CSP
−
902RFM207E
−
1
ROTORCRAFT FLIGHT MANUAL
MD900 (902 Configuration with PW 207E)
Normal Procedures
FAA Approved
Reissue 2
Original
4
−
30
Normal shutdown continued:
Rotor brake
(if installed):
Raise brake handle to release from stowed position
Rotate handle clockwise and apply brake by pulling
down on handle until handle locks aft. Release rotor
brake during last revolution unless conditions dictate
otherwise.
APPLY BELOW
70% N
R
Care should be taken while applying the rotor brake if the helicopter
is parked on a slippery or icy surface. Anti
−
torque control is
minimized at less than normal operating RPM when the engine is
not driving the rotor system. Full control of the helicopter during
these conditions may be limited.
IIDS
CHECK FOR
INDICATIONS OR
MESSAGES
NOTE
:
Wait for N
G
to reach 0% before entering the IIDS “Time Summary” menu to check
“LST FLT TIME” or “TOT FLT HR”. Failure to wait for N
G
to reach 0% may result
in incorrect time records.
Electrical master panel:
POWER
OFF AT 0% N
G
Key Switch
AS DESIRED
4
−
13. POST FLIGHT
Aircraft-investigate any suspected damage
CHECK
Rotor blades
CHECK BLADE
RETENTION BOLTS
(PINS)
Fuel and oil leaks
CHECK
Engine and rotor transmission oil levels
CHECK
NOTE
:
Engine oil level should be checked within 10 minutes after shutdown.
Logbook entries
COMPLETE
Flight manual and equipment
STOWED
Aircraft tiedowns, covers
AS REQUIRED
CAUTION
Summary of Contents for MD900 Explorer
Page 4: ......
