Tecnam P-Mentor - Page 44

1
st
Edition - Rev. 0
Section 2 – LIMITATIONS
INSTRUMENTATION MARKINGS
P-Mentor – Aircraft Flight Manual Page 2 - 8
EASA Approved
4. Instrumentation Markings
Table 2-3 – Avionics System Instrument Markings
INSTRUMENT
RED
ARC/BAR
Minimum
limit
WHITE
ARC
Advisory
GREEN
ARC
Safe
operation
YELLOW
ARC
Caution
RED
ARC/BAR
Maximum
limit
Engine Speed
(0-6000)
RPM
/
/
1400 - 5500
< 1400
5500 - 5800
> 5800
Manifold Press.
(0.0-32.0)
In.Hg
/
/
0.0 – 32.0
/
/
Manifold Temp.
(0-70)
°C
/
/
0 - 60
/
> 60
Oil Press.
(0.0-8.0)
bar
< 0.8
/
2.0 - 5.0
0.8 - 2.0
5.0 - 7.0
> 7.0
Oil Temp.
(4-145)
°C
< 50
/
50 - 110
110 - 130
> 130
Coolant Temp.
(4 - 130)
°C
/
/
4 - 120
/
> 120
Exhaust gas
temp.
(540 - 982)
°C
/
/
≤ 950
/
> 950
Fuel Press.
(2.3 – 3.7)
bar
< 2.5
/
2.8 – 3.2
2.5 – 2.8
3.2 – 3.5
> 3.5
Fuel Qty
(0 – 65)
litres
0 - 1
/
15 – 65
< 15
/
gal
0.0 – 0.3
4 - 17.2
< 4
Alternator Amm.
(0 - 30)
A
/
/
0 – 30
/
/
Battery Amm.
(0 - 50)
A
/
0 – 50
/
/
/
Essential Bus Volt
(10.0 – 16.0)
V
< 11.9
/
11.9 – 14.5
14.5 – 15.5
>15.5
Lane A/B Volt
(8.0 – 15.5)
V
< 9
/
12.7 – 14.8
9 – 12.7
>14.8