Meyers 200: Difference between revisions
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{{short description|Single-engined retractable-gear light aircraft}} |
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{|{{Infobox Aircraft Begin |
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{{Infobox aircraft |
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| name=Meyers 200 |
| name=Meyers 200 |
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| image= |
| image=Meyers 200 N2987T.jpg |
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| caption=A 1966-built Aero Commander 200D |
| caption=A 1966-built Aero Commander 200D |
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}}{{Infobox Aircraft Type |
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| type= |
| type= |
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| national_origin=United States of America |
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| manufacturer=[[Meyers Aircraft Company]] |
| manufacturer=[[Meyers Aircraft Company]] |
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| designer= |
| designer= |
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| first_flight= |
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| introduction=1955 |
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| retired= |
| retired= |
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| status= |
| status= |
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| primary_user= |
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| more_users= <!--Limited to three in total; separate using <br /> --> |
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| produced= <!--years in production--> |
| produced= <!--years in production--> |
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| number_built= |
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| program cost= <!--Total program cost--> |
| program cost= <!--Total program cost--> |
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| unit cost=$12,500 less radios in 1960 <!--Incremental or flyaway cost for military or retail price for commercial aircraft--> |
| unit cost=$12,500 less radios in 1960 <!--Incremental or flyaway cost for military or retail price for commercial aircraft--> |
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| developed_from= |
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| variants |
| variants= |
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The ''' |
The '''Meyers 200''' is a single-engined light aircraft produced in the United States in the 1950s and 1960s. |
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==Design== |
==Design== |
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It was the brainchild of [[Al Meyers]] and was a development of his [[Meyers 145]] design. The holder of a number of speed records in its class, the Meyers 200 is widely admired for its clean lines, and is also known for its exceptionally sturdy airframe. This strength is derived from a tubular [[41xx steel|4130 chrome-moly steel]] truss structure with [[aluminum]] skin that protects occupants.<ref>{{cite journal| |
It was the brainchild of [[Al Meyers]] and was a development of his [[Meyers MAC-145]] design. The holder of a number of speed records in its class, the Meyers 200 is widely admired for its clean lines, and is also known for its exceptionally sturdy airframe. This strength is derived from a tubular [[41xx steel|4130 chrome-moly steel]] truss structure with [[aluminum]] skin that protects occupants.<ref>{{cite journal|journal=Sport Aviation|date=June 1960}}</ref> |
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===Acquisition by Aero Commander=== |
===Acquisition by Aero Commander=== |
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In [[1966 in aviation|1966]], the [[ |
In [[1966 in aviation|1966]], the [[Aero Commander]] division of [[North American Aviation#Merger and acquisition|North American Rockwell]] purchased the rights to the Meyers 145 and 200, as part of a strategy to capture a share of the light aircraft market in the United States. During this time it was in the James Bond film ''[[You Only Live Twice (film)|You Only Live Twice]]''. Known briefly as the '''Aero Commander 200''', it soon emerged that the firm could not produce the design economically. Meyers' firm had been virtually hand-building each aircraft and no [[Jig (tool)|jigs]] or tooling for the kind of [[mass production]] envisaged by Aero Commander even existed at the time the rights were bought. Having spent US$4 million to produce just US$3 million worth of product, Aero Commander ceased production in [[1968 in aviation|1968]] and sold the rights to the [[Interceptor Corporation]], which developed a [[turboprop]]-powered version as the [[Interceptor 400]]. Ownership of the rights eventually passed to Prop-Jets, Inc., later known as Interceptor Aircraft Corporation. In 2014 the Global Parts Group, via a separately formed affiliate company called Interceptor Aviation Inc, purchased the rights along with all associated assets and intellectual property related to the Meyers 200 and Interceptor 400 model aircraft. |
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==Operational service== |
==Operational service== |
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The Meyers 200D has never had an in-flight structural failure and has never had |
The Meyers 200D has never had an in-flight structural failure and has never had a [[Federal Aviation Administration]] mandated [[Airworthiness directive|Airworthiness Directive]] (AD) issued against the airframe. The [[41xx steel|4130 chrome-moly steel]] tubular [[roll cage]] and understructure act like a race car protective cage during a crash. Several Meyers aircraft have been [[Emergency landing|forced down]] in the trees and off airport runways with documented instances of the occupants walking away with only minor injuries or a broken bone. |
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==Variants== |
==Variants== |
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===Meyers=== |
===Meyers=== |
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[[ |
[[File:Meyers200A.jpg|thumb|right|Meyers 200A]] |
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* '''200''' |
* '''200''' — single prototype powered by [[Continental O-470]] |
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* '''200A''' |
* '''200A''' — production version powered by [[Continental O-470|Continental IO-470]] (11 built) |
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* '''200B''' |
* '''200B''' — (17 built) |
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* '''200C''' |
* '''200C''' — raised roof-line and larger windshield (9 built) |
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* '''200D''' |
* '''200D''' — engine replaced with [[Continental O-520|Continental IO-520-A]] and flush riveted wings (8 built) |
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===[[Aero Commander]]=== |
===[[Aero Commander]]=== |
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[[ |
[[File:Meyers-200.jpg|right|thumb|An Aero Commander 200D Taxiing]] |
