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FAA || Written || Exam || with || precise ||
detailed || solutions
What || is || one || purpose || of || wing || flaps? || - || ✔✔To || enable || the || pilot || to || make || steeper || approaches || to || a || landing || without || increasing || the || airspeed. One || of || the || main || functions || of || flaps || during || approach || and || landing || is || to: || - || ✔✔Increase || the || angle || of || descent || without || increasing || the || airspeed. What || is || the || purpose || of || the || rudder || on || an || airplane? || - || ✔✔To || control || yaw. Which || is || not || a || primary || flight || control || surface? A. || Flaps B. || Stabilator C || Ailerons || - || ✔✔A. || Flaps The || elevator || controls || movement || around || which || axis? || - || ✔✔Lateral. Which || statement || is || true || concerning || primary || flight || controls? A. || The || effectiveness || of || each || control || surface || increases || with || speed || because || there || is || more || flow || over || them B. || Only || when || all || three || primary || flight || controls || move || in || sequence || do || the || airflow || and || pressure || distribution || change || over || and || around || the || airfoil. C. || Primary || flight || controls || include || ailerons, || rudder, || elevator, || and || trim || systems || - || ✔✔A. || The || effectiveness || of || each || control || surface || increases || with || speed || because || there || is || more || flow || over || them. Which || of || the || following || is || true || concerning || flaps?
A. || Flaps || are || attached || to || the || leading || edge || of || the || wing || and || are || used || to || increase || wing || lift. B. || Flaps || allow || an || increase || in || the || angle || of || descent || without || increasing || airspeed. C. || Flaps || are || high || drag || devices || deployed || from || the || wings || to || reduce || lift. || - || ✔✔B. || Flaps || allow || and || increase || in || the || angle || of || descent || without || increasing || airspeed. Which || device || is || a || secondary || flight || control? A. || Spoilers B. || Ailerons C. || Stabilators || - || ✔✔A. || Spoilers Trim || systems || are || designed || to || do || what? || - || ✔✔They || relieve || the || pilot || of || the || need || to || maintain || constant || back || pressure || on || the || flight || controls. The || four || forces || acting || on || an || airplane || in || flight || are: || - || ✔✔Lift, || Weight, || Thrust, || & || Drag When || are || the || four || forces || that || act || on || an || airplane || in || equilibrium? || - || ✔✔During || unaccelerated || flight. What || is || the || relationship || of || lift, || drag, || thrust, || and || weight || when || the || airplane || is || in || straight-and-level || flight? || - || ✔✔Lift || equals || weight. Thrust || equals || drag. Which || statement || relates || to || Bernoulli's || principle? || - || ✔✔Air || traveling || faster || over || the || curve || upper || surface || of || an || airfoil || causes || lower || pressure || on || the || top || surface.
Floating || caused || by || the || phenomenon || of || ground || effect || will || be || most || realized || during || an || approach || to || land || when || at... || - || ✔✔Less || than || the || length || of || the || wingspan || above || the || surface. What || must || a || pilot || be || aware || of || as || a || result || of || ground || effect? || - || ✔✔Induced || drag || decreases; || therefor, || any || excess || speed || at || the || point || of || flare || may || cause || considerable || floating. Ground || effect || is || most || likely || to || result || in || which || problem? || - || ✔✔Becoming || airborne || before || reaching || recommended || takeoff || speed. What || force || makes || an || airplane || turn? || - || ✔✔The || horizontal || component || of || lift. An || airplane || said || to || be || inherently || stable || will... || - || ✔✔require || less || effort || to || control. What || determines || the || longitudinal || stability || of || an || airplane? || - || ✔✔The || location || of || the || CG || with || respect || to || the || center || of || lift. Changes || in || the || center || of || pressure || of || a || wing || affect || the || aircraft's... || - || ✔✔Aerodynamic || balance || and || controllability. An || airplane || has || been || loaded || in || such || a || manner || that || the || CG || is || located || aft || of || the || aft || CG || limit. || One || undesirable || flight || characteristic || a || pilot || might || experience || with || this || airplane || would || be... || - || ✔✔Difficulty || in || recovering || from || a || stalled || condition. What || causes || an || airplane || (except || a || T-tail) || to || pitch || nosedown || when || power || is || reduced || and || controls || are || not || adjusted? || - || ✔✔The || downwash || on || the || elevators ||
from || the || propeller || slipstream || is || reduced || and || the || elevator || effectiveness || is || reduced Loading || an || airplane || to || the || most || aft || CG || will || cause || the || airplane || to || be... || - || ✔✔Less || stable || at || all || speeds. In || what || flight || condition || is || torque || effect || the || greatest || in || a || single-engine || airplane? || - || ✔✔Low || airspeed, || high || power, || high || angle || of || attack. The || left || turning || tendency || of || an || airplane || caused || by || P-factor || is || the || result || of || the... || - || ✔✔Propeller || blade || descending || on || the || right, || producing || more || thrust || than || the || ascending || blade || on || the || left. When || does || P-factor || cause || the || airplane || to || yaw || to || the || left? || - || ✔✔When || at || high || angles || of || attack. The || amount || of || excess || load || that || can || be || imposed || on || the || wing || of || an || airplane || depends || upon || the... || - || ✔✔Speed || of || the || airplane. Which || basic || flight || maneuver || increases || the || load || factor || on || an || airplane || as || compared || to || straight-and-level || flight? || - || ✔✔Turns. During || an || approach || to || a || stall, || an || increased || load || factor || will || cause || the || aircraft || to... || - || ✔✔Stall || at || a || high || airspeed. In || the || Northern || Hemisphere, || a || magnetic || compass || will || normally || indicate || a || turn || toward || the || north || if... || - || ✔✔An || aircraft || is || accelerated || while || on || an || east || of || west || heading. During || flight, || when || are || the || indications || of || a || magnetic || compass || accurate? || - || ✔✔Only || in || straight-and-level || unaccelerated || flight.
