B767 Engines and APU 2024/2025 Exam
Questions with 100% Correct Answers |
Latest Update
Note: Two GE Engines are rated at 60,200 pounds each. - 🧠ANSWER ✔✔
Note: N1 Rotor Consists of Fan, LP Compressor, Turbine Section on
common shaft. - 🧠ANSWER ✔✔
Note: N2 rotor consists of HP Compressor, and turbine section on common
shaft. - 🧠ANSWER ✔✔
Note: N1 and N2 rotors are mechanically independent. - 🧠ANSWER ✔✔
Note: N2 rotor drives the engine accessory gear box. - 🧠ANSWER ✔✔
Note: Each engine is controlled by an electronic engine controller (EEC) It
monitors auto-throttle and flight crew inputs through the thrust levers to
automatically control the engines. - 🧠ANSWER ✔✔
Note: Upper EICAS screen show primary engine indications - 🧠ANSWER
✔✔
COPYRIGHT©JOSHCLAY 2025/2026. YEAR PUBLISHED 2025. COMPANY REGISTRATION NUMBER: 619652435. TERMS OF USE. PRIVACY 1
STATEMENT. ALL RIGHTS RESERVED
, Note: The secondary engine indications are displayed on the lower part of
the EICAS screen. - 🧠ANSWER ✔✔
When do secondary engine indications automatically display? - 🧠ANSWER
✔✔When the display initially receives electrical power.
A secondary engine parameter is exceeded.
Note: Primary and secondary engine indications are displayed on EICAS in
compact format whenever a CRT fails. - 🧠ANSWER ✔✔
Note: Limitations for primary engine indications are show by amber or red
lines on the gauge. If one of those parameters are reach, the whole gauge
changes colors. These limitations change based on outside factors. -
🧠ANSWER ✔✔
What is the T.M.C? - 🧠ANSWER ✔✔Thrust Management Computer.
What does the thrust management computer do? - 🧠ANSWER
✔✔Calculates a reference N1 based on existing pressure altitude and
ambient temperature data.
COPYRIGHT©JOSHCLAY 2025/2026. YEAR PUBLISHED 2025. COMPANY REGISTRATION NUMBER: 619652435. TERMS OF USE. PRIVACY 2
STATEMENT. ALL RIGHTS RESERVED
Questions with 100% Correct Answers |
Latest Update
Note: Two GE Engines are rated at 60,200 pounds each. - 🧠ANSWER ✔✔
Note: N1 Rotor Consists of Fan, LP Compressor, Turbine Section on
common shaft. - 🧠ANSWER ✔✔
Note: N2 rotor consists of HP Compressor, and turbine section on common
shaft. - 🧠ANSWER ✔✔
Note: N1 and N2 rotors are mechanically independent. - 🧠ANSWER ✔✔
Note: N2 rotor drives the engine accessory gear box. - 🧠ANSWER ✔✔
Note: Each engine is controlled by an electronic engine controller (EEC) It
monitors auto-throttle and flight crew inputs through the thrust levers to
automatically control the engines. - 🧠ANSWER ✔✔
Note: Upper EICAS screen show primary engine indications - 🧠ANSWER
✔✔
COPYRIGHT©JOSHCLAY 2025/2026. YEAR PUBLISHED 2025. COMPANY REGISTRATION NUMBER: 619652435. TERMS OF USE. PRIVACY 1
STATEMENT. ALL RIGHTS RESERVED
, Note: The secondary engine indications are displayed on the lower part of
the EICAS screen. - 🧠ANSWER ✔✔
When do secondary engine indications automatically display? - 🧠ANSWER
✔✔When the display initially receives electrical power.
A secondary engine parameter is exceeded.
Note: Primary and secondary engine indications are displayed on EICAS in
compact format whenever a CRT fails. - 🧠ANSWER ✔✔
Note: Limitations for primary engine indications are show by amber or red
lines on the gauge. If one of those parameters are reach, the whole gauge
changes colors. These limitations change based on outside factors. -
🧠ANSWER ✔✔
What is the T.M.C? - 🧠ANSWER ✔✔Thrust Management Computer.
What does the thrust management computer do? - 🧠ANSWER
✔✔Calculates a reference N1 based on existing pressure altitude and
ambient temperature data.
COPYRIGHT©JOSHCLAY 2025/2026. YEAR PUBLISHED 2025. COMPANY REGISTRATION NUMBER: 619652435. TERMS OF USE. PRIVACY 2
STATEMENT. ALL RIGHTS RESERVED
