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4 May 10

Intake51.JPG (1571410 bytes) The new Bowers ram air is installed.  I had to trim the intake step down tubing dramatically to make it fit with the cowling.  I rounded the metal edges and polished them.  Rod enlarged the filtered air reed valve openings and that should improve MP when using filtered air. Intake52.JPG (1571982 bytes)

 

ACS did a poor job for the first time in a long time.  I ordered spark plugs from them and they still have not arrived.

I discovered the reason for the static on the intercom and got it corrected.  The headset jack had vibrated loose and was grounding to the airframe.

I finally got the right cabin cover removed after one of the mounting screws stripped out.  I bought a screw extractor, but it broke off.  It did get the screw loosened by 1/2 turn and that was all I needed.  I kept working it by cutting deeper slots in it and using a screwdriver to gradually work it out.

After getting the cover off, I removed the forward baggage floor to allow access to the brake reservoirs.  The left brake is weak so I'm going to bleed it.

And I checked the Schottky diode and it appears to be functioning correctly.  So, now I need to rewire the diode and test it again.  This time I'm going to leave the cover off until I get it working right.

 

5 May 10

Lots done today.  But, Aircraft Spruce still has not delivered the spark plugs.

Got the OAT for the EFIS Lite installed.  The TAS and winds have not been working, so I decided to install the OAT while the airplane is down.

Also, filled the brakes.  The weak left brake was because the reservoir was empty.  The right side was almost empty, too.  They are topped up again and strong - but I have no idea where the fluid leaked out.  The lines and fittings are all clean.  I'll watch them more closely in the future.

I got the Schottky diode reversed and all indications are now normal.  I can power the standby bus using only the standby battery and the main battery will also feed the standby.  The reverse flow is stopped unless the bus tie is used.  So, just they way I'd intended. Schottky04.JPG (1567196 bytes)

 

As soon as the plugs arrive, I'll install them, put the cowlings back on, and go test fly with the new plugs and 39 degree advance on the P Mags.  I've been running 35 degree advance, but talked to Brad at E Mag Air and he said there's no reason to not run at 39 degrees advance.

 

8 May 10        Today - 1.9        Total - 78.8        Fuel - 29.4    L - 15.6    R - 13.8    FC - 34.9    Adj to 710

First flight since SnF and the missing screw in the intake.  No MP change or improvement with the larger ram air intake.

Today's plan

    Check fuel consumption and change FF

    Do a high speed pass at Wade Skelton's house

    Watch EGT/CHT for change due to timing and air dam changes

    Monitor Standby voltage for 14v

    Do TAS runs

    Check TAS and winds on EFIS Lite

    Check Brakes

    Try flying only AOA on final

    Try EFIS checklists

    Enter and fly RNAV approach

    Check VOR reception

    Check G indications on EFIS 1 and Lite

    Check P Mag for min RPM for operation

Had a fouled plug on the right P Mag so had to run the engine to burn it clean.  Then, the airplane just didn't seem to be performing normally after takeoff, so I stayed in the pattern for 3 passes to make sure it was going to run okay.

Before too long, the EFIS One indicated and overheat situation.  Looks like I'll need to add an avionics fan to blow on the EFIS.  Couldn't get the AP to work well - possibly because the EFIS was overheating.  It would hold altitude - sort of - but heading hold would not capture.  It tracked the GPS fairly well after it cooled down.

Did several high speed passes at Wade Skelton's house but had to slow down after that because the rubber channel at the right wing root came loose and was slapping against the fuselage.

The static problem reappeared after I thought I'd solved it - so more work to do.

The fuel consumption did not match with the fuel computer, so I'm wondering what's going on.  It was farther apart than last time.

The EGTs look no different, but the CHTs are higher.  I made two changes that may affect the CHTs.  First I changed the max timing advance on the P Mags from 35 degrees BTDC to 39 degrees.  In theory, that should make the temps drop a bit.  I also added a bit of metal tape to the #1 and #2 cylinders air dams to bring the CHTs closer together.  It'll take a few more flights to gather enough info, but it appears the CHTs are higher across all the cylinders when other variables such as OAT, RPM, MP and FF are are matched up with earlier engine readings.

