N44443 Test (Updated Feb 2020)
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1.  The propeller is a ______ unit with the control located on the control quadrant between the throttle and mixture controls. (2-2) *
4 points
2.  The alternate air induction system provides another source of ___________. (2-2) *
4 points
3.  The Arrow is equipped with a retractable tricycle landing gear which is ____________actuated by a _______________ powered reversible pump.  (2-3) *
4 points
4. To INCREASE power, one would increase the _______ first then the ________ lever second. (7-6) *
4 points
5.  Flaps may be lowered at airspeeds up to ______ MPH and the gear can be extended at speeds up to _______MPH if desired.  (7-7) *
4 points
6.  What is the allowable range for the vacuum gauge?  _______” Hg. +/- ______” Hg at 2000 RPM. (8-2) *
4 points
7.  The electric fuel pump should be turned off momentarily during ground check to confirm operation of the _________________?  (7-4) *
4 points
8.  In cold weather, or the first flight of the day, the prop control should be cycled at least _______________ times at ____________ RPM’s while not letting the RPM's get below 1500. (7-4, checklist) *
4 points
9.  The Arrow has two fuel tanks, each with a ______ gallon capacity.  Total useable fuel is________ gallons?    (2-9) *
4 points
10.  Before attempting to reset a circuit breaker allow a cooling off period of _________________ is required.  (8-1) *
4 points
11.  The ammeter displays __________ on the charging system (alternator),  use the ________ to check its operation.  (2-14) *
4 points
12.  Prolonged slips, skids, and running turning takeoffs can cause _______________.  (8-2) *
4 points
13.  If oil pressure is not indicated within _____, shut down the engine and determine the cause.   (7-3)
4 points
Clear selection
14.  The best glide speed is _______. (4-3) *
4 points
15.  The demonstrated max crosswind component is ______ (mph).  (3-3) *
4 points
16.  If an engine failure in-flight is caused by fuel exhaustion, power will not be restored after tanks are switched for up to ______ seconds.  (4-3) *
4 points
17.  When securing the aircraft, never push on the __________of any aircraft.  (10-7) *
4 points
Required
18.  In order to protect the starting motor, starting procedures concerning cranking/cooling periods/ should limit cranking periods to ____________ with __________ periods of rests:  (7-3) *
4 points
19.  Engine fuel leaning procedures during cruise flight use the mixture to reach ______, then adjust to ______ of peak:  (7-6) *
4 points
20.  The emergency landing gear extension process involves releasing ______ to the hydraulic system such that the gear may lower by gravity: (2-3) *
4 points
21.  The 3 green landing gear lights and the “In Transit” light tell the pilot the position of the landing gear.  What can cause the green lights to not be visible?  (8-1) *
4 points
22.  Tire pressures for the Arrow are ______ for the front, and _______ for the mains (1-4). *
4 points
23. The Oleo strut provides shock absorption for landings, preflight checks should check that the nose strut has ______ inches visible and the mains with ______ inches visible, +/- 0.25". (10-6) *
4 points
24.  When towing the aircraft, never turn the nose wheel more than _______ to avoid damaging the steering mechanism. (10-1) *
4 points
25.  Starter manufacturers recommend that cranking periods be limited to _____ seconds total with a ____ minute rest between cranking periods.  Longer cranking periods will shorten the life of the starter.  Individual cranking efforts should not exceed 10 seconds.
4 points
Clear selection
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