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bmcd308 0
I thought that to be certified under D, the drop test was at a higher speed than under C. Can anyone enlighten me?
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riggerrob 643
Quote>>TSO C23C and D<<
I thought that to be certified under D, the drop test was at a higher speed than under C. Can anyone enlighten me?
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Under TSO C23C and D, the manufaturer must prove that the rig will survive opening at 150 knots with 254 pounds.
However, under TSO C23D, they have the OPTION of certifying a rig to heavier weights or higher air speeds.
Hooknswoop 19
QuoteUnder TSO C23C and D, the manufaturer must prove that the rig will survive opening at 150 knots with 254 pounds.
However, under TSO C23D, they have the OPTION of certifying a rig to heavier weights or higher air speeds.
w/ TSO C23-D they can go as low as 220 pounds, like the PD-106R
Derek
sabr190 0
When do you think manufactures will try to engineer a harness/container system to cater to the growing number of jumpers who fly small parachutes, but would like a reserve that is more suited to their weight or personal preference? Lets face it, a 220lb jumper landing unconcious under a PD106 reserve is a real possibility, and that jumper becoming a fatality report due to that landing is a real scary thought.
"The needs of the many out weigh the needs of the few, or the one" - rehmwa
Hooknswoop 19
QuoteWhen do you think manufactures will try to engineer a harness/container system to cater to the growing number of jumpers who fly small parachutes, but would like a reserve that is more suited to their weight or personal preference?
When there is enough of a market to make a profit off of the new sizes.
Derek
QuoteQuoteUnder TSO C23C and D, the manufaturer must prove that the rig will survive opening at 150 knots with 254 pounds.
However, under TSO C23D, they have the OPTION of certifying a rig to heavier weights or higher air speeds.
w/ TSO C23-D they can go as low as 220 pounds, like the PD-106R
Derek
The test weight must not be less then 264 pounds, and the test weight is maximum operating weight limit(220pounds) x 1.2, that equals 264 pounds. The test speed must be not less than 180 KEAS, maximum operating speed x 1.2 or 150 KEAS. All tests under 4.3.4 (strength test) must be done with the same canopy, harness, components.
Sparky
I just got tired of owners of high speed airplanes (i.e. $1.5 million P-51 Mustangs and jet trainers) bringing low speed parachutes to me for repack. I tried explaining the regulations and engineering limitations to the first few dozen, but after it became clear that they were not listening, I quit wasting my breath. Most of those pilots have already decided that they will go down in flames before bailing out of their precious warbird.
In an effort to preserve my own sanity, I quit lecturing.
An analogy would be an aircraft mechanic who is legally obliged to maintain an airplane in accordance with manufacturer's manuals, airworthiness directives, service bulletins, FARS, etc. But his liability stops at the hangar door.
If a pilot decides to overload an airplane, there is nothing the mechanic can do.
While working at Square One, I packed hundreds of tiny reserves, rarely knowing the size of the customer.
To clarify a point in the TSO process: under TSO C23C and D, a manufacturer must drop test until he has proven that his equipment will survive opening at 150 knots with 254 pounds suspended weight. After that, smart manufacturers placard smaller canopies at lighter weights, because no one expects the fat boy's ankles to survive landing a 97 reserve.
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