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* '''200''' |
* '''200''' — Aero Commander version of the 200D (77 built) |
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* '''200''' |
* '''200''' — Aero Commander version of the 200E (1 prototype built) |
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* '''T200E''' |
* '''T200E''' — experimental twin-engine conversion - never built |
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===Interceptor=== |
===Interceptor=== |
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* '''[[Interceptor 400|400]]''' |
* '''[[Interceptor 400|400]]''' — Turboprop based on the 200 <ref>{{cite journal|journal=Air Progress|date=December 1971|page=19}}</ref> |
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==Specifications (Meyers 200D)== |
==Specifications (Meyers 200D)== |
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{{Aircraft specs |
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===General characteristics=== |
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|ref=Jane's All the World's Aircraft 1967–68<ref name="jawa67p186">{{Harvnb|Taylor|1967|p=186}}</ref> |
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* '''Crew:''' one pilot |
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|prime units?=imp |
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* '''Capacity:''' 3 passengers |
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<!-- |
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* '''Length:''' 24 ft 4 in (7.42 m) |
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General characteristics |
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* '''Wingspan:''' 30 ft 6 in (9.30 m) |
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--> |
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* '''Height:''' 7 ft 4 in (2.24 m) |
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|genhide= |
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* '''Wing area:''' 162 ft² (15.0 m²) |
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* '''Empty:''' 1,940 lb (882 kg) |
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* '''Loaded:''' 3,000 lb (1,364 kg) |
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* '''Maximum takeoff:''' 3,000 lb (1,364 kg) |
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* '''Powerplant:''' 1x [[Continental IO-520]]A, 285 hp (209 kW) |
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|crew=1 |
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===Performance=== |
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|capacity=3 passengers |
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* '''Maximum speed:''' 239 mph (385 km/h) |
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|length m= |
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* '''Range:''' 1,200 miles (1,931 km) |
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|length ft=24 |
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* '''Service ceiling:''' 18,500 ft (5,640 m) |
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|length in=4 |
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* '''Rate of climb:''' 1,350 ft/min (412 m/min) |
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|length note= |
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* '''Wing loading:''' 18.5 lb/ft² ( kg/m²) |
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|span m= |
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* '''Power/Mass:''' 10.5 hp/lb ( kW/kg) |
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|span ft=30 |
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|span in=6 |
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|span note= |
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|height m= |
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|height ft=7 |
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|height in=4 |
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|height note= |
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|wing area sqm= |
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|wing area sqft=161.5 |
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|wing area note= |
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|aspect ratio=<!-- sailplanes --> |
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|airfoil='''root:''' [[NACA airfoil|NACA 23015]]; '''tip:''' [[NACA airfoil|NACA 4412]]<ref name="Selig">{{cite web |last1=Lednicer |first1=David |title=The Incomplete Guide to Airfoil Usage |url=https://m-selig.ae.illinois.edu/ads/aircraft.html |website=m-selig.ae.illinois.edu |accessdate=16 April 2019}}</ref> |
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|empty weight kg= |
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|empty weight lb=1940 |
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|empty weight note= |
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|gross weight kg= |
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|gross weight lb= |
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|gross weight note= |
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|max takeoff weight kg= |
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|max takeoff weight lb=3000 |
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|max takeoff weight note= |
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|fuel capacity={{convert|40|USgal|impgal L|abbr=on}} normal |
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|more general= |
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<!-- |
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Powerplant |
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--> |
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|eng1 number=1 |
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|eng1 name=[[Continental O-520|Continental IO-520-A]] |
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|eng1 type=air-cooled six-cylinder horizontally-opposed |
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|eng1 kw=<!-- prop engines --> |
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|eng1 hp=285<!-- prop engines --> |
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|eng1 note= |
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|power original= |
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|prop blade number=<!-- propeller aircraft --> |
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|prop name= |
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|prop dia m=<!-- propeller aircraft --> |
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|prop dia ft=<!-- propeller aircraft --> |
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|prop dia in=<!-- propeller aircraft --> |
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|prop dia note= |
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<!-- |
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Performance |
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--> |
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|perfhide= |
