# Service difficulty reports: N329PQ

A list on [N329PQ](https://openairdocs.org/aircraft/N329PQ.md).

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

- [SDR REXA2024103001169](https://openairdocs.org/sdr/REXA2024103001169.md): Floorbeam · corroded · Oct 29, 2024 · N329PQ · Cndair CL6002D24 · Fuselage Main, Floor Beam
  > LH CENTER COCKPIT FLOOR BEAM @ LBL 12.00 IS CRACKED AT 280 CONNECTION POINT. REPAIR TO CENTER COCKPIT FLOOR BEAM AT LBL 12.00 AT F.S. 280 IAW MHIRJ REO 690-53-11-1879, REV --, DATED 2024-10-22.
- [SDR REXA2024111101461](https://openairdocs.org/sdr/REXA2024111101461.md): Angle · corroded · Oct 25, 2024 · N329PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > GALLEY SERVICE DOOR LOWER SILL ANGLE IS HEAVILY CORRODED BETWEEN FS319 AND FS349. REMOVED AND REPLACED GALLEY SERVICE DOOR LOWER SILL ANGLE PN: SH670-31986-1 IAW CRJ900 SRM TASKS 51-42-06-001-001-A01 AND 51-42-21-001-001-A01.
- [SDR REXA2024102400947](https://openairdocs.org/sdr/REXA2024102400947.md): Angle · cracked · Oct 20, 2024 · N329PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > UPON REMOVAL OF LH FS 280 WEB FOUND WEB ANGLE PN:(CC670-34117-3) TO HAVE A DAMAGED FASTENER HOLE. LOCATE DRILLED AND INSTALLED NEW SERVICEABLE LH FS WEB ANGLE PN:(CC670-34117-5) IAW CRJ 900 SRM 51-42-06-001-001-A01 AND 51-40-11-001-001-A01.
- [SDR REXA2024110801443](https://openairdocs.org/sdr/REXA2024110801443.md): Floorbeam · cracked · Oct 17, 2024 · N329PQ · Cndair CL6002D24 · Fuselage Main, Floor Beam
  > RH CENTER COCKPIT FLOOR BEAM AT RBL 12.00 IS CRACKED AT 280 CONNECTION POINT. REPAIRED CONNECTION POINT. AT RBL12.00 AND FS280.00 IAW MHIRJ REO 690-53-11-1873 REV-- DATED 2024-10-17.
- [SDR REXA2024110501421](https://openairdocs.org/sdr/REXA2024110501421.md): Angle · corroded · Oct 17, 2024 · N329PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > "PASSENGER DOOR LOWER SILL ANGLE IS HEAVILY CORRODED BETWEEN F.S.310 TO F.S.349 PAX DOOR LOWER SILL ANGLE (KICK PLATE) HAS CORROSION ENTIRE THE CROSS-SECTIONAL ON BOTH SIDE OF THE ANGLE, 100% CORRODED IN SOME SPOT. FOUND TO BE ""OUT OF LIMITS"" IAW CRJ-900 S
- [SDR REXA2024102901128](https://openairdocs.org/sdr/REXA2024102901128.md): Angle · corroded · Oct 16, 2024 · N329PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > "280 J-ANGLE IS CORRODED IN MULTIPLE AREAS BETWEEN LBL9 AND RBL9 F.S. 280 ""J"" ANGLE P/N: CC670-34095-1 FOUND TO BE EXCESSIVELY CORRODED WITH NO ALLOWABLE DAMAGE LIMITS PROVIDED IN SRM. ANGLE REQUIRES REPLACEMENT. RECEIVED LOCATED AND DRILLED SERVICEABLE J-A
- [SDR REXA2024102801087](https://openairdocs.org/sdr/REXA2024102801087.md): Floorbeam · corroded · Oct 16, 2024 · N329PQ · Cndair CL6002D24 · Fuselage Main, Floor Beam
