# Service difficulty reports: N341PQ

A list on [N341PQ](https://openairdocs.org/aircraft/N341PQ.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

- [SDR REXA2025102900970](https://openairdocs.org/sdr/REXA2025102900970.md): Windshield · smoke · Oct 23, 2025 · N341PQ · Cndair CL6002D24 · Window System Wiring
  > FO POWER INPUT ON HEAT WINDSHEILD SMOKING FOLLOWED QRH AND SMOKE STOPPED POWER INPUT WAS ALSO HOT TO THE TOUCH REPLACED RH WINDSHIELD W/ NEW IAW J/C 900-56-900-901 FAULT CLEARED. COMPLETED SMOKE/FUME EVENT DATA COLLECTION SHEET.
- [SDR REXA2025020500148](https://openairdocs.org/sdr/REXA2025020500148.md): Angle · cracked · Dec 31, 2024 · N341PQ · Cndair CL6002D24 · Nacelle/Pylon Miscellaneous Structure
  > CRACK ON ANGLE SUPPORT OF LEFT PYLON ON FS1031 ANGLE SUPPORT OF LEFT PYLON ON FS1031 WAS REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01 AND SRM 51-- 42-21-001-001-A01
- [SDR REXA2025020500146](https://openairdocs.org/sdr/REXA2025020500146.md): Seat Track · corroded · Dec 31, 2024 · N341PQ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON FLOOR SEAT RAIL RBL 9 BTW FS=349 TO FS=379 AT PAX CABIN DUE TO EXCESIVE DAMAGE ON FLOOR SEAT RAIL RBL 9 BTW FS=349 TO FS=379 WAS REPLACED PER CRJ-900 SRM 53-21-49-101-001-A01, AMM 53-00-49-400-801-A12 AND AMM 53-00-49-000-801-A12
- [SDR REXA2025020500145](https://openairdocs.org/sdr/REXA2025020500145.md): Support · cracked · Dec 31, 2024 · N341PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CRACK ON CORNER TO THE RH SUPPORT OF THE JB6 AT FWD EQUIPMENT COMOARTMENT RH SUPPORT OF THE JB6 AT FWD EQUIPMENT COMPARTMENT WAS REPLACED PER CRJ 900 SRM 51-42-06-001-001-A01
- [SDR REXA2025020500142](https://openairdocs.org/sdr/REXA2025020500142.md): Bracket · cracked · Dec 31, 2024 · N341PQ · Cndair CL6002D24 · Cargo/Baggage Doors
  > CRACK ON LOWER BRACKET ON AFT TRACK AT AFT BAGGAGE DOOR DAMAGED BRACKET ON AFT TRACK AT AFT BAGGAGE DOOR WERE REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01
- [SDR REXA2025020500141](https://openairdocs.org/sdr/REXA2025020500141.md): Hinge · corroded · Dec 31, 2024 · N341PQ · Cndair CL6002D24 · Fuselage, Door Hinge
  > CORROSION IN FWD AND AFT HINGE OF SILL COVER LOCATED IN FS 1000.00 AND 1047.00 AT AFT BAGGAGE BAY DOOR CUTOUT DUE TO EXCESSIVE CORROSION IN FWD AND AFT HINGE OF SILL COVER LOCATED IN FS 1000.00 AND 1047.00 AT AFT BAGGAGE BAY DOOR CUTOUT WERE REPLACED PER CRJ-
- [SDR REXA2025020500140](https://openairdocs.org/sdr/REXA2025020500140.md): Plate · corroded · Dec 31, 2024 · N341PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION ON LOWER SILL PROTECTOR PLATE AT R1 DOOR DUE TO EXCESSIVE CORROSION ON LOWER SILL PROTECTOR PLATE AT R1 WAS REPLACED BY NEW ONE AND VERIFIED PER CRJ900 SRM 53-21-23-10-002-A02 AND SRM 53-21-23-001-002-A01 ITEM 56C
- [SDR REXA2025020500139](https://openairdocs.org/sdr/REXA2025020500139.md): Angle · corroded · Dec 31, 2024 · N341PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION IN ANGLES (04 EA) LOCATED BETWEEN FS319.00 AND 349.00 IN WL 72.50 AT GALLEY SERVICE DOOR EXTERNAL CUTOUT STRUCTURE DUE TO EXCESIVE DAMAGE ON ANGLES (04 EA) & WEB MACHINED GALLEY PROTECTOR (2EAS) WERE REPLACED PER CRJ-900 SRM 53-21-23-101-002-A02 PA
