# Service difficulty reports: N510AE

A list on [N510AE](https://openairdocs.org/aircraft/N510AE.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 4 · 163 reports

- [SDR VNAA2026041416402](https://openairdocs.org/sdr/VNAA2026041416402.md): Control Lever · unserviceable · Apr 10, 2026 · N510AE · Cndair CL6002C10 · Landing Gear Selector
  > GEAR DISAGREE ON CLIMBOUT. / REMOVED AND INSTALLED LANDING GEAR CONTROL-PANEL LEVER IAW CRJ 700 AMM 32-31-01-000/400-802. OPERATIONAL TEST OF THE LANDING GEAR EXTENSION/RETRACTION SYSTEM GOOD IAW CRJ 700 AMM 32-30-00-710-801.
- [SDR VNAA202602090064](https://openairdocs.org/sdr/VNAA202602090064.md): Mount · damaged · Feb 10, 2026 · N510AE · Cndair CL6002C10 · Engine Mount Section
  > R/H FWD ENGINE MOUNT HAS DAMAGE ON LOWER FITTING MARKED WITH RED TAPE,
- [SDR VNAA202602090025](https://openairdocs.org/sdr/VNAA202602090025.md): Door Frame · corroded · Feb 10, 2026 · N510AE · Cndair CL6002C10 · Fuselage Main, Structure
  > FS 280.00 DOOR POST AT RBL 9 IS CORRODED, 670-53-11-745-4, -6, LOWER DOOR POST
- [SDR VNAA202602090026](https://openairdocs.org/sdr/VNAA202602090026.md): Hinge · gouged · Feb 10, 2026 · N510AE · Cndair CL6002C10 · Fuselage, Door Hinge
  > PAX DOOR PIANO HINGE (FUSELAGE SIDE) HAS MULTIPLE GOUGES BETWEEN THE LUGS,
- [SDR VNAA202602090024](https://openairdocs.org/sdr/VNAA202602090024.md): Door Frame · corroded · Feb 10, 2026 · N510AE · Cndair CL6002C10 · Fuselage Main, Structure
  > FS 280.00 DOOR POST AT LBL 9 IS CORRODED, 670-53-11-745-3, LOWER DOOR POST, FS 280 LOWER DOOR POST
- [SDR VNAA202602090027](https://openairdocs.org/sdr/VNAA202602090027.md): Seat Track · corroded · Feb 10, 2026 · N510AE · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > L/H SIDE SEAT RAIL IS CORRODED BETWEEN F.S. 409 TO F.S. 485,,
- [SDR VNAA202602090023](https://openairdocs.org/sdr/VNAA202602090023.md): Angle · corroded · Feb 10, 2026 · N510AE · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > FS 280.00 CROSSBEAM J ANGLE IS CORRODED, CC670-34095-1, J ANGLE
- [SDR VNAA202602090028](https://openairdocs.org/sdr/VNAA202602090028.md): Seat Track · gouged · Feb 10, 2026 · N510AE · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > THE L/H SIDE SEAT RAIL HAS MULTIPLE TOOLING MARKS, NICKS AND GOUGES FROM APPROX. FS 485 - FS565 AT STGR 15L.
- [SDR VNAA202602090022](https://openairdocs.org/sdr/VNAA202602090022.md): Stringer · corroded · Feb 10, 2026 · N510AE · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > STRINGER 18R IS CORRODED BETWEEN FS 295.00 AND 310.00, SH670-31631-1, STRINGER
- [SDR VNAA202602090029](https://openairdocs.org/sdr/VNAA202602090029.md): Seal Rest · corroded · Feb 10, 2026 · N510AE · Cndair CL6002C10 · Electrical/Electronic Compartment Doors
  > AVI BAY DOOR SEAL RETAINERS WERE CORRODED AND DENTED FROM IMPROPER RIVET INSTALL. NO ALLOWABLE LIMITS IN SRM. R&R REQ.
