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
−
14
ENGINE FAILURE AFTER TDP
Indications:
Normal engine out indications.
Conditions:
Category A timer displays GO.
Procedures:
Decrease collective to prevent rotor droop and adjust power to OEI 2.5 minute
limit.
Continue takeoff/climb and accelerate to above 40 KIAS (74 Km/H).
Assure power set to OEI 2.5 minute limits.
Climb at 45 KIAS (83 Km/H) to 200 FT (61M) HAT.
Accelerate to V
Y
.
Climb at V
Y
and OEI MCP (Ref. Section II).
Refer to Section III for single engine emergencies.
Takeoff timer -
OFF
2-1/2MIN. OEI LIMIT
HIGE AT 3.5 FT (1M)
SKID HEIGHT
TDP
CONTINUED TAKEOFF DISTANCE
ACCELERATE TO
V
TOSS
(40 KIAS)
(74KM/H)
CLIMB
OEI MCP
AT V
Y
35 FT
8 SECONDS
200 FT (61M) HAT
ACCELERATE TO
V
Y
f927
−
043a
CLIMB AT 45 KIAS
(83KM/H)
(11m)
Figure 11
−
3.4. Continued Takeoff
Summary of Contents for MD900 Explorer
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