FAA Aviation Mechanic – ACS Airman Certification Standards Knowledge Test — Questions and Answers
Question 1: MRM (Maintenance Resource Management) training is analogous to CRM (Crew Resource Management) for pilots and focuses on:
- Improving tool inventory and parts tracking systems
- Certifying mechanics in advanced avionics troubleshooting
- Optimizing human performance and team communication to reduce maintenance errors (Correct answer)
- Standardizing shift schedules to reduce fatigue
Correct answer: Optimizing human performance and team communication to reduce maintenance errors
MRM applies CRM principles—communication, situational awareness, decision-making, and teamwork—to the maintenance environment to reduce human-error-caused accidents.
Question 2: What continuing education is typically required in weight & balance?
- Only education obtained before certification matters
- Training is only needed in the first year of certification
- Regular training to stay current with industry standards, regulations, and best practices (Correct answer)
- No continuing education is ever required
Correct answer: Regular training to stay current with industry standards, regulations, and best practices
Professional fields require ongoing education to ensure practitioners stay current with evolving standards, technologies, regulations, and best practices in their specialty.
Question 3: What is the most important ethical consideration for ACS professionals in hydraulic & pneumatic systems?
- Maximizing personal profit from each engagement
- Sharing all client information publicly
- Maintaining objectivity, integrity, and confidentiality in all professional work (Correct answer)
- Avoiding all challenging work assignments
Correct answer: Maintaining objectivity, integrity, and confidentiality in all professional work
ACS professionals must maintain the highest ethical standards including objectivity, integrity, and confidentiality to protect clients and uphold professional credibility.
Question 4: The ASRS (Aviation Safety Reporting System) offers reporters immunity from FAA certificate action primarily to:
- Encourage candid, voluntary disclosure of safety hazards (Correct answer)
- Reward mechanics financially for reporting
- Provide legal immunity in civil lawsuits
- Replace mandatory accident reporting requirements
Correct answer: Encourage candid, voluntary disclosure of safety hazards
ASRS immunity protects reporters so they will voluntarily disclose safety-relevant incidents without fear of certificate action, improving overall system safety.
Question 5: Which type of hydraulic seal is most commonly used between two parts that have relative motion (dynamic application)?
- O-ring or lip seal in a dynamic groove (Correct answer)
- Metal crush washer
- Anaerobic sealant
- O-ring used as a static seal
Correct answer: O-ring or lip seal in a dynamic groove
Dynamic seals such as O-rings installed in dynamic grooves or lip seals are designed to prevent leakage between moving components.
Question 6: Which 14 CFR Part governs the certification of aviation mechanics?
- Part 91
- Part 43
- Part 147
- Part 65 (Correct answer)
Correct answer: Part 65
14 CFR Part 65 covers airmen other than flight crewmembers, including the certification requirements and privileges of aviation mechanics.
Question 7: What is the most important ethical consideration for ACS professionals in composite materials & repair?
- Maintaining objectivity, integrity, and confidentiality in all professional work (Correct answer)
- Maximizing personal profit from each engagement
- Sharing all client information publicly
- Avoiding all challenging work assignments
Correct answer: Maintaining objectivity, integrity, and confidentiality in all professional work
ACS professionals must maintain the highest ethical standards including objectivity, integrity, and confidentiality to protect clients and uphold professional credibility.
Question 8: In reciprocating engine ignition timing, what does 'BTDC' mean and why is it used?
- Below Top Dead Center; the piston fires at its lowest point to maximize power stroke length
- Behind Top Dead Center; alternate term for retarded ignition timing
- Between Two Dead Centers; timing between compression and power strokes
- Before Top Dead Center; spark is fired early so combustion pressure peaks as the piston passes TDC (Correct answer)
Correct answer: Before Top Dead Center; spark is fired early so combustion pressure peaks as the piston passes TDC
BTDC means Before Top Dead Center; the spark fires early because combustion takes time, allowing peak pressure to build just after TDC for maximum mechanical advantage on the piston.
Question 9: Which risk assessment model used in aviation maintenance identifies likelihood and severity to prioritize hazards?
- Risk matrix (likelihood Ă— severity) (Correct answer)
- PAVE checklist
- 5M model
- DECIDE model
Correct answer: Risk matrix (likelihood Ă— severity)
A risk matrix that evaluates both the likelihood of an event and its potential severity is the standard tool for prioritizing hazards in SMS and maintenance risk management.
