# Service difficulty reports: N349PQ

A list on [N349PQ](https://openairdocs.org/aircraft/N349PQ.md).

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

- [SDR REXA2025020700102](https://openairdocs.org/sdr/REXA2025020700102.md): Bracket · cracked · Jan 21, 2025 · N349PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CRACK ANGLE BTW FS1144.00 TO FS1162.00 AND STGR 9LH AT AFT EQUIPMENT COMPARTMENT CRACK ANGLE BTW FS1144.00 TO FS1162.00 AND STGR 9LH AT AFT EQUIPMENT COMPARTMENT WAS REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01 PAR 6.C
- [SDR REXA2025020700101](https://openairdocs.org/sdr/REXA2025020700101.md): Seat Track · corroded · Jan 21, 2025 · N349PQ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SEAT TRACK LOCATED BTW FS364.00 TO FS367.00 AND LBL27.00. SEAT TRACK LOCATED BTW FS364.00 TO FS367.00 AND LBL27.00 WAS EVALUATED OUT OF LIMITS DUE TO EXCESSIVE DAMAGE THEREFORE IT WAS REPLACED PER CRJ-900 SRM 53-21-49-101-001-A01 AND AMM 53-00-49-
- [SDR REXA2025021100165](https://openairdocs.org/sdr/REXA2025021100165.md): Plate · damaged · Jan 10, 2025 · N349PQ · Cndair CL6002D24 · Cargo/Baggage Doors
  > BENT AND WEAR ON SEAL RETAINERS AND LOWER PLATES AT FWD AND CENTRAL BAGGAGE DOOR. SEAL RETAINERS WERE CONFORMED PER CRJ-900 SRM 51-24-21-001-001-A01 AND (PT) (FPI) WAS ACCOMPLISHED ON COLD WORKED AREA, NO CRACKS WERE FOUND PER CRJ-900 SRM 51-24-21-001-001-A
- [SDR REXA2025021100164](https://openairdocs.org/sdr/REXA2025021100164.md): Hinge Fitting · worn · Jan 10, 2025 · N349PQ · Cndair CL6002D24 · Ailerons
  > AFTER RH AILERON REMOVAL: WEAR WAS FOUND IN RH AILERON HINGE #3 FITTING WEAR IN RH AILERON HINGE #3 FITTING WAS REPAIRED PER REO 690-57-51-404 REV - -
- [SDR REXA2025021100163](https://openairdocs.org/sdr/REXA2025021100163.md): Hinge Fitting · worn · Jan 10, 2025 · N349PQ · Cndair CL6002D24 · Ailerons
  > AFTER RH AILERON REMOVAL: WEAR WAS FOUND IN RH AILERON HINGE #2 FITTING WEAR IN RH AILERON HINGE #2 FITTING WAS REPAIRED PER REO 690-57-51-404 REV - -
- [SDR REXA2025021000177](https://openairdocs.org/sdr/REXA2025021000177.md): Angle · cracked · Jan 10, 2025 · N349PQ · Cndair CL6002D24 · Passenger/Crew Doors
  > CRACK ON ANGLE OF INNER SKIN AT AFT SIDE OF PASSENGER DOOR CRACK ON ANGLE OF INNER SKIN AT AFT SIDE OF PASSENGER DOOR WAS REPAIRED PER CRJ 900 SRM 52-11-04-201-002-A01.
