

|
|||||||
|
Effective Date(s): April 14, 2010 57. Revise §45.11 to read as follows: (a) (1)
Includes the information specified in §45.13 using an approved method of
fireproof marking; (2) Must be secured in such a manner that
it will not likely be defaced or removed during normal service, or lost
or destroyed in an accident; and (3) Except as provided in
paragraphs (d) through (h) of this section, must be secured to the
aircraft fuselage exterior so that it is legible to a person on the
ground, and must be either adjacent to and aft of the rear-most entrance
door or on the fuselage surface near the tail surfaces. (b) (1) Must include the information specified in §45.13 using an
approved method of fireproof marking; (2) Must be affixed to
the engine at an accessible location; and (3) Must be secured
in such a manner that it will not likely be defaced or removed during
normal service, or lost or destroyed in an accident. (c) (1) Be
placed on a non-critical surface; (2) Contain the information
specified in §45.13; (3) Not likely be defaced or removed
during normal service; and (4) Not likely be lost or destroyed
in an accident. (d) (e) (1) Legible to a person on the ground, (2)
Located either adjacent to and aft of the rear-most entrance door or on
the fuselage near the tail surfaces, and (3) Displayed in such
a manner that they are not likely to be defaced or removed during
normal service. (f) For powered parachutes and
weight-shift-control aircraft, the identification plate required by
paragraph (a) of this section must be secured to the exterior of the
aircraft fuselage so that it is legible to a person on the ground.
(g) The identification plate described in paragraph (a) of this
section may be secured to the aircraft at an accessible location near an
entrance for— (1) Aircraft produced for— (i)
Operations under part 121 of this chapter, (ii) Commuter
operations (as defined in §119.3 of this chapter), or (iii)
Export. (2) Aircraft operating under part 121 of this chapter
and under an FAA-approved continuous airworthiness maintenance program;
or (3) Aircraft operating in commuter air carrier operations
(as defined in §119.3 of this chapter) under an FAA-approved continuous
airworthiness maintenance program. (h)
|
|||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||