# Service difficulty reports: N304PQ

A list on [N304PQ](https://openairdocs.org/aircraft/N304PQ.md).

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

- [SDR REXA2024111901503](https://openairdocs.org/sdr/REXA2024111901503.md): Acm · odor · Nov 17, 2024 · N304PQ · Cndair CL6002D24 · Cabin Cooling System
  > SUP - AT APPROX 10000FT THE DESCENT THE SMELL OF SMOKE WAS DETECTED IN THE FLIGHT DECK. SMOKE WAS OBSERVED COMING FROM THE CA SIDE AIR VENTS AS WELL AS OBERSVERD BY THE FA IN THE MAIN CABIN INSOLATED SOURCE OF SMOKE. THE L/H PACK WILL NOT COOL - BLOW WHITE SM
- [SDR REXA2024070300498](https://openairdocs.org/sdr/REXA2024070300498.md): Former · corroded · Jun 11, 2024 · N304PQ · Cndair CL6002D24 · Emergency Exits
  > RH FWD EMERGENCY EXIT DOOR (S/N: SB1397) UPPER FORMER IS CRACKED AT AFT LUG REPAIRED RH FWD EMERGENCY EXIT DOOR (S/N: SB1397) UPPER FORMER IAW ENDEAVOR EA CRJ952-16729 REV IR DATED 5/26/2024.
- [SDR REXA2024102801029](https://openairdocs.org/sdr/REXA2024102801029.md): Floorbeam · corroded · May 24, 2024 · N304PQ · Cndair CL6002D24 · Fuselage Main, Floor Beam
  > R/H F.S. 280 CROSS BEAM IS HEAVILY CORRODED AT CORNER OF TOP FLANGE. R/H F.S. 280 CROSSBEAM IS CORRODED WITH DEEP PITTING ON OUTER UPPER CORNER BETWEEN BL 0 AND RBL 12. NO ALLOWABLE DAMAGE LIMITS PROVIDED IN CRJ-900 SRM. BEAM REQUIRES REPLACEMENT. REMOVED RH F
- [SDR REXA2024102801028](https://openairdocs.org/sdr/REXA2024102801028.md): Floorbeam · corroded · May 24, 2024 · N304PQ · Cndair CL6002D24 · Fuselage Main, Floor Beam
  > L/H F.S. 280 CROSS BEAM IS CORRODED ON CORNER OF TOP FLANGE. L/H F.S. 280 CROSS BEAM IS HEAVILY CORRODED WITH DEEP PITTING ON OUTER UPPER CORNER BETWEEN BL 0 AND LBL 12. NO ALLOWABLE DAMAGE LIMITS PROVIDED IN CRJ-900 SRM. BEAM REQUIRES REPLACEMENT. REMOVED LH
- [SDR REXA2024102801027](https://openairdocs.org/sdr/REXA2024102801027.md): Angle · corroded · May 24, 2024 · N304PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > "F.S. 280 ""J"" ANGLE IS CORRODED. F.S. 280 ""J"" ANGLE P/N CC670-34095-1 FOUND TO BE EXCESSIVELY CORRODED WITH NO ALLOWABLE DAMAGE LIMITS PROVIDED. REMOVED CORRODED J ANGLE IAW CRJ-900 SRM 51-42-06/21-001-001-A01. INSTALLED NEW ""J"" ANGLE P/N: CC670-34095-
- [SDR REXA2024090300675](https://openairdocs.org/sdr/REXA2024090300675.md): Floorbeam · cracked · May 24, 2024 · N304PQ · Cndair CL6002D24 · Fuselage Main, Floor Beam
  > LH FS 280 COCKPIT FLOOR BEAM AT LBL 12.50 IS CRACKED IN FWD O/B RADIUS. REPAIRED PER MHIRJ REO# 690-53-11-1766 REV. -- DATED 2024-05-25.
