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Cirrus SR20 G6 POH – SUU Actual Exam
2026/2027: Complete Test with Latest Updated
Questions and Answers | Already Passed for Pilot
Success – Pass Guaranteed - A+ Graded
Section 1: General Information & Limitations (12 Questions)
Q1: What is the maximum structural cruising speed (VNO) for the Cirrus SR20 G6?
A. 133 KIAS
B. 146 KIAS [CORRECT]
C. 163 KIAS
D. 178 KIAS
Correct Answer: B
Rationale: The SR20 G6 VNO (maximum structural cruising speed) is 146 KIAS as specified in
Section 2 (Limitations) of the Cirrus SR20 G6 POH. This is the maximum speed for normal
operations in smooth air. VNE (never exceed) is 163 KIAS (Option C). VA (maneuvering speed)
varies with weight but is approximately 133 KIAS at max gross weight (Option A). Option D
exceeds all published limitations.
Q2: What is the maximum takeoff weight for the Cirrus SR20 G6?
A. 2,800 lbs
B. 3,000 lbs [CORRECT]
C. 3,100 lbs
D. 3,400 lbs
Correct Answer: B
Rationale: Per the SR20 G6 POH Section 2 (Limitations), the maximum takeoff weight is 3,000
lbs (3,040 lbs maximum ramp weight). This is a critical memory item for SUU stage checks.
Option A is below maximum. Option C and D exceed SR20 structural limits (SR22 weights).
Students frequently confuse SR20 and SR22 weight limitations.
Q3: The Continental IO-360-ES engine in the SR20 G6 is rated at what horsepower?
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A. 180 HP
B. 200 HP
C. 215 HP [CORRECT]
D. 310 HP
Correct Answer: C
Rationale: The Continental IO-360-ES engine is rated at 215 HP at 2700 RPM as specified in
POH Section 1 (General) and Section 2 (Limitations). This is a memory item for SUU oral
examinations. Option A was the original SR20 engine rating (later upgraded). Option B is not
used. Option D is the SR22 engine rating (Continental IO-550), a common distractor.
Q4: What is the total usable fuel capacity of the SR20 G6?
A. 40 gallons
B. 48 gallons
C. 56 gallons [CORRECT]
D. 81 gallons
Correct Answer: C
Rationale: The SR20 G6 has 56 gallons usable fuel (28 gallons per wing tank) as specified in
POH Section 1 and 2. This provides approximately 4-5 hours endurance depending on power
settings. Option A reflects older aircraft configurations. Option B is incorrect. Option D is the
SR22 fuel capacity (81 gallons), a common student error.
Q5: What is the maximum operating altitude for the Cirrus SR20 G6?
A. 10,000 feet
B. 14,000 feet
C. 17,500 feet [CORRECT]
D. 25,000 feet
Correct Answer: C
Rationale: Per POH Section 2 (Limitations), the maximum operating altitude is 17,500 feet
pressure altitude. This limitation is based on the non-pressurized cabin, oxygen requirements (14
CFR 91.211), and engine performance characteristics. Options A and B are below the service
ceiling. Option D exceeds the aircraft's capabilities and would require pressurization and turbine
power.
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Q6: What is the maximum flap extended speed (VFE) for the Cirrus SR20 G6?
A. 100 KIAS
B. 119 KIAS [CORRECT]
C. 133 KIAS
D. 146 KIAS
Correct Answer: B
Rationale: VFE (maximum flap extended speed) is 119 KIAS per POH Section 2. This is the
maximum speed at which flaps may be extended or operated. Exceeding VFE can cause
structural damage to the flap system. Option A is too conservative. Option C is VA (maneuvering
speed at max weight). Option D is VNO (normal operating speed).
Q7: The Cirrus SR20 G6 is certified in what category?
A. Normal Category only
B. Utility Category only
C. Normal and Utility Category [CORRECT]
D. Aerobatic Category
Correct Answer: C
Rationale: The SR20 G6 is certified in both Normal and Utility Categories per the Type
Certificate Data Sheet and POH Section 1. In Utility Category, certain maneuvers (spins, steep
turns >60°) are permitted with weight restrictions (typically max 2,700 lbs for Utility). Normal
Category prohibits spins and limits bank angles to 60°. This is critical for SUU training
operations and utility category maneuvers during commercial training.
Q8: What is the minimum oil capacity for the Continental IO-360-ES engine?
A. 4 quarts
B. 6 quarts
C. 8 quarts [CORRECT]
D. 12 quarts
Correct Answer: C
Rationale: Per POH Section 1 and engine specifications, the minimum oil capacity is 8 quarts
(with 2 quarts minimum for operation). Maximum capacity is approximately 8-9 quarts. This is a
preflight inspection item at SUU. Low oil quantity can cause engine failure; students must verify
oil level is within dipstick marks during preflight.
