What is the Cessna 172 Skyhawk?

The Cessna 172 Skyhawk is an American-built, four-seat, single-engine aircraft with a high-wing configuration. It is manufactured by Cessna and is recognized as the most-produced aircraft in history, having been developed from the earlier Cessna 170 model.

When did the Cessna 172 first fly, and what was its predecessor?

The Cessna 172 first flew on June 12, 1955. It was developed from the 1948 Cessna 170, with the key difference being the addition of tricycle landing gear instead of the 170's conventional landing gear.

What makes the Cessna 172 historically significant in terms of production numbers?

The Cessna 172 holds the distinction of being the most-produced aircraft in history. Cessna and its partners had built over 44,000 units by 2015, and the aircraft remains in production today, with a brief hiatus between 1986 and 1996.

What were the primary competitors of the Cessna 172 in the light general aviation market?

Throughout its history, the Cessna 172's main competitors included the Beechcraft Musketeer and the Grumman American AA-5 series. More recently, the Piper PA-28 Cherokee, Diamond DA40 Diamond Star, and Cirrus SR20 are considered competitors.

How did the Cessna 172 evolve from the Cessna 170 in its early design?

The Cessna 172 began as a variant of the Cessna 170, initially featuring tricycle landing gear and a redesigned tailfin. It was first certified as the Model 172 by being added to the Cessna 170's type certificate, later receiving its own.

What aesthetic changes were made to the Cessna 172 in the early 1960s?

In 1960, the 172A model introduced revised landing gear and a swept-back tailfin, which became a standard feature. By 1963, the 172D featured a cut-down rear fuselage with an aft window, marketed as 'Omni-Vision,' enhancing rear visibility.

Why did Cessna halt production of the 172 in 1986, and when did it resume?

Cessna halted production of the 172 in 1986 primarily due to escalating product liability costs. Production resumed in 1996 with the introduction of the Cessna 172R Skyhawk.

What types of modifications are available for the Cessna 172 through Supplemental Type Certificates (STCs)?

The Cessna 172 can be modified with various STCs, including upgrades for increased engine power (from 180 to 210 hp), installation of constant-speed propellers, compatibility with automobile gasoline, additional fuel tank capacity, drag-reducing wheel pants, and STOL (Short Takeoff and Landing) kits.

What notable world record was set using a Cessna 172?

From December 1958 to February 1959, Robert Timm and John Cook set the world record for refueled flight endurance in a Cessna 172. They flew for 64 days, 22 hours, 19 minutes, and 5 seconds, covering approximately 150,000 miles, as part of a fundraising effort for the Damon Runyon Cancer Fund.

What was the significance of the 172A model introduced for the 1960 model year?

The 172A, introduced for the 1960 model year, featured a swept-back vertical tail and rudder, which became a characteristic design element for subsequent models. It was also the first 172 variant certified for floatplane operations.

How did the Cessna 172B, introduced for the 1961 model year, differ from previous versions?

The 172B featured shorter landing gear, lengthened engine mounts, a reshaped cowling, a pointed propeller spinner, and an increased gross weight. It also adopted the stepped firewall and wider instrument panel from the Cessna 175, and the 'Skyhawk' name was introduced as a deluxe option package.

What improvements were introduced with the 1962 Cessna 172C model?

The 1962 Cessna 172C introduced fiberglass wingtips, redesigned wheel fairings, a key starter (replacing the pull-starter), and optional autopilot. The seats were also redesigned for six-way adjustability, with an optional child seat available.

What was the 'Omni-Vision' feature and in which model year was it introduced?

The 'Omni-Vision' feature, introduced in the 1963 Cessna 172D, consisted of a cut-down rear fuselage with a wraparound rear window, significantly improving rear visibility. This model also featured a one-piece windshield and an increased horizontal stabilizer span.

What key electrical system change occurred with the 1964 Cessna 172E?

The 1964 Cessna 172E featured a redesigned instrument panel with center-mounted avionics and the adoption of circuit breakers to replace the electrical fuses used in earlier models.

What significant change in flap operation was introduced with the 1965 Cessna 172F?

The 1965 Cessna 172F introduced electrically operated flaps, replacing the previous lever-operated system. This model also featured improved instrument lighting.

How did the 172G model, introduced for the 1966 model year, differ from the 172F?

The 1966 Cessna 172G featured a longer, more pointed spinner. It was offered in a basic 172 version and an upgraded Skyhawk version, with the Skyhawk being more expensive.

