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Aviation - FAQ

More Cessna 172 History and Facts

by Chris Harris ATU Student and Instructor
(Bates City, MO)

Cessna 172 Picture

Cessna 172 Picture

Starting with the 172D

The 1963 172D model introduced the lower rear fuselage with wraparound Omni-Vision rear window and a one-piece windshield. New rudder and brake pedals were also added. 1146 172Ds were built.

1963 also saw the introduction of the 172D Powermatic. This was equipped with a Continental GO-300E producing 175 horsepower (130 kW) and a cruise speed 11 mph (18 km/h) faster than the standard 172D. In reality this was not a new model but was a Cessna 175 Skylark that had been renamed for its last year of production. The Skylark had gained a reputation for poor engine reliability and the renaming of it as a 172 was a marketing attempt to regain sales through rebranding. The move was not a success and neither the 1963 Powermatic nor the Skylark were produced again after the 1963 model year.

172E

The 172E was the 1964 model. The electrical fuses were replaced with circuit breakers. Gross weight was increased to 2,300 lb (1,000 kg) where it would stay until the 172P. 1401 172Es were built that year as production continued to increase.

172F

The 172F introduced electrically-operated flaps to replace the previous lever-operated system. It was built in France by Reims Cessna as the F172 until 1971. These models formed the basis for the US Air Force's T-41A Mescalero primary trainer.

A total of 1436 172Fs were completed.

172G

The 1966 172G introduced a more pointed spinner and sold for USD$12,450 in its basic 172 version and USD$13,300 in the upgraded Skyhawk version. 1597 were built.

172H

The 1967 model 172H was the last Continental O-300 powered model. It also introduced a shorter-stroke nose gear oleo to reduce drag and improve the appearance of the aircraft in flight. A new cowling was used, introducing shock-mounts that transmitted lower noise-levels to the cockpit and reduced cowl cracking. The electric stall warning horn was replaced by a pneumatic one.

The 1967 model 172H sold for USD$10,950 while the Skyhawk version was USD$12,750. 839 were built that year, representing the first year that production was less than the year before.

172I

The 1968 model marked the beginning of the Lycoming powered 172s. The familiar 172 needed to be re-engined because Cessna had cancelled its contract with Continental for their venerable 0-300 6-cyl engine of 145 horsepower (108 kW).citation needed

The "I" model was introduced with a Lycoming O-320-E2D engine of 150 hp (110 kW), an increase of 5 hp (3.7 kW) over the Continental powerplant. The increased horsepower resulted in an increase in optimal cruise from 130 mph (210 km/h) TAS to 131 mph (211 km/h) TAS. There was no change in the sea level rate of climb at 645 feet (197 m) per minute.

The 172I also introduced the first standard "T" instrument arrangement. The 172I saw an increase in production to record levels with 1206 built.

172J

The Cessna Company planned to drop the previous 172 configuration for the 1968 model year and replace it with a cantilever-wing/stabilator configuration that would be the 172J. However, as time for model introduction neared, those dealers who were aware of the change began applying pressure on the factory to continue the previous configuration. They felt the new model would be less usable as a trainer. Consequently, and at the last minute, the decision was made to continue the 172 in its original configuration. The planned 172J configuration would be introduced as a new model, the 177. The deluxe option would become the 177 Cardinal. The "J" designation was never publicly used.

172K

The next model year was the 1969 "K" model. The 1969 172K had a redesigned vertical fin cap and reshaped rear windows. Optional long range 52 US gallon wing fuel tanks were offered. The rear windows were slightly enlarged by 16 square inches. The 1969 model sold for USD$12,500 for the 172 and USD$13,995 for the Skyhawk, with 1170 made.

The 1970 model was still called the 172K but sported fiberglass, downward-shaped, conical wing tips. Fully articulated seats were offered as well. Production in 1970 was 759 units.

172L

The 172L, sold during 1971 and 1972, replaced the main landing gear, which were originally flat spring steel with tapered, tubular steel gear legs. The new gear had a width that was increased by 12 inches (300 mm).4 The new tubular gear was lighter, but required aerodynamic fairings to maintain the same speed and climb performance as experienced with the flat steel design. The "L" also had a plastic fairing between the dorsal fin and vertical fin to introduce a greater family resemblance to the 182's vertical fin.

The 1971 model sold for USD$13,425 in the 172 version and USD$14,995 in the Skyhawk version. 827 172Ls were sold in 1971 and 984 in 1972.

172M


The 172M of 1973-76 gained a drooped wing leading edge for improved low speed handling. This was marketed as the "camber-lift" wing.

The 1974 172M was also the first to introduce the optional 'II' package which offered higher standard equipment, including a second nav/comm radio, an ADF and transponder. The baggage compartment was increased in size and nose-mounted dual landing lights were available as an option.

The 1975 model 172M sold for USD$16,055 for the 172, USD$17,890 for the Skyhawk and USD$20,335 for the Skyhawk II. Total production of "M" models was 7306 over the four years it was manufactured.

In 1976, Cessna stopped marketing the aircraft as the 172 and began exclusively using the "Skyhawk" designation. This model year also saw a redesigned instrument panel to hold more avionics.

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