- [SDR REXA2024103101253](https://openairdocs.org/sdr/REXA2024103101253.md): Door Frame · cracked · May 22, 2024 · N304PQ · Cndair CL6002D24 · Emergency Exits
  > L/H FWD EMERGENCY EXIT DOOR (S/N: SB1398) UPPER FORMER IS CRACKED AT AFT LUG REPAIRED L/H FWD EMERGENCY EXIT DOOR WITH ENDEAVOR AIR EA CRJ952-16730, DATED 5/26/2024 REV IR IAW ENDEAVOR AIR EA CRJ952-16730, DATED 5/26/2024 REV IR.
- [SDR REXA2020120700822](https://openairdocs.org/sdr/REXA2020120700822.md): Seat Track · corroded · Nov 23, 2020 · N304PQ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > FLOOR SEAT TRACK CORRODED AT RBL 9.0 BETWEEN FS 349.00 AND 379.00. REMOVED AND REPLACE FLOOR SEAT TRACK AT RBL 9.0 BETWEEN FS 349.00 AND 485.00, IAW CRJ 900 AMM 53-00-49-400-801-A12 AND REO NR 670-53-00-343 REV -N DATED 2019-07-16.
- [SDR REXA202012070825](https://openairdocs.org/sdr/REXA202012070825.md): Floorbeam · corroded · Nov 22, 2020 · N304PQ · Cndair CL6002D24 · Fuselage Main, Floor Beam
  > FWD "J" ANGLE CORRODED AT FS 280 BETWEEN RBL 11 AND LBL 11 AND CLIPS ATTACHED TO "J" ANGLE CORRODED. REMOVED AND REPLACED J ANGLE AND REPLACED/REPAIRED CORRODED CLIPS, IAW SRM 57-42-06-001-001-A01, 51-42-21-001-001-A01, 51-21-06-001-001-A01.
- [SDR REXA2020120700830](https://openairdocs.org/sdr/REXA2020120700830.md): Floorbeam · corroded · Nov 20, 2020 · N304PQ · Cndair CL6002D24 · Fuselage Main, Floor Beam
  > FS 280 LT FLOOR SUPPORT CROSSBEAM IS CORRODED. REMOVED & REPLACED LT FLOOR SUPPORT P/N CC670-34094-1S, IAW CRJ 900 SRM 51-42-06-001-001-A01, 51-42-13-001-001-A01 AND 51-42-21-001-001-A01, 51-42-22-001-001-A01.
- [SDR REXA2020120700831](https://openairdocs.org/sdr/REXA2020120700831.md): Skin · cracked · Nov 16, 2020 · N304PQ · Cndair CL6002D24 · Wing, Plate/Skin
  > LT WING LEADING EDGE PANEL NR 522BL HAS APPROXIMATELY 4 INCH CRACK AT UPPER SKIN MID SECTION OF PANEL (81530411) JOB#. COMPLIED WITH REPAIR LT WING LEADING EDGE PANEL NR 522BL, IAW CRJ 900 EA NO CRJ957-10956.
- [SDR REXA2020120700821](https://openairdocs.org/sdr/REXA2020120700821.md): Floor Support · corroded · Nov 16, 2020 · N304PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > RT FLOOR SILL CORRODED BETWEEN FS 319 AND FS 364. REPAIRED AREA IAW EA CRJ953-10961 DATED 11/3/20 REV IR.
- [SDR REXA2020120700820](https://openairdocs.org/sdr/REXA2020120700820.md): Intercostal · corroded · Nov 16, 2020 · N304PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > INTERCOSTAL IS CORRODED BETWEEN FS 364 TO 349 AND STRINGERS 27 AND 26R. REMOVED & REPLACED INTERCOSTAL FS 364-349 BETWEEN STR 27 & 26R, IAW SRM 51-42-06-001-001-A01. REMOVED & REINSTALLED ORIGINAL GUSSETS, IAW SRM 51-42-21-001-001-A01.
- [SDR REXA2020120700818](https://openairdocs.org/sdr/REXA2020120700818.md): Door Sill · corroded · Nov 16, 2020 · N304PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CARGO DOOR CUTOUT LOWER SILL ANGLE IS CORRODED. REMOVED, DRILLED UP AND REPLACED CARGO DOOR CUTOUT LOWER SILL ANGLE, IAW SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01 AND 51-42-21-001-001-A01. ATTACHED CERT AS REQUIRED.
