26:
196:. The aspect ratio of 9.6:1 was high for aircraft at the time it was designed. The wing has 7 degrees of dihedral for directional stability. A four inch propeller shaft extension allows the engine to be mounted closer to the aircraft's center of gravity. The nose gear steers through the control yoke and not the rudder pedals.
241:
replacement. The Cessna evaluation program ran through 1971 and 1972. While performance was similar to a C-150, the aircraft suffered from high cabin noise levels as well as cooling problems, while not providing any performance advantages over the Cessna 150.
519:
184:
characteristics. The flaps are two-position and mechanically operated by a flap handle on the cabin floor between the seats. The engine starter is foot-actuated and the nose-wheel steering is connected to the control wheel.
175:
The aircraft's design placed the wing behind the cabin and allowed easy entry via automobile-like doors on each side of the cabin. The propeller is well protected and provides safety on the ground in comparison to
213:
Serial numbers 1, 2 and 3 were produced in 1950, while 4 and 5 were built in 1953. The five pre-production prototypes were the only examples built. The retail price of the aircraft was set at $ 4,200 - $ 4,500.
546:
154:
62:
268:
In May 2009 the five production aircraft were still on the US registry listed as
Anderson Greenwood AND-51-A. By August 2018 only two remained registered in the US.
172:. Eventually, only five more examples were built before Anderson Greenwood abandoned the project in favour of producing aircraft components for other manufacturers.
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650:
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165:. The name of the last member of the design team was not included in the product name as it was thought it would not boost sales.
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457:
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542:
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250:
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168:
The prototype first flew in
October 1947, but plans to mass-produce the aircraft were interrupted by the
206:
on 20 September 1950 in the normal category. The certification includes a prohibition on aerobatics and
261:
In 1986 the
Anderson Greenwood Company donated an AG-14, serial number 3, registered as N314AG to the
787:
671:
277:
46:
265:
Aviation
Foundation. By the end of August 2008 it was no longer registered to the foundation.
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177:
567:
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135:
8:
150:
51:
612:. No. Forty–one, Midsummer 1990. Bromley, UK: Tri-Service Press. pp. 49–53.
613:
586:
453:
234:
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368:
4-cylinder air-cooled horizontally-opposed piston engine, 90 hp (67 kW)
246:
222:
110:
153:'s sole aircraft design was actually a collaborative effort of three engineers:
608:
181:
808:
617:
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aircraft. The airfoil employed is a NACA 4418 giving high lift and a stable
344:
127:
25:
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was ideal for minimal wing-body airflow separation that is intrinsic to a
199:
The AG-14 has very good visibility and one reviewer termed it "amazing".
763:"From The Odd Airplane File, Part Three: Anderson Greenwood Model AG-14"
566:
Visschedijk, Johan, Walter van
Tilborg and Karl Smithl (December 2003).
238:
230:
169:
226:
131:
339:
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engine of 100 hp (75 kW), with the goal of a possible
645:
541:
514:
218:
709:. London: Sampson Low, Marston & Co. pp. 197c–198c.
452:, page 13. Werner & Werner Corp, Santa Monica CA, 1977.
631:
225:
for evaluation. Cessna designed and constructed a single
130:. It is an all-metal, shoulder-wing monoplane of pod-and-
210:. One reviewer termed it as "positively spin resistant."
670:
495:
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444:
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440:
438:
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276:The final AG-14 built in 1953 was donated to the
806:
490:
291:Flying 1950 : The Anderson Greenwood AG-14,
122:is a two-seat utility aircraft developed in the
500:Phelps, Mark (May 1988). "Baby Twin Boomber".
433:
793:Photo of production aircraft at Oshkosh 2009
753:Hoadley, E. "The Anderson Greenwood AG-14."
624:
591:: CS1 maint: multiple names: authors list (
788:Photos of prototype and production aircraft
698:
565:
547:"FAA Registry Make / Model Inquiry Results"
245:An AG-14 was also used as the basis of the
217:In 1969 one AG-14 aircraft was acquired by
825:1940s United States civil utility aircraft
559:
280:in Houston, Texas where it is on display.
389:120 mph (190 km/h, 100 kn)
283:
704:
537:
535:
471:
469:
467:
465:
395:110 mph (180 km/h, 96 kn)
722:"The Incomplete Guide to Airfoil Usage"
707:Jane's All the World's Aircraft 1950-51
606:Meyman, Jos. "The Mississippi Marvel".
475:
229:aircraft of similar configuration, the
807:
760:
749:. London: Studio Editions. p. 60.