If || the || pitot || tube || and || outside || static || vents || become || clogged, || which || instruments || would || be || affected? || - || ✔✔The || altimeter, || airspeed || indicator, || & || vertical || speed || indicator. Which || instrument(s) || wil || become || inoperative || if || the || static || vents || become || clogged? || - || ✔✔Airspeed, || altimeter, || and || vertical || speed. What || does || the || red || line || on || an || airspeed || indicator || represent? || - || ✔✔Never- exceed || speed. What || is || an || important || airspeed || limitation || that || is || not || coded || on || airspeed || indicators? || - || ✔✔Maneuvering || speed What || is || absolute || altitude || - || ✔✔The || vertical || distance || of || the || aircraft || above || the || surface. What || is || true || altitude? || - || ✔✔The || vertical || distance || of || the || aircraft || above || sea || level. What || is || density || altitude? || - || ✔✔The || pressure || altitude || corrected || for || nonstandard || temperature. Under || what || conditions || is || pressure || altitude || and || density || altitude || the || same || value? || - || ✔✔At || standard || temperature. Under || what || condition || is || indicated || altitude || the || same || as || true || altitude? || - || ✔✔When || at || sea || level || under || standard || conditions. Under || what || condition || will || pressure || altitude || be || equal || to || true || altitude? || - || ✔✔When || standard || atmospheric || conditions || exist.
What || is || pressure || altitude? || - || ✔✔The || altitude || indicated || when || the || barometric || pressure || scale || is || set || to || 29.92. Altimeter || setting || is || the || value || to || which || the || barometric || pressure || scale || of || the || altimeter || is || set || so || the || altimeter || indicates... || - || ✔✔True || altitude || at || field || elevation. If || it || is || necessary || to || set || the || altimeter || from || 29.15 || to || 29.85 || what || change || occurs? || - || ✔✔ 700 || foot || increase || in || indicated || altitude. || (The || altimeter-indicated || altitude || moves || in || the || same || direction || as || the || altimeter || setting || and || changes || about || 1,000 || ft. || for || every || change || of || 1" || Hg.) If || a || pilot || changes || the || altimeter || setting || from || 30.11 || to || 29.96 || what || is || the || approximate || change || in || indication? || - || ✔✔Altimeter || will || indicate || 150 || feet || lower. If || a || flight || is || made || from || an || area || of || low || pressure || into || an || area || of || high || pressure || without || the || altimeter || setting || being || adjusted, || the || altimeter || will || indicate... || - || ✔✔Lower || than || the || actual || altitude || above || sea || level. If || a || flight || is || made || from || an || area || of || high || pressure || into || an || area || of || lower || pressure || without || the || altimeter || setting || being || adjusted, || the || altimeter || will || indicate... || - || ✔✔Higher || than || the || actual || altitude || above || sea || level. Which || condition || would || cause || the || altimeter || to || indicate || a || lower || altitude || than || true || altitude? A. || Air || temperature || lower || than || standard B. || Atmospheric || pressure || lower || than || standard C. || Air || temperature || warmer || than || standard || - || ✔✔C. || Air || temperature || warmer || than || standard.
