Beechcraft 95 Travelair N195JR

This beautiful Beech 95 Travel Air is an eye-catcher at air shows and fly-ins and both an impressive classic and a convenient family cruiser! It was built as a competitor to the Cessna 310 and the Piper Apache, Beechcraft chose to reuse the name Travel Air, which was the predecessor to Beechcraft: the Travel Air Manufacturing Company.

The design of the Beech 95 Travel Air was based on the successful single engine Beech 35 Bonanza: it was fitted with the vertical stabilizer of the T-34 Mentor military trainer and two four-cylinder Lycoming O-360 engines. Its wing spar and the thicker gauge aluminum on the leading edgewere borrowed from the large Model 50 Twin Bonanza. The landing gear was also taken from the T-34 Mentor, which was built to train pilots for future aircraft carrier landings.
The Beech 95 Travel Air was powered by two Lycoming O-360-A1A engines at 180 horsepower (130 kW) at 2700rpm each. With 75% power, the Travel Air cruises 200 mph at 7,500ft.

Aircraft, Engine and Propeller:

  Aircraft: built in 1957. Serial nrTD-15. Its current second owner owns the aircraft since 1992. TT Airframe 6596 hrs.Completely overhauled and restored and newly painted in 2004.Has always been hangered. Complete logbooks. Next Annual August 2021.
  Engines: Left: Lycoming 0-360-A1A, S/N RL-39560-36E, 433 hrs. TSMOH 2000 hrs.TBO.
Right: Lycoming 0-360-A1A, S/N L26230-36A, 690 hrs. TSMOH 2000 hrs. TBO.
  Propellers: Left: Hartzell HC-C2YK-2, new 2004. serial nr AU 11355B, 517 hrs. Right: Hartzell HC-C2YK-2, new 2004. serial nr AU11345B, 517 hrs.

Avionics:

  Auto-pilot S-Tec Thirty Alt
  Garmin 695
  Garmin 340 audio panel
  KRT 2 radio (8.33 Khz)
  Garmin GTX 328 Transponder
  Nav/Com Bendix/King KX 125 TSO
  Com/GPS Bendix/King KLX 135A
  DME King KN 62 TSO
  ADF Bendix /King KR 87 TSO

Specifications:

  Gross weight: 4200 lbs.(luggage rear: max 400 Lbs.,front: 270 lbs.).
  Useful load: 1650 lbs. actual.
  Cruise speed: 160 Kts.
  Endurance: 6 hrs.
  Maximum range:(143 kts) 1050 miles on 112 gal.
  Fuel tanks: main 50 gal,total 112 gal (106 gal usable), aux 62 gal.
  New main tires August 2019
  New ELT batt.August 2018
  Heater: Janitrol, 50.000 btu.Completely overhauled in 2011.

Viewing location: Flugplatz Nordhorn-Lingen, Germany (EDWN: 10 km from the Dutch border).
For more information:

  sales@amnetherlands.nl

Yakovlev YAK-52 – LY-FOU

This sensational eye-catcher is a real Cold War Soviet primary trainer. The Yak-52 was designed as an aerobatic trainer for students in the Soviet DOSAAF training organisation and was first flown in 1976. This aircraft, registered LY-FOU, was built in 1981 in licence by Aerostar in Romania. The aircraft was completely overhauled in 2012.
LY-FOU has been newly painted in 2012. Colours: Black with red stars.
The aircraft can be viewed at Spa in Belgium (EBSP).

Aircraft, Engine and Propeller:

  Yakovlev YAK-52
  S/N: 811704, produced in: 1981. Total hours: 1882
  Color: Black with red stars 
  Engine: Vedeneïev M-14P, TTSO: 87 hrs
  Propeller: V-530 TA-D35, TTSO : 87 hrs

Avionics:

  COM: Com: Becker CU6401-1 (8,33 kHz) – Intercom; Transponder: Becker BXP6403-2 mode S; Artificial Digital Horizon: RC Allen RCA2610

Viewing location: EBSP, SPA-La Sauvenière, Belgium
For more information:

  sales@amnetherlands.nl

Aeromot AMT-200S Super Ximango

The Aeromot AMT-100 Ximango is a modernized Fournier RF-10 motor glider with a 100 hp Rotax 912S2. The AMT-200S Super Ximango is a two-place side-by-side, retractable gear, low wing, T-tail, motorized glider of all fiberglass/carbon fiber/epoxy resin construction. Equipped with spoilers, it can simulate the flight characteristics of a glider in aerial maneuvers and in the pattern. It can transition from powered flight to soaring in approximately three seconds. It can also be used for cross-country training because it allows pilots to practice soaring techniques without the risk of an off-field landing. The wings can be folded for storage or transportation.

