Instructions for Continued Airworthiness. Instructions for continued airworthiness and maintenance manuals having airworthiness limitation sections must be provided as prescribed in 14 CFR § 21.50.
Instructions for Continued Airworthiness. Each aircraft, aircraft engine, and propeller must be accompanied by instructions for continued airworthiness and manufacturer’s maintenance manuals having airworthiness limitation sections, as prescribed in 14 CFR § 21.50.
Instructions for Continued Airworthiness. Instructions for continued airworthiness and maintenance manuals having airworthiness limitation sections must be provided as prescribed in JAR-21 Subpart N.
Instructions for Continued Airworthiness. Instructions for continued airworthiness and maintenance manuals having airworthiness limitation sections must be provided by the certificate holder as prescribed in EASA Part 21. (c) Aircraft Flight Manual, Operating Placards and Markings, Weight and Balance Report, and Equipment List. Each aircraft must be accompanied by an approved Aircraft Flight Manual, including all applicable supplements. The aircraft must also have the appropriate operating placards and markings, a current weight and balance report, and a list of installed equipment.
Instructions for Continued Airworthiness. Each TSO article exported to the United States must be accompanied by instructions for continuing airworthiness as prescribed in each TSO. In the event that the TSO article does not require any specific instructions for continuing airworthiness, the DGCA will obtain a written statement from the applicant that specifies that no instructions for continuing airworthiness are required.
Instructions for Continued Airworthiness. The DGCA has deemed FAA- approved instructions for continuing airworthiness acceptable for all aircraft, aircraft engines, propellers, and articles exported from the United States to India.
Instructions for Continued Airworthiness. Each aircraft, aircraft engine, and propeller must be accompanied by instructions for continued airworthiness and manufacturer’s maintenance manuals having airworthiness limitation sections, as prescribed in CAAI Aircraft Certification Procedure
Instructions for Continued Airworthiness. Each aircraft will be accompanied by instructions for continued airworthiness and manufacturer's maintenance manuals having airworthiness limitation sections. SLOVENIAN IMPORT REQUIREMENTS The following identifies those additional requirements that will be complied with as a condition of acceptance of products imported into Slovenia, or for use on Slovenian-registered aircraft.
a) Declaration of airworthiness for export issued by The Civil Aviation Administration of China (CAAC) based on airworthiness review of a microlight aircraft with following aircraft data: Aircraft status (New) Type: Model: Manufacturer: Serial Number: Year of production: Aircraft total time: (hours: minutes / landings) Engine Type: Engine Manufacturer: Engine Serial Number: Year (date) of production of engine : Date of engine installation: Engine total time: Engine hour (reading): Propeller Type: Propeller Manufacturer: Propeller Serial Number: Year (date) of production of propeller: Date of installation of propeller: Propeller time in service:
b) Statement / Certificate of conformity of the ultralight aircraft issued by aircraft manufacturer,
Instructions for Continued Airworthiness. The FAA will retain determinations of equivalent levels of safety, special conditions and exemptions.
Instructions for Continued Airworthiness. Instructions for continued airworthiness and on the part, or included on the appropriate airworthiness approval document if it is impractical to mark the part. In addition:
