Export your learner materials as an interactive game, a webpage, or FAQ style cheatsheet.
Unsaved Work Found!
It looks like you have unsaved work from a previous session. Would you like to restore it?
Total Categories: 5
The Cessna 172's prominence in Cessna's navigational boxes signifies its central role in the company's product history.
Answer: True
The Cessna 172's prominence in Cessna's navigational boxes signifies its central role and lineage within the company's product history, not a minor one.
What is the Cessna 172 Skyhawk primarily known for in terms of production history?
Answer: Being the most produced aircraft in history.
The Cessna 172 Skyhawk is primarily recognized as the most-produced aircraft in history, reflecting its extensive manufacturing and widespread use.
The Cessna 172 first flew in 1955, predating its predecessor, the Cessna 170.
Answer: False
The Cessna 172 first flew in 1955, not 1948, and was developed from the Cessna 170.
The primary distinction between the Cessna 172 and its predecessor, the Cessna 170, was the addition of tricycle landing gear.
Answer: True
The Cessna 172 was developed from the Cessna 170, with the principal design difference being the incorporation of tricycle landing gear instead of the 170's conventional landing gear.
The 172A model, introduced for the 1960 model year, was the first variant certified for floatplane operations.
Answer: True
The 172A model, introduced for the 1960 model year, was indeed the first variant of the Cessna 172 to be certified for floatplane operations.
Which aircraft served as the direct predecessor to the Cessna 172, differing mainly in its landing gear configuration?
Answer: Cessna 170
The Cessna 170 served as the direct predecessor to the Cessna 172, with the primary difference being the 172's adoption of tricycle landing gear.
The Cessna 172 Skyhawk is characterized by its high-wing configuration and single-engine design.
Answer: False
The Cessna 172 Skyhawk is characterized by a high-wing configuration and a single-engine design, contrary to the assertion of a low-wing and twin-engine configuration.
The 'Omni-Vision' feature, enhancing rear visibility, was introduced in the 1963 Cessna 172D model.
Answer: True
The 'Omni-Vision' feature, characterized by a cut-down rear fuselage and aft window, was introduced in the 1963 Cessna 172D model to improve rear visibility.
The Cessna 172B, introduced for the 1961 model year, adopted the 'Skyhawk' name as a standard trim level.
Answer: False
The 'Skyhawk' name was introduced as a deluxe option package with the 1961 Cessna 172B, not as a standard trim level across all models.
The 1964 Cessna 172E model replaced electrical fuses with circuit breakers in its redesigned instrument panel.
Answer: True
The 1964 Cessna 172E featured a redesigned instrument panel that incorporated circuit breakers, replacing the electrical fuses used in prior models.
The 1965 Cessna 172F model transitioned from electrically operated flaps to a lever-operated system.
Answer: False
The 1965 Cessna 172F model introduced electrically operated flaps, replacing the previous lever-operated system.
The 1967 Cessna 172H featured a shorter-stroke nose gear oleo designed to reduce drag.
Answer: True
The 1967 Cessna 172H featured a shorter-stroke nose gear oleo, which was designed to reduce drag and improve the aircraft's flight appearance.
The Cessna 172I model saw an increase in horsepower, utilizing a Lycoming engine that boosted cruise speed slightly.
Answer: False
The Cessna 172I model was equipped with a Lycoming engine, not a Continental engine, which provided a slight increase in horsepower and cruise speed.
The Cessna 172J was canceled because its proposed cantilever wing design proved too complex to manufacture.
Answer: False
The Cessna 172J was canceled not due to manufacturing complexity, but because the continued popularity of the existing 172 design with dealers and flight schools led Cessna to maintain its production.
The 1971 Cessna 172L model introduced tapered, tubular steel landing gear legs, which increased the landing gear track.
Answer: True
The 1971 Cessna 172L model introduced tapered, tubular steel landing gear legs, replacing the original flat spring steel legs, which resulted in an increased landing gear track.
