Please Support X-Plane.org by Clicking the Advertisement Below


 

CarterCopter Next CC

NxCC

for X-Plane 6.51

© Mark Fisher, 2003 ~ mf70@hotmail.com

Note: A Pilot’s Operating Handbook (POH) is a primer on the operation of a specific aircraft. This POH is intended as a primer on the operation of the X-Plane model of the CarterCopter Next CC (NxCC). It is designed to run under the flight simulator X-Plane, with a full-featured free demo available from www.x-plane.com. This X-Plane model is freeware; it may be freely modified, copied, and redistributed, provided a) it is not part of any for-profit package other than X-Plane itself, and b) credit for this design is given to Mark Fisher and Austin Meyer.

Thanks to the test pilots: Otha Vaughn, Kevin Smith, Joe Churchman, and Doug Marker. And you! If you have any questions or suggestions about this model please contact me at the above e-mail address.
This model: For a number of reasons, this model is not an exact replica of the real NxCC. "Flying" techniques discussed here should not be taken as a full and direct description of skills needed in the real NxCC.


Overview:

The CarterCopter is a hybrid aircraft. It operates in three modes: At all times, "steer small." Work to find the smallest input that will have the desired effect. Over-control only masks the response of the aircraft.

As a general rule DON'T let forward speed drop below about 70 knots (certainly keep above 50-60) unless you are coming in for a zero roll landing or at high altitude and experimenting.

Unique Controls:

There is an unfamiliar control on the throttle quadrant – the "Rotor Trim" lever. This does not directly control the rotor. Instead it controls the link between the elevator trim and the rotor pitch cyclic. In the "up" position, the rotor mirrors the pitch trim, allowing pitch trim before the elevator is effective. In the "down" position, the rotor pitch cyclic is not affected by elevator trim.

There is also a "collective" control. This controls the pitch of the rotor blades. This is used as a lift control in helicopter mode, and as a rotor rpm control in autogiro and fixed wing modes.

A final addition in the NxCC is the customized Electronic Flight Instrumentation System (EFIS). This generates several cheery warnings. FLAPPING WARNING and FLAPPING CRITICAL warn of excessive rotor lift – reduce rotor pitch.

X-Plane key commands:

Almost all control functions are available from within the cockpit by clicking on the appropriate part of the screen. You may use "Special | Show mouse control areas" to highlight the "hot" areas of the screen. Some general controls - viewpoint especially, are accessed either from the menu structure or from the keyboard. Some vital views: "W" = forward view, "Q" = look left, "E" = look right, "A" = following view, <Shift-"\"> = outside view. Other useful keys: "G" = landing gear toggle, "B" = brake toggle. Other needed keys will be indicated as they are needed in carets - "<>".

Running Take-Offs

Principles:

The NxCC will be acting as an autogiro. At takeoff, the NxCC has two sources of energy: the thrust of the engine-prop unit, and lift from the inertia-rotor unit.
The first step is to store sufficient takeoff energy in the rotor system. This is done via the "Pre-Rotate" buttons.

Procedure:

Set altimeter. <Enter, select ATIS report>
Engage fourth button down (ROT) on EFIS.<Mouse>
Set radios.<Mouse>
Collective at 0° (White area) <F5 - F6>.
Set autopilot to planned cruise altitude.<Mouse>
Pitch trim at bottom – nose up trim. < [ - ] >
Set VVI to desired vertical speed (500).
Throttle at idle <F1>.
Rotor trim at top.<Mouse>
Flaps to first notch (5°) (Not installed on real NxCC)

Jump Take-Offs (zero roll take-off)

Principles:

The NxCC will be acting as a helicopter for the first 100 vertical feet of flight, and then transition to autogiro mode at 100 Ft. AGL, where it will accelerate to slow flight speed of 70 knots.

The period of time between takeoff and the establishment of flight speed is quite short. The entire period should be treated as a takeoff – if there is any delay in establishing flight, the aircraft should be landed again immediately.

Procedure:

Climb Out to Low Speed Cruise

Principles:

The NxCC will be operating as a conventional autogiro. The rotor will be tipped back around 5°, and will be supporting over half the weight. Rotor rpm will be around 220 rpm. (More rpm = greater drag and less forward speed and greater engine power is needed – the goal here is to minimize fuel consumption and avoid using excessive engine power.) Too little collective and the rotor rpm will go over 300 and this needs more power from the engine to keep up airspeed.

Don't let speed drop below about 70 knots (certainly keep above 50-60 as it can be difficult to regain speed ESPECIALLY if flying at a low altitude).

You may see a FLAPPING WARNING. If so, "steer small," and reduce collective pitch gently.

Procedure:

High Speed Cruise

Principles:

The NxCC will be operating primarily as a fixed wing aircraft. As the aircraft is trimmed forward to balance increasing wing lift, the rotor will be almost completely aligned with the line of flight. Because it is not absorbing energy, 1) it will slow down to under 140 RPM, and 2) the reduced drag will allow the NxCC to continue to accelerate. This is that "High m " flight!

Procedure:

Descent from High Speed Cruise

The NxCC will be operating primarily as a fixed wing aircraft. As power is reduced and aircraft is trimmed forward to maintain speed, the rotor will be almost completely aligned with the line of flight. High m flight will continue.

Transition to Autogiro Mode

As power is reduced and trim is brought back to maintain altitude, the rotor disk will capture more airflow and gain energy, increasing its rpm. Restore "Rotor Trim" to "Max." To build rpm more rapidly, reduce the collective to –2° until rotor speed is around 300 rpm, then increase collective to maintain that speed.

Run-On Landings

With rotor stabilized at 300 rpm, adjust engine power for desired rate of descent. Maintain airspeed of at least 100 knots. Fly a normal approach, but use collective to flare. Pulling back on the stick will tip rotor back, slowing the aircraft, but reducing braking effectiveness.

Vertical Landings (zero roll landing)

Principles:

The NxCC is now going to enter helicopter mode, using the stored energy of the rotor to control descent. Caution: at 300 rotor rpm, there is only enough energy for one descent – you can’t hover! A vertical descent is possible from altitude, but a forward approach gives better visibility and control.

Procedure: