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weight and performance calculations for the Boeing 737-700 Transavia Boeing 737-7K2(WL) PH-XRY c/n 33463 taking off at Schiphol airport, February 2024 © bvdz. This aircraft was delivered in March 2003.

Boeing 737-700

role : medium-range jet airliner

importance : ****

first flight : February 1997 operational : October 1997 (Southwest)

country : United States of America

design :

production : 93 aircraft at Renton (Washington)

general information :

The -700 is the first of the next-generation 737s. It is based on the 737-300 and was also initially referred to as -300X. The -700 is 23cm longer than the -300. It can fly non-stop over the US.

primary users : Transavia

Accommodation:

flight crew : 2 cabin crew : 5

passengers : seating for 128 in two class : 12 business class and 116 economy class seats

( 32 -in pitch) high density seating for 149 passengers

engine : 2 GE-Snecma CFM56-7B20 turbofan engines of 88.96 [KN] thrust

dimensions :

wingspan : 34.30 [m], length overall: 33.60 [m], height : 12.50 [m]

wing area : 125 [m^2] fuselage exterior width : 3.76 [m]

weights :

operating empty weight : 37640 [kg] max. structural payload : 17010 [kg]

Zero Fuel weight (ZFW) : 54650 [kg] max. landing weight (MLW) : 58060 [kg]

max. take-off weight : 69400 [kg] weight fuel : 20828 [kg] usable fuel

performance :

Max. operating Mach number (Mmo) : 0.82 [Mach] (920 [km/hr]) at 7160 [m]

critical Mach speed : 0.78 [Mach]

max. cruising speed : 880 [km/hr] (Mach 0.81 ) at 9150 [m] (36 [%] power)

economic cruising speed : 829 [km/hr] (Mach 0.76 ) at 9150 [m]

service ceiling : 12500 [m]

range with max fuel and MTOW : 5436 [km] (ATA domestic fuel reserves - 370.0 [km]

alternate)

range with max fuel : 5806 [km] (no reserves)

endurance : 7.00 [hours]

description :

cantilever low-wing monoplane with retractable landing gear with nose wheel

Wings : two main spar fail-safe wing structure

with double slotted trailing edge flaps with full-span slotted LE flaps (slats) ,with

spoilers airfoil : NACA with supercritical cross-section average thickness/chord ratio :

10.0 [%], sweep angle 3/4 chord: 25.0 [°]

engines attached with pylons to the wing, main landing gear attached to the wings, fuel

tanks in the wings and fuselage