- [SDR REXA2025020500138](https://openairdocs.org/sdr/REXA2025020500138.md): Support · corroded · Dec 31, 2024 · N341PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION ON SUPPORT OF HYDRAULIC LINES OF MLG LH/RH. DUE TO EXCESSIVE DAMAGE SUPPORT OF HYDRAULIC LINES OF MLG LH/RH WERE REPLACED PER CRJ900 AMM 20-21-00-910-801-A01 AND CRJ900 SRM 51-41-02-001-001-A01
- [SDR REXA2025020500137](https://openairdocs.org/sdr/REXA2025020500137.md): Hinge · corroded · Dec 31, 2024 · N341PQ · Cndair CL6002D24 · Fuselage, Door Hinge
  > CORROSION IN FITTINGS AND HINGE OF ACCESS PANEL 196ER (WASTE PANEL) FITTINGS AND HINGE OF ACCESS PANEL 196ER (WASTE PANEL) WERE REPLACED PER CRJ900 AMM 52-45-01 (CONFIGA01) AND CRJ900 SRM 51-41-02-001-001-A01 //PART MANUFACTURED (P/N:CC670-39095-3)WAS PERFOR
- [SDR REXA2025010800024](https://openairdocs.org/sdr/REXA2025010800024.md): Floor Support · corroded · Dec 31, 2024 · N341PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION ON FLOOR SILL FS319.70 AND RBL 43 AT PAX CABIN DUE TO EXCESSIVE DAMAGE, FLOOR SILL FS.280 TO FS.319 AND RBL 43 AT PAX CABIN WAS REPLACED PER CRJ-900 SRM 51-42-13-001-001-A01, SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01
- [SDR REXA2025010800022](https://openairdocs.org/sdr/REXA2025010800022.md): Support Bracket · corroded · Dec 31, 2024 · N341PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION ON SUPPORT LOCATED IN FS 897.70 AND BETWEEN STR 22R/23R AT AREA OF WASTE PANEL DUE TO EXCESIVE DAMAGE ON SUPPORT LOCATED IN FS 897.70 AND BETWEEN STR 22R/23R AT AREA OF WASTE PANEL WAS REPLACED PER CRJ-900 SRM 51-10-06-001-001-A01 AND SRM 51-41-02-0
- [SDR REXA2025010800021](https://openairdocs.org/sdr/REXA2025010800021.md): Angle · corroded · Dec 31, 2024 · N341PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION IN LOWER SILL LOCATED BETWEEN FS 319.00 AND 349.00 WL 72.50 AT GALLEY SERVICE DOOR EXTERNAL CUTOUT STRUCTURE. DUE TO EXCESIVE DAMAGE IN LOWER SILL LOCATED BETWEEN FS 319.00 AND 349.00 WL 72.50 AT GALLEY SERVICE DOOR EXTERNAL CUTOUT STRUCTURE WAS REP
- [SDR REXA2022082100678](https://openairdocs.org/sdr/REXA2022082100678.md): Charger · inoperative · Aug 15, 2023 · N341PQ · Cndair CL6002D24 · Emergency Lighting
  > L/H AFT OVERWING EXIT EXTERIOR LIGHT INOP SEE NRWC 859512 R/R ATTERY CHARGER ASSY PS37 IAW CRJ900 AMM 33-51-17 OPC GOOD P/N OFF/ON 11-0049 S/N OFF 23106 S/N ON 22680
- [SDR REXA2021071300497](https://openairdocs.org/sdr/REXA2021071300497.md): Drag Angle · cracked · Jul 10, 2021 · N341PQ · Cndair CL6002D24 · Vertical Stabilizer
  > VERT. STAB LH AFT DRAG ANGLE CRACKED. REPAIRED VERTICAL STAB LH AFT DRAG ANGLE IAW CRJ900 SRM 55-31-00-201-001-A01.
- [SDR REXA2021071300496](https://openairdocs.org/sdr/REXA2021071300496.md): Drag Angle · cracked · Jul 10, 2021 · N341PQ · Cndair CL6002D24 · Vertical Stabilizer
  > VERT. STAB RH AFT DRAG ANGLE CRACKED. REPAIRED VERTICAL STAB RH AFT DRAG ANGLE IAW SRM 55-31-00-201-001-A01.