- [SDR REXA2025020700103](https://openairdocs.org/sdr/REXA2025020700103.md): Angle · corroded · Jan 10, 2025 · N349PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION ON KICK PLATE BTW FS 310.00 TO FS 349.00 AT SURROUND STRUCTURE PASSENGER DOOR. DUE TO EXCCESIVE DAMAGE ON KICK PLATE BTW FS 310.00 TO FS 349.00 WAS REPLACED PER CRJ 900 SRM 51-10-06-001-001-A01 AND SRM 51-42-06-001-001-A01
- [SDR REXA2025013100111](https://openairdocs.org/sdr/REXA2025013100111.md): Angle · corroded · Jan 10, 2025 · N349PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION AT MOUNTING ANGLE AND 3 LOWER SILL ANGLES (WEB FLOOR PROTECTOR ANGLES) BTW FS=319 TO FS=349 OF SERVICE DOOR SURROUND STRUCTURE DUE TO EXCESSIVE DAMAGE, MOUNTING ANGLE LOCATED BTW FS=319 TO FS=349 OF SERVICE DOOR SURROUND STRUCTURE WAS REPLACED PER
- [SDR REXA2025013000106](https://openairdocs.org/sdr/REXA2025013000106.md): Floorbeam · cracked · Jan 10, 2025 · N349PQ · Cndair CL6002D24 · Fuselage Main, Floor Beam
  > CRACKED CENTER COCKPIT FLOOR BEAM LOCATED AT FS280.00 AND RBL12.00 FLOOR INTERNAL SUPPORT STRUCTURE BELOW FLIGHT COMPARTMENT. CENTER COCKPIT FLOOR BEAM LOCATED AT FS280.00 AND RBL12.00 FLOOR INTERNAL SUPPORT STRUCTURE BELOW FLIGHT COMPARTMENT WAS REPAIRED
- [SDR REXA2025013000104](https://openairdocs.org/sdr/REXA2025013000104.md): Floor Support · corroded · Jan 10, 2025 · N349PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > CORROSION ON TWO FLOOR PANEL ANGLE SUPPORTS FIRST LOCATED BTW FS316.00 TO FS342.00 AND LBL42.00, SECOND LOCATED BTW FS344.00 TO FS347.00 AND LBL42.00 AT CABIN PAX (W1). FIRST ANGLE SUPPORT LOCATED BTW FS316.00 TO FS342.00 AND LBL42.00 WAS EVALUATED OUT OF LIMI
- [SDR REXA2025012900099](https://openairdocs.org/sdr/REXA2025012900099.md): Bumper · worn · Jan 10, 2025 · N349PQ · Cndair CL6002D24 · Trailing Edge Flaps
  > LH AND RH FLAP VANE BUMPERS WORN NBUMPERS ON FLAP VANE LH (1EA) AND RH (2EAS) WERE REPLACED PER CRJ 900 SRM 51-42-10-001-001-A01 PAR 8.C AND SRM 51-41-02-001-001-A01
- [SDR REXA2025012300076](https://openairdocs.org/sdr/REXA2025012300076.md): Seat Track · corroded · Jan 10, 2025 · N349PQ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SEAT TRACK LOCATED BTW FS377.00 TO FS382.00 AND LBL9.00. DUE TO EXCESIVE DAMAGE ON SEAT TRACK LOCATED BTW FS377.00 TO FS382.00 AND LBL9.00 WAS REPLACED PER CRJ-900 AMM 53-00-49-000-801 (CONFIG A12, SRM 53-21-49-101-001-A01 AND AMM 53-00-49-400-80
- [SDR REXA2025012300075](https://openairdocs.org/sdr/REXA2025012300075.md): Seat Track · corroded · Jan 10, 2025 · N349PQ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SEAT TRACK LOCATED BTW FS349.00 TO FS379.00 AND RBL9.00. DUE TO EXCESIVE DAMAGE ON SEAT TRACK WAS REPLACED PER CRJ-900 AMM 53-00-49-000-801 (CONFIG A12, SRM 53-21-49-101-001-A01 AND AMM 53-00-49-400-801 (CONFIG A12)
- [SDR REXA2021120801126](https://openairdocs.org/sdr/REXA2021120801126.md): Lamp · inoperative · Dec 5, 2021 · N349PQ · Cndair CL6002D24 · Emergency Lighting
