Update 18th April 2016: The helicopter HB-YNB has now 311 total hours (flying-, not blockhours!) This means about 100  hours during the last 12 month.

First contact with the Helicopter  (CH-7 Heli-Sport)

What you see is the new model Charlie with new cowling and the gear fairings for better and faster cruise performance. Together with Ligi Barbero I could do a one hour test flight. Ligi is a very good flight instructor and he had no fear to let me try everything I wanted to find out, including a simulated auto-rotation. After this weekend I was completely convinced, that this is the helicopter I’m going to build Modell Charlie, see the carbon fairings and new shaped engine cowling

FP03122006A0000Z

Preparation for 1st take-off

FP03122006A00011[1]

Is there room enough for my legs?

July 2006: I decided to pick up the kit in Torino myself, not only because the shipment and the cage would be very expensive, but also because I thought, that it would be a nice trip to Torino. We departed on a Sunday afternoon and arrived in a nice small hotel about 8pm. After a delicious Italian meal and a very nice wine we slept very well and were ready the next morning at the Strada Trafero del pino, 102-10132 Torino as agreed, 9am. After a very warm welcome by Claudio Barbero we started to pack Armin’s Ford-Transit. Our aim was to show up at customs at Ponte Tresa, a small border crossing-point near the city of Lugano, not later than 3pm. We were informed that the customs close their offices at 6pm. To be there rather early was a good decision. It turned out that the Italian custom officer was not happy with my papers. He wanted to be sure that we were not going to export critical military material. Thank God, Claudio Barbero was still in his office and could provide the custom office with the required declaration. The swiss customs-officer then was very kind, he even worked overtime to let us pass, a few days later I promptly received all the papers I will need later on when I will do the registration of the helicopter at FOCA. Late in the evening we arrived in Furna /Switzerland and quickly unpacked the Ford and stowed everything in the workshop.

FP03122006A00015[1]Welding the fuselage, Claudio Barbero, right, fuselage is under pressure to make sure there’s no leak

FP03122006A00016[1]Armin Egli, a good friend was so kind as to help me picking up the 1st Kit with his car.

FP03122006A00017[1]Happy but tired we arrived late at night in Furna

At home, I firstly had to find out what was / is in all the boxes! First kit, lot 1, includes basically all material without the main gearbox, tail rotor, rotor blades and engine. Everything is nicely packed and numbered, so the material is easy to find later on when assembling starts following the construction manual. The fuselage comes with a primer on it; one has just to select his favourite colour and can apply it. I decided to use the new bright and shiny orange Ford is using for their new car. From my previous project I knew a good paint shop in Pfaeffikon, Carrosserie Sandtner AG, Spenglerei + Spritzwerk, www.sandtner.ch. I prepared everything I thought should be painted and got it ready to be picked up. Horst Sandtner was so kind and lent me his mazda to carry all the stuff to bring it to his paint shop and back to my workshop.

FP03122006A0001E[1]…still an almost empty workshop…..

FP03122006A0001F[1]Content checked and ready to be used!

FP03122006A0001G[1]First lot ready to paint.

First assembly steps(26.08.2006)
After finding out how the construction manual works, I could start with the first steps. (CD, HTML based, instead of the manual, the lap-top is required in the workshop.) I quickly found out, that the bolts used to mount the skids to the gear were too short, 1-3 threads were not visible after tightening the nut. I know that this will not be accepted during the EAS (http://www.experimental.ch/) / FOCA (http://www.aviation.admin.ch/) inspection later on. Consequently I had to order a „mechanic’s kit, bolts and nuts“ from Aircraft Spruce.

FP03122006A0000K[1]Back from Sandtner, a very nice job!

FP03122006A0000L[1]First step is to put the gear on to the skids

FP03122006A0000M[1]…and after a while it already looks like a helicopter!

Pedals(09.09.2006)
The installation of the pedals and the corresponding rod until up to where the tail boom starts was a nice and easy job.

