CSP
−
902RFM207E
−
1
ROTORCRAFT FLIGHT MANUAL
MD900 (902 Configuration with PW 207E)
Emergency and
Malfunction Procedures
FAA Approved
Reissue 2
Original
3
−
26
COLLECTIVE FRICTION FAILURE
Conditions:
Collective friction release failure
Indications:
25 lb (11.34 kg) of force required to move the collective up or down.
Procedures:
Set collective friction release switch to 5 lb position in an attempt to reduce
control forces.
Continue flight.
Advise maintenance.
Conditions:
Collective friction fails to engage
Indications:
Collective control movements will require only 5 lb (2.27 kg) of force.
Procedures:
Continue flight; advise maintenance.
3
−
10. PITOT/STATIC SYSTEM MALFUNCTION: SINGLE OR DUAL PITOT
TUBE INSTALLATION
STATIC SYSTEM MALFUNCTION
Indications:
Altimeter and IVSI (if installed) show no change in indication during
climb/descent.
Conditions:
Primary static source is clogged.
Procedures:
Alternate static source toggle valve (on
affected side)
PULL UP
NOTE
:
The altimeter will indicate 60 feet less during climb operations.
F92
−
024
CO-PILOT PITOT TUBE ALTERNATE STATIC SOURCE
TOGGLE VALVE LOCATED ON OPPOSITE SIDE OF
INSTRUMENT PANEL.
NOTE:
TO OPERATE TOGGLE VALVE, PULL
VALVE HANDLE UP. TO RETURN TO PRIMARY
STATIC SOURCE, PUSH HANDLE DOWN.
Figure 3
−
4. Alternate Static Source Toggle Valve
Summary of Contents for MD900 Explorer
Page 4: ......
