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3Xtrim
3X55 Trener
3X47 Ultra
Navigator 600

 

3xtrm-Tren

 

First flown in 1996, the 3X55 Trener (English: Trainer) and 3X47 Ultra are a family of ultralight civil aircraft produced in Poland by the 3Xtrim Aircraft Factory. Both are two-seat, high-wing, strut-braced monoplanes with fixed tricycle undercarriage and available only as completed aircraft. There are also 450 Ultra and 495 Ultra Plus sub-variants of the 3X47 Ultra, with gross weights adjusted for national ultralight regulations.
 
Former SZD sailplane engineer Adam Kurbiel designed the predecessor of 3X55, the EOL-VLA, to conform to European JAR-VLA rules. That plane was modified through the years to meet Canadian Advanced Ultralight and US Light Sport Aircraft rules. The 3X47 version is specifically for the European market to meet those standards.
 
The designation 3X55 means “3Xtrim Aircraft - 550 kg gross weight” while the 3X47 refers to its 470 kg gross weight.
The US light sport aircraft version of the 3X55 is known as the Navigator 600 and has a 1320 pound maximum gross take-off weight.
 
The European versions feature extensive structural use of carbon fibre to achieve lightness, while the 3X55 is predominantly of fibreglass construction. Otherwise the two aircraft are similar in appearance and performance.
The 3X55 powerplant options are the 80 hp (60 kW) Rotax 912UL, the 100 hp (75 kW) 912ULS or the 80 hp (60 kW) Jabiru 2200. The 3X55 can be equipped with either a three-bladed, fixed pitch Czech-made Woodcomp wood/fibreglass SR 200 propeller or an electrically adjustable Woodcomp SR 2000 propeller, with an optional constant speed unit.
The fuselage and vertical tail of the 3X55 is a one-piece structure made from fibreglass. The firewall is a Fiberfrax ceramic/aluminium sandwich. The cockpit is 47.5 inches (1.21 m) wide at the elbows. Crew access is via a door on each side of the cockpit that hinges upwards and is supported by a gas strut.
 
The control sticks are located conventionally in front of each seat. The standard throttle arrangement is one panel-mounted centre throttle, but a second throttle located on the left side of the panel is optional, allowing the left-seat pilot to fly with either hand on the throttle or stick.
 
The wings are strut-braced with a single spar and are made from fibreglass and foam with a 15.5% TsAGI.R3 airfoil. The wing has a span of 31 .5 feet and an area of 127.4 sq ft (11.84 sq.m), which gives it a wing loading of 9.5 lbs/sq ft at gross weight. The aircraft has removable wings, with single locking pins and quick-disconnect controls which can be easily hooked up and inspected from inside the cockpit.
 
The wings have conventional Frise ailerons and slotted flaps. The elevator and rudder are also conventional. Ailerons and elevator are controlled by dual centre-mounted sticks through push-pull tubes, while the rudder is controlled by cables. The rudder cables attach to the rudder by wrapping around the wide bottom diameter of the rudder itself. The pitot tube is mounted in the left-hand strut.
 
The flaps are operated by a ceiling-mounted flap handle with detents for 0, 15 and 30 degrees of deflection. The flaps are controlled directly with the handle attached to a flap centre-section behind the fuselage and the wing flaps plug into the flap centre-section. Flaps are normally set to 15 degrees for take-off and 30 degrees for landing.
 
The fuel tank is located behind the right-hand seat. The quantity can be read directly through a sight gauge behind the seat. The standard tank is 70 litres (18 US gallons) with 87 litres (23 US gallons) optional. The standard fuel is premium auto fuel, but it can run on 100LL as well. Behind the left-hand seat is a small baggage compartment, with additional baggage space above and behind both seats.
 
The main landing gear consists of sprung fibreglass gear legs with 5X5.00 tires as standard on graphite wheel rims. Larger 6X6.00 tires are optional. The nose gear is a single-fork design also made from fibreglass. Nose gear suspension is a compressed rubber donut system. The plane comes in one colour – white, but owners can add their own vinyl decals to finish the plane as desired.
 
The 3X55 first flew in 1996 and by the summer of 2006 about 60 aircraft of both types had been produced with a base price of US$99,900.

 

3xtrm-Tren-2


Krzysztof Wieczorek won the 16th FAI World Precision Flying Championship in 2004 and took the 3rd place in the 14th FAI World Rally Flying Championship in 2004 flying 3Xtrim aircraft. In the 17th FAI World Precision Flying Championship in 2006, 3Xtrim took the 1st (Krzysztof Wieczorek) and 3rd (Krzysztof Skrętowicz) places.

 

Specifications:
 
550 Trener
Engine: 1 × Rotax 912, 73.4 kW (98.6 hp)
Wingspan: 10.03 m (32 ft 11 in)
Length: 6.87 m (22 ft 6½ in)
Height: 2.40 m (7 ft 10¾ in)
Wing area: 12.40 sq.m (133.5 sq.ft)
Empty weight: 325 kg (717 lb)
Max. takeoff weight: 550 kg (1,212 lb)
Never exceed speed: 220 km/h (118 knots, 136 mph)
Cruise speed: 170 km/h (91 knots, 106 mph)
Stall speed: 70 km/h (38 knots, 44 mph)
Range: 750 km (405 nmi, 466 mi)
Service ceiling: 4,000 m (13,120 ft)
Rate of climb: 4.5 m/s (886 ft/min)
Crew: 1
Capacity: 1 passenger

 

3X55 Trainer     
Engine: Rotax 912 ULS
Wing span: 9.60m / 31.5ft
Length: 6.87m / 22.5ft
Height: 2.4m / 7.9ft
Wing area: 11.84sq.m / 127.4sq.ft
Cabin width: 1.2m / 47.2in
Wing load: 46.5 kg/sq.m / 9.52lbs/sq.ft
Max. take-off weight: 550kg / 1212 lbs
Empty weight: 325 kg / 716lbs
Useful load: 225 kg / 496lbs
Fuel tank capacity std: 18.5Impg / 23.2 US gal
Never Exceed Speed (IAS) VNE: 109kts
Cruise speed max. cont. Power (IAS): 100kts
Cruise speed 75% power (IAS): 88kts
Stall speed  (IAS) Vso: 39kts
Manoeuvering Speed (IAS) VA: 75kts
Maximum Flap Extended Speed (IAS) VFE full flaps: 62kts
Maximum Flap Extended Speed (IAS) VFE take-off flaps: 74kts
Maximum climb rate: 1000ft/min / 62kts IAS
Take-off distance 50ft obstacle: 918ft / 280m
Range: 388NM / 720km

 

 


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