Jump to content
Main menu
Main menu
move to sidebar
hide
Navigation
Main page
Recent changes
Random page
Help about MediaWiki
Special pages
Niidae Wiki
Search
Search
Appearance
Create account
Log in
Personal tools
Create account
Log in
Pages for logged out editors
learn more
Contributions
Talk
Editing
Cessna 172
(section)
Page
Discussion
English
Read
Edit
View history
Tools
Tools
move to sidebar
hide
Actions
Read
Edit
View history
General
What links here
Related changes
Page information
Appearance
move to sidebar
hide
Warning:
You are not logged in. Your IP address will be publicly visible if you make any edits. If you
log in
or
create an account
, your edits will be attributed to your username, along with other benefits.
Anti-spam check. Do
not
fill this in!
==Design and development== [[File:Cessna172Skyhawk1957model01.jpg|thumb|Early Cessna 172s, like this 1957 model, had a "[[fastback]]" rear cabin with no rear window and featured a "square" fin design.]]The Cessna 172 started as a tricycle landing gear variant of the [[taildragger]] [[Cessna 170]], with a basic level of standard equipment. In January 1955, Cessna flew an improved variant of the Cessna 170, a [[Continental O-300|Continental O-300-A]]-powered Cessna 170C with larger elevators and a more angular tailfin.<ref name="simpson">{{cite journal |last=Simpson |first= Rod |date=June 2009 |title=Cessna 172 β Simply, the World's Most Successful Light Aircraft? |journal=Air-Britain Aviation World |publisher=[[Air-Britain]] |volume=61 |issue=120 |pages=158β163 |issn=1742-996X}}</ref> Although the variant was tested and certified, Cessna decided to modify it with a tricycle landing gear, and the modified Cessna 170C flew again on June 12, 1955.<ref name="simpson" /> To reduce the time and cost of certification, the type was added to the Cessna 170 [[type certificate]] as the Model 172.<ref name="simpson" /> Later, the 172 was given its own type certificate.<ref name="3A12">{{cite web |last=[[Federal Aviation Administration]] |date=February 2006 |title=Type Certificate Data Sheet No. 3A12 |url=https://drs.faa.gov/browse/excelExternalWindow/814B2FB4DC1615008625871E005ED037.0001 |access-date=2024-06-09}}</ref><ref name="A799">{{cite web |last=[[Federal Aviation Administration]] |date=November 2004 |title=Type Certificate Data Sheet No. A-799 |url=http://www.airweb.faa.gov/Regulatory_and_Guidance_Library/rgMakeModel.nsf/0/51dcd703defaa00486257243006811e2/$FILE/A-799.pdf |url-status=dead |archive-url=https://web.archive.org/web/20110608055100/http://www.airweb.faa.gov/Regulatory_and_Guidance_Library/rgMakeModel.nsf/0/51dcd703defaa00486257243006811e2/$FILE/A-799.pdf |archive-date=2011-06-08 |access-date=2010-02-21}}</ref> The 172 became an overnight sales success, and over 1,400 were built in 1956, its first full year of production.<ref>Clark, Anders (1 January 2015). "[https://disciplesofflight.com/cessna-172-skyhawk/ Cessna 172 Skyhawk] {{Webarchive|url=https://web.archive.org/web/20150814142814/https://disciplesofflight.com/cessna-172-skyhawk/ |date=2015-08-14 }}". Disciples of Flight. Retrieved 12 August 2015</ref> Early 172s were similar in appearance to the 170s, with the same straight aft fuselage and tall landing gear legs, although the 172 had a straight tailfin while the 170 had a rounded fin and rudder. In 1960, the 172A incorporated revised landing gear and the swept-back tailfin, which is still in use today. The final aesthetic development, found in the 1963 172D and all later 172 models, was a lowered rear deck allowing an aft window. Cessna advertised this added rear visibility as "[[Cessna#Marketing initiatives|Omni-Vision]]".<ref name="Clarke" /> Production halted in the mid-1980s, but resumed in 1996 with the 160 hp (120 kW) Cessna 172R Skyhawk. Cessna supplemented this in 1998 with the 180 hp (135 kW) Cessna 172S Skyhawk SP.{{Citation needed|date=June 2012}} ===Modifications=== The Cessna 172 may be modified via a wide array of [[supplemental type certificate]]s (STCs), including increased engine power and higher gross weights. Available STC engine modifications increase power from {{convert|180|to|210|hp|kW|0|abbr=on}}, add [[constant-speed propeller]]s, or allow the use of [[Avgas#Automotive gasoline|automobile gasoline]]. Other modifications include additional fuel tank capacity in the [[wing tip]]s, added baggage compartment tanks, added [[wheel pants]] to reduce drag, or enhanced landing and takeoff performance and safety with a [[STOL]] kit.<ref>{{cite web |url=http://www.aopa.org/pilot/btn172/btn9407.html |title=Airframe Additions |access-date=2010-04-28 |url-status=dead |archive-url=https://web.archive.org/web/20080526153149/http://www.aopa.org/pilot/btn172/btn9407.html |archive-date=2008-05-26 }} ''AOPA Pilot'', May/July 1994</ref> The 172 has also been equipped with the {{convert|180|hp|kW|0|abbr=on}} [[fuel injected]] [[Superior Air Parts Vantage]] engine.<ref>{{cite web|title=Superior Skyhawk SV|url=http://www.superiorairparts.com/vantage-engine/skyhawk-sv/|author=[[Superior Air Parts]]|work=superiorairparts.com|access-date=17 April 2018|archive-url=https://web.archive.org/web/20180518085207/http://www.superiorairparts.com/vantage-engine/skyhawk-sv/|archive-date=18 May 2018|url-status=live}}</ref>
Summary:
Please note that all contributions to Niidae Wiki may be edited, altered, or removed by other contributors. If you do not want your writing to be edited mercilessly, then do not submit it here.
You are also promising us that you wrote this yourself, or copied it from a public domain or similar free resource (see
Encyclopedia:Copyrights
for details).
Do not submit copyrighted work without permission!
Cancel
Editing help
(opens in new window)
Search
Search
Editing
Cessna 172
(section)
Add topic