FP29102006A00011[1]Installation of Pedals

FP29102006A00012[1]Tail Rotor: First direction change

FP29102006A00013[1]

Tail Rotor: 2nd direction change

Assembly of Tailboom(10.09.2006)
The installation of the two bearing holder inside the tail boom was not easy. For me the instruction in the manual was not clear enough. In fact I had to remove the two holders again (!) after installation to interchange them. I made a short sketch, just in case I have to do it again next time. -:)

 

FP03122006A0000H[1]Front end

FP03122006A0000I[1]Rear end, ready to install tailrotor gearbox

FP03122006A0000J[1]Waiting to be installed after engine installation

Installation of Collective and Cyclic (10.09.2006)
A very nice job to do! The quality of the parts is amazing. Each step is very well illustrated in the manual.

FP29102006A0001A[1]only the cyclic itself has do be connected

FP29102006A0001B[1]ready to connect to the engines cables

FP29102006A00019[1]Collective, Cyclic together, view from left rear

Safety pin collective (21.10.2006)
These two bolts are turning with the collective.These nuts originally are metal self locking types. To be on the safe side I replaced them with castle nuts, drilled a hole and used a safety pin.

FP18112006A00005[1]Right

FP18112006A00006[1]Left

Rotax 912/914 line maintenance seminar (23.10.2006)
Being used to operate the Rotax 912 in my Kitfox I found it very useful to participate and spend one and a half day for these two engines, 912 and 914. (See: Franz-Aircraft) I got a lot of hints and tricks during the two days and I’m sure, it will make the installation / operation of the engine in my helicopter easier later on.

FP03122006A0001H[1]Do not turn this connector! (controls fuelpressure during high engine power)

FP03122006A0001I[1]Turbine with waste gate

FP03122006A0001J[1]Oel-pump, a second layer is connected on Rotax 914 for return oil from turbine

Preparing water/oil cooler (04.11.2006)
Preparation of the cooling system, waiting to be installed after engine installation

FP12112006A0000S[1]Watercooling (small Fan)

FP12112006A0000T[1]Oil & Watercooler (big Fan)

FP12112006A0000U[1]Both together, ready to install (this system will be replaced later on as a more efficient cooler-system is available)

Stby instruments/collision avoiding system) (05.11.2006)
Since I intend to install the Dynon FlightDEK-D180 instrument, I will need a liquid compass as back-up, a stby ASI and a stby Altimeter. The EWC100 is available from Ediatec (http://www.ediatec.ch/), it contains an obstacle database and also warns you of conflicting traffic (if the other traffic is also equipped with Flarm or EWC100 and closer than 2km).The digital display starts at a distance of 2km and below.

FP03122006A0001K[1]ECW100

FP03122006A0001L[1]EWC100, GPS Antenna, Data Antenna, Power Cable

FP03122006A0001M[1]Stby Instrument: ASI & Altimeter

Installation of battery holder (18.11.2006)
Installation of battery holder and connection of ground cable to the fuselage. 24th Nov 06: I received the callsign / numberplate from FOCA: HB-YNB (lateron battery installed more forward, below foot-area, CG issue)

FP03122006A0001A[1]Fuselage-side

FP03122006A00018[1]Battery Holder with Ground Connection

FP03122006A00019[1]Battery-side

Implementation/adaption of Dynon DEK180 (06.01.2007)
Instead of the Rotax Fly-Dat I will use the Dynon DEK 180. On first glance just „a minor change“ but a lot of work!

FP12052007A0000N[1]Working with the electric system

FP12052007A0000O[1]Dynon part of electric system

FP12052007A0000P[1]Engine cable with tags

Cabin installation with my brother Guido (01.04.2007)
This is the first try to fix the cabin onto the Fuselage. But to take a seat for the very first time is a lot of fun! We both together decided to loose some weight until the very first flight!

FP12052007A0000T[1]First try

FP12052007A0000U[1]Fixing cabin lower part

FP12052007A0000V[1]We both together decided to loose some weight until the very first flight!

Pick-up of 2nd kit, installation of mainrotor gearbox (01.04.2007)
We could pick up the 2nd part of the Kit March 26th 2007, everything worked fine and this time custom clearing was very quick. Content of Kit 2 was: Main Rotor Gear with Mast, Tail Rotor and the Blades.

FP12052007A0000Q[1]My brother Guido, looking to be very precise

FP12052007A0000S[1]According installation manual: Tilt after installation: 2.5° forward and .5° to the right

FP12052007A0000R[1]Weight about 35-40kgs

Cabin (05.04.2007)
To adjust the cabin on the fuselage took a while, but all in all a perfect job they do at Heli Sport!

