Planes

2013 Embraer Phenom 300

2013 Embraer Phenom 300

 

The Embraer EMB-505 Phenom 300 is a single pilot certified light business jet developed by the Brazilian aerospace manufacturer Embraer. It can carry up to 11 occupants.[4]

 

Embraer began designing the Phenom 300 after finding that potential customers of the Phenom 100 would also like a bigger aircraft. It was a new design with the aim of allowing operation to smaller airports such as London City and Telluride Regional Airport.

It first flew on 29 April 2008,[3] and received its type certification on 3 December 2009.[5] On 29 December 2009 Embraer delivered the first Phenom 300 to Executive Flight Services at the company’s headquarters at São José dos Campos, Brazil.[6]

On 31 January 2020, Embraer announced significant upgrades to the Phenom 300, with maximum speed increased from Mach 0.78 to 0.80 (446 to 464 kn, 826 to 859 km/h), and range increased from 1,992 to 2,010 nmi (3,689 to 3,723 km). Rated engine thrust was increased from 3,360 to 3,478 lbf (14.95 to 15.47 kN) on upgraded PW535E1 turbofans.[7] In 2022, its equipped price was $10.295M.[8]

 

The Phenom 300 is a twin-engined cantilever monoplane with low-positioned, swept wings. It has a horizontal stabiliser in a T-tail configuration and a retractable tricycle landing gear. It has two rear-pylon-mounted Pratt & Whitney Canada PW535E turbofan engines. The enclosed cabin has room for nine passengers and a two-pilot crew; during single-pilot operation an additional passenger can be carried. Access to the cockpit and cabin is via an airstair on the left-hand side.

Its structural life is 28,000 flight cycles or 35,000 hours. It is built of 18% composite materials; it has winglets, but not thrust reversers.[3] The Phenom 300 has single-point refueling and an externally serviced private rear lavatory.[5]

General characteristics

  • Crew: 1 or 2 pilots
  • Capacity: 6 passengers (standard configuration) + 1 in cockpit; maximum of 10 incl.[40] 1 in cockpit and 1 on belted toilet)
  • Length: 15.64 m (51 ft 4 in)
  • Wingspan: 15.91 m (52 ft 2 in)
  • Height: 5.1 m (16 ft 9 in)
  • Max takeoff weight: 8,150 kg (17,968 lb)
  • Fuel capacity: 2,428kg[5]
  • Pressurization: 9.4 psi (0.65 bar)[41]
  • Cabin height: 4.9 ft (1.49 m)[5]
  • Cabin width: 5.1 ft (1.55 m)[42]
  • Cabin length: 5.23 m (17.2 ft)[5]
  • Powerplant: 2 × PW535E1[7] turbofans, 15.471 kN (3,478 lbf) thrust each

Performance

  • Maximum speed: 859 km/h (534 mph, 464 kn)
  • Range: 3,723 km (2,313 mi, 2,010 nmi) with IFR reserves, 5 occupants
  • Service ceiling: 13,716 m (45,000 ft)
  • Wing loading: 286 kg/m2 (59 lb/sq ft)
  • Fuel burn: 346 kg/h at 364 kn, 456 kg/h at 431 kn (at FL410)[5]
  • Take-off distance: 978 m (3,209 ft) MTOW, SL, ISA[38]
  • Landing distance: 674 m (2,212 ft) 4 occupants at 200 lb each, NBAA IFR reserves, SL, ISA[38]

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