F
F
L
L
I
I
G
G
H
H
T
T
M
M
A
A
N
N
U
U
A
A
L
L
F
F
O
O
R
R
U
U
L
L
T
T
R
R
A
A
L
L
I
I
G
G
H
H
T
T
A
A
E
E
R
R
O
O
P
P
L
L
A
A
N
N
E
E
U
U
F
F
M
M
–
–
1
1
3
3
Date of Issue: 30. 1. 2008
3-1
3.1
Introduction
Section 3 provides checklist and amplified procedures for coping
with emergencies that may occur.
Emergencies caused by aeroplane or engine malfunctions are ex-
tremely rare if proper pre-flight inspections and maintenance are practised.
However, should an emergency arise, the basic guidelines de-
scribed in this section should be considered and applied as necessary to
correct the problem.
For best glide ratio, speeds and performance please see section 5.
performance.
3.2
Engine failure
3.2.1
Engine failure during take-off run
1. Throttle
- retard to idle
2. Ignition
- off
3.2.2
Engine failure immediately after take-off
1. Speed
- keep gliding speed at 100 km/h
- sinking rate cca. 1,25 m/s
2. Altitude
- below 50 m: land in take-off direction
-
over 50 m: choose landing area
3. Wind
- evaluate direction and velocity
4. Landing area
- choose free area without obstacles,
into wind
5. Flaperon
- extend as needed
6. Air brake
- extend as needed
7. Fuel valve
- off
Содержание UFM - 13 LAMBADA
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