The Aeromot AMT-100S Super Ximango has dual flight controls. The canopy is a one-piece design, allowing for excellent visibility. The Super Ximango is very popular with individual owners and flying schools in Europe, Australia and the USA (where 14 examples are being operated by the U.S. Air Force Academy designated as the TG-14a). The Ximango is also being operated by NASA at Armstrong Flight Research Center.

Although originally designed in France by René Fournier, this modernized version of the Fournier RF-10 motor glider was developed and built by the Grupo Aeromot Aircraft Corporation of Brazil.

This AMT-200S Super Ximango was built in 2007 and is one of the last Super Ximango´s built by Aeromot. This Superior TMG has always been hangered. The Super XimangoG-XYZT has a brand new engine and propeller. One of the best touring motor gliders still available. In excellent condition, very low hours on the air frame and almost zero on the engine and propeller. Tinted (blue) Canopy, Pitot-Static System, Cockpit Heater, WingFolding System and Hinge Fairings (complete).Installed Options:  High-Performance Winglets, Pilot / Copilot Toebrakes, Cockpit Auxiliary Power Outlets.

Aircraft, Engine and Propeller:

  Airframe: Registration G-XYZT, Serial # SN 200.176. (One of the last Super Ximango´s built). TTSN Airframe 350 hrs (apprx). ARC valid until July 22nd 2022.
  Engine: Rotax 912 S2 (100 hp; TBO 2000 hr or 15 Years). Almost new. TTSN Engine apprx 45 hrs and apprx 14,5 years.
  Propeller: Hoffman. TTSN Propellor 0 hrs and apprx 6 years. The propeller has a wood core and is fiberglass covered. It is a variable pitch propeller and can be set to climb, cruise or feathered pitch.

Avionics:

Garmin Aera 500
Dynon EFIS-D10A
Dynon EMS-D10
Garmin VHF Nav/Com GNC-255a
  Garmin GTX 328 Transponder
Garmin GTX 328 mode S transponder
LX NAV FD computer and GPS navigation system
Sigtronic SPA 400 intercom
ELT
PCAS XRX portable collision avoidance system

Specifications:

  Trainer and Cross-Country platform.
  Power Plant: ROTAX 912S4.
  Thrust: 100 hp at 5800 rpm at sea level.
  Length: 26 ft 6 in.
  Height: 6 ft 4 in.
  Wingspan: 57 ft 4 in (58 ft with wing tip extensions).
Maximum Takeoff Weight: 1874 lbs
Max Speed: 132 kts indicated
Glide Ratio: 31:1
Ceiling: 20,000 ft msl
Empty weight: 658 kg.
MTOW: 850 kg.
Max Positive G Limit: 5.3 (at maneuvering airspeed)
Max Negative G Limit: 2.65 (at maneuvering airspeed)
Range: 400-500 Nautical Miles
Crew: 2 (student pilot or passenger and instructor pilot)>

For more information:

  sales@amnetherlands.nl

Scottish Aviation Bulldog Series 100 PH-BLD

The Scottish Aviation Bulldog is a two-seat side-by-side (with optional third seat) training aircraft. The prototype Bulldog flew on 19 May 1969 at Shoreham Airport (UK). The first order for the type was for 78 from the Swedish Air Board. Production rights and the Swedish order were taken over from Beagle by Scottish Aviation (Bulldog) Limited. All subsequent aircraft were built at Prestwick Airport by Scottish Aviation, later by British Aerospace. The first 58 aircraft were delivered to the Swedish Air Force in 1971. Twenty more aircraft were delivered to the Swedish Army.

