Leonardo AW119 Kx / MKII Koala

A119 · Helicopter · model reference data — adjust with your weighing record

Leonardo AW119 Kx / MKII Koala—

	kg	CG
TO	—	—	—
LD	—	—	—
ZF	—	—	—

Result · envelope

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	Weight kg	CG in
TO	—	—	—
LD	—	—	—
ZF	—	—	—

MAX GROSS 2,850 kg (6,283 lb)

TO takeoff (fuel loaded) · LD landing (after burn) · ZF zero fuel.

X axis: CG (in) · Y: weight (kg) · red line = MTOW.

AW119 — three limits this profile does not compute for you. (1) LATERAL CG is a certified limit on this type (-2.4 to +2.4 in, tightening to ±2.1 in at 6283 lb): check it on RFM Fig. 1-5. (2) BAGGAGE is modelled as zone 1 (192.1 in). Loading further aft (zones 2-5, up to 253.2 in) adds moment: total baggage is limited to 150 kg AND 63,708 lb-in — see RFM Table 6-9. (3) FUEL FLOW 163 L/h is derived from Leonardo published endurance at max-range speed; at cruise it is higher. Use your own figures for fuel planning.

Load

Pilot 0 kg

Front passenger 0 kg

Mid row left (aft-facing) 0 kg

Mid row center (aft-facing) 0 kg

Mid row right (aft-facing) 0 kg

Rear row left 0 kg

Rear row center 0 kg

Rear row right 0 kg

Baggage zone 1 0 kg

Fuel (2 main tanks) 0 L / 595

Flight time 35 min

Total: — LEndurance: —Reserve: —

163 L/h

⚠ Empty weight / CG — model placeholder, tap to set yours

Empty (lb)

Empty CG (in)

AW119: your empty weight already includes engine and transmission oil, hydraulic fluid, fixed ballast and unusable fuel (RFM Section 6). Do not add them again.

These are generic model reference figures and will differ from your specific airframe (equipment, avionics, paint). Enter the empty weight and CG from your aircraft's actual weighing record (lb/in, per the POH) before relying on any result — saved on this device.

Performance · hover

Elevation 2300 ft

QNH 1013 hPa · 29.92 inHg

OAT 20 °C

Press. Alt: — ftDA: — ft

MAX GROSS · IGE

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MAX GROSS · OGE

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Approximate ceilings from MTOW spec (IGE 11,000 / OGE 7,300 ft). POH §5 hover charts govern.