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Air gliding and Flying school Prijedor
 
 

Excursion's informations


Our offer is based on whole-day trips for student pilots and their companions and it is adjusted to clients

We are in friendly relations with regional partners :

Air gliding schools from Bosnia, Croatia, Slovenia


Because of the very favorable weather conditions and free airspace primary activity of the club is gliding. Many testify that this is the most beautiful form of flight when the pilot and glider merge in search of heights and distances using winds, mountain slopes and thermal air currents which in our region does not lack, indeed, Prijedor and its surroundings abound Meteorological diversity that benefits all the techniques of aeronautical races .

Aero Club "Prijedor"
Prijedor is aviation sports organization, which was founded davne 1952.godine . For dealing with aviation sport takes a lot of expertise, discipline in the implementation of all elements of flight , starting from the preparation of the country to the realization in the air , and personal courage .
As one of the most important partners in the work of the Aero Club and the town of Prijedor accordingly Aero Club Prijedor wants to be involved in the program event marking the Day of the town of Prijedor on 16 May .
It should be noted that the Aero Club of Prijedor this year marked a specific jubilee
- 20 years parachute Petrovdanskog Cup and 10 years
- Blanik Cup
two international events held continuously in the town of Prijedor.

Blanik Cup is a regional competition that is organized at the airport every year and each year increased the quality and number of competitors. Also sailing camps and weekend visiting sailors from different European countries over a long period of sailing the annual club activities that contribute to the promotion and development of yachting, tourism and this region of the world as an attractive tourist and sports destination.

Glidin school in Aero Club "Prijedor"
Prijedor is registered 2010, and we in last five years had 40 students pilot and 4 instructor that have successfully finished their training lessons.
Who ever experienced or mastered flying boats remained indifferent and again he returns because of the indescribable feeling that gives this sport or in the words of Leonardo da Vinci:

"Once you've felt flight,
you'll go underground eyes on the sky,
where have you been
and where you want to go "



Contact us for any information or advice


Airport Urije

Basic characteristics of Urije airport are:

• The runway is 900m long grass and a width of 100 m
• Airport is at an altitude of 180m
• The coordinates of 44 48 30 north latitude and 16 42 53 east of Greenwich
• The airport is equipped with two hangars gas stations and necessary working space .
• The reference temperature is 26.5 C
• Airport “ Urije “ in Prijedor only has authorization for VFR flights at night in BIH
• Classroom is an integral part of the airport and schools.

It is important to note that there is no satisfactory an access road infrastructure and airport is only 2 kilometers far from center of Prijedor city

From decembre 2015 until march 2016 we need to build new hangar and concret runway 700 meters x 10 meters and asphalt taxiway. This will be founded by IPA fond from European union, whith in project CAN.


Airplane for towing glider


A. Utva 75

General characteristics

• Crew: 2
• Capacity: 210 kg (460 lb) max
• Length: 7.11 m (23 ft 4 in)
• Wingspan: 9.73 m (31 ft 11 in)
• Height: 3.15 m (10 ft 4 in)
• Wing area: 14.63 m2 (157.5 sq ft)
• Aspect ratio: 6.5
• Empty weight: 685 kg (1,510 lb) equipped
• Max takeoff weight: 960 kg (2,116 lb)
• Fuel capacity: standard:160 l (42 US gal; 35 imp gal): with drop tanks 360 l (95 US gal; 79 imp gal)
• Powerplant: 1 × Lycoming IO-360-B1F 4-cyl. Air-cooled horizontally-opposed piston engine, 134 kW (180 hp)
• Propellers: 2-bladed Hartzell HC-C2YK-1BF/F7666A variable-pitch metal propeller

Performance
• Maximum speed: 215 km/h (134 mph; 116 kn)
• Cruising speed: 165 km/h (103 mph; 89 kn)
• Stall speed: 95 km/h (59 mph; 51 kn) flaps up at idle 82 km/h (51 mph; 44 kn) 25° flap at idle
• Range: 800 km (497 mi; 432 nmi)
• Ferry range: 1,080 km (671 mi; 583 nmi)
• Service ceiling: 4,000 m (13,123 ft) • g limits: +6 -3
• Rate of climb: 4.5 m/s (890 ft/min)


