roll into a bank and the up wing will suddenly read full and the low wing will read empty, it's just a limitation of the float type sender.
Usually it's the latter.That said, I've never seen this "bouncing" you're talking about. Does it happen all the time? Or does it sometimes read normally and sometimes bounce?
That part of the preflight seriously pisses me off since I started flying the newer Skyhawks.Anything that has that many fuel sumps can't be safe.
That said, I've never seen this "bouncing" you're talking about. Does it happen all the time? Or does it sometimes read normally and sometimes bounce?
That part of the preflight seriously pisses me off since I started flying the newer Skyhawks.
I wish we had cool stuff to rent around here. There isn't really anything other than the run of the mill Cessnas and Pipers, unless you want to pay an arm and a leg for a Cirrus or a Diamond.That's why I started flying our club's Tiger insetad of the 172S models, even though it meant another checkout. Has the same 180hp, but it is a hell of a lot easier to pre-flight and feels more stable in the air. It is also equipped with a 430W, so the fact that the glide slope at my field has been inop for the past 3 months hasn't mattered to me.
The gauges are not required to be calibrated to read that quantity. Sorry, but they just aren't. Check the reg again. You'll see it clearly if you can comprehend the sentence. My point remains, the only time you can be sure that gauge is accurate is when it reads zero and you're out of usable fuel. At that point, if it is inaccurate, it needs to be written up and the airplane is unairworthy.It also requires that they indicate the amount of usable fuel in flight, which you claim is not a requirement. I don't know why you think an English sentence doesn't mean exactly what it says.
Unless the author is going to re-write the regulation, his opinion is just that...and you know what they say about opinions.This author also thinks your position is greatly mistaken:
http://www.av8n.com/fly/fuel-gauges.htm
He offers nothing that would persuade you otherwise, but does provide some suggestions about reasonable tolerances.
lots of argument over this. Bottom line, it should be in the ball park, however, "In flight" is pretty vague.
In level flight with 1/2 tanks the gauges should read about 1/2, roll into a bank and the up wing will suddenly read full and the low wing will read empty, it's just a limitation of the float type sender.
Are they accurately indicating the quantity in each tank? nope.
Is it illegal? nope.
Am I gonna pin my hopes on a fuel gauge... absolutely not.
Am I gonna land when one reads low or empty unexpectedly? You bet.
That said, I've never seen this "bouncing" you're talking about. Does it happen all the time? Or does it sometimes read normally and sometimes bounce?
because the indicator is not required to be calibrated to read the usable fuel quantity in
You don't seem to understand the concept of calibration, which is why you're misreading the reg. Anyway, are you going to ignore the evidence I supplied from AC 29.2C, Certification of Transport Category Rotorcraft, which shows you that your interpretation is incorrect?
Surely you aren't going to attempt to argue that fixed wing aircraft and rotorcraft are certificated under the same regulations, are you?
Do you have an identical AC or a link to one for airplanes? An AC that specifies part 29 does not apply to part 23 or 25. You are grasping at straws. Again, rotorcraft regulations to not apply to fixed wing aircraft unless noted.No, but the regulation is the same. This is from 14 CFR 29.1337b) Fuel quantity indicator. There must be means to indicate to the flight crew members the quantity, in gallons or equivalent units, of usable fuel in each tank during flight. In addition—
(1) Each fuel quantity indicator must be calibrated to read “zero” during level flight when the quantity of fuel remaining in the tank is equal to the unusable fuel supply determined under §29.959;
Do you have an identical AC or a link to one for airplanes? An AC that specifies part 29 does not apply to part 23 or 25. You are grasping at straws.
It isn't the "identical" regulation. The regulation(s) in question are in parts 23 and 25, not 29. It's as simple as that. You can try to spin it anyway you like, but that doesn't affect the fact that the fuel quantity indicator isn't required to be calibrated except to read zero with no usable fuel left in the tank.I'm showing you how the FAA interprets the requirement. It's the identical regulation. If you claim that "calibration" in identical regulations in different parts has different meanings, then you're really being unreasonable.