maximum takeoff weight

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maximum takeoff weight

The maximum gross weight, as a result of design or operational limitations, at which an aircraft is permitted to takeoff.
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At the same airplane's Normal-category max takeoff weight of 2550 pounds, wing loading and power loading decrease proportionately by approximately 14 percent.
" Martin said the Bolkow BO-105 it replaced last November was a "fineCrew: 1 pilot Capacity: Seven passengers or two crew and two patients (air ambulance variant) Length: 39ft 11in Height: 11ft 6in Empty weight: 3,208lb Max takeoff weight: 6,415lb Engine: 2 x Turbomeca Arrius 2B2 turboshaft engines or 2 x Pratt & Whitney Canada PW206B turboshaft engines Main rotor diameter: 33ft 6in Main rotor area: 879 sq ft Cruising speed: 158mph Never exceed speed: 178mph Range: 395 miles EUROCOPTER EC135: THE FACTS CONCERT TICKETS Tickets for a grand concert at Caernarfon Castle climaxing in a marathon walk across Wales by 15 celebrities led by opera singer Rhys Meirion are selling fast.
"Icon says the A5 requires a max takeoff weight of 1,680 pounds because of structural changes that will make the airplane spin resistant under Part 23 certification standards," writes blogger Stephen Pope.
A320 technical specifications overall length [m] 37.57 geometric wingspan [m] 34.10 wing area [[m.sup.2]] 122 aspect ratio 9.39 wing sweep (25% chord) [deg] 25 height [m] 11.76 max cabin width [m] 3.70 fuselage diameter [m] 3.95 thickness-to-chord ratio 0.153 engines (2x) CFM International CFM56-5 series max operating Mach number 0.82 max lift coefficient at takeoff 2.56 max takeoff weight tonnes 73.50 max landing weight tonnes 64.50 max zero-fuel weight [tonnes] 61 max fuel canacity [1] 24210 Tab.
Here are the numbers: LMC-130J SAIC-30M Max Takeoff Weight (kg) 74,545 79,545 106.71% 75,545 Takeoff Roll (kg) 945 577 61.06% 661,363 kg Landing Roll (m) 497 337 67.81% Max Range w/ Max Fuel (km) 6,852 8,017 117.00% Max Range /Payload (km) 4,407 698 158.54% Differential Max Takeoff Weight (kg) 75,545 Takeoff Roll (kg) -368 661,363 kg Landing Roll (m) -160 Max Range w/ Max Fuel (km) 1,165 Max Range /Payload (km) 2,580
It's common in airplanes above the size of most single-engine retractables to have a max takeoff weight higher than its max landing weight.
That loading assumes a 450-kg (990 pounds) max takeoff weight. Hansen will aim for +6 and -3Gs for the version it will sell, perhaps with a weight limit.
Max takeoff weight for the Mark II is the same as the Mark I, 3600 pounds, with an advertised useful payload with full fuel (88 gallons usable) of 1085 pounds.