Category A Operations
Takeoff and Landing Procedures
CSP
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902RFM207E
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1
ROTORCRAFT FLIGHT MANUAL
MD900 (902 Configuration with PW 207E)
FAA Approved
Reissue 2
Revision 4
11
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25
F927
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044
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2
ÎÎÎÎÎÎÎÎÎÎÎÎÎÎÎÎÎÎÎ
ÎÎÎÎÎÎÎÎÎÎÎÎÎÎÎÎÎÎÎ
300 FT (91.4 M)
(18.3 M)
60 FT
IP
30 FT
(9.1 M)
200FT (61M)
TDP
100 FT
(30.5 M)
OBSTACLE
35 FT (10.7 M)
240 FT
(73.2 M)
2.5 MIN OEI PROFILE AT V
TOSS
LANDING PROFILE
(NOT TO SCALE)
(30.5M)
100FT
(30.5M)
100FT
OBSTACLE
Figure 11
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3.14. Example
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Confined Heliport CTO Profile and Distance to Clear
100ft/30.5m Obstacle.
Determine allowable weight limit from Heliport/Elevated Helipad WAT chart
(Ref. Figure 11-2.3).
Determine TDP (Ref. Table 11-3.3)
Power assurance check
PASS
Pre takeoff check
PERFORM
Heliport elevation
NOTE HELIPORT ELEVATION WHILE AT FLAT PITCH
Vertical Takeoff
ESTABLISH CORRECT SIGHT PICTURE BY CLIMBING VERTICALLY TO IP
100 FT (30.5 M) UNTIL THE FAR EDGE OF THE HELIPORT IS JUST ABOVE
THE SIGHT PLANE OF THE INSTRUMENT PANEL GLARE SHIELD.
CONTINUE CLIMB REARWARD, MAINTAINING SAME SIGHT PICTURE TO
200 FT (61M) TDP HAT USING THE BAROMETRIC ALTIMETER.
At TDP
PITCH NOSE DOWN TO AND ACCELERATE TO V
TOSS
AND ADJUST
COLLECTIVE TO 2.5 MIN. OEI POWER.
From 200ft/61m to
300ft/91.4m AGL
AT 300FT/91.4M AGL (REF. TABLE 11-3.1), ACCELERATE TO V
Y
AND CLIMB
TO 1000FT/305M AT OEI MCP.
Summary of Contents for MD900 Explorer
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