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MARK & MILES MALONE
Serial Number TD-560
MFR Year 1963
Model B95/B95A
Changes in the B95 version included a 19-inch (480 mm) cabin stretch to increase rear cabin area and the horizontal stabilizer and elevators were enlarged for better pitch control. A curved vertical stabilizer dorsal fairing is the most noticeable change. It also included a fifth seat, wider chord flaps, and an increased gross weight of 100 pounds. The 1961 Model B95A featured fuel injected Lycoming IO-360-B1A engines. A total 150 B95's were built in 1960, and 81 B95A's were built between 1961 and 1962 (serial numbers TD-453 through TD-533). The 1960 model was priced at $51,500 and the 1961-62 model was priced at $49,500.
IMG_9468
GOSTOMSKI JOHN J TRUSTEE/ GOSTOMSKI MARY F TRUSTEE
Serial Number 41LSA
MFR Year 2007
The AirMax SeaMax is a Brazilian single-engine, amphibious light sport aircraft (LSA) and Fédération Aéronautique Internationale microlight originally manufactured by AirMax Construções Aeronáuticas of Jacarepaguá.
By 2015 the manufacturer was Seamax Brasil of Sao Paulo.
The SeaMax was designed in 1999. A prototype was flown in 2000 and the first production aircraft left the factory in 2001.
The SeaMax is constructed using composite materials and metal components. It has a two-seat, side-by-side configuration cabin with a bubble canopy which is hydraulically raised for access. The high-wing is strut-braced and the tail is a cruciform tail. The aircraft's tricycle landing gear is retractable for landing on water. It is powered by a 100 hp (75 kW) Rotax 912ULS pusher configuration engine mounted above the wing to avoid water ingestion.
IMG_9366
GOSTOMSKI JOHN J TRUSTEE/ GOSTOMSKI MARY F TRUSTEE
Serial Number 41LSA
MFR Year 2007
The AirMax SeaMax is a Brazilian single-engine, amphibious light sport aircraft (LSA) and Fédération Aéronautique Internationale microlight originally manufactured by AirMax Construções Aeronáuticas of Jacarepaguá.
By 2015 the manufacturer was Seamax Brasil of Sao Paulo.
The SeaMax was designed in 1999. A prototype was flown in 2000 and the first production aircraft left the factory in 2001.
The SeaMax is constructed using composite materials and metal components. It has a two-seat, side-by-side configuration cabin with a bubble canopy which is hydraulically raised for access. The high-wing is strut-braced and the tail is a cruciform tail. The aircraft's tricycle landing gear is retractable for landing on water. It is powered by a 100 hp (75 kW) Rotax 912ULS pusher configuration engine mounted above the wing to avoid water ingestion.
ALLER DAVID C TRUSTEE / ALLER CLETA R TRUSTEE
Serial Number 19944
MFR Year 1951
170A
In 1949 Cessna began marketing the 170A, an all-metal 170 with zero-dihedral wing tapered outboard of the slightly-enlarged plain flaps, and a single strut replacing the "V" strut of the 170. This and subsequent versions of the 170 shared the fin/rudder shape of the larger Cessna 190 and 195 models.
IMG_9252
ERIKA J & CHRISTOPHER J COPELAND
Serial Number 929-73
MFR Year 1973
7ECA, Citabria Standard, Citabria Aurora
Introduced in 1964, the 7ECA was the first version of the design and utilized the Continental O-200-A engine of 100 horsepower (75 kW). When introduced, it featured wood-spar wings and oleo-shock main gear. Within the first year of production, Champion began offering the Lycoming O-235-C1 engine of 115 horsepower (86 kW) as an alternative to the Continental. In 1967, Champion switched to spring steel main gear legs; by then, the Lycoming engine had become the standard. On acquiring the design, Bellanca gave this model the name Citabria "Standard" and began using the 115 horsepower (86 kW) Lycoming O-235-K2C engine. When American Champion reintroduced the 7ECA in 1995 as the Citabria "Aurora, " the biggest change was the use of metal-spar wings; the most recent significant design change has been the switch to aluminum main gear legs in 2004.