- [SDR VNAA202602090021](https://openairdocs.org/sdr/VNAA202602090021.md): Stringer · corroded · Feb 10, 2026 · N510AE · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > STRINGER 26R IS CORRODED BETWEEN FS 280.00 AND 310.00, SH670-31634-2, STRINGER
- [SDR VNAA202602090030](https://openairdocs.org/sdr/VNAA202602090030.md): Step · corroded · Feb 10, 2026 · N510AE · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR TOP STEP PANEL CORRODED. REQUIRES REPLACEMENT., PAX DOOR TOP STEP
- [SDR VNAA202602090031](https://openairdocs.org/sdr/VNAA202602090031.md): Seat Track · corroded · Feb 10, 2026 · N510AE · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > R/H SIDE SEAT RAIL IS CORRODED BETWEEN F.S. 863 TO F.S. 969,
- [SDR VNAA202602090020](https://openairdocs.org/sdr/VNAA202602090020.md): Hinge · gouged · Feb 10, 2026 · N510AE · Cndair CL6002C10 · Fuselage, Door Hinge
  > THE FWD CARGO DOOR AFT HINGE FITTING IS GOUGED ALONG THE UPPER EDGE. SH670-33840-8, HINGE FITTING BAG BAY
- [SDR VNAA202602090032](https://openairdocs.org/sdr/VNAA202602090032.md): Seat Track · corroded · Feb 10, 2026 · N510AE · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > L/H SIDE SEAT RAIL IS CORRODED BETWEEN F.S. 785.15 TO F.S. 863.
- [SDR VNAA202602090033](https://openairdocs.org/sdr/VNAA202602090033.md): Seat Track · corroded · Feb 10, 2026 · N510AE · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > R/H SIDE SEAT RAIL IS CORRODED BETWEEN F.S. 785.15 TO F.S. 863.
- [SDR VNAA202602090019](https://openairdocs.org/sdr/VNAA202602090019.md): Pan · gouged · Feb 10, 2026 · N510AE · Cndair CL6002C10 · Fuselage Main, Structure
  > L/P BLEED PAN FOUND TO HAVE 4EA GOUGES FROM CONTACT WITH GROUND AIR CONNECTION COVER. PLATE, MM670-35224-001
- [SDR VNAA202602090034](https://openairdocs.org/sdr/VNAA202602090034.md): Seat Track · corroded · Feb 10, 2026 · N510AE · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > R/H SIDE SEAT RAIL IS CORRODED BETWEEN F.S. 863 TO F.S. 969.
- [SDR VNAA202602090036](https://openairdocs.org/sdr/VNAA202602090036.md): Slat Track · damaged · Feb 10, 2026 · N510AE · Cndair CL6002C10 · Leading Edge Devices
  > LH SLAT TRACK 3-3 HAS WEAR DAMAGE,
- [SDR VNAA202602090018](https://openairdocs.org/sdr/VNAA202602090018.md): Landing · bent · Feb 10, 2026 · N510AE · Cndair CL6002C10 · Nacelle/Pylon, Main Frame
  > LH PYLON LANDING FOR PANEL 412DT IS BENT. MM670-37123-011 DOUBLER
- [SDR VNAA202602090037](https://openairdocs.org/sdr/VNAA202602090037.md): Window Post · corroded · Feb 10, 2026 · N510AE · Cndair CL6002C10 · Fuselage Main, Structure
  > RH SIDE POST (601R33223-2) REQUIRES REPLACEMENT TOP FASTENER HOLE IS CRACKED, POST, WINDSHIELD SIDE
- [SDR VNAA202602090038](https://openairdocs.org/sdr/VNAA202602090038.md): Bulkhead Web · corroded · Feb 10, 2026 · N510AE · Cndair CL6002C10 · Fuselage Main, Bulkhead
  > FS 280 BULKHEAD RH WEB IS CORRODED.
- [SDR VNAA202602090017](https://openairdocs.org/sdr/VNAA202602090017.md): Support Angle · corroded · Feb 10, 2026 · N510AE · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR FWD SUPPORT ANGLE CORRODED AND REQUIRE REPLACEMENT. 601R3187431-3S, FS 310
- [SDR VNAA202602090039](https://openairdocs.org/sdr/VNAA202602090039.md): Floorbeam · corroded · Feb 10, 2026 · N510AE · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > LH FS280 CROSSBEAM IS CORRODED AT BL0 ON TOP FWD EDGE. FOUND TO BE OUT OF LIMITS IAW CRJ-700 SRM 53-00-00-101-001-A01 DUE TO DEPTH OF CORROSION AND CORROSION ACROSS MULTIPLE ELEMENTS. REQUIRES REPLACEMENT.
- [SDR VNAA202602090040](https://openairdocs.org/sdr/VNAA202602090040.md): Floorbeam · corroded · Feb 10, 2026 · N510AE · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > RH FS280 CROSSBEAM IS CORRODED AT RBL6 ON TOP FWD EDGE. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-00-101-001-A01 DUE TO DEPTH OF CORROSION AND CORROSION ACROSS MULTIPLE ELEMENTS. REQUIRES REPLACEMENT.