The standby buss voltage settled at 13.8 and stayed there all day, so it looks like the electrical system is finally working as designed.

After connecting the EFIS Lite OAT, I should have had valid TAS and wind indications on the EFIS Lite.  The TAS indications were well off the mark, but the wind readout appeared to be reasonably close and steady - much better than the EFIS One.  EFIS Lite 126 KIAS/119 KTAS while EFIS One was 126 KIAS and 131 KTAS.  EFIS One had no wind readout and EFIS Lite indicated 241/33.

The brakes are solid once again.

The AFS 3400 checklist pages are not usable.  The font is tiny and unreadable with any turbulence at all.

Tried a VOR approach using Virtual VOR on the EFIS One, but result was not conclusive.  I need to better understand the EFIS.  SL30 was getting a good VOR signal, but it would not display on the EFIS.

I forgot to check the EFIS G meters and the P Mags at shutdown.  I need to turn off power to the P Mags and see at what RPM the engine dies.  That tells me the RPM at which the internal P Mag generator will stop producing power.

Overall, good to get airborne again, but frustrations with several issues.

TAS Calcs indicate winds were 250/13 and TAS was 131.  So, if I can correct the EFIS Lite OAT measurements, the E Lite winds and TAS may get reasonably close to accurate.

Engine Readings

OAT RPM MP FF OilP OilT 1 2 3 4
71 2469 23.7 13.3 80 179 EGT 1373 1341 1370 1286
CHT 338 379 383 356
OAT RPM MP FF OilP OilT 1 2 3 4
71 2470 23.7 11.2 79 179 EGT 1463 1383 1449 1368
CHT 332 373 377 353

 

10 May 10        Today - 0.9        Total - 80.5

Took Wade Skelton (SWA pilot and RV-8 builder) for flight from his grass strip.  My first landing and takeoff on a grass strip in this RV.  The nose gear handled it fine.  I kept the stick full aft.  Airplane sure gets dirty - I'm glad I don't have to operate on a grass strip all the time.  I had to fly over and clear off the deer before landing.

The radio/intercom static wasn't so mysterious after all.  I thought through what I might have changed recently and discovered that I had selected the nav radio ident feature and was getting static from it.

Somehow I have some binding on the control cable for the ram air, so I'll need to work on it.

Iridium01.JPG (1644529 bytes) The NGK Iridium plugs finally arrived.

Right shows the fine 3mm electrode

Now if I could only remove the old plugs from the adapters

Iridium02.JPG (1618676 bytes)

 

11 May 10        Today - 1.0        Total - 81.5

Freed up the ram air cable, but it has started binding again, so there's more to the story.  I'll pull the cowling when I get back from DAL.

Flew an ILS to KDAB and the GS was intermittently jumpy.  May have been an airplane on the ground interrupting the signal.

I did a max power run at 1000' and got a rather disappointing 184 KIAS.  I didn't have the mixture leaned quite enough and the OAT was about 76 and it was very rough air - still it should have gone faster.  Also flew more TAS check runs.  The EFIS One TAS readings are accurate within 1 knot.  The EFIS Lite TAS is still way off, so I'm guessing the OAT needs adjustment - or maybe it's not getting power.  I'll check the power and check it with a thermometer.  The EFIS Lite wind calcs may be accurate once I get the TAS corrected.  The EFIS One winds are out to lunch.

Also, lately the EFIS One Mag heading has been slow to come up.  I'm not sure what's going on there.  I'll check the connections.

Judging from the new engine readings, the changes I made to the engine have raised the CHTs.  Compared to previous readings, the latest CHTs are much higher.  The changes were to change the left mag (top plugs) to a 39 degree advance (other one is still at 35 degrees) and adding some metal tape to the aid dams to block some cooling air.  The tape was intended to even up the temps, but it brought the #2 temp all the way up to match #3 - the highest one.  It's hard to know which change made the most effect, but I suspect it was the timing change.  I'll remove the tape next time and compare the temps again.

