P92 Echo Super
Maintenance Manual
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3.10.2 Inspection panels
Inspection points that are not in plain view may be accessed through inspection ports and/or removal of panels or fai rings as
detailed below:
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1.
Inspection Ports on wing underside
- access to aileron differential bellcrank – main spar and torque box; -
inspection of wing-to-strut attachment
2.
Upper strut fairing
- inspection of strut-to-wing attachment
3.
Lower strut fairing
- inspection of strut-to-fuselage attachment
4.
Tailcone underside portholes
- access to: stabilator control rod pass-through; battery relay; front attachment of
vertical stabilizer; inspection of aft structure and of cables for rudder control
5.
Battery porthole
- access to battery (not normally installed)
6.
Tailcone end fairing
- access to stabilator torque tube and attachments to control lever; -attachment of vertical
stabilizer aft spar; -rudder bellcrank; -trim actuator and pushrods
7.
Aft cabin bulkhead and baggage compartment floor
- inspection of aft fuselage section and attachments; -
inspection of stabilator control system and of cable pulleys for rudder control; - access to flap actuator; - access to
aileron control cable turnbuckles
8.
Forward cabin side panels
- access to half-wing
‟
s forward attachment; -access to fuel line tank outflow
9.
Cabin ceiling panel
- access to bellcrank joining cabin cable circuit to wing pushrods for aileron control
10.
Instrument panel cover
- access to instrumentation and radio
11.
Engine cowling
- access to engine and related systems; - access to main components of electrical system - access
to nose gear strut and steering assembly mechanism
12.
Propeller spinner
- access to propeller hub
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3.11 Inspection
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3.11.1 INTRODUCTION
TECNAM considers the inspection schedule outlined below compulsory for the safe operation 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 912 ULS / S engine
, unless otherwise stated in the present manual, it is compulsory to adhere to
maintenance requirements as reported in the Engine
‟
s Operator
‟
s Manual (p/n 899 370).
For the
GT propeller,
refer to manufacturer
‟
s maintenance manual
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Airframe and systems inspection schedule is as follows:
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Inspections for airworthiness before first flight of day as specified in Flight Manual
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Periodic inspections at 100 hours
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Special inspections added to normal periodic inspections
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Singular inspection, when aircraft has been exposed to conditions that may have damaged one or more of its
components
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If aircraft is rarely used, a “100 hour inspection” must be performed yearly
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Replacement of parts subject to usage limitations are specified in par. 3.14
Inspections and checks, unless specifically indicated, apply to the following:
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Structures in general:
- Condition of panel covers, ribs, frames, stringers etc., absence of cracks,
deformation, rivet slackening, corrosion and any other apparent sign of damage
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Moving 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
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Fluid lines and hoses:
- Absence of leaks, cracks, dents, chafing, proper radius, deterioration
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Bolts and attachments:
- Proper tightening and safetying, absence of cracks or nicks, absence of
corrosion and punctiform corrosion, damage to thread, wear and excessive play.
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22
Revision Date: 10-29-2007
Revision Number: 3.01
Summary of Contents for P92 Echo Super
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