FAA Flight Engineer study plan

Diagram from memory the four-stroke reciprocating cycle and label valve timing events, then annotate where detonation and preignition originate

Explain the function and failure consequences of the constant-speed propeller governor, wastegate, and magneto in a reciprocating powerplant

Trace the fuel, oil, and ignition paths through a reciprocating engine and identify each component that can interrupt them

Compute density altitude and manifold pressure changes for three hypothetical departure scenarios

Compare turbopropeller and turbojet powerplant architecture, naming the compressor, combustion, turbine, and accessory sections and their failure signatures

Explain how EPR, N1, N2, ITT/TGT, and fuel flow are sensed and what each indicates about engine health

Describe thrust reverser, bleed air, and anti-ice system interactions and the abnormal indications each produces

Summarize limitations and operating envelopes for at least three powerplant types from memory

Sequence the memory items for engine fire, engine failure in flight, and rapid depressurization for each powerplant class

Explain the aerodynamics behind V1, Vr, and V2 decisions and how an engine failure before and after V1 changes the crew response

Describe propeller feathering, autofeather, and single-engine handling for turbopropeller aircraft

Identify the systems that fail or degrade after a single engine loss and the checklist actions that follow

Practice the abnormal and emergency checklist flows for hydraulic, electrical, pressurization, and fuel system failures without prompts

Explain how smoke, fire, and fume events differ in detection and suppression across powerplant and cabin systems

Describe upset prevention and recovery principles including stall, unusual attitude, and wind shear response

Identify the crew coordination callouts that accompany each emergency checklist

Compute takeoff and landing distance using pressure altitude, temperature, wind, and runway slope corrections

Calculate weight and balance for a multiengine aircraft using the center of gravity envelope and forward and aft limits

Explain how CG position affects stall speed, cruise performance, and controllability

Build a fuel plan including reserve, alternate, holding, and contingency fuel for a 500-nautical-mile trip

Interpret performance charts for climb, cruise, and driftdown and identify the limiting factor in each case

Explain how density altitude, contamination, and runway condition change accelerate-stop and takeoff decision distances

Describe how center of gravity and loading affect trim, drag, and fuel burn in cruise

Solve ten mixed performance and weight and balance problems under time pressure

Define the roles and responsibilities of the flight engineer, pilot flying, and pilot monitoring during normal and abnormal operations

Explain how crew resource management principles apply to workload distribution, briefing, and challenge-and-response

Describe systems management decisions such as fuel balancing, pressurization scheduling, and electrical load shedding

Analyze at least two accident case studies for crew coordination and systems management breakdowns

Review all four domains using a spaced-repetition deck and close every gap flagged in earlier weeks

Complete a full-length timed practice exam under test conditions

Re-teach the three weakest topics aloud as if briefing a crew

Build a final one-page summary sheet of limitations, memory items, and formulas