairdocs.org/sdr/REXA2021041600230.md): Floorbeam · corroded · Apr 1, 2021 · N325PQ · Cndair CL6002D24 · Fuselage Main, Floor Beam
  > L/H 280 BEAM CORRODED BEYOND LIMITS. REQUIRES REPLACEMENT. REMOVED AND REPLACED CORRODED 280 BEAM WITH NEW SERVICEABLE 280 BEAM IAW CRJ 900 SRM 51-42-13-001-001-A01,51-42-21-001-001-A01,AND 51-42-06-001-001-A01.
- [SDR REXA2021041600228](https://openairdocs.org/sdr/REXA2021041600228.md): Frame · corroded · Apr 1, 2021 · N325PQ · Cndair CL6002D24 · Fuselage Main, Frame
  > FOUND FRAME SECTOR 364 BETWEEN STRINGER 18R AND 20R PLUG REINFORCEMENT ANGLE TO BE CORRODED. REPAIRED CENTER FS 364 FRAME IAW CRJ 900 SRM 51-42-06-001-001-A01,51-42-21-001-001-A01 FRAME AND REINFORCEMENT ANGLE FABRCATED IAW MHIRJ SNIEO SH670-31070-501,SH670-3
- [SDR REXA2021041600220](https://openairdocs.org/sdr/REXA2021041600220.md): Frame · corroded · Apr 1, 2021 · N325PQ · Cndair CL6002D24 · Fuselage Main, Frame
  > FS 364 FRAME IS CORRODED BETWEEN STGR 26R AND 25R ON LOWER FLANGE. REPAIRED FS 364 CORROSION BETWEEN STR 26R AND 25R ON LOWER FLANGE IAW ENDEAVOR EA CRJ 953-11206 REV IR DATE 2-15-21.
- [SDR REXA2021041600231](https://openairdocs.org/sdr/REXA2021041600231.md): Frame · corroded · Mar 31, 2021 · N325PQ · Cndair CL6002D24 · Fuselage Main, Frame
  > FS FRAME 319 CORRODED BETWEEN STRINGER 18 AND 19R. REMOVED UNSERVICEABLE FS FRAME 319 IAW CRJ 900 SRM 51-42-06-001-001- AND 51-42-21-001-001-A01. RECEIVED LOCATED, DRILLED AND INSTALLED NEW SERVICEABLE FS 319 FRAME P/N SH 670-32029-3 IAW CRJ 900 SRM 51-40-1
- [SDR REXA2021041600226](https://openairdocs.org/sdr/REXA2021041600226.md): Seat Track · corroded · Mar 31, 2021 · N325PQ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > RH SIDEWALL SEAT RAIL HAS MINOR CORROSION BETWEEN FS 849.00 AND FS 865.00. REMOVED AND INSTALLED FABRICATED SEAT RAIL IAW CRJ 900 AMM 53-00-99-000(A12). FABRICATED SEAT RAIL IAW 670-53-00-343 REV M 20
- [SDR REXA2021041600233](https://openairdocs.org/sdr/REXA2021041600233.md): Longeron · corroded · Mar 30, 2021 · N325PQ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > LONGERON 23 RH LOCATED BETWEEN FS 333 AND FS 364 IS CORRODED. UPON FURTHER INVESTIGATION FOUND CORRODED LONGERON TO BE AT STR 25 RH LOCATED, DRILLED AND INSTALLED IAW CRJ 900 SRM 51-42-06-001-001-A01 AND 51-40-11-001-001-A01.
- [SDR REXA2021041600241](https://openairdocs.org/sdr/REXA2021041600241.md): Stringer · corroded · Mar 29, 2021 · N325PQ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > FOUND STRINGER 19R AFT OF FS 349 TO 364 TO BE CORRODED. REPAIRED STRINGER BETWEEN FS 349-364 IAW CRJ 900 SRM 53-00-03-201-001-A02.
