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1951 FOUGA CM-170R Magister Ex-Military

Jet
€ 22,000 $ 24,570
(VAT free)
1951 FOUGA CM-170R Magister Ex-Military 1951 FOUGA CM-170R Magister Ex-Military 1951 FOUGA CM-170R Magister Ex-Military
1951 FOUGA CM-170R Magister Ex-Military 1951 FOUGA CM-170R Magister Ex-Military 1951 FOUGA CM-170R Magister Ex-Military

Aircraft information

Registration: 682
Year of construction: 1951
Total time (TTAF): 4100 TT
Country: Israel
City/Aerodrome: Tel Aviv
Price: € 22,000 / $ 24,570 (VAT free)

General description

AIRCRAFT DESCRIPTION
Type Fouga Magister CM 701 - Upgraded to Improved Fouga
The aircraft is a multi-mission improved trainer. The aircraft has a single mid-wing, two cockpits in tandem, three-point landing gear, V-shaped tail assembly and carries its engines in the wing roots. This aircraft is used for primary, basic and advanced training and can also be used for light bombing and ground support missions.

TECHNICAL DATA
Dimensions
? Overall length 10.05m
? Overall height 2.80m
? Wing span with wingtip tanks 12.15m
? Wing span without wingtip tanks 11.33m
? Wing area 17.30m
Wing
? Leading Edge Sweepback 13°
? Trailing Edge Sweepback 0°
Maximum Take-Off Weight 3,400 kg
Empty Weight 2,157 kg
Maximum Limited Space (at no less than 0.75 mach) 400 Kts
Ceiling Altitude 25,000 ft
Powerplant: TURBOMECA MARBORE VI-P
? Number of Engines 2
? Type Marbore VI
? Maximum Sea Level Static Thrust at Take-Off 480kg (each)
? Fuel Capacity
? Main (front) 255 lit
? Main (AFT) 475 lit
? Tip Tanks 125 lit
? Maximum Fuel Capacity 980 lit

COCKPITS
The cockpits of the IMPROVED FOUGA are designed for greater training effectiveness. These cockpits offer more space, better man-machine interface and an advanced instrument panel providing more pilot comfort, convenience and safety.

ANEMOMETRIC SYSTEM
The anemometric system feeds the following flight instruments:
? Speed and mach indicators
? Altimeters
? Rate-of-climb indicators
The system's improvements include:
? Separate systems for front and rear cockpits (2 pilot tubes, 2 static ports)
? System drainage improvements
? Flexible piping with unlimited service life
? Improvements in pilot heating system reliability

WARNING SYSTEM
This aircraft has a highly effective and sophisticated system to simulate failures from the rear cockpit by audio and visual means. During simulation, the instructor continues to receive real warning, whereas the trainee receives the simulated warnings. Types of warnings include fire, oil pressure, oxygen, generator, fuel pressure, battery and more.

AUTOMATIC STARTING SYSTEM
The automatic starting system of the IMPROVED FOUGA has shows a reduction of abortive starts, part of which are with engine flame out and reduction of unnecessary workload on trainees.

FUEL SYSTEM
The IMPROVED FOUGA fuel system gives better filtration and has more capacity as a result of the following:
? Replacement of pump
? Replacement of filter with pop-out model
? Replacement of tank filling caps including under and overpressure valve in fuselage tank
? Improvements in isolation valve for pressurization
? Replacement of dump and drain valves
? Replacement of piping fittings by wigo-flex type fitting
? New electrical valves or automatic starting

LIQUID OXYGEN (LOX)
The new LOX system installed in the IMPROVED FOUGA is noted for its safety, easy maintenance and reliable operation.

ANTI COLLISION FEATURE
? Red strobe lights with intensity of 140 candle power and a rate of flash - 100 per minute
? Prevention of cockpit illumination by:
? Locating the back lamp properly
? Painting of wing-tip tanks with absorbing paint

ENGINE
The IMPROVED FOUGA is supplied with a Marbore VI-P turbo jet engine. The engine includes:
? A single stage, single intake, centrifugal compressor
? Single stage axial turbine
? Centrifugal fuel injection
? One annular combustion chamber
? Maximum engine revolutions 21,500 RPM
? Idling speed on ground 6,500 RPM
? Maximum sea level static thrust 1,060 lb (480 kg)
? Static thrust at idling RPM 44 lb (20 kg)
? Weight of one engine
(including jet pipe and accessories) 387.2 lb (176 kg)

Airplane time

Date of Delivery 1957, Upgraded at 1981
Total Airframe Hours 4529.33
Total Landings 21370

Avionics

System Qty Model
intercom 2 P801
UHF-DF 1 ARA 48/ARA 50
IFF 1 TPS 660

Remarks

Complete plane with 2 Marbore Engines (improved, Marbore-6)
The plane is dusty, need to be restored

Last updated: 30.08.2015
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Seller

NewView Hardware Solutions
Ran Alon
Zur Moshe, Israel
Phone: +972542100088
Web: http://www.newview-hs.com
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