ATPL PERFORMANCE EXAM
QUESTIONS AND ANSWERS
032.01.01.01.01 - Describe the application of certification specification (CSs) with
regard to the different kinds of aeroplanes. - Correct Answers -An EASA aircraft
certification that allows for continued safe flight and landing in case of failure without
exceptional pilot skills or strength - assistance from manufacturer emergency
procedures.
SAfe performance and structurally when performing its duties
Initially, JAR-OPS in 1998 before EASA made CS.
CS - LSA - Light sport aircraft
CS - VLA - Very Light Aeroplane
CS - 23 - Normal, Utility, Aerobatic and Commuter
CS -25 - Large turbine-powered aircraft
032.01.01.01.02 - Describe the general differences between aeroplanes certified
according to CS-23 (CS 23.1, CS 23.3) and CS-25 (CS 25.1, CS 25.20). - Correct
Answers -CS - 23 (Normal, Utility. Aerobatic):
Less than or equal to 5670kg
Less than or equal to 9 passenger (excluding pilots)
Single or Multi engine (propeller or turbine)
CS - 23 Commuter:
Less than or equal to 8618kg
Less than or equal to 19 passenger (excluding pilots)
Propeller driven twin engine
CS - 25 Large turbine aircraft intended for commercial air transport operations
031.01.01.02.01 - Describe the basic concept that the applicable operational
requirements differ depending on aeroplane performance. - Correct Answers -EU - OPS
1 minimum performance level to reach for Class A, B or C aircraft. (operational
requirements)
Together with CS (certification requirements) we get a high standard of safety.
Class A aircraft - we consider engine failure for all stages of flight
Class B aircraft - engine failure is not assumed below 300ft
031.01.01.01.02.02 - Describe the performance classes for commercial air transport
according to the applicable operational requirements. - Correct Answers -Class A -
QUESTIONS AND ANSWERS
032.01.01.01.01 - Describe the application of certification specification (CSs) with
regard to the different kinds of aeroplanes. - Correct Answers -An EASA aircraft
certification that allows for continued safe flight and landing in case of failure without
exceptional pilot skills or strength - assistance from manufacturer emergency
procedures.
SAfe performance and structurally when performing its duties
Initially, JAR-OPS in 1998 before EASA made CS.
CS - LSA - Light sport aircraft
CS - VLA - Very Light Aeroplane
CS - 23 - Normal, Utility, Aerobatic and Commuter
CS -25 - Large turbine-powered aircraft
032.01.01.01.02 - Describe the general differences between aeroplanes certified
according to CS-23 (CS 23.1, CS 23.3) and CS-25 (CS 25.1, CS 25.20). - Correct
Answers -CS - 23 (Normal, Utility. Aerobatic):
Less than or equal to 5670kg
Less than or equal to 9 passenger (excluding pilots)
Single or Multi engine (propeller or turbine)
CS - 23 Commuter:
Less than or equal to 8618kg
Less than or equal to 19 passenger (excluding pilots)
Propeller driven twin engine
CS - 25 Large turbine aircraft intended for commercial air transport operations
031.01.01.02.01 - Describe the basic concept that the applicable operational
requirements differ depending on aeroplane performance. - Correct Answers -EU - OPS
1 minimum performance level to reach for Class A, B or C aircraft. (operational
requirements)
Together with CS (certification requirements) we get a high standard of safety.
Class A aircraft - we consider engine failure for all stages of flight
Class B aircraft - engine failure is not assumed below 300ft
031.01.01.01.02.02 - Describe the performance classes for commercial air transport
according to the applicable operational requirements. - Correct Answers -Class A -
