FAA Proposes CF34 Engine Inspections Following Fatal Challenger Crash

The FAA proposed new inspections for CF34 engines after a fatal 2024 Challenger crash linked to corrosion-related thrust loss.

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Key Takeaways:

  • The FAA has proposed new inspections and operational checks for General Electric CF34-series engines following a 2024 fatal business jet accident.
  • The proposal addresses concerns about undetected corrosion in the engine's variable geometry (VG) system, which was linked to a near-simultaneous loss of thrust in a Bombardier Challenger 604 crash.
  • The new requirements, affecting over 1,100 engines on Bombardier Challenger 600 series and CRJ200 aircraft, include borescope inspections, VG system functional checks, and recurring restart tests.
  • Compliance periods vary by engine model and configuration, with some engines requiring immediate inspection and others having up to two years, potentially including quarterly restart tests.
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The Federal Aviation Administration (FAA) issued a notice of proposed rulemaking (NPRM) that would require new inspections and operational checks for General Electric CF34-series engines, following a 2024 fatal business jet accident that raised concerns about undetected corrosion.

Published May 1, the proposal would affect more than 1,100 engines installed on Bombardier Challenger 600 series aircraft and Bombardier CRJ200 airliners. The NPRM outlines a combination of borescope inspections, variable geometry (VG) system functional checks, and, for some engines, recurring restart tests—measures that vary by engine model and configuration.

While the FAA does not directly cite a specific accident, the action is widely tied to the February 2024 crash of a Bombardier Challenger 604 operated by Hop-A-Jet. The aircraft experienced a near-simultaneous loss of thrust in both engines on approach, resulting in two fatalities.

Investigators found that corrosion within the engines’ VG system components can restrict movement, causing them to fall out of schedule and increasing the risk of compressor instability and thrust loss. The National Transportation Safety Board (NTSB) concluded that corrosion in both engines led to compressor stalls and a total loss of thrust. The investigation also cited insufficient maintenance guidance for detecting corrosion during prior troubleshooting.

Under the proposed directive, certain engines would require inspection before further flight, while others would be subject to phased compliance periods of up to two years. Some configurations would also mandate restart testing at regular intervals, potentially as often as every three months. If discrepancies are found, required actions could include additional maintenance or engine removal.

The FAA estimates the proposal would impact approximately 1,152 U.S.-registered engines. Public comments are open through mid-June 2026, after which the agency will consider final rulemaking.

Amelia Walsh

Amelia Walsh is a private pilot who enjoys flying her family’s Columbia 350. She is based in Colorado and loves all things outdoors including skiing, hiking, and camping.
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