What changes were made to the landing gear and engine cowling in the 1967 Cessna 172H?

The 1967 Cessna 172H featured a shorter-stroke nose gear oleo to reduce drag and improve flight appearance. It also introduced a new cowling with shock mounts for reduced noise and cowl cracking, and replaced the electric stall warning horn with a pneumatic one.

What engine upgrade did the 1968 Cessna 172I receive, and how did it affect performance?

The 1968 Cessna 172I was equipped with a Lycoming O-320-E2D engine, producing 150 horsepower, an increase of 5 hp over the previous Continental engines. This resulted in a slight increase in optimal cruise speed from 130 mph to 131 mph true airspeed (TAS).

What was the intended purpose of the Cessna 172J, and why was it canceled?

The Cessna 172J was planned as a replacement for the 172, featuring a more sloping windshield and a strutless cantilever wing. However, its development was canceled because the popularity of the existing 172 with dealers and flight schools led Cessna to continue its production.

What modifications were made to the tail and windows in the 1969 Cessna 172K?

The 1969 Cessna 172K featured a redesigned tailfin cap and enlarged rear windows, increasing their area by 16 square inches. Optional long-range wing fuel tanks were also offered.

What was the significant change in the landing gear introduced with the 1971 Cessna 172L?

The 1971 Cessna 172L introduced tapered, tubular steel landing gear legs, replacing the original flat spring steel legs. This change increased the landing gear width by 12 inches but required aerodynamic fairings to maintain performance.

What new wing design was incorporated into the 1973 Cessna 172M?

The 1973 Cessna 172M featured a 'Camber-Lift' wing with a drooped leading edge, designed to improve low-speed handling characteristics.

What distinguished the 'Skyhawk II' model introduced in 1974?

The 1974 Cessna 172M introduced the 'Skyhawk II' variant, which offered higher standard equipment levels compared to the baseline 172M and Skyhawk models. This included a second nav/comm radio, an ADF and transponder, larger baggage compartment, and dual nose-mounted landing lights.

When did Cessna begin exclusively using the 'Skyhawk' designation, and what instrument panel change occurred around that time?

Cessna began exclusively using the 'Skyhawk' designation starting with the 1976 model year. This model year also saw a redesigned instrument panel to accommodate more avionics, with gauges relocated for improved pilot readability.

What was the key feature of the 1977 Cessna 172N Skyhawk/100?

The 1977 Cessna 172N, named 'Skyhawk/100', was powered by a 160 horsepower Lycoming O-320-H2AD engine designed to run on 100-octane fuel, unlike previous engines that used 80/87 octane fuel. This model also introduced pre-select flap control and optional rudder trim.

Why was there no 'O' model Cessna 172?

Cessna skipped the 'O' model designation for the 172 to avoid confusion with the number zero.

What engine reliability issue led to the development of the 172P Skyhawk P?

The 172P Skyhawk P, introduced for the 1981 model year, replaced the Lycoming O-320-H2AD engine found in the 172N, which had proven to be unreliable. The 172P featured the Lycoming O-320-D2J engine.

What change was made to the landing lights in the 1982 Cessna 172P?

For the 1982 model year, the landing lights on the Cessna 172P were moved from the nose to the wings. This relocation was intended to increase the lifespan of the bulbs.

What was the 'Cutlass' designation, and how did it relate to the 172P?

The 'Cutlass' designation was introduced for the 1983 model year with the 172Q. This aircraft was essentially a 172P equipped with a more powerful 180 horsepower Lycoming O-360-A4N engine, offering improved cruise speed and useful load compared to the 172P.

What were the key features of the 1996 Cessna 172R Skyhawk R?

The 1996 Cessna 172R Skyhawk R was powered by a derated Lycoming IO-360-L2A engine producing 160 horsepower. It was the first Cessna 172 with a factory-fitted fuel-injected engine and featured significant interior improvements, including soundproofing, a new ventilation system, and upgraded seats.

What engine powers the 1998 Cessna 172S Skyhawk SP, and how does it compare to the 172R?

The 1998 Cessna 172S Skyhawk SP is powered by a Lycoming IO-360-L2A engine producing 180 horsepower, a 20 hp increase over the 172R's engine due to a higher maximum engine RPM. This also resulted in an increased maximum takeoff weight for the 172S.