- [SDR VNAA202602090016](https://openairdocs.org/sdr/VNAA202602090016.md): Intercostal · corroded · Feb 10, 2026 · N510AE · Cndair CL6002C10 · Passenger/Crew Doors
  > FOUND PAX DOOR DD7A INTERCOSTAL TO BE CORRODED. INSTALLED NEW SERVICEABLE PAX DOOR FWD MID DD7A INTERCOSTAL PN:601R318083-1 IAW CRJ700 SRM 51-42-06-001-001-A01 FS 310-349 INSIDE PAX DOOR
- [SDR VNAA202602090041](https://openairdocs.org/sdr/VNAA202602090041.md): Support Angle · cracked · Feb 10, 2026 · N510AE · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > LH SUPPORT ANGLE FOR 221ALF IS CRACKED ON AFT INBD SIDE.
- [SDR VNAA202602090042](https://openairdocs.org/sdr/VNAA202602090042.md): Angle · cracked · Feb 10, 2026 · N510AE · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > RH SUPPORT ANGLE FOR 221ALF IS CRACKED. CORRECTED
- [SDR VNA2026F00004](https://openairdocs.org/sdr/VNA2026F00004.md): Support Angle · cracked · Feb 10, 2026 · N510AE · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > RH SUPPORT ANGLE FOR 221ALF IS CRACKED.
- [SDR VNAA202602090015](https://openairdocs.org/sdr/VNAA202602090015.md): Intercostal · corroded · Feb 10, 2026 · N510AE · Cndair CL6002C10 · Passenger/Crew Doors
  > FOUND PAX DOOR FWD DD1 INTERCOSTAL TO BE CORRODED. 600-31902-259
- [SDR VNAA202602090014](https://openairdocs.org/sdr/VNAA202602090014.md): Intercostal · corroded · Feb 10, 2026 · N510AE · Cndair CL6002C10 · Passenger/Crew Doors
  > FOUND PAX DOOR AFT DD3 INTERCOSTAL TO BE CORRODED. 601R3180585-1
- [SDR VNAA202602090043](https://openairdocs.org/sdr/VNAA202602090043.md): Seat Track · corroded · Feb 10, 2026 · N510AE · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > R/H SIDE SEAT RAIL IS CORRODED BETWEEN F.S. 379 TO F.S. 485.
- [SDR VNAA202602090044](https://openairdocs.org/sdr/VNAA202602090044.md): Seat Track · corroded · Feb 10, 2026 · N510AE · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > FLOOR SEAT RAIL LOCATED AT LBL 9 FROM F.S. 379 TO F.S. 485 HAS MULTIPLE AREAS OF CORROSION, NICKS, AND GOUGES.
- [SDR VNAA202602090013](https://openairdocs.org/sdr/VNAA202602090013.md): Intercostal · corroded · Feb 10, 2026 · N510AE · Cndair CL6002C10 · Passenger/Crew Doors
  > FOUND PAX DOOR AFT DD2 INTERCOSTAL TO BE CORRODED 601R318052-1,
- [SDR VNAA202602090045](https://openairdocs.org/sdr/VNAA202602090045.md): Seat Track · corroded · Feb 10, 2026 · N510AE · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > FLOOR SEAT RAIL LOCATED AT LBL 9 BETWEEN F.S. 485.00 AND F.S. 581 FOUND TO BE CORRODED, WITH NICKS AND GOUGES.
- [SDR VNAA202602090012](https://openairdocs.org/sdr/VNAA202602090012.md): Intercostal · corroded · Feb 10, 2026 · N510AE · Cndair CL6002C10 · Passenger/Crew Doors
  > FOUND PAX DOOR AFT DD1 INTERCOSTAL TO BE CORRODED. 601R31902-318, INTERCOSTAL "
- [SDR VNA2026F00003](https://openairdocs.org/sdr/VNA2026F00003.md): Intercostal · corroded · Feb 10, 2026 · N510AE · Cndair CL6002C10 · Passenger/Crew Doors
  > FOUND PAX DOOR AFT DD1 INTERCOSTAL TO BE CORRODED. 601R31902-318, INTERCOSTAL "
- [SDR VNAA202602090046](https://openairdocs.org/sdr/VNAA202602090046.md): Seat Track · corroded · Feb 10, 2026 · N510AE · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > FLOOR SEAT RAIL LOCATED AT LBL 9 BETWEEN F.S. 581 AND F.S. 677 FOUND TO BE CORRODED, WITH NICKS AND GOUGES.