FP12052007A0000W[1]Cabin, lower part

FP12052007A0000X[1]Gear Fairing

FP12052007A0000Y[1]Cabin, ready to fix

Adjustment of Canopy (21.04.2007, on my birthday!)
Fixing of canopy takes some time, a remaining gap will be covered later. Next step is covering the rear side of cabin with fireproof material.

FP12052007A0000Z[1]Opening-closing hinge

FP12052007A00010[1]Canopy closed

FP12052007A00011[1]First closing-opening from inside

Fire Wall (26.05.2007, on my birthday!)
Material: 0.3mm,steel, Glue: GYSO (www.gyso.ch) Polyflex 444, Paint: Dupli-Color, silver, heat-resistant to 800° C

FP03062007A00003[1]Fire-wall(Swiss Modification)

FP03062007A00004[1]Ready for paintshop

FP03062007A00002[1]0.3mm steel, ready to glue on

Fixing/adjustment of cowling (02.06.2007)
Before painting all the adjustments have to be done, also the cutout for the fuel filler cap. The inside of the cowlig doors are painted with heat resistant paint, silver, 800°C

FP03062007A00005[1]Installation of tailboom, to have the center for the cowling

FP03062007A00006[1]FP03062007A00007[1]Rubber band installation

Painting (16.06.2007)

FP04082007A0001W[1]

FP04082007A0001X[1]

Rigging (04.08.2007)
Rigging of Cyclic Control and Collective.
Stick fully aft must bring a pitch up of 16°, stick full down must bring a pitch down of 14° on water level indication.
Stick full left must bring 9-10° bank, stick full right must bring 8-9° bank indication on water level.
Collective: Adjust to have a 2mm distance from the bottom in the slot. (Collective in full down position

FP04082007A0001Y[1]Cyclic

FP04082007A0001Z[1]Rigging of Cyclic Control

FP04082007A00020[1]Rotor Head

Gear (19.08.2007)
Thanks to Ernst Baumgartner and Karl Hediger I have the best and nicest Gear you can have for a helicopter!
(later on I exchanged the gear with a two wheel-gear, not as nice, but more practicable)

FP19082007A0001Z[1]Removable gear

FP19082007A00020[1] - Kopie

FP19082007A0001Y[1] - KopieCabine, Oil, Fuelvalve (09.09.2007)
Image 1: Due to the narrow location, I had to find a possibility to drill the two holes: Stokys

FP09092007A0000P[1]Drilling with Stokys! (Seatbelts)

FP09092007A0000Q[1]Covers: Fuelwindow, Radio, Shoulder Harness

FP09092007A0000R[1]  Watch the Chipdetector below, very proud of, got it from Viktor Strausak

Oil Reservoir/Intrument Panel/Thermostat Rotax (27.10.2007)
Dynon: With new software 4.0 installed, running on internal Battery
Rotax is selling this Thermostat, keeping water temperature at a fix point of about 80 C

FP27012008A0003H[1]Oil Reservoir installed

FP27012008A0003I[1]Dynon, running  on internal power

FP27012008A0003J[1]Original Rotax Thermostat

Cooling Kit available from Heli-Sport (28.12.2007)
To avoid hot water/engine temperature while hoovering during high OAT, Heli-Sport is selling a cooling kit to be used with water thermostat

FP27012008A0003K[1]Looking forward

FP27012008A0003L[1]Looking forward

Engine preparation for installation (10.01.2008)

FP27012008A0003P[1]914 as shipped, out of the box

FP27012008A0003R[1]914, carburator removed

FP27012008A0003Q[1]Engine mount installed

Alternator installation (11.01.2008)
(Later replaced with EPA power alternator, rear installation)

Alt3

Cooling fan installation (19.01.2008)

cf2Cooling fan installed

cfan1View front-aft

Pully installation, including fan wheel(19.01.2008)

FP27012008A0003S[1]Oliver, my son, pully Installation

FP27012008A0003U[1]Cut „Halsmutter“ M8 to about 17mm

FP27012008A0003T[1]…..and install

 

Crew, ready to install engine (20.01.2008)

Marian and Oliver

FP27012008A0003Z[1]Marian

FP27012008A0003Y[1]Christina, the photographer!

Engine installation (20.01.2008)

FP27012008A00041[1]…ready….

