Exam 9A: Airbus Appendix Creation - Part 1

1. In Airworthiness Limitations Section (ALS) Part 1, which covers “Safe Life Airworthiness Limitation Items (SL – ALI)” where would you typically find the spreadsheet for it.

a. This is a separate document on the Airbus website.
b. This is in the PDF document for Airworthiness Limitations Section (ALS) Part 1.
c. There is no spreadsheet for the Airworthiness Limitations Section (ALS) Part 1.

2. For Airbus in AIRBUS – ALS Part 2 – Damage Tolerant Airworthiness Limitation Items (DT – ALI) the Limit of Validity (LOV) can be described as which of the following:

a. The limit for the Landing Gear.
b. The limit for the Engines and Pylons.
c. The limit for the structural maintenance program.

3. The Weight Variant in AIRBUS – ALS Part 1 Safe Life Items will determine which parameters for the aircraft in the following:

a. The specification of the repair material required in all repairs carried out on the aircraft.
b. The Maximum Take Off Weight – MTOW, the Maximum Landing Weight – MLW and the Maximum Zero Fuel Weight – MZFW.
c. It is used to calculate the total range for the aircraft based on take off weight and fuel burn.

Exam 9A: Airbus Appendix Creation – Part 1

Exam 9A: Airbus Appendix Creation – Part 1

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