  > RH 280 CROSSBEAM SHOWS SIGN OF CORROSION IN MULTIPLE AREAS FROM RBL42 TO BL0 RH FS 280 CROSSBEAM (PN# CC670-34010-970 IS CORRODED BEYOND REPAIRABLE LIMITS DUE TO CORROSION THROUGH THE EXTRUDED RADIUS. NO LIMITATIONS PROVIDED IN SRM. INSTALLED NEW SERVICEABLE R
- [SDR REXA2024102801086](https://openairdocs.org/sdr/REXA2024102801086.md): Floorbeam · corroded · Oct 16, 2024 · N329PQ · Cndair CL6002D24 · Fuselage Main, Floor Beam
  > LH 280 CROSSBEAM SHOWS SIGNS OF CORROSION IN MULTIPLE AREAS FROM LBL42 TO BL0 REMOVED CORROSION ON L/H FS280 CROSSBEAM (PN# CC670-34010-969) IAW CRJ900SRM 51-21-06-001-001-A01, DEEP PITTING IN ONE LOCATIONS WHERE UP TO 100% MATERIAL LOSS WAS FOUND. DUE TO THE
- [SDR REXA2021061100416](https://openairdocs.org/sdr/REXA2021061100416.md): Handle · cracked · Jun 3, 2021 · N329PQ · Cndair CL6002D24 · Emergency Exits
  > LEFT HAND AFT EMERGENCY OVERWING EXIT LOWER HAND WAS FOUND TO BE UNSERVICEABLE. REPLACED L/H AFT EMERGENCY OVERWING EXIT LOWER HANDLE WITH SERVICEABLE PART IAW CRJ900 AMM 25-26-09-000-802-A02 AND 25-26-09-400-802-A02.
- [SDR REXA2021061100417](https://openairdocs.org/sdr/REXA2021061100417.md): Floorbeam · corroded · May 24, 2021 · N329PQ · Cndair CL6002D24 · Fuselage Main, Floor Beam
  > FS 280 BEAM CORRODED BETWEEN LD12 AND RL12. REMOVED AND REPLACED WITH NEW SERVICEABLE L/H AND R/H CROSSBEAMS AND APPLIED PAINT AND CIC IAW CRJ 900 SRM 51-77-00-001-001-AO1, SRM 51-40-11-001-001(A01), SRM 51-42-06-001-001-A01, 51-42-22-001-001-A01.
- [SDR REXA2021061100414](https://openairdocs.org/sdr/REXA2021061100414.md): Crossbeam · corroded · May 24, 2021 · N329PQ · Cndair CL6002D24 · Fuselage Main, Structure
  > FS 280.00 FWD J ANGLE CORRODED IN MULTIPLE PLACES. REMOVED AND INSTALLED NEW FS 280.00 J ANGLE AND INSTALLED CROSSBEAM UPPER CAP. REF JOB 81532911 OP 257 FOR REMOVAL AND INSTALL OF CROSS- BEAM AT LBL 12 TO RBL 12. PAINTED AND APPLIED CIC IAW CRJ 900 SRM 51-
- [SDR REXA2021061100415](https://openairdocs.org/sdr/REXA2021061100415.md): Floor Support · corroded · May 21, 2021 · N329PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > FLOOR BEAM AT LBL 27 HAS MULTIPLE SPOTS OF CORROSION FROM FS 1000.00 TO FS 1047.00. C/W REPAIR OF FLOORBEAM AT LBL 27 FROM FS 1000.00 TO FS 1047.00 IAW ENDEAVOR EA CRJ953-11648 DATE 5/13/21, REV.IR.
- [SDR REXA2020082000624](https://openairdocs.org/sdr/REXA2020082000624.md): Battery Pack · inoperative · Aug 14, 2020 · N329PQ · Cndair CL6002D24 · Emergency Lighting
  > RH FWD EXT. EMERGENCY LIGHT INOPERABLE. REPLACED #2 EPSU BATTERY PACK IAW AMM 33-51-17, SEE CONT. CARD FOR DETAILS P/N 2013-1ASMI; S/N ON 12503; S/N OFF97315.