Question 10: During a preflight fuel check, a pilot/mechanic finds a small amount of water in the fuel sample. The correct action is:
- Drain only the affected sump and continue
- Ground the aircraft indefinitely until the tank is removed
- Continue sampling and draining until no water is found, verifying the sample is clear (Correct answer)
- Add fuel system icing inhibitor and return to service
Correct answer: Continue sampling and draining until no water is found, verifying the sample is clear
When water is found in a fuel sample, continue draining and sampling from all sumps until all samples are consistently clear and free of water, then verify the quantity before flight.
Question 11: What is the primary radiation safety concern for technicians performing X-ray radiographic inspection?
- Chemical burns from radiographic film developer solutions
- Cumulative exposure to ionizing radiation increasing the risk of biological harm (Correct answer)
- Ultraviolet skin burns from the X-ray tube housing
- Hearing damage from high-frequency radiation noise
Correct answer: Cumulative exposure to ionizing radiation increasing the risk of biological harm
Ionizing radiation (X-rays and gamma rays) can damage living tissue and DNA; cumulative occupational exposure is regulated by the NRC/OSHA, and technicians must use dosimetry badges and stay within annual dose limits.
Question 12: During an overhaul, how are engine cylinders typically cleaned?
- Sandpaper
- High-pressure water jet
- Bead blasting (Correct answer)
- Chemical wash
Correct answer: Bead blasting
Cylinders are usually cleaned by bead blasting to remove carbon and debris.
Question 13: An aircraft landing gear extends normally but the green 'gear down and locked' light does not illuminate. The FIRST troubleshooting step should be:
- Check the position switch and wiring circuit associated with the indicator light
- Assume the gear is down and locked since it extended normally
- Manually verify gear position via the viewing port and check the indicator light bulb (Correct answer)
- Perform an emergency landing immediately
Correct answer: Manually verify gear position via the viewing port and check the indicator light bulb
The safest first step is to visually verify gear position via mirror or viewing port, then check if the indicator bulb is burned out before assuming a more serious fault.
Question 14: When must an FAA Form 337 be submitted after a major repair or alteration?
- Only if the aircraft is registered under Part 121
- Within 90 days of the aircraft's next annual inspection
- Within 48 hours of completion
- Within 30 days after approval for return to service (Correct answer)
Correct answer: Within 30 days after approval for return to service
14 CFR 43.9 requires Form 337 to be submitted to the FAA Aircraft Registration Branch within 48 hours, while one copy is kept with the aircraft records.
Question 15: Ethics in aviation maintenance requires that a mechanic who is pressured by a supervisor to approve an unairworthy aircraft should:
- Follow supervisor instructions since they carry final authority
- Refuse to sign off and escalate to higher authority or the FAA if necessary (Correct answer)
- Complete the task but file an anonymous ASRS report after the flight
- Approve with a written note limiting personal liability
Correct answer: Refuse to sign off and escalate to higher authority or the FAA if necessary
A mechanic's signature on a return-to-service constitutes a personal safety certification; no supervisor can legally override this, and escalation to the FAA is always available.
Question 16: What is the correct procedure when an engine fire occurs during start on a reciprocating aircraft engine?
- Apply carburetor heat and reduce throttle to idle
- Continue cranking with mixture at idle cutoff and throttle full open to draw fire into engine (Correct answer)
- Immediately shut off fuel and use fire extinguisher on the engine
- Continue cranking to draw the fire into the engine while keeping the mixture rich
Correct answer: Continue cranking with mixture at idle cutoff and throttle full open to draw fire into engine
Continuing to crank with mixture cut off and throttle full open creates airflow that can draw burning fuel back into the induction system and extinguish the fire.
Question 17: The FAA's Aviation Safety Hotline (1-800-255-1111) is used to report:
- Near-midair collisions only
- Alleged violations of aviation regulations or safety concerns (Correct answer)
- Weather hazards to ATC
- Lost or stolen airman certificates
Correct answer: Alleged violations of aviation regulations or safety concerns
The FAA Safety Hotline allows anyone to anonymously report suspected regulatory violations or safety hazards to the FAA.
Question 18: Which method is primarily used to detect corrosion on aircraft structures?
- X-ray imaging
- Visual inspection (Correct answer)
- Magnetic field mapping
- Ultrasonic inspection
Correct answer: Visual inspection
Visual inspection is the first method to identify corrosion before using specialized tests.
