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Here are some results
from my flight test last week.
Matt
FLIGHT TEST DATA |
| Aircraft N# ___366B______ |
Model ____360________ |
Date of flight _____12/22______ |
Time off _8:30AM___ |
Time on _11:15 AM |
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Test I |
Test 2 |
Test 3 |
Test 4 |
Test 5 |
Test 6 |
| Indicated altitude |
8000 |
8000 |
9000 |
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| Pressure altitude |
7610 |
7610 |
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| Density altitude |
8320 |
8320 |
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| OAT |
2 C |
2 C |
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| MAP (Not Nec. WOT) |
23.0 |
22.0 |
22.0 |
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| RPM |
2400 |
2400 |
2400 |
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| Fuel flow (gph) |
8.8 |
8.1 |
8.2 |
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| EGT range (100 LOP) |
1320 - 1440 |
1330 - 1420 |
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| CHT range |
270 - 298 |
270 - 295 |
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| Knots calibrated airspeed |
182 |
177 |
177 |
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| Knots true airspeed |
203 |
199 |
204 |
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| Turbulence |
smooth air |
smooth air |
smooth air |
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| -----Original Message-----
From: Lancair Mailing List
[mailto:lml@lancaironline.net]On Behalf Of Metcalfe, Lee,
AIR
Sent: Wednesday, December 22, 2004 12:39 PM
To: Lancair
Mailing List
Subject: [LML] Re: airspeed vs.
power
Looks
like a lot of us are goofing off today!?!? Here's a spreadsheet I just
did to capture data for the GFTP (Grayhawk Flight Test
Protocol).
Moondog
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