14 CFR Part 34
PART 34—FUEL VENTING AND EXHAUST EMISSION REQUIREMENTS FOR TURBINE ENGINE POWERED AIRPLANES
- PART 34—FUEL VENTING AND EXHAUST EMISSION REQUIREMENTS FOR TURBINE ENGINE POWERED AIRPLANES
- Chapter I—Federal Aviation Administration, Department of Transportation › Subchapter C—Aircraft
- Subpart A—General Provisions
- § 34.1 Definitions.
- § 34.2 Abbreviations.
- § 34.3 General requirements.
- § 34.4 Incorporation by Reference.
- § 34.5 Special test procedures.
- § 34.6 Aircraft safety.
- § 34.7 Exemptions.
- § 34.9 Exceptions.
- Subpart B—Engine Fuel Venting Emissions (New and In-Use Aircraft Gas Turbine Engines)
- § 34.10 Applicability.
- § 34.11 Standard for fuel venting emissions.
- Subpart C—Exhaust Emissions (New Aircraft Gas Turbine Engines)
- § 34.20 Applicability.
- § 34.21 Standards for exhaust emissions.
- § 34.23 Exhaust Emission Standards for Engines Manufactured on and after July 18, 2012.
- § 34.25 Non-volatile particulate emissions standards (nvPM).
- Subpart D—Exhaust Emissions (In-use Aircraft Gas Turbine Engines)
- § 34.30 Applicability.
- § 34.31 Standards for exhaust emissions.
- Subpart E—Certification Provisions
- § 34.48 Derivative engines for emissions certification purposes.
- Subpart F [Reserved]
- Subpart G—Test Procedures for Engine Exhaust Gaseous Emissions (Aircraft and Aircraft Gas Turbine Engines)
- § 34.60 Introduction.
- §§ 34.61-34.71 [Reserved]
- Subpart H—Test Procedures and Compliance Demonstration for Non-Volatile Particulate Matter Emissions
- § 34.71 Non-volatile particulate matter (nvPM) test procedures.
- § 34.73 Demonstration of compliance for nvPM emissions.
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