Performance Data
CSP–520N–1
MD 520N (500N) ROTORCRAFT FLIGHT MANUAL
TM
Original
5–5
FAA Approved
20
18
16
14
12
10
8
6
4
2
0
–2
–40
–30
–20
–10
0
10
20
30
40
1.36
1.34
1.32
1.30
1.28
1.26
1.24
1.22
1.20
1.18
1.16
1.14
1.12
1.10
1.08
1.06
1.04
1.02
1.00
TEMPERATURE, DEGREES C
–40
–30
–20
–10
0
10
20
30
40
50
60
70
80
90
100
TEMPERATURE, DEGREES F
DENSITY
AL
TITUDE X 1000 FEET
DENSITY
F
ACT
OR
F05–014
Figure 5–2. Density Altitude Chart
