TL-Ultralight TL-2000 StingSport weight & balance
POH figures for the type
- MTOW1320 lb
- MLM1320 lb
- Typical empty805 lb
- Typical empty CG83.4 in
Envelope chart. Takeoff 1070 lb at 83.6 in.
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PEOPLE
BAGGAGE
Baggage compartment, pilot side + Baggage compartment, copilot side + Aft baggage shelf (aft deck) together: max 60 lb
FUEL
EMPTY MASS · YOUR AIRCRAFT
Typical for the type, 805 lb at 83.4 in. Edit it to your aircraft’s own, from its weighing report.
Your own figures, kept in this browser.
Data source
AOI Section 2 p.2-6 (Operational Weight Limits, CG Limits); Section 6 pp.6-7 to 6-10, Figure 6.1 and Figure 6.2 (pages 20-91 of tl-2000-stingsport-lsa__poh__aircraft-operating-instruction-2005-12.pdf) · version type
- No CG envelope chart is printed; only a constant CG range of 80.2 in (22% MAC) to 86.7 in (34% MAC) aft of datum. The envelope given is a rectangle; its lower mass edge (780 lb) is the Standard Empty Weight, not a printed limit.
- Maximum ramp weight 1320 lb (same as MTOW and max landing weight).
- Main fuel: manual states 20.5 USG = 120 lb at 6 lb/USG (20.5 x 6 = 123 lb); usable quantity not stated on these pages. Max main fuel listed as 120 lb.
- Wing aux tanks (6 USG each, 12 USG / 72 lb total) only if installed; arm 80.1 in from Figure 6.2.
- Baggage: 20 lb per side compartment, 20 lb aft shelf, 60 lb total at baggage station; all three locations use the single baggage arm 117.0 in.
- Typical empty weight example (Figure 6.1): 805 lb at 83.4 in; the text refers to an EWCG of 80.83 in (Figure 6.3) - inconsistent, use your aircraft's actual weighing record. Standard Empty Weight printed as 780 lb (no arm given).
- Instrument panel arm 59.5 in is given for equipment changes, not a loading station.
- 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.
| Station | Load | Mass lb | Arm in | Moment lb·in/1000 |
|---|---|---|---|---|
| Empty aircraft | 805 | 83.4 | 67.1 | |
| Pilot | 175 | 90.1 | 15.8 | |
| Copilot / Passenger | 0 | 90.1 | 0.0 | |
| Baggage compartment, pilot side | 0 | 117.0 | 0.0 | |
| Baggage compartment, copilot side | 0 | 117.0 | 0.0 | |
| Aft baggage shelf (aft deck) | 0 | 117.0 | 0.0 | |
| Main fuel tank | 10 USG | 60 | 68.4 | 4.1 |
| Wing aux tanks (6 USG each side, if installed) | 5 USG | 30 | 80.1 | 2.4 |
| Zero fuel | 980 | 84.6 | 82.9 | |
| Takeoff | 1070 | 83.6 | 89.4 |
AOI Section 2 p.2-6 (Operational Weight Limits, CG Limits); Section 6 pp.6-7 to 6-10, Figure 6.1 and Figure 6.2 (pages 20-91 of tl-2000-stingsport-lsa__poh__aircraft-operating-instruction-2005-12.pdf). For reference only; the aircraft’s flight manual and weighing report are the final authority. https://zulucheck.com/wb/type/tl-stingsport/
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