![]()  | 
            37000 Feet | Browse and search NASA's Aviation Safety Reporting System  | 
            
                
  | 
        
| Attributes | |
| ACN | 730865 | 
| Time | |
| Date | 200702 | 
| Local Time Of Day | 0601 To 1200 | 
| Place | |
| Locale Reference | airport : zzz.airport | 
| State Reference | US | 
| Altitude | agl single value : 0 | 
| Aircraft 1 | |
| Operator | common carrier : air carrier other  | 
| Make Model Name | Rockwell North American Civil Twin Jet | 
| Operating Under FAR Part | Part 91 | 
| Flight Phase | ground : taxi | 
| Person 1 | |
| Affiliation | government : military | 
| Function | other personnel other | 
| Qualification | technician : inspection authority | 
| ASRS Report | 730865 | 
| Person 2 | |
| Affiliation | government : military | 
| Function | flight crew : captain oversight : pic  | 
| Events | |
| Anomaly | aircraft equipment problem : critical | 
| Independent Detector | other flight crewa | 
| Consequence | other other  | 
| Supplementary | |
| Problem Areas | Aircraft | 
| Primary Problem | Aircraft | 
Narrative:
Background: T/M/south sabreliner T39G is a military owned aircraft maintained by contractor. By contract only FAA-pma parts are to be utilized. Incident: prior to takeoff the pilot experienced an uncommanded right engine shutdown; accompanied by a fuel leak (right engine). Maintenance reported the fuel flow transmitter to be the cause of both the fuel leak and uncommanded engine shutdown. Cause: the fuel flow had failed internally due to (6 each) allen head bolts backing out. The F/F transmitter separated into two halves when it was removed from the engine. When all 6 of the internal bolt backed out it broke an internal guide tube. Preventive action: safety wire allen head bolts.
Original NASA ASRS Text
Title: A MIL T39G SABRELINER ACFT HAD AN UNCOMMANDED R ENGINE SHUTDOWN ACCOMPANIED BY A FUEL LEAK DUE TO FAILURE OF FUEL FLOW XMITTER.
Narrative: BACKGROUND: T/M/S SABRELINER T39G IS A MIL OWNED ACFT MAINTAINED BY CONTRACTOR. BY CONTRACT ONLY FAA-PMA PARTS ARE TO BE UTILIZED. INCIDENT: PRIOR TO TKOF THE PLT EXPERIENCED AN UNCOMMANDED R ENG SHUTDOWN; ACCOMPANIED BY A FUEL LEAK (R ENG). MAINT RPTED THE FUEL FLOW XMITTER TO BE THE CAUSE OF BOTH THE FUEL LEAK AND UNCOMMANDED ENG SHUTDOWN. CAUSE: THE FUEL FLOW HAD FAILED INTERNALLY DUE TO (6 EACH) ALLEN HEAD BOLTS BACKING OUT. THE F/F XMITTER SEPARATED INTO TWO HALVES WHEN IT WAS REMOVED FROM THE ENG. WHEN ALL 6 OF THE INTERNAL BOLT BACKED OUT IT BROKE AN INTERNAL GUIDE TUBE. PREVENTIVE ACTION: SAFETY WIRE ALLEN HEAD BOLTS.
Data retrieved from NASA's ASRS site as of January 2009 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.