Maintenance Manual V001
FRECCIA
Maintenance Manual V001
FRECCIA
Seite 32
Seite 33
3. INSPECTIONS
This section contains some requirements concerning inspections and basic maintenance, which
are to be observed in order to maintain the performance and reliability of a new airplane. It also
contains procedures for the correct handling of the airplane and servicing, recommended by the
airplane manufacturer.
It is reasonable to proceed according to a prescheduled scheme of lubrication and maintenance,
appropriate to the operating conditions and climate.
3.1. SCHEDULED AIRPLANE INSPECTIONS
The scope and the intervals of the inspection schedule are defined.
Tasks to be carried out in relation to scheduled inspections of engine, propeller, rescue system
and equipment, are defined in the respective applicable manuals or operating and maintenance
instructions.
The owner and operator are responsible to insure that all handling, servicing and maintenance are
only carried out by qualified personnel.
The table below indicates recommended maintenance periods.
Table legend:
C
Check-up - visual only, check for free play and whether everything is in position
DO IT YOURSELF
CL
Cleaning
DO IT YOURSELF
LO
Lubricating, oiling - lubricate all designated parts and spots using proper lubricant
DO IT YOURSELF
R
Replacement - replace designated parts regardless of state and condition.
You are encouraged to DO undemanding replacements YOURSELF, otherwise have
replacements done by AUTHORISED SERVICE PERSONNEL
SC
Special check-up - measuring, verifying tolerances and functionality
DONE BY AUTHORISED SERVICE PERSONNEL ONLY
O
Overhaul
2.19. PROPELLER
Manufacturer: DUC HELICES
Model: 3-blade Inconel SWIRL clockwise
Diameter: 1730 mm
For propeller inspection and maintenance refer to original propeller manufacturer´s Manuals.
Propeller removal, installation and replacement can only done of Pro.Mecc or propeller ma-
nufacturer authorized service center.
2.20. BRAKE SYSTEM
The braking system consists of one brake lever positioned in the middle of control panel, that by
the mean of a brake pump operate on the two brake system on the rear wheel.
The left and right brake share a common fluid reservoir installed on the top right of the firewall.
Care must be taken to avoid applying brake pressure when using rudder on the ground.
The parking brake control valve is mounted in the middle of the two seats, rear to the central con-
trol panel. The parking brake is OFF if the control lever is rotated vertically upwards, and it is ON
if the control lever is rotated orizzontally to the sense of flight.
Schematic of the system is represented below.
Fluid replacement: BRAKE FLUID DOT 4.