  > EXTERIOR EMERGENCY LIGHT BY PAX DOOR INOP REMOVED AND REPLACED EMERGENCY LIGHT LAMP IAW CRJ-900 AMM 33-51-15. OPS CHECK GOOD. P/N OFF/ON: 8GH002473-08
- [SDR REXA2021081200568](https://openairdocs.org/sdr/REXA2021081200568.md): Angle · bent · Aug 1, 2021 · N349PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > L/H ANGLE SUPPORT FOR FLOOR PNL LIGHTNING DIVERTER IS BEND BEYOND LIMITS BETWEEN FS 310 AND FS 333. REMOVED AND REPLACED L/H ANGLE SUPPORT FS 310-333 IAW CRJ 900 SRM 51-42-13-001-001-A01. WVAC EMP #579269
- [SDR REXA2021081200555](https://openairdocs.org/sdr/REXA2021081200555.md): Intercostal · corroded · Jul 31, 2021 · N349PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > LH AND RH AVIONICS DOOR FWD INTERCOSTALS ARE CORRODED, BETWEEN FS 349 AND FS 364. REMOVED AND REPLACED INTERCOSTALS 27L ABD 27R AT FS 349 TO FS 364. REMOVED AND REINSTALLED 2 EA GUSSETS AND 2 EA. ANGLES AND PROX SWITCH BRACKET IAW CRJ 900 SRM'S 51-40-11-001-0
- [SDR REXA2021081200554](https://openairdocs.org/sdr/REXA2021081200554.md): Intercostal · corroded · Jul 31, 2021 · N349PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > LH AND RH AVIONICS DOOR FWD INTERCOSTALS ARE CORRODED, BETWEEN FS 349 AND FS 364. REMOVED AND REPLACED INTERCOSTALS 27L ABD 27R AT FS 349 TO FS 364. REMOVED AND REINSTALLED 2 EA GUSSETS AND 2 EA. ANGLES AND PROX SWITCH BRACKET IAW CRJ 900 SRM'S 51-40-11-001-0
- [SDR REXA2021081200552](https://openairdocs.org/sdr/REXA2021081200552.md): Electrical Box · cracked · Jul 31, 2021 · N349PQ · Cndair CL6002D24 · Fuselage Main, Structure
  > EXTERNAL PWR PROVISIONS BOX CRACKED AT SEVERAL LOCATIONS. REMOVED AND REPLACED AC POWER RECEPTACLE AND EXT POWER PROVISIONS BOX. OP CKS GOOD IAW 24-41-03-000/400-801-A01, 51-42-06-001-001-A01, AND AMM 24-41-00-861-801-A01.
- [SDR REXA2021081200558](https://openairdocs.org/sdr/REXA2021081200558.md): Intercostal · corroded · Jul 29, 2021 · N349PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > INTERCOSTALS BELOW SERVICE DOOR (4 TOTAL) AT STR 20R ARE CORRODED. LOCATED BETWEEN FS 310 AND FS 364. DISPLACED WIRE BUNDLE & TERM MODULES & REINSTALLED IAW ESPM 20-12-00 STA 333. DISPLACED & REINSTALLED FWD LAV HOSE IAW AMM 58-11-17-000/400-801-A06. DISPLACE
- [SDR REXA2021081200556](https://openairdocs.org/sdr/REXA2021081200556.md): Intercostal · corroded · Jul 29, 2021 · N349PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > INTERCOSTALS BELOW SERVICE DOOR (4 TOTAL) AT STR 20R ARE CORRODED. LOCATED BETWEEN FS 310 AND FS 364. DISPLACED WIRE BUNDLE & TERM MODULES & REINSTALLED IAW ESPM 20-12-00 STA 333. DISPLACED & REINSTALLED FWD LAV HOSE IAW AMM 58-11-17-000/400-801-A06. DISPLA
- [SDR REXA2021081200567](https://openairdocs.org/sdr/REXA2021081200567.md): Bulkhead Web · corroded · Jul 28, 2021 · N349PQ · Cndair CL6002D24 · Fuselage Main, Bulkhead
  > L/H LOWER WEB AT FS 280 BOLTHEAD IS CORRODED UNDER CROSSBEAM. COMPLIED WITH REPAIR OF THE FS 280.00 LH LOWER WEB IAW CRJ 900 SRM 53-11-10-201-004-A01.