FP27012008A00042[1]

FP27012008A00043[1]Ready to lift half up

Engine installed! (20.01.2008)

FP27012008A00044[1]…installed, aft section…

FP27012008A00045[1]…Marian, very concentrated…

FP27012008A00046[1]Oliver and „Papi“

FP27012008A00047[1] 

FP27012008A00048[1]

FP27012008A00049[1]

Cooling system (02.02.2008)

FP06042008A0000Z[1]Left cooler, incl. Thermostat cooler

FP06042008A00010[1]…see Rotax water Thermostat on the left…

FP06042008A00011[1]Rotax Thermostat

Cooling system (02.02.2008)

FP03022008A0002W[1]Note additional distance to have enough room for steering rod

FP03022008A0002X[1]   Tube from waterpump to R water-cooler

FP03022008A0002Y[1]Connection between R cooler to L watercooler

Clutch installation (02.02.2008)
Clutch: after tightening with 150Nm to max. 160Nm it must fit like picture 1 shows, if not, unscrew again and turn 1 or 2 teeth and try again. (this is to have tailrotor still connected in case something brakes in the coupling.)

FP03022008A00035[1]It has to look like this after tightening with 150Nm

FP03022008A00036[1]Alu stripe to hold against during tightening

FP03022008A00037[1]Clutch, ready to connect tailrotor shaft

 

Engine Mount (02.02.2008)

FP03022008A00032[1]Left, front

FP03022008A00033[1]left, aft

FP03022008A00034[1]Engine stabilizer, below

Oil system(16.02.2008)
Installation of oil-circuit system according Rotax 914 installation manual. To avoid damage due to vibration the oil pressure sensor is not directly mounted to the engine housing. Note that this installation needs an additional grounding of the sender (red wire)

FP27052009A00002[1]Oil Reservoir

FP27052009A00003[1]Oil pressure Sender

FP27052009A00004[1]Remote installation of oil pressure Sender

Gearbox-oil-cooling 1 (23.02.2008)
Main gear-box oil cooling system

FP24032008A0002G[1]Oil-pump for main gear, view from left

FP24032008A0002H[1]…view from behind

FP24032008A0002I[1]…..view from right

Gearbox-oil-cooling 2 (24.02.2008)
Oil-cooler installation, in front of water-oil cooler. Oil runs from gearbox lower forward fitting to the filter, from filter to pump-IN, from pump-OUT into cooler and then from cooler back to the gearbox, upper rear fitting.

FP24032008A00025[1]Oil filter (above), below oil cooler

FP24032008A00026[1]Main gearbox oil filter Installation

FP24032008A00027[1]Oil cooler

Fuel System Installation 1 (22.03.2008)
To have exact fuel available at any moment during flight, I decided to install a Return Flow Controller from Matronics.

FP24032008A0002J[1]The best Fuelselector available in market….! (Andair, England)

FP24032008A0002K[1]…how it looks from behind

FP24032008A0002L[1]Forward Flow Transducer

Fuel System Installation 2 (23.03.2008)

FP06042008A00015[1]Filter, pumps

FP06042008A00016[1]Pumps, fueltransducer, fwd and return flow

..then the line goes to the……

Fuel System Installation 3 (24.03.2008)

FP06042008A00018[1]….to the carburator..

Also the fuel-return line has his Return Flow Transducer

Pumps, incl. fuel pressure sender for Dynon

Pick-up of „Rolling-Hangar“ (28.03.2008)
Today is another great day: Finally I could pick-up the „Rolling-Hangar“ together with my friend Noldi Schwaninger. The Klaesi team did a very nice job, see http://www.klaesi.ch/. The hangar is isolated and should keep the helicopter in a nice and friendly climate. Total length of the box is 7m50. Max. Driving speed is between 80-90kmh. Maximum allowed vehicle weight is 3.5 tons. There is still a payload of 1250kg available with the box mounted on the vehicle. (Remember: Helicopter should end-up with around 285kg)

Fuel System Installation 4 (31.03.2008)
Fuel-tank holder installation: The fixing with textile fixation straps is only for the temporary fixing of RH-tank good enough, for fix installation of L-tank a fixation with metal straps is required

FP06042008A0001E[1]Left tank protection

FP06042008A0001F[1]L-Tank holder, TCU behind

FP06042008A0001G[1]R-Tank holder, protection

TCU (02.04.2008)
Servo motor for waste gate, mounted behind LH tank holder

FP06042008A0001I[1]Gas cable, connected to governor/collective

FP06042008A0001J[1]L-Carburetor

FP06042008A0001K[1]R-Carburetor

Trim System (26.04.2008)
Longitudinal / side trim
The movable rod of servomotor has to line with nose up and down bar of cyclic. Before fixing make sure the movable servomotor rod is fully extended. Warning: do not power the trim motor only to extend the rod, rather turn it out manually until you hear the „click“ from stop-switch!
Side trim: good to drill hole for the bolt when still room available, before installation of battery, etc.