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|max speed kmh= |
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|max speed mph=215 |
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|max speed kts= |
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|max speed note= |
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|max speed mach=<!-- supersonic aircraft --> |
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|cruise speed kmh=333 |
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|cruise speed mph=210 |
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|cruise speed kts= |
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|cruise speed note=(max cruise) |
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|stall speed kmh= |
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|stall speed mph=54 |
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|stall speed kts= |
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|stall speed note=(wheels and flaps down) |
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|never exceed speed kmh= |
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|never exceed speed mph= |
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|never exceed speed kts= |
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|never exceed speed note= |
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|range km= |
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|range miles=900 |
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|range nmi= |
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|range note=(normal fuel, 45 minutes reserve) |
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|endurance=<!-- if range unknown --> |
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|ceiling m= |
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|ceiling ft=18500 |
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|ceiling note= |
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|climb rate ms= |
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|climb rate ftmin=1400 |
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|climb rate note= |
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|time to altitude= |
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|thrust/weight= |
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|more performance= |
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*'''Take-off run to 50 ft (15 m):''' {{convert|1200|ft|m|abbr=on}} |
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*'''Landing run from 50 ft (15 m):''' {{convert|1150|ft|m|abbr=on}} |
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|avionics= |
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}} |
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==See also== |
==See also== |
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'''Related development:''' |
'''Related development:''' |
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*[[Meyers 145]] - |
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*[[Interceptor 400]] |
*[[Interceptor 400]] |
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*[[Meyers MAC-145]] |
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'''Comparable aircraft:''' |
'''Comparable aircraft:''' |
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*[[Beechcraft Bonanza]] |
*[[Beechcraft Bonanza]] |
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*[[ |
*[[Bellanca Viking]] |
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*[[Johnson Rocket 185]] |
*[[Johnson Rocket 185]] |
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*[[Ryan Navion]] |
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==References== |
==References== |
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{{Reflist}} |
{{Reflist}} |
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*{{cite book|last=Taylor|first=John W. R.|title=Jane's All The World's Aircraft 1967–68|year=1967|publisher=Sampson Low, Marston & Company|location=London|authorlink=John W. R. Taylor}} |
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==External links== |
==External links== |
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{{ |
{{commons category|Meyers 200}} |
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* [http://www.meyersmovement.com/ Meyers Movement Home Page] |
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* [http://www.meyersaircraft.com/ Meyers Aircraft Home Page] |
* [http://www.meyersaircraft.com/ Meyers Aircraft Home Page] |
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* [http://www.deans-world.com/Meyers200/Welcome.html Meyers owner enthusiast site] |
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* [http://www.pilotfriend.com/aircraft%20performance/Micco/meyers.htm Meyers/Micco aircraft history, performance and specifications] - Pilotfriend |
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* [http://www.airbum.com/pireps/PirepMeyers200D.html Aviation Journalist Bud Davisson's review of the Meyers 200D] |
* [http://www.airbum.com/pireps/PirepMeyers200D.html Aviation Journalist Bud Davisson's review of the Meyers 200D] |
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* [https://www.avweb.com/used-aircraft-guide-digest/buying-a-used-aircraft-meyers-200/ AVweb used aircraft review] |
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* [http://www.meyersaircraftowners.org/ Meyers Aircraft Owners Home Page] |
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* [http://www.meyersfoundation.org/ Meyers Foundation] |
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{{Aero Commander aircraft}} |
{{Aero Commander aircraft}} |
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{{aviation lists}} |
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[[Category:United States civil utility aircraft |
[[Category:1950s United States civil utility aircraft]] |
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[[Category:Single-engine aircraft]] |
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[[Category:Meyers aircraft|200]] |
[[Category:Meyers aircraft|200]] |
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[[Category:Aero Commander aircraft|200]] |
[[Category:Aero Commander aircraft|200]] |
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[[Category:Single-engined tractor aircraft]] |
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[[Category:Low-wing aircraft]] |
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[[Category:Aircraft first flown in 1955]] |
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[[Category:Aircraft with retractable tricycle landing gear]] |
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[[Category:Single-engined piston aircraft]] |
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Latest revision as of 17:19, 2 December 2024
| Meyers 200 | |
|---|---|
 A 1966-built Aero Commander 200D | |
| General information | |
| National origin | United States of America |
| Manufacturer | Meyers Aircraft Company |
| History | |
| Introduction date | 1955 |
The Meyers 200 is a single-engined light aircraft produced in the United States in the 1950s and 1960s.
