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|
Attributes | |
ACN | 1010652 |
Time | |
Date | 201205 |
Local Time Of Day | 0601-1200 |
Place | |
Locale Reference | ZZZ.Airport |
State Reference | US |
Environment | |
Flight Conditions | VMC |
Light | Daylight |
Aircraft 1 | |
Make Model Name | Amateur/Home Built/Experimental |
Operating Under FAR Part | Part 91 |
Flight Phase | Descent |
Route In Use | Direct |
Flight Plan | None |
Component | |
Aircraft Component | Reciprocating Engine Assembly |
Person 1 | |
Function | Single Pilot |
Qualification | Flight Crew Air Transport Pilot (ATP) Flight Crew Instrument Flight Crew Multiengine |
Experience | Flight Crew Last 90 Days 10 Flight Crew Total 3300 Flight Crew Type 8 |
Events | |
Anomaly | Aircraft Equipment Problem Critical Inflight Event / Encounter Fuel Issue |
Narrative:
Aircraft was being flown under part 91 on a special airworthiness certificate for experimental (amateur-built) aircraft. The purpose of the flight was to conduct flight testing phase I flight limitations issued for this aircraft. Two miles short of the intended landing field (the airfield specified as home base in the aircraft's phase I operating limitations) the engine stopped due to fuel starvation. I landed uneventfully in a field. There was no damage to the aircraft or to property on the ground. I refueled and; with the permission of the farmer who owns the field; took off to return to base. At the time of the flight; the aircraft had flown fewer than five of the phase I flight hours. As the aircraft had experienced cylinder-head cooling issues; most flight time to date had focused on getting the cht's within limits. This flight was meant to test a new; enlarged cooling baffle that had been installed for that purpose. Because of the need to address the cooling issues; I had not yet had time to perform the planned test flights to verify expected fuel flow; nor to cross-check expected fuel-quantity indications (as shown on the ground with the aircraft in flight attitude) with the actual indications airborne. As a result; actual fuel quantity was less than expected. When I realized that; about twenty miles from base; I immediately began my return to home field; the fuel supply ran out just outside of glide range. Per my test plan; developed with the assistance of AC 90-89A; test flights to determine actual fuel flow and to crosscheck airborne fuel-quantity indications are planned. The data derived will provide planning data that will prevent a recurrence of this incident.
Original NASA ASRS Text
Title: Experimental aircraft pilot experiences fuel exhaustion while attempting to return to base during a Phase 1 test flight. An emergency landing in a farmers field ensues without damage to the aircraft.
Narrative: Aircraft was being flown under Part 91 on a special airworthiness certificate for Experimental (amateur-built) aircraft. The purpose of the flight was to conduct flight testing Phase I flight limitations issued for this aircraft. Two miles short of the intended landing field (the airfield specified as home base in the aircraft's Phase I operating limitations) the engine stopped due to fuel starvation. I landed uneventfully in a field. There was no damage to the aircraft or to property on the ground. I refueled and; with the permission of the farmer who owns the field; took off to return to base. At the time of the flight; the aircraft had flown fewer than five of the Phase I flight hours. As the aircraft had experienced cylinder-head cooling issues; most flight time to date had focused on getting the CHT's within limits. This flight was meant to test a new; enlarged cooling baffle that had been installed for that purpose. Because of the need to address the cooling issues; I had not yet had time to perform the planned test flights to verify expected fuel flow; nor to cross-check expected fuel-quantity indications (as shown on the ground with the aircraft in flight attitude) with the actual indications airborne. As a result; actual fuel quantity was less than expected. When I realized that; about twenty miles from base; I immediately began my return to home field; the fuel supply ran out just outside of glide range. Per my test plan; developed with the assistance of AC 90-89A; test flights to determine actual fuel flow and to crosscheck airborne fuel-quantity indications are planned. The data derived will provide planning data that will prevent a recurrence of this incident.
Data retrieved from NASA's ASRS site as of July 2013 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.