FAA AC 25.571-1A PDF

FAA AC 25.571-1A PDF

Name:
FAA AC 25.571-1A PDF

Published Date:
03/05/1986

Status:
[ Revised ]

Description:

Damage Tolerance And Fatigue Evaluation Of Structure

Publisher:
Federal Aviation Administration

Document status:

Active

Format:

Electronic (PDF)

Delivery time:

10 minutes

Delivery time (for Czech version):

200 business days

SKU:

faa-ac-25-571-1a_2796738

PURPOSE.

This advisory circular (AC) sets forth an acceptable means of compliance with the provisions of Part 25 of the Federal Aviation Regulations (FAR) dealing with the damage-tolerance and fatigue evaluation requirements of aircraft structure.

Edition :	A
File Size :	1 file , 680 KB
Number of Pages :	11
Published :	03/05/1986

History

FAA AC 25.571-1D

FAA AC 25.571-1D

Published Date: 01/13/2011

Damage Tolerance And Fatigue Evaluation Of Structure

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FAA AC 25.571-1B

FAA AC 25.571-1B

Published Date: 02/18/1997

Damage Tolerance And Fatigue Evaluation Of Structure

10.50 €

FAA AC 25.571-1A

FAA AC 25.571-1A

Published Date: 03/05/1986

Damage Tolerance And Fatigue Evaluation Of Structure

9.90 €

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