- [SDR REXA2021071300494](https://openairdocs.org/sdr/REXA2021071300494.md): Door Sill · corroded · Jul 2, 2021 · N341PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > RH FLOOR SILL CORRODED, FS 280.00 FS 284.00. TCI 53-10-219. UPON FURTHER INVESTIGATION CORROSION FOUND TO BE ALL THE WAY THROUGH FLOOR SILL REMOVED FLOOR SILL IAW CRJ 900 SRM 51-42-21,13-06-001-001-A01. REMOVED CANNON PLUGS FROM AOA AND INTERCOM SWITCH AND D
- [SDR REXA2021071300491](https://openairdocs.org/sdr/REXA2021071300491.md): Doubler · corroded · Jun 26, 2021 · N341PQ · Cndair CL6002D24 · Fuselage Main, Plate/Skin
  > FWD LOWER TCAS ANTENNA DOUBLER CORRODED, BLO, FS 295.00 - FS 310. REMOVED AND REPLACED FWD LWR TCAS ANTENNA DOUBLER FROM FS 295 - FS 310 IAW CRJ900 SRM 51-42-21-001-001-A01, 51-42-06-001-001-A01 AND 51-40-11-001-001-A01.
- [SDR REXA2021071300490](https://openairdocs.org/sdr/REXA2021071300490.md): Frame · corroded · Jun 26, 2021 · N341PQ · Cndair CL6002D24 · Fuselage Main, Frame
  > FS 310.00 LOWER FRAME SECTOR CORRODED STGR 25L-25R. COMPLIED WITH REMAINING STEPS OF CRJ 900 SRM 53-00-06-201-006-A01.
- [SDR REXA2021071300492](https://openairdocs.org/sdr/REXA2021071300492.md): Frame · corroded · Jun 25, 2021 · N341PQ · Cndair CL6002D24 · Fuselage Main, Frame
  > FS 295.0 LOWER FRAME SECTOR CORRODED, STGR 25L - 25R. REPAIRED AREA IAW EA CRJ953-11797.
- [SDR REXA2021071300493](https://openairdocs.org/sdr/REXA2021071300493.md): Stringer · corroded · Jun 24, 2021 · N341PQ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > FS 280.00 - FS 333.00 STGR 25R CORRODED, SEVERAL SPOTS. REMOVED AND REPLACED FS 280 - FS 333 STR 25R AND SPLICE IAW CRJ 900 SRM'S 51-40-11-001-001-A01, 51-42-06-001-001-A01 AND 51-42-21-001-001- A01.
- [SDR REXA2021071300498](https://openairdocs.org/sdr/REXA2021071300498.md): Seat Track · corroded · Jun 22, 2021 · N341PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > FLOOR SEAT TRACK AT RBL9 FROM FS 349 TO FS 485 IS CORRODED. REMOVED AND REPLACED FLOOR SEAT TRACK AT RBL 9 FROM FS 349 TO FS 348 IAW CRJ 900 AMM 53-00-49-400-801-A12 AND SRM 53-00-49-201-002-A01.
- [SDR REXA2021071300495](https://openairdocs.org/sdr/REXA2021071300495.md): Floorbeam · corroded · Jun 15, 2021 · N341PQ · Cndair CL6002D24 · Fuselage Main, Floor Beam
  > FS 280.00 TRANSVERSE FLOORBEAM, COCKPIT FLOOR SUPPORT J ANGLE CORRODED. REMOVED J ASSY ANGLE AND REPLACED WITH NEW J ASSY ANGLE P/N: CC670-340095-1 IAW CRJ 900 SRM 51-42-21-001-001-A01, 51-42-06-001-001-001-A01, 51-25-16-001-001-A01, 51-21-11-001-001-A01.
- [SDR REXA2019090201281](https://openairdocs.org/sdr/REXA2019090201281.md): Light · inoperative · Sep 2, 2019 · N341PQ · Cndair CL6002D24 · Emergency Lighting
  > WHILE PERFORMING ROUTINE-900 FOUND RT FWD EMERGENCY LIGHT ON TOP OF WING OUT. RELAMPED RT FWD EMERGENCY LIGHT IAW AMM 33-51-15 P/N: 8GH005123-06.
- [SDR REXA2018080870676](https://openairdocs.org/sdr/REXA2018080870676.md): Unknown · odor · Aug 7, 2018 · N341PQ · Cndair CL6002D24 · Air Distribution System
  > ELECTRICAL BURNING ODOR IN THE FLIGHT DECK. COMPLIED WITH AMM 002736 AND FIM 21-21-00-810-806. NO FAULTS FOUND.