Question 19: A mechanic is troubleshooting an aircraft electrical system where the ammeter shows a continuous discharge. The most likely cause is:
- Excessive electrical load from avionics
- The battery is fully charged and not accepting a charge
- A failed alternator or generator not supplying charging current (Correct answer)
- An open circuit in the landing light circuit
Correct answer: A failed alternator or generator not supplying charging current
A continuous ammeter discharge reading indicates the alternator or generator is not producing current and the battery is supplying all electrical loads.
Question 20: What is the purpose of an Airworthiness Directive (AD)?
- To recommend optional upgrades
- To approve new parts for installation
- To mandate corrective action for unsafe conditions (Correct answer)
- To document scheduled maintenance intervals
Correct answer: To mandate corrective action for unsafe conditions
ADs are legally enforceable regulations issued by the FAA to correct unsafe conditions found in aircraft, engines, propellers, or appliances.
Question 21: An aircraft engine exhibits low oil pressure during ground run-up but normal pressure in flight. What is the most likely cause?
- Diluted oil from fuel contamination
- Worn main bearings
- Clogged oil suction screen
- Faulty oil pressure relief valve (Correct answer)
Correct answer: Faulty oil pressure relief valve
A stuck-open oil pressure relief valve can allow excess oil to bypass at low RPM, causing low pressure at idle that normalizes at higher power settings.
Question 22: What is the purpose of a pneumatic system bootstrap reservoir?
- Pressurize the reservoir above atmospheric pressure to prevent pump cavitation at altitude (Correct answer)
- Store excess bleed air for use during engine failure
- Act as an expansion chamber for thermal growth of pneumatic tubing
- Cool pneumatic fluid before it enters actuators
Correct answer: Pressurize the reservoir above atmospheric pressure to prevent pump cavitation at altitude
A bootstrap reservoir is pressurized above the fluid inlet pressure so the hydraulic or pneumatic pump receives adequate inlet pressure, preventing cavitation at high altitudes.
Question 23: A reciprocating engine exhibits detonation during high-power operation. Which of the following will most effectively reduce detonation?
- Advancing ignition timing
- Leaning the mixture further
- Enriching the fuel-air mixture (Correct answer)
- Reducing cooling airflow
Correct answer: Enriching the fuel-air mixture
Enriching the mixture reduces cylinder temperatures and lowers the tendency for detonation by decreasing peak combustion temperatures.
Question 24: In a pneumatic de-icing system, what is the function of a distributor valve?
- Regulate bleed air pressure to the de-ice boots to a safe working pressure
- Sequence the inflation and deflation of individual de-ice boot sections (Correct answer)
- Control the flow rate of bleed air to maintain boot inflation time
- Filter moisture from bleed air before it reaches the de-ice boots
Correct answer: Sequence the inflation and deflation of individual de-ice boot sections
The distributor valve sequences inflation of leading-edge boot sections in the correct order to most effectively shed ice while minimizing bleed air consumption.
Question 25: A pitot-static system check reveals the altimeter reads 200 feet higher than field elevation with the static port open on a standard day. This indicates:
- A leak in the static system that must be repaired
- The aircraft is at a higher elevation than the airport reference point
- The altimeter is functioning correctly within tolerance
- The altimeter has an excessive scale error requiring calibration or replacement (Correct answer)
Correct answer: The altimeter has an excessive scale error requiring calibration or replacement
An altimeter error of 200 feet at field elevation exceeds the FAA allowable tolerance of ±75 feet and requires calibration or replacement.
Question 26: What does the term 'floating ground' indicate in aircraft wiring troubleshooting?
- A grounded circuit with proper continuity
- A wire that is not connected to any circuit
- A shielded coaxial cable ground
- A ground wire with excessive resistance or an open circuit (Correct answer)
Correct answer: A ground wire with excessive resistance or an open circuit
A floating ground refers to a ground connection that has high resistance or is completely open, preventing proper circuit completion.
Question 27: A mechanic who makes a maintenance error that goes undetected and results in an accident may face all of the following EXCEPT:
- Criminal prosecution
- Automatic loss of all future FAA employment eligibility (Correct answer)
- Civil lawsuit from affected parties
- FAA certificate action
Correct answer: Automatic loss of all future FAA employment eligibility
While mechanics can face certificate action, criminal charges, and civil liability, there is no automatic statutory bar from all FAA employment eligibility following an accident.
