CallAir A-9: Difference between revisions
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{{Short description|American agricultural aircraft}} |
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{{Infobox aircraft |
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| name=A-9 |
| name=A-9 |
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| image=Aero Cmmdr A-9B Ag Cmmdr Super N7922V Driggs ID 22.06.94R edited-2.jpg |
| image=Aero Cmmdr A-9B Ag Cmmdr Super N7922V Driggs ID 22.06.94R edited-2.jpg |
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| caption=CallAir A-9B glider tug at Driggs Idaho in June 1994 |
| caption=CallAir A-9B glider tug at Driggs Idaho in June 1994 |
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}}{{Infobox Aircraft Type |
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| type= Agricultural aircraft |
| type= Agricultural aircraft |
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| national_origin=United States |
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| manufacturer=[[Intermountain Manufacturing Company]], [[Aero Commander (aircraft manufacturer)|Aero Commander]] |
| manufacturer=[[Intermountain Manufacturing Company]], [[Aero Commander (aircraft manufacturer)|Aero Commander]] |
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| designer= |
| designer= |
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| first_flight=1963<ref name="JAWA65 p246-7"/> |
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| introduction= |
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| retired= |
| retired= |
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| status= |
| status= |
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| produced= |
| produced= |
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| primary_user= |
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| number_built= |
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| developed_from= [[CallAir Model A]] |
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| variants |
| variants= |
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| developed_into= |
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}} |
}} |
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[[File:Callair A-9 N8234H (4818166805).jpg|thumb|N8234H, an original CallAir A-9 c/n 1211, before they were taken over by IMCO, and later by Rockwell Aero Commander]] |
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: ''For the [[USAF]] unmanned Quail drone aircraft, see [[ADM-20 Quail]].'' |
: ''For the [[USAF]] unmanned Quail drone aircraft, see [[ADM-20 Quail]].'' |
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The '''IMCO CallAir A-9''' is |
The '''IMCO CallAir A-9''' is an [[agricultural aircraft]] that first flew in 1962, a development of the company's previous successful crop-dusters. It is typical of aircraft of its type - a single-seat aircraft with a low [[monoplane|wing]] incorporating [[Aerial application|spraying]] gear. |
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==Design and development== |
==Design and development== |
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The [[Call Aircraft Company]] (CAC) had built the [[CallAir Model A]] series of light utility and agricultural aircraft. Following the purchase of CAC in 1962 by [[Intermountain Manufacturing Company]] (IMCO) the latter produced a new agricultural derivative of the Callair, the CallAir A-9. Production of the new aircraft started in 1963.<ref name="JAWA65 p246-7">Taylor 1965, pp. 246–247.</ref> |
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Like the earlier CallAir aircraft, the A-9 is a single-engined [[monoplane]] with a braced low wing. It is of mixed construction, with a fabric-covered steel-tube fuselage structure and a wood-and-fabric wing. The pilot sits behind the chemical hopper, and the cockpit is enclosed by two removable, bottom-hinged doors that form the left and right side windows. The aircraft is powered by a single [[Lycoming O-540]] [[flat-six]] piston engine.<ref name="JAWA65 p246-7"/><ref name="manual">[http://www.soarelsinore.org/docs/a9.pdf "A-9 Owners Manual: Serials 1048, 1111, 1117 & Up"] {{webarchive|url=https://web.archive.org/web/20140807063751/http://www.soarelsinore.org/docs/a9.pdf |date=2014-08-07 }}. Retrieved 23 February 2013.</ref> Later, some A-9s have been adapted for glider towing operations. |
Like the earlier CallAir aircraft, the A-9 is a single-engined [[monoplane]] with a braced low wing. It is of mixed construction, with a fabric-covered steel-tube fuselage structure and a wood-and-fabric wing. The pilot sits behind the chemical hopper, and the cockpit is enclosed by two removable, bottom-hinged doors that form the left and right side windows. The aircraft is powered by a single [[Lycoming O-540]] [[flat-six]] piston engine.<ref name="JAWA65 p246-7"/><ref name="manual">[http://www.soarelsinore.org/docs/a9.pdf "A-9 Owners Manual: Serials 1048, 1111, 1117 & Up"] {{webarchive|url=https://web.archive.org/web/20140807063751/http://www.soarelsinore.org/docs/a9.pdf |date=2014-08-07 }}. Retrieved 23 February 2013.</ref> Later, some A-9s have been adapted for glider towing operations. |