The 'Camber-Lift' wing, designed to improve low-speed handling, was a feature of the 1973 Cessna 172M.
Answer: True
The 1973 Cessna 172M model featured a 'Camber-Lift' wing with a drooped leading edge, specifically designed to improve low-speed handling characteristics.
The 'Skyhawk II' variant, introduced in 1974, offered reduced standard equipment compared to the baseline 172M.
Answer: False
The 'Skyhawk II' variant, introduced in 1974, offered higher standard equipment levels compared to the baseline 172M and Skyhawk models.
The Cessna 172N, introduced in 1977, was powered by an engine designed to run on 100-octane fuel.
Answer: True
The Cessna 172N was powered by an engine designed for 100-octane fuel, not 80/87 octane fuel as stated in the original assertion.
Cessna skipped the 'O' model designation for the 172 to avoid confusion with the number zero.
Answer: True
Cessna intentionally skipped the 'O' model designation for the 172 to prevent potential confusion with the numeral zero.
The 172P Skyhawk P replaced the unreliable Lycoming O-320-H2AD engine with a more dependable Lycoming O-320-D2J.
Answer: True
The 172P Skyhawk P model was indeed introduced to replace the less reliable Lycoming O-320-H2AD engine with the more dependable Lycoming O-320-D2J.
In the 1982 Cessna 172P, landing lights were moved from the nose to the wings to increase bulb lifespan.
Answer: True
The landing lights on the 1982 Cessna 172P were moved from the nose to the wings, a change intended to increase the lifespan of the bulbs.
The 'Cutlass' designation was introduced for the 1983 Cessna 172Q model, which featured a 180 hp engine.
Answer: True
The 'Cutlass' designation was introduced for the 1983 Cessna 172Q model, which was equipped with a 180 hp engine, not a standard 160 hp engine.
The 1996 Cessna 172R Skyhawk R was the first 172 model to feature a factory-fitted fuel-injected engine.
Answer: True
The 1996 Cessna 172R Skyhawk R was the first model to feature a factory-fitted fuel-injected engine, not a diesel engine.
The Cessna 172S Skyhawk SP, introduced in 1998, has a more powerful engine than the 172R model.
Answer: True
The Cessna 172S Skyhawk SP features a more powerful 180 hp engine compared to the 172R's 160 hp engine.
The Cessna 175 Skylark was rebranded as the P172D Powermatic due to its excellent engine reliability.
Answer: False
The Cessna 175 Skylark was rebranded as the P172D Powermatic due to its reputation for poor engine reliability, not excellent reliability.
The R172K Hawk XP was particularly favored for floatplane operations due to its standard 160 hp engine.
Answer: False
The R172K Hawk XP was favored for floatplane operations due to its more powerful 195 hp engine and constant-speed propeller, which significantly improved water takeoff performance compared to the standard 172's 160 hp engine.
The 172RG Cutlass RG was distinguished by its fixed landing gear and a standard 150 hp engine.
Answer: False
The 172RG Cutlass RG was distinguished by its retractable landing gear and a 180 hp engine, not fixed landing gear and a 150 hp engine.
The J172T Turbo Skyhawk JT-A, introduced in 2015, was powered by a Pratt & Whitney PT6 turboprop engine.
Answer: False
The J172T Turbo Skyhawk JT-A, introduced in 2015, was powered by a Continental CD-155 diesel engine, not a Pratt & Whitney PT6 turboprop.
The 172TD Skyhawk TD project, which aimed to use a Thielert Centurion 2.0 engine, was successfully completed and entered production.
Answer: False
The 172TD Skyhawk TD project, aiming to use a Thielert Centurion 2.0 engine, was canceled in 2013 due to Thielert's bankruptcy, and did not enter production.
The Cessna 172B model featured shorter landing gear and an increased gross weight compared to earlier versions.
