11.2b Airframe Symmetry Flashcards
What can misalignment of an aircraft cause ?
Poor flying quality and handling
How can misalignment be found ?
By performing a symmetry check and an alignment check using dedicated instruments
When must an aircraft symmetry check be performed?
-any structural repair
-when the aircraft has been subjected to severe conditions
-the flight crew reports unusual flight conditions
-wrinkled or buckled structural skins
- loose or sheared fasteners
- areas of badly fitting access and inspection panels
what must be done before checking airframe symmetry?
aircraft must be jacked or levelled to ensure datum line is where it should be
on small aircraft how is symmetry checked ?
usually have small pegs or blocks that are parallel to the datum lines. a spirit level and straight edge are rested ontop of these
other than using a spirit level, what other method can be used to check aircraft symmetry?
the grid method, using a plum bob
what are the usual areas that alignment checks are performed?
- wing dihedral angle
-wing incidence angle - verticality of the fin
- engine alignment
- a symmetry check
- horizontal stabiliser incidence
how can dihedral be checked ?
special dihedral board can should be placed in specified positions.
if dihedral boards are not available to check dihedral, what else can be used ?
a straight edge and an inclinometer
what can be present when checking dihedral wings ?
dihedral can sometimes be horizontal or on rare occasions anhedral
why is incidence checked ?
to ensure the wing is free from twist
what can be used to check incidence ?
an incidence board
when should fin verticality be checked ?
once the horizontal stabilisers have been rigged correctly
how is the fin verticality checked ?
string or a tape measure are strung from prescribed points on the fin and horizontal stabiliser, they must be within prescribed limits
how are engines checked for alignment?
method depends on the type of mounting. however generally, a measurement is taken from the centreline of the mounting to the longitudinal centreline of the fuselage