CSP
−
902RFM207E
−
1
Performance Data
ROTORCRAFT FLIGHT MANUAL
MD900 (902 Configuration with PW 207E)
FAA Approved
Reissue 2
Revision 5
5
−
25
5
−
7.
RATE OF CLIMB
−
AEO
Description:
These charts show the rate of climb vs pressure altitude at twin engine
(AEO) MCP (ref. Figure 5-19 thru Figure 5-25) or TOP (ref. Figure 5-28 thru
Figure 5-35) at the best rate of climb speed.
NOTE
:
These charts based on an electrical load of 30%, heater OFF, and
air-conditioning OFF.
Use of Chart:
The following example explains the correct use of the chart in
Example
:
Wanted: Rate of climb
Known: Pressure altitude = 3000 feet
Known: Outside air temperature = 20
°
C
Method: Enter the left side of chart at the known pressure altitude of 3000 feet.
Move to the right to the 20
°
C temperature curve and then directly down
to read rate of climb of 4200 feet per minute.
Summary of Contents for MD900 Explorer
Page 4: ......
