Schweizer 2-33, Руководство по эксплуатации

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A-CR-CCP-402/MB-001 SCHWEIZER 2-33 AOIs
1-1
SECTION 1 – AIRCRAFT & SYSTEMS DESCRIPTION
GENERAL DESCRIPTION
1. The 2-33 is a conventional two-place tandem intermediate training glider manufactured by
Schweizer Aircraft Corporation, Elmira, New York. Its construction is all metal with a fabric cover
on the fuselage and the horizontal tail surfaces. It has a one-piece canopy for increased visibility.
The wings are tapered in the outboard section and have spoilers/dive brakes incorporated.
2. There are two variants of the 2-33. The 2-33A included a larger rudder with an
aerodynamic balance horn. The 2-33AK came as a kit that was completed by the buyer.
(above para added 2016)
3. As all aircraft have been standardized to a large extent, no differentiation will be made
between models in this manual and 2-33 will be used to denote all variants.
(above para added 2016)
SPECIFICATIONS
Length 25 ft 9 in
Span 51 ft 0 in
Height 9 ft 3 ½ in
Wing Area 219.48 sq ft
Aspect Ratio 11.85 : 1
Tire Pressures Hydraulic Brakes: 28-30 psi Mechanical Brakes : 15 psi
Figure 1-1 Specifications
(chart updated 2016)
SEATING CONFIGURATION
4. The ACGP 2-33 Glider is a tandem two seat configuration enabling solo or dual flight.
5. Solo flight is conducted from the front seat only
(above para added 2016)
6. Some pilots may require seat spacers and cushions to ensure the required sight line
over the nose. See Section 3 NORMAL PROCEDURES - USE OF SEAT SPACERS AND
SEAT CUSHIONS for proper installation and information on acceptable condition.
(above para added 2016)