Periodic Inspection Guide - Beechcraft TRAVEL AIR 95 Shop Manual

PERIODIC
INSPECTION
GUIDE
100-HOUR
INSPECTION
GUIDE
NOTE
This inspection procedure meets the intent of FAR 91.217 (b)
(4L
The owner or operator is primarily responsible
for
maintaining the airplane in an airworthy condition, including compliance
with
all applicable Airworthiness Directives as specified in Part
39
of the Federal Aviation Regulations. It is further
the
responsibility
of the owner or operator
to ensure that the airplane
is inspected in conformity with the requirements of Parts 43
and 91 of the Federal Aviation Regulations.
Beech
Aircraft
Corporation
has prepared this inspection guide to assist the owner
or operator
in
meeting the
foregoing
responsibilities.
This
inspection guide is not
intended
to be all-inclusive,
for no such guide
can
replace
the good
judgment
of a certified airframe
and powerplant
mechanic
in
the performance of his duties. As the one
primarily responsible
for the airworthiness
of the airplane,
the owner or operator
should select only qualified personnel to
maintain the airplane.
The time periods for the
inspections
noted in this schedule are
based
on normal usage under average environmental
conditions.
Airplanes operated in extremely humid tropics, or
in
exceptionally cold,
damp
climates, etc., may need more frequent
inspections
for
wear, corrosion, lubrication, and/or
lack
of maintenance. Under
these adverse conditions, perform periodic
inspections
in
compliance
with
this guide at more
frequent
intervals until the operator can set his own inspection periods based
on the contingencies of field experience.
A 100-hour
inspection
MUST
be
accomplished
within each 12-month period for
compliance
with
the Federal Aviation Regulations. To the extent that the airplane
is
operated in excess of 100 hours per year,
Beech Aircraft
Corporation
strongly
recommends
that the airplane be inspected
at 100-hour
intervals
rather
than annually. The
100-hour
interval
between performance of the procedures specified herein should NEVER
be exceeded
by more than 10 hours,
and then only
if
the additional time
is
required to reach a place where the
inspection
can
be
satisfactorily accomplished.
While this guide may be used as an outline,
detailed information
of the many systems and components in the airplane will be
found in
the
various
sections of this shop manual and the pertinent
vendor publications.
It is also recommended
that
reference
be
made to the applicable maintenance
handbooks,
service
instructions,
service
letters, service bulletins.
installations
instructions,
and
vendor's
specifications
for
torque
values,
clearances, settings, tolerances,
and other
requirements.
It should
further be
verified that all interior and exterior placards are legible and
in
place during the
inspection.
In the final analysis, it is
the responsibility
of the
owner
or operator to ensure that the airframe and powerplant mechanic inspecting the airplane has
access to the previously
noted
documents
as well as to this inspection guide.
NOTE
In addition
to
the
inspections
prescribed
by
this schedule, the altimeter system and all
ATC
transponders MUST be
tested and
inspected
at
24-month intervals in
compliance
with
the requirements specified
in
FAR
Parts
91.170 and
91.177 under
Title
14 of the
Code
of Federal Regulations.
Additional
100-hour
inspection
guides
may be obtained
under Part Number
95-5900268
or
subsequent.
C3
7-l