2006年3月22日 · This relates to the leading edge slats of the 767. Originally, SB 57A0039 addressed corrosion and disbond issues, and was specified by AD 93-14-19. 57A0039 called out for an inspection and that was it.

Flaps and Slats: Flap 1 = Slats only; Powered by Centre Hydraulic System; Alternate system uses Right AC/DC. Manoeuvring speeds allow for 25° bank plus 15° of bank safety factor before buffet is encountered. Flap Load Relief: If flap airspeed placard limit is exceeded with Flaps in the 25 or 30 position, flaps automatically retract to 20 ...

The trailing edge flaps and leading edge slats are high lift devices that increase wing lift and decrease stall speed during takeoff, approach, and landing. The flaps and slats are normally operated with hydraulic power from the Centre Hydraulic system. An Alternate system allows the flaps and slats to be operated by electric motors.

2001年1月26日 · On the Boeing 757/767, the flaps/slats deployment are activated by a single action lever and extend/retract automatically. On selection of "1", the leading edge slats are deployed to 50% of their travel as well as a modest extension of the trailing edge flaps.

2018年6月28日 · Airbus inboard slats can come closer to the struts than on Boeing airplanes and don't need an auxiliary device to protect the inboard wing. "Seal" Kruegers are used on the 767, 777 and 787 to fill the "hole" between the outboard end of the inboard slat and the strut. Leading edge sweep also plays a part in this geometrically complicated area.

Boeing 767 Technical Information, based on the pre-dumbed-down version of the Boeing Technical Manual, with additional material from Thomas Cook Airlines

2008年9月18日 · When the flaps are set to the 1 detent, the thrust management computer estimates the slats moving to the flaps 1 position linearly in 5 seconds. There is a microswitch on the thrust lever assembly specifically for this. Flap position is used to generate max speeds in EPR/N1 ref mode, but this seems to be more general.

2006年7月17日 · Any 767 captains or first officers around to shed some light on the subject? One webpage suggests it's possible to get a 767 off the ground with something called "flaps 1". Apparantly, this is no trailing edge flaps, but they do deploy the slats. Can this be done with a fully loaded 767 about to cross the Atlantic, though? Let me know Mario

It describes the primary and secondary flight control systems that provide control around the pitch, roll, and yaw axes. These include the ailerons, rudder, elevator, spoilers, leading edge slats, trailing edge flaps, and stabilizer trim. It also includes diagrams showing the basic components and their function in aircraft control.

2009年8月31日 · On some of my recent flights, I've noticed that most Boeing models have multiple slat settings. 737 (mid-gen and NG ), 757, 767, and 777 all deploy the slats further downward on the leading edge of the wing during landing.