- [SDR VNAA202602090011](https://openairdocs.org/sdr/VNAA202602090011.md): Retainer · corroded · Feb 10, 2026 · N510AE · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR AFT SUPPORT ANGLE/SEAL RETAINER IS CORRODED. PAX DOOR AFT SUPPORT ANGLE, 601R318732-3S "
- [SDR VNAA202602090047](https://openairdocs.org/sdr/VNAA202602090047.md): Seat Track · corroded · Feb 10, 2026 · N510AE · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > FLOOR SEAT RAIL LOCATED AT LBL 9 BETWEEN F.S. 693 AND F.S. 830 FOUND TO BE CORRODED, WITH NICKS AND GOUGES.
- [SDR VNAA202602090048](https://openairdocs.org/sdr/VNAA202602090048.md): Seat Track · corroded · Feb 10, 2026 · N510AE · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > FLOOR SEAT RAIL LOCATED AT LBL 9 BETWEEN F.S. 830 AND F.S.985 FOUND TO BE CORRODED, WITH NICKS AND GOUGES.
- [SDR VNAA202602090049](https://openairdocs.org/sdr/VNAA202602090049.md): Seat Track · corroded · Feb 10, 2026 · N510AE · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > FLOOR SEAT RAIL LOCATED AT RBL 9 BETWEEN F.S. 349.00 AND F.S. 485.00 FOUND TO BE CORRODED, WITH NICKS AND GOUGES.
- [SDR VNAA202602090050](https://openairdocs.org/sdr/VNAA202602090050.md): Seat Track · corroded · Feb 10, 2026 · N510AE · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > FLOOR SEAT RAIL LOCATED AT RBL 9 BETWEEN F.S. 485.00 AND F.S. 581 FOUND TO BE CORRODED, WITH NICKS AND GOUGES.
- [SDR VNAA202602090010](https://openairdocs.org/sdr/VNAA202602090010.md): Actuator · corroded · Feb 10, 2026 · N510AE · Cndair CL6002C10 · Trailing Edge Flaps
  > LH BUTE DOOR ACTUATOR AT WS 264 IS CORRODED, 600-10246-1, BUTE DOOR ACTUATOR
- [SDR VNAA202602090051](https://openairdocs.org/sdr/VNAA202602090051.md): Seat Track · corroded · Feb 10, 2026 · N510AE · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > FLOOR SEAT RAIL LOCATED AT RBL 9 BETWEEN F.S. 581 AND F.S. 677 FOUND TO BE CORRODED, WITH NICKS AND GOUGES.
- [SDR VNAA202602090052](https://openairdocs.org/sdr/VNAA202602090052.md): Seat Track · corroded · Feb 10, 2026 · N510AE · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > FLOOR SEAT TRACK LOCATED AT RBL 9 BETWEEN F.S. 677.00 AND F.S. 830.00 FOUND TO BE CORRODED, WITH NICKS AND GOUGES.
- [SDR VNAA202602090053](https://openairdocs.org/sdr/VNAA202602090053.md): Seat Track · corroded · Feb 10, 2026 · N510AE · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK AT LBL 27, FS 364-FS485 IS CORRODED.
- [SDR VNAA202602090009](https://openairdocs.org/sdr/VNAA202602090009.md): Accumulator · no test · Feb 10, 2026 · N510AE · Cndair CL6002C10 · Landing Gear Brake System
  > SYSTEM NR 3 HYDRAULIC BRAKE ACCUMULATOR FAILED THE PRESSURE-DECAY RATE FUNCTIONAL CHECK. BRAKE ACCUMULATOR REQUIRES REPLACEMENT. 90006691, HYDRAULIC BRAKE ACCUMULATOR
- [SDR VNAA202602090054](https://openairdocs.org/sdr/VNAA202602090054.md): Seat Track · corroded · Feb 10, 2026 · N510AE · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK AT LBL 27, FS485 - FS 581 IS CORRODED. SEAT TRACK
- [SDR VNAA202602090008](https://openairdocs.org/sdr/VNAA202602090008.md): Panel · chafed · Feb 10, 2026 · N510AE · Cndair CL6002C10 · Ailerons
  > FOUND PANEL 699AB TO BE CHAFED, CC670-13000, SHROUD AILERON,

Next page: https://openairdocs.org/aircraft/N510AE/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 = 'N510AE' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N510AE/reports

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