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|
Attributes | |
ACN | 341856 |
Time | |
Date | 199607 |
Day | Wed |
Local Time Of Day | 1201 To 1800 |
Place | |
Locale Reference | airport : 7a2 |
State Reference | AL |
Altitude | agl bound lower : 0 agl bound upper : 0 |
Environment | |
Flight Conditions | VMC |
Light | Daylight |
Aircraft 1 | |
Controlling Facilities | tracon : nmm |
Operator | general aviation : personal |
Make Model Name | Any Unknown or Unlisted Aircraft Manufacturer |
Operating Under FAR Part | Part 91 |
Flight Phase | landing other |
Flight Plan | None |
Person 1 | |
Affiliation | Other |
Function | observation : passenger |
Qualification | pilot : atp pilot : cfi pilot : instrument pilot : commercial |
Experience | flight time last 90 days : 80 flight time total : 4300 flight time type : 25 |
ASRS Report | 341856 |
Person 2 | |
Affiliation | Other |
Function | flight crew : single pilot |
Qualification | pilot : private |
Events | |
Anomaly | non adherence : far other anomaly other |
Independent Detector | other flight crewa |
Resolutory Action | none taken : insufficient time |
Consequence | Other |
Supplementary | |
Primary Problem | Flight Crew Human Performance |
Air Traffic Incident | Pilot Deviation |
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.
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.