7 photos from Wikimedia Commons · credits & licences
- 1. G-FRZN (8512083613): Mark Harkin· CC BY 2.0
- 2. AW109 Grand (ONT) 2: Sky Larson· CC BY-SA 2.0
- 3. Agusta A-109S Grand RA-01903 (4702565463): Aleksandr Markin· CC BY-SA 2.0
- 4. Agusta A109S Grand, Mexico - Government JP7316860: André Du-pont (Mexico Air Spotters)· GFDL 1.2
- 5. Agusta A109S Grand, Private JP7221910: Aldo Bidini· GFDL 1.2
- 6. Agusta A109S Grand, Private JP7224821: Aldo Bidini· GFDL 1.2
- 7. Private, I-EASV, Agusta A-109S Grand (17181433065): Anna Zvereva from Tallinn, Estonia· CC BY-SA 2.0
what is it?
The AgustaWestland AW109S Grand is a lightweight, twin-engine, eight-seat multi-purpose helicopter built by the Italian manufacturer AgustaWestland. This rotorcraft has been developed from AgustaWestland AW109 by lengthening the cabin and main rotor blades with different tip design. The Agusta Grand is fitted with two Pratt & Whitney Canada PW207C engines whereas its predecessor AW109E has two Pratt & Whitney Canada PW206C engines.
How to recognise it: 2 turboshaft engines · 10.8 m main rotor
base stats
Bars compare against all aircraft: 3,500 km/h, 20,000 km, 850 seats; size and number built on a log scale up to 640 t (An-225) and 45,000 built (Cessna 172).
fun facts
- Top speed is 2.4× a car on the Dutch motorway (130 km/h).
- Rotor of 10.8 m: about 2 cars parked nose to tail.
turboshaft: A turbine that turns a shaft, usually a helicopter rotor.
spec sheet
- first flight
- —
- introduced
- 2005
- status
- in production
- number built
- —
- role
- sar/utility helicopter
- makers
- AgustaWestland
- engines
- 2× Pratt & Whitney Canada PW207C
- crew
- 1
- passengers
- 7
- length
- 13 m
- rotor diameter
- 10.8 m
- height
- 3.4 m
- max take-off weight
- 3,175 kg
- top speed
- 311 km/h
- cruise speed
- 289 km/h
- range
- —
- ceiling
- 4,938 m
Specs are for the version in the Wikipedia article's specification section. Blank means the sources don't say.
family
Sources: Wikidata Q21062070, Wikipedia: AgustaWestland AW109S Grand (CC BY-SA 4.0).Updated 2026-10-24.
