All Activity

I'd refer you to AC 90-119. PBN, Performance Based Navigation. Read especially Chapter 12. AC_90-119_Coord_Copy.pdf

I believe WAAS also provides more accurate lateral guidance; not just vertical.

https://greenwayscc.com/blogs/articles/polymer-coating-or-ceramic-coating-which-is-right-for-your-car#:~:text=When it comes to durability,months%2C requiring reapplication more frequently.

I’ve actually wondered about this recently so…. I’ll be the dumb guy. Why would WAAS be required when vertical guidance is not consistent with a VOR approach?

The problem wasn’t that Lucas couldn’t make a good system it was the company’s using their product paid minimum pounds for the complete packages so corners had to be cut to remain profitable. Many formula one teams used their injection and ignition systems to great success during the sixties and seventies including one of the most successful engines in the sport the ford Cosworth DFV

Can a stand alone VOR (Not "or GPS") approach be completely flown using GPS as the primary source of navigation--especially on the final approach segment? Too many people either don't know the answer to that question, answer it incorrectly, or are confused by AIM 1-2-3 Notes (4) and (5). Careful reading of AIM 1-2-3 with support from AC 90-119 (draft) provides the answer. My intention is just to provide the answer without going into a long dissertation. The answer is a qualified, YES. Qualifications: 1. A WAAS RNAV system TSO'd under TSO-C129 capable of navigating the final approach segment. 2. The underlying VOR must be operational. Confusion arises by misinterpreting Note (4) in AIM 1-2-3. It states, "Pilots may not substitute (my highlight) for the NAVAID providing lateral guidance for the final approach segment). Note (5) says, "Use of a suitable RNAV system as a means to navigate on the final approach segment of an instrument approach procedure based on a VOR, TACAN, or NDB signal, is allowable. The underlying NAVAID must be operational and the NAVAID monitored for final segment course alignment". At first glance it appears that Notes (4) and (5) are contradictory. They are not. The critical word it SUBSTITUTE. Substitute in Note (4) means using GPS exclusively for the approach. Note (5) refers to using a "suitable navigation system" (for example a GTN 750) used in conjunction with the underlying VOR to run the approach. Thus a VOR approach can be run using "a suitable navigation system" (WAAS GPS certified under TSO-129) as the primary source of navigation as long as the underlying VOR is operational and monitored along the final approach segment with either a CDI or bearing pointer.

Fyi, software engineer here, if your getting nude or porn or sex store ads. It is NOT the site. it's YOU, lay off the porn and your search history. Destroying society anyway.

Yeah the real infestation happened over a few days in early August - then it was hundreds of topics being posted in just a few hours. Prior to that we had them here and there but nothing like that. Crazy thing is today I had a spammer register, pay the $2 fee for instant validation and then immediately make a bunch of spam posts. I'm expecting them to file for some kind of refund/chargeback through PayPal now. Hopefully that will not become the new problem...

Price?

As I understand it, ceramic waxes use silica (SiO2) in place of carnauba. SiO2 is a component of ceramics and hence the marketing term "ceramic" for these waxes. There are probably varying qualities of this stuff and it will be difficult to tell the difference from the marketing hype.

I can’t exactly remember where I got my mechanical fuel pump, but it was overhauled/exchanged. Maybe through Spruce or Aircraft Accessories? It was probably 2020, and it was always ~30-31psi on the ground - measured by an edm-930.

Al Jesmer at Precision Airmotive has stated that the RSA fuel injection servo works fine with input fuel pressures in the range of 20-35 psi. I have heard that at one point Lycoming was shipping fuel pumps that exceeded the 30 psi limit that Mooney put in the airframe limitations. However, the rebuilt IO-360-A3B6 that I got from Lycoming in late 2018 does not have this issue, so if it was a problem, Lycoming seems to have corrected it.

Form, fit, function...been around a while, especially with older aircraft....haven't heard on one instance where it's been an issue and neither has Cygnet with all the ones they have sold to Mooney drivers

Whatever these various coatings are, I doubt that they are "ceramic" as the term is genrally understood in material sciences. If I recall corectly, ceramics are generally mixtures of various inorganic minerals and water that are formed to desired shape and subsequently hardened by exposure to high temperatures. Most of the "ceramic coating" products that I looked at state that they are polymers which would indicate presence of organic compoounds, hence not ceramics. Marketing hype at its best . Notwithstanding the hype, some of the products do seem to provide good protection to automobiles and aircraft. I might try one of these to see.

As Scott mentioned above you may need to change the actual yoke (behind the panel). You will have to change the part that connects the forward portion of the two yoke shafts. The newer style (and I am referencing the Ovation parts which I used) have bronze bearings and are different from what is in the E. John Breda

Wow! That thing is thirsty! But I bet it screams!

YUP!

Interesting because I never saw them but if they were only for a couple of weeks - a couple of weeks ago -I may have been out of the country when it happened

No, 39”/2600rpm is max. Id guess the cruise settings are slightly higher hp to be 65% of 220hp rather than 210hp, but I doubt it’s much different.

I’m surprised nobody has pointed this out, so maybe there’s something I’m missing, but this has been happening on a lot of Mooneys. I thought we traced it down to a newer style/brand fuel pump that has a tendency to hit right at the max of 30 or just above it, especially on the ground. I know my F was doing that after we replaced the fuel pump. I guess what I’m saying is it’s probably correct, and it is not a problem. The fuel servo can take something like 40 to 60 psi. I think @PT20J has the specs that the engine can actually tolerate.

Engine: TSIO520NB (Rocket STC) ROP only so far, it tends to miss once every 10 to 30 seconds if I run LOP. Just need to spend some time investigating which cylinder is overly lean and adjusting it. I run at one of the following: 31" MP, 2,300 RPM @ 18.5 GPH (72%) 32" MP, 2,400 RPM @ 19.8 GPH. (76%) 33" MP, 2,400 RPM @ 21 GPH (78%) (Very rare) If I'm in a hurry or there are headwinds, I use the higher power settings. Otherwise the lower ones.

I knew your airplane was modified. I was curious to know if the added 10 HP changed the settings much compared to a stock 252. Is 36" your max MP to achieve the 220 hp?

They were in just about everything British: Morris, BSA, Norton, Triumph, MG, Jaguar, Rover, Mini, Austin, and probably a bunch of others.

To be clear, the problem recently solved by Craig was spam topics -- not spam adverts. Everybody got them whether they had paid their $10/year or not.

Ovations have split left/right switches for the taxi lights, and a split switch for the landing lights. So you can control each bulb in each wing separately. Is that what you want? If you ignore the labeling you could wire the split switch to be taxi and landing on one side. Schematic with p/n's below, plus pic of similar switch from interweb search