I feel for you having to fly commercial so much. That just wears a person out...
Check post #5707 and this is from another posting of mine#7680>
Actually, we are in the market for a used Cessna 208 (Caravan) The reliability of the turbo-prop is the main reason, and the mega-carry capacity..
The 208 is also much cheaper used than the Pilatus.
As for the Citation, things happen real fast in a jet, I don't know if I could enjoy myself, but yes, the INVN bucks are pretty nice!!!
bobcroweaircraft.com
The Australian CAA study concluded that the single turbine was at least as safe as the piston twin in regard to engine-failure related accidents, and also stated that "forced landings at night are not necessarily as hazardous as might be expected and are mostly survivable: the fatal accident rate at night, while higher than by day, is only about 8 percent." The Australian CAA concluded that the probability of a fatal accident due to engine failure on a single-engined turbine aircraft was 0.07 per 100,000 hours, compared to "the best performing piston twins" rate of 0.15 per 100,000 hours. That says you’re at least twice as safe in a turbine single as in a piston twin.
UK CAA analysis of fatal accidents to aircraft of less than 5,700kg (12,500lb) on both private and commercial operations from 1985 to 1994 showed only 6 out of 166 (3.6 percent) were due to engine stoppage. The UK data included 4 fatals to light twins due to loss of control following engine failure or asymmetric power, compared to 9 fatals in single-engined aircraft, based on a sample of 8 million flight hours. Taking into account the probable number of hours of single and twin-engined aircraft in the sample, this indicates a far higher frequency of powerplant-related fatal accidents on twins than singles; (there are 7,500 singles on the UK register compared to 350 light twins).
Analysis by Robert E. Breiling associates for Pilatus Aircraft concluded that piston-engined general aviation aircraft were involved in 2.86 times more accidents than turboprop aircraft per 100,000 flight hours, when considering all causes.
The Swedish CAA study of the mid-1980s concluded that the fatal accident rate for single-turboprops, due to engine failure, was estimated at 0.13 per 100,000 flight hours. The study concluded that operations with SE turboprops are comparable with other commercial operations.
Cessna C208 Caravan fatals in the USA, 1985-1996 (2.6 million flight hours), were 0.56 per 100,000 hours; fatal accidents due to mechanical failures of the engine were zero. Of the five non-fatal accidents involving engine failure or shutdown, three occurred in 1990 and 1991 due to oil loss, because the oil cap was left off or improperly installed; a modification has been introduced to prevent such an occurrence. The remaining two were actual engine mechanical failures (scavenge pump and gas producer turbine failures). |
