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US-72-03-03R3 : Electrical Wing Flap Actuators - Inspection / Modification

Number US-72-03-03R3
Issued by United States of America  United States of America
Issue date 1984-10-01
Effective date 1984-10-15
EASA approval number
ATA Chapter 27
Approval Holder
/ Type Designation
  • TEXTRON AVIATION INC.
    • 150
      • 150F
      • 150G
      • 150H
      • 150J
      • 150K
      • 150L
      • A150K
      • A150L
    • 172 (Skyhawk)
      • 172F
      • 172G
      • 172H
      • 172I
      • 172K
      • 172L
    • 177 (Cardinal)
      • 177
      • 177A
      • 177B
    • 177RG (Cardinal RG)
    • 182 (Skylane)
      • 182E
      • 182F
      • 182G
      • 182H
      • 182J
      • 182K
      • 182L
      • 182M
      • 182N
    • 206/U206 (Super Skywagon)
      • 206
      • TU206A
      • TU206B
      • TU206C
      • TU206D
      • TU206E
      • U206
      • U206A
      • U206B
      • U206C
      • U206D
      • U206E
    • 207 (Skywagon)
      • 207
      • T207
    • 210 (Centurion)
      • 210-5 (205)
      • 210-5A (205A)
      • 210D
      • 210E
      • 210F
      • 210G
      • 210H
      • 210J
      • 210K
      • T210F
      • T210G
      • T210H
      • T210J
    • P206/TP206 (Super Skylane)
      • P206
      • P206A
      • P206B
      • P206C
      • P206D
      • P206E
      • TP206A
      • TP206B
      • TP206C
      • TP206D
      • TP206E
    • R172 (Hawk XP)
      • R172E
      • R172F
      • R172G
      • R172H
Revision This AD revises FAA AD 72-03-03 R2 (Amendment 39-1478), effective June 27, 1972.
Correction Not applicable
Supersedure None
Publication(s) and related information Cessna Service Letter (SL) SE70-16, dated June 12, 1970, or later FAA-approved revision; or SL SE72-2, dated March 24, 1972, or SL SE72-17 Revision 1 dated January 12, 1973.
Remarks This AD is not the State of Design AD for France-manufactured (Reims Aviation) aeroplanes - see DGAC France AD 72-60 (F-1972-060) issued 02 May 1972. This AD does not apply to Argentina-manufactured A182 aeroplanes, which are not validated in Europe. Comments regarding this AD should be referred to the Safety Information Section, Certification Directorate, EASA; E-mail: ADs [at] easa.europa [dot] eu.

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