Asking because of Air India 171. Pilots and their unions are objecting to it because of “privacy” reasons. What do you think about it?
Asking because of Air India 171. Pilots and their unions are objecting to it because of “privacy” reasons. What do you think about it?
Pretty easy fix? There might be an emergency checklist somewhere that requires you to shut off engines. Testing the fuel cut off is part of the pre flight, at least for small airplanes. I see no reason why it wouldn’t be for larger airplanes.
Unless you’re type rated in the airframe or work for Boeing, I would refrain from offering simple fixes.
Also radar altitude? Do they not use pitot tubes for altitude?
Ohhhhhhh buddy you activated my trap card. I happen to have multiple type ratings, and I still consider myself far from an expert. However I do still hold a CFI so I’m going to try to teach you some stuff!
Every airplane that I’ve been required to have a type rating for has a radar altimeter. A lot of systems already use that information, from auto landings, to caution message inhibits, down to GLD spoilers. Watch any “landing an airliner” YouTube videos, I feel pretty safe in saying generally you will hear an audible “50, 40, 30, 20, 10”, that information is usually derived from the radar altimeter.
While you are correct, there are emergency checklists that do require engine shutdowns, there are very few that would require that to be done weight off wheels and under 1000ft AGL. Off the top of my head, the ditching (landing in water) checklist would, but that could be tied to a ditching switch, if equipped, which since I don’t have a 787 type, I don’t know if it does, but I would guess it probably does.
Seeing as you know what a pitot tube is I’m going to assume you at least have some interest in flying. The pitot tube is used for airspeed, what you’re probably thinking of is the other part of that system called the static port. That’s used for things like altitude and vertical speed.
Circling back to my “simple fix”, my current airframe has triple redundant hydraulics with dual redundant pumps for each. So for something that has that much redundancy, don’t you think something as critical as an engine should require more than one switch to shutdown, at least at an altitude of high vulnerability? Just food for thought.
Lmao didn’t know we were playing yugioh, but I will defer to the CFI over my checks credentials former student pilot knowledge.
Pitot tubes measure a plane’s airspeed. It’s static ports that measure barometric pressure. radar altitude directly measures the distance between the ground and the plane using radio waves is more useful on final approach