14CFR Part 21
Title 14: Aeronautics and Space
PART 21—CERTIFICATION PROCEDURES FOR PRODUCTS AND PARTS
Contents
Special Federal Aviation Regulation No. 88—Fuel Tank System Fault Tolerance Evaluation Requirements
Subpart A—General
§21.1 Applicability and definitions.
§21.2 Falsification of applications, reports, or records.
§21.3 Reporting of failures, malfunctions, and defects.
§21.4 ETOPS reporting requirements.
§21.5 Airplane or Rotorcraft Flight Manual.
§21.6 Manufacture of new aircraft, aircraft engines, and propellers.
§21.7 Continued airworthiness and safety improvements for transport category airplanes.
§21.8 Approval of articles.
§21.9 Replacement and modification articles.
Subpart B—Type Certificates
§21.11 Applicability.
§21.13 Eligibility.
§21.15 Application for type certificate.
§21.16 Special conditions.
§21.17 Designation of applicable regulations.
§21.19 Changes requiring a new type certificate.
§21.20 Compliance with applicable requirements.
§21.21 Issue of type certificate: normal, utility, acrobatic, commuter, and transport category aircraft; manned free balloons; special classes of aircraft; aircraft engines; propellers.
§21.23 [Reserved]
§21.24 Issuance of type certificate: primary category aircraft.
§21.25 Issue of type certificate: Restricted category aircraft.
§21.27 Issue of type certificate: surplus aircraft of the Armed Forces.
§21.29 Issue of type certificate: import products.
§21.31 Type design.
§21.33 Inspection and tests.
§21.35 Flight tests.
§21.37 Flight test pilot.
§21.39 Flight test instrument calibration and correction report.
§21.41 Type certificate.
§21.43 Location of manufacturing facilities.
§21.45 Privileges.
§21.47 Transferability.
§21.49 Availability.
§21.50 Instructions for continued airworthiness and manufacturer's maintenance manuals having airworthiness limitations sections.
§21.51 Duration.
§21.53 Statement of conformity.
§21.55 Responsibility of type
PART 21—CERTIFICATION PROCEDURES FOR PRODUCTS AND PARTS
Contents
Special Federal Aviation Regulation No. 88—Fuel Tank System Fault Tolerance Evaluation Requirements
Subpart A—General
§21.1 Applicability and definitions.
§21.2 Falsification of applications, reports, or records.
§21.3 Reporting of failures, malfunctions, and defects.
§21.4 ETOPS reporting requirements.
§21.5 Airplane or Rotorcraft Flight Manual.
§21.6 Manufacture of new aircraft, aircraft engines, and propellers.
§21.7 Continued airworthiness and safety improvements for transport category airplanes.
§21.8 Approval of articles.
§21.9 Replacement and modification articles.
Subpart B—Type Certificates
§21.11 Applicability.
§21.13 Eligibility.
§21.15 Application for type certificate.
§21.16 Special conditions.
§21.17 Designation of applicable regulations.
§21.19 Changes requiring a new type certificate.
§21.20 Compliance with applicable requirements.
§21.21 Issue of type certificate: normal, utility, acrobatic, commuter, and transport category aircraft; manned free balloons; special classes of aircraft; aircraft engines; propellers.
§21.23 [Reserved]
§21.24 Issuance of type certificate: primary category aircraft.
§21.25 Issue of type certificate: Restricted category aircraft.
§21.27 Issue of type certificate: surplus aircraft of the Armed Forces.
§21.29 Issue of type certificate: import products.
§21.31 Type design.
§21.33 Inspection and tests.
§21.35 Flight tests.
§21.37 Flight test pilot.
§21.39 Flight test instrument calibration and correction report.
§21.41 Type certificate.
§21.43 Location of manufacturing facilities.
§21.45 Privileges.
§21.47 Transferability.
§21.49 Availability.
§21.50 Instructions for continued airworthiness and manufacturer's maintenance manuals having airworthiness limitations sections.
§21.51 Duration.
§21.53 Statement of conformity.
§21.55 Responsibility of type