MD Helicopters MD900 with PW206E, Руководство по эксплуатации самолета

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CSP–900 RFM206E–1
ROTORCRAFT FLIGHT MANUAL
Model MD 900 With PW 206E
Increased Internal
Gross Weight Operations
FAA Approved
Original
11–4
11–5. PERFORMANCE DATA
The MD900 meets the FAR Part 36−H noise requirements for level flight, takeoff/
climb, and approach descent profiles at the certified maximum gross weight of 6500
LB.
MD900 NOISE CHARACTERISTICS
ENGINE: PW 206E, GROSS WEIGHT: 6500 LB
Configuration * VH (KTAS)
(S.L. @25
°
C)
Level Flyover
EPNL
(EPNdB)
Takeoff
EPNL
(EPNdB)
Approach
EPNL
(EPNdB)
Clean aircraft, doors on, no
external kits. 130.3 KTAS 93.7 94.7 95.7
* V
H
airspeed is for demonstrating compliance to 14 CFR Part 36 Appendix
H only and does not imply approval to exceed established V
NE
airspeeds.
Performance charts:
Rate of climb charts
Ref. Section V for interpretation instructions on the rate of climb charts.
Height velocity diagram
The cross hatched area represents airspeed/altitude combinations to be
avoided while operating between 6250 and 6500 LBS gross weight.
F90–165
ÌÌÌÌÌÌÌ
ÌÌÌÌÌÌÌ
ÌÌÌÌÌÌÌ
ÌÌÌÌÌÌÌ
ÌÌÌÌÌÌÌ
ÌÌÌÌÌÌÌ
ÌÌÌÌÌÌÌ
ÌÌÌÌÌÌÌ
160
140
120
100
80
60
40
20
0
0 5 10 15 20 25 30
AVOID AREA
AIRSPEED − KNOTS
AL
TITUDE −
AGL
(FEET)
SMOOTH, HARD
SURFACE − WIND
CALM
Figure 11–5. Height Velocity Diagram
Hover Performance
Hover performance is displayed in graph form. Refer to Figure 11−8 and
Figure 11−9.
NOTE
: Critical wind azimuth limitations may apply. Refer to Figure 11–2.