About: Aerotec Uirapuru

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About: Aerotec Uirapuru Sponge Permalink

An Entity of Type : dbkwik:resource/AGhloO_nVTaFp7GvOmHv5Q==, within Data Space : 134.155.108.49:8890 associated with source dataset(s)

The Aerotec A-122 Uirapuru was a Brazilian military trainer aircraft. It was a low-wing monoplane with tricycle undercarriage that accommodated the pilot and instructor side-by-side. It first flew on 2 June 1965. In October 1967, the Brazilian Air Force ordered 30 aircraft to replace the obsolete Fokker S.11s and S.12s (T-21s and T-22s) that were operating in the Air Force Academy. Later, they ordered another 40, and then 30 more. These were designated T-23. In 1980 interest by the airforce in an improved version led to the development of the Uirapuru II.

Attributes	Values
rdf:type	Aircraft Type
rdfs:label	Aerotec Uirapuru
rdfs:comment	The Aerotec A-122 Uirapuru was a Brazilian military trainer aircraft. It was a low-wing monoplane with tricycle undercarriage that accommodated the pilot and instructor side-by-side. It first flew on 2 June 1965. In October 1967, the Brazilian Air Force ordered 30 aircraft to replace the obsolete Fokker S.11s and S.12s (T-21s and T-22s) that were operating in the Air Force Academy. Later, they ordered another 40, and then 30 more. These were designated T-23. In 1980 interest by the airforce in an improved version led to the development of the Uirapuru II.
sameAs	dbr:Aerotec_Uirapuru
dcterms:subject	dbkwik:resource/FUwnXua-41_8iqKSDDJhpQ== dbkwik:resource/iMlwGhmMJJV362ccAvHqRg== dbkwik:resource/ha5mecJrF9UuI0hTOgOPWQ== dbkwik:resource/igX5bNaGvJo3jT9qxCHO1A==
dbkwik:military/pr...iPageUsesTemplate	dbkwik:resource/AaGpNMKXeCEx6k1ovZIRVg== dbkwik:resource/ODD2urn6xOTu5tfNx3dKHA== dbkwik:resource/pTEKXoXwy_QJD-cbbKl3EQ== dbkwik:resource/8c65HClsHBgkxfJdWXaRHw== dbkwik:resource/cbsrEQx1xy51eXd2rIQtLg== dbkwik:resource/uj4mWs4uzKe7a19-7FYfVg== dbkwik:resource/78N_Nvke6VIxDXvbfqkysA== dbkwik:resource/wOXzR82AaBJBSaPLR4xPGQ== dbkwik:resource/rnvnddlA753uo3kHZyN8wQ== dbkwik:resource/DOWwjsa-FAruKoB0h0tKBw==
max takeoff weight alt	1825.0
airfoil	NACA 43013
climb rate main	4.0
number of props	1(xsd:integer)
length alt	660.4000000000001
span main	8.50 m
Produced	1968(xsd:integer)
cruise speed main	185.0
more performance	14400.0
cruise speed alt	100(xsd:integer)
height alt	660.4000000000001
Type	Primary Trainer
type of prop	4(xsd:integer)
range alt	429(xsd:integer)
length main	6.60 m
power alt	160.0
area main	13.5
power main	119.0
stall speed alt	48(xsd:integer)
height main	2.70 m
span alt	27(xsd:integer)
range main	800.0
Manufacturer	Aerotec
max speed main	225.0
engine (prop)	Lycoming O-320-B2B
climb rate alt	787.0
ceiling main	4,500 m
National Origin	Brazil
empty weight main	540.0
stall speed main	88.0
area alt	145.3
First Flight	1965-06-02(xsd:date)
max speed alt	122(xsd:integer)
jet or prop?	prop
never exceed speed alt	165(xsd:integer)
empty weight alt	1191.0
plane or copter?	plane
ceiling alt	17000.0
max takeoff weight main	840.0
never exceed speed main	307.0
Crew	Two
Number Built	155(xsd:integer)
ref	Jane's All The World's Aircraft 1971-72
abstract	The Aerotec A-122 Uirapuru was a Brazilian military trainer aircraft. It was a low-wing monoplane with tricycle undercarriage that accommodated the pilot and instructor side-by-side. It first flew on 2 June 1965. In October 1967, the Brazilian Air Force ordered 30 aircraft to replace the obsolete Fokker S.11s and S.12s (T-21s and T-22s) that were operating in the Air Force Academy. Later, they ordered another 40, and then 30 more. These were designated T-23. The Bolivian Air Force ordered 36 examples in 1974, which flew until 1997, and in 1975 the Paraguayan Air Force bought 8 aircraft to replace the Fokker T-21 (S.11). In 1986, six more were donated by the FAB. Most of them were withdrawn from service in 1992, replaced by the Enaer T-35 Pillán. As of 2009, only one T-23 is in flying conditions. Thirty others were sold in the civilian market. A total of 155 were built including prototypes by the time production finished in 1977. The T-23 suffered fatal accidents during spin training. The problem was resolved after a crash in which an instructor described his stricken aircraft's responses to his control inputs all the way to the end. Uirapurus then received a fin under the rear fuselage to correct the issue. In 1980 interest by the airforce in an improved version led to the development of the Uirapuru II.

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