# Service difficulty reports: N524AE

A list on [N524AE](https://openairdocs.org/aircraft/N524AE.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 3 · 131 reports

- [SDR VNAA2026052018201](https://openairdocs.org/sdr/VNAA2026052018201.md): Ballast · unserviceable · May 18, 2026 · N524AE · Cndair CL6002C10 · Passenger Compartment Lighting
  > BURNING ODOR COMING FROM OVERHEAD BIN VENT 1-3A. PERFORMED ABNORMAL SMELL IN CABIN INSPECTION IAW FIM 21-22-00-810-806. SIDEWALL LIGHTS OVER SEATS 2 AND 3 ARE OUT AND WITH RECERT FAN OFF SMELL DECREASED SIGNIFICANTLY. REMOVED AND REPLACED BOTH BALLAST OVER SE
- [SDR VNAA2024122711101](https://openairdocs.org/sdr/VNAA2024122711101.md): Acm · unserviceable · Dec 23, 2024 · N524AE · Cndair CL6002C10 · Cabin Cooling System
  > THE CREW REPORTED THERE WAS A BURNING SMELL IN THE COCKPIT (NO SMOKE NOTED) WITH A SLIGHT HAZE IN THE CABIN WHILE BOARDING. THE EVENT LASTED BETWEEN 5 TO 10 MINUTES AND THERE WAS NO MEDICAL ATTENTION REQUIRED. / REMOVED AND REPLACED RH ACM IAW AMM 21-51-08-000
- [SDR VNAA2024082711105](https://openairdocs.org/sdr/VNAA2024082711105.md): Window · unserviceable · Aug 25, 2024 · N524AE · Cndair CL6002C10 · Flight Compartment Windows
  > R SIDE WINDOW ARCING / INSTALLED FLIGHT COMPARTMENT RH SIDE WINDOW IAW CRJ700 AMM 56-12-01-400-801-A01-PSA. LEAK CHECK AND OPERATIONAL TEST OF WINDOW TEMP CONTEROLLER IAW CRJ700 AMM 21-31-00-910-801-A01 AND AMM 30-41-06-710-801-A01 RESPECTIVELY. ALL CHECKS GO
- [SDR VNAA20230829018](https://openairdocs.org/sdr/VNAA20230829018.md): Intercostal · corroded · Aug 29, 2023 · N524AE · Cndair CL6002C10 · Fuselage Main, Frame
  > STGR 21L INTERCOSTAL IS CORRODED BETWEEN FS 319.70 AND FS 333.
- [SDR VNAA2023082919](https://openairdocs.org/sdr/VNAA2023082919.md): Intercostal · corroded · Aug 29, 2023 · N524AE · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > STGR 21L INTERCOSTAL IS CORRODED BETWEEN FS 319.70 AND FS 333.
- [SDR VNAA202308290018](https://openairdocs.org/sdr/VNAA202308290018.md): Seat Track · corroded · Aug 29, 2023 · N524AE · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION FOUND ON RBL 9 FLOOR SEAT RAIL BETWEEN FS 581.00-677.00
- [SDR VNAA202308290017](https://openairdocs.org/sdr/VNAA202308290017.md): Seat Track · corroded · Aug 29, 2023 · N524AE · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION FOUND ON LH SIDE SEAT RAIL BETWEEN FS 379.00-485.00
- [SDR VNAA202308290016](https://openairdocs.org/sdr/VNAA202308290016.md): Striker · dented · Aug 29, 2023 · N524AE · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR LOWER SURROUND IS DENTED IN MULTIPLE PLACES
- [SDR VNAA202308290015](https://openairdocs.org/sdr/VNAA202308290015.md): Stringer Clip · corroded · Aug 29, 2023 · N524AE · Cndair CL6002C10 · Fuselage Main, Attach Fittings
  > STR CLIP CORRODED AT F.S.586 AND STR 25L.
- [SDR VNAA202308290014](https://openairdocs.org/sdr/VNAA202308290014.md): Plate · corroded · Aug 29, 2023 · N524AE · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > FORWARD BAGGAGE BAY DOOR SILL AFT JOINT PLATE AT F.S.533 HAS 2 CORRODED FASTENERS.
- [SDR VNAA202308290013](https://openairdocs.org/sdr/VNAA202308290013.md): Plate · corroded · Aug 29, 2023 · N524AE · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > FORWARD BAGGAGE BAY DOOR SILL FORWARD JOINT PLATE AT F.S.533 HAS 7 CORRODED FASTENERS.
- [SDR VNAA202308290012](https://openairdocs.org/sdr/VNAA202308290012.md): Stringer · corroded · Aug 29, 2023 · N524AE · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > STGR 27 IS CORRODED BETWEEN FS 310 AND FS 319.70.
