Rotax 918 iS EP | EAB MTOW 2,600 lbs | CG 15%–28% MAC
Enter actual weights for this flight.
Loaded point ● and end-of-flight point ○ must stay inside the green box.
Enter once per aircraft at time of weighing. Empty weight & CG auto-populate above. Defaults: ANG-01 s/n 005, weighed 08 Jun 2022, datum = propeller nose.
When CG is between 7% and 15% MAC, maintain approximately 10% throttle throughout the flare and touchdown. Per POH this range is for experienced pilots ONLY — begin with 66 lbs ballast in the aft luggage compartment, fly 5–10 hours, then reduce ballast gradually to build familiarity.
Extension: max 80 KTAS — above 80 KTAS the nose gear may fail to lock down; if used as a speed brake above 80 KTAS, retract and re-extend below 80 KTAS to ensure nose-gear lock. Retraction: max 100 KTAS.
Best glide speed (Vbg) = 92 KTAS. Use for maximum glide range in engine-out scenarios.
Structural maximum 300 lbs; recommended operational maximum 120 lbs. All combinations must stay within both weight and CG limits. Combinations "1P+3L+b" and "2P+3L+b" are PROHIBITED — outside the CG envelope.
W&B Act TW-0300-00290175-000 · ANG-01 s/n 005 · Weighed 08 Jun 2022.
Reference tool only — the pilot in command is responsible for verifying loading against the approved POH/aircraft flight manual before every flight.