# Service difficulty reports: N542EA

A list on [N542EA](https://openairdocs.org/aircraft/N542EA.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 2 · 91 reports

- [SDR VNAA20260328005](https://openairdocs.org/sdr/VNAA20260328005.md): Hinge · corroded · Mar 9, 2026 · N542EA · Bombdr CL6002D15 · Fuselage, Door Hinge
  > CORROSION ON FWD/ MIDDLE/ AFT HINGE OF FLAP STEP PLATE AT AFT BAGGAGE BAY DOOR CUTOUT. CORROSION ON MIDDLE HINGE OF FLAP STEP PLATE AT AFT BAGGAGE BAY DOOR CUTOUT WAS REMOVED PER CRJ-700 SRM 51-21-06-001-001-A01 AND EVAUATED WITHIN LIMITS PER CRJ-700 SRM 53-
- [SDR VNAA20260328004](https://openairdocs.org/sdr/VNAA20260328004.md): Drag Angle · cracked · Feb 10, 2026 · N542EA · Bombdr CL6002D15 · Vertical Stabilizer Miscellaneous Structure
  > DURING INSPECTION OF THE TASK CARD 300-07-JIC IT WAS DETECTED CRACK ON RIGHT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.62% STGR DATUM TO STGR DATUM TO 67.5% REAR SPAR DATUM WAS FOUND. AFT DRAG ANGLE BTW 55.62% STGR DATUM TO STGR DATUM T
- [SDR VNAA20260328003](https://openairdocs.org/sdr/VNAA20260328003.md): Floor Support · cracked · Feb 10, 2026 · N542EA · Bombdr CL6002D15 · Fuselage Miscellaneous Structure
  > CRACK ON FLOOR SUPPORT RBL 12.0 BTW FS 221.73 TO FS 229.00 AT FWD FUSELAGE INTERNAL STRUCTURE (FLIGHT COMPARTMENT FLOOR STRUCTURE BELOW WL 79.50). CRACK ON FLOOR SUPPORT RBL 12.0 BTW FS 221.73 TO FS 229.00 AT FWD FUSELAGE INTERNAL STRUCTURE (FLIGHT COMPARTMEN
- [SDR VNAA20260328010](https://openairdocs.org/sdr/VNAA20260328010.md): Seat Track · corroded · Feb 8, 2026 · N542EA · Bombdr CL6002D15 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION SIDE SEAT RAIL RETAINERS, LH SIDE ON FS708 AND RH SIDE FROM FS785 TO FS797 AT PAX CABIN. CORROSION ON SIDE SEAT RAIL RETAINERS, LH SIDE ON FS708 AND RH SIDE FROM FS785 TO FS797 (PAX CABIN) WAS REMOVED PER CRJ-700 SRM 51-21-06-001-001-A01 AND REWORKE
- [SDR VNAA20260328009](https://openairdocs.org/sdr/VNAA20260328009.md): Seat Track · corroded · Feb 8, 2026 · N542EA · Bombdr CL6002D15 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON LH SIDE SEAT RAILS; (2 SECTIONS) FROM FS379 TO FS573, (3 SECTIONS) FROM FS661 TO FS761 AND (2 SECTIONS) FROM FS785 TO FS953 AT PAX CABIN. CORROSION ON LH SIDE SEAT RAILS; (2 SECTIONS) FROM FS379 TO FS573, (3 SECTIONS) FROM FS661 TO FS761 AND (2
- [SDR VNAA20260328007](https://openairdocs.org/sdr/VNAA20260328007.md): Hinge Fitting · corroded · Feb 8, 2026 · N542EA · Bombdr CL6002D15 · Ailerons
  > CORROSION IN THE INNER AREA OF THE BORE LUGS AT AILERON FITTING 1, CENTRAL FITTING (L1, L2, L3, L4, L5, L6) AND FITTING 4 (UPPER AND LOWER) OF LH WING AILERON. BORE LUGS HINGE FITTING NO. 1 & 4 (LOWER), CENTER HINGE FITTING BORE LUGS L1, L3, L4, L6 WERE CLEA
- [SDR VNAA20260328006](https://openairdocs.org/sdr/VNAA20260328006.md): Fitting · corroded · Feb 8, 2026 · N542EA · Bombdr CL6002D15 · Fuselage Miscellaneous Structure
  > WORKSHOP INTERIOR SHEET METAL: CORROSION FLOOR FITTING IN FRONT ACCESS 107 (1EA) ON GALLEY 1. FLOOR FITTING IN FRONT ACCESS 107 (1EA) ON GALLEY 1 WAS REPLACED PER SAFRAN CMM 25-33-44
- [SDR VNAA2025090211101](https://openairdocs.org/sdr/VNAA2025090211101.md): Transceiver · fluctuates · Aug 29, 2025 · N542EA · Cndair CL6002C10 · Ground Proximity System
  > IN-FLIGHT AT FL20.0 WE EXPERIENCED THE RA START TO MAKE 25.00FT, 500FT, 100FT CALL OUTS AND FLUCTUATE. / REMOVED AND REPLACED RAD ALT #1 IAW CR7 AMM 34-44-01-000/400-801-A02-PSA. BIT CHECKS GOOD.