Question 28: What is the primary purpose of performing a cold cylinder check during engine diagnostics?
- To identify cylinders not firing or producing power (Correct answer)
- To measure cylinder wall wear
- To verify compression ratio
- To check valve spring tension
Correct answer: To identify cylinders not firing or producing power
A cold cylinder check identifies cylinders that are not contributing power, indicating ignition failure, fuel starvation, or mechanical issues.
Question 29: Under 14 CFR 65.81, a certificated mechanic may exercise the privileges of their certificate only if they have:
- Performed work in their certificate's category within the preceding 24 months (Correct answer)
- Served as a pilot-in-command within the preceding 6 months
- Attended an FAA safety seminar within the preceding 12 months
- Passed a practical test within the last 24 months
Correct answer: Performed work in their certificate's category within the preceding 24 months
14 CFR 65.81 requires that a mechanic have performed work in the applicable category or subcategory within the preceding 24 months to exercise certificate privileges.
Question 30: What type of seal is most commonly used in aircraft landing gear actuating cylinders?
- Teflon tape-wrapped pipe thread seals
- Mechanical carbon face seals
- Labyrinth seals
- Lip-type dynamic seals (O-rings with backup rings) (Correct answer)
Correct answer: Lip-type dynamic seals (O-rings with backup rings)
O-ring seals with backup rings are the standard dynamic seals in hydraulic actuating cylinders, preventing fluid bypass past the piston and rod.
Question 31: What ethical standards guide ACS professionals in their work?
- Maximizing personal profit is the primary ethical obligation
- Integrity, objectivity, confidentiality, and professional competence in all engagements (Correct answer)
- Ethics only apply when clients are watching
- Ethical standards are suggestions, not requirements
Correct answer: Integrity, objectivity, confidentiality, and professional competence in all engagements
Professional ethics require maintaining the highest standards of integrity, objectivity, and confidentiality while continuously developing competence.
Question 32: Aircraft brake assemblies with multiple discs (stacked rotors and stators) are typically used on:
- Helicopters exclusively
- Light general aviation aircraft under 6,000 lbs
- Agricultural aircraft only
- High-performance and large transport category aircraft requiring high heat capacity (Correct answer)
Correct answer: High-performance and large transport category aircraft requiring high heat capacity
Multiple-disc brakes are used on high-performance and large aircraft because the stacked rotor/stator design provides greater heat capacity and stopping force than single-disc systems.
Question 33: An aircraft has a moment of 186,000 in-lb and a weight of 2,400 lb. What is the CG location?
- 78.5 inches
- 77.5 inches (Correct answer)
- 75.0 inches
- 80.0 inches
Correct answer: 77.5 inches
CG = Moment Ă· Weight = 186,000 Ă· 2,400 = 77.5 inches.
Question 34: What is the purpose of a fuel crossfeed system on a multi-engine aircraft?
- To preheat fuel in cold weather
- To feed both engines from either tank to manage fuel load or feed a live engine from any tank after an engine failure (Correct answer)
- To dump fuel overboard in an emergency
- To transfer fuel only to the landing gear hydraulic reservoir
Correct answer: To feed both engines from either tank to manage fuel load or feed a live engine from any tank after an engine failure
A crossfeed system allows either engine to draw from any tank, balancing fuel loads and enabling a surviving engine to draw from the opposite side's tank after an engine failure.
Question 35: What is the purpose of a current limiter (fuse link) installed in series with an aircraft alternator?
- To disconnect the alternator during engine start
- To protect the main bus wire from excessive current if the alternator fails internally (Correct answer)
- To protect the alternator from reverse current flow
- To regulate alternator output voltage
Correct answer: To protect the main bus wire from excessive current if the alternator fails internally
A current limiter protects the heavy alternator output cable from damage in the event of an alternator internal short circuit.
Question 36: During a pre-takeoff run-up, the engine idles smoothly but surges at mid-throttle. What is the most likely cause?
- Magneto P-lead grounding intermittently
- Accelerator pump defect in the carburetor (Correct answer)
- Idle mixture set too lean
- Oil pressure relief valve sticking
Correct answer: Accelerator pump defect in the carburetor
The accelerator pump provides an extra fuel shot during throttle advancement; a defective pump causes a lean surge at mid-throttle as the main jets take over.
