AMT-200S Maint Manual

AMT 200S 

MAINTENANCE MANUAL 200-25

MAINTENANCE MANUAL AMT 200S

SECTION:1

SECTION 1 - DESCRIPTIONS, SYSTEMS, RIGGINGS AND PLACARDS 1. Mot Motorg orglid lider er Cha Charact racteri eristic stics s 1.1

Basic Dimensions

Wing span Wing span with winglets (optional) Wing span (wings folded) Length Maximum height 1.2

Wings

Wing surface (area) Dihedral Profile  Angle of incidenc incidence e Wing torsion 1.3

30% 10.24 ft (3.12 m) 7.32 Sqft (0.68 m 2)

Airbrakes

Position  Airbrake  Airbrak e span span Type

1.5

201.29 Sqft (18.70 m 2) 2° 30' Naca 64 3618 2° -2°

Ailerons

Percent to wing chord (depth)  Aileron span  Aileron surface (area) 1.4

57.32 ft (17.47 m) 57.97 ft (17.67 m) 33.30 ft (10.15 m) 26.50 ft (8.08 m) 6.33 ft (1.93 m)

at 45% of wing chord 4.76 ft (1.45 m) Schempp hirth on upper wing surface

Horizontal Stabilizer 

Horiz. stabilizer span Horiz. stabilizer surface (area) Elevator surface Horiz. stabilizer - angle of incidence

12.07 ft (3.68 m) 31.21 Sqft (2.90 m 2) 10.23 Sqft (0.95 m2) -1°

Page 1.1 MM - 200-25

 August 10, 2004 - Rev. 8

MAINTENANCE MANUAL AMT 200S

1.6

SECTION:1

Vertical Empennage

22.93 Sqft (2.13m 2) 7.42 Sqft (0.69m 2)

Vertical empennage surface (area) Rudder surface (area) 1.7

Landing Gear  

Conventional: Two main gears with a tail wheel coupled at the rudder. For ground operation the tail wheel disengages automaticaly when the minimum curve radius is reached. Main Mai n landi landing ng gea gearr shock shock abso absorbe rber: r: Pressur Pressure e 130 psi ( 9,14 kg/ kg/cm cm 2) >0°C Pressure 145 psi (10,19 kg/cm 2)