- [SDR VNAA2025073111102](https://openairdocs.org/sdr/VNAA2025073111102.md): Hose · chafed · Jul 26, 2025 · N542EA · Cndair CL6002C10 · Hydraulic System, Main
  > HYD SYSTEM 2 LOW PRESSURE CAUTION MESSAGE IN FLIGHT WITH 0% QUANTITY. FOUND HYD 2 DAMPENER FLEX HOSE TO BE CHAFED THROUGH BY ADEL CLAMP. REMOVED AND REPLACED HOSE AND CLAMP IAW AMM 29-11-59-000/400-801. OPS CHECK/LEAK CHECK GOOD.
- [SDR VNAA2025032411101](https://openairdocs.org/sdr/VNAA2025032411101.md): Steering Sys · malfunctioned · Mar 21, 2025 · N542EA · Cndair CL6002C10 · Landing Gear Steering System
  > STEERING INOP AFTER TAKEOFF. / PERFORMED OPS CHECK OF THE NOSEWHEEL STEERING IAW CRJ700 AMM 32-51-00-710-801. OPS CHECK GOOD AT THIS TIME. NO DEFECTS NOTED.
- [SDR VNAA2025021211101](https://openairdocs.org/sdr/VNAA2025021211101.md): Skin · dented · Feb 10, 2025 · N542EA · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > DENT ON LH FUSELAGE AFT OF AFT NLG DOOR. / REPAIRED LH FUSELAGE BETWEEN FS250.00- FS265.00 STR24L-STR23L IAW REO 670-53-11-2096 AND CRJ700 SRM REF 51-42-21.
- [SDR VNAA2024110511102](https://openairdocs.org/sdr/VNAA2024110511102.md): Unknown · odor · Nov 1, 2024 · N542EA · Cndair CL6002C10 · Air Distribution System
  > SMOKE CONDITION IN CABIN, CONDITION IMPROVED WHEN PACKS SHUT OFF. / INSPECTED AIRCRAFT IAW CRJ700 FIM 21ˆ’21/22ˆ’00ˆ’810ˆ’806-A01 AND FOUND B1 CODE 211943--RH PACK AUTOFAILED CAUTION MSG DISPLAYED. ISOLATED ISSUE TO THE RH PACK, VENTIALATED AIRCRAFT CABIN
- [SDR VNAA202209249992](https://openairdocs.org/sdr/VNAA202209249992.md): Floorbeam · corroded · Sep 14, 2022 · N542EA · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > CORROSION ON UPPER FACE OF FLOOR BEAM LBL 9 BTW FS 1000.00 TO FS 1069.00 ON AFT CARGO COMPARTMENT FLOOR STRUCTURE.
- [SDR VNAA2022092499910](https://openairdocs.org/sdr/VNAA2022092499910.md): Stringer · corroded · Sep 13, 2022 · N542EA · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > CORROSION ON STRINGER 27 BTW FS 349.00 TO FS 353.00 OF MAIN AVIONICS COMPARTMENT INTERNAL STRUCTURE.
- [SDR VNAA202209249999](https://openairdocs.org/sdr/VNAA202209249999.md): Stringer Splice · corroded · Sep 11, 2022 · N542EA · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > CORROSION WAS FOUND ON STRINGER SPLICE FS 333.00 ON STRINGER 23RH AT MAIN AVIONICS COMPARTMENT INTERNAL STRUCTURE.
- [SDR VNAA202209249991](https://openairdocs.org/sdr/VNAA202209249991.md): Stringer Clip · cracked · Sep 11, 2022 · N542EA · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > CRACK ON STRINGER ATTACHED ANGLE ON STGR 7LH FS1051.30 ON AFT BAGGAGE BAY DOOR SURROUND STRUCTURE.