B. Citabria 7GCBC


General characteristics

• Crew: one
• Capacity: one passenger
• Length: 22 ft 9 in (6.93 m)
• Wingspan: 33 ft 5 in (10.19 m)
• Height: 6 ft 5 in (1.96 m)
• Wing area: 165 sq ft (15.3 m2)
• Aspect ratio: 6.8:1
• Airfoil: NACA 4412
• Empty weight: 1,110 lb (503 kg)
• Gross weight: 1,650 lb (748 kg)
• Powerplant: 1 × Lycoming O-320-A2B four cylinder, four-stroke, horizontally opposed aircraft engine, 150 hp (110 kW)

Performance
• Cruise speed: 126 mph (109 kn; 203 km/h)
• Stall speed: 51 mph (44 kn; 82 km/h)
• Never exceed speed: 162 mph (141 kn; 261 km/h)
• Range: 500 mi (434 nmi; 805 km)
• Service ceiling: 12,000 ft (3,658 m)
• G limits: +5/-2
• Rate of climb: 1,120 ft/min (5.7 m/s)
• Wing loading: 10.0 lb/sq ft (49 kg/m2)


C. Piper PA 18

General characteristics

• Crew: 1
• Capacity: 1 passenger
• Length: 22 ft 7 in (6.88 m)
• Wingspan: 35 ft 2½ in (10.73 m)
• Height: 6 ft 8½ in (2.02 m)
• Wing area: 178.5 sq ft (16.58 m²)
• Airfoil: USA 35B
• Aspect ratio: 7:1
• Empty weight: 930 lb (422 kg)
• Max. takeoff weight: 1,750 lb (794 kg)
• Powerplant: 1 × Lycoming O-320 air-cooled flat four, 150 hp (112 kW)

Performance
• Never exceed speed: 132 kn (246 km/h, 153 mph)
• Maximum speed: 113 knots (208 km/h, 130 mph) at sea level
• Cruise speed: 100 kn (185 km/h, 115 mph) (75% power)
• Stall speed: 38 knots (69 km/h, 43 mph) flaps down
• Range: 399 nmi (735 km, 460 mi)
• Service ceiling: 19,000 ft (5,595 m)


D. Morane Sauliner 893


General characteristics

• Crew: one pilot
• Capacity: three passengers
• Length: 7.24 m (23 ft 9 in)
• Wingspan: 9.74 m (31 ft 11 in)
• Height: 2.80 m (9 ft 2¼ in)
• Wing area: 12.3 m² (132 ft²)
• Empty weight: 570 kg (1,257 lb)
• Max. takeoff weight: 1,050 kg (2,315 lb)
• Powerplant: 1 × Lycoming O-360-A3A air cooled flat four piston engine, 134 kW (180 hp)

Performance
• Maximum speed: 240 km/h (129 knots, 149 mph)
• Cruise speed: 225 km/h (121 knots, 140 mph)
• Stall speed: 92 km/h (50 knots, 57.5 mph)
• Range: 1,300 km (702 nm, 807 mi)
• Service ceiling: 3,600 m (11,800 ft)
• Rate of climb: 3.85 m/s (758 ft/min)
• Wing loading: 85.4 kg/m² (17.5 lb/ft²)
• Power/mass: 0.13 kW/kg (0.078 hp/lb)



Gliders



A. Blanik L 13

General characteristics

• Crew: 2
• Length: 8.4 m (27 ft 7 in)
• Wingspan: 16.2 m (53 ft 2 in)
• Wing area: 19.15 m2 (206.1 sq ft)
• Aspect ratio: 13.7
• Airfoil: Root: NACA 652A 615, Tip: NACA 652A 612
• Empty weight: 292 kg (644 lb) equipped
• Gross weight: 500 kg (1,102 lb)

Performance
• Stall speed: 62 km/h (39 mph; 33 kn) (Flaps 0°), 56 km/h (34.8 mph; 30.2 kn) (Flaps 10°)
• Never exceed speed: 240 km/h (149 mph; 130 kn)
• Rough air speed max: 145 km/h (90.1 mph; 78.3 kn)
• Aerotow speed: 140 km/h (87.0 mph; 75.6 kn)
• Winch launch speed: 100 km/h (62.1 mph; 54.0 kn)
• Terminal velocity: with full airbrakes 258 km/h (160 mph; 139 kn)
• g limits: +5 -2.5 at 136 km/h (84.5 mph; 73.4 kn)
• Maximum glide ratio: 28.2 at 93 km/h (57.8 mph; 50.2 kn)
• Rate of sink: 0.84 m/s (165 ft/min) at 83 km/h (51.6 mph; 44.8 kn)
• Wing loading: 26.1 kg/m2 (5.3 lb/sq ft)


