CHAPTER 4
PAGE 4
PAGE DATE: 17. March 2014
MAINTENANCE MANUAL EXTRA 330LX
04-00-00 GENERAL
For each inspection listed here, refer to the applicable
chapter in this manual.
I M P O R T A N T It is the operator's responsibility to make sure that time
limits or life limits for items in this chapter are not
exceeded.
The airworthiness limitations items include mandatory re-
placement times and structural inspection intervals which
may only be changed with permission of the applicable
airworthiness authority.
The Airworthiness Limitations section is FAA approved and
specifies maintenance required under Secs. 43.16 and 91.403
of the Federal Aviation Regulations unless an alternative
program has been FAA approved. *)
*) Legible statement pertaining to non US registered air-
planes:
The Airworthiness Limitations section is approved by the
regulatory authority and specifies maintenance required
under Secs. 43.16 and 91.403 of the Federal Aviation Regu-
lations unless an alternative program has been approved by
the regulatory authority.
04-00-01 Temperature Limit
Composite structure is qualified up to 72°C (162°F). Struc-
ture temperatures above this limit are not approved. In order
not to exceed this temperature limit, only initial color
codes, paint scheme and paint specification applied to the
composite structure of each individual airplane ex-factory
must be used when finish restoration is required.
Intended changes to either color codes, paint scheme or
paint material must be approved by the competent Aviation
Authority (for U.S. registered airplanes by the appropriate
FAA Aircraft Certification Office [ACO]) or through the
To Next Page
Loading...