- [SDR VNAA202209229997](https://openairdocs.org/sdr/VNAA202209229997.md): Stringer · corroded · Sep 11, 2022 · N542EA · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > CORROSION ON STRINGER 24RH BTW FS 333.00 TO FS 364.00 OF MAIN AVIONICS COMPARTMENT INTERNAL STRUCTURE
- [SDR VNAA202209249993](https://openairdocs.org/sdr/VNAA202209249993.md): Frame · corroded · Sep 5, 2022 · N542EA · Cndair CL6002C10 · Fuselage Main, Frame
  > CORROSION ON FRAME AT STGR 26LH & FS1031.00 AT AFT BAGGAGE BAY.
- [SDR VNAA202209229995](https://openairdocs.org/sdr/VNAA202209229995.md): Strip · corroded · Sep 4, 2022 · N542EA · Cndair CL6002C10 · Aerodynamic Fairings
  > CORROSION ON METALIC STRIP (1EA) AT FORWARD UNDERWING FAIRNG 193AB.
- [SDR VNAA2022092499911](https://openairdocs.org/sdr/VNAA2022092499911.md): Seat Track · corroded · Aug 23, 2022 · N542EA · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION AT SEAT RAIL OF STRINGER 15LH BETWEEN FS863 - FS969
- [SDR VNAA202209249994](https://openairdocs.org/sdr/VNAA202209249994.md): Seat Track · corroded · Aug 23, 2022 · N542EA · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION AT SEAT RAIL OF STRINGER 15LH BETWEEN FS 581 - FS 661
- [SDR VNAA202209229994](https://openairdocs.org/sdr/VNAA202209229994.md): Seat Track · corroded · Aug 23, 2022 · N542EA · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION AT SEAT RAIL OF STRINGER 15LH BETWEEN FS708+5 - FS 761.00
- [SDR VNAA202209249997](https://openairdocs.org/sdr/VNAA202209249997.md): Seat Track · corroded · Aug 15, 2022 · N542EA · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION AT SEAT RAIL OF RBL9 BETWEEN FS581.40 - FS677.0
- [SDR VNAA202209249996](https://openairdocs.org/sdr/VNAA202209249996.md): Seat Track · corroded · Aug 15, 2022 · N542EA · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION AT SEAT RAIL OF RBL9 BETWEEN FS485.0 - FS581.0
- [SDR VNAA202209249995](https://openairdocs.org/sdr/VNAA202209249995.md): Seat Track · corroded · Aug 15, 2022 · N542EA · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION AT SEAT RAIL OF RBL9 BETWEEN FS349.0 - FS485.
- [SDR VNAA202210119993](https://openairdocs.org/sdr/VNAA202210119993.md): None · gouged · Aug 14, 2022 · N542EA · Bombdr BD1001A10 · Fuselage Structure (General)
  > SCRIBE LINES WERE FOUND ON LONGERON ATTACHMENT BTW FS 696.00 TO FS 801 AT STGR 17LH
- [SDR VNAA202210119992](https://openairdocs.org/sdr/VNAA202210119992.md): None · gouged · Aug 14, 2022 · N542EA · Bombdr BD1001A10 · Fuselage Structure (General)
  > SCRIBE LINES WERE FOUND ON LONGERON ATTACHMENT BTW FS 696.00 TO FS 801 AT STGR 17RH
- [SDR VNAA202210119991](https://openairdocs.org/sdr/VNAA202210119991.md): None · corroded · Aug 14, 2022 · N542EA · Bombdr BD1001A10 · Standard Practices/Structures
  > CORROSION ON WHEEL BINS ATTACHMENT ANGLES (2 EA) BTW FS 797.00 TO FS 830.40 RBL 16 AND LBL 49 ON MAIN WHEEL WELL
- [SDR VNAA2022092499912](https://openairdocs.org/sdr/VNAA2022092499912.md): Intercostal · corroded · Aug 14, 2022 · N542EA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > CORROSION WAS FOUND ON INTERCOSTAL AT STRINGER 20R, BTW FS 310.00 AND FS 319.70 ON MAIN AVIONICS COMPARTMENT
- [SDR VNAA202209249998](https://openairdocs.org/sdr/VNAA202209249998.md): None · corroded · Aug 14, 2022 · N542EA · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > CORROSION WAS FOUND ON MID CAP ANGLE ON STGR 18LH BTW FS 310.00 TO FS 349.00
- [SDR VNAA202209229993](https://openairdocs.org/sdr/VNAA202209229993.md): Seat Track · corroded · Aug 14, 2022 · N542EA · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION AT SEAT RAIL BETWEEN FS847+5 - FS967 ON STRINGER 15RH
- [SDR VNAA202209229992](https://openairdocs.org/sdr/VNAA202209229992.md): Seat Track · corroded · Aug 14, 2022 · N542EA · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION AT SEAT RAIL BETWEEN FS785+4 - FS847+15 ON STRINGER 15RH
- [SDR VNAA202209229991](https://openairdocs.org/sdr/VNAA202209229991.md): Seat Track · corroded · Aug 14, 2022 · N542EA · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION AT SEAT RAIL BETWEEN FS708+4 - FS761 ON STRINGER 15RH
- [SDR VNAA202209209991](https://openairdocs.org/sdr/VNAA202209209991.md): Floorbeam · corroded · Aug 14, 2022 · N542EA · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > CORROSION ON UPPER FACE OF FLOOR BEAM LBL 27 BTW FS 1000.00 TO FS 1047.00 ON AFT CARGO COMPARTMENT FLOOR STRUCTURE.
