Brunei DCA CPL AGK - Airframe, Systems & Power Plant study plan
Brunei DCA CPL AGK - Airframe, Systems & Power Plant · Give each week a clear focus.
8 weeks · About 7 hours per week
Airframe structures: fuselage, wings, empennage, primary and secondary flight controls
Draw and label the primary load paths of a semi-monocoque fuselage, identifying skin, stringers, frames, bulkheads and floor beams, and explain what each carries.
Compare the structural layout of a cantilever wing with that of a braced wing, and describe how spar webs, spar caps, ribs and skin-stringer panels share bending and torsional loads.
Trace the control chain for ailerons, elevators and rudder from cockpit input through cables, push-pull rods, bell cranks, pulleys, turnbuckles and stops, and state the purpose of each component.
Distinguish primary from secondary flight controls and explain the function of flaps, slats, spoilers, trim tabs and balance tabs, including mass balance and flutter prevention.
Explain the purpose of structural inspection items such as stress corrosion, fatigue cracking and lightning-strike bonding in airframe construction.
Your checkpoint
A hand-drawn or digital airframe diagram set covering fuselage, wing and empennage load paths plus a labelled flight-control chain, with a one-page written explanation of each component's function, self-marked against a checklist of 15 required labels.
Hydraulic systems: reservoirs, pumps, accumulators, valves, actuators and system indications & Landing gear, wheels, brakes and anti-skid systems
Describe the layout and function of a typical hydraulic system: reservoir, filters, engine-driven and electric pumps, accumulators, pressure relief and selector valves, and actuators.
Explain how accumulator pre-charge provides emergency pressure and damps pressure surges, and interpret typical hydraulic system indications such as pressure, quantity and low-pressure warning.
Identify the components of a retractable landing gear system, including drag struts, torque links, uplocks, downlocks, sequencing and squat switches, and describe the normal and emergency extension sequence.
Explain brake system operation from pedal input through master cylinders or power brake valves to brake units, and describe the role of anti-skid systems and their wheel speed sensors.
State the inspection and servicing considerations for landing gear, tyres, wheels and brakes, including tyre creep, wear limits and hydraulic fluid contamination.
Your checkpoint
A written systems walkthrough of at least 800 words describing a complete gear-retraction and braking cycle with every hydraulic component in sequence, plus a self-made 20-item component-to-function matching quiz answered at 90% or better.
Piston engine fundamentals: configuration, induction, ignition, carburetion/fuel injection, lubrication and cooling & Propellers: theory, constant-speed units, feathering, synchronising and propeller icing
Describe the configuration of horizontally opposed and inline piston engines, naming the major components of the crankcase, crankshaft, connecting rods, pistons, cylinders, valves and valve train.
Explain the four-stroke cycle and the induction system, including carburettor venturi operation, mixture control, carburettor icing and the purpose of carburettor heat.
Describe fuel injection and ignition systems, including magnetos, spark plugs, ignition timing and the reason for dual ignition.
Explain lubrication and cooling in piston engines, covering oil pumps, oil coolers, pressure and scavenge flow, and air cooling with cylinder fins and baffles.
Explain propeller theory including blade angle, angle of attack, pitch, slip, thrust and centrifugal loads, and describe constant-speed unit operation, feathering and synchronising.
Describe propeller icing and the protection methods used, and explain the effect of ice on thrust and vibration.
Your checkpoint
A one-page engine-and-propeller summary sheet with a labelled four-stroke diagram, a labelled constant-speed propeller diagram and 10 written cause-and-effect statements, checked against the study text with every error corrected and logged.
Gas turbine engines: construction, compressor/combustion/turbine sections, lubrication, starting and thrust augmentation & Electrical systems: DC/AC generation, distribution, batteries and circuit protection
Describe the construction and function of the compressor, combustion chamber and turbine sections of a gas turbine engine, and explain how each stage contributes to thrust.
Explain gas turbine lubrication and starting, including starter types, ignition sequence, light-up indications and the parameters monitored during start.
Describe thrust augmentation methods and the differences between turbojet, turbofan, turboprop and turboshaft configurations.
Explain DC and AC generation on aircraft, including generators, alternators, voltage regulators, bus bars and distribution, and describe battery types and their care.
Explain circuit protection devices including fuses, circuit breakers and current limiters, and state when each is used.
Your checkpoint
A comparative table of gas turbine engine types and sections plus a labelled electrical distribution single-line diagram from generator to bus to load, accompanied by a 25-question self-test on weeks 1-4 material scored and reviewed.
