Limitations
CSP–520N–1
MD 520N (500N) ROTORCRAFT FLIGHT MANUAL
R
Original
2–11
FAA Approved
AIRSPEED
150 KNOTS
42 TO 150 KNOTS
0 TO 89.8 PSI
89.8 TO 101.8 PSI
101.8 PSI
112.2 PSI
TORQUEMETER
129 KNOTS
810
°
C
752 TO 810
°
C
360 TO 752
°
C
843
°
C
TURBINE OUTLET TEMPERATURE
ANALOG / DIGITAL
ANALOG
400 TO 752
°
C
752 TO 810
°
C
810
°
C
899
°
C
927
°
C
150
°
C*
*Max. TOT for Lightoff
É
É
F05–008–2
0
1
2
3
4
5
N
2
RPM
99 AND 100 %
99 TO 100%
106.5%
ROTOR RPM
410 AND 508 RPM
410 TO 508 RPM
0
10
20
30
40
50
60
70
80
90
100
110
120
DUAL TACHOMETER
(FACE SHOWN TWICE FOR CLARITY)
TOT
C X 100
0
2
4
6
8
10
12
N
1
TACHOMETER
59 AND 105%
64 TO 105%
Figure 2–4. Instruments (Sheet 2 of 2)
