About Us

Atlantic Flight Academy AFA was founded in 2011 in order to give Professional Pilot Training according to National and International Civil Aviation rules and regulations with the aim of meeting the increasing need of qualified pilots in fast-growing aviation industry.

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Barbaros Hayrettin Paşa mah. 1994 sok. No:14, Kat/3, 34522 Esenyurt/İstanbul

info@afa.aero

Headquarters: +90 212 662-20-13

DA20 AIRCRAFTS

The DA20's instrumentation and standard Garmin G500 avionics are designed for safety, a positive learning transfer, reliability and value. The DA20 is available in two engine variants. Choose between a Bombardier Rotax 912 iS3c Sport with 100 HP (DA20i Katana) and a fuel injected 125 hp Continental Motors IO-240 (DA20-C1 airplane).

15 x DA20 AIRCRAFTS :

  • TC-EOA
  • TC-EOC
  • TC-EOD
  • TC-EOE
  • TC-EOF
  • TC-EOG
  • TC-EOH
  • TC-EOI
  • TC-EOJ
  • TC-EOK
  • TC-EOS
  • TC-EOT
  • TC-EOV
  • TC-GAS
  • TC-GAG

DA20 C1 Dimensions

DA20 C1 Mass and Loading

  • Seats
  • Empty weight
  • Useful load
  • Max. take off mass
  • Fuel capacity total

  • 2
  • 535 kg.
  • 265 kg.
  • 800 kg.
  • 91 lt./65,5 kg.

  • 2
  • 1180 lbs.
  • 584 lbs.
  • 1764 lbs.
  • 24 US gal./144,4 lbs.

DA20 C1 PERFORMANCE (MTOM, ISA)

  • Max. cruise speed
  • Stall speed, landing configuration
  • Rate of climb (MSL)
  • Range at 55 % (8,000 ft)
  • Fuel Consumption at 55 % (8,000 ft)
  • Take-off ground roll / Take off distance (MSL, 50 ft)
  • Landing ground roll / Landing distance (MSL, 50 ft)
  • Max. operating altitude
  • Max. demonstrated crosswind

  • 240 km/h TAS
  • 67 km/h CAS
  • 4.2 m/s
  • 973 km
  • 20 l/h
  • 383 m / 500 m
  • 201 m / 415 m
  • 4,000 m
  • 37 km/h

  • 130 kts TAS
  • 36 kts CAS
  • 830 ft/min
  • 525 nm
  • 5.3 US gal/h
  • 1,256 ft / 1,640 ft
  • 661 ft/ 1,360 ft
  • 13,100 ft
  • 20 kts

DA40 AIRCRAFTS

The DA40 fully integrated G1000 NXi flight deck, incorporating the latest features with optional ultra-precise GFC700 Automatic Flight Control System, offers superior situational awareness, convenience and safety. Available equipment provides Traffic Advisories, Synthetic Vision Technology, Satellite WX and Entertainment, and more.

4 x DA40-NG AIRCRAFTS :

  • TC-EOM
  • TC-EON
  • TC-EOO
  • TC-EOP

DA40 NG DIMENSIONS, MASS and LOADING

  • Seats
  • Empty weight
  • Useful load
  • Max. take off mass
  • Fuel capacity total
  •  Main Tank (Fuel)
  •  Auxiliary Tank (Fuel)

  • 4
  • 900 kg.
  • 410 kg.
  • 1310 kg.
  • 147 lt./118 kg.
  • 106 lt./84 kg.
  • 41 lt./33 kg.

  • 4
  • 1984 lbs.
  • 904 lbs.
  • 2888 lbs.
  • 39 US gal./261 lbs.
  • 28 US gal./188 lbs.
  • 11 US gal./74 lbs.

DA40 NG PERFORMANCE (MTOM, ISA)

  • Max. speed (14,000 ft, MCP)
  • Cruise speed at 60 % (14,000 ft)
  • Cruise speed at 75 % (6,000 ft)
  • Stall speed, landing configuration
  • Rate of climb (ISA SL)
  • Range at 60 % (incl. auxiliary tank)
  • Range at 45 % (incl. auxiliary tank)
  • Fuel consumption
  • Take-off ground roll (ISA SL)
  • Landing ground roll (ISA SL)
  • Max. operating altitude
  • Max. demonstrated crosswind

  • 285 km/h TAS
  • 231 km/h TAS
  • -
  • 107 km/h CAS
  • 3.5 m/s
  • 1741 km
  • -
  • 19.5 l/h (@60%)
  • 370 m
  • 270 m
  • 5,000 m
  • 46 km/h

  • 154 kts TAS
  • 125 kts TAS
  • -
  • 58 kts CAS
  • 690 ft/min
  • 940 nm
  • -
  • 5.1 US gal/h (@60%)
  • 1,214 ft
  • 886 ft
  • 16,400 ft
  • 25 kts

DA42 AIRCRAFTS

The DA42 is powered by the Austro Engine 168hp AE300 with a single power lever control.
The 3 blade MT hydraulic constant speed propellers feature advanced blade geometry for efficient performance, smoothness and low noise. Automatically controlled by each engine’s digital engine control - feathering is as simple as flipping a single switch.
The fully integrated Garmin G1000 NXi is complemented by a long list of avionics options - such as an integrated weather radar and Synthetic Vision - to perfectly suit your mission.

3 x DA42-NG AIRCRAFTS :

  • TC-EOB
  • TC-EOR
  • TC-EOY

DA40 NG DIMENSION, MASS and LOADING

  • Seats
  • Empty weight
  • Useful load
  • Max. take off mass
  • Fuel capacity total
  •  Main Tank (Fuel)
  •  Auxiliary Tank (Fuel)

  • 4
  • 1,410 kg.
  • 589 kg.
  • 1,999 kg.
  • 289 lt./231 kg.
  • 189 lt./151 kg.
  • 100 lt./80 kg.

  • 4
  • 3,109 lbs.
  • 1,299 lbs.
  • 4,407 lbs.
  • 76.4 US gal./512 lbs.
  • 50 US gal./335 lbs.
  • 26.4 US gal./177 lbs.

DA42 NG PERFORMANCE (MTOM, ISA)

  • Max. speed (16,000 ft, MCP) 1,760 kg TOW
  • Cruise speed at 75 % (16,000 ft)
  • Stall speed, landing configuration
  • Rate of climb (ISA SL) 1,760 kg TOW
  • Single Engine Service Ceiling
  • Range at 60 % (12,000 ft, incl. auxiliary tank)
  • Consumption at 60 % in total
  • Take-off ground roll (ISA SL), 1,760 kg TOW
  • Landing ground roll (ISA SL)
  • Max. operating altitude
  • Max. demonstrated crosswind

  • 365 km/h TAS
  • 325 km/h TAS
  • 113 km/h CAS
  • 7.9 m/s
  • 5,486 km
  • 2,250 km
  • 39.4 l/h (@60%)
  • 280 m
  • 340 m
  • 5,486 m
  • 46 km/h

  • 197 kts TAS
  • 176 kts TAS
  • 61 kts CAS
  • 1550 ft/min
  • 18,000 ft/min
  • 1,215 nm
  • 10.4 US gal/h (@60%)
  • 919 ft
  • 1,115 ft
  • 18,000 ft
  • 25 kts