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SUU Fixed Wing Private Pilot Exam 2026/2027 | 150+ Questions & Answers | Cirrus SR20 G6, V-Speeds, FAA Regulations, Weather, Airspace & Aeromedical Factors | Southern Utah University

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SUU Fixed Wing Private Pilot Questions 2026/2027 is a comprehensive 34-page private-pilot exam-preparation resource containing 150+ questions, answers and supporting illustrations focused on the Cirrus SR20 G6 and essential fixed-wing aviation knowledge. The aircraft-specific section covers critical V-speeds such as Vr, Vx, Vy, Vref, Vg, Vne, Vno, Vs0, Vs1, Vfe and parachute deployment speed. It also reviews the Lycoming IO-390-C3B6 engine, its stated 215 HP rating at 2700 RPM, oil temperature and pressure limitations, maximum takeoff and landing weight, baggage limitations and reference datum. Weight-and-balance questions explain center of gravity, arm, forward versus aft CG characteristics and the potential consequences of operating outside approved CG limitations. Aircraft airworthiness, inspections and equipment requirements receive extensive coverage. Students review annual and 100-hour inspections, Airworthiness Directives, VOR checks for IFR operations, altimeter/pitot-static inspections, transponder inspections and ELT requirements as presented in the document. The resource distinguishes Service Bulletins from Airworthiness Directives and explains Special Flight Permits and circumstances in which they may be issued. FAA day and night VFR equipment requirements are also reviewed, including the airspeed indicator, altimeter, tachometer, oil-pressure and temperature gauges, fuel gauges, magnetic compass, ELT, seat belts, anti-collision lights, position lights and electrical power source. Pilot privileges, limitations and regulatory knowledge constitute another major study area. The document reviews private-pilot privileges, pro-rata cost sharing, business-related flying, charitable flights, demonstration flights and other operations identified in the supplied material. Passenger-carrying recency requirements cover three takeoffs and landings within the preceding 90 days, with separate nighttime conditions. Students also review required pilot logbook entries, flight reviews, alcohol restrictions, oxygen-use rules, required preflight information and NTSB Part 830 concepts involving accidents, incidents, serious injuries, substantial aircraft damage and mandatory reporting circumstances. A substantial portion concentrates on aviation weather and weather-information products. METARs, TAFs, winds and temperatures aloft, AWOS, ASOS, PIREPs, AIRMETs, SIGMETs, Convective SIGMETs, surface analysis charts and significant weather prognostic charts are addressed. The guide differentiates AIRMET Tango, Sierra and Zulu and reviews severe turbulence, icing, volcanic ash, thunderstorms and reduced-visibility conditions. Atmospheric fundamentals include composition of the atmosphere, unequal heating, Coriolis force, moisture, humidity, relative humidity, dew point, atmospheric stability and high- and low-pressure systems. Weather hazards and meteorological processes are particularly detailed. Students review the cumulus, mature and dissipating stages of thunderstorms; wake, clear-air, mountain-wave, convective and mechanical turbulence; wind shear and microbursts; and clear, mixed and rime ice. Fog types include radiation, advection, precipitation-induced, upslope, steam and ice fog. The material also covers cold, warm, stationary and occluded fronts; sea, land, valley, mountain and katabatic winds; temperature inversions; cloud classifications; troposphere, stratosphere, mesosphere and thermosphere; and stable versus unstable air masses. Aeromedical factors and human performance are another important examination area. The resource defines spatial disorientation and reviews night myopia, inversion illusion, Coriolis illusion, elevator illusion, false horizon, flicker vertigo, the leans, autokinesis, graveyard spiral and somatogravic illusion. Hypoxia is divided into hypoxic, hypemic, stagnant and histotoxic types, with symptoms such as fatigue, impaired judgment, headache, reduced vision and cyanosis included in the supplied answers. Students also encounter stress, fatigue, hyperventilation, motion sickness, middle-ear and sinus issues and decompression-sickness considerations following scuba diving. Airspace and flight operations are covered through Military Operations Areas, Controlled Firing Areas, Warning Areas, Restricted Areas, Alert Areas, Prohibited Areas and National Security Areas. The document additionally reviews military training routes, Temporary Flight Restrictions, Terminal Radar Service Areas, published VFR routes, parachute operations and special flight rules areas. Instrument-system questions address pitot and static-system blockages and their effects on the airspeed indicator, altimeter and vertical speed indicator. Emergency preparation includes an engine-out sequence beginning with establishing best-glide speed, selecting a landing site and proceeding through troubleshooting, approach, radio and shutdown considerations. The final sections consolidate weather theory, aeronautical decision-making and flight knowledge. Topics include cloud-formation requirements, visibility categories, wind patterns, load factor and the DECIDE model: Detect, Estimate, Choose, Identify, Do and Evaluate. This broad coverage makes the document useful not only for reviewing Cirrus SR20 G6 operating figures but also for studying regulations, meteorology, human factors, airworthiness and operational decision-making associated with fixed-wing private-pilot training. Because this description summarizes the uploaded study guide, numerical values and answers are represented as supplied in the document rather than independently verified against current FAA publications or the current SR20 Pilot’s Operating Handbook. Relevant students: Southern Utah University fixed-wing aviation students, SUU private pilot students, Cirrus SR20 G6 student pilots, Private Pilot Certificate candidates, aviation and professional-pilot students, FAA knowledge-test learners, and students reviewing aircraft systems, V-speeds, regulations, airspace, aviation weather, aeromedical factors, weight and balance and private-pilot operations. Keywords: SUU Fixed Wing Private Pilot Questions, SUU Private Pilot Exam 2026, SUU aviation questions and answers, Cirrus SR20 G6 questions, Cirrus SR20 G6 exam, private pilot questions and answers, private pilot exam 2026, private pilot study guide, FAA private pilot exam, private pilot knowledge test, SR20 G6 V speeds, Cirrus SR20 V speeds, Lycoming IO 390 C3B6, aircraft weight and balance, center of gravity aircraft, FAA airworthiness requirements, aircraft inspections, FAR 91.205, VFR day equipment, VFR night equipment, private pilot privileges and limitations, pilot recency requirements, aviation weather exam, METAR and TAF, winds aloft, AIRMET, SIGMET, Convective SIGMET, aviation weather hazards, thunderstorm stages, microburst aviation, aircraft icing, aviation fog types, special use airspace, TFR aviation, aeromedical factors, spatial disorientation, hypoxia aviation, pitot static system, engine out emergency, NTSB 830, aviation decision making, DECIDE model, Southern Utah University aviation

