Sling 4 TSi weight & balance

Data source

POH DC-POH-001-X-F-3.5 Rev 3.5, Section 6.3 (CG arms), 6.4 (CG Envelope), 6.5, 6.7 (example) (pages 39-183 of sling-4-tsi__poh__rev-3-5.pdf) · version type

• The CG envelope is drawn in %MAC. It was converted to arm with arm = 1602 + %MAC × 13.39 mm (LEMAC 1602 mm, MAC 1339 mm).
• The forward and aft limits use the printed values 1847 mm (18% MAC) and 2043 mm (33% MAC). The formula gives 1843 mm and 2044 mm for those points.
• The intermediate vertices (24% MAC at 950 kg and 28% MAC at 490 kg) were computed as 1923 mm and 1977 mm.
• The envelope's lowest mass is 490 kg.
• MAUW is 950 kg (2,094 lb). No separate landing, zero-fuel or ramp mass is printed.
• No seat or baggage maximum loads are given on these pages. Check the placards and the Section 2 limitations.
• Fuel is entered by mass (kg) in the CG form. Tank capacity, usable fuel and fuel density are not given on these pages.
• The typical empty value (500 kg at 1873 mm) is only the manual's example. Use the actual weighing report for your aircraft.
• The 916 iS variant is in the Section 9 supplement and may have different weight and balance data. Verify if applicable.
• Read from the POH by ZuluCheck and checked by a second reading; verify against your own manual.

For reference only. The aircraft’s approved flight manual and weighing report are the final authority.