- [SDR REXA2020120700817](https://openairdocs.org/sdr/REXA2020120700817.md): Plate · chafed · Nov 16, 2020 · N304PQ · Cndair CL6002D24 · Fuselage Structure (General)
  > WHILE PERFORMING REPAIR 670-53-61-1382. FOUND 1 LOCATION TO BE OUT OF LIMITS. REPAIR OR REPLACEMENT REQUIRED. REPAIRED AREA IAW ENDEAVOR EA NO: CRJ953-10976.
- [SDR REXA2020120700829](https://openairdocs.org/sdr/REXA2020120700829.md): Attach Angle · corroded · Nov 14, 2020 · N304PQ · Cndair CL6002D24 · Service Doors
  > SERVICE DOOR MOUNTING ANGLE AT FS 310 TO FS 349 IS CORRODED. REMOVED & REPLACED SE DOOR MOUNTING ANGLE AT FS 310 TO 349, IAW SRM 51-42-06-001-001-A01.
- [SDR REXA2020120700828](https://openairdocs.org/sdr/REXA2020120700828.md): Seat Track · corroded · Nov 14, 2020 · N304PQ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > RT CABIN SIDE SEAT RAIL FROM FS 744.15 TO FS 761.85 HAS CORROSION AT FWD END. INSTALLED NEW SERVICEABLE RT SIDE SEAT RAIL P/N SH690-36285-1 BETWEEN FS 744.15 AND FS 761.85, IAW CRJ 900 AMM 53-00-49-400-801-A12.
- [SDR REXA2020120700827](https://openairdocs.org/sdr/REXA2020120700827.md): Seat Track · corroded · Nov 14, 2020 · N304PQ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > LT CABIN SIDE SEAT RAIL FROM FS 785.15 TO FS 847.00+8.40 HAS CORROSION AT FWD END. FABRICATED AND DRILLED SEAT TRACK RAIL FOR STA 785.15 TO 847.00+08.40, IAW CRJ 900 EO BA690-30000 REV 2008-00 03/08/13. INSTALLED SEAT TRACK RAIL AT STA 785.15 TO 847.00+08.40
- [SDR REXA2020120700824](https://openairdocs.org/sdr/REXA2020120700824.md): Seat Track · corroded · Nov 14, 2020 · N304PQ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > FLOOR SEAT TRACK CORRODED AT LBL 27.00 BETWEEN FS 364 AND FS 394. FABRICATED REPLACEMENT SEAT RAIL, IAW CRJ900 SRM 53-00-49-201-A01. REMOVED AND REPLACED SEAT RAIL, IAW CRJ900 AMM 53-00-49-000-400-801-A12.
- [SDR REXA2020120700823](https://openairdocs.org/sdr/REXA2020120700823.md): Seat Track · corroded · Nov 14, 2020 · N304PQ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > FLOOR SEAT TRACK CORRODED AT LBL 9.00 BETWEEN FS 364 AND FS 394. REMOVED & REPLACED SEAT TRACK AT LBL 9 BETWEEN FS 364-394, IAW CRJ 900 AMM 53-00-49-400-801-A12.
- [SDR REXA2020120700819](https://openairdocs.org/sdr/REXA2020120700819.md): Intercostal · corroded · Nov 11, 2020 · N304PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > INTERCOSTAL IS CORRODED AT STRINGER 26R BETWEEN FRAMES FS 349-364. REMOVED & REPLACED INTERCOSTAL AT STR 26R FS 349-364 & ATTACHMENT ANGLE, IAW SRM 51-42-21-001-001-A01 & 51-40-11-001-001-A01.
- [SDR REXA2020120700826](https://openairdocs.org/sdr/REXA2020120700826.md): Seat Track · corroded · Nov 6, 2020 · N304PQ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > LT CABIN SIDE SEAT RAIL FROM FS 744.15 TO FS 761.85 HAS CORROSION AT FWD END. INSTALLED NEW SERVICEABLE LT SIDE SEAT RAIL P/N SH690-36285-1 BETWEEN FS 744.15 TO 761.85, IAW CRJ 900 AMM 53-00-49-400-801-A12.
