thenewarea51 Posted April 5, 2013 Posted April 5, 2013 Hi, I know HIGE and HOGE charts require aircraft weight, temperature, and pressure altitude to calculate a ceiling. I know pressure altitude is read off of the altimeter when it is set to 29.92, but when I'm flying a helicopter, I can set the altimeter to 29.92 and read the pressure alt, but I can't consult the charts while flying. Does anyone have any tips on doing this on the ground before a flight? Do I just use the standard rule of thumb for temperature, ie. 2 deg C per 1000' and for pressure altitude, calculate the pressure altitude at my departure point and then subtract a 1 inch per 1000' to come up with a figure for an LZ at a higher altitude? Does anyone have any tips or tricks for this? Thank you Quote
Astro Posted April 5, 2013 Posted April 5, 2013 ((29.92 - altimeter setting) x 1000) + field elevation = PA Quote
pilot#476398 Posted April 5, 2013 Posted April 5, 2013 I had to find the pressure altitude at an off airport LZ as part of the performance planning part of my commercial checkride. Just subtract 29.92 from the current setting, multiply that by 1000, and add it to the LZ elevation. That should give you the pressure altitude at your LZ,...I think, it has been a while? Quote
Wally Posted April 6, 2013 Posted April 6, 2013 (edited) Flying into an environment that will limit power (hot and high) I work a graph of limits from RFM graphs, etc., of temps and altitudes where the HOGE weight starts falling. You need HOGE for most helo operations...Example, a grid with 3500' PA and 40 deg. C allows book max gross; 4000' and 35C; 4500' and 30C. Estimate altitude at the LZ (or use the altimeter PA as described), note the OAT., adjust for surface heat, and interpolate between the points. I chart this for every 500' PA in conditions I'm likely to encounter.I won't be higher than 5500 in my service area, and I'll never be lighter than "X" at the LZ, so I don't figure for improbables. This grid is a quick reference at dispatch/departure and prelanding.Then, do a power check! and use whatever rule of thumb necessary to check your calculation- 1% NG/3% TQ is 200 lbs, for instance... The lapse rate is for free air, and local conditions are whatever exist where the aircraft actually is. Local, surface heating will change density altitudes faster than predicted lapses. The last thing you want to do is be stuck where you can't depart, so leave yourself some margin until you know how much slack you need. Edited April 6, 2013 by Wally Quote
Gomer Pylot Posted April 9, 2013 Posted April 9, 2013 You can't know the actual DA without knowing the actual temp and humidity, and that changes constantly. All you can do is use the best information you have available, and give yourself some margin. You can use standard lapse rates if that's all you have, but again, leave some margin because actual conditions will almost certainly be non-standard, one way or another. Quote
avbug Posted April 9, 2013 Posted April 9, 2013 I use the field elevation, or site elevation, and don't get concerned with calculating pressure altitude. The known or approximate elevation is good enough, and more than adequate for making performance calculations. Quote
Dragbrace Posted April 9, 2013 Posted April 9, 2013 Another tool is to note the DA at a known location near your destination. Calculate the elevation differences and plug that into your performance charts. Its not precise as noted above, but will give you a good idea of what you will be facing. Quote
eagle5 Posted April 9, 2013 Posted April 9, 2013 Read it off your transponder. Not all transponders give PA, plus that won't help pre flight calculations much! Quote
thenewarea51 Posted April 9, 2013 Author Posted April 9, 2013 Thanks everyone, does anyone use Skew-T plots at all? Quote
avbug Posted April 10, 2013 Posted April 10, 2013 I used skew-t when flying atmospheric research, because it's what the scientists conducting the program used. It was the focus of our morning briefing. Not so much right now. Quote
Rupert Posted April 12, 2013 Posted April 12, 2013 Pressure altitude, or altitude, changes constantly. Just use the elevation of the LZ as it appears on a map. If a little fuzziness on exact altitude matters that much, it means you don't have enough power reserve. You want to have too much power; not just enough. Go with the documented LZ elevation. Quote
ridethisbike Posted April 18, 2013 Posted April 18, 2013 Pressure altitude, or altitude, changes constantly. Just use the elevation of the LZ as it appears on a map. If a little fuzziness on exact altitude matters that much, it means you don't have enough power reserve. You want to have too much power; not just enough. Go with the documented LZ elevation. That's my take away... Quote
Counterrotate Posted April 28, 2013 Posted April 28, 2013 Pressure altitude, or altitude, changes constantly. Just use the elevation of the LZ as it appears on a map. If a little fuzziness on exact altitude matters that much, it means you don't have enough power reserve. You want to have too much power; not just enough. Go with the documented LZ elevation.+1 Any time you are going to need to "thread the needle" in order to pull something off, you should just stay on the ground. Quote
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