If || the || engine || oil || temperature || and || cylinder || head || temperature || gauges || have || exceeded || their || normal || operating || range, || the || pilot || may || have || been || operating || with... || - || ✔✔too || much || power || and || with || the || mixture || set || too || lean. What || action || can || a || pilot || take || to || aid || in || cooling || an || engine || that || is || overheating || during || a || climb? || - || ✔✔Reduce || rate || of || climb || and || increase || airspeed. What || is || one || procedure || to || aid || in || cooling || an || engine || that || is || overheating. || - || ✔✔Enrich || the || fuel || mixture. How || is || engine || operation || controlled || on || an || engine || equipped || with || a || constant- speed || propeller? || - || ✔✔The || throttle || controls || power || output || as || registered || on || the || manifold || pressure || gauge || and || the || propeller || control || regulates || engine || RPM. A || precaution || for || the || operation || of || an || engine || equipped || with || a || constant-speed || propeller || is || to... || - || ✔✔Avoid || high || manifold || pressure || settings || with || low || RPM What || is || an || advantage || of || a || constant-speed || propeller? || - || ✔✔Permits || the || pilot || to || select || the || blade || angle || for || the || most || efficient || performance. One || purpose || of || the || dual || ignition || system || on || an || aircraft || engine || is || to || provide || for... || - || ✔✔Improved || engine || performance. || (also || increased || safety) If || the || ignition || switch || ground || wire || becomes || disconnected, || the || magneto... || - || ✔✔May || continue || to || fire. With || regard || to || carburetor || ice, || float-type || carburetor || systems || in || comparison || to || fuel || injection || systems || are || generally || considered || to || be... || - || ✔✔More || susceptible || to || icing.
Which || condition || is || most || favorable || to || the || development || of || carburetor || icing? || - || ✔✔Temperature || between || 20 ºF || and || 70 ºF || and || high || humidity. The || possibility || of || carburetor || icing || exist || even || when || the || ambient || air || temperature || is || as... || - || ✔✔High || as || 70 ºF || and || the || relative || humidity || is || high. If || an || aircraft || is || equipped || with || a || fixed-pitch || propeller || and || a || float-type || carburetor, || the || first || indication || of || carburetor || ice || would || most || likely || be... || - || ✔✔Loss || of || RPM. The || operating || principle || of || float-type || carburetors || is || based || on || the... || - || ✔✔Difference || in || air || pressure || at || the || venturi || throat || and || the || air || inlet. The || presence || of || carburetor || ice || in || an || aircraft || equipped || with || a || fixed-pitch || propeller || can || be || verified || by || applying || carburetor || heat || and || noting... || - || ✔✔A || decrease || in || RPM || and || then || a || gradual || increase || in || RPM. Generally || speaking, || the || use || of || carburetor || heat || tends || to... || - || ✔✔Decrease || engine || performance. Applying || carburetor || heat || will... || - || ✔✔Enrich || the || fuel/air || mixture. What || change || occurs || in || the || fuel/air || mixture || when || the || carburetor || heat || is || applied? || - || ✔✔The || fuel/air || mixture || becomes || richer. During || the || run-up || at || a || high-elevation || airport, || a || pilot || notes || a || slight || engine || roughness || that || is || not || affected || by || the || magneto || check || but || grows || worse || during || the || carburetor || heat || check. || Under || these || circumstances, || what || would || be || the || most || logical || initial || action? || - || ✔✔Check || the || results || obtained || with || a || leaner || setting || of || the || mixture.
o || properly || purge || water || from || the || fuel || system || of || an || aircraft || equipped || with || fuel || tank || sumps || and || afuel || strainer || quick || drain, || it || is || necessary || to || drain || fuel || from || the... || - || ✔✔Fuel || strainer || drain || and || the || fuel || tank || sumps. On || aircraft || equipped || with || fuel || pumps, || when || is || the || auxiliary || electric || driven || pump || used? || - || ✔✔In || the || event || engine-driven || fuel || pump || fails. Which || would || most || likely || cause || cylinder || head || temperature || and || engine || oil || temperature || gauges || to || exceed || their || normal || operating || ranges? A. || Using || fuel || that || has || a || lower-than-specified || fuel || rating B. || Using || fuel || that || has || a || higher-than-specified || fuel || rating C. || Operating || with || higher-than-normal || oil || pressure || - || ✔✔A. || Using || fuel || that || has || a || lower-than-specified || fuel || rating. What || should || be || the || first || action || after || starting || an || aircraft || engine? || - || ✔✔Adjust || for || proper || RPM || and || check || for || desired || indication || on || the || engine || gauges. Should || it || become || necessary || to || hand || prop || an || airplane || engine, || it || is || extremely || important || that || a || competent || pilot... || - || ✔✔Be || at || the || controls || in || the || cockpit. An || electrical || system || failure( || battery || and || alternator) || occurs || during || flight. || In || this || situation, || you || would... || - || ✔✔Experience || avionics || equipment || failure. A || positive || indication || on || an || ammeter... || - || ✔✔Shows || the || rate || of || charge || on || the || battery. To || keep || a || battery || charged, || the || alternator || voltage || output || should || be... || - || ✔✔Higher || than || the || battery || voltage. Which || of || the || following || is || a || true || statement || concerning || electrical || systems?
