I have been flying my 81 P58 since last August and put on 60 hours but can't seem to get the #2 and #4 cylinders to an acceptable temperature on climb out or in cruise. When I bought the airplane, the fuel flow was set to low and the prebuy inspection showed that cylinders 2-5 needed to be overhauled. When I accepted delivery, I had my mechanic send the fuel system to B&S to have the flow dividers matched and calibrated. The problem is at takeoff power, I still only get 30gph which B&S says is the maximum that Continental allows. It is very difficult to keep #2 and #4 below 400 on climb out (2500 rpm 35inches) and above 12,000 feet, both climb above 400 to 415.
In addition, at cruise I have to keep the left engine cowl flap open to keep both of these cylinder down. Here's what my Insight monitor read:
#1 1417 347
#2 1502 404
#3 1449 354
#4 1455 403
#5 1402 368
#6 1425 377
TIT 1523
These temperates are at 15,000ft 40 degrees OAT, cowl flap open, 17.2 gph, IAS 145 knots, 2300 rpm, 30 inches. If I close the cowl flap, #2 and #4 would go above 425 quickly.
To compare, my right engine reads with cowl flap closed:
#1 1423 331
#2 1502 360
#3 1428 354
#4 1462 365
#5 1394 359
#6 1400 342
We have checked baffling and though both sides are old, they look good. I have replaced both the #2 and #4 CHT probes. Considering the EGT readings of #2(1502) and #4 (1455) are slightly higher, I think I have a fuel related problem. I had my mechanic clean the injectors but this didn't help.
Anyone got ideas or suggestions?