Re: ELT installation
I used to sell airplane parts in Anchorage about 10 years ago and we brought in the Ameri-king elt's because of the D battery option....and they were JUNK, every one that we had in stock had cracks around the screw holes. An FAA inspector from FSDO had bought one for his personal airplane and he brought it back because the advertised voice transmit capability did not work. After trying 4 more, we gave him his money back. You get what you pay for when it comes to ELT's. The D batteries used must also have the manufacturers expiration date to be useable.....If you are doing a new installation, you MUST have the remote capability to turn it on. Whether its with the switch or the ELT itsself. Another little side note, if you install it, you now have to test the structure for the mount to make sure that it does not deflect the airframe more than .030" with about 100lbs of static pressure. My numbers maybe wrong but I think that I am in the right ballpark. There is also a stipulation that it cannot be mounted to the fuselage skin. We had this training in the IA seminar last march from the Fairbanks FSDO.
here is a link for the FAA's powerpoint presentation....
http://www.faa.gov/about/office_org/...t#263,8,SEARCH OF THE REGULATIONS:
I used to sell airplane parts in Anchorage about 10 years ago and we brought in the Ameri-king elt's because of the D battery option....and they were JUNK, every one that we had in stock had cracks around the screw holes. An FAA inspector from FSDO had bought one for his personal airplane and he brought it back because the advertised voice transmit capability did not work. After trying 4 more, we gave him his money back. You get what you pay for when it comes to ELT's. The D batteries used must also have the manufacturers expiration date to be useable.....If you are doing a new installation, you MUST have the remote capability to turn it on. Whether its with the switch or the ELT itsself. Another little side note, if you install it, you now have to test the structure for the mount to make sure that it does not deflect the airframe more than .030" with about 100lbs of static pressure. My numbers maybe wrong but I think that I am in the right ballpark. There is also a stipulation that it cannot be mounted to the fuselage skin. We had this training in the IA seminar last march from the Fairbanks FSDO.
here is a link for the FAA's powerpoint presentation....
http://www.faa.gov/about/office_org/...t#263,8,SEARCH OF THE REGULATIONS:
Comment