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SUU Fixed Wing Private Pilot
Questions (Cirrus SR20 G6)
2026/2027 Exam All Answers
and Illustrations Given



Vr (rotation speed) - ANSWER ✔✔71 knots


Vx (lift off) - ANSWER ✔✔71 knots


Vx (At obstacle) - ANSWER ✔✔81 knots


Vy (best rate of climb) - ANSWER ✔✔92 knots


Go around - ANSWER ✔✔81 knots


Max cross wind - ANSWER ✔✔20 knots

,Vfe (max airspeed with flaps 50%) - ANSWER ✔✔150 knots


Vref (landing reference speed 50 feet above the ground) - ANSWER

✔✔78 knots


Vg (best glide) - ANSWER ✔✔92-100 knots


Vpd (max speed to deploy parachute) - ANSWER ✔✔133 knots


Vno (max cruising speed) - ANSWER ✔✔164 knots


Vne (never exceed) - ANSWER ✔✔201 knots


Vs0 (Stall speed full flaps) - ANSWER ✔✔62 knots


Vs1 (stall speed cruise) - ANSWER ✔✔71 knots


Vo (maximum operation maneuvering speed) - ANSWER ✔✔133-114

knots


Vfe (max airspeed with flaps 100%) - ANSWER ✔✔110 knots


Cirrus SR20 G6 engine - ANSWER ✔✔Lycoming IO-390-C3B6


Engine power rating - ANSWER ✔✔215 HP at 2700 RPM


Maximum Engine RPM - ANSWER ✔✔2700 RPM


Maximum oil temp - ANSWER ✔✔235 F

,Minimum oil temp for takeoff - ANSWER ✔✔100 F


Oil pressure Minimum idle - ANSWER ✔✔25 PSI


Oil pressure max startup - ANSWER ✔✔115 PSI


Normal oil pressure range during flight - ANSWER ✔✔55-95 PSI


Maximum takeoff/landing weight - ANSWER ✔✔3150 lbs


Maximum weight in baggage compartment - ANSWER ✔✔130 lbs


reference datum location - ANSWER ✔✔100 inches forward of the

firewall


What inspections are required to maintain airworthiness? - ANSWER

✔✔AD's as required


Annual- every 12 months

VOR- every 30 days (IFR)

100 hour- every 100 hours

Altimeter/Pitot Static- every 24 months (IFR)

Transponder- every 24 months

ELT- every 12 months, 1/2 battery life, or 1 hour cumulative use


3
COPYRIGHT©JOSHCLAY 2026/2027. YEAR PUBLISHED 2026. COMPANY REGISTRATION NUMBER: 619652435. TERMS OF USE. PRIVACY
STATEMENT. ALL RIGHTS RESERVED

, What must an airworthiness certificate have on it to be legal? -

ANSWER ✔✔a signature


What is the SR20 G6 glide ratio? - ANSWER ✔✔9:1 roughly 1.4 NM

to 1000'

Can you operate an aircraft above its maximum demonstrated

crosswind? - ANSWER ✔✔Yes, but you are operating out of the

range tested by test pilots.


SR20 maximum weight - ANSWER ✔✔3150 lbs


Why is balance of the aircraft important? - ANSWER ✔✔to maintain

positive control of the aircraft.


How will an aircraft behave with a forward CG? - ANSWER

✔✔forward CG results in greater flight stability and reduced danger of

sudden stalling, but also increased drag


How will an aircraft behave with an aft CG? - ANSWER ✔✔A CG

near the aft reduces drag and reduces stability of the aircraft


What is the difference between arm and CG? - ANSWER ✔✔an Arm

is the distance in inches from the reference datum line to the CG of an

item while CG is the point at which the object would balance

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Number of pages
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