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
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18
ENGINE FAILURE PRIOR TO LDP
Indications:
Normal engine failure indications
Conditions:
Prior to LDP
Procedures:
NOTE
:
The pilot may elect to perform the following procedures or continue the approach
and landing by following the procedures stated for ‘‘Engine Failure After LDP’’.
Increase power to OEI 2.5 minute limit.
Accelerate to above 40 KIAS (74 Km/H).
Climb to 200 FT (61m) at 45 KIAS (83 Km/H).
Accelerate to V
Y
.
Continue climb at V
Y
and observe OEI limits (Ref. Section II).
Refer to Section III for single engine emergencies.
2-1/2MIN. OEI LIMIT
LDP
35 KIAS (65KM/H)
100 FT (30M) AGL
ENGINE FAILURE
PRIOR TO LDP
CLIMB OEI MCP
AT V
Y
OEI MCP
ACCELERATE
TO V
Y
f927
−
046a
CLIMB AT 45 KIAS
(83KM/H)
200 FT
(61M) HAT
Figure 11
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3.7. Balked Landing
Summary of Contents for MD900 Explorer
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