Engine Readings

OAT RPM MP FF OilP OilT 1 2 3 4
76 2675 28.9 17.8 82 173 EGT 1377 1349 1375 1301
CHT 359 383 395 356
OAT RPM MP FF OilP OilT 1 2 3 4
71 2498 25.2 13.7 81 178 EGT 1425 1403 1424 1336
CHT 325 362 362 332
OAT RPM MP FF OilP OilT 1 2 3 4
71 2496 25.2 13.7 81 176 EGT 1427 1404 1425 1338
CHT 326 363 363 334
OAT RPM MP FF OilP OilT 1 2 3 4
70 2397 24.5 12.6 81 176 EGT 1388 1362 1380 1298
CHT 316 356 355 326
OAT RPM MP FF OilP OilT 1 2 3 4
71 2400 24.3 11.5 81 176 EGT 1461 1434 1458 1364
CHT 316 351 355 327
OAT RPM MP FF OilP OilT 1 2 3 4
75 2423 27.3 13.3 81 179 EGT 1454 1429 1449 1361
CHT 325 363 366 336

 

18 May 10        Today - 0.9        Total - 82.4        Added 1 Qt oil

I'd promised a flight to a local HS kid and today we did the flight.  It turns out this kid is as natural a pilot as I've seen.  He's as natural a pilot as my son - and that is really saying something.  It was his first ever flight and he was completely at ease in the air.  I could easily talk him through maneuvers - even aileron rolls and loops.  So, we'll have to do more flights later.

 

22 May 10        Today - 1.6        Total - 84.8        22.1 Gal    11.3 L    10.8 R    FC - 25.3

Flew to Tampa today for the EAA meeting.  Ran at 24 square and indicated 150 and trued 170.  The fuel computer is still not reading correctly - it indicated 25.3 after refilling with 22.1 gallons.  So, I have to analyze what is going on with it.

Exhaust18.JPG (1458576 bytes) I put some heat resistant tape on the engine mount where the exhaust pipe has been rubbing.  The tape was gone and the wear spot was much worse when I returned.  I've grounded the airplane until I have a solution.  I think I'm going to have to get a welder to add a sleeve to the tube to add back in the strength.  I'm hoping I don't have to pull the engine to do the welding.  I'm also going to work with the exhaust maker (Larry Vetterman) to come up with something that will work without rubbing. Exhaust19.JPG (1081896 bytes)

Engine Readings - it is apparent that at a given RPM, MP and FF, all EGTs are lower and all CHTs are higher with the new 39 degree advance on the P Mags.  The most significant change is the increased CHT on cylinder #2.

OAT RPM MP FF OilP OilT 1 2 3 4
71 2458 24.1 12.3 80 176 EGT 1479 1401 1479 1393
CHT 320 343 361 336
OAT RPM MP FF OilP OilT 1 2 3 4
70 2400 23.9 11.7 80 175 EGT 1474 1396 1476 1391
CHT 312 335 355 330
OAT RPM MP FF OilP OilT 1 2 3 4
74 2404 22.8 10.6 83 179 EGT 1453 1424 1437 1356
CHT 322 360 366 338
OAT RPM MP FF OilP OilT 1 2 3 4
75 2406 23.9 11.3 81 177 EGT 1491 1406 1486 1402
CHT 310 335 354 330
OAT RPM MP FF OilP OilT 1 2 3 4
75 2410 23.8 10.6 81 176 EGT 1455 1383 1457 1372
CHT 297 321 341 320
OAT RPM MP FF OilP OilT 1 2 3 4
78 2410 27.8 12.4 81.2 179 EGT 1498 1421 1489 1407
CHT 311 340 356 332

 

31 May 10

OilCoolerAirDeflector.JPG (1588911 bytes) The firewall behind the oil cooler has been getting very hot due to hot exhaust air from the cooler, so I decided to make an aluminum ramp to keep the firewall and associated wiring cooler.  It took a while to get the shape right, but it finally fit and looks like it will work.  It may cause a rise in the oil temp because of restricted air flow due to less exit area.  But, I'll check it out when I fly next and if it gets too hot, I'll trim away the ramp until the temps are good again.
Also got a sniffle valve from Air Flow Performance and installed it with an aluminum drainage tube.  I didn't add a clamp to support the tube, but it is very short and feels solid using only the B nut to hold it.  If I find it moves too much, I'll add some support. SniffleValve.JPG (1547403 bytes)