- [SDR REXA2021081200566](https://openairdocs.org/sdr/REXA2021081200566.md): Vertical Beam · corroded · Jul 28, 2021 · N349PQ · Cndair CL6002D24 · Fuselage Main, Structure
  > FS 280, LBL 9.0 VEPT BEAM FOR FLIGHT DECK ENTRY DOOR HAS CORROSION AT W.L. 80.00. REPAIRED FS 280.00, LBL 9 VERTICAL BEAM FOR FLIGHT DECK ENTRY DOOR WAS REPAIRED IAW CRJ 900 SRM 53-11-10-201-006-A01.
- [SDR REXA2021081200564](https://openairdocs.org/sdr/REXA2021081200564.md): Floorbeam · corroded · Jul 27, 2021 · N349PQ · Cndair CL6002D24 · Fuselage Main, Floor Beam
  > UPON REMOVAL OF F.S. 280 FWD J-ANGLE FOUND L/H CROSSBEAM TOP FWD CORNER TO HAVE PITTING CORROSION. REMOVED AND REINSTALLED F.S. 280 SHEAR BOX TOP PLATE IAW CRJ900 SRM 51-42-06-001-001-A01 AND 51-42-13-001-001-A01. REMOVED AND REINSTALLED F.S. 280 CROSSBEAM ST
- [SDR REXA2021081210551](https://openairdocs.org/sdr/REXA2021081210551.md): Door Sill · corroded · Jul 26, 2021 · N349PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > AFT BAGGAGE BAY DOOR SILL CORRODED BETWEEN FS 1000 AND FS 1047. REMOVED AND REPLACED AFT CARGO DOOR SILL IAW CRJ900 SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01 AND 51-42-13-001-001-A01 AND REINSTALLED COMBING IAW CRJ900 SRM 51-42-02-001-001-A01, DOOR SILL
- [SDR REXA2021081200562](https://openairdocs.org/sdr/REXA2021081200562.md): Fitting · corroded · Jul 25, 2021 · N349PQ · Cndair CL6002D24 · Fuselage Main, Attach Fittings
  > CENTER CARGO TIE DOWN FITTING MOUNTS (QTY 2) AT FS 629.00 AND FS 661.00+16, LBL 24 ARE CORRODED. REMOVED, LOCATED AND DRILLED AND INSTALLED NEW SERVICEABLE TIE DOWN FITTING MOUNTS 2 EACH AT FS 629.00 & FS 661.00+16 LBL 24 IAW SRM 51-42-06-001-001-A01 AND 51-
- [SDR REXA2021081200565](https://openairdocs.org/sdr/REXA2021081200565.md): Floorbeam · corroded · Jul 23, 2021 · N349PQ · Cndair CL6002D24 · Fuselage Main, Floor Beam
  > UPON REMOVAL OF F.S. 280 FWD J-ANGLE FOUND R/H CROSSBEAM TOP FWD CORNER TO HAVE PITTING CORROSION. REMOVED RH SHEAR BOX TOP PLATE TO GAIN ACCESS AND INSTALLED SAME SERVICEABLE RH SHEAR BOX TOP PLATE, AND REMOVED, LOCATED AND DRILLED AND INSTALLED NEW RH FS
- [SDR REXA2021081200563](https://openairdocs.org/sdr/REXA2021081200563.md): Seat Track · corroded · Jul 23, 2021 · N349PQ · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach Fittings
  > LH SIDE SEAT RAIL CORRODED BETWEEN F.S. 744.15 AND F.S. 761.85. FOUND OUT OF LIMITS IAW CRJ900 SRM 53-41-51-101-001-A02. REMOVED AND REPLACED SIDE SEAT RAIL AT FS 744.15 AND FS 761.85 IAW CRJ900 AMM 53-00-49400-801-A12 AND 53-00-49-000-801-A02.
- [SDR REXA2021081200561](https://openairdocs.org/sdr/REXA2021081200561.md): Stringer · corroded · Jul 21, 2021 · N349PQ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > STRG 27 IS CORRODED BETWEEN FS 280 AND FS 295.00. REMOVED AND REPLACED STGR 27 FS 280- FS 295 WITH NEW SERVICEABLE P/N $H670-31642-1$ IAW CRJ 900 SRM 51-42-21-001-001-A01 AND 51-42-06-001- 001-A01.