B. Blanik L 23

General characteristics

• Crew: 2
• Length: 8.5 m (27 ft 11 in)
• Wingspan: 16.2 m (53 ft 2 in)
• Height: 1.9 m (6 ft 3 in)
• Wing area: 19.15 m2 (206.1 sq ft)
• Airfoil: root: NACA 632A-615 ; tip:NACA 632A-612
• Empty weight: 310 kg (683 lb)
• Max takeoff weight: 510 kg (1,124 lb) dual

Performance
• Stall speed: 56 km/h (35 mph; 30 kn) at max t/o weight dual
• Never exceed speed: 256 km/h; 159 mph (138 kn) in smooth air at max t/o weight dual
160 km/h (86 kn; 99 mph) in rough air
150 km/h (81 kn; 93 mph) on aero-tow
120 km/h (65 kn; 75 mph) on winch launch
130 km/h (70 kn; 81 mph) flaps extended
• g limits: +5.3 -1.5 at max t/o weight dual, +6 -3 at max t/o weight solo
• Maximum glide ratio: 28 at 90 km/h (49 kn; 56 mph) at max t/o weight dual
• Rate of sink: 0.82 m/s (161 ft/min) at 80 km/h (43 kn; 50 mph) at max t/o weight dual
• Wing loading: 26.63 kg/m2 (5.45 lb/sq ft) max dual


C. Bergefalke II 55/2

General characteristics

• Crew: 2
• Length: 8 m (26 ft 3 in)
• Wingspan: 16.6 m (54 ft 6 in)
• Wing area: 17.7 m2 (191 sq ft)
• Aspect ratio: 15.6
• Airfoil: Mü-Profil 14.5%
• Empty weight: 246 kg (542 lb)
• Max takeoff weight: 440 kg (970 lb)

Performance
• Stall speed: 60 km/h (37 mph; 32 kn)
• Never exceed speed: 160 km/h (99 mph; 86 kn)
• Rough air speed max: 120 km/h (74.6 mph; 64.8 kn)
• Aerotow speed: 120 km/h (74.6 mph; 64.8 kn)
• Winch launch max speed: 85 km/h (52.8 mph; 45.9 kn)
• Terminal velocity: 205 km/h (127.4 mph; 110.7 kn) (max all-up weight + full airbrakes / flaps)
• g limits: +4 -2
• Maximum glide ratio: 28:1at 80 km/h (49.7 mph; 43.2 kn)
• Rate of sink: 0.72 m/s (142 ft/min) at 72 km/h (44.7 mph; 38.9 kn)
• Wing loading: 24.8 kg/m2 (5.1 lb/sq ft)


D. Bergefalke III

General characteristics

• Crew: 2
• Length: 8 m (26 ft 3 in)
• Wingspan: 16.6 m (54 ft 6 in)
• Wing area: 17.7 m2 (191 sq ft)
• Aspect ratio: 15.6
• Airfoil: Mü-Profil 14.5%
• Empty weight: 246 kg (542 lb)
• Max takeoff weight: 440 kg (970 lb)

Performance
• Stall speed: 60 km/h (37 mph; 32 kn)
• Never exceed speed: 160 km/h (99 mph; 86 kn)
• Rough air speed max: 120 km/h (74.6 mph; 64.8 kn)
• Aerotow speed: 120 km/h (74.6 mph; 64.8 kn)
• Winch launch max speed: 85 km/h (52.8 mph; 45.9 kn)
• Terminal velocity: 205 km/h (127.4 mph; 110.7 kn) (max all-up weight + full airbrakes / flaps)
• g limits: +4 -2
• Maximum glide ratio: 28:1at 80 km/h (49.7 mph; 43.2 kn)
• Rate of sink: 0.72 m/s (142 ft/min) at 72 km/h (44.7 mph; 38.9 kn)
• Wing loading: 24.8 kg/m2 (5.1 lb/sq ft)
 
 

Air gliding and Flying school Prijedor


- Starts from:
Prijedor
- Also available transfers from:
Banjaluka, Zagreb, Sarajevo
(Send request for transfer)
- Excursion duration:
08:00 - 20:00
- Departure date:
Every day
- Active from :
01.04.-01.10.
 

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