Question 37: Which safety precaution is MOST critical when sanding or grinding carbon fiber composites?
- Wetting the surface with water before any mechanical work
- Wearing eye protection only, as carbon dust is non-toxic
- Working only in outdoor environments to dilute carbon dust
- Using respiratory protection (P100 respirator) and skin coverage to prevent inhalation and irritation (Correct answer)
Correct answer: Using respiratory protection (P100 respirator) and skin coverage to prevent inhalation and irritation
Carbon fiber dust is a respirable particulate and a skin irritant; NIOSH-approved P100 respirators and protective clothing are required during any dry sanding or grinding.
Question 38: What career advancement paths exist for ACS certified professionals?
- Only changing careers provides advancement
- Leadership roles, specialized consulting, education and training, and executive management positions (Correct answer)
- Advancement requires leaving the field entirely
- No advancement is possible beyond initial certification
Correct answer: Leadership roles, specialized consulting, education and training, and executive management positions
Certified professionals can advance through specialization, leadership roles, consulting, academic/training positions, and executive management within their field.
Question 39: What type of hydraulic pump is most commonly used in high-performance aircraft as an engine-driven pump due to its variable output capability?
- Gear pump
- Centrifugal pump
- Variable displacement piston pump (Correct answer)
- Vane pump
Correct answer: Variable displacement piston pump
Variable displacement piston pumps can adjust their output flow based on system demand, maintaining constant pressure while reducing heat generation and power consumption when demand is low.
Question 40: An aircraft with an expired annual inspection is considered:
- Airworthy with a ferry permit
- Unairworthy and may not be operated (Correct answer)
- Airworthy if no new defects are found
- Airworthy for day VFR operations only
Correct answer: Unairworthy and may not be operated
An aircraft whose annual inspection has expired is not in compliance with 14 CFR 91.409 and is therefore unairworthy and may not be legally operated.
Question 41: Which wire gauge would be correct for a 20-ampere circuit run 15 feet in a non-bundle, non-conduit installation?
- 22 AWG
- 18 AWG
- 20 AWG
- 14 AWG (Correct answer)
Correct answer: 14 AWG
Per FAA AC 43.13-1B wire sizing charts, a 20-ampere circuit at 15 feet requires 14 AWG wire to limit voltage drop to 1 volt.
Question 42: When bleeding an aircraft hydraulic system, why is it important to work from the component farthest from the reservoir first?
- To ensure maximum fluid velocity through the lines
- To allow gravity to pull fluid through the system naturally
- To purge all air systematically toward the reservoir and prevent air pockets (Correct answer)
- To protect the reservoir from contamination during bleeding
Correct answer: To purge all air systematically toward the reservoir and prevent air pockets
Bleeding from the farthest point ensures air bubbles are progressively pushed back toward the reservoir rather than trapped in the system.
Question 43: An aircraft with a Continental fuel-injected engine experiences engine roughness after takeoff that smooths out as power is reduced. This symptom most closely suggests:
- A rich mixture condition, possibly caused by a malfunctioning fuel control unit (Correct answer)
- Magneto timing retarded beyond limits
- A cracked cylinder head affecting compression
- A lean condition caused by a blocked injector nozzle
Correct answer: A rich mixture condition, possibly caused by a malfunctioning fuel control unit
Roughness at high power that smooths at reduced power suggests an over-rich condition, as excess fuel is more problematic at higher power where flow is greatest.
Question 44: What is the correct procedure if a hydraulic system fluid sample indicates particle contamination above allowable limits?
- Filter the system fluid through progressively finer portable filters
- Replace the hydraulic fluid and clean or replace contaminated components per maintenance manual (Correct answer)
- Add a chemical dispersant to the fluid to dissolve the particles
- Continue operation but reduce system pressure by 10% to compensate
Correct answer: Replace the hydraulic fluid and clean or replace contaminated components per maintenance manual
Contamination above allowable limits requires fluid replacement and inspection/cleaning of components because dispersants are not approved and portable filtering may not address the contamination source.
Question 45: Which NDT method is most effective for detecting surface and near-surface cracks in ferromagnetic aircraft components?
- Magnetic particle inspection (Correct answer)
- Eddy current testing
- Dye penetrant inspection
- Ultrasonic testing
Correct answer: Magnetic particle inspection
Magnetic particle inspection (MPI) is specifically designed for ferromagnetic materials and can reveal both surface and subsurface discontinuities by applying a magnetic field and iron particles.
