![]() |
If this is your first visit, be sure to check out the FAQ by clicking the link above. You may have to register before you can post: click the register link above to proceed. To start viewing messages, select the forum that you want to visit from the selection below. |
|
|
Thread Tools | Display Modes |
|
#1
|
|||
|
|||
![]()
I recently installed an EI FP5L fuel flow instrument in my Tri-Pacer. I
would notice that at irregular intervals, it would reset it self. I'd catch the green Remaining LED flashing as it does after a power on self test. I could never get it to fail in flight. I pulled and prodded all the wiring, replaced the circuit breaker, tapped on the instrument, etc etc. Talking to EI, the mentioned the possibility of RFI getting into the thing. I keyed the radio on all the frequencies that I normally use and again it didn't fail. Next I returned the instrument---you guessed it no defect found! Well when I got it back I hooked a battery charger to the plane and turned the master switch on and let it cook for a while. After a time of trying all different combinations of stuff turned on and off to try to make the fuel monitor reset, I finally found if the radio is keyed WITH the strobe on, bingo !! the fuel flow resets.!!!! The strobe is mounted on the vertical stabilizer. All grounds are run to a good common ground with the exception of the strobe which uses the airframe as a return. I haven't checked the SWR on the radio yet, but for the life of me I can't figure out why turning the strobe on makes the damn thing reset when keying the radio. Although it did it in the hangar, apparently this isn't 100% true in flight since the strobe is always on, and the thing resets intermittently. Anyone have an idea?? Thanks Paul N1431A |
#2
|
|||
|
|||
![]()
You have an RF leak from a com coaxial cable connector
somewhere. Probably a bad ground at the connector. This is a common problem with electronic voltage regulators, as they are sensitive to much smaller currents than mechanical regulators and will misread interference as an overvoltage condition, and will drop the alternator offline when the mike is keyed if there's any RF leakage. Look at the connector at the antenna. Condensation in the aircraft ceiling will corrode it. Dan |
#3
|
|||
|
|||
![]()
Does anybody have a clue what this feller is saying or why he is saying it?
Why would the cable connector itself be more likely to have a failure than a break in the coax shield itself? What does an electronic voltage regulator have to do with it? Why wouldn't it burp with straight RF rather than requiring the strobe to be on? My hit is that both the strobe AND the transmitter are getting into the engine analyzer, but neither of them of themselves are of a level to cause the problem. HOwever, added together they rise above the trigger point. I'd start looking at a way to put a filter on the A+ supply lead going from the battery bus to the analyzer and see if this doesn't cure the problem. Rat Shack sells "alternator whine filters" that may do the trick. At least they are inexpensive and an easy try. Jim wrote in message oups.com... You have an RF leak from a com coaxial cable connector somewhere. Probably a bad ground at the connector. This is a common problem with electronic voltage regulators, as they are sensitive to much smaller currents than mechanical regulators and will misread interference as an overvoltage condition, and will drop the alternator offline when the mike is keyed if there's any RF leakage. Look at the connector at the antenna. Condensation in the aircraft ceiling will corrode it. Dan |
#4
|
|||
|
|||
![]()
Ditto on what Jim said... it sounds like a conducted susceptiblity
problem, not a radiated susceptbility problem. That means that transient noise is conducting into the analyzer via the power lead and upsetting it, not via radio waves through the air. A decent PI filer should fix it, and the one that Jim mentioned is probably sufficient... Dean |
#5
|
|||
|
|||
![]() |
#6
|
|||
|
|||
![]()
Voltage dropout is a type of conducted susceptibility noise. The
length of the dropout determines whether it is just a transient, or a true brownout. Avionics systems are supposed to be able to handle short term dropouts associated with bus switching, etc. Maybe this one is poorly designed... Dean |
Thread Tools | |
Display Modes | |
|
|
![]() |
||||
Thread | Thread Starter | Forum | Replies | Last Post |
Heater problem fixed! | Jim Burns | Owning | 14 | December 17th 04 10:38 PM |
RF interference issue again (esp. for E Drucker and Jim Weir and other RF wizards) | Snowbird | Owning | 77 | December 3rd 03 09:10 PM |
Help with serious Glider Registration Problem | Soaring | 5 | November 12th 03 04:01 PM | |
EGT Problem | Dennis O'Connor | Owning | 4 | August 27th 03 04:25 PM |
Problem: Ground Speed Estimate with Volkslogger and WinPilot | RamyYanetz | Soaring | 3 | August 26th 03 03:06 PM |