STAll
SPEEDS·
POWER
IDLE
<f1
N
.I:lo
NOTES:
1.
THE MAXIMUM ALTITUDE LOSS EXPERIENCED WHILE CONDUCTING STALLS IN AC·
CORDANCE WITH FAR 23.201 WAS 400
FEET.
2.
MAXIMUM NOSE DOWN PITCH ATIITUDE
AND
ALTITUDE LOSS DURING RECOVERY
FROM
ONE ENGINE INOPERATIVE STALLS PER FAR 23.205 ARE
5'
AND 100 FEET RE·
SPECTIVELY.
3.
A NORMAL STALL RECOVERY TECHNIQUE MAY
BE
USED.
EXAMPLE:
WEIGHT
3&77
LBS
FLAPS
DOWN
(ON)
ANGLE OF BANK 30'
STALL SPEED
........................•....
64KTS lAS
62KTSCAS
~w
:t.a
0·-'
... 0
:I
::::I
I»
<
::::I
S
~
:
'.
...
.
"q'jt'[IJ1'1'1'1~""'"
1+1'"
.
.....
.
...
",':,:':'::.'.:::
-
...
- . .
_.
. .. -
lAS - INDICATED AIRSPEED . • .
:':'CAS
- CALIBRATED AIRSPEED
I
iii
I I , I ,
Iii
iii
I I
iii'
I
m···'·'·!-I
......
-4-
••••
~t:t.:.J:I~~:J.:l~+~
-I
••
-
d.,
.
+1=1+1+
.
FLAPS UP
w
~
I:
:~
0:
·Ih
'0:
90
5
60 2
I
~
(J)
70
~
Ii;
:li:t:tt:t.t:li-J:l:l:l:l:lttl:l±I±I:l
•..•...
Co.
I»
::::I
c:
I»
-<
....
~
eo
. FLAPS DOWN
(ON
llmITP='"
~
EEl:!:!:!...
•.•.•...•.
3&00
3600 3400 3200
WEIGHT
- POUNDS
m
3000
2600
o
10
20 30 40 50 60
ANGLE OF BANK - DEGREES
50
50
OJ
m
em
c 0
ox
:To
(i)::u
~
)-
~:!I
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