- [SDR REXA2020120700825](https://openairdocs.org/sdr/REXA2020120700825.md): Seat Track · corroded · Nov 6, 2020 · N304PQ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > LT CABIN SIDE SEAT RAIL FROM FS 744.15 TO FS 761.85 HAS CORROSION AT FWD END. INSTALLED NEW SERVICEABLE LT SIDE SEAT RAIL P/N SH690-36285-1 BETWEEN FS 744.15 TO 761.85, IAW CRJ 900 AMM 53-00-49-400-801-A12.
- [SDR REXA2017061800715](https://openairdocs.org/sdr/REXA2017061800715.md): Smoke Detector · broken · Jun 18, 2017 · N304PQ · Cndair CL6002D24 · Smoke Detection
  > FWD LAV SMOKE DETECTOR RESET BUTTON IS BROKEN. DEFERRED FWD LAV SMOKE DET SYS IAW MEL 26-15-1 CAT C PER MOC 96184. REMOVED AND REPLACED FWD LAV SMOKE DETECTOR IAW AMM 26-16-01. OPS CHECK GOOD.
- [SDR REXA2017031300368](https://openairdocs.org/sdr/REXA2017031300368.md): Charger · inoperative · Mar 13, 2017 · N304PQ · Cndair CL6002D24 · Emergency Lighting
  > FWD ENTRANCE COMPARTMENT AFT WALL AND GALLEY TRIM EMERGENCY EXIT LIGHTS FAILED OPS CHECKS. REMOVED AND REPLACED ON EMERGENCY LIGHT BATTERY CHARGER NR 1 IAW CMM 25-60-03. OPS TESTED GOOD IAW AMM 33-51-00-710-802.
- [SDR REXA2017031200382](https://openairdocs.org/sdr/REXA2017031200382.md): Housing · cracked · Mar 12, 2017 · N304PQ · Cndair CL6002D24 · Electrical/Electronic Compartment Doors
  > AVIONICS DOOR HANDLE HOUSING FOUND TO BE CRACKED AT THE BASE. REMOVED AND REPLACED THE DOOR HANDLE HOUSING IAW AMM 52-42-03. OPS CHECKED GOOD IAW AMM 52-42-00-710-801.
- [SDR REXA2017031200381](https://openairdocs.org/sdr/REXA2017031200381.md): Intercostal · corroded · Mar 12, 2017 · N304PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > MAIN AVIONICS DOOR FWD SURROUND, RIGHT LATCH PIN INTERCOSTAL ATTACH FLANGE CORRODED, BS 349 TO 364. REMOVED AND REPLACED THE INTERCOSTAL IAW SRM 51-42-06 AND 51-42-21. OPS TESTED GOOD IAW AMM 52-42-00-710-801.
- [SDR REXA2017031100380](https://openairdocs.org/sdr/REXA2017031100380.md): Post · corroded · Mar 11, 2017 · N304PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > BS 280 BULKHEAD LOWER LEFT DOOR POST CORRODED AT LBL 11. REPAIRED THE POST IAW REO 670-53-11-745.
- [SDR REXA2017031100379](https://openairdocs.org/sdr/REXA2017031100379.md): Angle · corroded · Mar 11, 2017 · N304PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > BS 280 BULKHEAD RIGHT DOOR POST LOWER ANGLE CORRODED AT RBL 11. REMOVED AND REPLACED LOWER ANGLE IAW REO 670-53-11-745.
- [SDR REXA2017031100378](https://openairdocs.org/sdr/REXA2017031100378.md): Angle · corroded · Mar 11, 2017 · N304PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > BS 280 BULKHEAD LEFT DOOR POST LOWER ANGLE CORRODED AT LBL 11. REMOVED AND REPLACED LOWER ANGLE IAW REO 670-53-11-745.