 

FP27042008A0002P[1]Longitudinal Trim

FP27042008A0002Q[1]Side Trim

Preparation of winch Installation (03.05.2008)
Preparation of winch, remote controlled, to pull helicopter up/down.
Sutter GmbH, Elektro-Seilwinde 2000lbs-900/1800kg f. Quads Linhai ua
4 ST x 504358 KFZ-RELAIS FRC6BA-1-DC12V 1XEIN 150 A, 1 ST x 190904 2-KANAL-RF-FERNBEDIENUNGSSET – FG

 

FP03052008A0000E[1]Remote control, 2 ch

FP03052008A0000F[1]Whole set, ready to install

Rolling hangar, video system installation(04.05.2008)
Video installation:
2 ST x 855140 FUNK-ZUSATZKAMERA FÜR 853432
1 ST x 853432 FARB-TFT-RÜCKFAHRVIDEOSYSTEM FUNK

Service Bulletin 38 (10.05.2008)
SB 38, dated 5th May 2007 says:
The main tank (left) in the Charlie version is at a such distance from the exhaust manifold of cylunder 2 that it does not affect the tank by normal working. By supposition of a break of the exhaust manifold near the outlet of the cylinder 2, the exhaust gas at hot temperature could turn towards the tank, with negative consequences, therefore we suggest to apply a suitable protection on the surface of the tank near the manifold.
I decided to protect both tanks, R and L.

FP12052008A0000X[1]Left Tank, steel, covered with hi-speed tape

FP12052008A0000Y[1]Additional Right Tank

Installation of Battery, master Relay and Shunt (20.07.2008)
Due to EFIS installation (lighter instruments) and due to advice of other builders I decided to install the battery forwrd, below the cabin floor.

FP20072008A0000S[1]Battery and Shunt

FP20072008A0000T[1]Battery Installation

FP20072008A0000U[1]Master Fuse (80A), Master Relay and Shunt

EGT probe Installation(11.10.2008)

FP12102008A00008[1]EGT, M8 screw, locking: M3

TCU Connection (11.10.2008)
The Mapper-Card is between the engine and the TCU-Box[/fusion_text]

FP12102008A00005[1]Mapper Card

FP12102008A00006[1]Mapper card, mounted on top of engine wiring box

FP12102008A00007[1]View from left side

Battery Charging (18.10.2008)
I have installed a battery charger plug to keep the 12V Batt always at a good level. The „keep alive power“ for the internal back-up battery of the Dynon EFIS DEK 180 is only charged, if the plug is connected. This to prevent taking current from aircraft battery while stored (to avoid low battery voltage).

FP19102008A0001Q[1]Battery Keep alive plug

FP19102008A0001R[1]Plug with internal bridge from +12V to „keep alive pwr Dynon

FP19102008A0001S[1]Eng Oil Chip Detector

Instruments (01.11.2008)
Instruments, ready to connect everything!

FP19072009A0002Q[1]DEK 180 on internal power

FP19072009A0002R[1]…still something to do!

FP19072009A0002S[1]…and the view half closed

EFIS, first tests (01.03.2009)

FP06012012A00005[1]Elec power on all instruments

FP19072009A0002Q[1]Instruments with switching Panel

FP01032009A0000M[1]Not yet bundled

FP27052009A00009[1]

Connecting Tailboom to the Fuselage (25.04.2009)

FP27052009A00008[1]

Mounting of Tailboom, -Gearbox (25.04.2009)

FP27052009A00005[2]Tail gearbox

FP27052009A00006[1]Tal gearbox

FP27052009A00007[1]Tail rotor

Anticollition light (26.05.2009)
LED beacon Its size (2.5″ dia. x 3″ high) Utilizing LED (Light Emitting Diode) technology, Whelen is able to provide the following advantages compared to existing light assemblies.

