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
−
27
ÎÎÎÎÎÎÎÎÎÎÎÎÎÎÎÎÎÎ
(18.3 M)
60 FT
(30.5M)
100FT HATMIN TDP
IP
REJECTED TAKEOFF
30 FT
(9.1 M)
TDP
IP
200 FT (6 1M)
100 FT (30.5 M)
OBSTACLE
240FT
F927
−
044
−
5
(NOT TO SCALE)
2.5 MIN OEI PROFILE AT V
TOSS
30 FT (9.1 M)
TO
(73.3M)
IP
(30.5M)
100FT
OBSTACLE
240FT (73.3M)
Figure 11
−
3.15. Example
−
Short Field Takeoff Profile
Determine allowable weight limit from Heliport/Elevated Helipad WAT chart (Ref.
Figure 11-2.3.).
Determine IP HAT based on short field length (Ref. Table 11-3.2).
Determine TDP HAT based on obstacle height (Ref. Table 11-3.3).
Determine Rearward Ground Distance from far edge of the helipad
(Ref. Table 11-3.3).
Vertical Takeoff
ESTABLISH CORRECT SIGHT PICTURE BY CLIMBING VERTICALLY TO IP
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 at TDP
PITCH NOSE DOWN, ACCELERATE TO V
TOSS
AND ADJUST COLLECTIVE
TO PREVENT ROTOR DROOP. ADJUST POWER TO 2.5 MINUTE OEI LIMIT.
From variable 200FT/61M
to 300FT/91.4M Segment I
AGL
AT 300FT/91.4M AGL (REF. TABLE 11-3.3), ACCELERATE TO V
Y
AND CLIMB
TO 1000FT/305M AT OEI MCP.
Summary of Contents for MD900 Explorer
Page 4: ......
