Airplane Factory SLING 4
Pilot Operating Handbook
Page | 5-3
DC-POH-001-X-C-3
Revision : 1.3
5.1
Introduction
The presented data has been computed from actual flight tests, with the
aircraft and engine in good condition and applying average piloting
techniques.
If not stated otherwise, the performance stated in this section is valid for
maximum take-off weight (920 kg / 2028.25 lb) under ISA conditions.
The performance stated in this section is valid for SLING 4 aircraft fitted
with a ROTAX 914 UL 85.76 kW (115 hp) engine and an Airmaster AP332
propeller.
5.2
Take-off and landing distance
Take-off distances:
50 ft ISA (MAUW)
Surface
Take-off run
Take-off distance over 15 m (50 ft) obstacle
Concrete 270 m / 886 ft
450 m / 1476 ft
7000 ft Density altitude (MAUW)
Surface
Take-off run
Take-off distance over 15 m (50 ft) obstacle
Concrete 355 m / 1165 ft
600 m / 1969 ft
Summary of Contents for SLING 4
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