744:
499:
413:11.7 lb/sq ft (57 kg/m)
271:
256:
188:Wind tunnel testing determined that a
713:
532:
462:
422:0.0645 hp/lb (0.1060 kW/kg)
374:2-bladed fixed-pitch pusher propeller
719:
664:
574:from the original on 30 January 2008
630:
323:34 ft 7 in (10.54 m)
13:
686:from the original on 17 March 2023
605:
508:
317:22 ft 0 in (6.71 m)
14:
846:
781:
329:7 ft 9 in (2.36 m)
263:Experimental Aircraft Association
138:, side-by-side seating and fixed
520:"Aircraft specification no. 4a1"
24:
747:Jane's Encyclopedia of Aviation
705:Bridgman, Leonard, ed. (1950).
647:Federal Aviation Administration
543:Federal Aviation Administration
516:Federal Aviation Administration
335:120 sq ft (11 m)
249:test bed aircraft built by the
134:configuration, equipped with a
820:Single-engined pusher aircraft
761:Wagner, Scott (26 July 2007).
745:Taylor, Michael J. H. (1989).
651:"Make / Model Inquiry Results"
639:
599:
407:700 ft/min (3.6 m/s)
221:Aircraft Company and taken to
145:
1:
476:Hoadley, Ed (December 1950).
426:
401:16,500 ft (5,000 m)
835:Aircraft first flown in 1947
251:Mississippi State University
7:
815:Anderson Greenwood aircraft
798:
358:1,400 lb (635 kg)
10:
851:
676:"Anderson Greenwood AG-14"
478:"Anderson-Greenwood AG-14"
352:850 lb (386 kg)
106:
98:
90:
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77:
57:
45:
37:
32:
23:
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120:Anderson Greenwood AG-14
726:m-selig.ae.illinois.edu
672:Lone Star Flight Museum
450:1978 Aircraft Directory
296:General characteristics
278:Lone Star Flight Museum
830:Shoulder-wing aircraft
284:Specifications (AG-14)
140:tricycle undercarriage
178:tractor configuration
366:Continental C90-12FP
194:pusher configuration
272:Aircraft on display
257:Operational history
33:General information
680:lonestarflight.org
649:(30 August 2018).
233:, equipped with a
163:Lomis Slaughter Jr
151:Anderson Greenwood
71:Lomis Slaughter Jr
52:Anderson Greenwood
767:Aero News Network
720:Lednicer, David.
504:. pp. 51–55.
448:Plane and Pilot:
235:Continental O-200
202:The aircraft was
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91:Introduction date
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399:Service ceiling:
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247:XAZ-1 Marvelette
159:Marvin Greenwood
136:pusher propeller
111:XAZ-1 Marvelette
67:Marvin Greenwood
41:Utility aircraft
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757:December, 1950.
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782:External links
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633:Sport Aviation
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609:Air Enthusiast
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411:Wing loading:
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393:Cruise speed:
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356:Gross weight:
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124:United States
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770:. Retrieved
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688:. Retrieved
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654:. Retrieved
641:
635:. p. 7.
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626:
607:
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576:. Retrieved
568:"Cessna XMC"
561:
550:. Retrieved
545:(May 2009).
523:. Retrieved
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155:Ben Anderson
149:
128:World War II
119:
117:
99:First flight
78:Number built
63:Ben Anderson
47:Manufacturer
772:14 November
380:Performance
372:Propellers:
362:Powerplant:
311:1 passenger
146:Development
809:Categories
578:2008-01-09
552:2009-05-17
525:2009-05-17
483:2009-05-17
427:References
418:Power/mass
333:Wing area:
239:Cessna 150
231:Cessna XMC
170:Korean War
656:30 August
618:0143-5450
345:NACA 4418
321:Wingspan:
309:Capacity:
289:Data from
227:prototype
204:certified
799:See also
731:16 April
690:17 March
684:Archived
674:(2023).
587:cite web
572:Archived
107:Variants
58:Designer
340:Airfoil
327:Height:
315:Length:
86:History
755:Flying
616:
456:
219:Cessna
161:&
69:&
303:Crew:
208:spins
182:stall
19:AG-14
774:2017
733:2019
692:2023
658:2018
614:ISSN
593:link
454:ISBN
364:1 ×
132:boom
118:The
102:1947
94:1950
38:Type
811::
765:.
724:.
682:.
678:.
589:}}
585:{{
570:.
534:^
492:^
464:^
435:^
157:,
142:.
65:,
776:.
735:.
694:.
660:.
620:.
595:)
581:.
555:.
528:.
486:.
420::
342::
305:1
81:5
Text is available under the Creative Commons Attribution-ShareAlike License. Additional terms may apply.
