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You are using an out of date browser. It may not display this or other websites correctly. You should upgrade or use an alternative browser. Prev 1 β¦ Go to page. Go to page. First Prev 12 of 36 Go to page. LisaM Airman. Ok lets get started on the P, bit by bit. First the astonishing inability of Lockheed to upgrade the cooling system inc intercoolers to deal wth the greater power developed by Allison.
This meant the performance was officialy fixed across multiple models: " The maximum speed and climb performance of the various P models is, however, something of a mystery. Although rated takeoff power from the XP through the PH increased from bhp to bhp the Tactical Planning Charts issued by Wright Field show all variants with a similar speed.
Closer examination of the charts will reveal that all P powerplants, through the H model, are limited to bhp, due to "inadequate cooling. Heads would have rolled but somehow Lockheed got a pass on that. Now this, plus the extreme and unnecessary complexity of the controls was probably the major factor in the incredible engine unreiability suffered when in service in the 8th. That makes much more sense that the claim that the 'low' temps seperated the lead from the fuel, because the P suffered from excessive temps, not too low ones.