- [SDR REXA2018042700321](https://openairdocs.org/sdr/REXA2018042700321.md): Battery Pack · inoperative · Apr 27, 2018 · N341PQ · Cndair CL6002D24 · Emergency Lighting
  > AFT OVERWING EMERGENCY LIGHTS AND INTERIOR EMERGENCY FLOODLIGHTS FOUND INOPERATIVE. REMOVED & REPLACED THE BATTERY PACKS IAW AMM 33-51-17. OPS CHECKED GOOD.
- [SDR REXA2017122001310](https://openairdocs.org/sdr/REXA2017122001310.md): Door Sill · corroded · Dec 20, 2017 · N341PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > RT FLOOR SILL HAS CORROSION AT FS 280. REMOVED CORROSION WITH 100% MAT LOSS REPAIRED FLOOR SILL IAW SRM 53-21-43.
- [SDR REXA2017122001309](https://openairdocs.org/sdr/REXA2017122001309.md): Drag Angle · cracked · Dec 20, 2017 · N341PQ · Cndair CL6002D24 · Passenger/Crew Doors
  > PAX DOOR AFT DRAG ANGLE CRACKED. REPAIRED PAX DOOR AFT DRAG ANGLE IAW SRM 52-11-04.
- [SDR REXA2017122001308](https://openairdocs.org/sdr/REXA2017122001308.md): Angle · corroded · Dec 20, 2017 · N341PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > FLOOR PANEL SUPPORT ANGLE AT FWD SIDE OF F.S. 280 CROSSBEAM HAS CORROSION BETWEEN RBL11 AND LBL11. REMOVED AND REPLACE FLOOR PANEL SUPPORT ANGLE IAW SRM 51-42-06.
- [SDR REXA2017122001281](https://openairdocs.org/sdr/REXA2017122001281.md): Flashlight · inoperative · Dec 20, 2017 · N341PQ · Cndair CL6002D24 · Emergency Equipment
  > FWD F/A FLASHLIGHT BATTERY INDICATOR DOES NOT BLINK EVERY 5 SECONDS. REPLACED FWD F/A FLASHLIGHT ASSY IAW AMM 25-61-02-400-801-A10. PERFORMED AN OPS CHECK IAW AMM 25-61-00-710-801-A04. NO DEFECTS NOTED.
- [SDR REXA2017121901307](https://openairdocs.org/sdr/REXA2017121901307.md): Web · cracked · Dec 19, 2017 · N341PQ · Cndair CL6002D24 · Passenger/Crew Doors
  > PAX DOOR FWD WEB CRACKED IN 2 EA PLACES AT RADIUS OF MID STEP. REPAIRED PAX DOOR FWD WEB IAW SRM 52-11-04.
- [SDR REXA2017121901306](https://openairdocs.org/sdr/REXA2017121901306.md): Web · cracked · Dec 19, 2017 · N341PQ · Cndair CL6002D24 · Passenger/Crew Doors
  > PAX DOOR AFT WEB CRACKED IN 2 EA PLACES AT RADIUS OF MID STEP. REPAIRED PAX DOOR AFT WEB IAW SRM 52-11-04.
- [SDR REXA2017081600888](https://openairdocs.org/sdr/REXA2017081600888.md): Fire Bottle · leaking · Aug 16, 2017 · N341PQ · Cndair CL6002D24 · Fire Bottle, Portable
  > DURING EE-900 FOUND AFT FIRE EXTINGUISHER LEAKING. R&R AFT FIRE EXTINGUISHER PER EE-900 JOB CARD.
- [SDR REXA2016110102131](https://openairdocs.org/sdr/REXA2016110102131.md): Smoke Detector · no test · Nov 1, 2016 · N341PQ · Cndair CL6002D24 · Smoke Detection
  > FA REPORTED AFT LAVATORY SMOKE DETECTOR WILL NOT TEST. REMOVED & REPLACED THE SMOKE DETECTOR IAW AMM 26-16-01 OPS TESTED GOOD.
- [SDR REXA2015012500074](https://openairdocs.org/sdr/REXA2015012500074.md): Mechanism · out of adjust · Jan 25, 2015 · N341PQ · Cndair CL6002D24 · Passenger/Crew Doors
  > MAIN CABIN PAX DOOR WILL NOT OPEN FROM INSIDE. ADJUSTED PAX DOOR INNER HANDLE DETENT ROLLER MECHANISM IAW AMM 52-11-02. OPERATIONS CHECKED GOOD. NO FURTHER DEFECTS NOTED. OK FOR SERVICE.

## 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 = 'N341PQ' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N341PQ/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.
