Optional Equipment
Crew Door Modification
CSP
−
902RFM207E
−
1
ROTORCRAFT FLIGHT MANUAL
MD900 (902 Configuration with PW 207E)
Original
10
−
94
FAA Approved
Reissue 2
Cockpit door removal:
Open cockpit door.
Pull lower end of gas strut (1) up away from pivot post ball fitting (2) to remove.
NOTE
:
Fit between lower socket end of strut and ball fitting is by interference. Removal
of strut from its attachment requires a snap action motion to pull away the socket
end from the post ball fitting.
Push door release handle (3) forward to disengage pull rod assemblies (10) and
release cockpit door retaining bosses (4).
NOTE
:
When activating cockpit door release mechanism, spacer, washer, and retaining
bosses
(6, 5, 4) will
fall loose as the pull rods
(10)
are retracted. Place loose
attaching hardware in a suitable location for reinstallation
Remove complete door assembly with retainers (7) in place on fork (8) assemblies.
Cockpit door installation:
NOTE
:
Refer to Figure 10
34 for proper placement of attaching hardware.
Install cockpit door assembly into door frame with retainers and spacer (7, 5)
in place on fork assemblies (8).
Install washer (6), door restraint (9), and retaining boss (4) to lower fork assembly
(8).
Install spacer (5) and retaining boss (4) on upper fork assembly (8).
Align pull rods (10) with retaining bosses (4).
Pull door release handle (3) backward and verify insertion of pull rods into retain
ing bosses.
Push down lower end of gas strut (1) onto lower pivot post ball fitting (2) to
attach.
Close cockpit door.
Summary of Contents for MD900 Explorer
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