Features
* Lamp Life – light source has shown conservative lab life results greater than 20,000 hours
* Reduced Power Consumption – More efficient than alternative light sources
* No external power supply
* Reduced operating Costs
* Shock & Vibration Resistant – No fragile filament
* Utilizes State-of-the-Art Surface Mount Technology
* No EMI or RFI Interference
* FAA TSO-C96a Class III Approved
* Hard Coated Clear Polycarbonate Lens
* Unit complies with color requirements per FAR Parts 23, 25, 27 and 29 for Aviation Red
* Reduced Weight (0.55 lbs.)
* 3 year warranty

Specifications
* Lamp: LED (Light Emitting Diode)
* Voltage: 14 VDC or 28 VDC
* Input Current: 1.2 AVG @ 14 V
* LED Color: Aviation Red
* Approx. Life: 10,000 Hours
* Weight: 0.55 Lbs.

FP27052009A0000E[1]

FP27052009A0000F[1]Muffler, turbine (26.05.2009)
View from below/behind to turbine, muffler.
See also water Thermostat.

FP29082009A00005[1]Muffler

FP27052009A0000I[1]Intake Air to TurbineFP27052009A0000J[1]

Air Filter mounting

Mounting of LH Fueltank (30.05.2009)
Left tank installation, including protection of heat to the tank from possible leaking exhaust pipe.

FP26092009A0001R[2]L-Tank, markings until 16 ltrs

FP31052009A00049[1]Fixing at the top

FP31052009A0004A[2]…and view from below…

Hobs meter Installation (31.05.2009)
To have the Hobsmeter recording only flight time you need a microswitch contact closing when collective is lifted. Watch the very thin steel arm below collective

FP31052009A0004B[1]Hobs meter, as installed in instrument Panel

FP31052009A0004C[1]Micro switch with thin steel arm

Undercarriage (18.07.2009)

FP19072009A0002T[1]Transport wheels

FP19072009A0002U[1]Step

FP19072009A0002V[2]Rotor blades (25.07.2009)
The leading edge of both rotor blades are covered with 3M Polyurethane Protective Tape 8561. The tape sells normaly only as 33m x 10cm rolls. I got 4m thanks to a friend. I used 1.60 m on each blade to protect the leading edge.
This is to allow flights in light rain and as a general protection.

FP15012012A00002[1]3M Polyurethane Protective Tape 8561

Very first engine run (01.08.2009)
The great moment came on 1st August 2009: A great day, after about 3 years of building the very first engine run!
Engine temperatures, pressures, engine rpm all within limits and correct indication.
Missing was the rotor rpm indication. This later turned out that there was a mistake in the wiring leading to a defect on the voice warning card. This problem could be fixed after sending the unit to the manufacturer.
This is a great opportunity to say „thank you very much“ to my construction adviser Meinrad Frey, to my neighbor Armin Egli and of course also to my wife Christina!
As the workshop is quite at high altitude (1480m above sea level) I had to dislocate the helicopter during the winter down into a hall of a good friend. See the following link to see a nice video.

FP20122009A00008[2]Very first run, a bit smoke!

FP20122009A00009[2]After 24Min, still all o.k.

FP20122009A0000A[2]Happy, all went fine!

Heat Protection, Water Reservoir (08.08.2009)
Turbine can get very hot, protection of water tubes makes sence.

FP29082009A00005[1]Heatprotection

FP29082009A00006[1]Fixing left side

FP29082009A00007[1]Cooling water: relief on highest Point

Fuel Quantity Calibration (19.09.2009)
Fuel Tank left: Useable fuel quantity 30.6 liters, not useable 1 liter. The fuel probe is a Princeton Capacitive Fuel Level Probe, 5 set point model.
First: calibrate the fuelprobe, EMPTY, 1/4 set point, 1/2 set point, 3/4 set point and FULL and then the calibration in EFIS/EMS according DEK180 Manual.