A. || The || master || switch || provides || current || to || the || electrical || system B. || The || airspeed || indicator || is || driven || by || the || electrical || system C. || Lights || and || radios || use || the || electrical || system || for || power || - || ✔✔C. || Lights || and || radios || use || the || electrical || system || for || power. The || numbers || 9 || and || 27 || on || the || approach || ends || of || the || runway || indicate || that || the || runway || is || orientated || approximately... || - || ✔✔090* || and || 270* || Magnetic. The || numbers || 8 || and || 26 || on || the || approach || ends || of || the || runway || indicate || that || the || runway || is || orientated || approximately... || - || ✔✔ 080 º || and || 260 º || Magnetic. When || approaching || taxiway || holding || lines || from || the || side || with || the || continuous || line, || the || pilot... || - || ✔✔Should || not || cross || the || lines || without || ATC || clearance. What || is || the || purpose || of || the || runway/runway || hold || position || sign? || - || ✔✔Denotes || intersecting || runways. What || does || the || outbound || destination || sign || identify? || - || ✔✔Identifies || direction || to || takeoff || runways. When || turning || onto || a || taxiway || from || another || taxiway, || what || is || the || purpose || of || the || taxi || way || directional || sign? || - || ✔✔Indicates || designation || and || direction || of || taxiway || leading || out || of || an || intersection. What || purpose || does || the || taxiway || location || sigh || serve? || - || ✔✔Identifies || taxiway || on || which || an || aircraft || is || located. An || airport's || rotating || beacon || operated || during || daylight || hours || indicates... || - || ✔✔That || weather || at || the || airport || located || in || Class || D || airspace || is || below || basic || VFR || weather || minimums.
A || below || glide || slope || indication || from || a || pulsating || approach || slope || indicator || is... ||
- || ✔✔A || pulsating || red || light. When || approaching || to || land || on || a || runway || served || by || a || visual || approach || slope || indicator || (VASI), || the || pilot || shall... || - || ✔✔Maintain || an || altitude || at || or || above || the || glide || slope. While || operating || in || class || D || airspace, || each || pilot || of || an || aircraft || approaching || to || land || on || a || runway || served || by || a || visual || approach || slope || indicator || (VASI) || shall... || - || ✔✔Maintain || an || altitude || at || or || above || the || glide || slope || until || a || lower || altitude || is || necessary || for || a || save || landing. A || slightly || high || glide || slope || indication || from || a || precision || approach || path || indicator || is... || - || ✔✔Three || white || lights || and || one || red || light. Wingtip || vortices || are || created || only || when || an || aircraft || is... || - || ✔✔Developing || lift. Wingtip || vortices || created || by || large || aircraft || tend || to... || - || ✔✔Sink || below || the || aircraft || generating || the || turbulence. How || does || the || wake || turbulence || vortex || circulate || around || each || wing || tip? || - || ✔✔Outward, || upward, || & || around || each || tip. When || taking || off || or || landing || at || an || airport || where || heavy || aircraft || are || operating, || one || should || be || particular || alert || to || the || hazards || of || wing || tip || vortices || because || this || turbulence || tends || to... || - || ✔✔Sink || into || the || flight || path || of || the || aircraft || operating || below || the || aircraft || generating || the || turbulence. The || greatest || vortex || strength || occurs || when || the || generating || aircraft || is. || - || ✔✔Heavy, || clean, || & || slow.
