Pilot´s Operating Handbook of ATEC 322 Faeta LSA with Rotax 912iS engine
ATEC v.o.s. Libice nad Cidlinou, Czech Republic
Page 28 of 56
5.1.
Introduction
The Chapter contents the information on speed indicator calibration, stalling speed and other
performances of the ATEC 322 FAETA with ROTAX 912 iS Sport engine and propeller FITI ECO
COMPETITION 2L/1680 mm adjusted to the pitch of 20°.
5.2.
Air Speed Indicator Corrections
CAS (kt)
IAS (kt)
Deviation (kt)
Note
35,8
32,8
-3
V
S0
45,0
42,7
-2,3
V
S1
50
48,6
-1,4
63
62,8
-0,2
V
F
70
71,1
+1,1
80
82,3
+2,3
90
93,6
+3,6
V
A
90
93,6
+3,6
100
104,7
+4,7
110
116,0
+6,0
120
127,2
+7,2
V
H
130
138,3
+8,3
136,1
145,2
+9,1
V
NE
150
160,7
+10,7
151,2
162,0
+10,8
V
D
5.3.
Stall Speed (CAS)
Engine idle
Flaps retracted
Flaps I (10°)
Flaps II (20°)
Flaps III (35°)
Solo flight
42,1 kt
39,7 kt
36,8 kt
34,0 kt
1285 lb
45 kt
41,3 kt
38,2 kt
35,8 kt
Engine off
Flaps retracted
Flaps I (10°)
Flaps II (20°)
Flaps III (35°)
Solo flight
42,1 kt
39,7 kt
36,8 kt
34,0 kt
1285 lb
45 kt
41,3 kt
38,2 kt
35,8 kt
