Category A Operations
Takeoff and Landing Procedures
CSP
−
902RFM207E
−
1
ROTORCRAFT FLIGHT MANUAL
MD900 (902 Configuration with PW 207E)
FAA Approved
Reissue 2
Revision 4
11
−
23
(30.5M)
100FT
30 FT
(9.1 M)
200 FT (61M)
TDP
100 FT
(30.5 M)
OBSTACLE
35 FT (10.7 M)
ÎÎÎÎÎÎÎÎÎÎÎÎÎÎÎÎÎÎÎÎ
ÎÎÎÎÎÎÎÎÎÎÎÎÎÎÎÎÎÎÎÎ
240 FT
(73.2 M)
300 FT (91.4 M)
2.5 MIN OEI PROFILE AT V
TOSS
(18.3 M)
60 FT
(NOT TO SCALE)
F927
−
044
−
4
LANDING PROFILE
IP
(30.5M)
100FT
OBSTACLE
Figure 11
−
3.12. Example
−
Rejected Takeoff to Clear Obstacle Greater Than
30ft/9.m and up to 100ft/30.5m.
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.
CONTINUE CLIMB REARWARD, MAINTAINING SAME SIGHT PICTURE TO
200 FT (61M) TDP 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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