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Propeller strike during start-up, Fokker F27... - Onderzoeksraad voor ...

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1.8 Aids to navigation<br />

Not applicable.<br />

1.9 Communication<br />

Communication between ground crew and flightcrew is possible through an interphone system.<br />

Microphone and headset jacks for the groundcrew are located near the external power<br />

receptacle directly below the first officer’s sliding window. The microphones and headsets are<br />

used from the moment the crew is ready to <strong>start</strong> the engines. At this time the microphone<br />

selector switch is selected in the cockpit to open intercom so the flightcrew microphones are hot.<br />

As a result the mechanic will hear everything that is said on the flightdeck. The mechanic has to<br />

push a transmit button on his microphone to be heard by the flightcrew.<br />

The <strong>Fokker</strong> 50 has two independent very high frequency (VHF) radios. When only the aircraft<br />

batteries are powering the electrical system (for example when both engines are shutdown<br />

without the auxiliary power unit (APU) operating or external power being connected), only one<br />

VHF radio is available. In this situation the aircraft interphone system is also unavailable.<br />

1.10 Airport information<br />

The aircraft was parked at position B86 facing South West at Amsterdam Airport Schiphol Bapron;<br />

the heading was approximately 240º.<br />

The immediate area surrounding the aircraft was dry and free from fuel and oil spills (see<br />

appendix A).<br />

1.11 Flight recorders<br />

1.11.1 Cockpit voice recorder<br />

The CVR was used for this investigation. Four channels are available, but only three are used<br />

on the KLC <strong>Fokker</strong> 50 aircraft. The audio signals of the captain’s and first officer’s audio selector<br />

panels are recorded on separate channels and one channel records the audio signal picked <strong>up</strong><br />

by the area microphone. The recording was of good quality and lasted for approximately six<br />

minutes after engine shut down. All conversations between captain, first officer and mechanic<br />

were clearly audible.<br />

Several distinctive sounds could be heard on the CVR. When the mechanic plugged in his<br />

headset a characteristic click was heard on the first officer’s audio channel. The same click was<br />

heard when he disconnected his headset and a few seconds later the area microphone channel<br />

recorded an unusual “ffrrrt” sound. It is assumed that this was the sound of the mechanic coming<br />

into contact with the propeller.<br />

The time interval between the click when the mechanic disconnected his headset and the sound<br />

of him coming in contact with the propeller was between three to four seconds.<br />

The time between the mechanic coming in contact with the propeller and the activation of the<br />

engine shut down was about seventeen seconds.<br />

50

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