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Cessna 152 - Regn: 9M-CES

Although not a Team Arrow aircraft, syndicate member Graham procured this aircraft in 2010  and had it delivered into Malaysia in May of the same year. Graham is sole owner of this aircraft, now registed in Malaysia as 9M-CES.

Team Arrow members, and other pilots, have flown this delightful aircraft with its easy and forgiving nature.

First delivered in 1977 as the 1978 model year, the 152 was a modernisation of the proven Cessna 150 design. The 152 was intended to compete with the new Beechcraft Skipper and Piper Tomahawk, both of which were introduced the same year. Additional design goals were to improve useful load through a gross weight increase to 1670 lbs (757 kg), decrease internal and external noise levels and run better on the then newly introduced 100LL fuel.

As with the 150, the great majority of 152s were built at the Cessna factory in Wichita, Kansas. A number of aircraft were also built by Reims Aviation of France and given the designation F152/FA152.

Production of the 152 was ended in 1985 when Cessna ended production of all of their light aircraft; by that time, a total of 7,584 examples of the 152, including A152 and FA152 Aerobat aerobatic variants, had been built worldwide.

Spec Details

General

  • Cessna 152
  • Reg No: N46812
  • Ser. No: 15283110
  • Total Time: 8377
  • Engine: 372

Avionics

  • Avionics Master Switch
  • Cessna RT-385A Digital Nav/Com
  • Mode C Transponder
  • Flightcom 403MC Intercom
  • VOR indicator
  • New 406Mhz ELT with remote arming
     

Airframe

  • Fully Refurbished
  • New Paint Brown and Cream in 2007
  • New Two tone Leather interior, carpets, seat belts, Plastic in 2007
  • New Glass
  • Air Scoops on each side windows
  • Rudder Stop kit
  • Electric Flaps
  • Tail Beacon
     

History

  • Private owner for many years after use in various flight schools.
  • Owner fully overhauled the aircraft in 2007 inside and out to “as new” condition.
  • Was always hangered since overhaul.  
     
Images of 9M-CES

 

Misc Notes

The 152's airframe is an all metal construction. It is primarily aluminium 2024-T3 alloy, although some components such as wing tips and fairings are made from glass-reinforced plastic. The fuselage is a semi-monocoque structure: it has vertical bulkheads and frames joined by longerons which run the length of the fuselage. The metal skin of the aircraft is riveted, which allows loads to be spread out over the structure. The wings are of a strut-braced design and have a 1 degree dihedral angle. The tapered (outboard) portion of each wing has one degree of washout (the chord of the tip section has one degree lower angle of attack than the chord at the end of the constant-width section). This allows greater aileron effectiveness during a stall, although it is much less than the 3 degrees used in Cessna 172 wings.

The Cessna 152 is equipped with differential ailerons that move through 20 degrees upwards and 15 degrees downwards. It has modified Fowler (slotted, aft-traveling) flaps which are electrically operated and deploy to a maximum of 30 degrees. The rudder can move 23 degrees to either side and is fitted with a ground adjustable trim tab. The elevators move up through 25 degrees and down through 18 degrees. An adjustable trim tab is installed in the right elevator and is controlled by a small wheel in the center of the control console. The trim tab moves 10 degrees up and 20 degrees down relative to the elevator chordline.

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