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RFguy

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Everything posted by RFguy

  1. RFguy
    Starter pulls about 150A at 10V for a 3300 with good compressions. at oil and engine cold @ 18 degC.
  2. RFguy
    yeah but you didnt give those in the same post, you had different posts with different things in them ! still, overall sounds like good performance.
  3. RFguy
    it's a good video.... Looks bad for Continental, good for Lycoming. and less than ideal for continental company behaviour.
  4. RFguy
    And , a fully charged , unloaded (but not on the charger) 12V lead acid AGM battery at 50 deg C would read about 12.15V where as at 25 deg C would read 12.6V Any attempt to charge it at high temperature, with a non temperature compensated charger would very much overcharge it
  5. RFguy
    Well... you mentioned "23.3 in". was that manifold pressure , or just the pressure altitude ?
  6. RFguy
    ahh so that's wide open throttle then (IE manifold pressure is approx same as (static) air pressure) ? or is that Manifold pressure gauge ? .
  7. RFguy
    Jabs are air flow forward facing and jabs dont have any problems with their fuel delivery.
  8. RFguy
    What type of battery is it and what is the terminal voltage ?? If it has not been below 10.5V for any sustained period (weeks) , its probably fine. a footnote- those deciding on battery location, consider heavy FRP non conductive cover over the terminals- consider what might happen in an accident and have say, an aluminium panel or member squash onto the battery terminals. Now you have a fire. I have seen MANY experimental aircraft have this flaw (in my opinion) , and some factory 24- aircraft.
  9. RFguy
    https://www.recreationalflying.com/topic/38878-jab-down-chinchilla-airport-260223/?do=findComment&comment=542249&_rid=11148 " the seatbelt wad torn from the fuselage and a hole remains where it was bolted in. "
  10. RFguy
    Dont get too wound up about the exact flapped stall speed, measuring airspeed accurately at high AoAs is difficult ... (not to mention dependence of AUW weight, CoG location, ) Sounds good Skip, at least writing it out here can provoke your brain a bit as your write. My observation is that flaps on some aircraft dont really change stall speed much , more used to increase decent rate and increase drag and tweak the attitude a bit. There are others here that can offer far more. Which way is the aft trim required at 'high speed cruise' ?
  11. RFguy
    arm yourself with a good stethoscope (1.5m length of soft silicone (or not too hard PVC ) tubing jammed into your ear hole) (note that's EAR hole) and some soapy water (cylinder -head interface leaks / intake gasket/exhaust couplings - Jabiru)
  12. RFguy
    being a 19- experimental aircraft with you as the builder affords you a high degree of flexibility in ways to kill yourself of course. That is the big plus of 19- changing the reflex / static pos of any of the control surfaces (aielerons) or high lift devices (flaps) will have a relatively big change to stall characteristics, all types of provoked stalls of course. If you have plenty of altitude, I'd suggest you write up a good barrage of repeatable stall testing . That thing has a big rudder and you wont load it tail heavy so recovery with correct technique and altitude is likely. There WOULD BE a flight test regime from the manufacturer. Maybe test against that ?
  13. RFguy
    My observations are there is a fair spread of leakdown results in the manner at which they are done. They can can be certainly made to look good, so best (most applicable) method as as described in the relevant engine manual from the manufacturer. Depending on the ailment, some will be worse just before or just after TDC (maybe ring related) , some will be worse static at TDC (maybe valve related) . some will be worse during rocking the crankshaft around TDC (maybe ring related) , there are other variations (cylinder -head interface leaks etc, cracks etc) AND COMBINATIONS !
  14. RFguy
    Oh yeah . I see .I didnt see those other pictures. my bad I see someone has stuck it into a db https://aviation-safety.net/wikibase/308770 Jabiru are going to have to do something about seat belt anchors failing, that's another I have heard about from a factory aircraft. *unacceptable*
  15. RFguy
    and for logbooks and maintenance, convention (and you really do want to stick to convention for such a critical engine health vital sign) is to write down the figure of the two gauges in psi. The type with a % gauge requires assumptions and assumptions are no good.... Buy the one used by aircraft technicians, has correct orifice, and correct gauging.
  16. RFguy
    jesus.... Barto, was it a 'LSA55 ? hopefully there will be an investigation and AD on the seatbelt restraints. -glen
  17. RFguy
    Then.... by the book, the pilot would be charged with manslaughter whether he was licensed & current, and the aircraft was maintained per rules ..or not. ----Since it meets the definition , purely and simply of manslaughter. Now, what actually happens in a court - the reckless attitude will not help him defend this charge.
  18. RFguy
    this one looks like a good option May be available locally , also. https://www.aircraftspruce.com/categories/building_materials/bm/menus/to/test_cylinders.html I have one of these https://www.aircraftspruce.com/catalog/topages/diffpresse3m.php I see they have one with the rotax plug thread https://www.aircraftspruce.com/catalog/topages/diffpress12mm.php
  19. RFguy
    The ATSB report has a fair chunk of info in it.
  20. RFguy
    I dont agree that the UBER example is relevant to this. The airplane SHOULD have had EXPERIMENTAL plastered everywhere,. Maybe the manslaughter charge is just pressure to get a plead of guity on everything else.
  21. RFguy
    The manslaughter wont get up. it wasnt charter, pax tasks own risk in light airplane. The CASA admin charges will get up and they will throw the book at him.. aggrevated. he'll have to plead guity to all of them , since there is no contest.
  22. RFguy
    mmm. I'd like you to locate the regulator, unplug from the harness , physically inspect the connector in situ, and replug it in snug. Also is your engine a Gen4 with the CB in series with the alternator stator ? anyway, buy a spare breaker . carry it . take a look at the wiring- make sure all plugs for instruments panel pushed home. Could be a bit of equipment got an overvoltage and decided to crowbar (puts a short on the bus) , maybe something not right in the regulator/alternator wiring.
  23. RFguy
    There is no such thing as random for this . The total load all active should not trip the breaker. When you say just after startup- was this as you increased RPM so the battery voltage began to rise as the battery began to take charge ? Or before you went over 1500 RPM ? Roscoe, take a good look with glasses on and lots of light at the wiring you can see. Change the circuit breaker. See if it occurs again.
  24. RFguy
    The Jabiru passenger cell looks intact. As usual, the Jabiru airframe looks after the pax . Jabiru should use this in marketing. Everything breaks off around you but the pax cell seems to hold together. This is a very good result IMO. I would like a four point harness though.
  25. RFguy
    Good result if pax are in stable condition . Cannot see fuel vents so likely is inboard tank variety. Jabs rarely have fuel delivery issues (good design) and shouldnt have vapour issue with pump on, so something else. Wasnt particularly hot at AP at 0930 local (24C) http://www.bom.gov.au/products/IDQ60801/IDQ60801.99402.shtml
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