![]() |
If this is your first visit, be sure to check out the FAQ by clicking the link above. You may have to register before you can post: click the register link above to proceed. To start viewing messages, select the forum that you want to visit from the selection below. |
|
|
Thread Tools | Display Modes |
|
#1
|
|||
|
|||
![]()
The airframe maker often modifies the engine and
accessories, thus the POH is the authority. STC'd systems modify that. So, if you and I keep posting sound advice, perhaps the rest of the group will develop a higher level of learning. "Allen" wrote in message .. . | | "Jim Macklin" wrote in message | ... | Not exactly. It depends on whether the gauge is calibrated | to an exact temperature or whether the gauge is used only to | find relative peak and degrees above and below. It also | depends on where the probe(s) are installed. EGT has the | probes about 4 inches past the exhaust valves, | | On single-probe EGT systems such as on John's Cessna 340 the probe is | located toward the tail end of the exhaust riser, well ahead of the turbo | but past the 4" point. This was determined (by Cessna) to be the point | where the exhaust gas is hottest. Cessna POH for the 340 recommends running | at peak for many power settings below about 62%. Cessna designed their own | exhaust systems on their twins, Beechcraft had TCM design their exhaust as a | unit with the engine. | | Allen | | |
Thread Tools | |
Display Modes | |
|
|
![]() |
||||
Thread | Thread Starter | Forum | Replies | Last Post |
AOPA Stall/Spin Study -- Stowell's Review (8,000 words) | Rich Stowell | Aerobatics | 28 | January 2nd 09 02:26 PM |
Backup Flight Data Recorder? | Fox Two | Soaring | 14 | August 27th 06 09:42 AM |
The Deaf vs. The Colorblind | Bret Ludwig | Piloting | 17 | August 21st 06 02:08 AM |
Catastrophic Decompression; Small Place Solo | Aviation | Piloting | 193 | January 13th 04 08:52 PM |
Change in TAS with constant Power and increasing altitude. | Big John | Home Built | 6 | July 13th 03 03:29 PM |