Page
33
of
33
rudder
LSA Major Repair and/or
Alteration (MRA)
Doc#: MRA011-21
Rev: A00
Replaces: n/a
Date: 16.09.2021
After the MRA has been completed weight and balance is
Not
required
×
Required
BLOCK 9 - VERIFICATION (to be filled out by the manufacturer)
Testing on the ground should be performed to make sure all systems work normally, and all engine
parameters are in check. Carry out a thorough visual inspection of the fuselage belly, main LDG strut,
firewall and seat pan, after the first flight, subsequent to the modifications being performed. Check for
any signs of damage. Notify your local Pipistrel dealer of all and any issues.
BLOCK 10 - ENGINEERING DATA (not applicable)
BLOCK 11 - OPERATING INSTRUCTIONS (to be filled out by the manufacturer)
Changes to airworthiness
limitations:
Changes to operating
instructions:
BLOCK 12 - INSTRUCTIONS FOR CONTINUED AIRWORTHINESS
(to be filled out by the manufacturer)
The following shall be added to, or revised in, the Maintenance Manual for the specific aircraft to which this
MRA applies. This MRA shall be placed in the back of the Maintenance Manual for the specific aircraft to
which this MRA applies. The Maintenance Manual Record of Revisions page shall note the date and
description of the changes that were incorporated into the Maintenance Manual
END OF MRA
