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B77W

From SKYbrary Wiki
Aircraft
Name 777-300ER
Manufacturer BOEING
Body Wide
Wing Fixed Wing
Position Low wing
Tail Regular tail, mid set
WTC Heavy
APC D
Type code L2J
RFF Category 9
Engine Jet
Engine count Multi
Position Underwing mounted
Landing gear Tricycle retractable
Mass group 5


Manufacturered as:

Boeing 777-300ER


BOEING 777-300ER

BOEING 777-300ER BOEING 777-300ER 3D

Description

The 777-300ER ("ER" for Extended Range) is the B-market version of the 777-300. It features raked and extended wingtips, a new main landing gear, reinforced nose gear, and extra fuel tanks. The -300ER also has a strengthened fuselage, wings, empennage (tail assembly), and engine attachments. The maximum range is 7,930 nm14,686,360 m
14,686.36 km
48,183,595.836 ft
, made possible due to a higher MTOW along with the increased fuel capacity. The -300ER can fly approximately 34% farther than the -300 with a full load of passengers and cargo. B77W is member of the B777 family of aircraft.

Technical Data

Wing span 64.8 m212.598 ft
Length 73.9 m242.454 ft
Height 18.5 m60.696 ft
Powerplant 2 x GE90-115B (511 kN).
Engine model General Electric GE90

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) 168 kts IAS 200 kts IAS 300 kts IAS 300 kts MACH 0.83 TAS 490 kts MACH 0.84 IAS 300 kts IAS 240 kts Vapp (IAS) 149 kts
Distance 3000 m ROC 3000 ft/min ROC 2500 ft/min ROC 2000 ft/min ROC 1500 ft/min MACH 0.84 ROD 1000 ft/min ROD 3000 ft/min MCS 250 kts Distance 1800 m
MTOW 351530351,530 kg
351.53 tonnes
kg
Ceiling FL430 ROD 1500 ft/min APC D
WTC H Range 78257,825 nm
14,491,900 m
14,491.9 km
47,545,603.709 ft
NM

Accidents & Serious Incidents involving B77W

  • A320/B773, Dubai UAE, 2012 (RI HF) (On March 20 2012 a Ural Airlines Airbus A320 failed to taxi as instructed after vacating the landing runway 12L at Dubai and crossed the lit stop bar of an intersection access to runway 12R before stopping just in time to prevent a collision with a Boeing 777-300ER about to pass the intersection at very high speed on take off. Taxi clearance had been correctly given and acknowledged. The aircraft commander had extensive aircraft type experience but the inexperienced First Officer appeared to be undergoing early stage line training with a Safety Pilot present. The Investigation is continuing.)
  • B773, Lagos Nigeria, 2010 (RE HF) (On 11 Jan 2010, an Air France Boeing 777-300ER successfully rejected a night take off from Lagos from significantly above V1 when control column pressure at rotation was perceived as abnormal. The root and secondary causes of the incident were found to be the failure of the Captain to arm the A/T during flight deck preparation and his inappropriate response to this on the take off roll. It was considered that his performance may have being an indirect consequence of his decision to take a 40 minute period of in-seat rest during the 90 minute transit stop at Lagos.)
  • B773, vicinity Toronto Canada, 2012 (LOC AW) (On 28 May 2012 a GE90-powered Air Canada Boeing 777-300ER experienced sudden failure of the right engine during the initial climb after take off. There were no indications of associated engine fire and the failed engine was secured, fuel jettisoned and a return to land made. The Investigation found that the failure was related to a known manufacturing defect which was being controlled by repetitive boroscope inspections, the most recent of which was suspected not to have identified deterioration in the affected part of the engine.)
  • C525 / B773, vicinity London City UK, 2009 (LB LOS AGC HF) (On 27 July 2009, a Cessna 525 departing from London City failed to comply with the initial 3000 ft QNH SID Stop altitude and at 4000 ft QNH in day VMC came into close proximity on an almost reciprocal heading with a Boeing 777-300ER. Actual minimum separation was approximately 0.5nm laterally and estimated at between 100 ft and 200 ft vertically.)