Boeing 737 Elevator. The elevator on a 737 is much smaller than the horizontal stabilizer If the elevator suddenly fell off all pitch control using the yoke would be lost The aircraft would still be able to fly however pitch control would need to be done using the electric trim switch on the yoke.
There are five sets of pitot tubes on the 737 organized into two groups the pitot tubes on the nose are used for airspeed measurements independent for the pilot and copilot and one as a backup There are two pitot tubes on the tail that are for the “.
Freewing AL37 (aka Boeing 737 Max) view from elevator
Supermarine and North American partially solved their pitch stability problems with bobweights in the elevator circuits This might be a viable and inexpensive 737 MAX solution We also know that Whitcomb winglets and Spillman sails increase a wing’s effective span with little or no effect on structure weight plus a useful decrease in drag.
Imagine you were happily flying a Boeing 737 when suddenly
PDF fileDATA for BOEING 737 TYPE CONTROL YOKE Width at Top of Yoke 345 mm Width at Bottom of Yoke 260 mm Height of Yoke 195 mm Diameter of Yoke Handle or Thinkness of Yoke 32 36 mm Position of AutoPilot Disconnect 80 mm above lower yoke Length of AutoPilot Disconnect Assemble 60 mm Width of the ClipBoard at the Top 95 mm Width of the ClipBoard at the.
B737 NG
The US FAA issued an Emergency airworthiness directive (AD) 20100651 to all owners and operators of Boeing 737600 700 700C 800 900 and 900ER series airplanes The FAA received a report of failure of the aft attach lugs on the left elevator tab control mechanism which resulted in severe elevator vibration.
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In normal maneuvering the pilot displaces the elevator by applying an elevator control force The pilot then trims the stabilizer by driving it to a new position to remove the elevator control force This new stabilizer position is faired with the elevator If they are not faired (one is down and the other is up) one cancels out the other.