MD Helicopters MILVIZ MD530F, Руководство по летной эксплуатации вертолетов, Страница: 185 / 326

CSP
−
HE/HS
−
1
Performance Data
MD 500
(Models 369HE/HS/HM) ROTORCRAFT FLIGHT MANUAL
Landing Gear, Tail Rotor Blade Abrasion Strips Installed, Takeoff Power
<<<< Allison 250
−
C20 >>>>
FAA Approved
Revision 5
5
−
31
P
R
E
S
S
U
R
E
A
L
T
IT
U
D
E
−
M
E
T
E
R
S
P
R
E
S
S
U
R
E
A
L
T
IT
U
D
E
−
F
E
E
T
THIS CHART BASED ON CABIN HEAT, ENGINE
ANTI−ICE OFF,
ELECTRICAL LOAD 30 AMPERE.
250−C20 ENGINE
REDUCE WEIGHT CAPABILITY LBS AS FOLLOWS
REDUCE HOVER WEIGHT CAPABILITY
PRESSURE CABIN ANTI
−
BOTH
1. 33 LB WITH SCAVENGE AIR ON
2.. 50 LB WITH MAIN ROTOR ABRASION TAPE INSTALLED
3. REDUCE HOVER CEILING 400 FT ABOVE CRITICAL ALTITUDE OVER
ALT. FT
SEA LEVEL
TO
HEAT
ICE
AND ABOVE ANY OTHER HOVER REDUCTION FOR ANY OTHER 12,000 132 144 288
20,000
INSTALLED KIT (OR BASIC AIRCRAFT) WHEN THE PARTICLE SEPARATOR
IS INSTALLED.
16,000
20,000
116
98
123
108
250
217
INCREASE (OR DECREASE) WEIGHT
CAPABILITY (ABOVE CRITICAL ALTITUDE)
PER 10 AMPERE REDUCTION (OR INCREASE)
IN ELECTRICAL LOAD
6,000
18,000
OAT°C −
5 15 35
WT LBS 2 5 7
16,000
14,000
12,000
10,000
8,000
6,000
4,000
2,000
0
5,000
4,000
3,000
2,000
1,000
GROSS WEIGHTS ABOVE 2550 LB
MUST BE EXTERNAL AND JETTI-
SONABLE
0