MD Helicopters 369E, Rotorcraft Flight Manual

Page: 63 / 264

Limitations
CSP − E − 1 ROTORCRAFT FLIGHT MANUAL
MD 500E
(Model 369E)
Revision 14
2 − 17
FAA Approved
250 − C20R/ 2
V
NE
IAS (KNOTS)
OAT PRESS ALT X 1000 GROSS WT = 2001 TO 2500 LB
°
C 0 2 4 6 8 10 12 14 16 18
− 30 141 136 131 126 122 117 113 97 83
− 20 148 143 138 133 129 124 105 89 78
− 10 150 145 140 135 116 97 83
0 151 146 129 106 90 78
10 152 117 98 84
20 132 107 91 79
30 119 100 86 NO FLIGHT
40 138 110 93 81
45 128 106 91 79
FOR AUTOROTATION V
NE
REDUCE SPEED BY 21K
(90K MIN); DO NOT EXCEED CHART V
NE
MAX V
NE
130 KTS WITH LESS THAN 35 LB FUEL
250 − C20R/ 2
V
NE
IAS (KNOTS)
OAT PRESS ALT X 1000 GROSS WT = 2501 TO 3000 LB
°
C 0 2 4 6 8 10 12 14 16 18
− 30 141 136 131 126 122 111 94 80 68
− 20 148 143 138 133 122 101 86 74 62
− 10 150 145 140 110 93 80 68
0 151 122 102 87 74 63
10 152 141 111 94 81 69
20 124 103 88 76 64
30 144 113 96 82 71 NO FLIGHT
40 126 105 90 77 66
45 121 101 87 75 64
FOR AUTOROTATION V
NE
REDUCE SPEED BY 21K
(95K MIN); DO NOT EXCEED CHART V
NE
MAX V
NE
130 KTS WITH LESS THAN 35 LB FUEL
Figure 2 − 7. V
NE
Placards − Rolls Royce 250 − C20R/2 (Sheet 2 of 2)