- [SDR REXA2018070200585](https://openairdocs.org/sdr/REXA2018070200585.md): Light · inoperative · Jun 27, 2018 · N329PQ · Cndair CL6002D24 · Emergency Lighting
  > LT OVERWING EMER LIGHT OUT. R&R LT WING INSPECTION LIGHT IAW 33-51-15. OPS CHECK NORMAL.
- [SDR REXA2018011600028](https://openairdocs.org/sdr/REXA2018011600028.md): Oxygen Mask · unwanted deploy · Jan 16, 2018 · N329PQ · Cndair CL6002D24 · Passenger Oxygen System
  > PASSENGER OXYGEN MASKS DEPLOYED. REPACKED THE OXYGEN MASKS IAW AMM 35-21-09.
- [SDR REXA2017100401079](https://openairdocs.org/sdr/REXA2017100401079.md): Drag Angle · cracked · Oct 4, 2017 · N329PQ · Cndair CL6002D24 · Passenger/Crew Doors
  > PAX DOOR AFT DRAG ANGLE CRACKED AT PULLEY, REPAIRED THE DRAG ANGLE IAW SRM 52-11-04.
- [SDR REXA2017100401078](https://openairdocs.org/sdr/REXA2017100401078.md): Hinge · cracked · Oct 4, 2017 · N329PQ · Cndair CL6002D24 · Passenger/Crew Doors
  > LOWER FOLDING PAX DOOR STEP 832AB HAS A CRACKED HINGE. REMOVED AND REPLACED THE HINGE ON PAX DOOR STEP IAW SRM 51-41-02.
- [SDR REXA2017100301083](https://openairdocs.org/sdr/REXA2017100301083.md): Web · cracked · Oct 3, 2017 · N329PQ · Cndair CL6002D24 · Passenger/Crew Doors
  > PAX DOOR AFT WEB IS CRACKED AT THE LOWER PART OF 832CT RISER. REPAIRED THE WEB IAW SRM 51-12-00.
- [SDR REXA2017100301082](https://openairdocs.org/sdr/REXA2017100301082.md): Floor Support · corroded · Oct 3, 2017 · N329PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > MAIN CABIN RIGHT FLOOR SUPPORT IS CORRODED BS 280 - 295, RBL 41. REPAIRED THE FLOOR SUPPORT IAW REO 670-53-21-139.
- [SDR REXA2017100301081](https://openairdocs.org/sdr/REXA2017100301081.md): Web · cracked · Oct 3, 2017 · N329PQ · Cndair CL6002D24 · Passenger/Crew Doors
  > PAX DOOR FWD WEB IS CRACKED AT THE LOWER PART OF 832DT RISER. REMOVED THE DAMAGE AND INSTALLED A DOUBLER REPAIR IAW SRM 52-11-04, ZONE Z.
- [SDR REXA2017100301080](https://openairdocs.org/sdr/REXA2017100301080.md): Panel · cracked · Oct 3, 2017 · N329PQ · Cndair CL6002D24 · Cargo Compartments
  > AFT CARGO WIFI EQUIPMENT CABINET HAS SHEET METAL DAMAGE. RT SIDE. WELDED PERMANENT REPAIR TO AFT CARGO WI-FI EQUIPMENT CABINET PANEL IAW REO 670-51-00-098.
- [SDR REXA2017100201072](https://openairdocs.org/sdr/REXA2017100201072.md): Extinguisher · leaking · Oct 2, 2017 · N329PQ · Cndair CL6002D24 · Fire Bottle, Portable
  > AFT CABIN WATER FIRE BOTTLE HANDLE DAMAGED AND WAS FOUND TO BE LEAKING FROM BOTTLE. REMOVED AND REPLACED AFT CABIN FIRE BOTTLE IAW AMM 26-23-01-000-801A23, STEP 4A, AND 26-23-01-400-801 A23 STEP 4,A.
