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
−
19
ENGINE FAILURE AFTER LDP
Indications:
Normal engine failure indications.
Conditions:
After to LDP
Procedures:
Continue approach.
Perform OEI landing.
2-1/2MIN. OEI LIMIT
50/25 FT
ENGINE FAILURE
AFTER LDP
DECELERATE
CATEGORY A LANDING DISTANCE
OPEN AIRFIELD/HELIPORT/ELEVATED HELIPAD
f927
−
047a
LDP
35 KIAS (65KM/H)
100 FT (30M) AGL
(15/8m)
Figure 11
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3.8. Continued Landing
Summary of Contents for MD900 Explorer
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