RV-List Digest Archive

Thu 11/23/06


Total Messages Posted: 10



Today's Message Index:
----------------------
 
     1. 04:09 AM - Re: RV-8 Service Ceiling (Dana Overall)
     2. 05:19 AM - Re: RV-8 Service Ceiling (DOUGPFLYRV@aol.com)
     3. 05:52 AM - Re: Dynon electrical questions (Charles Reiche)
     4. 07:09 AM - Re: Dynon electrical questions (Frank Stringham)
     5. 08:10 AM - Re: RV-8 Service Ceiling (Larry Bowen)
     6. 11:55 AM - Day/night VFR requirements (Gerry Filby)
     7. 01:09 PM - Re: Day/night VFR requirements (Hedrick)
     8. 01:11 PM - Re: Day/night VFR requirements (Doug Weiler)
     9. 02:44 PM - Re: Day/night VFR requirements (Mike Robertson)
    10. 08:40 PM - Re: Day/night VFR requirements (Gerry Filby)
 
 
 


Message 1


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    Time: 04:09:43 AM PST US
    From: "Dana Overall" <bo124rs@hotmail.com>
    Subject: Re: RV-8 Service Ceiling
    Use the 20K but just for fun go to Mike Stewart's, aka Kahuna from TeamRV, and check out his high altitude ride in his Super 8. Dana Overall Richmond, KY i39 RV-7 slider, Imron black, "Black Magic" O 360 A1A, C/S C2YK-1BF/F7666A4 http://rvflying.tripod.com/id30.html do not archive >From: Kelly McMullen <kellym@aviating.com> >To: rv-list@matronics.com >Subject: Re: RV-List: RV-8 Service Ceiling >Date: Wed, 22 Nov 2006 21:20:35 -0700 > > >Better to tell the shop to use 20,000 ft. Otherwise you need an altimeter >certified higher, either 30 or 35K, which will cost you more. No sense in >doing it unless you intend to use it. >Ron Lee wrote: >> >> >>>Can someone please provide the accepted service ceiling for an RV-8 with >>>an IO-360 and Sensenich metal prop. 'Shop checking my altimeter and >>>transponder in place says needs this altitude figure. >> >>I would use 23,000' according to this link: >> >>http://www.vansaircraft.com/public/rv-8per.htm >> >>180 HP and solo. >> >>I never has anyone ask me the same for my plane. >> >>Ron Lee >> >> >> > > _________________________________________________________________ Get the latest Windows Live Messenger 8.1 Beta version.Join now. http://ideas.live.com


    Message 2


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    Time: 05:19:16 AM PST US
    From: DOUGPFLYRV@aol.com
    Subject: Re: RV-8 Service Ceiling
    We have always used a 20,000' altimeter. Doug Preston RV-7A N196VA


    Message 3


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    Time: 05:52:32 AM PST US
    From: Charles Reiche <charlieray@optonline.net>
    Subject: Re: Dynon electrical questions
    I would seriously consider using the signal grounds the way shown on the print and not tying them to airframe ground. With noise on the power bus and return flow currents flowing through the skin of the aircraft, even though you are reading 0 on your meter now, there may be a difference in potential or AC on the "ground" when you are running and flying. If you are worried about having extra signal grounds available at the dynon for future use, bring all your sensor signal grounds together and leave some extra pigtails there about 4" long and cap them off with heat shrink after folding the end of the wire over, this allows you to come back later and butt splice or solder in without getting too crazy into the plug. Charlie ----- Original Message ----- From: "Dana Overall" <bo124rs@hotmail.com> Sent: Wednesday, November 22, 2006 8:56 PM Subject: RV-List: Dynon electrical questions > > First off, Happy Thanksgiving everyone. > > Working on the final sensor hookups firewall forward and have a couple > questions for you Dynon installers. > > Dynon list pins 5,16 & 17 as shared sensor grounds with pin 3 being the > avionics bus ground. I wired in the fuel pressure sensor and simply ran a > ground from the sensor to the my ground bus and grounded using the 5,16, > 17. I got the same 0 reading both ways on the screen. Any problem going > directly to the bus? The reason I ask, if I add something in the future > and use up 5,16 and 17 on my initial install, I want to be able to have an > out without splicing. > > Pin 18 is the +5V excitation wire for sensors such as carb temp and > manifold pressure. Since this is only one wire, I was thinking of using a > small bus bar to leave open future possibilities. Anyone got any pics of a > simple splice? > > Getting close and loving it. > > Just a hint http://rvflying.tripod.com/blackwing1.jpg > > Dana Overall > Richmond, KY i39 > RV-7 slider, Imron black, "Black Magic" > O 360 A1A, C/S C2YK-1BF/F7666A4 > http://rvflying.tripod.com/id30.html > do not archive > > _________________________________________________________________ > MSN Shopping has everything on your holiday list. Get expert picks by > style, age, and price. Try it! > http://shopping.msn.com/content/shp/?ctId00,ptnrid=176,ptnrdata 0601&tcode=wlmtagline > > >