FP26092009A0001R[2]Left Tank, total 31.6 Liters

FP26092009A0001S[2]Placard left tank

FP26092009A0001T[2]Princeton, 5SP model

Fuel Quantity Calibration (20.09.2009)
Fuel quantity is very accurate; tolerance is 0.5 liter over the whole tank quantity. While actual quantity in tank is almost 11 liters, indication on EFIS is 10.5 liters. The yellow range starts at 10 liters, this corresponds to about 30 minutes flight time. The red range starts at 4 liters; this is shortly after the mechanical low fuel level warning light, set at 5 liters, mounted in left tank, will come on.
At 4 liters remaining fuel the EFIS warning is also readable on headset, the 8 minutes should be sufficient to make an immediate landing.

FP26092009A0001U[1]Almost 11 Liters in tank

FP26092009A0001V[1]EMS: Fuel page

FP26092009A0001W[1]EFIS & Fuel page

1st Testrun with rotor blades installed (21.11.2009)
After installation and static balancing of both rotor blades we were eager to find out about how it feels like when the rotor was turning.

1st test run was with weight on skids (about 70kgs each side), this to avoid any problems in case of heavy vibrations.
Result: almost no vibrations!
The decision was to remove the weight for the second run
The run was very smooth as well, in fact compared to a Robinson: I was never starting up an R22 with such low vibrations!

Engine removal after overspeed (12.02.2010)
I publish these pictures because in aviation we have the tradition, that we should talk about our mistakes so that others must not make them again!
After first rotor test runs, the engine had logged 1 hour and 52 minutes only, I was checking the setting in the TCU(turbine control unit) again and discovered an engine over speed in the stored data file. According Rotax maintenance manual rpm more than 6200 rpm means an engine overhaul!
Reason for the overspeed: My mistake, I selected initially for the very first engine run the wrong engine-rpm-probe for the EFIS input!
As a consequence I had to remove the engine and drive it to Munich for a complete overhaul and pick it up 4 weeks later again! (One weekend to remove it and 4 days Easter-holiday to install it again!)
Lessons learned: Never run the freshly installed engine for the first time without controlling and observing engine rpm via data link and laptop!
Quite an expensive mistake, but after engine overhaul the TBO was increased from 1500 hours to 2000 hours, at least that!
The engineers at Franz in Munich did a very nice job, I could pickup the engine again after about 4 weeks only. By the way: During the very first engine run I found an rpm difference between EFIS indication and TCU rpm of only about 10 rpm!

FP01052010A00002[2]What a picture: engine removed again!

FP01052010A00003[2]Transport to Rotax dealer Franz in Munich

FP01052010A00004[2]

One month later: Servicable engine

Markings, HB-YNB (26.04.2010)
This nice job was done by a company called
SIGN-FACTORY Schilderhersteller GmbH
Graf-Maximilian-Straße 18
6845 Hohenems, Austria,
the owner’s name is Patrick Brunner, e-mail: patrick.brunner@indepro.ch

FP01052010A00005[2]Selina, working very concentrated!

FP01052010A00006[2]Now it’s already Helicopter NB!

FP03102010A0001X[2]Left side already finished

W & B, weighing of helicopter (22.05.2010)
Weighing of project is always an exciting moment!
To keep it short: 301 kgs, with pilot 381 kgs!!

FP07082010A00019[1]Center of Gravity by common sence!

FP07082010A0001A[1]Weighing Team: Kari Haller and Meinrad Frey

FP07082010A0001B[1]Weighing

FP15012012A00003[1]Fotoshooting! (03.10.2010)

FP15012012A00004[1]

FP15012012A00005[1]Instruments, hall (03.10.2010)
Helicopter is ready to be inspected by FOCA.
I could finish my helicopter in the hall of Baumgartner Ernst, Markus and Peter. Thank you very much!

FP03102010A0001T[1]Instruments

FP03102010A0001S[1]Instruments

FP03102010A0001V[2]Lobag Maschinenbau

FP03102010A0001U[1]Outside, ready to fly! (03.10.2010)
Fotoshooting on a very nice Sunday.

FP03102010A0001X[2]

FP03102010A0001W[2]FOCA Inspection (29.10.2010)
FOCA Inspection, last hurdle before receivieng the permit to fly!

FP03112010A00002[1]Hanspeter Bellwald & Leo Halberstadt, FOCA

FP03112010A00003[1]All done!

FP03112010A00004[1]PERMIT TO FLY!

Very first flight! (20.11.2010)
Today was the day, I was dreaming since summer 2006!
I made my very first flight with my helicopter!
Charlie Bachmann, the testflight Advisor was of great help. Thanks to his experience we could do 3 flights with a total of 1h35 flying time!

