07 February 2021

Test Flight 5



Test Flight: 5

Date: Saturday February 6th 2021

Hobbs Start: 6.7 Hobbs End: 8.1

Description: A shorter flight than the previous trying to get back before the gusting cross-wind picked up into the 20s (I made it back when it was still 10kt right cross). With a little more trust in the autopilot, flew most of the flight via the Garmin. 1) I was able to get a nice slow mixture lean in order to gather another set of data before I start swapping on injector sizes. 2) I got some decent numbers at 4500 for 60% power LOP and 75% power ROP. I wanted to grab those numbers because I am going to start putting the wheel pants on. 3) I finally remembered to calibrate the pitch offset on the PFD. 4) I calibrated two of the AoA settings (viewable and caution). The controllers were busy all around, good job guys.

Objectives: Fuel topoff, preflight and run-up of the aircraft, normal take off with 0 degree flaps, depart the pattern for engine break in, auto pilot deployment, engine leaning data gathering, pitch offset calibration, AoA calibration, return to base, normal full flap landing.

Airplane Start Condition: 60 gallons of fuel, 9 qts of oil as read on the dip stick, 50lbs of ballast in the baggage compartment, single pilot (150lbs)

Airplane End Condition: 39.4 gallons of fuel, 8.75 qts of oil as read on the dip stick (probably .25 on the belly), 50lbs of ballast in the baggage compartment, single pilot (150lbs)

Test Flight Track Log:

Pilot Notes:
  1. Autopilot was pretty rock solid. Heading, Nav, Alt, IAS, VS mode all functioned well
  2. AoA calibration will need to be dialed in more as well as the actual Stall run needs to be calibrated yet.
  3. 9qts of oil is still too much for that sump. A fair bit of oil on the belly and post flight checks verify that is all coming from the crank case vent.
  4. Heat vents are pretty difficult to push open (yes, I thought I was being smart and installed them as a push rather than pull to open). Once at airpseed, there may just be too much force to have this in a push configuration, it feels like it is going to bend the push pull cable. That said, heat works well.
  5. Left tank fuel vent is much better. I pulled it up further to the top of the tank as it was pissing fuel when the fuel trucks were filling to the bottom of the filler neck.
  6. There is an odd behavior with what I think is mono/stereo on the audio panel. Either my audio recording works and the "alert" noises have a little static, or my phone wont pick up the transmissions but the audio alerts sound perfect.
Open Squawks:
    1) COM2 breaking squelch on COM1 TX. COM2 sensitivity weaker than COM1. COM2 could use a ground plane.
      2) Need to set "Flight" vs "Ground" calibration on the fuel levels. 

      5) While the charging system is stable, I would still like to see if I can get the 0.2v differential out of the x-feed contactor. That is, my AUX bus when the alternator is on runs at a voltage 0.2v lower than MAIN. It is not that surprising given the number of connectors between the two busses. In order for the AUX battery to get alternator voltage it has to get through terminals on the MAIN contactor, X-FEED contactor, and then the AUX contactor. One or more of those terminal to terminal connections needs to be cleaned. 


      Verified Closed Squawks:
      N/A


      02 February 2021

      Pilot Operating Handbook



      The complete handbook (living document) is on google drive and can be found at the following location: N5412K - PoH

      Vy Calibration Runs (Sawtooth Climb Performance)


      While this is not complete data by any means, this session allowed me to get used to the procedure while at the same time not getting bored just running around in cruise circles. I need to repeat this session with 0 degree flaps as soon as I get the wheel pants on. Also, yes, I do have an EFIS that is recording at 1Hz and the abbreviated method of this calculation would be faster. That said, I am in Phase I and I am taking into account that it benefits me to learn the plane while still close to the airport, so longer procedures are not an issue. Calculations were based on this method. OAT was 6C at altitude and the airplane starting conditions had me weighing in at 2230lbs.

      I ended up doing x8 valid 60 second climbs dropping the indicated air speed 5 knots per run. I started with 120 KIAS and ended at 85 KIAS. I still need to take this down to 75 but I want to run the power on stall tests before going lower. The figure below shows the 8 runs (the first one I am removing from the data set because I forgot to set a timer). The top sawtooth graph is Autopilot IAS versus Indicated Altitude. The bottom graph is KIAS versus Vertical Speed. A reminder on Vx and Vy. Vx is the slowest (IAS), and is the Maximum ANGLE of climb.  It allows one to climb to altitude within the shortest horizontal distance. Vy is slightly faster, and is the Maximum RATE of climb. It allows one to climb to altitude in the shortest time.



      <todo: get the excel diagram output here>


      Below are the calculated angles as defined by Google Earth Pro: