- 13.4.3 Pitot Tube Installation
- 13.4.2 Static Port
- 13.2.1 Instrument Panel Mounting
- 13.3.2 Ground Power Plug
- 13.0 Electrical System Documentation
- 13.0 Wire Labels
- 13.2.2 / 13.6.2 Aft wiring complete
- 13.8.1 Magnetometer connections
- 13.9.2 Autopilot Roll Servo Wire Routing Modification
- 13.7.1 Avionics Shelf
- 13.8.1 Magnetometer Mounting Bracket – Completed
- 13.8.1 Magentometer Bracket
- 13.1.6 Transponder Antenna Ground Plane
- 13.5.1 Navigation/Strobe Wing Root Connectors
- 13.0 Electrons are flowing
- 13.9.2 Autopilot Roll Servo Mounting
- 13.3.4 Overhead Switch Panel Wiring
- 13.2.2 Engine Wiring
- 13.6.2 Primary Alternator Connection
- 13.7.1 Avionics Shelf
- 13.8.1 OAT probe
- 13.2.2 EIS wiring
- 13.2 EFIS and Instrument Panel Layout
- 13.6 Ground Block – Part II
- 13.7.4 Headset jacks
- 13.3.4 Overhead Switch Panel
- 13.6 Ground blocks
- 13.8.2 Annunicator Panel
- 13.8.2 Annunicator Panel
- 13.8.2 Annunicator Panel
- 13.6 Electrical supply lines
- 13.6.3 Ground Power Receptacle
- 13.2 Instrument Panel Layout
- 13.3.5 Avionics Wiring
- 13.9.2 Auto Pilot Pitch Servo Mounting
- 13.7 Avionics and Wiring
- 13.7 Wiring
- 13.2 Panel painting
- 13.2 Panel installation
- 12.3.5 Minor setback on Avionics wiring
- 13.8.2 Annunciator Panel Problem
- 13.1.9 ELT Installation
- 13.6 Power Supply
- 13.7.4 It’s always something…
- 13.0 Wire routing
- 13.1.8 GPS Antenna Shelf
- 13.7.4 Audio Panel Relocation
- 13.0 Wire Routing (Remediation)
- 13.6.1 Battery Hold-Down
- 13.2.1 Instrument Panel – Final Install
- 13.3.3 / 13.5.3 Trim & Landing Light Test
- 13.8.1 EFIS alternate power
- 13.5.2 Cabin Lighting
- 13.1.4 Glideslope Antenna
- 13.3.4 Overhead Switch Panel
- 13.99 Instrument Panel overlays
- 13.99 Installing Engraved parts
- 13.99 Instrument Panel Lighting
- 13.4 Pitot/Static Remediation
- Static Port Conundrum
- GPS Replacement
- Secondary EFIS Power
- 13.99 Electrical System Diagram
- 13.99 – Current Sensor Repair
- 13.99 – ADS-B in antenna
- 13.99 – Switch panel update
- 13.4 – More Static Port Fun
Prior to having the airworthiness inspection done, I was planning on getting the pitot/static/transponder check done. Friend and fellow builder Bob (who’s V-twin had a first flight 2 days after mine!) suggested checking the system for leaks prior to the check.
When I checked, it leaked like a sieve. Couldn’t hold the altitude and airspeed for less than a second. I pulled the panel (no small feat) and tightened all the fittings and still leaked. I isolated parts of the system and still had leaks. Spent a whole day trying to fix this and had to cancel the test, reassemble everything for the inspection, and come up with a plan B (actually, Plan A since the current system is a Plan B).
This brings us to our lesson for the day. When learning to fly, you’re told that when a loss of power occurs, that you select a suitable landing spot (within gliding range) and stick with it! Too often, as people descend, they see another spot that looks much better. But when they try to make that spot, they run out of altitude. Now obviously, there are exceptions. But the idea of “Make a plan and stick to it” has merit.
This also applies to building. With the pitot/static plumbing, I researched all the different choices for tubing and fittings. What I decided on was “quick connect” system sold by SteinAir. I came across these when I was looking for a alternate static valve that had a toggle switch control. The parts weren’t the cheapest (at least I thought), but it looked like a good choice.
Then someone told me that you can get “the exact” same type of fittings from Home Depot. Early on, I made the decision not to use non-aviation parts unless I was absolutely certain that it either didn’t impact safety or that I could determine that the part was as good or better than the traditional aviation grade part. I could not make that determination with the Home Depot grade parts so that idea was dismissed.
Then I heard “Why are you going to use those fancy, expensive parts? Cessna, Piper, Beech have been using plain old NyloSeal parts for years and they work just fine.” Well, I didn’t have a good answer for that. So I ordered a bunch of NyloSeal fittings and tubing from Aircraft Spruce. I mean, if it’s been working for everyone else, right?
Before ordering, I drew up a diagram:
Once all the parts were in, I hooked everything up and secured the fittings and tubing where necessary.
Here’s a picture after I installed the tubing and put the panel in place. The arrows are pointing a various tubes and fittings.
Not the prettiest installation, but it’s behind the panel and with all those fittings, there’s only so much you can do.
Once I discovered that the system was leaking and I couldn’t get it to not leak, I decided to go back to my original plan.
So I made up a new diagram. In the process, I decided to eliminate the “test points” in the system. I had asked the shop that’s been doing the pitot/static checks on the Cessna about what they like to see in a pitot/static system and he told me “test points so I don’t have to tap into a line.” But it occurred to me that a single test point adds three connections to the system. After I redesigned the system, for the new hardware, between eliminating the test points and having a 5-port manifolds, I reduced the number of connections from 44 to 28.
I also used the “banjo” elbows for attaching to the static ports on the sides of the fuselage. These fittings are very low profile which means that the interior trim will fit closer to the fuselage. Here’s a picture of a standard elbow (left) and the “banjo” elbow (right). Oh yeah, another huge benefit is that both elbows are full 360 degree swivel. Which means you don’t have to worry about “clocking” the fittings to get them pointed in the right direction.
The end result is a much neater installation that had no leaks. I also used red tubing for the pitot side and clear tubing for the static side to make it easier to identify the two different lines.
This is what I removed.