Flight Test Data			N727RH
				7/3/2004
CRUISE:
Altimeter			29.87
Weight			1509
Indicated			Full			???	Density
Altitude	OAT°C	MP	Throttle	RPM	KIAS	TAS	Altitude	FF
17000	-2.7		Y	2500	107	145.5	18963	7.2	(I do not plan to cruise at 2500 RPM, but was curious…)
17000	-2.7	15.1	Y	2400	102	138.7	18963	6.2
15000	1.9	16.7	Y	2400	117	154.4	16858	6.5
13000	4.8	18.1	Y	2400	125	160.0	14753	7.0
11000	7.9	19.5	Y	2400	134	166.2	12647	7.7
10000
9000
8000
7000	17.6	22.8	Y	2400	146	169.36	8878	8.8
6000	20.0	23.1	No	2400	144	164.16	7991	8.8	75% should have been corrected .17"per+10°F>ISA=3*.17=23.6"
									my estimate: 23.1"=72.5% power with OAT correction
									since manual shows 65%=21.1, 75%=23.1 (standard)
									thus I was .5" too low
CLIMB:
Alt.	Time	VSI	KIAS	MP	RPM	FF	OAT°C	Mixture
TO(400')	1543						28.0	Full Rich
3000	1546	700	90	25.0	2500	12.0		Full Rich
5000	1549	500	88	24.0	2500	12.0		Full Rich
7000	1551	500	85	22.2	2500	11.8		Full Rich
9000	1554	500	75	20.6	2500	11.6		Full Rich
10000	1556	500	75	20.0	2500	11.4	9.0	Full Rich
11000	1558	400	70	19.0	2500	11.2		Full Rich
12000	1600	400	68	18.2	2500	10.0		Leaned mixture
13000	1602	350	68	17.8	2500	9.8	3.2	Leaned mixture
14000	1604	350	68	16.8	2500	9.4	1.8	Leaned mixture
15000	1607	350	66	16.2	2500	9.0	0.0	Leaned mixture
16000	1610	250	65	15.5	2500		-1.4	Leaned mixture
16900	1613	200	62	15.0	2500			Leaned mixture
17000	1613:45	Level-off			2500		-3.3	Leaned mixture
WEIGHT:
			17,000'		T/O
EW			1196		1196
Pilot			185		185
Bags, O2			20		20
Fuel	Gallons	18	108	25	150
Total			1509		1551