Decreased interference drag, silent aft cabin, a lot of usable cable at the front, enhanced accessible of the engines for maintenance, as well as little piping for fuel and bleeds would be achieved with wing mounted engines. The wing’s life would receive a boost from these engines due to an enhanced ease of bending. However, unfortunately this advantage was unreliable since the two wings performed abysmally during static experiments at 95% of load and thus the engines were redesigned. According to Brady (1999), the fin size was enlarged to facilitate engine out operations against the centerline thrust of the plane, and support the wing-mounted engine.
The deducted surface clearance the wings had to be an important element of the wing. In turn, a short chord was warranted. Engines placed on the wings extended both front and aft of the wing to deduct aerodynamic interference and the parallel top line of the nacelle formed a steam tube over the wing to even reduce drag. As for the low mounted engine, the worries were dismissed because Boeing 720B had engines lower than 737. These engines were operating just fine since they had operated for four years without major difficulties.
For the last wing, the particulars needed good short field performance and economy at high altitude. The final design of wing placed layout had weight saving of 700 kilograms over the equivalent. It also had performance advantages. Furthermore, the familiarity with other Boeings such as 707 added another advantage of wing mounted layout. Advantages of the new plane The heritage of 737 lies in Jack Steiner’s contribution more so in its fuselage cross section. His major contribution was to use a lot of knowledge gathered from the development of 727 to improve on 737.
It gave rise to cost saving in commodity used to assemble the tools. With six bread seats, the plane had one extra seat compared to the BAC 111 and the DC-9 and further had the ability to carry a single standard size cargo container within the main deck, which was an enormous improvement. The new design was more spacious enabling Boeing to adopt standard fittings such as toilet and stairs (Shaw, 1999). The aircrafts spacious nature enabled it to be used as a freighter. This was a duty that the older versions of Boeings were not able to accomplish and the competing aircrafts remained beaten.
Application of off-the-peg make up was fast and affordable during the designing and production. It further facilitated engineers and pilots change and embrace the modern development as they adopted the aircraft. Eventually on February 19th 1965, Boeing announced the 737-100 after Lufthansa had ordered 10 aircrafts. Lufthansa made history as the first foreign airline to fly a US made plane. Testing and additional modifications The first 737 Boeing flight took place on 9 April 1967. This was two years following the project launching.
The assistant direct at Boeing, Brien Wygle was in charge and was co-piloted by Lew Wallick. The flight took two and half hours before the aircraft finally landed in Paine field. Flight testing took place and continued at a very fast pace. The prototype took 47hrs 37 minutes to arrive in the first month. After a while, six aircraft were put in the flight test and endorsement program. These aircrafts flew 1300hrs of flying tests to ascertain the quality of the aircrafts. During the testing period, a lot of alterations were made to the planes.
For instance, the testing of inflatable main landing gear doors seals. Later though, the doors were improved and modernized through the addition of strips (Shaw, 1999). The first 737’s experienced several technical challenges such as clamshell door thrust reversers which failed to work well and a shimmy in its landing gear. The airplane was however impressive from the word go and finally got FAA certification on 15 Dec 1967. The first model, 100, was 94 feet long and had a capacity of 115 passengers.
It had an MTOW of about 42,411 kilograms less compared to 900 series.
Read More