- [SDR REXA2021081200560](https://openairdocs.org/sdr/REXA2021081200560.md): Stringer · corroded · Jul 21, 2021 · N349PQ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > STRG 25R IS CORRODED BETWEEN FS 280.00 AND FS 295.00. REMOVED AND REPLACED CORRODED STGR 25R FS 280- FS 333 WITH NEW SERVICEABLE P/N $H670-31212-24 IAW CRJ900 SRM 51-42-21-001-001-A01 AND 51-42-06-001-001-A01.
- [SDR REXA2021081200559](https://openairdocs.org/sdr/REXA2021081200559.md): Floorbeam · corroded · Jul 21, 2021 · N349PQ · Cndair CL6002D24 · Fuselage Main, Floor Beam
  > FS 280.00 CROSS BEAM FLOOR SUPPORT ANGLE IS CORRODED. REMOVED, LOCATED AND DRILLED AND INSTALLED NEW FS 280 CROSSBEAM FLOOR SUPPORT J-ANGLE IAW CRJ 900 SRM 51-42-06-001-001-A01, 51-40-11-001- 001-A01, 51-42-21-001-001-A01.
- [SDR REXA2021081200553](https://openairdocs.org/sdr/REXA2021081200553.md): Stringer · corroded · Jul 21, 2021 · N349PQ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > STR 26R IS CORRODED BETWEEN FS 280-FS 295, NEW SERVICEABLE STRINGER P/N $H670-31634-2$ AT STGR 26R FS 280.00 TO FS 333.00 IAW CRJ 900 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01.
- [SDR REXA2021081200551](https://openairdocs.org/sdr/REXA2021081200551.md): Stringer · corroded · Jul 21, 2021 · N349PQ · Cndair CL6002D24 · Fuselage Main, Longeron/Stringer
  > STR 26R IS CORRODED BETWEEN FS 280-FS 295. A NEW SERVICEABLE STRINGER P/N $H670-31634-2$ AT STGR 26R FS 280.00 TO FS 333.00 IAW CRJ 900 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01.
- [SDR REXA201806010429](https://openairdocs.org/sdr/REXA201806010429.md): Battery Pack · inoperative · May 31, 2018 · N349PQ · Cndair CL6002D24 · Emergency Lighting
  > EMERGENCY LIGHT IN CENTER CABIN DOES NOT STAY ILLUMINATED. REMOVED & REPLACED THE BATTERY PACKS PS37 & PS38 IAW AMM 33-51-17. OPS CHECKED GOOD. REMOVED & REPLACED PS37 BATTERY CHARGER IAW AMM 33-51-17. OPS CHECKED GOOD. ACFT OK FOR SERVICE.
- [SDR REXA2018022100158](https://openairdocs.org/sdr/REXA2018022100158.md): Web · cracked · Feb 21, 2018 · N349PQ · Cndair CL6002D24 · Passenger/Crew Doors
  > PAX DOOR STEP WEB IS CRACKED ON THE AFT SIDE. INSTALL A REPAIR IAW SRM 52-11-04.
- [SDR REXA2018022100157](https://openairdocs.org/sdr/REXA2018022100157.md): Web · cracked · Feb 21, 2018 · N349PQ · Cndair CL6002D24 · Passenger/Crew Doors
  > PAX DOOR STEP WEB IS CRACKED ON THE FWD SIDE. INSTALLED A REPAIR IAW SRM 52-11-04.
- [SDR REXA2018022000156](https://openairdocs.org/sdr/REXA2018022000156.md): Floorbeam · corroded · Feb 20, 2018 · N349PQ · Cndair CL6002D24 · Fuselage Main, Floor Beam
  > RIGHT BS 280 FLOORBEAM IS CORRODED. REMOVED AND REPLACED THE FLOORBEAM IAW SRM 51-42-06, 51-42-21, 51-42-13, AND REO 670-53-11-265.
