Narrative:

Normal flight planned for 4 hours, with 4 hours 45 mins fuel. I observed the PF lean for best power. The engine failed at 3 hours and 45 mins, due to fuel exhaustion. We landed on highway without damage to the aircraft or property. Mechanical inspection revealed left-front cylinder intake leak to cause erroneous leaning of the engine and high fuel burn rate. I suggest a 4 probe exhaust gas temperature system for early mechanical malfunction detection, and alternate tank selector (to left or right) on maximum range flts.

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Original NASA ASRS Text

Title: PAX (PLT) RPTS LNDG ON A HWY WHEN THE ACFT RAN OUT OF FUEL. THIS PLT RPTS A CYLINDER INTAKE LEAK THAT CAUSED A HIGH FUEL BURN RATE AS A RESULT OF ERRONEOUS LEANING OF THE ENG.

Narrative: NORMAL FLT PLANNED FOR 4 HRS, WITH 4 HRS 45 MINS FUEL. I OBSERVED THE PF LEAN FOR BEST PWR. THE ENG FAILED AT 3 HRS AND 45 MINS, DUE TO FUEL EXHAUSTION. WE LANDED ON HWY WITHOUT DAMAGE TO THE ACFT OR PROPERTY. MECHANICAL INSPECTION REVEALED LEFT-FRONT CYLINDER INTAKE LEAK TO CAUSE ERRONEOUS LEANING OF THE ENG AND HIGH FUEL BURN RATE. I SUGGEST A 4 PROBE EXHAUST GAS TEMP SYS FOR EARLY MECHANICAL MALFUNCTION DETECTION, AND ALTERNATE TANK SELECTOR (TO L OR R) ON MAX RANGE FLTS.

Data retrieved from NASA's ASRS site as of July 2007 and automatically converted to unabbreviated mixed upper/lowercase text. This report is for informational purposes with no guarantee of accuracy. See NASA's ASRS site for official report.