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IMCO was in turn purchased by [[Rockwell International]] in 1966, which built the plane under its [[Aero Commander (aircraft manufacturer)|Aero Commander]] division before shifting production to [[Mexico]] in 1971, under a [[joint venture]] there called [[AAMSA]]. Production |
IMCO was in turn purchased by [[Rockwell International]] in 1966, which built the plane under its [[Aero Commander (aircraft manufacturer)|Aero Commander]] division before shifting production to [[Mexico]] in 1971, under a [[joint venture]] there called [[AAMSA]]. Production ceased in 1984. |
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==Variants== |
==Variants== |
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;A-9 |
;A-9 |
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:Original variant, powered by a 235 [[horsepower|hp]] (175 kW) [[Lycoming O-540]]-B2B5. Built by IMCO and Aero Commander (as the '''Sparrow Commander''') |
:Original variant, powered by a 235 [[horsepower|hp]] (175 kW) [[Lycoming O-540]]-B2B5. Built by CallAir,<ref>{{cite web |title=N8234H CallAir A-9 |url=https://registry.faa.gov/aircraftinquiry/Search/NNumberInquiry? |website=FAA Registry N-Number Inquiry |access-date=5 October 2024}}</ref> IMCO and Aero Commander (as the '''Sparrow Commander''') |
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⚫ | |||
:Version with 290 hp (216 kW) [[Lycoming IO-540]] or [[Lycoming O-540|Lycoming TIO-540]].<ref>{{cite web |title=N7799V Aero Commander CallAir A-9B |url=https://registry.faa.gov/aircraftinquiry/Search/NNumberInquiry? |website=FAA Registry N-Number Inquiry |access-date=5 October 2024}}</ref> Built by Aero Commander (as the '''Quail Commander'''). |
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;B-1 |
;B-1 |
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:Enlarged A-9 with a 400 hp (298 kW) [[Lycoming IO-720]]-A1A engine and 42 ft 8 in (13.00 m) wingspan. First flight January 15, 1966.<ref name="JAWA66 p261-2">Taylor 1966, pp. 261–262.</ref> Built by IMCO and Aero Commander (as the '''Snipe Commander'''). |
:Enlarged A-9 with a 400 hp (298 kW) [[Lycoming IO-720]]-A1A engine and 42 ft 8 in (13.00 m) wingspan. First flight January 15, 1966.<ref name="JAWA66 p261-2">Taylor 1966, pp. 261–262.</ref> Built by IMCO and Aero Commander (as the '''Snipe Commander'''). 36 built.<ref name="Airlifep104"/> |
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;AAMSA A9B |
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: Licensed production by Aeronautica Agricola Mexicana SA (AAMSA) powered by {{convert|300|hp|kW|abbr=on}} Lycoming IO-540-K1A5 engine and {{convert|210|USgal|impgal L|abbr=on}} hopper. 101 built by AAMSA,<ref name="Janes 82 p155">Taylor 1982, p. 155</ref> with a further 17 assembled from Mexican-built components at [[Laredo, Texas]] by Aircraft Parts and Development Corporation.<ref name="Airlifep104"/> |
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⚫ | |||
;AAMSA A9B-M |
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:Version with 290 hp (216 kW) [[Lycoming IO-540]]. Built by Aero Commander (as the '''Quail Commander''') and by AAMSA (as the '''A9B-M Quail''') |
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: Improved version of A9M, with cut down rear fuselage, redesigned cockpit, and increased wing dihedral.<ref name="Janes 82 p155"/> 36 built.<ref name="Airlifep104">Simpson 1995, p. 104</ref> |
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;A9B-M Quail 'Naco' |
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:Two seat military trainer aircraft built in Mexico by AAMSA, based on A9B-M. Single example (EPA-1) preserved at [[Santa Lucia Air Force Base Num 1|Museo Militar de Aviación - MUMA]], Mexico City.<ref>{{cite web |title=EPA-1, AAMSA A-9B Quail |url=https://www.airhistory.net/photo/152133/EPA-1 |website=airhistory.net |access-date=5 October 2024}}</ref> |
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==Specifications (AAMSA A9B-M Quail)== |
==Specifications (AAMSA A9B-M Quail)== |
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|crew=1 |
|crew=1 |
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|capacity={{cvt|210|USgal|impgal |
|capacity={{cvt|210|USgal|impgal L}} or {{cvt|1600|lb}} of chemicals |
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|length ft=24 |
|length ft=24 |
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|length in=0 |
|length in=0 |
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|length note= |
|length note=(tail up) |
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|span ft=34 |
|span ft=34 |
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|span in=9 |
|span in=9 |
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|wing area sqft=181.9 |
|wing area sqft=181.9 |
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|wing area note= |
|wing area note= |
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|aspect ratio=<!-- sailplanes --> |
|aspect ratio=6.63:1<!-- sailplanes --> |
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|airfoil=Modified Clark Y |
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|airfoil=Clark Y<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 lb=1800 |
|empty weight lb=1800 |
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|empty weight note= |