- [SDR REXA2018021800155](https://openairdocs.org/sdr/REXA2018021800155.md): Channel · cracked · Feb 18, 2018 · N349PQ · Cndair CL6002D24 · Fuselage Miscellaneous Structure
  > PANEL 196DR CHANNEL IS CRACKED. REMOVED AND REPLACED THE CHANNEL IAW SRM 51-43-13-001-001-A01.
- [SDR REXA2017112601204](https://openairdocs.org/sdr/REXA2017112601204.md): Battery · inoperative · Nov 26, 2017 · N349PQ · Cndair CL6002D24 · Emergency Equipment
  > FA FLASHLIGHT BATTERY INOPERATIVE. R & R THE FLASHLIGHT BATTERY IAW AMM 25-61-02. OPS CHECKED GOOD.
- [SDR REXA2016102002009](https://openairdocs.org/sdr/REXA2016102002009.md): Smoke Detector · false indication · Oct 20, 2016 · N349PQ · Cndair CL6002D24 · Smoke Detection
  > WARNING MESSAGE FOR AFT LAVATORY SMOKE. RAN QRH AND WARNING WENT OUT AFTER BREAKERS WERE PULLED. PERFORMED AN AFT LAVATORY VISUAL INSPECTION, NO ABNORMALITIES NOTED. LAVATORY WASTE CAN NOTED EMPTY. NO ABNORMAL ODORS IN LAVATORY. RESET CIRCUIT BREAKERS CB
- [SDR REXA2016091001717](https://openairdocs.org/sdr/REXA2016091001717.md): Fan · odor · Sep 10, 2016 · N349PQ · Cndair CL6002D24 · Air Distribution Fan
  > RECIRCULATION FAN FAULT STATUS MESSAGE. STRONG ODOR IN CABIN & FLT DECK. PERFORMED OPS TEST OF RECIRCULATION FAN NR 2 IAW AMM 21-22-10,OPS CHECKED GOOD.
- [SDR REXA2016082301573](https://openairdocs.org/sdr/REXA2016082301573.md): Smoke Detector · false indication · Aug 23, 2016 · N349PQ · Cndair CL6002D24 · Fire Detection
  > SMOKE FWD LAVATORY MESSAGE, NO SMOKE OR FIRE UPON INSPECTION. REMOVED AND REPLACED THE FWD SMOKE DETECTION IAW AMM 26-16-00.
- [SDR REXA2016081601560](https://openairdocs.org/sdr/REXA2016081601560.md): Smoke Detector · false activation · Aug 16, 2016 · N349PQ · Cndair CL6002D24 · Smoke Detection
  > FWD LAVATORY SMOKE WARNING MESSAGE DURING FLIGHT, F/A INVESTIGATED, NO INDICATION OF SMOKE, RESET, THEN NORMAL OPS. PERFORMED AN OPERATIONAL TEST FOR THE FWD LAVATORY SMOKE DETECTOR IAW AMM 26-16-00. OPS TESTED GOOD. NO DEFECTS NOTED. ACFT OK FOR SERVICE.
- [SDR REXA2016072601425](https://openairdocs.org/sdr/REXA2016072601425.md): Connector · unsecure · Jul 26, 2016 · N349PQ · Cndair CL6002D24 · Fire Protection System Wiring
  > FWD LAV SMOKE MASTER WARNING & ASSOCIATED FWD LAV SMOKE DETECTOR ACTIVATION INTERMITTENT THROUGHOUT FLIGHT. (ACTIVATED 5-6 TIMES ENROUTE) LAV, WASTE BASKET & EXTINGUISHER NOZZLE WERE CHECKED EACH TIME WITH NO ANOMALIES. FALSE INDICATION SUSPECTED. SMOKE DET
- [SDR REXA2016021400154](https://openairdocs.org/sdr/REXA2016021400154.md): Glowstrip · missing · Feb 14, 2016 · N349PQ · Cndair CL6002D24 · Emergency Equipment
  > GALLEY, 3 PHOTO LUMINESCENT STRIP MISSING. REPLACED PHOTO LUMINESCENT STRIP IAW AMM 33-51-01.

## 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 = 'N349PQ' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N349PQ/reports

---
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