What was the purpose of the Cessna 175 Skylark rebranding as the P172D Powermatic?

Due to the Cessna 175 Skylark's reputation for poor engine reliability, Cessna rebranded it for the 1963 model year as the P172D Powermatic. This version featured a more powerful 175 hp Continental GO-300-E engine with a geared reduction drive and a constant-speed propeller, offering increased cruise speed.

What military variants were based on the R172E model?

The R172E served as the basis for the military's T-41 Mescalero program, with variants including the T-41B for the US Army, T-41C for the USAF Academy, and T-41D for the US Military Aid Program. These variants featured different electrical systems, engines, and equipment configurations.

What was the R172K Hawk XP, and what was its advantage for floatplane operations?

The R172K Hawk XP, introduced for the 1977 model year, was a civilian version powered by a 195 hp Continental IO-360 engine driving a constant-speed propeller. While its increased performance over the standard 172 was debated, it was well-regarded for floatplane use, as its extra power significantly improved water takeoff performance compared to the standard 172.

What distinguished the 172RG Cutlass RG from other 172 models?

The 172RG Cutlass RG, introduced in 1980, was unique among the 172 series for featuring retractable landing gear. It also had a more powerful 180 hp Lycoming O-360-F1A6 engine, a variable-pitch constant-speed propeller, and greater fuel capacity, resulting in a higher cruise speed and range.

What were the advantages and disadvantages of the 172RG Cutlass RG compared to a standard 172?

The 172RG offered higher cruise speed and greater range than the standard 172. However, it was significantly more expensive, had higher maintenance and insurance costs due to the retractable gear, and its center of gravity could be too far aft, affecting longitudinal stability.

What was the J172T Turbo Skyhawk JT-A, and why was it discontinued?

The J172T Turbo Skyhawk JT-A, introduced in 2015, was powered by a 155 hp Continental CD-155 diesel engine. It offered improved fuel efficiency and range but was discontinued in May 2018 due to poor sales, largely attributed to its high price, which was double that of diesel conversion kits for existing airframes.

What was the purpose of the canceled 172TD Skyhawk TD project?

The 172TD Skyhawk TD project, announced in 2007, aimed to produce a diesel-powered 172 using a Thielert Centurion 2.0 engine. It was canceled in 2013 due to Thielert's bankruptcy but was later refined into the Turbo Skyhawk JT-A.

Which military force used the Cessna T-41 Mescalero as a primary trainer?

The United States Air Force and Army utilized the Cessna T-41 Mescalero, a variant of the 172, as a primary trainer and for initial flight screening.

Which countries have operated the Cessna 172 or its variants in military or border patrol roles?

Numerous countries have operated the Cessna 172 or its variants, including the United States (Air Force, Army, Border Patrol), Ireland (Air Corps), Angola, Austria, Bolivia, Chile, Colombia, Ecuador, Guatemala, Honduras, Indonesia, Iraq, Liberia, Lithuania, Madagascar, Nicaragua, Pakistan, Philippines, Saudi Arabia, and Singapore.

What notable incident involved Mathias Rust and a Cessna F172P?

On May 28, 1987, German teenager Mathias Rust used a rented Reims Cessna F172P to fly unauthorized through Soviet airspace, landing near Red Square in Moscow without being intercepted by air defenses. This flight highlighted significant vulnerabilities in Soviet air defense systems at the time.

What was the cause of the mid-air collision between a Cessna 172 and PSA Flight 182 over San Diego in 1978?

The mid-air collision on September 25, 1978, between a Cessna 172 and a Boeing 727 (Pacific Southwest Airlines Flight 182) over San Diego was attributed to air traffic control error, resulting in 144 fatalities.

What happened to Ken Hubbs, a Chicago Cubs player, in relation to a Cessna 172?

Ken Hubbs, a Gold Glove award-winning second baseman for the Chicago Cubs, was killed on February 13, 1964, when the Cessna 172 he was piloting crashed near Utah Lake.

What tragic event occurred involving David Box, a lead vocalist for The Crickets, and a Cessna 172?

David Box, a lead vocalist for The Crickets, died on October 23, 1964, when the Cessna 172 he was traveling in crashed in Harris County, Texas, while en route to a performance. He was the second Crickets vocalist to die in a plane crash.

What was the outcome of the mid-air collision involving Atlantic Southeast Airlines Flight 2254 and a Civil Air Patrol Cessna 172 in 1990?

