# Service difficulty reports: N528EG

A list on [N528EG](https://openairdocs.org/aircraft/N528EG.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 · 126 reports

- [SDR VNAA2026101926501](https://openairdocs.org/sdr/VNAA2026101926501.md): Pcu · faulted · Oct 16, 2026 · N528EG · Cndair CL6002C10 · Drag Control System
  > OB FLT SPLRS AND OB SPOILERONS CAUTION IN FLIGHT. C/A INSTALLED NEW LH OB MULITFUNCTION SPOILER PCU IAW CRJ 700 AMM 27-62-01-400-801-A02-PSA. OPS CHECK AND LEAK CHECK GOOD.
- [SDR 1Q2R2026093020226](https://openairdocs.org/sdr/1Q2R2026093020226.md): Bracket · torn · Sep 28, 2026 · N528EG · Cndair CL6002C10 · Horizontal Stabilizer Miscellaneous Structure
  > ELEVATOR AFT CABLE QUADRANT CABLE, CABLE GUARD BRACKET TORN. PERFORMED PERMANENT REPAIR IAW RFTS-131207 REV. 0, AND EA 5520-2026-1137 REV -.
- [SDR 1Q2R2026101120190](https://openairdocs.org/sdr/1Q2R2026101120190.md): Pulley Bracket · damaged · Sep 14, 2026 · N528EG · Cndair CL6002C10 · Passenger/Crew Doors
  > POWER ASSIST MOTOR CABLE YOKE ASSEMBLY, AFT HOLE IN PULLEY MOUNTING BRACKET ELONGATED. PERFORMED PERMANENT REPAIR IN ACCORDANCE WITH RFTS-130879 REV. 0, DATED SEPTEMBER 14, 2026, AND MHI RJ REO 670-52-11-1604 REV. --, DATED SEPTEMBER 11, 2026.
- [SDR 1Q2R2026091320196](https://openairdocs.org/sdr/1Q2R2026091320196.md): Strap · gouged · Sep 13, 2026 · N528EG · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > BS 985, STRINGER 27 WAS GOUGED & 2 EA DENTS AND A BROKEN STRAP ASSY WHICH CAUSED THE DAMAGE.
- [SDR 1Q2R2026090220108](https://openairdocs.org/sdr/1Q2R2026090220108.md): Hinge · gouged · Sep 8, 2026 · N528EG · Cndair CL6002C10 · Spoilers
  > LEFT OTBD FLAP INBD SPOILER HINGE GOUGED ON THE CENTER HINGE.
- [SDR 1Q2R202610120158](https://openairdocs.org/sdr/1Q2R202610120158.md): Strap · corroded · Sep 7, 2026 · N528EG · Cndair CL6002C10 · Service Doors
  > GALLEY SERVICE DOOR FORWARD CIRCUMFERENCE JOINT AT STRGR 17 RH HAS CORROSION.
- [SDR 1Q2R2026092220197](https://openairdocs.org/sdr/1Q2R2026092220197.md): Diaphragm · cracked · Sep 7, 2026 · N528EG · Cndair CL6002C10 · Aerodynamic Fairings
  > LEFT LOWER WING-TO-FUSELAGE FAIRING AT BS 909 DIAPHRAGM IS CRACKED, 1.60" FROM LOWER T/E. PERFORMED PERMANENT REPAIR IAW RFTS-130820 REV. 0, AND REO 670-53-82-478 REV. -A.
- [SDR 1Q2R2026091320158](https://openairdocs.org/sdr/1Q2R2026091320158.md): Strap · corroded · Sep 3, 2026 · N528EG · Cndair CL6002C10 · Galley Doors
  > GALLEY SERVICE DOOR FWD CIRCUMFERENCE JOINT AT STGR17R HAS CORROSION. PERFORMED PERMANENT REPAIR IN ACCORDANCE WITH RFTS-130740 REV. 0,, AND EA 5241-2026-1004, REV -.
- [SDR 1Q2R2026082550044](https://openairdocs.org/sdr/1Q2R2026082550044.md): Vane · damaged · Aug 26, 2026 · N528EG · Cndair CL6002C10 · Trailing Edge Flaps
  > LEFT INBB FLAP BOLT HOLE FOR 548AB HAS BROKEN BOLT IN NUTPLATE AND HOLE IS ELONGATED.
- [SDR 1Q2R2026080320027](https://openairdocs.org/sdr/1Q2R2026080320027.md): Fitting · gouged · Jul 30, 2026 · N528EG · Cndair CL6002C10 · Fuselage Main, Structure
  > RIGHT SIDE STAY FITTING HAS GOUGES NEAR THE TOP OF FITTING. PERFORMED PERMANENT REPAIR IAW RFTS-130144 REV. 0, AND REO 670-57-11-043, REV -A,
- [SDR 1Q2R2026073050055](https://openairdocs.org/sdr/1Q2R2026073050055.md): Beam · chafed · Jul 30, 2026 · N528EG · Cndair CL6002C10 · Engine Thrust Reverser
  > LATCH BEAM CHAFED.
