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The EASA Safety Information Section

 
 

US-90-25-05R1 : [Correction] Corrosion Prevention and Control Program - Implementation

Number US-90-25-05R1
Issued by United States of America  United States of America
Issue date 2008-02-14
Effective date 2008-01-22
EASA approval number
Contributor Federal Aviation Administration (FAA)
ATA Chapter 05
Approval Holder
/ Type Designation
  • BOEING
    • 747
      • 747-100
      • 747-100B
      • 747-100B SUD
      • 747-200B
      • 747-200C
      • 747-200F
      • 747-300
      • 747-400
      • 747-400D
      • 747-400F
      • 747SP
      • 747SR
Revision This AD revises and replaces FAA AD 90-25-05 (amendment 39-6790), dated November 27, 1990.
Correction This AD was republished to correct the Docket Number, FAA-2007-0412.
Supersedure None
Publication(s) and related information Boeing Document D6-36022, "Aging Airplane Corrosion Prevention and Control Program, Model 747," Revision A, dated July 28, 1989.
Remarks Comments regarding this AD should be referred to the Safety Information Section, Certification Directorate, EASA;
E-mail: ADs [at] easa.europa [dot] eu