CSP−900RMM−2 MD Helicopters, Inc.
Rotorcraft Maintenance Manual
Page 204
Revision 34
05-50-00
Table 201. Hard Landing, Level I, Conditional Inspection (Cont.)
Registration No. Serial No. Helicopter Total Hours
Level I − Initial inspection after a suspected hard landing. If no damage or deformation is found after these
inspections, no additional inspection is necessary. If damage and/or deformation is found during the these
inspections, do the Level II hard−landing conditional inspections (ref. Table 202).
Model Initial
Ref. RMM
Section
Requirement
Fuselage
900 Examine upper deck fairings and cowlings:
Examine for correct alignment and obvious damage
Examine installation of fasteners
53−30−00
900 Examine upper deck skin panels (transmission and engine bays) for
deformation and buckling.
53−30−00
900 Examine upper deck mast fittings and adjacent area for damage or
deformation.
53−30−00
900 Examine upper deck engine mount fittings and adjacent area for
damage or deformation.
53−30−00
900 Examine underside of fuselage for signs of contact with the ground. 53−20−00
900 Examine tailboom for damage:
Examine lower surface for signs of contact with the ground
Examine upper surface for signs of rotor blade strike
53−40−00
900 Examine tailboom bumper:
Examine for obvious damage and deformation
Examine fasteners and components to tailboom for damage and
deformation
53−40−00
900 Examine vertical and horizontal stabilizers:
Examine for damage and deformation
Examine components and fasteners for damage, deformation, and
installation
Examine mating or adjacent pivoting surfaces of vertical stabilizers
for signs of hard or inadvertent contact
53−55−00
900 Examine horizontal stabilizer damper:
Examine for damage or deformation
Examine limiting pin for deformation and for signs of hard contact
with damper housing
53−55−00