    Message 4


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    Time: 07:09:25 AM PST US
    From: "Frank Stringham" <fstringham@hotmail.com>
    Subject: Dynon electrical questions
    Dana Happy Thanksgiving to you and to all I am going to solve the panel / audio portion grounding problem by using Bob's suggestions found at http://www.aeroelectric.com/ under Whats New...Chapter on Audio Systems...pages 11 -13. Good Luck Frank @ SGU and SLC ......RV7A.....wiring/fiberglass.........$$$$$$$$$$$$$ >From: "Dana Overall" <bo124rs@hotmail.com> >To: rv-list@matronics.com >Subject: RV-List: Dynon electrical questions >Date: Wed, 22 Nov 2006 20:56:28 -0500 > > >First off, Happy Thanksgiving everyone. > >Working on the final sensor hookups firewall forward and have a couple >questions for you Dynon installers. > >Dynon list pins 5,16 & 17 as shared sensor grounds with pin 3 being the >avionics bus ground. I wired in the fuel pressure sensor and simply ran a >ground from the sensor to the my ground bus and grounded using the 5,16, >17. I got the same 0 reading both ways on the screen. Any problem going >directly to the bus? The reason I ask, if I add something in the future and >use up 5,16 and 17 on my initial install, I want to be able to have an out >without splicing. > >Pin 18 is the +5V excitation wire for sensors such as carb temp and >manifold pressure. Since this is only one wire, I was thinking of using a >small bus bar to leave open future possibilities. Anyone got any pics of a >simple splice? > >Getting close and loving it. > >Just a hint http://rvflying.tripod.com/blackwing1.jpg > >Dana Overall >Richmond, KY i39 >RV-7 slider, Imron black, "Black Magic" >O 360 A1A, C/S C2YK-1BF/F7666A4 >http://rvflying.tripod.com/id30.html >do not archive > >_________________________________________________________________ >MSN Shopping has everything on your holiday list. Get expert picks by >style, age, and price. Try it! >http://shopping.msn.com/content/shp/?ctId00,ptnrid=176,ptnrdata 0601&tcode=wlmtagline > > _________________________________________________________________ Share your latest news with your friends with the Windows Live Spaces friends module.


    Message 5


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    Time: 08:10:57 AM PST US
    From: "Larry Bowen" <Larry@bowenaero.com>
    Subject: RV-8 Service Ceiling
    My recent xpdr check was done to 20K. They didn't ask me for that figure. - Larry Bowen Larry@BowenAero.com http://BowenAero.com > -----Original Message----- > From: Kelly McMullen [mailto:kellym@aviating.com] > Sent: Wednesday, November 22, 2006 11:21 PM > To: rv-list@matronics.com > Subject: Re: RV-List: RV-8 Service Ceiling > > > Better to tell the shop to use 20,000 ft. Otherwise you need > an altimeter certified higher, either 30 or 35K, which will > cost you more. > No sense in doing it unless you intend to use it. > Ron Lee wrote: > > > > > >> Can someone please provide the accepted service ceiling > for an RV-8 > >> with an IO-360 and Sensenich metal prop. 'Shop checking > my altimeter > >> and transponder in place says needs this altitude figure. > > > > I would use 23,000' according to this link: > > > > http://www.vansaircraft.com/public/rv-8per.htm > > > > 180 HP and solo. > > > > I never has anyone ask me the same for my plane. > > > > Ron Lee > > > > > > > > > Photoshare, and much much more: > > >


