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Beech Starship History Continued...

In the final test a fuselage section dropped at 17 ft/s incurred no damage, and the anthropomorphic dummies inside sustained a spinal load of only 1000 pounds.

Sled testing, to 269 for crew seats and 219 for passenger seats, has been done in keeping with the recently-established standards of the General Aviation Safety Panel.  

One of the greatest challenges to building and certifying an all-composite airframe is lightning protection. Unprotected composite material can be blown apart by a lightning strike. This occurs because graphite epoxy is 1000 times more resistant to current flow than aluminum, and the high resistance converts the current flow to heat.

Lightning protection was the subject of intensive study and testing; for instance a fuselage section absorbing a 200 000 amp simulated lightning strike generated in our test facility. Only 1 in 200 lightning strikes is likely to contain that much current. By comparison, normal US house current is only 20 amps.

We had to be able to demonstrate compliance with the Federal Aviation regulations concerning protection of structure and fuel systems, as do all metal aircraft, but we also had to show that Starship could sustain a lightning strike without damage to avionics or other electrical components.

This was accomplished by using a combination of fine wires in the first layer of composite skin and a ground-plane system to shield the electronics, allowing the lightning current to flow through and out, leaving only minor surface and cosmetic damage at the strike point.

There is an old saying that lightning will never strike the same place twice, but the FAA does not believe it for they were concerned about the ability to repair lightning strike damage in a way that would continue to offer lightning protection. To prove this, wires or thin aluminum sheets were added at the time of repair.

Struck lucky

During the course of final certification testing the number two prototype, NC-2, sustained lightning strike. The lightning attached itself to a test pod mounted on the aircraft, one being recorded on videotape at the time.  In  a  remarkable piece of footage the strike was filmed from inside the aircraft, showing the lightning striking the front of the pod and exiting from the Starship's tip-sail and rudder. The aircraft was unscathed.

The avionics system was developed specifically by Rockwell Collins Avionics, and consists of a 16 tube EFIS panel (Electronic Flight Information System). Basically, these are TV tubes that display information on the lines of a conventional T; the method is also known as the glass cockpit.

The primary flight display shows aircraft attitude, as well as the flight director commands, lateral deviation, glide slope, radio altitude and marker beacon. The pilot can select display of flight guidance modes, autopilot status, airspeed deviation, decision height alert, altitude alert, ILS deviation alert and minimum descent altitude alert as desired. Our philosophy is to provide the pilot with as much or as little information as desired to accomplish the job.

The airspeed indicator provides the classical dial readout, as well as outside air temperature and true air speed; it also has a trend feature which will predict the aircraft's speed in ten seconds at the current rate of acceleration or deceleration.

Over on the right of the T we have a unique instrument that combines the altimeter and vertical speed indicator functions, as well as an altitude alert. It displays barometric altitude, pre-selected altitude, barometric setting, and a flight-level one-eight-zero alert.

During an instrument approach, either crew member can set radio altitude decision height on their respective altitude awareness panels and the readout will appear on the primary flight display. Decision height and radio altitude display appear automatically on the screen when the radio altitude passes through 2500 ft descending.

Another key element of the T-display is navigation information, where the display shows the aircraft's horizontal navigation situation in a familiar manner, with heading,  selected  heading,  selected  navigation source, selected course and lateral deviation.

The primary navigation function can be displayed in any of three modes -- the Horizontal Situation Indicator (HSI) mode shows the full compass rose traditionally displayed on conventional EFIS and electromechanical displays; the are mode displays a 70" section of the compass, for a closer look at a developing situation; and the map mode adds a graphic representation of waypoints to the are display.

Starship's radar display can be superimposed on the are or map modes to assist in circumventing weather or turbulence. The radar itself is a Collins TWR-850 unit which uses Doppler technology to help predict where turbulence might exist.

Avionics enhance safety

Flight experience in the Starship prototypes has shown that the unit is capable of accurately detecting and displaying turbulence, sometimes in areas where conventional radar sets showed only light rain. The avionics display offers a conventional presentation, but one that is also enhanced with capabilities not previously available to the general aviation pilot. The design driver is function, with developed features that reduce workload and provide real-world information to increase the ease and safety of flight.

Engine instrumentation is also generated on video tubes, in a display called EICAS  (Engine Indication and Crew Alerting System). The engine instruments are presented in a traditional turbine display, but the pointers on Starship's EICAS change color from green to yellow or red to alert the crew to any abnormal condition.

Generally the philosophy in EICAS has been that simpler is better, and the system is designed to produce minimal or, in many cases, no display when the aircraft is operating normally. When an abnormal condition begins to occur, one of eighty color-coded caution, status and advisory annunciations light to alert the pilot. The system also records and stores the data, including the time and date it occurred.  

 

 

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