On April 9, 1990, an Embraer EMB 120 Brasilia (Atlantic Southeast Airlines Flight 2254) collided head-on with a Civil Air Patrol Cessna 172. The Cessna crashed, killing its two occupants, while the Brasilia managed an emergency landing.

What was the nature of the 2002 Tampa Cessna 172 incident involving Charles J. Bishop?

On January 5, 2002, a high school student named Charles J. Bishop stole a Cessna 172 and intentionally crashed it into the Bank of America Tower in Tampa, Florida. He was the sole fatality, and the damage caused was minimal.

What led to the 2009 incident where a stolen Cessna 172 landed on a highway in Missouri?

A student pilot stole a Confederation College Cessna 172N and flew it into U.S. airspace over Lake Superior. After being intercepted by NORAD F-16s, the aircraft eventually landed on Highway 60 in Ellsinore, Missouri, following a seven-hour flight. The pilot, suffering from depression, was arrested and later sentenced for the theft and illegal entry.

What was the cause of the August 16, 2015, mid-air collision near Brown Field Municipal Airport?

The mid-air collision on August 16, 2015, between a Cessna 172M and a North American Sabreliner, which resulted in five fatalities, was determined to be caused by air traffic control error. This incident prompted the NTSB to recommend enhanced training for controllers.

What is the maximum takeoff weight of the Cessna 172R Skyhawk R?

The maximum takeoff weight for the Cessna 172R Skyhawk R is 2,450 pounds (1,111 kg).

What are the key performance figures for the Cessna 172R?

The Cessna 172R has a cruise speed of 122 knots (140 mph, 226 km/h), a stall speed of 47 knots (54 mph, 87 km/h) with power off and flaps down, a never exceed speed of 163 knots (188 mph, 302 km/h), a range of 696 nautical miles, and a service ceiling of 13,500 feet.

What avionics package was optionally available for the Cessna 172R?

An optional Garmin G1000 primary flight display (PFD) avionics package was available for the Cessna 172R.

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The Ubiquitous Skyhawk

General Introduction

The Cessna 172 Skyhawk is an American four-seat, single-engine, high-wing, fixed-wing aircraft manufactured by the Cessna Aircraft Company. First flown in 1955, it has become the most produced aircraft in history, with over 44,000 units built as of 2015. It was developed from the 1948 Cessna 170, distinguished by its tricycle landing gear configuration.

Production and Legacy

The first production model was delivered in 1956. After a production hiatus from 1986 to 1996, manufacturing resumed and continues to this day. Its enduring popularity is a testament to its robust design, reliability, and versatility in general aviation, flight training, and personal transport.

Market Position

Throughout its history, the Cessna 172 has faced competition from aircraft such as the Beechcraft Musketeer, Grumman American AA-5 series, and Piper PA-28 Cherokee. More contemporary competitors include the Diamond DA40 Diamond Star and Cirrus SR20.

Foundational Design and Evolution

Genesis and Key Innovations

The Cessna 172 originated as a tricycle landing gear variant of the taildragger Cessna 170. The initial 1955 prototype, powered by a Continental O-300-A engine, was certified under the Cessna 170 type certificate. This configuration provided enhanced ground handling and stability.

Aesthetic and Aerodynamic Refinements

The 1960 model year introduced a significant design update with a swept-back vertical tail and rudder, a feature that has remained a hallmark of the aircraft. Further refinements in the 1963 172D model included a lowered rear fuselage and an "Omni-Vision" rear window, improving pilot visibility. Post-resumption production in 1996 incorporated modern interiors and avionics packages.

A Spectrum of Skyhawks: Model Evolution

Early Models (1956-1962)

The initial 172 (1956-1959) featured a Continental O-300-A engine. The 172A (1960) introduced a swept tail and O-300-C engine. The 172B (1961) incorporated shorter landing gear and the "Skyhawk" deluxe option, while the 172C (1962) added fiberglass wingtips and redesigned seats.

Mid-Generation Advancements (1963-1972)

The 172D (1963) brought the "Omni-Vision" rear window and increased gross weight. Subsequent models like the 172E (1964) featured updated instrument panels with circuit breakers, and the 172F (1965) introduced electrically operated flaps, also serving as the basis for the T-41A trainer. The 172I (1968) marked the transition to Lycoming engines (150 hp), and the 172L (1971-1972) adopted tapered tubular steel landing gear legs.