- [SDR REXA2021041500109](https://openairdocs.org/sdr/REXA2021041500109.md): Drag Angle · cracked · Mar 29, 2021 · N325PQ · Cndair CL6002D24 · Vertical Stabilizer
  > L/H VERT STAB AFT DRAG ANGLE, POSSIBLE CRACK. REPAIRED UFRT STAB L/H AFT DRAG ANGLE IAW CRJ 900 SRM 55-31-00-201-001-A01. WVAC EMP STAMP #769 MTC
- [SDR REXA2021041500108](https://openairdocs.org/sdr/REXA2021041500108.md): Angle · cracked · Mar 29, 2021 · N325PQ · Cndair CL6002D24 · Vertical Stabilizer
  > RH VERT STAB AFT DRAG ANGLE, POSSIBLE CRACK. REPAIRED UFRT STAB RH RT DRAG ANGLE (AFT) IAW CRJ 900 SRM 55-31-00-201-001-A01.
- [SDR REXA2021041500111](https://openairdocs.org/sdr/REXA2021041500111.md): Attach Fitting · chafed · Mar 28, 2021 · N325PQ · Cndair CL6002D24 · Fuselage Main, Attach Fittings
  > RH STUB FAIRING ATTACH BRACKET ON WING IS CHAFED. REMOVED AND REPLACED BRACKET IAW CRJ 900 SRM 51-42-21-001-001-A01.
- [SDR REXA2021041500110](https://openairdocs.org/sdr/REXA2021041500110.md): Attach Bracket · chafed · Mar 25, 2021 · N325PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > LH STUB FAIRING ATTACH BRACKET ON WING IS CHAFED. REPLACED L/H STUB FAIRING ATTACH BRACKET IAW CRJ 900 SRM 51-42-21-001-001-A01 NO DEFECTS NOTED.
- [SDR REXA2021041600223](https://openairdocs.org/sdr/REXA2021041600223.md): Strap · corroded · Mar 17, 2021 · N325PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > GALLEY SERVICE DOOR BELOW FLOOR OUTER STRAP @ FS 310 HAS TWO SMALL AREAS OF CORROSION. REMOVED, LOCATED, DRILLED AND INSTALLED A NEW SERVICEABLE GALLEY SERVICE DOOR BELOW FLOOR OUTER STRAP AT FS 310 IAW CRJ 900 SRM 51-40-11-001-001-A01 AND 51-42-21-001-001-A
- [SDR REXA2021041500222](https://openairdocs.org/sdr/REXA2021041500222.md): Angle · corroded · Mar 15, 2021 · N325PQ · Cndair CL6002D24 · Fuselage Main, Floor Beam
  > FS 280 CROSSBEAM J ANGLE CORRODED. RECEIVED PART CERTIFICATION FOR ANGLE P/N CC670-34095-3S AND ATTACHED TO JOB CARD 81532511 OP #257.
- [SDR REXA2021041600239](https://openairdocs.org/sdr/REXA2021041600239.md): Stringer · corroded · Mar 12, 2021 · N325PQ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > FOUND STGR 21 FWD RH FROM FS 280 TO 333 TO BE CORRODED. ALSO SPLICE ANGLE IS CORRODED AT FS 333. REMOVED, LOCATED, DRILLED AND INSTALLED A NEW SERVICEABLE STRINGER P/N: SH670-81636-1 IAW CRJ 900 SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01 AND 51-40-11-001
- [SDR REXA2021041600238](https://openairdocs.org/sdr/REXA2021041600238.md): Stringer · corroded · Mar 12, 2021 · N325PQ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > FOUND STGR 21 FWD RH FROM FS 280 TO 333 TO BE CORRODED. ALSO SPLICE ANGLE IS CORRODED AT FS 333. REMOVED, LOCATED, DRILLED AND INSTALLED A NEW SERVICEABLE STRINGER P/N: SH670-81636-1 IAW CRJ 900 SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01 AND 51-40-11-001
