# Service difficulty reports: N538EG

A list on [N538EG](https://openairdocs.org/aircraft/N538EG.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 · 125 reports

- [SDR VNAA202606180010](https://openairdocs.org/sdr/VNAA202606180010.md): Floor Support · corroded · Jun 18, 2026 · N538EG · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > RIGHT FLOOR SILL IS CORRODED BETWEEN F.S. 310 TO F.S. 319. REMOVED CORRODED SILL AND INSTALLED A SERVICABLE SILL IAW SRM 51-42-06-001-001-A01, SRM 51-42-13-001-001-A01 AND SRM 51-42-21-001-001-A01.
- [SDR VNAA202606180009](https://openairdocs.org/sdr/VNAA202606180009.md): Plate · corroded · Jun 18, 2026 · N538EG · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > FWD BAGGAGE BAY DOOR SURROUND STRUCTURE MOUNTING PLATE AT FS533 BETWEEN STGR26L AND STGR27 IS CORRODED. REMOVED AND REPLACED MOUNTING PLATE IAW SRM 51-40-11-001-001-A01, 51-42-21-001-001-A01, & SRM 51-42-22-001-001-A01.
- [SDR VNAA202606180008](https://openairdocs.org/sdr/VNAA202606180008.md): Angle · corroded · Jun 18, 2026 · N538EG · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > PAX DOOR UPPER SILL ANGLE IS CORRODED REPLACED SILL ANGLE.
- [SDR VNAA202606180007](https://openairdocs.org/sdr/VNAA202606180007.md): Plate · corroded · Jun 18, 2026 · N538EG · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > FWD BAGGAGE BAY DOOR SURROUND STRUCTURE MOUNTING PLATE AT FS581 BETWEEN STGR 22L AND STGR 23L IS CORRODED. REPLACED MOUNTING PLATE IAW SRM 51-42-22-001-001-A01, SRM 51-42-21-001-001-A01.
- [SDR VNAA202606180006](https://openairdocs.org/sdr/VNAA202606180006.md): Frame · corroded · Jun 18, 2026 · N538EG · Cndair CL6002C10 · Fuselage Main, Frame
  > FS 280 J ANGLE CORRODED. REMOVED FS 280 J ANGLE IAW SRM 51-42-21-001-001-A01 AND 51-42-06-001-001-A01. LOCATED AND DRILLED NEW SERVICEABLE J ANGLE ASSY IAW SRM 51-40-11-001-001-A01. INSTALLED NEW SERVICEABLE J ANGLE ASSY IAW SRM 51-42-06-001-001-A01, & 51-4
- [SDR VNAA202606180005](https://openairdocs.org/sdr/VNAA202606180005.md): Frame · corroded · Jun 18, 2026 · N538EG · Cndair CL6002C10 · Fuselage Main, Frame
  > FWD SIDE OF FRAME BS 319 CORRODED BETWEEN STGR 24L-25L. FRAME.
- [SDR VNAA202606180004](https://openairdocs.org/sdr/VNAA202606180004.md): Intercostal · corroded · Jun 18, 2026 · N538EG · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR FWD INTERCOSTAL DD7 FOUND TO BE CORRODED REQUIRED REPLACEMENT. REPLACED PAX DOOR FWD INTERCOSTAL DD7 IAW SRM 51-42-06-001-001-A01.
- [SDR VNAA202606180003](https://openairdocs.org/sdr/VNAA202606180003.md): Stringer · corroded · Jun 18, 2026 · N538EG · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > STGR 26R CORRODED BETWEEN FS 319-333 STRINGER,
- [SDR VNAA202606180001](https://openairdocs.org/sdr/VNAA202606180001.md): Angle · corroded · Jun 18, 2026 · N538EG · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR AFT ANGLE CAP HAS CORROSION ON THE FWD CORNER.
- [SDR VNAA2025122411101](https://openairdocs.org/sdr/VNAA2025122411101.md): Hydraulic Line · leaking · Dec 23, 2025 · N538EG · Cndair CL6002C10 · Hydraulic System, Main
  > LOSS OF HYD PRESSURE ON SYS 2.QTY @ 0%. FOUND HYDRAULIC SYSTEM 2 LEAK COMING FROM FWD OUTBOARD BRAKE ACCUMULATOR LINE. OUTBOARD BRAKE ACCUMULATOR LINE TORQUED IAW CRJ 700 AMM 32-43-16-400-801-A01-PSA. HYDRAULIC SYSTEM #2 BLED AND SERVICED IAW CRJ 700 AMM 29€
- [SDR VNAA2025062711101](https://openairdocs.org/sdr/VNAA2025062711101.md): Windshield · cracked · Jun 23, 2025 · N538EG · Cndair CL6002C10 · Flight Compartment Windows
  > CA WINDSHIELD CRACKED IN FLIGHT, REMOVE AND REPLACED LH WINDSHIELD IAW CRJ 700 AMM 56-11-01-000/400-801-A01-PSA. OPS CHECK GOOD. LEAK CHECK GOOD.