Modernization and Performance (1973-1998)

The 172M (1973-1976) featured a "Camber-Lift" wing for improved low-speed handling and became exclusively known as the "Skyhawk" from 1976. The 172N (1977-1980) introduced a 160 hp Lycoming engine. The 172P (1981-1986) used a more reliable Lycoming O-320-D2J and saw increased gross weight. The 172Q "Cutlass" (1983-1984) offered a 180 hp Lycoming O-360. Post-resumption, the 172R (1996-1998) featured a fuel-injected engine and improved soundproofing.

The Skyhawk SP Era (1998-Present)

The 172S Skyhawk SP, introduced in 1998, is powered by a 180 hp Lycoming IO-360-L2A engine, offering enhanced performance and a higher gross weight. This model is often equipped with the Garmin G1000 avionics suite and leather interiors, representing the current production standard.

Customization and Performance Enhancements

Supplemental Type Certificates (STCs)

The Cessna 172's adaptability is significantly enhanced through a wide array of Supplemental Type Certificates (STCs). These allow for substantial modifications, including upgrades to engine power, ranging from the standard 160-180 hp up to 210 hp, and the installation of constant-speed propellers for improved performance across various flight regimes.

Performance and Efficiency Upgrades

Owners can opt for modifications that improve operational efficiency and performance. These include the ability to use readily available automobile gasoline (mogas) in place of aviation gasoline (Avgas), extended wingtip fuel tanks for increased range, and aerodynamic enhancements like wheel pants to reduce drag. Specialized STOL (Short Takeoff and Landing) kits are also available to improve low-speed handling and short-field capabilities.

A Legacy of Flight

Origins and Development

The Cessna 172's first flight occurred on June 12, 1955, with its introduction to the market in 1956. It evolved from the earlier Cessna 170, incorporating tricycle landing gear for improved ground handling. The aircraft's design philosophy prioritized stability, ease of operation, and cost-effectiveness.

Production Milestones

Production initially ran from 1956 to 1986. Due to rising product liability costs, production was halted. It resumed in 1996 at Cessna's new facility in Independence, Kansas, with updated models reflecting advancements in avionics, materials, and safety features.

Industry Context

The 172 has consistently been a benchmark in the light aircraft segment. Its primary competitors have included aircraft from Piper, Beechcraft, and Grumman. The aircraft's widespread adoption has cemented its status as a cornerstone of general aviation worldwide.

Setting the Bar: Endurance Records

The Timm and Cook Endurance Flight

From December 4, 1958, to February 7, 1959, Robert Timm and John Cook achieved a remarkable feat by setting the world record for refueled flight endurance in a Cessna 172, registration N9172B. This historic flight lasted an astonishing 64 days, 22 hours, 19 minutes, and 5 seconds.

Scope and Purpose

During their record-setting flight, Timm and Cook covered an estimated 150,000 miles, equivalent to over six circumnavigations of the Earth at the equator. The flight was undertaken as a charitable effort to raise funds for the Damon Runyon Cancer Fund, highlighting the aircraft's capability and the crew's dedication.

Historic Preservation

The specific Cessna 172 that accomplished this endurance record, N9172B, is preserved and displayed at McCarran Field (now Harry Reid International Airport) in Las Vegas, Nevada, serving as a monument to aviation endurance and a significant chapter in the 172's history.

Global Reach: Military and Civilian Users

Military Service

The Cessna 172, particularly in its T-41 Mescalero variant, has been widely adopted by military forces globally as a primary trainer and for liaison duties. Its robust design and relatively low operating costs make it suitable for basic flight instruction and various support roles. Notable military operators include the United States Air Force, Army, and Border Patrol, as well as air forces in numerous countries across South America, Europe, and Asia.

Civilian Aviation

In the civilian sector, the Cessna 172 is a dominant force in flight training schools, charter operations, and private ownership. Its forgiving flight characteristics and widespread availability have made it an accessible platform for aspiring pilots and aviation enthusiasts alike. Its role in flight schools is critical for developing foundational piloting skills.

