AeroElectric-List Digest Archive

Fri 12/15/23


Total Messages Posted: 5



Today's Message Index:
----------------------
 
     1. 09:05 AM - Re: Re: Switch Question (Robert L. Nuckolls, III)
     2. 09:38 AM - Re: Switch Question (user9253)
     3. 10:31 AM - Re: Re: Switch Question (Robert L. Nuckolls, III)
     4. 12:50 PM - Re: Switch Question (farmrjohn)
     5. 04:03 PM - Re: Re: Switch Question (Robert L. Nuckolls, III)
 
 
 


Message 1


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    Time: 09:05:19 AM PST US
    From: "Robert L. Nuckolls, III" <nuckolls.bob@aeroelectric.com>
    Subject: Re: Switch Question
    At 06:14 PM 12/14/2023, you wrote: > >Reviving an old thread, when the original generator was swapped out >for an alternator they utilizedg only one pole of the two pole >switch to connect the batter to the bus, leaving the other side unused. >Would it be possible to utilize the unused poles to control a master >contractor leaving the heavy wiring from the batter to the switch >in place? That way when the switch was closed it would energize the >contractor and allow the connection to the bus, and provide a backup >method of disconnecting the battery should the contractor fail >closed for any reason. This is in anticipation of pursuing a >field approval for a contacor. Thanks, John Have you engaged an IA to assist in fabricating an Form 337 likely to be summarily approved? Find the maintenance manual drawings for the first airplane of the series that replaced the battery switch with a contactor. This is 'approved data'. Duplicate the architecture of that drawing in support of your 337 goes along way to getting it approved. Your risk of contactor-failure-by-sticking- closed is more remote now than it was 70 years ago. I've never heard of a 'back up battery disconnect' in any aircraft. Imitation is a demonstrated form of flattery . . . it's also a demonstrated prophylactic against bureaucratic disapproval. What airplane are we talking about? I may have the drawings you need in my library. Bob . . . //// (o o) ===========o00o=(_)=o00o======== < Go ahead, make my day . . . > < show me where I'm wrong. > ================================ In the interest of creative evolution of the-best-we-know-how-to-do based on physics and good practice.


    Message 2


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    Time: 09:38:11 AM PST US
    Subject: Re: Switch Question
    From: "user9253" <fransew@gmail.com>
    His airplane is an Alon Aircoupe that Univair now has the TCSD for. -------- Joe Gores Read this topic online here: http://forums.matronics.com/viewtopic.php?p=512789#512789


    Message 3


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    Time: 10:31:01 AM PST US
    From: "Robert L. Nuckolls, III" <nuckolls.bob@aeroelectric.com>
    Subject: Re: Switch Question
    At 11:37 AM 12/15/2023, you wrote: > >His airplane is an Alon Aircoupe that Univair now has the TCSD for. > >-------- >Joe Gores Okay, thanks Joe. It' been 20 years since I was last involved in any 'certifiable' field work on a TC aircraft so I dug back into some old files. There were individuals certificated by the FAA to accomplish various tasks. There are also various levels of documentation needed to support the project implementation. As I recall, there are 'repairs' and 'alterations.' They're also divided into 'major' and 'minor' classifications. Minor alternations are those that do not change performance of the airplane. This generally defined as less than 1 pound difference in empty weight of the aircraft (hence no change to w/b). No changes needed to the pilot's operating handbook. No alterations to any structural component of the airframe (like holes thru a spar). The proposed swap from manual battery switch to battery contactor could certainly fall in the minor category (unless you want to drill the spar carrythru to mount the contactor!) Check with your local FAA certified talent but waaayyy back when, I believe such a change could be accomplished with a log book entry by an appropriately qualified practitioner. No 337 necessary. Bob . . . //// (o o) ===========o00o=(_)=o00o======== < Go ahead, make my day . . . > < show me where I'm wrong. > ================================ In the interest of creative evolution of the-best-we-know-how-to-do based on physics and good practice.


    Message 4


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    Time: 12:50:30 PM PST US
    Subject: Re: Switch Question
    From: "farmrjohn" <faithvineyard@yahoo.com>
    Here is the original wiring diagram from the Alon maintenance manual (if I successfully added the attachment). The wiring has changed with the addition of an alternator in place of a battery. The circuit for field "F" on the regulator now comes via the alternator rather than the top pole of the switch as depicted. Looking at the current definition for minor alteration the question is does the addition of a contractor constitute a change to the basic design of the system. My IA and myself don't think so but I'm a bit concerned looking forward to a pre-sale inspection and the buyer's inspector thinking otherwise. A 337 field approval should eliminate any doubt in that case. John Read this topic online here: http://forums.matronics.com/viewtopic.php?p=512791#512791 Attachments: http://forums.matronics.com//files/aircoupe_electrical_system_213.pdf


    Message 5


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    Time: 04:03:20 PM PST US
    From: "Robert L. Nuckolls, III" <nuckolls.bob@aeroelectric.com>
    Subject: Re: Switch Question
    At 02:49 PM 12/15/2023, you wrote: > >Here is the original wiring diagram from the Alon maintenance manual >(if I successfully added the attachment). The wiring has changed >with the addition of an alternator in place of a battery. The >circuit for field "F" on the regulator now comes via the alternator >rather than the top pole of the switch as depicted. That's an architecture 'cartoon' common to most pilot's operating handbook for light aircraft. Drew up lots of them at Cessna. 'Approved data' would be from any 'hammer-n-tongs' document. At Cessna, our factory wirebook drawings were published in the maintenance manuals. Aircraft of this era may not have enjoyed this kind of documentation. I only have first hand knowledge of Beech, Cessna and Lear . . . places I've worked. That airplane may not ever have been graced with a factory battery contactor installation. It just means you don't have an 'approved' factory document . . . doesn't mean the drawing you attach to your 337 would not be approved. An alternator swap would always require a 337; it changes weight and balance and might be need to be tested for adequate cooling at best angle of climb (depending on mood of the approving authority). Swapping a switch for a contactor is zero risk and doesn't impact performance, w/b or operating instructions i.e. MINOR . . . no change of functionality. >Looking at the current definition for minor alteration the question >is does the addition of a contractor constitute a change to the >basic design of the system. My IA and myself don't think so but I'm >a bit concerned looking forward to a pre-sale inspection and the >buyer's inspector thinking otherwise. A 337 field approval should >eliminate any doubt in that case. John You're asking 'hair dressers' about 'heart surgery'. The authority resides with the individual who signs off the installation. If uncertain, that individual should/would consult with the local FSDO. A 337 adds to the FSDO workload . . . the gotta file the thing. Have your IA check it out with them . . . THEY are the 'surgeons'. Bob . . . //// (o o) ===========o00o=(_)=o00o======== < Go ahead, make my day . . . > < show me where I'm wrong. > ================================ In the interest of creative evolution of the-best-we-know-how-to-do based on physics and good practice.




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