Ex parte HENDERSON - Page 2




          Appeal No. 96-2800                                                          
          Application 08/149,042                                                      


               This is an appeal from the final rejection of claims 1-11              
          and 15-22, all the pending claims in the application.                       
               The subject matter relates to an unleaded aviation                     
          gasoline composition.  Claim 1 is illustrative of the appealed              
          claims and reads as follows:                                                
               1.  An unleaded aviation gasoline composition which                    
          comprises:                                                                  
          (a)  from 85 to 92 volume percent of aviation alkylate;                     
          (b)  from 4 to 10 volume percent of at least one ether                      
          selected from methyl tertiary-butyl ether, ethyl tertiary-                  
          butyl ether, methyl tertiary-amyl ether, and mixtures of any                
          two or all three of the foregoing ethers;                                   
          (c)  from zero to 10 volume percent of one or more other                    
          hydrocarbons falling in the aviation gasoline boiling range;                
          and                                                                         
          (d)  from 0.25 to 0.6 gram of manganese per gallon as one or                
          more cyclopentadienyl manganese tricarbonyl compounds;                      
          wherein the sum of the amounts of (a) and (b), and also of (c)              
          if present, is 100 volume percent; with the proviso that (a),               
          (b) and (d), and also (c) if present, are proportioned such                 
          that said composition has (i) an ASTM D 2382 heat of                        
          combustion of at least 18,000 BTU per pound, and (ii) a                     
          minimum knock value lean rating octane number of 100 as                     
          determined by ASTM Test Method D 2700 and wherein motor method              
          octane ratings are converted to aviation ratings in the manner              
          described in ASTM Specification D 910-90.                                   
               The references relied on by the examiner are:                          
          Carmody                       2,391,084           Dec. 18, 1945             
          Evans et al. (Evans)          2,409,746           Oct. 22, 1946             
          Brown et al. (Brown '351)     3,127,351           Mar. 31, 1964             
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