- [SDR VNAA2024082711106](https://openairdocs.org/sdr/VNAA2024082711106.md): Window · sparks · Aug 25, 2024 · N538EG · Cndair CL6002C10 · Flight Compartment Windows
  > L WINDOW HEAT CAUTION WITH ELECTRICAL ARCING / REMOVED AND INSTALLED LH SIDE WINDOW IAW CRJ 700 AMM 56-12-01-000/400-801. PERFORM OPS TEST OF WINDOW HEAT CONT IAW CRJ 700 AMM 30-41-06-710-810. PRESSURIZED AND LEAK TEST A/C IAW CRJ 700 AMM 21-31-00-910-801. AL
- [SDR VNAA202208149997](https://openairdocs.org/sdr/VNAA202208149997.md): Slat Track · corroded · Aug 14, 2022 · N538EG · Cndair CL6002C10 · Leading Edge Devices
  > PITTING CORROSION ON SLAT TRACKS 3-1, 3-2 UPPER SURFACE, SLAT #3 RH WING
- [SDR VNAA202208149996](https://openairdocs.org/sdr/VNAA202208149996.md): Slat Track · corroded · Aug 14, 2022 · N538EG · Cndair CL6002C10 · Leading Edge Devices
  > PITTING CORROSION ON SLAT TRACKS 2-1, 2-3 UPPER SURFACE & SLAT TRACK 2-2 UPPER/LOWER SURFACE; SLAT #2 RH WING.
- [SDR VNAA202208149995](https://openairdocs.org/sdr/VNAA202208149995.md): Slat Track · corroded · Aug 14, 2022 · N538EG · Cndair CL6002C10 · Leading Edge Devices
  > PITTING CORROSION ON SLAT TRACKS 1-1, 1-3 UPPER SURFACE & SLAT TRACK 1-2 UPPER/LOWER SURFACE; SLAT #1, RH WING
- [SDR VNAA202208149994](https://openairdocs.org/sdr/VNAA202208149994.md): Slat Track · corroded · Aug 14, 2022 · N538EG · Cndair CL6002C10 · Leading Edge Devices
  > PITTING CORROSION ON SLAT TRACKS 2-1, 2-3 UPPER SURFACE & SLAT TRACK 2-2 UPPER/LOWER SURFACE; SLAT #2 LH WING.
- [SDR VNAA202208149993](https://openairdocs.org/sdr/VNAA202208149993.md): Slat Track · corroded · Aug 14, 2022 · N538EG · Cndair CL6002C10 · Wing, Control Surfaces
  > PITTING CORROSION ON SLAT TRACKS 1-1, 1-3 UPPER SURFACE & SLAT TRACK 1-2 UPPER/LOWER SURFACE; SLAT #1 LH WING
- [SDR VNAA202208149992](https://openairdocs.org/sdr/VNAA202208149992.md): Skin · dented · Aug 14, 2022 · N538EG · Cndair CL6002C10 · Fuselage Structure (General)
  > DENT ON EXTERNAL FUSELAJE SKIN BTW FS STA 394 AND FS STA 409 BTW STGR 20RH AND STGR 19RH
- [SDR VNAA2022081401](https://openairdocs.org/sdr/VNAA2022081401.md): Skin · none · Aug 14, 2022 · N538EG · Cndair CL6002C10 · Wing, Plate/Skin
  > WEAR ON LOWER SKIN, BELOW FLAP HINGE BOX ACCESS PANELS, LH WING. (REF. WS 68, WS128, WS220 APROX).
- [SDR VNAA2022082799928](https://openairdocs.org/sdr/VNAA2022082799928.md): Canister · cracked · Jun 19, 2022 · N538EG · Cndair CL6002C10 · Fuel Storage
  > CRACK ON CANISTER, WELDED NO.3 IN STA. WS148 AT LH MAIN FUEL TANK.