Technical Specifications (172R Model)

Dimensions and Structure

Crew: 1
Capacity: 3 passengers, 120 lb (54 kg) baggage
Length: 27 ft 2 in (8.28 m)
Wingspan: 36 ft 1 in (11.00 m)
Height: 8 ft 11 in (2.72 m)
Wing Area: 174 sq ft (16.2 m²)
Empty Weight: 1,691 lb (767 kg)
Gross Weight: 2,450 lb (1,111 kg)

Performance Metrics

Powerplant: 1 × Lycoming IO-360-L2A, 160 hp (120 kW)
Propellers: 2-bladed metal, fixed pitch McCauley Model 1C235/LFA7570
Cruise Speed: 122 kn (140 mph, 226 km/h)
Stall Speed: 47 kn (54 mph, 87 km/h) (power off, flaps down)
Never Exceed Speed (V_NE): 163 kn (188 mph, 302 km/h) (IAS)
Range: 696 nmi (801 mi, 1,289 km)
Service Ceiling: 13,500 ft (4,100 m)
Rate of Climb: 721 ft/min (3.66 m/s)

Avionics and Fuel

Fuel Capacity: 56 US gal (210 L) (56 US gal usable)
Avionics: Optional Garmin G1000 primary flight display system, providing integrated navigation, communication, and flight instrument data.

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References

Goyer, Robert: "Skyhawk With a Bang", Flying magazine April 2008, pp. 64â68. Hachette Filipacchi US Media

A full list of references for this article are available at the Cessna 172 Wikipedia page

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Important Notice

This page was generated by an Artificial Intelligence and is intended for informational and educational purposes only. The content is based on a snapshot of publicly available data from Wikipedia and may not be entirely accurate, complete, or up-to-date.

This is not professional aviation advice. The information provided on this website is not a substitute for professional aviation consultation, pilot training, or adherence to official aircraft manuals and regulations. Always consult with certified flight instructors, aviation authorities, and official documentation for any operational decisions.

The creators of this page are not responsible for any errors or omissions, or for any actions taken based on the information provided herein.

Cessna 172: The Enduring Skyhawk

💡 Dive in with Flashcard Learning! 💡

The Ubiquitous Skyhawk ℹ️

✈️ General Introduction

📈 Production and Legacy

⚔️ Market Position

Foundational Design and Evolution ⚙️

🏗️ Genesis and Key Innovations

🎨 Aesthetic and Aerodynamic Refinements

A Spectrum of Skyhawks: Model Evolution 📜

🗓️ Early Models (1956-1962)

💡 Mid-Generation Advancements (1963-1972)

🚀 Modernization and Performance (1973-1998)

🌟 The Skyhawk SP Era (1998-Present)

Customization and Performance Enhancements 🛠️

🔧 Supplemental Type Certificates (STCs)

⚙️ Performance and Efficiency Upgrades

A Legacy of Flight ⏳

📜 Origins and Development

⏸️ Production Milestones

🤝 Industry Context

Setting the Bar: Endurance Records 🏆

⏱️ The Timm and Cook Endurance Flight

🌍 Scope and Purpose

🏛️ Historic Preservation

Global Reach: Military and Civilian Users 🌍

🎖️ Military Service

🧑‍✈️ Civilian Aviation

Technical Specifications (172R Model) 📊

📏 Dimensions and Structure

⚙️ Performance Metrics

🖥️ Avionics and Fuel

Teacher's Corner 🧑‍🏫

Edit and Print this course in the Wiki2Web Teacher Studio

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Gamer's Corner 🎮

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References

📜 References

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Disclaimer ⚠️

📜 Important Notice

Dive in with Flashcard Learning!

The Ubiquitous Skyhawk

General Introduction

Production and Legacy

Market Position

Foundational Design and Evolution

Genesis and Key Innovations

Aesthetic and Aerodynamic Refinements

A Spectrum of Skyhawks: Model Evolution

Early Models (1956-1962)

Mid-Generation Advancements (1963-1972)

Modernization and Performance (1973-1998)

The Skyhawk SP Era (1998-Present)

Customization and Performance Enhancements

Supplemental Type Certificates (STCs)

Performance and Efficiency Upgrades

A Legacy of Flight

Origins and Development

Production Milestones

Industry Context

Setting the Bar: Endurance Records

The Timm and Cook Endurance Flight

Scope and Purpose

Historic Preservation

Global Reach: Military and Civilian Users

Military Service

Civilian Aviation

Technical Specifications (172R Model)

Dimensions and Structure

Performance Metrics

Avionics and Fuel

Teacher's Corner

True or False?

Test Your Knowledge!

Gamer's Corner

Discover other topics to study!

References

Feedback & Support

Disclaimer

Important Notice