- [SDR REXA2021041600237](https://openairdocs.org/sdr/REXA2021041600237.md): Stringer · corroded · Mar 12, 2021 · N325PQ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > FOUND STRINGER 22R FWD FS. 349 TO 333 TO BE CORRODED, ALSO SPLICE ANGLE IS CORRODED AF FS. 333. REMOVED, LOCATED, DRILLED AND INSTALLED NEW SERVICEABLE STRINGERS IAW CRJ 900 SRM 51-42-06-001-001-A01 AND 51-40-11-001-001-A01, PN 670-31379-1. STRINGER SPLICE AN
- [SDR REXA2021041600236](https://openairdocs.org/sdr/REXA2021041600236.md): Stringer Splice · corroded · Mar 12, 2021 · N325PQ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > FOUND STRINGER 22R FWD FS. 349 TO 333 TO BE CORRODED, ALSO SPLICE ANGLE IS CORRODED AF FS. 333. REMOVED, LOCATED, DRILLED AND INSTALLED NEW SERVICEABLE STRINGERS IAW CRJ 900 SRM 51-42-06-001-001-A01 AND 51-40-11-001-001-A01, PN 670-31379-1. STRINGER SPLICE AN
- [SDR REXA2021041600225](https://openairdocs.org/sdr/REXA2021041600225.md): Seat Track · corroded · Mar 12, 2021 · N325PQ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT RAIL AT LBL 9 MULTIPLE SPOTS OF CORROSION FROM FS 379.0 TO FS 394.00. REMOVED, FABRICATED AND REPLACED SEAT TRACK FROM FS 364.00 TO 485.0 LBL 9.0 IAW CRJ 900 AMM 53-00-000/400-801-A12 AND REO 670-53-00-343 DATED 2019-07-16.
- [SDR REXA2021041600232](https://openairdocs.org/sdr/REXA2021041600232.md): Panel · bent · Mar 11, 2021 · N325PQ · Cndair CL6002D24 · Trailing Edge Flaps
  > UPON INSPECTION OF LH I/B MFS, FOUND WING PANEL FWD OF MFS TO BE BENT. INSTALLED NEW SERVICEABLE SEAL AND CHANNEL IAW CRJ 900 SRM'S 51-42-06-001-001-A01, 51-42-13-001-001-A01 AND 51-25-01-001-001-A01.
- [SDR REXA2021041500112](https://openairdocs.org/sdr/REXA2021041500112.md): Floor Support · corroded · Mar 11, 2021 · N325PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > R/H 280 TO 319 FS FLOOR SILL CORRODED. REMOVED, LOCATED AND DRILLED NEW SERVICEABLE R/H 280 FLOOR SILL P/N: SH 670-32-172-11 IAW CRJ 900 SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01, 51-42-13-001-001-A01, AND 51-92-21-001-001-A01 & INSTALL NEW SERVICEABLE
- [SDR REXA2021041500105](https://openairdocs.org/sdr/REXA2021041500105.md): Stringer · corroded · Mar 11, 2021 · N325PQ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > STRINGER 19R BETWEEN FS280.00 AND 310.00 CORRODED. REMOVED, LOCATED, DRILLED AND INSTALLED NEW SERVICEABLE STRINGER 19R BETWEEN FS 280.00-310.00 IAW CRJ 900 SRM 51-42-06-001-001-A01, 51-42-21001-001-A01, 51-40-11-001-01-A01.
- [SDR REXA2021041500098](https://openairdocs.org/sdr/REXA2021041500098.md): Seat Track · corroded · Mar 11, 2021 · N325PQ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > LH SIDEWALL SEAT RAIL HAS MINOR CORROSION BETWEEN FS 629.00 AND FS 645.00. FABRICATED NEW SEAT TRACK FOR L/H SIDEWALL IAW CRJ 900 SRM 53-00-49-201-002-A01 AND 51-40-11-001-001-A01. REMOVE AND INSTALLED IAW AMM 53-00-49-400-000-801-A02.

Next page: https://openairdocs.org/aircraft/N325PQ/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 = 'N325PQ' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N325PQ/reports

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