- [SDR VNAA2022082799927](https://openairdocs.org/sdr/VNAA2022082799927.md): None · corroded · Jun 19, 2022 · N538EG · Cndair CL6002C10 · Fuselage Internal Mounting Structure
  > CORROSION AT CHORD INNER (3) BELOW LOWER SILL BTW FS1000 TO FS1047 AT AFT CARGO COMPARTMENT
- [SDR VNAA2022082799926](https://openairdocs.org/sdr/VNAA2022082799926.md): Stringer · corroded · Jun 17, 2022 · N538EG · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > CORROSION ON STGR 26LH BTW. FS: 265 TO FS: 250 AT AVIONICS COMPARTMENT
- [SDR VNAA202208279992](https://openairdocs.org/sdr/VNAA202208279992.md): Exhaust Duct · bent · Jun 16, 2022 · N538EG · Cndair CL6002C10 · APU Exhaust System
  > BENT APU EXHAUST DUCT AFT EDGE, SEVERAL LOCATIONS.
- [SDR VNAA2022082799924](https://openairdocs.org/sdr/VNAA2022082799924.md): Access Panel · corroded · Jun 15, 2022 · N538EG · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > CORROSION ON ACCESS PANEL 699BB,542AZ
- [SDR VNAA2022082799941](https://openairdocs.org/sdr/VNAA2022082799941.md): Former · corroded · Jun 14, 2022 · N538EG · Cndair CL6002C10 · Passenger/Crew Doors
  > CORROSION IN SEVERAL AREAS ON FORMER FS311.75 (INTERLAL SIDE) BTW INTERCOSTAL DD6 AND DD5 AT PASSENGER DOOR.
- [SDR VNAA2022082799940](https://openairdocs.org/sdr/VNAA2022082799940.md): Former · corroded · Jun 14, 2022 · N538EG · Cndair CL6002C10 · Passenger/Crew Doors
  > CORROSION ON FORMER FS311.75 (INTERLAL SIDE) BTW INTERCOSTAL DD1 AND DD1A AT PASSENGER DOOR
- [SDR VNAA2022082799939](https://openairdocs.org/sdr/VNAA2022082799939.md): Former · corroded · Jun 14, 2022 · N538EG · Cndair CL6002C10 · Passenger/Crew Doors
  > CORROSION ON FORMER FS311.75 (INTERLAL SIDE) BTW INTERCOSTAL DD1 AND LOWER EDGE OF PASSENGER DOOR
- [SDR VNAA2022082799938](https://openairdocs.org/sdr/VNAA2022082799938.md): Seat Track · corroded · Jun 14, 2022 · N538EG · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION AT LBL9 SEAT RAIL BETWEEN FS 581 TO FS 677.(CPAX)
- [SDR VNAA2022082799937](https://openairdocs.org/sdr/VNAA2022082799937.md): Seat Track · corroded · Jun 14, 2022 · N538EG · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION AT RBL9 SEAT RAIL BETWEEN FS 485 AND FS 581(CPAX)
- [SDR VNAA2022082799936](https://openairdocs.org/sdr/VNAA2022082799936.md): Seat Track · corroded · Jun 14, 2022 · N538EG · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION AT RBL9 SEAT RAIL BETWEEN FS 677 AND FS 581(CPAX)
- [SDR VNAA2022082799935](https://openairdocs.org/sdr/VNAA2022082799935.md): Seat Track · corroded · Jun 14, 2022 · N538EG · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION AT SEAT RAIL BETWEEN FS 573AND FS 485, STRG 15LH (CPAX)
- [SDR VNAA2022082799934](https://openairdocs.org/sdr/VNAA2022082799934.md): Seat Track · corroded · Jun 14, 2022 · N538EG · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION AT SEAT RAIL BETWEEN FS 485 AND FS 581, STRG 15RH (CPAX)
- [SDR VNAA2022082799933](https://openairdocs.org/sdr/VNAA2022082799933.md): Seat Track · corroded · Jun 14, 2022 · N538EG · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION AT SEAT RAIL BETWEEN FS 379 AND FS 485, STRG 15RH (CPAX)
- [SDR VNAA2022082799932](https://openairdocs.org/sdr/VNAA2022082799932.md): Seat Track · corroded · Jun 14, 2022 · N538EG · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION AND GOUGES LATERAL SIDE RAIL STGR 15RH BTW FS 785.00/847.00
- [SDR VNAA2022082799931](https://openairdocs.org/sdr/VNAA2022082799931.md): Seat Track · corroded · Jun 14, 2022 · N538EG · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON LATERAL SIDE RAIL STGR 15 RH BTW FS713.00/742.00
- [SDR VNAA2022082799930](https://openairdocs.org/sdr/VNAA2022082799930.md): Seat Track · gouged · Jun 14, 2022 · N538EG · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > GOUGES ON LATERAL SIDE RAIL STGR 15 LH BTW FS873.00/939.00
- [SDR VNAA2022082799929](https://openairdocs.org/sdr/VNAA2022082799929.md): Seat Track · gouged · Jun 14, 2022 · N538EG · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > GOUGES ON LATERAL SIDE RAIL STGR 15 LH BTW FS677.00/801.00
- [SDR VNAA2022082799923](https://openairdocs.org/sdr/VNAA2022082799923.md): Canister · cracked · Jun 14, 2022 · N538EG · Cndair CL6002C10 · Fuel Storage
  > CRACK AT CANISTER, WELDED NO.3 IN STA. WS148 AT RH MAIN FUEL TANK.
