Safety Publications Tool

US-97-01-13 : Fuel, Oil and Hydraulic Hoses - Identification / Inspection / Replacement

Number US-97-01-13
Issued by United States of America  United States of America
Issue date 1997-01-22
Effective date 1997-02-03
EASA approval number
ATA Chapter 28, 29, 79
Approval Holder
/ Type Designation
  • TEXTRON AVIATION INC.
    • 150
      • 150
      • 150A
      • 150B
      • 150C
      • 150D
      • 150E
      • 150F
      • 150G
      • 150H
      • 150J
      • 150K
      • 150L
      • 150M
      • A150K
      • A150L
      • A150M
    • 152
      • 152
      • A152
    • 172 (Skyhawk)
      • 172
      • 172A
      • 172B
      • 172C
      • 172D
      • 172E
      • 172F
      • 172G
      • 172H
      • 172I
      • 172K
      • 172L
      • 172M
      • 172N
      • 172P
      • 172Q
    • 172RG
    • 175
      • 175
      • 175A
      • 175B
      • 175C
    • 177 (Cardinal)
      • 177
      • 177A
      • 177B
    • 177RG (Cardinal RG)
    • 180
      • 180
      • 180A
      • 180B
      • 180C
      • 180D
      • 180E
      • 180F
      • 180G
      • 180H
      • 180J
      • 180K
    • 182 (Skylane)
      • 182
      • 182A
      • 182B
      • 182C
      • 182D
      • 182E
      • 182F
      • 182G
      • 182H
      • 182J
      • 182K
      • 182L
      • 182M
      • 182N
      • 182P
      • 182Q
      • 182R
      • R182
      • T182
      • TR182
    • 185 (Skywagon)
      • 185
      • 185A
      • 185B
      • 185C
      • 185D
      • 185E
      • A185E
      • A185F
    • 188 (AGwagon)
      • 188
      • 188A
      • 188B
      • A188
      • A188A
      • A188B
      • T188C
    • 206/U206 (Super Skywagon)
      • 206
      • TU206A
      • TU206B
      • TU206C
      • TU206D
      • TU206E
      • TU206F
      • TU206G
      • U206
      • U206A
      • U206B
      • U206C
      • U206D
      • U206E
      • U206F
      • U206G
    • 207 (Skywagon)
      • 207
      • 207A
      • T207
      • T207A
    • 208 (Caravan I)
      • 208
      • 208B
    • 210 (Centurion)
      • 210
      • 210-5 (205)
      • 210-5A (205A)
      • 210A
      • 210B
      • 210C
      • 210D
      • 210E
      • 210F
      • 210G
      • 210H
      • 210J
      • 210K
      • 210L
      • 210M
      • 210N
      • 210R
      • P210N
      • P210R
      • T210F
      • T210G
      • T210H
      • T210J
      • T210K
      • T210L
      • T210M
      • T210N
      • T210R
    • 310
      • 310P
      • 310Q
      • 310R
      • T310P
      • T310Q
      • T310R
    • 335
    • 336
    • 337 (Super Skymaster)
      • 337
      • 337A
      • 337B
      • 337C
      • 337D
      • 337E
      • 337F
      • 337G
      • 337H
      • M337B
      • P337H
    • 340
      • 340
      • 340A
    • 401
      • 401
      • 401A
      • 401B
    • 402
      • 402
      • 402A
      • 402B
      • 402C
    • 404 (Titan)
    • 411
      • 411
      • 411A
    • 414
      • 414
      • 414A
    • 421
      • 421
      • 421A
      • 421B
      • 421C
    • 425 (Conquest)
    • P172D
    • P206/TP206 (Super Skylane)
      • P206
      • P206A
      • P206B
      • P206C
      • P206D
      • P206E
      • TP206A
      • TP206B
      • TP206C
      • TP206D
      • TP206E
    • R172 (Hawk XP)
      • R172E
      • R172F
      • R172G
      • R172H
      • R172J
      • R172K
    • T303 (Crusader)
Revision Not applicable
Correction Not applicable
Supersedure None
Publication(s) and related information Cessna SB CQB96-3, dated October 18, 1996; SB SEB96-15, dated October 18, 1996; SB CAB96-15, Revision 1, October 18, 1996; or SB MEB96-10, dated October 18, 1996, as applicable. Copies may be obtained from Cessna Aircraft Company, Product Support, P.O. Box 7706, Wichita, Kansas 67277. For the Reims-manufactured aircraft listed in these SBs, DGAC France AD 97-050(AB) dated 26 February 1997 is the State of Design AD.
Remarks 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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