- [SDR VNAA202308290011](https://openairdocs.org/sdr/VNAA202308290011.md): Skin Splice · corroded · Aug 29, 2023 · N524AE · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > SKIN SPLICE STRAP IS CORRODED AT FS 333 BETWEEN STGR 27 AND STGR 26R.
- [SDR VNAA202308290010](https://openairdocs.org/sdr/VNAA202308290010.md): Attach Angle · corroded · Aug 29, 2023 · N524AE · Cndair CL6002C10 · Fuselage Main, Attach Fittings
  > FS 280 FWD ANGLE ATTACHING TO THE CROSSBEAM IS CORRODED AT RBL 4.
- [SDR VNAA202308290009](https://openairdocs.org/sdr/VNAA202308290009.md): Intercostal · corroded · Aug 29, 2023 · N524AE · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > INTERCOSTAL AT RBL 2 IS CORRODED BETWEEN FS 349 AND FS 364.
- [SDR VNAA202308290008](https://openairdocs.org/sdr/VNAA202308290008.md): Intercostal · corroded · Aug 29, 2023 · N524AE · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > INTERCOSTAL AT STGR 26R IS CORRODED BETWEEN FS 349 AND FS 364
- [SDR VNAA202308290007](https://openairdocs.org/sdr/VNAA202308290007.md): Joint · corroded · Aug 29, 2023 · N524AE · Cndair CL6002C10 · Fuselage Structure (General)
  > F.S. 280 CIRCUMFERENTIAL JOINT IS CORRODED BETWEEN STGR 24L AND STGR 23L.
- [SDR VNAA202308290006](https://openairdocs.org/sdr/VNAA202308290006.md): Angle · corroded · Aug 29, 2023 · N524AE · Cndair CL6002C10 · Fuselage Structure (General)
  > CORROSION FOUND ON PAX DOOR UPPER SILL ANGLE.
- [SDR VNAA202308290005](https://openairdocs.org/sdr/VNAA202308290005.md): Angle · corroded · Aug 29, 2023 · N524AE · Cndair CL6002C10 · Passenger/Crew Doors
  > CORROSION FOUND ON PAX DOOR UPPER SILL ANGLE.
- [SDR VNAA202308290004](https://openairdocs.org/sdr/VNAA202308290004.md): Angle · corroded · Aug 29, 2023 · N524AE · Cndair CL6002C10 · Doors
  > CORROSION FOUND ON PAX DOOR LOWER SILL ANGLE.
- [SDR VNAA202308290003](https://openairdocs.org/sdr/VNAA202308290003.md): Vane · chafed · Aug 29, 2023 · N524AE · Cndair CL6002C10 · Trailing Edge Flaps
  > RH I/B FLAP VANE LEADING-EDGE IS CHAFED AT W.S. 48.95 APPROXIMATELY 8" LONG AND.008" DEEP.
- [SDR VNAA202308290002](https://openairdocs.org/sdr/VNAA202308290002.md): Skin · chafed · Aug 29, 2023 · N524AE · Cndair CL6002C10 · Trailing Edge Flaps
  > RH I/B FLAP VANE LEADING-EDGE IS CHAFED AT W.S. 48.95 APPROXIMATELY 8" LONG AND.008" DEEP.
- [SDR VNAA202308290001](https://openairdocs.org/sdr/VNAA202308290001.md): Seat Track · corroded · Aug 29, 2023 · N524AE · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION FOUND ON RBR 9 FLOOR SEAT RAIL BETWEEN FS 581.00-677.00
- [SDR VNAA202308290019](https://openairdocs.org/sdr/VNAA202308290019.md): Seat Track · corroded · Aug 29, 2023 · N524AE · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION FOUND ON RBR 9 FLOOR SEAT RAIL BETWEEN FS 581.00-677.00
- [SDR VNAA202308280035](https://openairdocs.org/sdr/VNAA202308280035.md): Striker · corroded · Aug 28, 2023 · N524AE · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > GALLEY DOOR LOWER SEAL RETAINER IS CORRODED AROUND SCREW HOLES ON THE AFT SIDE
- [SDR VNAA202308280034](https://openairdocs.org/sdr/VNAA202308280034.md): Fitting · gouged · Aug 28, 2023 · N524AE · Cndair CL6002C10 · Fuselage, Door Hinge
  > FWD BAGGAGE BAY DOOR AFT HINGE IS GOUGED.
- [SDR VNAA202308280020](https://openairdocs.org/sdr/VNAA202308280020.md): Frame · corroded · Aug 28, 2023 · N524AE · Cndair CL6002C10 · Fuselage Main, Frame
  > FS 379 FRAME IS CORRODED BETWEEN STR 20R AND 21R
- [SDR VNAA202308280021](https://openairdocs.org/sdr/VNAA202308280021.md): Stringer · corroded · Aug 28, 2023 · N524AE · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > STGR 26R IS CORRODED BETWEEN FS 295 AND FS 310.
