[Code of Federal Regulations]
[Title 14, Volume 1]
[Revised as of January 1, 2004]
From the U.S. Government Printing Office via GPO Access
[CITE: 14CFR34.10]

[Page 794]
 
                     TITLE 14--AERONAUTICS AND SPACE
 
CHAPTER I--FEDERAL AVIATION ADMINISTRATION, DEPARTMENT OF TRANSPORTATION
 
PART 34--FUEL VENTING AND EXHAUST EMISSION REQUIREMENTS FOR TURBINE ENGINE 
POWERED AIRPLANES--Table of Contents
 
 Subpart B--Engine Fuel Venting Emissions (New and In-Use Aircraft Gas 
                            Turbine Engines)
 
Sec. 34.10  Applicability.


    (a) The provisions of this subpart are applicable to all new 
aircraft gas turbine engines of classes T3, T8, TSS, and TF equal to or 
greater than 36 kilonewtons (8090 pounds) rated output, manufactured on 
or after January 1, 1974, and to all in-use aircraft gas turbine engines 
of classes T3, T8, TSS, and TF equal to or greater than 36 kilonewtons 
(8090 pounds) rated output manufactured after February 1, 1974.
    (b) The provisions of this subpart are also applicable to all new 
aircraft gas turbine engines of class TF less than 36 kilonewtons (8090 
pounds) rated output and class TP manufactured on or after January 1, 
1975, and to all in-use aircraft gas turbine engines of class TF less 
than 36 kilonewtons (8090 pounds) rated output and class TP manufactured 
after January 1, 1975.