Removal And Installation Methods; Interior Trim Access Panels; Panel Removal For Scheduled Inspection; Stress Panels - MD Helicopters MD Explorer Servicing And Maintenance

CSP−900RMM−2
B. Removal and Installation Methods
(Ref. Figure 205 through Figure 213)
MDHI does not recommend the
CAUTION
use of power tools. Use of power
tools during removal or installation of pan­
els and attaching hardware can overtorque
attaching hardware and damage nutplates,
composite doors, covers, panels, and fair­
ings.
Removal or installation of doors, covers,
panels, and fairings is shown in the removal
and installation method column in each table,
with a supporting illustration. The type
column in each table lists the fastener and the
quantity column lists the quantity used to
remove or install the door, cover, panel, and
fairing is listed.
Page 202
Revision 35
MD Helicopters, Inc.
Rotorcraft Maintenance Manual
06-00-00
C. Interior Trim Access Panels
Information on interior trim access panels is
provided in Section 25-00-00.
D. Panel Removal for Scheduled Inspection
The star sign (l) by an item number in a
figure, indicates the minimum number of
panels to be removed or opened for an Air­
frame Periodic Inspection.
E. Stress Panels
Make sure all attaching hard­
CAUTION
ware is installed in the stress
panels before you move the rotorcraft. Dam­
age to the airframe can occur.
The check sign (n) by an item number in a
figure, indicates the minimum number of
stress panels to be installed before moving the
aircraft.