- [SDR VNAA202308280022](https://openairdocs.org/sdr/VNAA202308280022.md): Seat Track · corroded · Aug 28, 2023 · N524AE · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION FOUND ON RBL 9 FLOOR SEAT RAIL BETWEEN FS 485.00-581.00.
- [SDR VNAA202308280023](https://openairdocs.org/sdr/VNAA202308280023.md): Stringer Splice · corroded · Aug 28, 2023 · N524AE · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > STGR 25R SPLICE IS CORRODED AT FS 333.
- [SDR VNAA202308280026](https://openairdocs.org/sdr/VNAA202308280026.md): Stringer Splice · corroded · Aug 28, 2023 · N524AE · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > STGR 25R SPLICE IS CORRODED AT FS 333.
- [SDR VNAA202308280025](https://openairdocs.org/sdr/VNAA202308280025.md): Door Sill · corroded · Aug 28, 2023 · N524AE · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > AFT CARGO BAY DOOR SILL IS CORRODED BETWEEN FS 1000 AND FS 1047 AT WL 72.
- [SDR VNAA202308280024](https://openairdocs.org/sdr/VNAA202308280024.md): Angle · corroded · Aug 28, 2023 · N524AE · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > CORROSION FOUND ON GALLEY SERVICE DOOR LOWER SILL ANGLE.
- [SDR VNAA202308280027](https://openairdocs.org/sdr/VNAA202308280027.md): Stringer · gouged · Aug 28, 2023 · N524AE · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > NICK/GOUGE ON STGR 24L BETWEEN FS 645 AND FS 661
- [SDR VNAA202308280028](https://openairdocs.org/sdr/VNAA202308280028.md): Fitting · corroded · Aug 28, 2023 · N524AE · Cndair CL6002C10 · Leading Edge Devices
  > L/H I/B FLAP HINGE ARM FITTING LUGS AT WS 54.55 ARE GOUGED
- [SDR VNAA202308280029](https://openairdocs.org/sdr/VNAA202308280029.md): Stringer · corroded · Aug 28, 2023 · N524AE · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > STGR 25R IS CORRODED BETWEEN FS 280 AND FS 333.
- [SDR VNAA202308280030](https://openairdocs.org/sdr/VNAA202308280030.md): Stringer · corroded · Aug 28, 2023 · N524AE · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > UPON REMOVING STRINGER 21R FORWARD FS 333 TO FS 477 FOUND THE STRINGER TO HAVE EXTREME EXFOLIATION IN MULTIPLE SPOTS.
- [SDR VNAA202308280031](https://openairdocs.org/sdr/VNAA202308280031.md): Stringer · corroded · Aug 28, 2023 · N524AE · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > UPON REMOVING STRINGER 21R FORWARD FS 333 TO FS 477 FOUND THE STRINGER TO HAVE EXTREME EXFOLIATION IN MULTIPLE SPOTS.
- [SDR VNAA202308280032](https://openairdocs.org/sdr/VNAA202308280032.md): Skin · dented · Aug 28, 2023 · N524AE · Cndair CL6002C10 · Wing, Plate/Skin
  > EA21-C7-53-287_REV-D (PERM REPAIR - FUSELAGE SKIN PANEL - FS509, STR16L) 1.WITHIN 1,500 FLIGHT HOURS AFTER SECTION I, ACCOMPLISH A PERMANENT REPAIR ATDISCREPANT AREA INACCORDANCE WITH APPROVED PROCEDURES.2. PERFORM ULTRASONIC THICKNESS (UT) INSPECTION PER NDTM
- [SDR VNAA202308280033](https://openairdocs.org/sdr/VNAA202308280033.md): Skin · dented · Aug 28, 2023 · N524AE · Cndair CL6002C10 · Wing, Plate/Skin
  > EA21-C7-53-287_REV-D (PERM REPAIR - FUSELAGE SKIN PANEL - FS509, STR16L) 1.WITHIN 1,500 FLIGHT HOURS AFTER SECTION I, ACCOMPLISH A PERMANENT REPAIR ATDISCREPANT AREA INACCORDANCE WITH APPROVED PROCEDURES.2. PERFORM ULTRASONIC THICKNESS (UT) INSPECTION PER NDTM
- [SDR VNAA2023082800033](https://openairdocs.org/sdr/VNAA2023082800033.md): Skin · damaged · Aug 28, 2023 · N524AE · Cndair CL6002C10 · Cargo/Baggage Doors
  > AFT CARGO DOOR, AFT UPPER CORNER: THE CABLE HAS SPLIT THE PULLEY IN HALF, CAUSING THE CABLE TO SAW-TOOTH INTO THE UPPER CROSSBEAM.
