PD9B01M0 1ST ISSUE 1/07/2019 27
9.5 Flap computer (if installed)
The flaps are simultaneously actuated by an electromechanical actuator and controlled electrically
by the pilot through a special single switch (flap computer) located on the instrument panel. Power
entering to the flap actuators is protected by a breaker. The flap computer allows the flaps to be
deployed in steps at pre-configured values. The flap computer is pre-set by the company. In case
reset is necessary, consult the OEM User Manual. Additional information is included in the in the
ANNEX A (Electrical & Avionics group) in order to manage this operation.
9.6 External power source (for engine startup)
Plug the Alpi Aviation standard connector (supplied in bundle with the aircraft) into the cowl port
side. Be sure that the red wire connects with the positive and black one with the negative in the
external power unit. Start as for normal operation. Be careful about the propeller when removing
the external plug. Additional information is included in the in the ANNEX A (Electrical & Avionics
group) in order to manage this operation.
CAUTION
WHEELS MUST BE CHOCKED. BRAKES MUST BE ON. FACE AIRCRAFT INTO WIND.
ENSURE PROPEL
LER IS CLEAR. ENSURE QUALIFIED PERSON IS IN THE PILOT’S SEAT.
10 Structural repair
10.1 Type of maintenance
According to ASTM F2483-12 definition, already recalled in para. 1.1, the maintenance, repair or
alteration prescribed for this operations are defined
Heavy
.
10.2 Minimum level of certification
- Repairman, Light Sport Aircraft-Maintenance (RLSA-M) or higher;
- For composite and wood components Alpi Aviation task specific training is required;
- Authorized Alpi Aviation Service Centres are equipped to perform this type of repairs.
10.3 Repair procedures
No structural repairs are authorized without further consultation with the manufacturer.
Structural repairs on composites or wood parts of this aircraft cannot be defined by standard
procedures. The combination of materials on this aircraft is in some areas unique. Therefore, in
any case, the individual repair procedure has to be agreed with the airframe manufacturer upfront.
Approval of the manufacturer is also necessary to ensure compliance with applicable standards
and regulations.
10.4 Materials necessary for small repairs
The minimum set of materials to accomplish small repairs are herein listed. For further details
contact the facility, see A.2 Original Equipment Manufacturer.
o
Filler (suitable for wood, steel, aluminum and plywood);
o
Fabric Glue;
o
Fabric primer;
o
Epoxy resin (with catalyzer);
