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| | #1 |
| Junior Member |
Is there a quick way to figure what the pivotal altitude will be for a specific groundspeed? edit: I accidentally put this here, it was meant for the CFI section. |
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| | #2 |
| Old Skool |
IDK about GS but do you know the formula for TAS?
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| | #3 |
| Junior Member | |
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| | #4 |
| Senior Member |
There's no requirement to figure it out in flight. If you're thinking about this for a checkride just calculate it before the oral based on the current winds aloft.
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| | #5 | |
| Moderator Join Date: May 2003 Location: GRR
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| | #6 |
| Old Skool Join Date: May 2003 Location: Denver Colorado
Posts: 3,022
| Do you? Since pivotal altitude is based on GS, your formula must include a conversion from TAS to GS, right?
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| | #7 |
| Old Skool Join Date: Jan 2007 Location: GKY
Posts: 1,703
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You can make a chart, using 5 knot increments. Should take less than a minute in Excel.
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| | #8 |
| Old Skool | I did that and put it in my little maneuvers book, actually makes it easier for students to grasp the concept.
__________________ Commercial Pilot, IR Gold Seal CFI, CFII TT: 950ish Part 91 Company pilot Will fish for pay |
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| | #9 |
| Old Skool Join Date: Jun 2007
Posts: 1,613
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There is the computational method, which applies to either KTS or MPH. Or you can just pick a starting altitude, say 1000' and start from there. Based on the wind speed (which affects your groundspeed) PA will vary depending on your location in the manuever. |
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| | #10 | |
| Junior Member | Thanks... Quote:
Mark | |
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| | #11 |
| Senior Member |
In Knots it's GS^2 / 11.3 MPH GS^2/15 ex 110 knots would be 1070 |
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