    Message 6


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    Time: 11:55:47 AM PST US
    Subject: Day/night VFR requirements
    From: Gerry Filby <gerf@gerf.com>
    What are the equipment requirements to operate day/night VFR ? I may be being dense but I'm finding it hard to locate a definitive list ... __g__ ========================================================== Gerry Filby gerf@gerf.com ----------------------------------------------------------


    Message 7


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    Time: 01:09:30 PM PST US
    From: "Hedrick" <khedrick@frontiernet.net>
    Subject: Day/night VFR requirements
    This is taken from- aopa.org Keith Hedrick Rv-6 Carlinville il 3LF ====================== Required Flight Instruments And Equipment VFR Day: ATOMS LEFR Memory Aid ATOMS Love Electrons Flying Round AA Altimeter, airspeed indicator TT Tachometer, temperature gauge OO Oil temperature, oil pressure gauges MM Magnetic compass, manifold pressure gauge SS Seat belt, shoulder harness L Landing gear position indicator (retractable-gear aircraft) E Emergency locator transmitter F Fuel quantity gauge for each tank R Rotating beacon VFR Night: Atoms LEFR + PLFA Memory Aid ATOMS LEFR plus Pilots Love Flying Airplanes P Position lights (green right wing, red left wing, white tail) L Landing light (only if used for hire, not flight instruction) F Fuses a spare set of each required type accessible to the pilot in flight A Anticollision light (red and/or white) rotating beacon IFR: Above VFR instruments and equipment for either day or night, plus RRSACAPD Memory Aid Read Regulations So Aviation Credentials Always Produce Dividends R Two-way radio R Gyroscopic rate of turn indicator (turn coordinator) S Slip/skid indicator (inclinometer) A Altimeter adjustable for barometric pressure C Clock with digital or sweep hour, minutes, and seconds display A Alternator or generator P Gyroscopic pitch and bank indicator (attitude indicator) D Gyroscopic direction indicator (heading indicator) Flight Instruments By Group Pitch Instruments Altimeter Airspeed indicator (ASI) Attitude indicator (AI) Vertical speed indicator (VSI) Bank Instruments Heading indicator (HI) Attitude indicator (AI) Turn coordinator Power Instruments Tachometer (RPM) Manifold pressure (MP-aircraft with constant-speed propellers) Airspeed indicator (ASI) Flight Instruments By System Pitot-Static Instruments Pressure altimeter Vertical speed indicator (VSI) Airspeed indicator (ASI) Gyroscopic (Vacuum) Instruments Attitude indicator (AI) Heading indicator (HI) Gyroscopic (Electric) Instruments Turn coordinator (many aircraft) -----Original Message----- From: owner-rv-list-server@matronics.com [mailto:owner-rv-list-server@matronics.com] On Behalf Of Gerry Filby Sent: Thursday, November 23, 2006 1:54 PM Subject: RV-List: Day/night VFR requirements What are the equipment requirements to operate day/night VFR ? I may be being dense but I'm finding it hard to locate a definitive list ... __g__ ========================================================== Gerry Filby gerf@gerf.com ----------------------------------------------------------