- [SDR REXA2017031100377](https://openairdocs.org/sdr/REXA2017031100377.md): Post · corroded · Mar 11, 2017 · N304PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > BS 280 BULKHEAD LOWER RIGHT DOOR POST CORRODED AT RBL 11. REPAIRED THE POST IAW REO 670-53-11-745.
- [SDR REXA2017031100376](https://openairdocs.org/sdr/REXA2017031100376.md): Floorbeam · corroded · Mar 11, 2017 · N304PQ · Cndair CL6002D24 · Fuselage Main, Floor Beam
  > CORROSION FOUND ON THE FLOORBEAM FS 280. REMOVED AND REPLACED THE FLOORBEAM IAW SRM 51-42-06, AND 51-42-13.
- [SDR REXA2017031100375](https://openairdocs.org/sdr/REXA2017031100375.md): Floorbeam · corroded · Mar 11, 2017 · N304PQ · Cndair CL6002D24 · Fuselage Main, Floor Beam
  > CORROSION FOUND ON THE FLOORBEAM BS 280. REMOVED AND REPLACED THE FLOORBEAM IAW SRM 51-42-06, & 51-42-13.
- [SDR REXA2017031100374](https://openairdocs.org/sdr/REXA2017031100374.md): Angle · corroded · Mar 11, 2017 · N304PQ · Cndair CL6002D24 · Fuselage Main, Floor Beam
  > BS 280 FLOORBEAM ANGLE CORRODED, LBL 11 TO RBL 11. REMOVED AND REPLACED WITH NEW FLOORBEAM ANGLE PER SRM 51-42-06.
- [SDR REXA2017031100373](https://openairdocs.org/sdr/REXA2017031100373.md): Bulkhead Web · corroded · Mar 11, 2017 · N304PQ · Cndair CL6002D24 · Fuselage Main, Bulkhead
  > RIGHT BS 280 BULKHEAD WEB CORRODED. REPAIRED IAW REO 670-53-11-594. REV A.
- [SDR REXA2017031000372](https://openairdocs.org/sdr/REXA2017031000372.md): Step · cracked · Mar 10, 2017 · N304PQ · Cndair CL6002D24 · Passenger/Crew Doors
  > ENTRY DOOR FWD STEP SUPPORT WEB HAS MULTIPLE CRACKS IN STEP RADIUS THIRD STEP FROM TOP. REMOVED DAMAGE AND REPAIRED IAW SRM 52-11-04.
- [SDR REXA2017031000371](https://openairdocs.org/sdr/REXA2017031000371.md): Stringer · corroded · Mar 10, 2017 · N304PQ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > STRINGER 26R ATTACH FLANGE CORRODED, BS 310 TO 319.70. REMOVED AND REPLACED THE STRINGER IAW SRM 51-42-06, 51-42-21, AND 53-00-06-491-868.
- [SDR REXA2017030900370](https://openairdocs.org/sdr/REXA2017030900370.md): Support Channel · cracked · Mar 9, 2017 · N304PQ · Cndair CL6002D24 · Aerodynamic Fairings
  > AFT WING TO BODY FAIRING SUPPORT CHANNEL IS CRACKED. REMOVED AND REPLACED THE SUPPORT CHANNEL IAW SRM-51-42-13.
- [SDR REXA2017030900369](https://openairdocs.org/sdr/REXA2017030900369.md): Step · cracked · Mar 9, 2017 · N304PQ · Cndair CL6002D24 · Passenger/Crew Doors
  > ENTRY DOOR AFT STEP SUPORT WEB HAS MULTIPLE CRACKS IN STEP RADIUS THIRD STEP FROM TOP. REMOVED DAMAGE AND REPAIRED IAW SRM 52-11-04.
