Boeing 767 B1.1

B1.1 engine and APU course, 767-300 with GE CF6-80C2 engines

The CF6-80C2 power plant (ATA 71–80) and the GTCP331 APU (ATA 49). Airframe chapters are not covered yet. 410 questions in 10 chapters, each with a worked explanation. 5 questions in every chapter are free; the rest come with the same subscription as the Part 66 modules.

Chapters

10 chapters · 410 questions

Try a few

One free question from each of 6 chapters. Pick your answer, then open the explanation.

  1. ATA 71 · CF6-80C2 Power Plant, Cowls and Mounts

    What type of engine is the CF6-80C2F on the 767-300?

    • A.Low bypass, three-spool turbofan
    • B.High bypass, geared single-rotor fan
    • C.High bypass, dual-rotor axial turbofan
    Show answer and explanation

    Correct answer: C. High bypass, dual-rotor axial turbofan

    The CF6-80C2F is a high bypass ratio, axial flow, dual-rotor (N1 and N2) turbofan with FADEC control.

  2. ATA 72, 73 · CF6-80C2 Engine and Fuel Distribution

    What drives the CF6-80C2 fan and low pressure compressor?

    • A.The accessory gearbox
    • B.The low pressure turbine
    • C.The high pressure turbine
    Show answer and explanation

    Correct answer: B. The low pressure turbine

    The fan and LPC form the N1 rotor, driven by the LPT. The HPC and HPT form the N2 rotor.

  3. ATA 74, 80 · CF6-80C2 Ignition and Starting

    Which rotor does the 767 CF6-80C2 pneumatic starter turn?

    • A.N1
    • B.Both N1 and N2
    • C.N2
    Show answer and explanation

    Correct answer: C. N2

    The starter turns the N2 rotor through the gearbox and the horizontal and radial drive shafts.

  4. ATA 75 · CF6-80C2 Engine Air Systems

    Which units control the CF6-80C2 engine air systems?

    • A.The pneumatic controller
    • B.The EEC and the HMU
    • C.The EICAS computers
    Show answer and explanation

    Correct answer: B. The EEC and the HMU

    The EEC commands and the HMU supplies servo fuel to the actuators and valves.

  5. ATA 76 · CF6-80C2 FADEC and Engine Controls

    Is there a mechanical link between the 767 thrust levers and the CF6-80C2 fuel control?

    • A.No, the EEC must work to run
    • B.Yes, a cable to the HMU
    • C.Yes, as a backup in hard mode
    Show answer and explanation

    Correct answer: A. No, the EEC must work to run

    There is no mechanical engine control connection; the EEC must be operational for the engine to run.

  6. ATA 77 · CF6-80C2 Engine Indicating

    What is the primary thrust indication on the 767 CF6-80C2?

    • A.N2
    • B.N1
    • C.EPR
    Show answer and explanation

    Correct answer: B. N1

    N1 (fan speed) is the primary thrust parameter on the GE-powered 767.

Questions about this course

What does this course cover?

The CF6-80C2 power plant (ATA 71–80) and the GTCP331 APU (ATA 49). Airframe chapters are not covered yet. It is written for the 767-300 with GE CF6-80C2 engines, in 10 chapters that follow the ATA order of the type course.

Is it included in the subscription?

Yes. Every chapter has 5 free questions to try, and all 410 questions come with the same Part66Exams subscription as the Part 66 modules, at no extra cost.

Are these the questions from my course exam?

No. They are written in our own words for revision. Your type course and the aircraft maintenance manual stay the authority, as limits and procedures can differ between airframes and operators.

Can I practise in another language?

Yes. Every question can be read in English or 15 other languages, with a switch back to the original English.