Question 46: How should an aircraft mechanic test a repaired fuel system for leaks before returning the aircraft to service?
- Visual inspection alone with the fuel caps open
- Dye penetrant test on all fittings
- Pressure test or operational test per the AMM with fuel system pressurized and all connections checked for leaks (Correct answer)
- Run the engine to operating temperature and inspect
Correct answer: Pressure test or operational test per the AMM with fuel system pressurized and all connections checked for leaks
After repair, the fuel system must be leak-tested per the AMM procedure, typically by pressurizing the system and inspecting all connections, fittings, and repaired areas for any leakage.
Question 47: An aircraft engine has a magneto drop of 175 RPM on one magneto and 50 RPM on the other during run-up. The maximum allowable drop is 125 RPM. What does this indicate?
- The magneto showing 175 RPM drop has an ignition problem requiring investigation (Correct answer)
- The magneto showing 50 RPM drop indicates a timing issue
- The engine should be run longer to warm up before re-checking
- Both magnetos are functioning normally
Correct answer: The magneto showing 175 RPM drop has an ignition problem requiring investigation
A magneto drop exceeding the maximum allowable limit (175 RPM vs. 125 RPM limit) indicates a faulty ignition component such as spark plugs, ignition leads, or the magneto itself.
Question 48: When an Airworthiness Directive is issued as an 'Emergency AD,' what is the typical compliance time frame?
- Within the next scheduled inspection interval
- 90 days from the issue date
- Immediately or within a very short specified period such as 24 hours (Correct answer)
- At the next annual inspection
Correct answer: Immediately or within a very short specified period such as 24 hours
Emergency ADs require immediate action or compliance within a very short window because the unsafe condition poses an immediate threat to safety.
Question 49: What is the advantage of a brake-by-wire (electro-hydraulic) braking system compared to a conventional hydraulic brake system?
- Eliminates the need for hydraulic fluid entirely by using electric motors
- Reduces aircraft weight by using smaller diameter brake lines
- Provides faster and more precise brake pressure modulation for anti-skid performance (Correct answer)
- Allows the pilot to apply greater mechanical advantage to brake pedals
Correct answer: Provides faster and more precise brake pressure modulation for anti-skid performance
Electro-hydraulic brake systems use electronic control to modulate hydraulic pressure with greater speed and precision than mechanical inputs alone, improving anti-skid performance.
Question 50: Under 14 CFR Part 65.92, a mechanic with both Airframe and Powerplant ratings may supervise and approve the return to service of aircraft maintained by:
- Only certificated repair stations
- Student pilots performing owner-authorized maintenance
- Certificated mechanics holding the appropriate ratings under their supervision
- Any person performing maintenance under their direct supervision per applicable regulations (Correct answer)
Correct answer: Any person performing maintenance under their direct supervision per applicable regulations
An A&P mechanic may supervise and approve work performed by others when the mechanic directly supervises the work and it is performed within applicable regulatory authority.
Question 51: An aircraft maintenance record entry for a 100-hour inspection must include all of the following EXCEPT:
- Date of inspection
- Total time in service
- Fuel quantity at time of inspection (Correct answer)
- Signature and certificate number of the person approving return to service
Correct answer: Fuel quantity at time of inspection
14 CFR 43.11 specifies required logbook entries for inspections; fuel quantity is not among the required items.
Question 52: The term 'useful load' is defined as the difference between:
- Maximum gross weight and basic empty weight (Correct answer)
- Maximum takeoff weight and maximum landing weight
- Ramp weight and takeoff weight
- Zero fuel weight and landing weight
Correct answer: Maximum gross weight and basic empty weight
Useful load = Maximum Gross Weight – Basic Empty Weight, and represents the total payload the aircraft can carry.
Question 53: When inspecting flexible hydraulic hose for serviceability, which condition requires immediate replacement?
- Minor routing deviation of less than 10% from the installed bend radius
- Slight surface scuffing on the outer protective jacket without wire braid exposure
- A small area of faded color on the outer jacket from UV exposure
- Wire braid visible through the outer cover at any point (Correct answer)
Correct answer: Wire braid visible through the outer cover at any point
Exposed wire braid indicates the outer protective cover is compromised, meaning the hose is susceptible to further damage and must be replaced immediately.