This Scottish Aviation Bulldog was built in 1972 for the Swedish Army (ARMEN). It served as ´61063´ as a trainer from 1972 – 2004. Hungary AviaRent Kft. HA-TUG: 2004 – 2012
Private Dutch ownership HA-TUG/PH-BLD since 2012

Aircraft, Engine and Propeller:

  Airframe: 3617 hrs. TT
  Engine: Lycoming IO-360-A1B6 200HP hrs.: 1420 SOH
  Propeller: Hartzell HC-C2YK-4C constant speed, 94 hrs. since new

Avionics:

  VHF Radio: Trig TY91 8.33 kHz
  VHF NAV: Becker NAV 2000 VOR
  Transponder: Trig TT 21 Mode S

Specifications:

  Year: 1972
  ICAO CofA
  Type Responsibility Agreement (TRA): DeHavilland
  Support Ltd. CAMO: AMN
  Aircraft has always been hangared
  Sale includes Cambrai Aircraft cover, towbar and some spare parts

Viewing location: AMN Teuge, The Netherlands
For more information:

  sales@amnetherlands.nl

Fuji FA-200-160 – PH-FJI

This aerobatic four-seater aircraft was built in Japan in 1973 by Fuji Heavy Industries Ltd.- Aircraft Division, and assembled at Teuge airport in The Netherlands by Gelderse Luchtvaartmij. PH-FJI has flown in the UK registered G-BBRE since 1973 and as G-KARI since 1984.
Currently registered as PH-FJI in The Netherlands, since January 2019. MTOW: 1059 kg.

Aircraft, Engine and Propeller:

  Fuji Heavy Industries LTD/Aero Subaru FA-200-160
  S/N: FA200-236, produced in: 1973. Total hours: 2528
  Color: Red and white
  Engine: Lycoming O-320-D2A reciprocating engine, 295 hrs since OH
  Propeller: McCauley Propeller 1C172/MGM fixed pitch metal, 37 hrs since OH

Avionics:

  NAVCOM: MX-170B, COM2: TY-96, XPDR: TT-31, DME: KN-64

Viewing location: AMN, Teuge Airport, The Netherlands
For more information:

  sales@amnetherlands.nl

Fuji FA-200-180 Aero Subaru D-ELHS

This aerobatic four-seater aircraft was built in Japan in 1970 by Fuji Heavy Industries Ltd.- Aircraft Division. The Fuji FA-200-180 Aero Subaru is an excellent aerobatics en upset recovery training aircraft, but also a nice and sturdy all-metal four seat tourer, offering its pilot and passenger an excellent panoramic view.

Aircraft, Engine and Propeller:

  Fuji Heavy Industries LTD FA-200-180 Aero Subaru
  S/N: FA200-080, produced in 1970. Total hours: 2658 hrs.
  Colors: The aircraft sports a blue, grey and white livery.
  Engine Manufacturer and Model: Lycoming IO-360-B1B rated at 180 hp 1113 hrs.
  Propeller: Propeller: McCauley Propeller 1C172/MGM fixed pitch metal, 408 hrs since OH

Avionics:

  –

Viewing location: Zelf Vliegen Flight Academy, Lelystad Airport, The Netherlands.
For more information:

  sales@amnetherlands.nl

New Aero AT-3 R100 EASA CS-VLA

The Aero AT-3 R100 is a new low wing two-seat training, sports, club and utility aircraft, manufactured in Poland by Aero AT. The structure is largely of all-metal construction. Deliveries commenced in 2002. It is certified under the EASA Very Light Aircraft regulations.
The AT-3 is an all-metal semi-stressed skin aircraft certified by EASA in the Very Light Airplane category. Developable surface construction with fairings and cowlings made of carbon-fibre glass composite. Main structural use solid rivets for strength, longevity and safety. Anti-corrosion protection by anodizing and cadmium plating makes each AT-3 series aircraft immune to the weather conditions. The tricycle undercarriage was specially designed to absorb heavy landings. Low operating cost, easy maintenance making the AT-3R ideal for club, group and training. Effective 3-stage flaps also make the AT-3 ideal for short field operation.
The low-wing aircraft has a side by side cockpit, is equipped with dual controls, a classic robust landing gear plus superb aerodynamics. It ensures high performance, good handling and exceptional flight characteristics.
The AERO AT-3R is available in five basic versions: AT-3 R100 ROTAX 912S Standard, AT-3 R100 ROTAX 912S Tourer Analog, AT-3 R100 ROTAX 912S Analog Tourer G5, AT-3 R100 ROTAX 912iSc Tourer Analog and AT-3 R100 ROTAX 912iSc Tourer G5.