Pneumatic and air-conditioning/pressurisation systems & Fuel systems: tanks, pumps, valves, quantity/flow indication and fuel management
Describe the sources of pneumatic power on an aircraft, including engine bleed, compressors and ground carts, and explain how bleed air is regulated and protected against overpressure and overheat.
Explain the operation of the air-conditioning system, including the air cycle machine, heat exchangers, water separation and temperature control, and describe cabin pressurisation with outflow valves and pressure controllers.
Describe the layout of fuel tanks, including integral, bladder and rigid types, and explain venting, baffles and the reasons for fuel imbalance limits.
Explain fuel pump types, selector and shut-off valves, cross-feed operation and the meaning of quantity and flow indications in the cockpit.
Explain fuel management considerations including contamination, water and sediment checks, fuel grade and the effect of temperature on fuel.
Your checkpoint
A systems narrative of at least 900 words following bleed air from engine to cabin and fuel from tank to engine, with a schematic for each system and a 15-item self-quiz on valves, indications and limitations scored at 85% or better.
Ice and rain protection, fire detection and extinguishing, and oxygen systems & Propellers: theory, constant-speed units, feathering, synchronising and propeller icing
Describe ice protection methods for airframe, propeller, pitot and static systems, distinguishing anti-icing from de-icing and thermal, chemical and pneumatic approaches.
Explain rain protection including windscreen wipers and rain repellent, and state the limitations imposed on operations in heavy rain.
Describe fire detection methods such as heat, smoke and rate-of-rise detectors, and explain the operation of fire extinguishing systems including agent types, bottles, squibs and discharge indication.
Explain oxygen system types, including gaseous and chemical generators, masks, regulators and the pre-flight checks required.
Revisit propeller icing and synchronising, and explain how propeller ice affects engine operation and what the pilot does about it.
Your checkpoint
A two-column comparison sheet for anti-icing versus de-icing across airframe, propeller and engine intake, plus a fire and oxygen system checklist of 20 pre-flight and in-flight action items, self-tested to 90% recall.
Airframe structures: fuselage, wings, empennage, primary and secondary flight controls & Hydraulic systems: reservoirs, pumps, accumulators, valves, actuators and system indications & Landing gear, wheels, brakes and anti-skid systems
Re-derive from memory the load paths and control chain from week 1, and correct any gaps found.
Re-explain hydraulic system components and indications, and solve at least 10 numerical or sequencing problems on pressure, accumulator pre-charge and actuator travel.
Re-explain landing gear, brake and anti-skid operation, and describe at least five failure modes with their cockpit indications and pilot actions.
Integrate airframe, hydraulic and gear knowledge by describing how a gear-door or flap hydraulic failure affects aircraft handling and what limitations apply.
Your checkpoint
A closed-book written test of 40 questions spanning domains 1, 2 and 5, completed in 60 minutes and scored at 80% or better, with every wrong answer rewritten correctly in your own words.
Pneumatic and air-conditioning/pressurisation systems & Electrical systems: DC/AC generation, distribution, batteries and circuit protection & Fuel systems: tanks, pumps, valves, quantity/flow indication and fuel management & Ice and rain protection, fire detection and extinguishing, and oxygen systems & Piston engine fundamentals: configuration, induction, ignition, carburetion/fuel injection, lubrication and cooling & Propellers: theory, constant-speed units, feathering, synchronising and propeller icing & Gas turbine engines: construction, compressor/combustion/turbine sections, lubrication, starting and thrust augmentation
Complete a timed mixed review covering all ten domains, weighting time in proportion to the published domain percentages.
Re-explain from memory the five highest-risk topics identified by your earlier test scores, without notes.
State the key limitations, warnings and normal operating figures for each system studied, in a single consolidated list.
Identify remaining weak areas and write a short revision list to carry into final exam preparation.
Your checkpoint
A full 60-question timed mock paper across all domains, scored at 85% or better, plus a one-page personal weak-area list with a concrete action for each item.
Milestones
Week 2: Can draw the hydraulic system and landing gear sequence from memory and name every component's function without notes, scoring at least 18 of 20 on the self-made matching quiz.
Week 4: Scores at least 75% on the 25-question self-test covering airframe, hydraulic, gear, piston engine, propeller, gas turbine and electrical material, and has corrected every error in writing.
Week 6: Scores at least 85% on a 30-question mixed test covering domains 3, 6, 7 and 9, and can explain anti-icing versus de-icing and fire bottle discharge without reference material.
Week 8: Scores at least 85% on the full 60-question timed mock paper, with no single domain below 70%, and holds a completed weak-area action list.