Par mums

Par pilotu skolu Eriva

Pilotu skola ERIVA ir LR Civilās aviācijas aģentūras (CAA) apstiprināta mācību organizācija, kas veic privātpilotu un profesionālu transporta aviolīniju pilotu apmācību.

Pirmos helikopteru pilotus sākām apmācīt jau 2004. gadā, taču ar vārdu ERIVA sākām strādāt 2007. gadā. Skolas vadības un vadošo mācībspēku pieredze nozarē ir vēl krietni lielāka.

gadu

pieredze apmācībā

ERIVA ir pirmā pilotu skola Latvijā, kas sāka piedāvāt saviem studentiem apgūt arī aviolīniju transporta pilota (ATP) teorijas kursu, kā arī lidojumu programmas profesionālo pilotu sagatavošanai. Par savu konkurētspējīgo priekšrocību uzskatām augsto kvalitāti, ko sasniedzam ar uzstādītajām augstajām prasībām pret studentiem.

Mūsu mērķis ir sagatavot augstas raudzes profesionāļus, kā arī privātpilotus, kas vēlas lidot tikai sava prieka pēc, tomēr augsti drošības standarti ir mūsu darbības fundaments.

Šobrīd mūsu studenti ir ne tikai transporta aviolīniju piloti Eiropas un pasaules vadošajās aviokompānijās, bet veiksmīgi veido savu karjeru arī biznesa aviācijā. Tāpat arī lepojamies, ka Latvijas Republikas Valsts robežsardzes helikopteru piloti ir mūsu apmācīti.

Mūsu apmācības
programmas

Aviācijas
angļu valoda

Iepazīšanos
lidojums

Jun 05

18:00-21:00

PPL(A) 29, 30 gr.

Meteorology, Lesson 2

May 29

18:00-21:00

PPL(A) 29, 30 gr.

Meteorology, Lesson 1

May 23

18:00-21:00

PPL(A) 30 gr.

Aircraft General Knowledge, Lesson 5

Andrejs Juzičs

May 16

18:00-21:00

PPL(A) 30 gr.

Aircraft General Knowledge, Lesson 4

Andrejs Juzičs

May 15

18:00-21:00

PPL(A) 29 gr.

Operational Procedures, Lesson 3. Exam

Sergejs Markovs

May 09

18:00-21:00

PPL(A) 30 gr.

Aircraft General Knowledge, Lesson 3

Andrejs Juzičs

May 08

18:00-21:00

PPL(A) 29 gr.

Operational Procedures, Lesson 2

Sergejs Markovs

May 04

18:00-21:00

PPL(A) 30 gr.

Flight Performance and Planning, Lesson 2

Āris Cēders

Mūsu
sertifikāti

LVA.FSTD.06

LVA.ATO.03

LVA.LTB.01

Mūsu flote

TECNAM P2008JC

The Tecnam P2008 is an Italian single-engine, high-wing two-seat aircraft built by Costruzioni Aeronautiche Tecnam.

General characteristics

Capacity: 2
Length: 6.93 m (22 ft 9 in)
Wingspan: 8.80 m (28 ft 10 in)
Height: 2.46 m (8 ft 1 in)
Wing area: 11.50 m² (123.8 sq ft)
Aspect ratio: 6.7
Airfoil: NACA 63A
Empty weight: 354 kg (780 lb)
Max takeoff weight: 600 kg (1,323 lb)
Fuel capacity: 110 L (24.2 Imp gal, 29.0 US gal)
Powerplant: 1 × Rotax 912S flat four air and water cooled piston, 73.5 kW (98.6 hp)
Propellers: 2-bladed Tonini GT fixed pitch

Performance

Cruise speed: 215 km/h (134 mph, 116 kn) economical, 65% power at 2,286 m (7,500 ft)
Stall speed: 73 km/h (45 mph, 39 kn) flaps down
Range: 1,277 km (793 mi, 690 nmi)
Service ceiling: 4,265 m (13,993 ft)
g limits: +4/-2
Rate of climb: 5.85 m/s (1,152 ft/min) at sea level

Avionics

Standard VFR, two screen EFIS.

FSTD (FNPT II)

Flight simulator based on TECNAM P2006T can perform ground operations, take-off, variety of flight manoeuvres, visual landing, including the failures of various systems of the aircraft.

Making the most of every resource of the professional simulator, you can considerably cut down expenses saving on costly time of flight and engine cycle life of the airplane.

Image of terrestrial and celestial surface are projected on curved screen, with the dimension of 400 x 200 cm and Horizontal Field of View of 180°.
The software provides an accurate flight model including the climb, the effect of flying, torque, auto-rotation, etc.
Over 20,000 airports and all navigation aids are available.
Standard and user-definable VFR and IFR weather conditions are included.

TECNAM P2006T

The Tecnam P2006T is an Italian high-winged, twin-engined all-metal light aircraft built by Сostruzioni Aeronautiche Tecnam.

General characteristics
·        Crew: 1 (pilot)
·        Capacity: 3 passengers or 618 pounds (280 kg) payload with full fuel
·        Length: 8.69 m (28 ft 6 in)
·        Wingspan: 11.40 m (37 ft 5 in)
·        Height: 2.84 m (9 ft 4 in)
·        Wing area: 14.75 m² (158.8 sq ft)
·        Aspect ratio: 8.80
·        Empty weight: 760 kg (1,675 lb)
·        Max takeoff weight: 1,230 kg (2,712 lb)
·        Fuel capacity: 200 litres (44 imp gal; 53 US gal)
·        Powerplant: 2 × Rotax 912S3 horizontally opposed four-cylinder geared piston engines, 75 kW (100 hp) each
·        Propellers: 2-bladed MT Propeller MTV-21, 1.78 m (5 ft 10 in) diameter constant-speed, fully feathering

Performance
·        Maximum speed: 287 km/h (178 mph, 155 kn)
·        Cruise speed: 250 km/h (155 mph, 135 kn)
·        Stall speed: 87 km/h (54 mph, 47 kn)
· Never exceed speed: 309 km/h (192 mph, 167 kn)
· Minimum control speed: 115 km/h (71 mph, 62 kn)
·        Range: 1,374 km (853 mi, 742 nmi)
·        Endurance: 4.25 hours
·        Service ceiling: 4,300 m (14,000 ft)
·        Rate of climb: 6.4 m/s (1,260 ft/min) 250 ft/min (single engine)
·        Wing loading: 78 kg/m² (16 lb/sq ft) at MTOW
· Power/mass: 0,162 hp/kg (0,07 hp/lb)