- [SDR VNAA202308280002](https://openairdocs.org/sdr/VNAA202308280002.md): Skin · damaged · Aug 28, 2023 · N524AE · Cndair CL6002C10 · Wing, Plate/Skin
  > LEADING EDGE 522AL HAS ONE DAMAGED FASTENER COUNTERSINK ON THE LOWER LEADING EDGE AT WS 178.00.
- [SDR VNAA202307020001](https://openairdocs.org/sdr/VNAA202307020001.md): Skin · gouged · Jul 2, 2023 · N524AE · Cndair CL6002C10 · Wing Structure
  > LH LEADING EDGE PANEL (FIXED UPPER SKIN) 521AT WAS FOUND TO HAVE GOUGE
- [SDR VNAA202207111111](https://openairdocs.org/sdr/VNAA202207111111.md): Trim Panel · unserviceable · Jul 8, 2022 · N524AE · Cndair CL6002C10 · Flight Control System
  > FLIGHT RETURNED TO FIELD AFTER TAKEOFF. CREW DISCOVERED THAT AILERON AND RUDDER TRIM WERE DEFLECTING SEVERELY TO THE LEFT. CREW THEN CONTACTED ATC AND DECLARED AN EMERGENCY. FLIGHT LANDED SAFELY AND TAXIED BACK TO GATE. CREW REPORTS LANDING OVERWEIGHT. CABIN W
- [SDR VNAA2021010321111](https://openairdocs.org/sdr/VNAA2021010321111.md): Ballast · failed · Dec 30, 2021 · N524AE · Cndair CL6002C10 · Passenger Compartment Lighting
  > FA REPORTED BURNING SMELL AT ROW 16,17 / TRACED ODOR TO BALLAST OF 16DF SIDEWALL LIGHTS. R/R 16 DF SIDEWALL LIGHT BALLAST IAW CRJ700 AMM 33-21-09-000/400-801. OPS AND SMELL TEST GOOD.
- [SDR VNAA202104081111](https://openairdocs.org/sdr/VNAA202104081111.md): Slat · damaged · Apr 4, 2021 · N524AE · Cndair CL6002C10 · Leading Edge Devices
  > DURING ROUTINE MAINTENANCE, TECHNICIANS REPORT THE LH #2 SLAT (P/N: CC670-12700-1, S/N: UNKNOWN) HAS A CHIP MISSING (DAMAGE #1) IN THE TRAILING EDGE (P/N CC670-12742-1) AT APPROXIMATELY SLAT STATION 249 MEASURING.28Ï¿½ WIDE X.22Ï¿½ DEEP. THE CORNERS OF THE C
- [SDR VNAA202103081111](https://openairdocs.org/sdr/VNAA202103081111.md): Skin · dented · Mar 4, 2021 · N524AE · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > DURING OVERNIGHT MAINTENANCE, A DENT WAS DISCOVERED ON THE RH FUSELAGE SKIN JUST FORWARD OF FS 220 ABOVE THE RH PITOT PROBE BETWEEN STGR 13A AND 14A. THE DENT MEASURES 2.05Ï¿½ X 2.0Ï¿½ X 0.016Ï¿½ DEEP AND IS NOT WITHIN ALLOWABLE DAMAGE LIMITS DUE TO EDGE OF DE
- [SDR VNAA2020100211101](https://openairdocs.org/sdr/VNAA2020100211101.md): Battery · discharged · Oct 2, 2020 · N524AE · Cndair CL6002C10 · Emergency Lighting
  > NR 4 EMERGENCY BATTERY NOT SUPPLYING VOLTAGE TO LT EXTERIOR AFT EMERGENCY LIGHT. REMOVED AND REPLACED NR 4 EMERGENCY BATTERY. OPERATIONS CHECK GOOD AT THIS TIME.
- [SDR VNAA2019100111102](https://openairdocs.org/sdr/VNAA2019100111102.md): Bulb · inoperative · Oct 1, 2019 · N524AE · Cndair CL6002C10 · Emergency Lighting
  > MX FOUND LEFT AND RIGHT OVER WING EXITS LOWER SIGNS HAS A LIGHT NOT ILLUMINATING. RELAMPED RIGHT AND LEFT OVER WING EXIT LOWER SIGN BULBS, OPS CHECKS GOOD.
- [SDR VNAA2019100111101](https://openairdocs.org/sdr/VNAA2019100111101.md): Lamp · inoperative · Oct 1, 2019 · N524AE · Cndair CL6002C10 · Emergency Lighting
  > MX FOUND AT SEAT 14 EMERGENCY OVERHEAD LIGHT WILL NOT ILLUMINATE.RELAMPED SEAT 14 OVERHEAD EMERGENCY FLOOD LAMP, OPS CHECKS GOOD IAW CRJ 700 AMM 33-51-09-000-801/400-801.

Next page: https://openairdocs.org/aircraft/N524AE/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 = 'N524AE' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N524AE/reports

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