Aircraft, Engine and Propeller:

  Aircraft: this new AT-3R is a two-seat, low wing, utility aircraft manufactured in Poland by Aero AT and delivered by AEROs official dealer for the Benelux: Zelf Vliegen Flight Academy.
  Engine: Rotax 912S / Rotax 912iSc, 100 hp (75 kW).
  Propeller: three-bladed composite ELPROP 3-1-1P propeller.

Avionics:

  Turn indicator 3 1/8″, Electronic clock M800, Electronic artificial horizon RCA2600, Directional indicator 3 1/8″, Garmin 2xG5 (PFD & DG/HSI), Avionic master switch, Voice activated intercom SPA-400, COM/NAV/GPS GTN650, COM/NAV Garmin GNC 255A + VOR, COM Garmin GTR 225A, Transponder Mode S ADS-B in Garmin GTX345, Transponder Mode S ADS-B, Garmin GTX335, GPS GARMIN AERA660, GPS GARMIN 696, GPS GARMIN 795, Anticollision system FLARM View 57, Hour meter with oil pressure switch, Flight hour meter plus many additional options.

Specifications:

  MTOW 630 kg (1388lb)
Empty weight 380 kg (837lb)
Useful load 250 kg (551lb)
Powerplant: 1 × Rotax 912S Elprop 3-1-1P, 100 hp (75 kW)
Never exceed speed: 236 km/h (127 kn)
Maximum speed: 220 km/h (119 kn)
Cruise speed: 200 km/h (108 kn)
Stall speed: 82 km/h (44 kn)
Range: 1300 km.

For more information:

  sales@amnetherlands.nl

New Blackshape Bk160 Gabriél EASA CS-VLA

The Blackshape Gabriél is a two-seat tandem training aircraft with outstanding performance and EASA CS-VLA certification. The aircraft is equipped with a modern glass cockpit with dual controls and is capable of top performance and flight qualities. The Gabriél is designed to offer operational training flexibility, comfortable crew accommodation and outstanding visibility.
Blackshape takes care of all the carbon fiber processes from lamination and moulding to autoclave processes and assembly. The wing aerodynamic design provides excellent behaviour at top speed and low stall/terminal speed, resulting in outstanding safety features and flight characteristics. This offer is for a factory new aircraft, offered by the official Blackshape dealer.

Aircraft, Engine and Propeller:

  Aircraft: the Blackshape Bk160 Gabriél is EASA CS-VLA certified built by Blackshape S.P.A. in Italy and delivered by Blackshapes official dealer for several countries in Europe: Zelf Vliegen Flight Academy.
  Engine: Lycoming IO-320-D1B: 160 hp (119 kW) at 2700 rpm.
  Propeller: Hartzell variable pitch propeller.

Avionics:

  Primary Flight Display: EFD1000 Pro, Aspen; Multi Flight Display: EFD1000, Aspen; Engine Monitoring: EDM900, J.P. Instruments; NAV1/COM1: GTN650, Garmin; NAV2/COM2: GNC255, Garmin; Transponder: GTX335R, Garmin; Audio Panel: GMA340, Garmin; Stall Warning; ELT: E04 406 MHz, ACK Technologies; KLR10 Lift Reserve Indicator (optional).

Specifications:

Dimensions: wing area: 10,31 m2, wing span: 9,00 m, height overall: 2,45 m,
length overall 7,45 m
Max. Takeoff Weight 850 kg
Takeoff Run 250 m
Takeoff Over 50ft Obstacle 360 m
Max Rate of Climb (MTOW, SL) 1550 fpm
Max Operating Altitude 15000 ft
Max Level Speed (SL) 164 KTAS
Landing Groundroll 190 m
Load Factor +4.4 / – 2 g
Max Endurance 3.2 h

For more information:

  sales@amnetherlands.nl

Socata TB-9 Tampico – PH-BEA

This TB-9 Tampico was built in 1990. Its last operational owner was NAV Flight Academy (Nederlandse Academie voor Verkeers- en beroepsvliegers) at Enschede Airport Twente in The Netherlands.
Built by Groupe Aérospatiale SOCATA in France.