Answer: True
The Cessna 172B, introduced for the 1961 model year, featured shorter landing gear and an increased gross weight compared to its predecessors.
The 1962 Cessna 172C model included an optional autopilot and redesigned seats with six-way adjustability.
Answer: True
The 1962 Cessna 172C model offered optional autopilot features and redesigned seats with six-way adjustability.
The 172H model replaced its electric stall warning horn with a pneumatic one.
Answer: True
The 172H model featured a replacement of the electric stall warning horn with a pneumatic system.
The Cessna 172K model offered optional long-range wing fuel tanks.
Answer: True
Optional long-range wing fuel tanks were made available for the 1969 Cessna 172K model.
The 172RG Cutlass RG featured retractable landing gear, making it unique within the 172 series.
Answer: True
The 172RG Cutlass RG was indeed unique within the 172 series for its incorporation of retractable landing gear.
The Cessna 172R has a maximum takeoff weight of 2,450 pounds.
Answer: True
The maximum takeoff weight specified for the Cessna 172R Skyhawk R is 2,450 pounds.
The Cessna 172R has a never-exceed speed (Vne) of 163 knots.
Answer: True
The never-exceed speed (Vne) for the Cessna 172R is indeed 163 knots.
The Cessna 172R is powered by a 160 horsepower Lycoming IO-360-L2A engine.
Answer: True
The Cessna 172R is powered by a Lycoming IO-360-L2A engine rated at 160 horsepower.
The Cessna 172R has a service ceiling of 13,500 feet.
Answer: True
The service ceiling of the Cessna 172R is 13,500 feet, not 10,000 feet.
The Cessna 172R utilizes a two-bladed propeller.
Answer: True
The Cessna 172R is equipped with a two-bladed propeller, not a three-bladed propeller.
The Cessna 172B model featured a redesigned cowling and a pointed propeller spinner.
Answer: True
The Cessna 172B model incorporated a redesigned cowling and a pointed propeller spinner as part of its updates.
The 1966 Cessna 172G model featured a longer, more pointed spinner compared to previous models.
Answer: True
The 1966 Cessna 172G model featured a longer, more pointed spinner, contrary to the assertion of a shorter, blunter spinner.
The Cessna 172I model was equipped with a 150 horsepower Lycoming engine, a slight increase over the previous Continental engines.
Answer: True
The Cessna 172I model was equipped with a 150 horsepower Lycoming O-320-E2D engine, representing a slight increase over the horsepower of the previous Continental engines used in earlier models.
The 1973 Cessna 172M model featured a 'Camber-Lift' wing designed to improve low-speed handling characteristics.
Answer: True
The 'Camber-Lift' wing introduced on the 1973 Cessna 172M was designed to enhance low-speed handling, not high-speed performance.
The 172RG Cutlass RG offered a higher cruise speed and greater range than the standard 172, but at a significantly higher cost.
Answer: True
While the 172RG Cutlass RG offered improved cruise speed and range, it came at a significantly higher cost compared to the standard Cessna 172.
Which model year introduced the 'Omni-Vision' feature, characterized by a cut-down rear fuselage and aft window?
Answer: 1963 (172D)
The 'Omni-Vision' feature, which included a cut-down rear fuselage and an aft window, was introduced with the 1963 Cessna 172D model.
The Cessna 172F, introduced for the 1965 model year, featured which significant operational change?
Answer: Electrically operated flaps.
The 1965 Cessna 172F model marked a significant operational change by introducing electrically operated flaps, replacing the previous manual lever system.
What engine powered the 1977 Cessna 172N 'Skyhawk/100', and what was unique about its fuel requirement?
Answer: 160 hp Lycoming O-320-H2AD, designed for 100-octane fuel.
The 1977 Cessna 172N 'Skyhawk/100' was powered by a 160 hp Lycoming O-320-H2AD engine, uniquely designed to operate on 100-octane fuel.
Which Cessna 172 model was the first to feature a factory-fitted fuel-injected engine?