- [SDR REXA2017012100072](https://openairdocs.org/sdr/REXA2017012100072.md): Engine · contaminated · Jan 21, 2017 · N304PQ · Cndair CL6002D24 · Engine (Turbine/Turboprop)
  > DURING DEPARTURE, A STRONG ODOR OF SMOKE IN THE COCKPIT AFTER AIRBORNE, 10 SEC SMOKE AFT LAVATORY WARNING MESSAGE ON EICAS. RAN QRH LANDED. INSPECTED AFT LAV FOR SMOKE ODOR IAW FIM TASK 21-21-00-810-806. NO DEFECT NOTED. THE COMPRESSOR WASH CHEMICAL FLUID
- [SDR REXA2017011600046](https://openairdocs.org/sdr/REXA2017011600046.md): Battery · inoperative · Jan 16, 2017 · N304PQ · Cndair CL6002D24 · Emergency Equipment
  > AFT FLASHLIGHT BATTERY INOPERATIVE. REMOVED AND REMOVED THE FLASHLIGHT IAW AMM 25-61-02. OPS GOOD. NO FURTHER DEFECTS NOTED.
- [SDR REXA2017011200039](https://openairdocs.org/sdr/REXA2017011200039.md): Elt · inoperative · Jan 12, 2017 · N304PQ · Cndair CL6002D24 · Emergency Locator Beacon
  > ELT G-SWITCH WILL NOT WORK. R&R ELT MAIN ASSY IAW AMM 25-62-02.
- [SDR REXA2016111602223](https://openairdocs.org/sdr/REXA2016111602223.md): Lead · inoperative · Nov 16, 2016 · N304PQ · Cndair CL6002D24 · Ignition Power Supply
  > RIGHT ENGINE DID NOT LIGHT OFF. MEETS ALL PARAMETERS BEFORE FUEL WAS INTRODUCED. NO LIGHT OFF. THE ODOR OF FUEL FILLED THE CABIN AFTER THE FAILED ENG START. REPLACED GRAY IGNITION LEAD AND IGNITOR PLUG, RT ENGINE, IAW AMM 74-20-01 OPS CHECK GOOD IAW AMM 71
- [SDR REXA2016082901666](https://openairdocs.org/sdr/REXA2016082901666.md): Oxygen Mask · leaking · Aug 29, 2016 · N304PQ · Cndair CL6002D24 · Crew Oxygen System
  > FIRST OFFICER`S OXYGNE MASK LEAKING WHEN PUSHING THE PUSH TO TEST LEVER. R & R THE OXYGEN MASK STOWAGE BOX IAW AMM 35-10-00. OPS CHECKED GOOD. NO LEAKS. ACFT OK FOR SERVICE. SERVICED CREW O2 TO 1800PSI.
- [SDR REXA2016011000022](https://openairdocs.org/sdr/REXA2016011000022.md): Door Seal · dirty · Jan 10, 2016 · N304PQ · Cndair CL6002D24 · Emergency Exits
  > CREW ESCAPE HATCH STILL LEAKING WATER BADLY ON GND UNPRESSURIZED. INSPECTED SEAL & CLEANED SEAL ON DOOR. OBSERVED FOR LEAKS, NO LEAKS NOTED. SEAL FOUND TO BE IN NORMAL CONDITION IAW AMM 52-22-00.
- [SDR REXA2016010900021](https://openairdocs.org/sdr/REXA2016010900021.md): Door Seal · saturated · Jan 9, 2016 · N304PQ · Cndair CL6002D24 · Emergency Exits
  > CREW ESCAPE HATCH HAS EXCESSIVE HATCH LEAK, ALONG LOWER RT SIDE. INSPECTED AFFECTED AREA, FOUND WATER WITHIN THE DOOR REMOVED & CLEANED DOOR SEAL AS NECESSARY. OPERATIONS CHECKED GOOD & NO LEAKS NOTED AT THIS TIME IAW AMM 52-22-00.
- [SDR REXA2015080200769](https://openairdocs.org/sdr/REXA2015080200769.md): Charger · inoperative · Aug 2, 2015 · N304PQ · Cndair CL6002D24 · Emergency Lighting
  > SEVERAL EMERGENCY LIGHT AT THE CENTER OF THE AIRCRAFT, INTERIOR & EXTERIOR, ARE VERY DIM, SOME ARE INOPERATIVE. R & R NR 3 EMERGENCY LIGHT BATTERY CHARGER IAW AMM 33-51-17. OPERATIONS CHECKED GOOD.

## 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 = 'N304PQ' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N304PQ/reports

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