Aircraft, Engine and Propeller:

  Daher Aerospace – Socata TB-9 Tampico
  S/N: 1130, produced in: 1990. Total hours: 3995
  Color: White, blue striping 
  Engine: Lycoming O-320-D2A, 1803 hours
  Propeller: Sensenich 74DM6S8-0-54 (Fixed Pitch Metal, 2-bladed) 1948 hours

Avionics:

  –

Viewing location: AMN, Teuge Airport, The Netherlands
For more information:

  sales@amnetherlands.nl

Socata TB-9C – PH-SXN

This TB-9C Tampico Club was built in 1993. Since 2009, it was operated by NAV Flight Academy (Nederlandse Academie voor Verkeers- en beroepsvliegers) at Enschede Airport Twente in The Netherlands.
Built by the French Groupe Aérospatiale SOCATA.

Aircraft, Engine and Propeller:

  Daher Aerospace – Socata TB-9C Tampico Club
  S/N: 1541, produced in: 1993. Total hours: 5758
  Color: White, red striping 
  Engine: Lycoming O-320-D2A, 2228 hours
  Propeller: Sensenich 74DM6S8-0-54 (Fixed Pitch Metal, 2-bladed) 1453 hours

Avionics:

  –

Available in May 2022

Viewing location: AMN, Teuge Airport, The Netherlands
For more information:

  sales@amnetherlands.nl

Sukhoi SU-29 – PH-KAH

This Sukhoi 29, currently registered PH-KAH and named ´Barefoot´, is a Russian two-seat sports aerobatics aircraft and a formidable aerobatic aircraft. In 2007, Ramon Alonso from Spain became world unlimited aerobatic champion flying this aircraft. The PH-KAH with construction number 78-02 was built in 1994. It started flying in the UK and in 2004 went to Spain. In 2011 the aircraft was purchased by Stephen van Dijck in the Netherlands. The aircraft sports a bright yellow and blue livery.

The Su-29 is a incredibly strong two-seater aircraft. The certified wing structural integrity was tested at 25 G. With a big symmetrical wing, large span ailerons and a large rudder it is one of the most successful aerobatic aircraft ever made. Up to 60% of the Su-29 aircraft structure is made of composite materials.

Titanium landing gear. MTOW 1220 kg. New canopy installed in 2014. EASA registered. Complete history including all manuals and log books available.

Aircraft, Engine and Propeller:

  Sukhoi SU-29
  S/N: 78-02, produced in: 1994. Total hours: 1034
  Color: Yellow 
  Engine: Vedeneïev M-14PF (400HP), TTSN: 523 hrs, installed: 22-05-2004
  Propeller: 2,6 meter, 3 bladed MTV-9-B-C/CL-27, TTSO: 34 hrs, overhauled: 16-05-2018

Avionics:

  COM: Garmin GTR225A, Intercom: PM2000; Transponder: Trig TT-21; Mounting provision for Garmin Area 500

Viewing location: AMN, Teuge Airport, The Netherlands
For more information:

  sales@amnetherlands.nl

Tecnam P-2010 – PH-KVL

This beautiful almost new Italian styled P-2010 was built in 2017 by Costruzioni Aeronautiche TECNAM S.p.A., in Capua, Italy. The Tecnam P Twenty-Ten brings together an advanced technology all carbon fibre fuselage with a metal wing to deliver a superlative single engined, four seat aeroplane. Balanced controls. Unsurpassed stability.

Registered as PH-KVL since October 2017. 3 Passenger doors, 1 baggage door and a professional (floor) photo hatch.

Aircraft, Engine and Propeller:

  Costruzioni Aeronautiche TECNAM S.p.A P-2010
  S/N: 044, produced in: 2017. Total hours: 350
  Color: White 
  Engine: Lycoming IO-360-M1A rated at 180hp, TTSN: 350 hrs.
  Propeller: Variable Pitch 2 Blade MT MTV-15-B/193-52, TTSN: 350 hrs.

Avionics:

  Garmin G1000 Nxi, G1000 Nxi. Integrated Flight Deck System, includes: GDU 1050 10-inch PFD, GDU 1050 10-inches MFD, Dual GEA 71 Engine & Airframe unit, Dual GIA 63WAAS, Com/nav/GPS/GS/Loc. GMA1347 Digital audio system. GMU44 Magnetometer, GDC72 Air data computer, GRS79 AHRS, GTP59 OAT, GTX345R Mode S transponder (ADS-B In and OUT). Complete IFR package with AP/VP Prop/ADF.

Viewing location: SOLD
For more information:

  sales@amnetherlands.nl