Answer: 172R Skyhawk R
The 1996 Cessna 172R Skyhawk R was the first model to be equipped with a factory-fitted fuel-injected engine.
The 172RG Cutlass RG differed from standard 172 models primarily due to which feature?
Answer: Its retractable landing gear.
The 172RG Cutlass RG was primarily distinguished from standard 172 models by its incorporation of retractable landing gear.
What was the main drawback of the 172RG Cutlass RG compared to a standard Cessna 172?
Answer: Higher purchase price and maintenance costs.
A significant drawback of the 172RG Cutlass RG compared to a standard Cessna 172 was its substantially higher purchase price and increased maintenance and insurance costs.
The Cessna 172RG Cutlass RG was distinguished by its retractable landing gear and a standard 180 hp engine.
Answer: True
The 172RG Cutlass RG was distinguished by its retractable landing gear and a standard 180 hp engine, setting it apart from earlier 172 models.
What was the reason for the cancellation of the 172TD Skyhawk TD project?
Answer: Thielert, the engine supplier, filed for bankruptcy.
The 172TD Skyhawk TD project was canceled primarily because Thielert, the supplier of the intended Centurion 2.0 diesel engine, filed for bankruptcy.
Which model year saw the introduction of the 'Skyhawk' name as a deluxe option package?
Answer: 1961 (172B)
The 'Skyhawk' name was introduced as a deluxe option package with the Cessna 172B, which was introduced for the 1961 model year.
What modification was made to the landing lights on the Cessna 172P for the 1982 model year?
Answer: They were moved from the nose to the wings.
For the 1982 model year, the landing lights on the Cessna 172P were relocated from the nose to the wings, a change intended to increase the lifespan of the bulbs.
The R172K Hawk XP variant was noted for its suitability for floatplane operations primarily because of its:
Answer: More powerful engine and constant-speed propeller.
The R172K Hawk XP was noted for its suitability for floatplane operations primarily due to its more powerful 195 hp engine and constant-speed propeller, which significantly improved water takeoff performance compared to the standard 172.
The Cessna 172I model, introduced in 1968, featured an engine upgrade that resulted in:
Answer: A slight increase in optimal cruise speed.
The Cessna 172I model, introduced in 1968, featured an engine upgrade to a 150 horsepower Lycoming engine, which resulted in a slight increase in optimal cruise speed.
What was the purpose of the 'Camber-Lift' wing design introduced on the 1973 Cessna 172M?
Answer: To enhance low-speed handling characteristics.
The 'Camber-Lift' wing design introduced on the 1973 Cessna 172M was intended to improve low-speed handling characteristics.
The Cessna 172R Skyhawk R featured which significant interior improvements?
Answer: Soundproofing, a new ventilation system, and upgraded seats.
The Cessna 172R Skyhawk R featured significant interior improvements, including enhanced soundproofing, a new ventilation system, and upgraded seats.
What was the primary reason the J172T Turbo Skyhawk JT-A was discontinued?
Answer: Poor sales due to its high price.
The J172T Turbo Skyhawk JT-A was discontinued due to poor sales, primarily attributed to its high price relative to diesel conversion kits for existing airframes.
The Cessna 172B, introduced for the 1961 model year, featured which of the following modifications?
Answer: Shorter landing gear and a pointed propeller spinner.
The Cessna 172B, introduced for the 1961 model year, featured modifications such as shorter landing gear, a reshaped cowling, and a pointed propeller spinner.
The 172P Skyhawk P model was introduced to address reliability issues associated with which previous engine?
Answer: Lycoming O-320-H2AD
The 172P Skyhawk P model was introduced to address reliability issues associated with the Lycoming O-320-H2AD engine used in the preceding 172N model.
The Cessna 172E model, introduced for the 1964 model year, featured which key change in its electrical system?
Answer: Replacement of fuses with circuit breakers.