The || wind || condition || that || requires || maximum || caution || when || avoiding || wake || turbulence || on || landing || is... || - || ✔✔Light, || quartering || tailwind. When || departing || behind || a || heavy || aircraft, || the || pilot || should || avoid || wake || turbulence || by || maneuvering || the || aircraft... || - || ✔✔Above || and || upwind || from || the || heavy || aircraft. When || landing || behind || a || large || aircraft, || the || pilot || should || avoid || wake || turbulence || by || staying... || - || ✔✔Above || the || large || aircraft's || final || approach || path || and || landing || beyond || the || large || aircraft's || touchdown || point. When || landing || behind || a || large || aircraft, || which || procedure || should || be || followed || for || vortex || avoidance? || - || ✔✔Stay || above || its || final || approach || flightpath || all || the || way || to || touchdown. During || a || night || flight,you || observe || a || steady || red || light || and || a || flashing || red || light || at || the || same || altitude. || What || is || the || general || direction || of || movement || of || he || other || aircraft? || - || ✔✔The || other || aircraft || is || crossing || to || the || left. During || a || night || flight, || you || observe || a || steady || white || light || and || a || flashing || read || light || ahead || and || at || the || same || altitude. || What || is || the || general || direction || of || movement || of || the || other || aircraft? || - || ✔✔The || other || aircraft || is || flying || away || from || you. During || a || night || flight, || you || observe || steady || red || and || green || lights || ahead || at || the || same || altitude. || What || is || the || general || direction || of || movement || of || the || other || aircraft? || - || ✔✔The || other || aircraft || is || approaching || head-on. The || most || effective || method || of || scanning || for || other || aircraft || for || collision || avoidance || during || daylight || hours || is || to || use... || - || ✔✔A || series || of || short, || regularly || spaced || eye || movements || to || search || each || 10 || degree || sector.
Automatic || Terminal || Information || Service || (ATIS) || is || the || continuous || broadcast || of || recorded || information || concerning... || - || ✔✔noncontrol || information || in || selected || high-activity || terminal || areas. Absence || of || the || sky || condition || and || visibility || on || an || ATIS || broadcast || indicates || that... || - || ✔✔The || ceiling || is || at || least || 5,000 || feet || and || visibility || is || 5 || miles || or || more A || blue || segmented || circle || on || a || Sectional || Chart || depicts || which || class || airspace? || - || ✔✔Class || D. Airspace || at || an || airport || with || a || part-time || control || tower || is || classified || as || Class || D || airspace || only... || - || ✔✔When || the || associated || control || tower || is || in || operation. When || a || control || tower || located || on || an || airport || within || class || D || airspace || ceases || operation || for || the || day, || what || happens || to || the || airspace || designation? || - || ✔✔The || airspace || reverts || to || Class || E || or || a || combination || of || Class || E || and || G || airspace || during || the || hours || the || tower || is || not || in || operation. A || non-tower || satellite || airport, || within || the || same || Class || D || airspace || as || that || designated || for || the || primary || airport, || requires || radio || communications || be || established || and || maintained || with || the... || - || ✔✔Primary || airport's || control || tower. Unless || otherwise || authorized, || two-way || radio || communications || with || Air || Traffic || Control || are || required || for || landings || or || takeoffs... || - || ✔✔At || all || tower || controlled || airports || regardless || of || weather || conditions. The || lateral || dimensions || of || Class || D || airspace || are || based || on... || - || ✔✔The || instrument || procedures || for || which || the || controlled || airspace || is || established. If || a || control || tower || and || an || FSS || are || located || on || the || same || airport, || which || function || is || provided || by || the || FSS || during || those || periods || when || the || tower || is || closed? || - || ✔✔Airport || Advisory || Service.
Prior || to || entering || an || Airport || Advisory || Area, || a || pilot || should... || - || ✔✔Contact || the || local || FSS || for || airport || and || traffic || advisories. When || should || pilots || state || their || position || on || the || airport || when || calling || the || tower || for || takeoff? || - || ✔✔When || departing || from || a || runway || intersection. The || normal || radius || of || the || outer || area || of || Class || C || airspace || is... || - || ✔✔ 20 || NM. All || operations || within || Class || C || airspace || must || be... || - || ✔✔In || communications || with || the || responsible || ATC || facility. The || vertical || limit || of || Class || C || airspace || above || the || primary || airport || is || normally... || - || ✔✔4,000 || feet. Under || what || conditions || may || an || aircraft || operate || from || a || satellite || airport || within || Class || C || airspace? || - || ✔✔The || pilot || must || contact || ATC || as || soon || as || practicable || after || takeoff. What || initial || action || should || a || pilot || take || prior || to || entering || Class || C || airspace? || - || ✔✔Contact || approach || control || on || the || appropriate || frequency. TRSA || Service || in || the || terminal || radar || program || provides... || - || ✔✔Sequencing || and || separation || for || participating || VFR || aircraft. From || whom || should || a || departing || VFR || aircraft || request || radar || traffic || information || during || ground || operations? || - || ✔✔Ground || control, || on || initial || contact. Basic || radar || service || in || the || terminal || radar || program || is || best || described || as... || - || ✔✔Safety || alerts, || traffic || advisories || and || limited || vectoring || to || VFR || aircraft.
