FLIGHT DESIGN CT - Chapter 04 - Airworthiness Limitations; 04-00.1 General; 04-00.2 Environmental Limitations; 04-00.3 Operational Limitation

Document Title Document No. Revision Date Section
Supplement S3 to the AMM CTLS-LSA –
CTLS-LSA with ROTAX 912iS
AF 0480 0011 02 16-Jul-14 04-00-1
Approval Ref.: Approved on the Basis of Manufacturer Self Declaration
CHAPTER 04 – AIRWORTHINESS LIMITATIONS
Contents
04-00.1 General
04-00.2 Environmental Limitations
04-00.3 Operational Limitation
04-00.4 Life Limited Components
04-00.1 General
This Section shows the mandatory limitations established by the airframe manufacturer.
These limitations shall be obeyed by the maintenance personnel.
In addition to this, the manufacturer recommends you to comply with the maintenance time
limits and to work with the maintenance checklists (refer to CHAPTER 05 – TIME LIMITS
AND MAINTENANCE CHECK).
In any case you must comply with the national maintenance requirements.
04-00.2 Environmental Limitations
Limitations provided in the basic aircraft AMM remain valid.
04-00.3 Operational Limitation
Limitations provided in the basic aircraft AMM remain valid.
04-00.4 Life Limited Components
The engine installation does not include life limited components. Time limits as listed in
CHAPTER 05 shall be used to ensure continued airworthiness of the Flight Design CTLS-
LSA.