- [SDR 1Q2R2026080220022](https://openairdocs.org/sdr/1Q2R2026080220022.md): Fitting · gouged · Jul 29, 2026 · N528EG · Cndair CL6002C10 · Main Landing Gear Attach Section
  > L/H SIDE STAY FITTING HAS GOUGE NEAR THE TOP OF FITTING. PERFORMED PERMANENT REPAIR IN ACCORDANCE WITH RFTS-130145 REV. 0, DATED JULY 29, 2026, AND MHI RJ REO 670-57-11-263 REV. --, DATED JULY 28, 2026.
- [SDR 1Q2R2026080220061](https://openairdocs.org/sdr/1Q2R2026080220061.md): Fitting · chafed · Jul 29, 2026 · N528EG · Cndair CL6002C10 · Fuselage, Wing Attach Fittings
  > RT WING TO FUSELAGE ATTACHMENT FITTING AT FS797.00 HAS TWO CHAFED AREAS. PERFORMED PERMANENT REPAIR IN ACCORDANCE WITH RFTS-130158 REV. 0, DATED JULY 29, 2026, AND MHI RJ REO 670-57-11-265 REV. --, DATED JULY 29, 2026.
- [SDR 1Q2R2026072920068](https://openairdocs.org/sdr/1Q2R2026072920068.md): Skin · dented · Jul 29, 2026 · N528EG · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > DENT FOUND IN ZONE 122 BELOW ADG COMPARTMENT DOOR BETWEEN FS169.00 AND FS202.00 BELOW WL79.50. PERFORMED PERMANENT REPAIR IN ACCORDANCE WITH RFTS-130058 REV. 0, DATED JULY 29, 2026 AND MHI RJ REO 670-51-00-85 REV. -A, DATED AUGUST 23, 2017 AND REO 670-53-11-23
- [SDR VNAA202206279995](https://openairdocs.org/sdr/VNAA202206279995.md): Door Sill · corroded · May 28, 2022 · N528EG · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > CORROSION ON BACKUP SILL (STGR 21L) BETWEEN FS310 AND FS333 AT PASSENGER DOOR SURROUND STRUCTURE.
- [SDR VNAA2022062699913](https://openairdocs.org/sdr/VNAA2022062699913.md): Stringer · corroded · May 25, 2022 · N528EG · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > CORROSION ON STGR 26LH BTW FS STA: 349 AND FS STA: 333 AT MAIN AVIONICS COMPARTMENT. (E/E)
- [SDR VNAA202206259992](https://openairdocs.org/sdr/VNAA202206259992.md): Intercostal · corroded · May 25, 2022 · N528EG · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > CORROSION ON INTERCOSTAL (RH) NEAR STGR 27 BTW FS STA: 364 AND FS STA: 349 AT E/E COMPARTMENT.
- [SDR VNAA2022062699912](https://openairdocs.org/sdr/VNAA2022062699912.md): Floor Support · corroded · May 15, 2022 · N528EG · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > CORROSION ON FLOOR SUPPORT IN STA. FS= 280 BETWEEN STRG 26LH TO 26RH AT MAIN AVIONICS COMPARTMENT. (E/E)
- [SDR VNAA2022062799922](https://openairdocs.org/sdr/VNAA2022062799922.md): Stringer Splice · corroded · May 13, 2022 · N528EG · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > CORROSION WAS FOUND ON STRINGER SPLICE 21RH BTW FS STA 349 AND FS STA 222 AT E/E.
- [SDR VNAA2022062799921](https://openairdocs.org/sdr/VNAA2022062799921.md): Web · corroded · May 12, 2022 · N528EG · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > CORROSION WERE FOUND ON HARDWARE OF FITTINGS AND CORROSION WAS FOUND ON PROTECTOR WEB FLOOR 4EA'S
- [SDR VNAA2022062799920](https://openairdocs.org/sdr/VNAA2022062799920.md): Seat Track · corroded · May 12, 2022 · N528EG · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON FLOOR SEAT RAIL AT LBL 27 BETWEEN FS571.00-FS693.00 AT PASSENGER CABIN.
- [SDR VNAA2022062799919](https://openairdocs.org/sdr/VNAA2022062799919.md): Seat Track · corroded · May 12, 2022 · N528EG · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON FLOOR DEAT RAIL AT LBL 9 BETWEEN FS571.00-FS683.00 AT PASSENGER CABIN.