    Message 8


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    Time: 01:11:47 PM PST US
    Subject: Re: Day/night VFR requirements
    From: Doug Weiler <dcw@mnwing.org>
    On 11/23/06 1:53 PM, "Gerry Filby" <gerf@gerf.com> wrote: > > > What are the equipment requirements to operate day/night VFR ? > I may be being dense but I'm finding it hard to locate a > definitive list ... Here is the list.. Doug Weiler ------------------------------ >From FAR 91.205: (a) General. Except as provided in paragraphs (c)(3) and (e) of this section, no person may operate a powered civil aircraft with a standard category U.S. airworthiness certificate in any operation described in paragraphs (b) through (f) of this section unless that aircraft contains the instruments and equipment specified in those paragraphs (or FAA-approved equivalents) for that type of operation, and those instruments and items of equipment are in operable condition. (b) Visual-flight rules (day). For VFR flight during the day, the following instruments and equipment are required: (1) Airspeed indicator. (2) Altimeter. (3) Magnetic direction indicator. (4) Tachometer for each engine. (5) Oil pressure gauge for each engine using pressure system. (6) Temperature gauge for each liquid-cooled engine. (7) Oil temperature gauge for each air-cooled engine. (8) Manifold pressure gauge for each altitude engine. (9) Fuel gauge indicating the quantity of fuel in each tank. (10) Landing gear position indicator, if the aircraft has a retractable landing gear. (11) For small civil airplanes certificated after March 11, 1996, in accordance with part 23 of this chapter, an approved aviation red or aviation white anticollision light system. In the event of failure of any light of the anticollision light system, operation of the aircraft may continue to a location where repairs or replacement can be made. (12) If the aircraft is operated for hire over water and beyond power-off gliding distance from shore, approved flotation gear readily available to each occupant and, unless the aircraft is operating under part 121 of this subchapter, at least one pyrotechnic signaling device. As used in this section, shore means that area of the land adjacent to the water which is above the high water mark and excludes land areas which are intermittently under water. (13) An approved safety belt with an approved metal-to-metal latching device for each occupant 2 years of age or older. (14) For small civil airplanes manufactured after July 18, 1978, an approved shoulder harness for each front seat. The shoulder harness must be designed to protect the occupant from serious head injury when the occupant experiences the ultimate inertia forces specified in 23.561(b)(2) of this chapter. Each shoulder harness installed at a flight crewmember station must permit the crewmember, when seated and with the safety belt and shoulder harness fastened, to perform all functions necessary for flight operations. For purposes of this paragraph (i) The date of manufacture of an airplane is the date the inspection acceptance records reflect that the airplane is complete and meets the FAA-approved type design data; and (ii) A front seat is a seat located at a flight crewmember station or any seat located alongside such a seat. (15) An emergency locator transmitter, if required by 91.207. (16) For normal, utility, and acrobatic category airplanes with a seating configuration, excluding pilot seats, of 9 or less, manufactured after December 12, 1986, a shoulder harness for (i) Each front seat that meets the requirements of 23.785 (g) and (h) of this chapter in effect on December 12, 1985; (ii) Each additional seat that meets the requirements of 23.785(g) of this chapter in effect on December 12, 1985. (17) For rotorcraft manufactured after September 16, 1992, a shoulder harness for each seat that meets the requirements of 27.2 or 29.2 of this chapter in effect on September 16, 1991. (c) Visual flight rules (night). For VFR flight at night, the following instruments and equipment are required: (1) Instruments and equipment specified in paragraph (b) of this section. (2) Approved position lights. (3) An approved aviation red or aviation white anticollision light system on all U.S.-registered civil aircraft. Anticollision light systems initially installed after August 11, 1971, on aircraft for which a type certificate was issued or applied for before August 11, 1971, must at least meet the anticollision light standards of part 23, 25, 27, or 29 of this chapter, as applicable, that were in effect on August 10, 1971, except that the color may be either aviation red or aviation white. In the event of failure of any light of the anticollision light system, operations with the aircraft may be continued to a stop where repairs or replacement can be made. (4) If the aircraft is operated for hire, one electric landing light. (5) An adequate source of electrical energy for all installed electrical and radio equipment. (6) One spare set of fuses, or three spare fuses of each kind required, that are accessible to the pilot in flight.


