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EMBRAER Phenom 300

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E55P
Aircraft
Name Phenom 300
Manufacturer EMBRAER
Body Narrow
Wing Fixed Wing
Position Low wing (winglets)
Tail T-tail
WTC Medium
APC B
Type code L2J
Engine Jet
Engine count Multi
Position Both sides of rear fuselage
Landing gear Tricycle retractable
Mass group 3


Manufacturered as:

EMBRAER EMB-505 Phenom 300
EMBRAER Phenom 300


EMBRAER Phenom 300

EMBRAER Phenom 300

Description

The Embraer EMB-505 Phenom 300 is a business jet aircraft.

Technical Data

Wing span 15.9 m52.165 ft
Length 15.6 m51.181 ft
Height 5.1 m16.732 ft
Powerplant 2 x Pratt & Whitney Canada PW535E turbofans, 14.2 kN each.
Engine model Pratt & Whitney Canada PW500

Performance Data

Take-Off Initial Climb
(to 5000 ft)
Initial Climb
(to FL150)
Initial Climb
(to FL240)
MACH Climb Cruise Initial Descent
(to FL240)
Descent
(to FL100)
Descent (FL100
& below)
Approach
V2 (IAS) kts IAS kts IAS kts IAS kts MACH TAS 450 kts MACH IAS kts IAS kts Vapp (IAS) kts
Distance 1130 m ROC ft/min ROC ft/min ROC ft/min ROC ft/min MACH 0.78 ROD ft/min ROD ft/min MCS kts Distance 799 m
MTOW 79507,950 kg
7.95 tonnes
kg
Ceiling FL450 ROD ft/min APC B
WTC M Range 18001,800 nm
3,333,600 m
3,333.6 km
10,937,007.882 ft
NM

Accidents & Serious Incidents involving E55P

  • E55P, Blackbushe UK, 2015 (On 31 July 2015 a Saudi-operated Embraer Phenom on a private flight continued an unstabilised day visual approach to Blackbushe in benign weather conditions. The aircraft touched down with excess speed with almost 70% of the available landing distance behind the aircraft. It overran and was destroyed by impact damage and fire and all occupants died. The Investigation concluded that the combination of factors which created a very high workload for the pilot "may have saturated his mental capacity, impeding his ability to handle new information and adapt his mental model" leading to his continuation of a highly unstable approach.)
  • E55P, St Gallen-Altenrhein Switzerland, 2012 (On 6 August 2012 an Embraer Phenom 300 initiated a late go-around from an unstabilised ILS/DME approach at St. Gallen-Altenrhein. A second approach was immediately flown with a flap fault which had occurred during the first one and was also unstabilised with touchdown on a wet runway occurring at excessive speed. The aircraft could not be stopped before an overrun occurred during which a collision with a bus on the public road beyond the aerodrome perimeter was narrowly avoided. The aircraft was badly damaged but the occupants were uninjured. The outcome was attributed to the actions and inactions of the crew.)