CPL AGK REVIEW EXAM QUESTIONS WITH
CORRECT ANSWERS
rapid |opening |and |closing |of |the |throttle. |- |CORRECT |ANSWER✔✔-A |detuning |of |engine |
crankshaft |couterweights |is |a |source |of |overstress |that |may |be |caused |by:
airspeed |and |RPM. |- |CORRECT |ANSWER✔✔-A |fixed-pitch |propeller |is |designed |for |best |
efficiency |only |at |a |given |combination |of
Left |around |the |vertical |axis, |and |to |the |right |around |the |longitudinal |axis |- |CORRECT |
ANSWER✔✔-A |propeller |rotating |clockwise |as |seen |from |the |rear, |creates |a |spiralling |
slipstream. |The |spiralling |slipstream, |along |with |torque |effect, |tends |to |rotate |the |airplane |to |
the
Idle |the |engine |and |momentarily |turn |the |ignition |off |- |CORRECT |ANSWER✔✔-A |way |to |detect
|a |broken |magneto |primary |grounding |lead |is |to
The |oil |level |being |too |low |- |CORRECT |ANSWER✔✔-An |abnormally |high |engine |oil |
temperature |indication |may |be |caused |by
Enrich |the |fuel/air |mixture |- |CORRECT |ANSWER✔✔-Applying |carburetor |heat |will
Should |not |normally |happen. |Indicates |a |magneto |not |grounding |in |OFF |position |- |CORRECT |
ANSWER✔✔-Before |shutdown, |while |at |idle, |the |ignition |key |is |momentarily |turned |OFF. |The |
engine |continues |to |run |with |no |interruption; |this
Installation |and |instrument |error |- |CORRECT |ANSWER✔✔-Calibrated |airspeed |is |best |descried |
as |indicated |airspeed |corrected |for
, Using |a |lower |grade |of |fuel |than |recommended |- |CORRECT |ANSWER✔✔-Detonation |can |be |
caused |by:
Detonation |may |occur |at |high-power |settings |when: |- |CORRECT |ANSWER✔✔-the |fuel |mixture |
ignites |instantaneously |instead |of |burning |progressively |and |evenly
The |unburned |fuel/air |change |in |the |cylinders |is |subjected |to |instantaneous |combustion |- |
CORRECT |ANSWER✔✔-Detonation |occurs |in |a |reciprocating |aircraft |engine |when
One |hundred |eighty |(180) |degrees |turn |- |CORRECT |ANSWER✔✔-Errors |in |both |pitch |and |bank
|indicator |or |an |attitude |indicator |are |usually |at |a |maximum |as |the |aircraft |rolls |out |of |a
The |circulation |of |lubricating |oil |- |CORRECT |ANSWER✔✔-For |internal |cooling, |reciprocating |
aircraft |engines |are |especially |dependent |on
Gains |altitude |with |no |mixture |adjustment |- |CORRECT |ANSWER✔✔-Fouling |of |spark |plugs |is |
more |apt |to |occur |if |the |aircraft
Exhaust |gases |leaking |into |the |cockpit |- |CORRECT |ANSWER✔✔-Frequent |inspections |should |be
|made |of |aircraft |exhaust |manifold-type |heating |systems |to |minimize |the |possibility |of
Weight |of |fuel |and |weight |of |air |entering |the |cylinder |- |CORRECT |ANSWER✔✔-Fuel/air |ratio |is
|the |ratio |between |the
Could |accidentally |start |if |the |propeller |is |moved |with |fuel |in |the |cylinder |- |CORRECT |
ANSWER✔✔-If |the |ground |wire |between |the |magneto |and |the |ignition |switch |becomes |
disconnected, |the |engine
CORRECT ANSWERS
rapid |opening |and |closing |of |the |throttle. |- |CORRECT |ANSWER✔✔-A |detuning |of |engine |
crankshaft |couterweights |is |a |source |of |overstress |that |may |be |caused |by:
airspeed |and |RPM. |- |CORRECT |ANSWER✔✔-A |fixed-pitch |propeller |is |designed |for |best |
efficiency |only |at |a |given |combination |of
Left |around |the |vertical |axis, |and |to |the |right |around |the |longitudinal |axis |- |CORRECT |
ANSWER✔✔-A |propeller |rotating |clockwise |as |seen |from |the |rear, |creates |a |spiralling |
slipstream. |The |spiralling |slipstream, |along |with |torque |effect, |tends |to |rotate |the |airplane |to |
the
Idle |the |engine |and |momentarily |turn |the |ignition |off |- |CORRECT |ANSWER✔✔-A |way |to |detect
|a |broken |magneto |primary |grounding |lead |is |to
The |oil |level |being |too |low |- |CORRECT |ANSWER✔✔-An |abnormally |high |engine |oil |
temperature |indication |may |be |caused |by
Enrich |the |fuel/air |mixture |- |CORRECT |ANSWER✔✔-Applying |carburetor |heat |will
Should |not |normally |happen. |Indicates |a |magneto |not |grounding |in |OFF |position |- |CORRECT |
ANSWER✔✔-Before |shutdown, |while |at |idle, |the |ignition |key |is |momentarily |turned |OFF. |The |
engine |continues |to |run |with |no |interruption; |this
Installation |and |instrument |error |- |CORRECT |ANSWER✔✔-Calibrated |airspeed |is |best |descried |
as |indicated |airspeed |corrected |for
, Using |a |lower |grade |of |fuel |than |recommended |- |CORRECT |ANSWER✔✔-Detonation |can |be |
caused |by:
Detonation |may |occur |at |high-power |settings |when: |- |CORRECT |ANSWER✔✔-the |fuel |mixture |
ignites |instantaneously |instead |of |burning |progressively |and |evenly
The |unburned |fuel/air |change |in |the |cylinders |is |subjected |to |instantaneous |combustion |- |
CORRECT |ANSWER✔✔-Detonation |occurs |in |a |reciprocating |aircraft |engine |when
One |hundred |eighty |(180) |degrees |turn |- |CORRECT |ANSWER✔✔-Errors |in |both |pitch |and |bank
|indicator |or |an |attitude |indicator |are |usually |at |a |maximum |as |the |aircraft |rolls |out |of |a
The |circulation |of |lubricating |oil |- |CORRECT |ANSWER✔✔-For |internal |cooling, |reciprocating |
aircraft |engines |are |especially |dependent |on
Gains |altitude |with |no |mixture |adjustment |- |CORRECT |ANSWER✔✔-Fouling |of |spark |plugs |is |
more |apt |to |occur |if |the |aircraft
Exhaust |gases |leaking |into |the |cockpit |- |CORRECT |ANSWER✔✔-Frequent |inspections |should |be
|made |of |aircraft |exhaust |manifold-type |heating |systems |to |minimize |the |possibility |of
Weight |of |fuel |and |weight |of |air |entering |the |cylinder |- |CORRECT |ANSWER✔✔-Fuel/air |ratio |is
|the |ratio |between |the
Could |accidentally |start |if |the |propeller |is |moved |with |fuel |in |the |cylinder |- |CORRECT |
ANSWER✔✔-If |the |ground |wire |between |the |magneto |and |the |ignition |switch |becomes |
disconnected, |the |engine