    Message 9


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    Time: 02:44:12 PM PST US
    From: Mike Robertson <mrobert569@hotmail.com>
    Subject: Day/night VFR requirements
    Check out FAR 91.205(b), (c), & (e). While the start says is is only applicable to standard category aircraft, the operating limitations that will be issued with the Special A/w cert will have a paragraph that says " Unless appropriately equipped in accordance with 21.205 for night and/or IFR flight, the aircraft is restricted to say VFR." Mike Robertson Das Fed ---------------------------------------- > Subject: RV-List: Day/night VFR requirements > From: gerf@gerf.com > To: rv-list@matronics.com > Date: Thu, 23 Nov 2006 11:53:57 -0800 > > > > What are the equipment requirements to operate day/night VFR ? > I may be being dense but I'm finding it hard to locate a > definitive list ... > > __g__ > > ========================================================== > Gerry Filby gerf@gerf.com > ---------------------------------------------------------- > > > > > _________________________________________________________________


    Message 10


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    Time: 08:40:13 PM PST US
    Subject: Day/night VFR requirements
    From: Gerry Filby <gerf@gerf.com>
    Thanks all !! (I get a mental block just looking at the cover of the FAR/AIM ..) Follow up question ... in the the "R" in "ATOMS LEFR" - I don't think I've ever seen a rotating beacon on an RV - do we have to comply ? g > > > This is taken from- aopa.org > > Keith Hedrick > Rv-6 > Carlinville il > 3LF > > > > Required Flight Instruments And Equipment > > > VFR Day: ATOMS LEFR > Memory Aid ATOMS Love Electrons Flying Round > > AA Altimeter, airspeed indicator > TT Tachometer, temperature gauge > OO Oil temperature, oil pressure gauges > MM Magnetic compass, manifold pressure gauge > SS Seat belt, shoulder harness > L Landing gear position indicator (retractable-gear aircraft) > E Emergency locator transmitter > F Fuel quantity gauge for each tank > R Rotating beacon > > VFR Night: Atoms LEFR + PLFA > Memory Aid ATOMS LEFR plus Pilots Love Flying Airplanes > > P Position lights (green right wing, red left wing, white tail) > L Landing light (only if used for hire, not flight instruction) > F Fuses a spare set of each required type accessible to the pilot in > flight > A Anticollision light (red and/or white) rotating beacon > > IFR: Above VFR instruments and equipment for either day or night, plus > RRSACAPD > Memory Aid Read Regulations So Aviation Credentials Always Produce > Dividends > > R Two-way radio > R Gyroscopic rate of turn indicator (turn coordinator) > S Slip/skid indicator (inclinometer) > A Altimeter adjustable for barometric pressure > C Clock with digital or sweep hour, minutes, and seconds display > A Alternator or generator > P Gyroscopic pitch and bank indicator (attitude indicator) > D Gyroscopic direction indicator (heading indicator) > > Flight Instruments By Group > > Pitch Instruments > > Altimeter > Airspeed indicator (ASI) > Attitude indicator (AI) > Vertical speed indicator (VSI) > > Bank Instruments > > Heading indicator (HI) > Attitude indicator (AI) > Turn coordinator > > Power Instruments > > Tachometer (RPM) > Manifold pressure (MP-aircraft with constant-speed propellers) > Airspeed indicator (ASI) > > Flight Instruments By System > > Pitot-Static Instruments > > Pressure altimeter > Vertical speed indicator (VSI) > Airspeed indicator (ASI) > > Gyroscopic (Vacuum) Instruments > > Attitude indicator (AI) > Heading indicator (HI) > > Gyroscopic (Electric) Instruments > > Turn coordinator (many aircraft) > > -----Original Message----- > From: owner-rv-list-server@matronics.com > [mailto:owner-rv-list-server@matronics.com] On Behalf Of Gerry Filby > Sent: Thursday, November 23, 2006 1:54 PM > To: rv-list@matronics.com > Subject: RV-List: Day/night VFR requirements > > > > What are the equipment requirements to operate day/night VFR ? > I may be being dense but I'm finding it hard to locate a > definitive list ... > > __g__ > > > Gerry Filby gerf@gerf.com > ---------------------------------------------------------- > > > > > > > > > _-> _-> _-> _-> _-> _-> _-> _-> _-> _-> _-> _-> _-> _-> _-> _-> _-> _-> _-> _-> _-> _-> _-> _-> _-> _-> _-> _-> _-> > > > -- __g__ Gerry Filby gerf@gerf.com ----------------------------------------------------------




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