CSP
−
902RFM207E
−
1
ROTORCRAFT FLIGHT MANUAL
MD900 (902 Configuration with PW 207E)
Normal Procedures
FAA Approved
Reissue 2
Original
4
−
5
FORWARD RIGHT SIDE
Right crew door:
Glass and vents
SECURITY, CONDITION
Hinges
CHECK
Latch system and handle
CHECK OPERATION
Door release handle
CONDITION
Door strut and strap
OPERATION, SECURITY, CONDITION
Crew Seat
CONDITION; NOTHING STOWED
UNDER SEAT
Pilot pedals:
Adjust
ADJUSTMENT PINS ENGAGED
Move pedals by hand
OBSERVE MOVEMENT OF THRUSTER
Electrical master panel:
POWER switch
BAT/EXT
IIDS panel:
CHECK LAMP TEST MODE (B.I.T.)
Fuel quantity
CHECK
NOTE
:
The fuel quantity indication will not display actual fuel weight when the fuel
system is ‘‘topped off’’. Remove fuel cap and pull lanyard to assure tank is full
by noting fuel level on the inside of filler neck (Ref. SECTION VIII). Fuel can be
trapped in filler neck by the flapper valve.
Lighting control panel
CHECK OPERATION OF LIGHTS AS
REQUIRED
Electrical master panel:
POWER switch
OFF
Crew door
CLOSE
FUSELAGE
−
RIGHT SIDE
Landing gear:
Skid tube step
SECURITY, CONDITION
Summary of Contents for MD900 Explorer
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