[Code of Federal Regulations]

[Title 14, Volume 1]

[Revised as of January 1, 2006]

From the U.S. Government Printing Office via GPO Access

[CITE: 14CFR34.10]



[Page 803]

 

                     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.