|empty weight note= |
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|max takeoff weight lb=3800 |
|max takeoff weight lb=3800 |
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|max takeoff weight note= |
|max takeoff weight note= |
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|fuel capacity= |
|fuel capacity={{convert|40|USgal|impgal L|abbr=on}} |
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|more general= |
|more general= |
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|minimum control speed kts= |
|minimum control speed kts= |
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|minimum control speed note= |
|minimum control speed note= |
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|range nmi= |
|range nmi=260 |
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|range note= |
|range note= |
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|combat range nmi= |
|combat range nmi= |
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|roll rate=<!-- aerobatic --> |
|roll rate=<!-- aerobatic --> |
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|glide ratio=<!-- sailplanes --> |
|glide ratio=<!-- sailplanes --> |
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|climb rate ftmin= |
|climb rate ftmin=850 |
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|climb rate note= |
|climb rate note= |
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|time to altitude= |
|time to altitude= |
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{{reflist}} |
{{reflist}} |
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;Bibliography |
;Bibliography |
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* {{cite book |last=Simpson |first=R. W. |title=Airlife's General Aviation |year=1995 |edition=Second |location=Shrewsbury |publisher=Airlife Publishing Ltd. |isbn=1-85310-577-5}} |
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* {{cite report |last1=Smith |first1=Michael R. |last2=Patrick |first2=John D. |title=Evaluation of the |
* {{cite report |last1=Smith |first1=Michael R. |last2=Patrick |first2=John D. |title=Evaluation of the CallAir A-9 Agricultural Aircraft: Technical Report |date=November 1966 |publisher=Aerophysics Department, Mississippi State University |url=http://apps.dtic.mil/sti/citations/AD0671079 |archive-url=https://web.archive.org/web/20210128141121/https://apps.dtic.mil/sti/citations/AD0671079 |url-status=live |archive-date=January 28, 2021 |access-date=20 December 2020}} |
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* [[John W. R. Taylor|Taylor, John W. R.]] ''Jane's All The World's Aircraft 1965-66''. London: Sampson Low, Marston & Company, 1965. |
* [[John W. R. Taylor|Taylor, John W. R.]] ''Jane's All The World's Aircraft 1965-66''. London: Sampson Low, Marston & Company, 1965. |
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* [[John W. R. Taylor|Taylor, John W. R.]] ''Jane's All The World's Aircraft 1966-67''. London: Sampson Low, Marston & Company, 1966. |
* [[John W. R. Taylor|Taylor, John W. R.]] ''Jane's All The World's Aircraft 1966-67''. London: Sampson Low, Marston & Company, 1966. |
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[[Category:Single-engined tractor aircraft]] |
[[Category:Single-engined tractor aircraft]] |
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[[Category:Aircraft first flown in 1963]] |
[[Category:Aircraft first flown in 1963]] |
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[[Category:IMCO aircraft]] |
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[[Category:Single-engined piston aircraft]] |
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[[Category:Aircraft with fixed conventional landing gear]] |
Latest revision as of 23:08, 27 November 2024
This article needs additional citations for verification. (December 2009) |
A-9 | |
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General information | |
Type | Agricultural aircraft |
National origin | United States |
Manufacturer | Intermountain Manufacturing Company, Aero Commander |
History | |
First flight | 1963[1] |
Developed from | CallAir Model A |
- For the USAF unmanned Quail drone aircraft, see ADM-20 Quail.
The IMCO CallAir A-9 is an agricultural aircraft that first flew in 1962, a development of the company's previous successful crop-dusters. It is typical of aircraft of its type - a single-seat aircraft with a low wing incorporating spraying gear.
Design and development
[edit]The Call Aircraft Company (CAC) had built the CallAir Model A series of light utility and agricultural aircraft. Following the purchase of CAC in 1962 by Intermountain Manufacturing Company (IMCO) the latter produced a new agricultural derivative of the Callair, the CallAir A-9. Production of the new aircraft started in 1963.[1]
Like the earlier CallAir aircraft, the A-9 is a single-engined monoplane with a braced low wing. It is of mixed construction, with a fabric-covered steel-tube fuselage structure and a wood-and-fabric wing. The pilot sits behind the chemical hopper, and the cockpit is enclosed by two removable, bottom-hinged doors that form the left and right side windows. The aircraft is powered by a single Lycoming O-540 flat-six piston engine.[1][2] Later, some A-9s have been adapted for glider towing operations.
