MD Helicopters MD Explorer - Flanged Housing Installation; Fork Assembly Installation; Fork Assembly Removal; Fork Assembly, Cockpit Door

CSP−900RMM−2 MD Helicopters, Inc.
Rotorcraft Maintenance Manual
Page 404
Revision 20
52-00-00
(6). Remove sealant from around housing
(15) and remove housing.
B. Flanged Housing Installation
(Ref. Figure 401)
Consumable Materials
(Ref. CSP−SPM)
Item Nomenclature
C107 Grease, Aircraft
C206 Sealing Compound
C310 Primer
Primer (C310)
(1). Wet install rivets (14) into flanged
housing (15) with primer (C310).
Sealing Compound (C206)
(2). Fillet seal edges of flanged housing (15)
using sealing compound (C206).
(3). Bond spacers (28 and 29) to upper
flanged housing (15) with sealing
compound (C206).
NOTE: Ensure retaining boss (12) is bonded in
correct orientation for pull rod (11) installa
tion.
(4). Bond upper retaining boss (12) to
spacer (29) with sealing compound
(C206).
(5). Install cockpit door fork assemblies (13)
(Ref. Section 52-00-00).
Grease, Aircraft (C107)
(6). Apply aircraft grease (C107) to ends of
pull rod assemblies.
(7). Activate cockpit door release handle
(16) and verify insertion of pull rods
(11) into retaining boss (12).
(8). Install cockpit door assembly (2) (Ref.
Section 52-00-00).
6. Fork Assembly, Cockpit Door
A. Fork Assembly Removal
(Ref. Figure 401)
NOTE: Left and Right side are typical.
(1). Remove cockpit door assembly (2) (Ref.
Section 52-00-00).
(2). Activate cockpit door release handle
(16) to disengage pull rod assemblies
(11).
(3). Remove fork assemblies (13) and
retainers (27).
B. Fork Assembly Installation
(Ref. Figure 401)
Consumable Materials
(Ref. CSP−SPM)
Item Nomenclature
C107 Grease, Aircraft
(1). Install cockpit door fork assemblies (13)
with retainers (27).
(2). Install door restraint end fitting (31) on
lower fork assembly (13).
Grease, Aircraft (C107)
(3). Apply aircraft grease (C107) to ends of
pull rod assemblies (11).
(4). Activate cockpit door release handle
(16) and verify insertion of pull rods
(11) into retaining boss (12).
(5). Install cockpit door assembly (2) (Ref.
Section 52-00-00).
7. Pull Rod Assembly
A. Pull Rod Assembly Removal
(Ref. Figure 401)
NOTE: Left and Right side are typical.