- [SDR VNAA202209229998](https://openairdocs.org/sdr/VNAA202209229998.md): Stringer · corroded · Aug 12, 2022 · N542EA · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > CORROSION ON STRINGER 22RH BTW FS 333.00 TO FS 349.00 ON MAIN AVIONICS COMPARTMENT INTERNAL STRUCTURE
- [SDR VNAA202209229996](https://openairdocs.org/sdr/VNAA202209229996.md): None · cracked · Aug 12, 2022 · N542EA · Cndair CL6002C10 · Fuel Servicing
  > CRACK ON AFT BACKING OF REFUEL DUCT SUPPORT STRUCTURE ON FS 679.00, BTW STGR 22RH AND 21RH.
- [SDR VNAA202210119994](https://openairdocs.org/sdr/VNAA202210119994.md): None · cracked · Aug 2, 2022 · N542EA · Bombdr BD1001A10 · Standard Practices/Structures
  > CRACKS ON LOWER PRESSURE SEAL RETAINER BOTH CORNERS AT FWD BAGGAGE BAY DOOR
- [SDR VNAA202201071111](https://openairdocs.org/sdr/VNAA202201071111.md): Gust Lock · false indication · Jan 5, 2022 · N542EA · Cndair CL6002C10 · Gust Lock Damper System
  > AS PILOT FYING ON SHORT FNAL INTO RWY 16 AT HPN (<500'AGL), GOT A GLD RELATED MASTER CAUTION MSG. DUE TO THE SHORT RUNWAY AND DOWNHILL SLOPE, I COMMENCED A GO-AROUND. MESSAGE EXTINGUISHED DURING THE CLIMB OUT BEFORE I COULD ASCERTAIN THE EXACT MESSAGE. GOT DEL
- [SDR VNAA2020080511101](https://openairdocs.org/sdr/VNAA2020080511101.md): Unknown · odor · Aug 3, 2020 · N542EA · Cndair CL6002C10 · Air Distribution System
  > STRONG BURNING ODOR IN AFT ROWS WHEN AC POWER APPLIED - INSPECTED AFT EQUIP. BAY, AND CAB LIGHTING, CYCLED AC POWER FROM CAT AND APU, AND CYC RH PACK NO DEFECTS NOTED SMELL NOT PRESENT. GVI NO DEFECTS NOTED
- [SDR VNAA2020062211101](https://openairdocs.org/sdr/VNAA2020062211101.md): Pump · failed · Jun 21, 2020 · N542EA · Cndair CL6002C10 · Hydraulic Pump (Electric/Engine), Main
  > HYDRAULICS SYSTEM FAILURE. FLIGHT CREW RAN THE QRH, AND DECLARED AN EMERGENCY. HYD PUMP 3A LOW PRESSURE CAUTION IN FLIGHT. REMOVED AND REPLACED NR 3A HYD ACMP. SERVICED 3A HYD SYS TO 55% AT 49 DEGREES C. PERFORMED OPERATIONAL AND LEAK CHECK. NO LEAKS AT T
- [SDR SIMA202002065009](https://openairdocs.org/sdr/SIMA202002065009.md): Skin · damaged · Feb 5, 2020 · N542EA · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > EXT. FUSELAGE SKIN HAS AREA OF DAMAGE BETWEEN FS 969.00 AND 985.00 AT STR 27.-C/A-C/W REPAIR IAW ERS-CR-53MR-4025
- [SDR SIMA202001287001](https://openairdocs.org/sdr/SIMA202001287001.md): Angle · cracked · Jan 27, 2020 · N542EA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > "L" ANGLE AT BL 26.0 ON RH SIDE IS CRACKED ON LOWER END. -C/A-FOUND STANCHION TO BE CRACKED BEHIND THE RH BULKHEAD. REMOVED AND REPLACED STANCHION BEHIND THE RH BULKHEAD IAW SRM 5-42-12. CHECK NRWC E767449 FOR INSTALLATION OF NEW "L" ANGLE.