IMCO was in turn purchased by Rockwell International in 1966, which built the plane under its Aero Commander division before shifting production to Mexico in 1971, under a joint venture there called AAMSA. Production ceased in 1984.
Variants
[edit]- A-9
- Original variant, powered by a 235 hp (175 kW) Lycoming O-540-B2B5. Built by CallAir,[3] IMCO and Aero Commander (as the Sparrow Commander)
- A-9B (Super)
- Version with 290 hp (216 kW) Lycoming IO-540 or Lycoming TIO-540.[4] Built by Aero Commander (as the Quail Commander).
- B-1
- Enlarged A-9 with a 400 hp (298 kW) Lycoming IO-720-A1A engine and 42 ft 8 in (13.00 m) wingspan. First flight January 15, 1966.[5] Built by IMCO and Aero Commander (as the Snipe Commander). 36 built.[6]
- AAMSA A9B
- Licensed production by Aeronautica Agricola Mexicana SA (AAMSA) powered by 300 hp (220 kW) Lycoming IO-540-K1A5 engine and 210 US gal (170 imp gal; 790 L) hopper. 101 built by AAMSA,[7] with a further 17 assembled from Mexican-built components at Laredo, Texas by Aircraft Parts and Development Corporation.[6]
- AAMSA A9B-M
- Improved version of A9M, with cut down rear fuselage, redesigned cockpit, and increased wing dihedral.[7] 36 built.[6]
- A9B-M Quail 'Naco'
- Two seat military trainer aircraft built in Mexico by AAMSA, based on A9B-M. Single example (EPA-1) preserved at Museo Militar de Aviación - MUMA, Mexico City.[8]
Specifications (AAMSA A9B-M Quail)
[edit]Data from Jane's All The World's Aircraft 1982-83 [9]
General characteristics
- Crew: 1
- Capacity: 210 US gal (170 imp gal; 790 L) or 1,600 lb (730 kg) of chemicals
- Length: 24 ft 0 in (7.32 m) (tail up)
- Wingspan: 34 ft 9 in (10.59 m)
- Height: 7 ft 8 in (2.34 m)
- Wing area: 181.9 sq ft (16.90 m2)
- Aspect ratio: 6.63:1
- Airfoil: Modified Clark Y
- Empty weight: 1,800 lb (816 kg)
- Max takeoff weight: 3,800 lb (1,724 kg)
- Fuel capacity: 40 US gal (33 imp gal; 150 L)
- Powerplant: 1 × Lycoming IO-540-K1A-5 6-cylinder air-cooled horizontally opposed piston engine, 300 hp (220 kW)
Performance
- Maximum speed: 104 kn (120 mph, 193 km/h)
- Cruise speed: 87 kn (100 mph, 161 km/h)
- Range: 260 nmi (300 mi, 480 km)
- Service ceiling: 16,000 ft (4,900 m)
- Rate of climb: 850 ft/min (4.3 m/s)
See also
[edit]Aircraft of comparable role, configuration, and era
References
[edit]- Notes
- ^ a b c Taylor 1965, pp. 246–247.
- ^ "A-9 Owners Manual: Serials 1048, 1111, 1117 & Up" Archived 2014-08-07 at the Wayback Machine. Retrieved 23 February 2013.
- ^ "N8234H CallAir A-9". FAA Registry N-Number Inquiry. Retrieved 5 October 2024.
- ^ "N7799V Aero Commander CallAir A-9B". FAA Registry N-Number Inquiry. Retrieved 5 October 2024.
- ^ Taylor 1966, pp. 261–262.
- ^ a b c Simpson 1995, p. 104
- ^ a b Taylor 1982, p. 155
- ^ "EPA-1, AAMSA A-9B Quail". airhistory.net. Retrieved 5 October 2024.
- ^ Taylor 1982, pp. 155–156.
- Bibliography
- Simpson, R. W. (1995). Airlife's General Aviation (Second ed.). Shrewsbury: Airlife Publishing Ltd. ISBN 1-85310-577-5.
- Smith, Michael R.; Patrick, John D. (November 1966). Evaluation of the CallAir A-9 Agricultural Aircraft: Technical Report (Report). Aerophysics Department, Mississippi State University. Archived from the original on January 28, 2021. Retrieved 20 December 2020.
- Taylor, John W. R. Jane's All The World's Aircraft 1965-66. London: Sampson Low, Marston & Company, 1965.
- Taylor, John W. R. Jane's All The World's Aircraft 1966-67. London: Sampson Low, Marston & Company, 1966.
- Taylor, John W. R. Jane's All The World's Aircraft 1982-83. London:Jane's Yearbooks, 1982. ISBN 0-7106-0748-2.
External links
[edit]Media related to CallAir A-9 at Wikimedia Commons