Cirrus SR20 G6 POH – SUU Actual Exam
2026/2027: Complete Test with Latest Updated
Questions and Answers | Already Passed for Pilot
Success – Pass Guaranteed - A+ Graded
Section 1: General Information & Limitations (12 Questions)
Q1: What is the maximum structural cruising speed (VNO) for the Cirrus SR20 G6?
A. 133 KIAS
B. 146 KIAS [CORRECT]
C. 163 KIAS
D. 178 KIAS
Correct Answer: B
Rationale: The SR20 G6 VNO (maximum structural cruising speed) is 146 KIAS as specified in
Section 2 (Limitations) of the Cirrus SR20 G6 POH. This is the maximum speed for normal
operations in smooth air. VNE (never exceed) is 163 KIAS (Option C). VA (maneuvering speed)
varies with weight but is approximately 133 KIAS at max gross weight (Option A). Option D
exceeds all published limitations.
Q2: What is the maximum takeoff weight for the Cirrus SR20 G6?
A. 2,800 lbs
B. 3,000 lbs [CORRECT]
C. 3,100 lbs
D. 3,400 lbs
Correct Answer: B
Rationale: Per the SR20 G6 POH Section 2 (Limitations), the maximum takeoff weight is 3,000
lbs (3,040 lbs maximum ramp weight). This is a critical memory item for SUU stage checks.
Option A is below maximum. Option C and D exceed SR20 structural limits (SR22 weights).
Students frequently confuse SR20 and SR22 weight limitations.
Q3: The Continental IO-360-ES engine in the SR20 G6 is rated at what horsepower?
,2
A. 180 HP
B. 200 HP
C. 215 HP [CORRECT]
D. 310 HP
Correct Answer: C
Rationale: The Continental IO-360-ES engine is rated at 215 HP at 2700 RPM as specified in
POH Section 1 (General) and Section 2 (Limitations). This is a memory item for SUU oral
examinations. Option A was the original SR20 engine rating (later upgraded). Option B is not
used. Option D is the SR22 engine rating (Continental IO-550), a common distractor.
Q4: What is the total usable fuel capacity of the SR20 G6?
A. 40 gallons
B. 48 gallons
C. 56 gallons [CORRECT]
D. 81 gallons
Correct Answer: C
Rationale: The SR20 G6 has 56 gallons usable fuel (28 gallons per wing tank) as specified in
POH Section 1 and 2. This provides approximately 4-5 hours endurance depending on power
settings. Option A reflects older aircraft configurations. Option B is incorrect. Option D is the
SR22 fuel capacity (81 gallons), a common student error.
Q5: What is the maximum operating altitude for the Cirrus SR20 G6?
A. 10,000 feet
B. 14,000 feet
C. 17,500 feet [CORRECT]
D. 25,000 feet
Correct Answer: C
Rationale: Per POH Section 2 (Limitations), the maximum operating altitude is 17,500 feet
pressure altitude. This limitation is based on the non-pressurized cabin, oxygen requirements (14
CFR 91.211), and engine performance characteristics. Options A and B are below the service
ceiling. Option D exceeds the aircraft's capabilities and would require pressurization and turbine
power.
, 3
Q6: What is the maximum flap extended speed (VFE) for the Cirrus SR20 G6?
A. 100 KIAS
B. 119 KIAS [CORRECT]
C. 133 KIAS
D. 146 KIAS
Correct Answer: B
Rationale: VFE (maximum flap extended speed) is 119 KIAS per POH Section 2. This is the
maximum speed at which flaps may be extended or operated. Exceeding VFE can cause
structural damage to the flap system. Option A is too conservative. Option C is VA (maneuvering
speed at max weight). Option D is VNO (normal operating speed).
Q7: The Cirrus SR20 G6 is certified in what category?
A. Normal Category only
B. Utility Category only
C. Normal and Utility Category [CORRECT]
D. Aerobatic Category
Correct Answer: C
Rationale: The SR20 G6 is certified in both Normal and Utility Categories per the Type
Certificate Data Sheet and POH Section 1. In Utility Category, certain maneuvers (spins, steep
turns >60°) are permitted with weight restrictions (typically max 2,700 lbs for Utility). Normal
Category prohibits spins and limits bank angles to 60°. This is critical for SUU training
operations and utility category maneuvers during commercial training.
Q8: What is the minimum oil capacity for the Continental IO-360-ES engine?
A. 4 quarts
B. 6 quarts
C. 8 quarts [CORRECT]
D. 12 quarts
Correct Answer: C
Rationale: Per POH Section 1 and engine specifications, the minimum oil capacity is 8 quarts
(with 2 quarts minimum for operation). Maximum capacity is approximately 8-9 quarts. This is a
preflight inspection item at SUU. Low oil quantity can cause engine failure; students must verify
oil level is within dipstick marks during preflight.