The 1964 Cessna 172E model featured a key change in its electrical system: the adoption of circuit breakers to replace the electrical fuses used in earlier models.
The Cessna 172L model, introduced in 1971, featured a change in its landing gear design, specifically:
Answer: Tapered, tubular steel legs replacing flat spring steel.
The Cessna 172L model, introduced in 1971, featured a change in its landing gear design, specifically the introduction of tapered, tubular steel legs that replaced the original flat spring steel legs.
The Cessna 172S Skyhawk SP, introduced in 1998, featured an engine upgrade compared to the 172R, resulting in:
Answer: An increase of 20 horsepower.
The Cessna 172S Skyhawk SP, introduced in 1998, featured an engine upgrade to a 180 horsepower Lycoming IO-360-L2A engine, a 20 hp increase over the 172R's engine.
The Cessna 172R has a specified rate of climb of:
Answer: 721 feet per minute
The Cessna 172R has a specified rate of climb of 721 feet per minute.
The Cessna 175 Skylark was rebranded as the P172D Powermatic primarily due to issues with its:
Answer: Engine reliability
The Cessna 175 Skylark was rebranded as the P172D Powermatic primarily due to its reputation for poor engine reliability.
By 2015, Cessna and its partners had produced over 44,000 units of the Cessna 172, making it the most-produced aircraft in history.
Answer: True
The Cessna 172 is recognized as the most-produced aircraft in history, with over 44,000 units built by 2015.
The Cessna 172 experienced a production halt between 1986 and 1996 primarily due to escalating product liability costs.
Answer: True
Cessna halted production of the 172 in 1986 primarily due to escalating product liability costs, resuming production in 1996.
What was the primary reason cited for Cessna halting the production of the Cessna 172 in 1986?
Answer: Escalating product liability costs.
Cessna halted production of the 172 in 1986 primarily due to escalating product liability costs, which made continued manufacturing financially untenable.
Which of the following was a competitor to the Cessna 172 in the light general aviation market?
Answer: Piper PA-28 Cherokee
The Piper PA-28 Cherokee is recognized as a significant competitor to the Cessna 172 in the light general aviation market.
The T-41 Mescalero, a military variant of the Cessna 172, was used by the United States Navy for pilot training.
Answer: False
The T-41 Mescalero, a variant of the Cessna 172, was utilized by the United States Air Force and Army for pilot training, not the Navy.
The Cessna 172's endurance record flight lasted for over 70 days.
Answer: False
The Cessna 172's endurance record flight, set by Robert Timm and John Cook, lasted for over 64 days, not 70 days.
The Reims Aviation license production primarily focused on military jet aircraft based on Cessna designs.
Answer: False
Reims Aviation produced Cessna aircraft under license, primarily piston-engine models like various F172 variants, not military jet aircraft.
The mid-air collision between PSA Flight 182 and a Cessna 172 in 1978 resulted in a significant number of fatalities, primarily attributed to:
Answer: Air traffic control error.
The mid-air collision between PSA Flight 182 and a Cessna 172 in 1978 was primarily attributed to air traffic control error, leading to a substantial number of fatalities.
What record did Robert Timm and John Cook set in a Cessna 172 between December 1958 and February 1959?
Answer: World record for refueled flight endurance.
Robert Timm and John Cook set the world record for refueled flight endurance in a Cessna 172 between December 1958 and February 1959, flying for over 64 days.
Which of the following countries has operated the Cessna 172 or its variants in military or border patrol roles?
Answer: Pakistan
Pakistan is among the numerous countries that have operated the Cessna 172 or its variants in military or border patrol roles.
What was the primary purpose of the Mathias Rust incident in 1987 involving a Reims Cessna F172P?
Answer: To highlight vulnerabilities in Soviet air defense systems.
The Mathias Rust incident in 1987, involving his flight in a Reims Cessna F172P to Moscow, served to highlight significant vulnerabilities in Soviet air defense systems.