- [SDR REXA2017062400722](https://openairdocs.org/sdr/REXA2017062400722.md): Sensor · defective · Jun 24, 2017 · N329PQ · Cndair CL6002D24 · Landing Gear Brake System
  > LEFT INBOARD BRAKE TEMP SENSOR GIVING ERRONEOUS INDICATIONS DEFERRED LT INBD BRAKE TEMP SENSOR UNDER ORIGINAL DATED OR 6-23-17 IAW MEL 32-46-10 MX PROCEDURES COMPLIED WITH. REMOVED AND REPLACED LT IB TEMP SENSOR IAW AMM 32-46-01. OPS CK GOOD, SHOT WIRES FROM A
- [SDR REXA2017050800573](https://openairdocs.org/sdr/REXA2017050800573.md): Filter · dirty · May 8, 2017 · N329PQ · Cndair CL6002D24 · Air Distribution System
  > RECIRC FAN FAULT ILLUMINATED & SMELL EMITTED RECIRC FAN NR 1 INOP. DEFERRED RECIRC FAN NR 1 IAW MEL 21-22-1 CAT C. R&R RECIRC NR 1 FILTER SYSTEM. OP CHECKS GOOD IAW AMM 21-22-12.
- [SDR REXA2016062501157](https://openairdocs.org/sdr/REXA2016062501157.md): Light · unsecure · Jun 25, 2016 · N329PQ · Cndair CL6002D24 · Emergency Lighting
  > FLOOR EMERGENCY TRACK STRIP ON LT SIDE AT FORWARD GALLEY PULLED UP CLEANED AREA AND REATTACHED TRACK STRIP IAW AMM 33-51-01. NO FURTHER DEFECTS NOTED.
- [SDR REXA2016022100237](https://openairdocs.org/sdr/REXA2016022100237.md): Strip · misinstalled · Feb 21, 2016 · N329PQ · Cndair CL6002D24 · Emergency Lighting
  > EXIT PATH STRIP ON FLOOR, RT SIDE, ROWS 18-20, IS INSTALLED BACKWARDS, ARROWS POINT TO BACK OF ACFT. R & R EXIT PATH STRIP ON RT SIDE, BETWEEN 18 - 20 IAW AMM 33-51-01.
- [SDR REXA2015120501172](https://openairdocs.org/sdr/REXA2015120501172.md): Filter · missing · Dec 5, 2015 · N329PQ · Cndair CL6002D24 · Emergency Lighting
  > EMERGENCY FLOOR PATH LIGHT STRIP, AT SEAT 13CD, EMER SECTION HAS 4'' INCH SECTION OF LIGHT FILTER MISSING. R & R DAMAGED LIGHT FILTER AS REQUIRED.
- [SDR REXA2015072700743](https://openairdocs.org/sdr/REXA2015072700743.md): Lens · wrong part · Jul 27, 2015 · N329PQ · Cndair CL6002D24 · Emergency Lighting
  > LIGHT ON EMERGENCY EXIT SIGN IN CABIN IS WHITE, BUT SHOULD LIGHT UP RED WHEN FLIGHT ATTENDANT CALLS FLIGHT DECK OR FLIGHT DECK CALLS THE CABIN. INSTALLED NEW RED LENS IAW AMM 33-51-07. PERFORMED OPERATIONAL TEST IAW AMM 33-51-00. OPERATIONS CHECKED GOOD. A
- [SDR REXA2015022500116](https://openairdocs.org/sdr/REXA2015022500116.md): Skin · dented · Feb 25, 2015 · N329PQ · Cndair CL6002D24 · Fuselage Main, Plate/Skin
  > DENT FOUND IN THE FUSELAGE SKIN AT FS 629.00 BETWEEN STRINGER 16L & 17L. THE DENT MEASURES 1.750” X 1.785” X.164” DEEP WITH A GOUGE IN THE CTR MEASURING.375” X.313” X.011” MATERIAL LOSS. THE SKIN IS FORMED FROM 0.150” THICK 2024-T3 ALUMINUM SHEET WITH A

## 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 = 'N329PQ' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N329PQ/reports

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