- [SDR VNAA2022062799918](https://openairdocs.org/sdr/VNAA2022062799918.md): Seat Track · corroded · May 12, 2022 · N528EG · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON FLOOR DEAT RAIL AT RBL 9 BETWEEN FS571.00-FS683.00 AT PASSENGER CABIN.
- [SDR VNAA2022062799917](https://openairdocs.org/sdr/VNAA2022062799917.md): Seat Track · corroded · May 12, 2022 · N528EG · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON FLOOR SEAT RAIL AT RBL 9 BETWEEN FS485.00-FS571.00 AT PASSENGER CABIN.
- [SDR VNAA2022062799916](https://openairdocs.org/sdr/VNAA2022062799916.md): Seat Track · corroded · May 12, 2022 · N528EG · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON LH SIDE SEAT RAIL AT WL85.25 BETWEEN FS861.00-FS969.00.
- [SDR VNAA2022062799915](https://openairdocs.org/sdr/VNAA2022062799915.md): Seat Track · corroded · May 12, 2022 · N528EG · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON RH SIDE SEAT RAIL AT WL85.25 BETWEEN FS861.00-FS969.00.
- [SDR VNAA2022062799914](https://openairdocs.org/sdr/VNAA2022062799914.md): Seat Track · corroded · May 12, 2022 · N528EG · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON LH SIDE SEAT RAIL AT WL85.25 BETWEEN FS785.15-FS861.00.
- [SDR VNAA2022062799913](https://openairdocs.org/sdr/VNAA2022062799913.md): Seat Track · corroded · May 12, 2022 · N528EG · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON RH SIDE SEAT RAIL AT WL85.25 BETWEEN FS785.15-FS861.00.
- [SDR VNAA2022062799912](https://openairdocs.org/sdr/VNAA2022062799912.md): Seat Track · corroded · May 12, 2022 · N528EG · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON RH SIDE SEAT RAIL AT WL85.25 BETWEEN FS713.00-FS761.85.
- [SDR VNAA2022062799911](https://openairdocs.org/sdr/VNAA2022062799911.md): Seat Track · corroded · May 12, 2022 · N528EG · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON RH SIDE SEAT RAIL AT WL85.25 BETWEEN FS675.00-FS713.00.
- [SDR VNAA2022062799910](https://openairdocs.org/sdr/VNAA2022062799910.md): Seat Track · corroded · May 12, 2022 · N528EG · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON RH SIDE SEAT RAIL AT WL85.25 BETWEEN FS477.40-FS573.00.
- [SDR VNAA202206279999](https://openairdocs.org/sdr/VNAA202206279999.md): Seat Track · corroded · May 12, 2022 · N528EG · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON RH SIDE SEAT RAIL AT WL85.25 BETWEEN FS379.00-FS477.40.
- [SDR VNAA202206279998](https://openairdocs.org/sdr/VNAA202206279998.md): Seat Track · corroded · May 12, 2022 · N528EG · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON LH SIDE SEAT RAIL AT WL85.25 BETWEEN FS573.00-FS669.40.
- [SDR VNAA202206279997](https://openairdocs.org/sdr/VNAA202206279997.md): Seat Track · corroded · May 12, 2022 · N528EG · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON LH SIDE SEAT RAIL AT WL85.25 BETWEEN FS477.40-FS573.00.
- [SDR VNAA202206279996](https://openairdocs.org/sdr/VNAA202206279996.md): Seat Track · corroded · May 12, 2022 · N528EG · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON LH SIDE SEAT RAIL AT WL85.25 BETWEEN FS379.00-FS477.40.
- [SDR VNAA202206279993](https://openairdocs.org/sdr/VNAA202206279993.md): Angle · corroded · May 11, 2022 · N528EG · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > SECONDARY NRC IN REF NRC 00124 [AFTER REMOVAL OF SETTLEMENT AREA OF LOWER SECTION OF WING-TO-FUSELAGE FAIRING (STRAP MID)]; MID ANGLES WERE FOUND WITH CORROSION AT FS STA 909.00.
- [SDR VNAA202206279992](https://openairdocs.org/sdr/VNAA202206279992.md): Access Panel · corroded · May 11, 2022 · N528EG · Cndair CL6002C10 · Wing, Plate/Skin
  > CORROSION ON ACCESS PANELS NBR 642AZ, 642BZ, 542AZ, AND 542BZ.
- [SDR VNAA202206279991](https://openairdocs.org/sdr/VNAA202206279991.md): Cap · corroded · May 11, 2022 · N528EG · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > CORROSION ON MID CAP ON L1 DOOR SURROUND STRUCTURE.