Question 54: What is the correct fiber orientation for a quasi-isotropic composite layup?
- Plies at 0°, +45°, -45°, and 90° (Correct answer)
- All plies at 0°
- Plies at 0°, 45°, and 90° with no -45°
- Alternating plies at 0° and 90° only
Correct answer: Plies at 0°, +45°, -45°, and 90°
A quasi-isotropic layup uses plies at 0°, +45°, -45°, and 90° to provide approximately equal stiffness and strength in all in-plane directions.
Question 55: What is the primary purpose of a hydraulic accumulator in an aircraft system?
- Regulate fluid temperature during high-load operations
- Filter contaminants from the hydraulic fluid
- Store hydraulic fluid under pressure to supplement the pump during peak demands (Correct answer)
- Convert hydraulic pressure to pneumatic pressure
Correct answer: Store hydraulic fluid under pressure to supplement the pump during peak demands
A hydraulic accumulator stores pressurized fluid to assist the pump during peak demand periods, such as when multiple systems operate simultaneously.
Question 56: Which organization publishes Service Bulletins (SBs) for type-certificated aircraft, and what is their regulatory status?
- The NTSB publishes SBs after accident investigations
- The FAA publishes SBs, and compliance is always mandatory
- ICAO publishes SBs, and compliance is mandatory for international operations
- The aircraft manufacturer publishes SBs, and compliance is generally recommended but not mandatory unless referenced by an AD (Correct answer)
Correct answer: The aircraft manufacturer publishes SBs, and compliance is generally recommended but not mandatory unless referenced by an AD
Manufacturers publish Service Bulletins as recommended actions; they become mandatory only when incorporated into an FAA Airworthiness Directive.
Question 57: A mechanic notices an aircraft's compass reads 10 degrees off during a compass swing. What is the appropriate corrective action?
- Adjust the compensation screws and update the compass correction card (Correct answer)
- Declare the compass unserviceable if error exceeds 5 degrees
- Replace the compass immediately
- File a maintenance discrepancy and allow the pilot to compensate mentally
Correct answer: Adjust the compensation screws and update the compass correction card
Compass deviation within allowable limits can be corrected by adjusting the compensating magnets and must be documented on an updated compass correction card.
Question 58: What is the function of a boost pump in an aircraft fuel system?
- It controls the fuel-air mixture ratio
- It replaces the engine-driven fuel pump as the primary pump
- It provides positive fuel pressure for starting, backup fuel pressure, and transfer between tanks (Correct answer)
- It filters fuel before delivery to the engine
Correct answer: It provides positive fuel pressure for starting, backup fuel pressure, and transfer between tanks
Electric boost pumps provide fuel pressure for engine starting, serve as backup if the engine-driven pump fails, and assist in fuel transfer between tanks.
Question 59: What is the scope of practice for ACS certification in hydraulic & pneumatic systems?
- The scope is determined individually by each professional
- There are no limits on what certified professionals can do
- Defined boundaries of competence and authority established by the certifying body and applicable regulations (Correct answer)
- Only the employer defines the scope of practice
Correct answer: Defined boundaries of competence and authority established by the certifying body and applicable regulations
Scope of practice defines the activities, procedures, and processes that a certified professional is authorized to perform based on their education, training, and certification level.
Question 60: What qualifications are needed for advanced aviation mechanics practice?
- Advanced certifications, specialized training, demonstrated experience, and ongoing professional development (Correct answer)
- Only a college degree in any subject
- No additional qualifications beyond initial certification
- Advanced practice requires no formal credentials
Correct answer: Advanced certifications, specialized training, demonstrated experience, and ongoing professional development
Advanced practice requires building upon foundational knowledge through specialized certifications, targeted training, and demonstrated competence in specific areas.
FAA Aviation Mechanic – ACS Airman Certification Standards Knowledge Test
The FAA Aviation Mechanic knowledge test evaluates candidates on general aviation maintenance principles, airframe systems, fuel/hydraulic systems, and NDT inspection skills required to earn an FAA Mechanic Certificate under the Airman Certification Standards (ACS) framework.
Exam Rules
- You can skip questions and return to them later
- Flag questions for review before submitting
- No feedback shown until you submit the entire exam
- Unanswered questions count as wrong — answer everything
- 10 pretest questions are mixed in and don't affect your score
- Timer auto-submits when time runs out
- Your progress is auto-saved every 30 seconds