- [SDR SIMA202001295006](https://openairdocs.org/sdr/SIMA202001295006.md): Bulkhead · corroded · Jan 25, 2020 · N542EA · Cndair CL6002C10 · Fuselage Main, Bulkhead
  > RH BULKHEAD WALL AT FS 280.00 HAS NUMEROUS AREAS OF CORROSION AT FLOOR LEVEL-C/A-COMPLETED RH BULKHEAD LOWER WEB REPAIR @ FS280.00 IAW SRM 53-11-10-201-004.
- [SDR SIMA202002034003](https://openairdocs.org/sdr/SIMA202002034003.md): Floorbeam · corroded · Jan 24, 2020 · N542EA · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > RH FLOOR BEAM AT FS280.00 IS CORRODED IN NUMEROUS SPOTS, WHERE IT IS SANDWICHED BETWEEN DRIP TRAY AND L ANGLE OF THE BULKHEAD. -C/A-REMOVED AND REPLACED RH FLOOR BEAM AT FS280.00 IAW SRM 51-42-06 AND SRM 51-42-13.
- [SDR SIMA20200203004](https://openairdocs.org/sdr/SIMA20200203004.md): Floorbeam · corroded · Jan 23, 2020 · N542EA · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > LH FLOOR BEAM AT FS280.00 IS CORRODED IN NUMEROUS SPOTS, WHERE IT IS SANDWICHED BETWEEN DRIP TRAY AND L ANGLE OF THE BULKHEAD. -C/A-RAR'D LH FLOOR BEAM AT FS2800.00 IAW SRM 51-42-06 AND 51-42-13
- [SDR SIMA202001273002](https://openairdocs.org/sdr/SIMA202001273002.md): Support Angle · cracked · Jan 23, 2020 · N542EA · Cndair CL6002C10 · Passenger/Crew Doors
  > PASSENGER DOOR AFT SIDE HAS A CRACKED STEP SUPPORT ANGLE NEXT TO THE HANDRAIL BRACKET. THIS WAS A PREVIOUS REPAIR. -C/A-REPAIRED PASSENGER DOOR AFT SIDE STEP ANGLE SUPPORT IAW 52-11-04-201-004-A01.
- [SDR SIMA2020020412008](https://openairdocs.org/sdr/SIMA2020020412008.md): Drag Angle · cracked · Jan 20, 2020 · N542EA · Cndair CL6002C10 · Passenger/Crew Doors
  > PASSENGER DOOR AFT DRAG ANGLE IS CRACKED AT PREVIOUS REPAIR.-C/A-REPAIRED PASSENGER DOOR AFT DRAG ANGLE IAW SRM 52-11-04.
- [SDR SIMA20200203007](https://openairdocs.org/sdr/SIMA20200203007.md): Skin · cracked · Jan 20, 2020 · N542EA · Cndair CL6002C10 · Passenger/Crew Doors
  > PASSENGER DOOR AFT SIDE SKIN HAS A CRACKED STEP SUPPORT ANGLE NEXT TO THE HANDRAIL BRACKET. THIS WAS A PREVIOUS REPAIR.-C/A-REPAIRED PASSENGER DOOR AFT SIDE STEP ANGLE SUPPORT IAW SRM 52-11-04-201-004-A01.
- [SDR SIMA2020020517014](https://openairdocs.org/sdr/SIMA2020020517014.md): Floorbeam · cracked · Jan 17, 2020 · N542EA · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > RH CENTER FLOOR BEAM AT BL12.00 IS CRACKED, LOCATED JUST FWD OF FLOOR BEAM AT FS 280.00. -C/A- REPAIRED RH CENTER COCKPIT FLOOR BEAM AT BL 12.00 IAW SRM 53-11-43.
- [SDR SIMA2020020517015](https://openairdocs.org/sdr/SIMA2020020517015.md): Floorbeam · cracked · Jan 17, 2020 · N542EA · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > LH CENTER FLOOR BEAM AT BL12.00 IS CRACKED, LOCATED JUST FWD OF FLOOR BEAM AT FS 280.00. -C/A- REPAIRED LH CENTER COCKPIT FLOOR BEAM AT BL 12.00 IAW SRM 53-11-43.

Next page: https://openairdocs.org/aircraft/N542EA/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 = 'N542EA' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N542EA/reports

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