FP06012012A00004[1]What a Feeling!

FP06012012A00003[1]

FP06012012A00002[1]First landing at high altitude (22.09.2011)
After my mountain examination flight and Robinson R44 type rating I had to do a mountain flight with my Kompress! At that time the ski’s were not yet installed, as you easily can see!

Landing place is called Huefifirn, next to the Planurahuette.

For landing at another place in the eastern part of Switzerland see: Madrisahorn

Hüfifirn, Glärnisch

FP06012012A00005[1]Look at the density altitude!

FP06012012A00006[1]Landing in almost fresh snow

FP06012012A00007[1]Later installed

Intercooler Installation (22.10.2011)
The maximum airbox temperature should never be higher than 88 ° celsius, above this temperature the waste-gate of the turbine will open to bypass air.
Since this would be dangerous during approach or take-off, I decided to install an intercooler to stay away from the 88 degrees.
Everything worked fine from the beginning and was tested during a flight to Huefifirn, Vorab and Grap Sogn Gion

___________________________________________________

This installation has been removed and I installed normal Rotax Airbox again. It contributed to an incident I had in October 2012.

At this moment I installed a temperature Sender in the airbox, I never noted more then 75 °, so an aircooler is not required and I have been up to 4150m in the meantime!

FP06012012A00008[1]View from left

FP06012012A00009[2]View from right

FP06012012A0000A[2]Corvatsch, 3200 m above sea Level

Lightweight Lithium Ion starter battery (22.12.2011)
Battery Fact Sheet Super B 5200, http://www.super-b.com/
Product Description
Lightweight Lithium Ion starter battery, 1.98 lb / 900 gram,
This newly developed battery is designed to replace the much heavier 10 to 12 Ah lead/acid battery. The super B 5200 is based on the safe Lithium Iron Phosphate technology (LiFePO4), better known as Lithium Ion.
The super B 5200 delivers up to 300 Cranking Amps.
The super B 5200 offers many advantages over conventional 10 to 12 Ah lead/acid batteries:
Weighs less: as much as 80% weight saving; 1.98 lb / 900 grams;
Recharges many times faster: within 5 minutes after starting your engine the battery will be recharged;
Is much smaller: 1/3 or less of the space; 4.49 inch, 3.2 inch, 2.4 inch (WxHxD) / 114mm x 81.25mm x 62mm (WxHxD);
Has a longer service life: more than 5 years instead of 2 to 3 years;
Has a low self-discharge rate.
Safety: Super B batteries are based on Lithium Iron Phosphate technology (LiFePO4). This so called Lithium Ion technology as used in the super B batteries is the safest Lithium Ion technology today.
Capacity
super B 5200 refers to 5.2 Ah (Amps/Hour), which represents the real nominal capacity under maximum continuous load. How different this is from lead / acid batteries where manufactures provide a 20 hour rating. For example the 10 Ah lead / acid batterie can be discharged over a period of 20 hours with a 0.5 Amp load. This is not very practical, as the same 10 Ah battery discharged with a 2,5 Amp load, for example a 25 Watt light bulb, will yield no more than 2.2 Ah of energy. The lead-acid battery, therefore, has less capacity when the load increases, which means that you can start more often with the super B.

FP15012012A00009[2]See the Difference!

FP15012012A0000A[2]Before

FP15012012A0000B[2]After

Cabin Heater Installation (15.01.2012)
To have it nice and warm an Eberspächer B1 LC Air Heater is installed.
To compensate the additional weight a lightweight Lithium Iron starter battery,  specially developed for motorcycles, jet-skis, snowmobiles, ATVs and Quads was installed.

FP15012012A00006[1]View from right below

FP15012012A00007[1]Air Inlet Cabine, R, very important: take the air to heat from inside the cabin as well, if not, heater will overheat and shut down! ( due to (almost) blocked airstream if the cabin is closed)

FP15012012A00008[1]Control unit, ON/OFF and Temp selector

Status of the helicopter right now (February 2015)
Helicopter is upgraded to model Kompress Charlie 2 (EPA power alternator, water-oil heatexchanger, means new Thermostat and watercooler, carbon blades, carbon stabilizer) and I just made my highest landing you can do in Switzerland.

 

Video: Monte-Rosa Satteltole, 4’150m/13’615ft!