Design
[edit]It was the brainchild of Al Meyers and was a development of his Meyers MAC-145 design. The holder of a number of speed records in its class, the Meyers 200 is widely admired for its clean lines, and is also known for its exceptionally sturdy airframe. This strength is derived from a tubular 4130 chrome-moly steel truss structure with aluminum skin that protects occupants.[1]
Acquisition by Aero Commander
[edit]In 1966, the Aero Commander division of North American Rockwell purchased the rights to the Meyers 145 and 200, as part of a strategy to capture a share of the light aircraft market in the United States. During this time it was in the James Bond film You Only Live Twice. Known briefly as the Aero Commander 200, it soon emerged that the firm could not produce the design economically. Meyers' firm had been virtually hand-building each aircraft and no jigs or tooling for the kind of mass production envisaged by Aero Commander even existed at the time the rights were bought. Having spent US$4 million to produce just US$3 million worth of product, Aero Commander ceased production in 1968 and sold the rights to the Interceptor Corporation, which developed a turboprop-powered version as the Interceptor 400. Ownership of the rights eventually passed to Prop-Jets, Inc., later known as Interceptor Aircraft Corporation. In 2014 the Global Parts Group, via a separately formed affiliate company called Interceptor Aviation Inc, purchased the rights along with all associated assets and intellectual property related to the Meyers 200 and Interceptor 400 model aircraft.
Operational service
[edit]The Meyers 200D has never had an in-flight structural failure and has never had a Federal Aviation Administration mandated Airworthiness Directive (AD) issued against the airframe. The 4130 chrome-moly steel tubular roll cage and understructure act like a race car protective cage during a crash. Several Meyers aircraft have been forced down in the trees and off airport runways with documented instances of the occupants walking away with only minor injuries or a broken bone.
Variants
[edit]Meyers
[edit]
- 200 — single prototype powered by Continental O-470
- 200A — production version powered by Continental IO-470 (11 built)
- 200B — (17 built)
- 200C — raised roof-line and larger windshield (9 built)
- 200D — engine replaced with Continental IO-520-A and flush riveted wings (8 built)
- 200 — Aero Commander version of the 200D (77 built)
- 200 — Aero Commander version of the 200E (1 prototype built)
- T200E — experimental twin-engine conversion - never built
Interceptor
[edit]Specifications (Meyers 200D)
[edit]Data from Jane's All the World's Aircraft 1967–68[3]
General characteristics
- Crew: 1
- Capacity: 3 passengers
- Length: 24 ft 4 in (7.42 m)
- Wingspan: 30 ft 6 in (9.30 m)
- Height: 7 ft 4 in (2.24 m)
- Wing area: 161.5 sq ft (15.00 m2)
- Airfoil: root: NACA 23015; tip: NACA 4412[4]
- Empty weight: 1,940 lb (880 kg)
- Max takeoff weight: 3,000 lb (1,361 kg)
- Fuel capacity: 40 US gal (33 imp gal; 150 L) normal
- Powerplant: 1 × Continental IO-520-A air-cooled six-cylinder horizontally-opposed, 285 hp (213 kW)
Performance
- Maximum speed: 215 mph (346 km/h, 187 kn)
- Cruise speed: 210 mph (333 km/h, 180 kn) (max cruise)
- Stall speed: 54 mph (87 km/h, 47 kn) (wheels and flaps down)
- Range: 900 mi (1,400 km, 780 nmi) (normal fuel, 45 minutes reserve)
- Service ceiling: 18,500 ft (5,600 m)
- Rate of climb: 1,400 ft/min (7.1 m/s)
- Take-off run to 50 ft (15 m): 1,200 ft (370 m)
- Landing run from 50 ft (15 m): 1,150 ft (350 m)
See also
[edit]Related development:
Comparable aircraft:
References
[edit]- ^ Sport Aviation. June 1960.
{{cite journal}}: Missing or empty|title=(help) - ^ Air Progress: 19. December 1971.
{{cite journal}}: Missing or empty|title=(help) - ^ Taylor 1967, p. 186
- ^ Lednicer, David. "The Incomplete Guide to Airfoil Usage". m-selig.ae.illinois.edu. Retrieved 16 April 2019.
- Taylor, John W. R. (1967). Jane's All The World's Aircraft 1967–68. London: Sampson Low, Marston & Company.
External links
[edit]
Wikimedia Commons has media related to Meyers 200.