10.4 Air Operations Flashcards
Who must create the tech log?
Air operator
Who is the MEL created by and who approves it?
Made by operator and approved by CAA
Can the MEL be less restrictive than the MMEL?
No
Can be more restrictive but never less
What is the CDL?
Configuration Deviation List
How are emergency break in point marked?
Marked by a hash line triangle
Has to be red
An aircraft is being used by an operator for commercial air transport and wishes to also operate with extended range twin operations (ETOPS) or All weather Operations (AWOPS). What parts of Air Ops would the operator need to reference to find out how to gain his AOC?
Part- ORO, Part- CAT, Part- SPA
How is approval to “Operate an aeroplane for the purpose of commercial air transport” indicated?
Air operators certificate (AOC)
If an operator has a presence in several countries, where must they apply for an AOC?
Where they have their principle place of business in the UK
When must an air operator allow the CAA access to their operation?
Whenever the CAA want to visit to ensure compliance
Continued airworthiness of aircraft is whose responsibility?
Air operator unless started otherwise in the lease contract
What is, and who creates, an aircraft maintenance programme?
Details maintenance actions to be carried out and when to do them
Created by the operator and CAA approved
What documents must an aircraft have to record the maintenance actions, and other relevant information, and who creates it?
Technical Log created by the Air Operator (Approved by the CAA)
What is the function of the maintenance planning document?
Provided by the manufacturer allowing the operator to compile his own maintenance programme based on its contents
If an operator does not have a part 145 approval how does it prove to the CAA that it can maintain airworthiness of its aircraft fleet?
The must have a contract with a part 145 approved organisation that is acceptable to the CAA and how the contract to the CAA
What are structure significant items (SSI)?
Items which contribute significantly to loads applied during flight, grounds loads, pressurisation, and where a failure threatens the structural integrity and the safety of the aircraft