Category A Operations
Takeoff and Landing Procedures
CSP
−
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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22
11
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3.6. REJECTED TAKEOFF
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CONFINED HELIPORT
REJECTED TAKEOFF PROCEDURES
ÎÎÎÎÎÎÎÎÎÎÎÎÎÎÎÎÎÎÎÎÎÎÎ
ÎÎÎÎÎÎÎÎÎÎÎÎÎÎÎÎÎÎÎÎÎÎÎ
(18.3 M)
60 FT
240 FT
(73.2 M)
(39.6 M)
130 FT
30 FT
(9.1 M)
TDP
30 FT
(9.1 M)
OBSTACLE
35 FT (10.7 M)
F927
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044
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3
300 FT (91.4 M)
(NOT TO SCALE)
IP
2.5 MIN OEI PROFILE AT V
TOSS
LANDING PROFILE
(30.5M)
100FT
(30.5M)
100FT
OBSTACLE
Figure 11
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3.11. Example
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Rejected Takeoff To Clear a 30ft/9.1m Obstacle
Determine allowable weight limit from Heliport/Elevated Helipad WAT chart (Ref.
Figure 11-2.3.).
Determine TDP HAT (Ref. Table 11-3.1)
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 (REF.
FIGURE 11-3.10).
CONTINUE CLIMB REARWARD, MAINTAINING SAME SIGHT PICTURE TO
130 FT (39.6 M) HAT USING THE BAROMETRIC ALTIMETER.
Engine failure prior to
TDP
PITCH NOSE DOWN AND ADJUST COLLECTIVE TO PREVENT ROTOR
DROOP.
Landing
ESTABLISH LANDING ATTITUDE AND APPLY COLLECTIVE TO CUSHION
LANDING.
Summary of Contents for MD900 Explorer
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