P2002 Sierra
SECTION B
M A I N T E N A N C E M A N U A L
pag.
B-18
2
st
Edition, April 22
th
, 2008
INSPECTION & SERVICING
13
INSPECTION
13.1
INTRODUCTION
•
TECNAM considers inspection schedule outlined below compulsory for the oper-
ational safety of the airframe and of the systems over an extended period of time.
Described servicing requirements pertain to operation in non-extreme climatic
conditions.
•
For the Rotax 912ULS engine, unless otherwise stated in the present Manual, it is
compulsory to adhere to maintenance requirements as reported in the Engine
Maintenance Manual furnished by the engine’s manufacturer (p/n 899372 Issue 0
of 1/9/1998 and later versions).
•
For the Tonini propeller, please refer to its Maintenance Manual
•
Airframe and systems inspection schedule is as follows:
A.
Inspections for airworthiness before first flight of day as specified in Flight
Manual.
B.
Periodic inspections at every 100 hours.
C.
Special inspections, added to normal periodic.
D.
Singular inspection, when aircraft has been exposed to fortuitous events that
may have damaged one or more of its components.
If aircraft is rarely used, inspection at 100 hours must be performed
yearly.
*
Replacement of parts subject to usage limitations are specified in par. 14.2
*
Inspections and checks, unless specifically indicated, apply to the following
S
TRUCTURES IN GENERAL
- Condition of panel covers, ribs, frames, stringers etc.,
absence of cracks, deformation, rivet slackening, corrosion and any other ap-
parent sign of damage.
M
OVING PARTS
- Lubrication, security of attachment, safetying of bolts, absence of
excessive play, proper adjustment, proper travel, condition of attachments and
hinges, absence of corrosion, deformation, rivet slackening, cleanliness.
F
LUID LINES AND HOSES
- Absence of leaks, cracks, dents, chafing, proper radius,
deterioration.
B
OLTS AND ATTACHMENTS
- Proper tightening and safetying, absence of cracks or
nicks, damage to thread, wear and excessive play.