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[70.193.200.102]) by mx.google.com with ESMTPSA id v41sm49248692yhi.19.2014.02.24.04.57.59 for (version=TLSv1 cipher=ECDHE-RSA-RC4-SHA bits=128/128); Mon, 24 Feb 2014 04:57:59 -0800 (PST) From: Todd Long Content-Type: text/plain; charset=us-ascii Content-Transfer-Encoding: quoted-printable Mime-Version: 1.0 (1.0) Subject: Re: [LML] G3x installation experience X-Original-Message-Id: <732EDA79-B15E-4054-AF66-94FECE534033@gmail.com> X-Original-Date: Mon, 24 Feb 2014 06:57:59 -0600 References: In-Reply-To: X-Original-To: Lancair Mailing List X-Mailer: iPhone Mail (11B554a) Nice review. Where's the pictures? We all like pictures Thinking of doing Ga= rmin too.=20 Sent from my iPhone > On Feb 24, 2014, at 6:24, N20087 wrote: >=20 > Folks >=20 > I thought I might share my experience with my avionics upgrade in my 360. = I decided to remove my Stec 55, sandel HSI and king remote gyro sell it all= and install the g3x system. I got 5k and change for the TSOed stuff and th= en tossed in 2k for the g3x with external autopilot control and 2 servos for= pitch and roll. >=20 > I chose the g3x for various reasons including the following=20 >=20 > I have a good deal of time behind the G1000 a lot and very used to the use= r interface > I think the gfc 700 is the best ga autopilot out there and the g3x shares a= lot of its technology > I already had 2 GNS 430s in my panel along with a Garmin transponder. I ex= pected the interfacing to work reliably on the same brand equipment=20 > Garmin documentation is fantastic, complete and accurate=20 > I have found Garmin support to be top notch as I am sure the other brands a= re but I did not want finger pointing between vendors when dealing with inte= gration of components; I wanted just one neck to ring >=20 >=20 > The entire removal and install took 3 weeks from engine shutdown to first f= light. Since I work full time this was a weekends and evening activity. A w= ord to the wise, don't do this kind of thing in a cold hanger in the depths o= f winter. Ask me how I know! >=20 > Pointers for others thinking of using this product >=20 >=20 > There is some wiggle room on system pricing with the dealers > Make sure you check lead times on all parts and get a delivery commitment a= s part of the deal > Make sure you inventory EVERYTHING on receipt. You may have to ask your d= ealer to make good on some missing items > The quality of the Garmin connectors/backshells is exceptional but they ar= e expensive. Don't accept substitutions. Garmin backshells are heavy alumi= num with a unique grounding bar that makes terminations easier and very effe= ctive=20 > Use a spreadsheet to map out your cable schedule with pin numbers and wire= colour for each connector > Buy a quality wire stripper, the kind that grabs the cable and then rips t= efzel down to the shield and then individual cores=20 > I standardized on 22awg all round even though 24awg can be used in many in= terconnects=20 > 22awg strips more reliably and does better with crimps > The connector kits come with quality machined d-sub pins/sockets, you will= need to buy more because you will screw up=20 > Invest in a quality pin compression tool > You will use a lot of zip ties for mocking things up - buy lots > Test your cables as you make them and make sure none of the cores are shor= ted to the shield=20 > Map out your panel using a cad tool (autocad has a free 1 month eval) and t= he dxf files for cutouts that Garmin provide > You can take your aircraft AL sheet and final panel layout dxf file to you= r local laser/water jet cutter to make the replacement sections. Note 2024 a= luminum needs a larger bending radius than shops are used to doing. =20 > You must purchase a gps antenna that connects to the pfd to use the synthe= tic vision feature >=20 > Once you wire up the PFD, ADAHRS and OAT sensor exactly per the manual you= can test the bare bones system. =20 > You must follow the magnetometer calibration procedure to the letter. > The system uses CAN bus for communications. This technology requires term= inations on each end. I terminated at the PFD and at the pitch servo > The servo mounting kits are pretty decent and complete but in the end I re= purposed what I already had which needed little modification > The magnetometer interference test is very useful in determining the insta= llation position. The sensor is mounted to one side of the hat rack below th= e floor. My tests passed for all electrical devices except the pitch servo c= lutch engagement. It was over by a max of 20%. In speaking to Garmin I migh= t get away with it. Having flown a few times now and using the ap there hav= e been no ill effects i.e. Bad headings or red Xs.=20 > I did not jack the aircraft as suggested by Garmin to verify interference e= ffects of the hydraulic pump since my pump is mounted on the inside of the f= irewall. =20 > The capstan servo kit does not include mounting brackets > You will need to make your own pitch servo bridle if you are using a capst= an scheme > I did not connect the auto trim system as I figured I would do this later > Even in a 360, there is a need to adjust pitch trim when changing speeds s= ignificantly with the ap engaged > if you use Garmin transponders make sure the firmware is up to date to ens= ure the RS232 connection to the ADAHRS works correctly > Make sure the autopilot servos are set to operate in the right direction o= n the ground otherwise things could get interesting really fast in the air. = In my case I had to reset the direction from the normal out of the box dire= ction, all a function of your mechanical mounting arrangement >=20 > So how does it fly? In a word, excellent! >=20 > The PFD screen really is big enough for a 360. The user interface is more= intuitive than the G1000.=20 > Very few integration headaches, just follow the Garmin directions > The highway in the sky feature along with the flight director and flight p= ath marker is really neat. But beware it can really dumb down your instrume= nt scan > The screen is plenty bright in sun > Tuning the auto pilot took about 10 minutes of tweaking the gains. The de= fault torque values are pretty close already=20 > Flying a coupled LPV approach is just amazing, it behaved flawlessly witho= ut much fuss even on a slightly bumpy day with a 12 kt x wind component. Th= e system flew an order of magnitude more smoothly and accurately than the or= iginal Stec 55. The integration ith the GNS430W is very well done. I really= did not have to change how I did things (buttonology) to fly an approach re= lative to the sandel but the presentation on the HSI is far better > Indicated air speed climb is quite usefull but should only be used in rela= tively smooth conditions as you will find the AP sawing on the controls. It= does a good job maintaining air speed, better than I ever could but I think= it is too hard on the controls. Sometimes you just have to hand fly! > Vertical speed climb is better damped but you would need to be on top of c= hanging the desired rate as performance bumps up against the edge of the env= elope > The up/down thumb wheel on the AP is really cool and handy > The default setting for sink rate Alarm is not consistent with Lancairs.=20= >=20 >=20 > Things yet to do >=20 > Install the Garmin AOA pitot > Install ADSB receiver for WX > Fix bitching Betty > fly more!=20 >=20 > Tom > Lnc2 312 hrs >=20 >=20 >=20 >=20 > -- > For archives and unsub http://mail.lancaironline.net:81/lists/lml/List.htm= l