question for all...and chaps like avbug, bobysamd, wrightavia etc i.e. all you guys and gals with loads of experience (with aeroplanes
)
recently had a discussion with a fellow aviator in my company re piston engine handling procedures....this was on a C402C.
We've been taught that you bring the mixture back a bit (1/3 to maybe 1/2 of full rich) after start, for the taxi so the plugs dont foul up.
Then during the before T/O checks , right to left, rpm 1700, bring the mixtures back till you get a rise in rpm and then drop, to make sure they work, then prop check, and mags.
Now the Issue:
my colleague disagrees with the above and does the mixture check after start, by bringing the mixtures back till he sees a temp rise EGT.
This because he reckons there are not very close tolerances between the piston, rings and sleeve and the pistons needs to heat up fast to avoid 'slapping around in the sleeves', and reducing the mixture with 1700rpm will burn the rings ......?
Another point was :
Descent, after FREDA checks, Ive been taught by two previous CP's to bring the power back from cruise (29'MP, 2350RPM,90FF, with Cowls closed) to 26'MP, leaving the rest the same. next power reduction will be in circuit with 24-26'MP, 2500RPM, and 100FF. Reasoning was that you reduce the power changes since after take-off by half each time
i.e. Max power for T/O was 39'MP, 2700RPM and FF for T/O, the MP is reduced 9-10' to 30 or Top of green for climb and then 29' for cruise. Thus for descent reduce change by half again and set 26' (first redcution was about 10' , second was about 5, and third about 2)....
Colleague (and I am aware of this method, as I use it on the C210 and similar a/c) is to reduce the MP 1' per minute or 1000' of altitude lost. This of course being to reduce chances of shock cooling.
The discussion then turned to the virtues of certain manufacturer's piston engines as Continental is viewed by some as a 'wimpy' engine, in having TBO of 1600hrs and Lycoming as 'stronger' or 'tougher' engine with TBO of, methinks 2000hrs.....
I have never had any major problems with Continental engines, apart from a llittle bit of vapourlock in a C310, and stubbourn starting when hot........but then again, the Lycomings in the BN2 Islander can be b!itches to start when theyre hot as well!
We also discussed the problems with aviation training , as it seems a lot of instructors teaching new pupes to fly, are still 'wet behind the ears' themselves ' and lack the real-world experience you gain out on the line. certainly this can compound 'bad' engine handling habits....
This is a bit of a long post, but youre views and opinions would be welcomed.
One last thing: Is anybody aware of a book or DVD or course or something that covers these above topics? Experince gained from real worls operations etc?
Cheers

recently had a discussion with a fellow aviator in my company re piston engine handling procedures....this was on a C402C.
We've been taught that you bring the mixture back a bit (1/3 to maybe 1/2 of full rich) after start, for the taxi so the plugs dont foul up.
Then during the before T/O checks , right to left, rpm 1700, bring the mixtures back till you get a rise in rpm and then drop, to make sure they work, then prop check, and mags.
Now the Issue:
my colleague disagrees with the above and does the mixture check after start, by bringing the mixtures back till he sees a temp rise EGT.
This because he reckons there are not very close tolerances between the piston, rings and sleeve and the pistons needs to heat up fast to avoid 'slapping around in the sleeves', and reducing the mixture with 1700rpm will burn the rings ......?
Another point was :
Descent, after FREDA checks, Ive been taught by two previous CP's to bring the power back from cruise (29'MP, 2350RPM,90FF, with Cowls closed) to 26'MP, leaving the rest the same. next power reduction will be in circuit with 24-26'MP, 2500RPM, and 100FF. Reasoning was that you reduce the power changes since after take-off by half each time
i.e. Max power for T/O was 39'MP, 2700RPM and FF for T/O, the MP is reduced 9-10' to 30 or Top of green for climb and then 29' for cruise. Thus for descent reduce change by half again and set 26' (first redcution was about 10' , second was about 5, and third about 2)....
Colleague (and I am aware of this method, as I use it on the C210 and similar a/c) is to reduce the MP 1' per minute or 1000' of altitude lost. This of course being to reduce chances of shock cooling.
The discussion then turned to the virtues of certain manufacturer's piston engines as Continental is viewed by some as a 'wimpy' engine, in having TBO of 1600hrs and Lycoming as 'stronger' or 'tougher' engine with TBO of, methinks 2000hrs.....
I have never had any major problems with Continental engines, apart from a llittle bit of vapourlock in a C310, and stubbourn starting when hot........but then again, the Lycomings in the BN2 Islander can be b!itches to start when theyre hot as well!
We also discussed the problems with aviation training , as it seems a lot of instructors teaching new pupes to fly, are still 'wet behind the ears' themselves ' and lack the real-world experience you gain out on the line. certainly this can compound 'bad' engine handling habits....
This is a bit of a long post, but youre views and opinions would be welcomed.
One last thing: Is anybody aware of a book or DVD or course or something that covers these above topics? Experince gained from real worls operations etc?
Cheers