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Flight Safety Crest Epilogue
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Aircraft Accident Summary
Incident photo
Type: Hornet CF188933

Date: 13 January 2005

Location: Tinker AFB, Oklahoma,USA

The Pilot in Command (PIC) and second pilot were enroute from Cold Lake, Alberta, to Naval Air Station Key West, Florida as part of an exercise deployment. An enroute fuel stop was planned at Tinker Air Force Base (AFB), Oklahoma. Approximately 100 Nautical Miles (NM) from Tinker and at an altitude of 39,000 feet, the crew experienced indications of right engine oil pressure fluctuations. The checklist items were actioned and the right engine was shut down. The crew declared an emergency and began their descent.

The crew planned for an arrested landing via a visual straight in approach to runway 12. Within 2 NM of touchdown and unable to visually identify the Bak 12 arrestor cable on the runway, the PIC decided to land at the runway threshold. Just prior to touchdown, the aircraft's arrestor hook caught the E-5 arrestor gear in the undershoot area of runway 12, 70' before the threshold. The aircraft's main landing gear then touched down prior to the runway threshold. After encountering difficulty with directional control, the PIC used emergency braking to bring the aircraft to a halt on runway 12, 7500' from the threshold. After conducting a normal shutdown, both pilots egressed uninjured. The aircraft sustained "D" category damage; the E-5 arrestor cable and runway also sustained damage.

The Flight Safety Investigation revealed that the CF-18 crew were unaware that the tail-hook touchdown point can be over 500 feet prior to the intended aim-point (depending on variables such as glide path angle, and angle of attack). Recommendations include amending manuals to ensure aircrew are aware of the difference in touchdown points.

The engine oil pressure fluctuations were caused by a faulty connector which had failed due to a cracked oil pressure transmitter bracket. False oil pressure indications have resulted in approximately 15 single-engine landings over the past five years. Recommendations include a re-design of the transmitter bracket, and modifications to the inspection procedures.

 


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   Date modified: 2006-05-11
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