- [SDR VNAA202206269999](https://openairdocs.org/sdr/VNAA202206269999.md): Skin · corroded · May 11, 2022 · N528EG · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > CORROSION ON DRAIN HOLES AT FUSELAGE EXTERNAL SKIN BTW FS939.00/953.00 AND STGR 26LH/RH.
- [SDR VNAA202206259991](https://openairdocs.org/sdr/VNAA202206259991.md): Skin Panel · corroded · May 11, 2022 · N528EG · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > CORROSION ON EXTERNAL FUSELAGE SKIN AND FASTENERS BETWEEN STGR 16R-STGR 24R AND FS 1000.00-FS 1108.00
- [SDR VNAA2022062699911](https://openairdocs.org/sdr/VNAA2022062699911.md): Fairing · corroded · May 10, 2022 · N528EG · Cndair CL6002C10 · Aerodynamic Fairings
  > CORROSION ON SETTLEMENT AREA OF FAIRING 193AB EXTERNAL STRUCTURE FS800.
- [SDR VNAA202206279990](https://openairdocs.org/sdr/VNAA202206279990.md): Angle · corroded · May 9, 2022 · N528EG · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > CORROSION ON LOWER SILL ANGLE (SEVERAL LOCATIONS) AT SERVICE DOOR SURROUND STRUCTURE. (RE. BEHIND LOWER FITTING).
- [SDR VNAA2022062699920](https://openairdocs.org/sdr/VNAA2022062699920.md): Slat Track · corroded · May 9, 2022 · N528EG · Cndair CL6002C10 · Leading Edge Devices
  > PITTING CORROSION ON SLAT TRACKS 3-1 (SEVERAL LOCATION AT UPPER SURFACE) & 3-2 (SEVERAL LOCATION AT UPPER & LOWER SURFACE), SLAT #3, RH WING.
- [SDR VNAA2022062699919](https://openairdocs.org/sdr/VNAA2022062699919.md): Slat Track · corroded · May 9, 2022 · N528EG · Cndair CL6002C10 · Leading Edge Devices
  > PITTING CORROSION ON SLAT TRACKS 2-1 (SEVERAL LOCATION AT UPPER SURFACE), 2-2 & 2-3 (SEVERAL LOCATION AT UPPER & LOWER SURFACE), SLAT #2, RH WING.
- [SDR VNAA2022062699918](https://openairdocs.org/sdr/VNAA2022062699918.md): Slat Track · corroded · May 9, 2022 · N528EG · Cndair CL6002C10 · Leading Edge Devices
  > PITTING CORROSION ON SLAT TRACKS 1-1, 1-2, & 1-3 (SEVERAL LOCATION AT UPPER & LOWER SURFACE), SLAT #1, RH WING.
- [SDR VNAA2022062699917](https://openairdocs.org/sdr/VNAA2022062699917.md): Slat Track · corroded · May 9, 2022 · N528EG · Cndair CL6002C10 · Leading Edge Devices
  > PITTING CORROSION ON SLAT TRACKS 3-1 (SEVERAL LOCATION AT UPPER SURFACE) & 3-2 (SEVERAL LOCATION AT UPPER & LOWER SURFACE), SLAT #3, LH WING.
- [SDR VNAA2022062699916](https://openairdocs.org/sdr/VNAA2022062699916.md): Slat Track · corroded · May 9, 2022 · N528EG · Cndair CL6002C10 · Leading Edge Devices
  > PITTING CORROSION ON SLAT TRACKS 2-1, 2-2, & 2-3 (SEVERAL LOCATION AT UPPER & LOWER SURFACE), SLAT #2, LH WING.
- [SDR VNAA2022062699915](https://openairdocs.org/sdr/VNAA2022062699915.md): Slat Track · corroded · May 9, 2022 · N528EG · Cndair CL6002C10 · Leading Edge Devices
  > PITTING CORROSION ON SLAT TRACKS 1-1, 1-2, & 1-3 (SEVERAL LOCATION AT UPPER & LOWER SURFACE), SLAT #1, LH WING.
- [SDR VNAA2022062699914](https://openairdocs.org/sdr/VNAA2022062699914.md): Stringer · corroded · May 9, 2022 · N528EG · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > CORROSION ON STGR 21RH BTW FS STA: 349 AND FS STA: 333 AT MAIN AVIONICS COMPARTMENT. (E/E)
- [SDR VNAA202206269997](https://openairdocs.org/sdr/VNAA202206269997.md): Strap · corroded · May 8, 2022 · N528EG · Cndair CL6002C10 · Fuselage, Wing Attach Fittings
  > CORROSION ON SETTLEMENT AREA LOWER SECTION OF WING-TO-FUSELAGE FAIRING AT FS STA 909.00.

Next page: https://openairdocs.org/aircraft/N528EG/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 = 'N528EG' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N528EG/reports

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