- [SDR VNAA2022082799922](https://openairdocs.org/sdr/VNAA2022082799922.md): Seat Track · corroded · Jun 14, 2022 · N538EG · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > NICKS, CORROSION & SCRATCHES ON LH SIDE SEAT RAIL (SEVERAL LOCATIONS), PAX CABIN. (REF. BTW FS379-FS469).
- [SDR VNAA2022082799921](https://openairdocs.org/sdr/VNAA2022082799921.md): Seat Track · corroded · Jun 14, 2022 · N538EG · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > NICKS AND CORROSION ON SEVERAL AREAS OF SEAT RAIL LBL9 BTW FS677.00/863.00
- [SDR VNAA2022082799920](https://openairdocs.org/sdr/VNAA2022082799920.md): Seat Track · corroded · Jun 14, 2022 · N538EG · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > NICKS AND WEAR ON SEVERAL AREAS OF SEAT RAIL RBL9 BTW FS677.00/863.00
- [SDR VNAA2022082799919](https://openairdocs.org/sdr/VNAA2022082799919.md): Seat Track · corroded · Jun 14, 2022 · N538EG · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION AT RBL9 SEAT RAIL BETWEEN FS 349 AND FS 485(CPAX)
- [SDR VNAA2022082799918](https://openairdocs.org/sdr/VNAA2022082799918.md): Seat Track · corroded · Jun 14, 2022 · N538EG · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION AT LBL9 SEAT RAIL BETWEEN FS 485TO FS 581.
- [SDR VNAA2022082799917](https://openairdocs.org/sdr/VNAA2022082799917.md): Seat Track · corroded · Jun 14, 2022 · N538EG · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION AT SEAT RAIL BETWEEN FS 677 AND FS 581, STRG 15LH
- [SDR VNAA2022082799916](https://openairdocs.org/sdr/VNAA2022082799916.md): Seat Track · corroded · Jun 14, 2022 · N538EG · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION AT SEAT RAIL BETWEEN FS 581 AND FS 661, STRG 15RH
- [SDR VNAA2022082799915](https://openairdocs.org/sdr/VNAA2022082799915.md): Rib · cracked · Jun 14, 2022 · N538EG · Cndair CL6002C10 · Wing, Rib/Bulkhead
  > CRACK ON RIB LEADING EDGE SS57.16 AT LH WING
- [SDR VNAA2022082799914](https://openairdocs.org/sdr/VNAA2022082799914.md): Seat Track · corroded · Jun 14, 2022 · N538EG · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > NICS AND CORROSION ON SEVERAL AREAS OF SEAT RAIL LBL9 BTW FS863.00/985.00.00
- [SDR VNAA202208229991](https://openairdocs.org/sdr/VNAA202208229991.md): Canister · cracked · Jun 14, 2022 · N538EG · Cndair CL6002C10 · Fuel Storage
  > CRACK AT CANISTER, WELDED NO.3 IN STA. WS148 AT RH MAIN FUEL TANK.
- [SDR VNAA2022082799913](https://openairdocs.org/sdr/VNAA2022082799913.md): Fitting · corroded · Jun 13, 2022 · N538EG · Cndair CL6002C10 · Fuselage Main, Attach Fittings
  > CORROSION ON AFT CLOSING FITTING, PAX SURROUND STRUCTURE FUSELAGE FRAME (REF. SILL AREA).
- [SDR VNAA2022082799912](https://openairdocs.org/sdr/VNAA2022082799912.md): Stringer · cracked · Jun 13, 2022 · N538EG · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > CRACK ON STRINGER 03L & FS280, INTERNAL STRUCTURE, PAX CABIN.

Next page: https://openairdocs.org/aircraft/N538EG/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 = 'N538EG' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N538EG/reports

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.