Safety Publications Tool

US-2012-11-09R1 : NOT ADOPTED - EASA INFORMATION ATTACHED

Number US-2012-11-09R1
Issued by United States of America  United States of America
Issue date 2015-08-03
Effective date 2012-07-27
EASA approval number
ATA Chapter 35
Approval Holder
/ Type Designation
  • BOEING
    • 707
      • 707-100
      • 707-100B
      • 707-200
      • 707-300
      • 707-300B
      • 707-300C
      • 707-400
    • 717
      • 717-200
    • 720
      • 720
      • 720B
    • 727
      • 727
      • 727-100
      • 727-100C
      • 727-200
      • 727-200F
      • 727C
    • 737
      • 737-100
      • 737-200
      • 737-200C
      • 737-300
      • 737-400
      • 737-500
      • 737-600
      • 737-700
      • 737-700C
      • 737-800
      • 737-900
      • 737-900ER
    • 747
      • 747-100
      • 747-100B
      • 747-100B SUD
      • 747-200B
      • 747-200C
      • 747-200F
      • 747-300
      • 747-400
      • 747-400D
      • 747-400F
      • 747-8
      • 747-8F
      • 747SP
      • 747SR
    • 757
      • 757-200
      • 757-200CB
      • 757-200PF
      • 757-300
    • 767
      • 767-200
      • 767-300
      • 767-300F
      • 767-400ER
    • 777
      • 777-200
      • 777-200LR
      • 777-300
      • 777-300ER
      • 777F
    • 787
      • 787-8
      • 787-9
    • DC-10
      • DC-10-10
      • DC-10-10F
      • DC-10-15
      • DC-10-30
      • DC-10-30F
      • DC-10-40
      • DC-10-40F
    • DC-8
      • DC-8-11
      • DC-8-12
      • DC-8-21
      • DC-8-31
      • DC-8-32
      • DC-8-33
      • DC-8-41
      • DC-8-42
      • DC-8-43
      • DC-8-51
      • DC-8-52
      • DC-8-53
      • DC-8-55
      • DC-8-61
      • DC-8-61F
      • DC-8-62
      • DC-8-62F
      • DC-8-63
      • DC-8-63F
      • DC-8-71
      • DC-8-71F
      • DC-8-72
      • DC-8-72F
      • DC-8-73
      • DC-8-73F
      • DC-8F-54
      • DC-8F-55
    • DC-9
      • DC-9-11
      • DC-9-12
      • DC-9-13
      • DC-9-14
      • DC-9-15
      • DC-9-15F
      • DC-9-21
      • DC-9-31
      • DC-9-32
      • DC-9-32F
      • DC-9-33F
      • DC-9-34
      • DC-9-34F
      • DC-9-41
      • DC-9-51
      • DC-9-81
      • DC-9-82
      • DC-9-83
      • DC-9-87
    • MD-10
      • MD-10-10F
      • MD-10-30F
    • MD-11
      • MD-11
      • MD-11F
    • MD-88
    • MD-90
      • MD-90-30
  • GULFSTREAM AEROSPACE CORPORATION
    • G-1159
      • G-1159 (GII)
      • G-1159A (GIII)
      • G-1159B (GIIB)
    • G-159 (GI)
    • GIV
      • GIV
      • GIV-X
    • GV
      • GV
      • GV-SP
  • LEARJET, INC.
    • 24
      • 24
      • 24A
      • 24B
      • 24B-A
      • 24C
      • 24D
      • 24D-A
      • 24E
      • 24F
      • 24F-A
    • 25
      • 25
      • 25A
      • 25B
      • 25C
      • 25D
      • 25F
    • 28
    • 29
    • 31/35/36
      • 31
      • 31A
      • 35
      • 35A
      • 36
      • 36A
    • 45
    • 55
      • 55
      • 55B
      • 55C
    • 60
  • LOCKHEED MARTIN CORPORATION
    • 1329 (Jetstar)
      • 1329-23A
      • 1329-23D
      • 1329-23E
      • 1329-25
    • 188 (Electra II)
      • 188A
      • 188C
    • 382 (Hercules)
      • 382
      • 382B
      • 382E
      • 382F
      • 382G
      • 382J
    • L-1011 (Tristar)
      • L-1011-385-1
      • L-1011-385-1-14
      • L-1011-385-1-15
      • L-1011-385-3
  • MARYLAND AIR INDUSTRIES, INC.
    • FAIRCHILD F-27
    • FAIRCHILD FH-227
  • SABRELINER CORPORATION
    • NA-265
      • NA-265
      • NA-265-20
      • NA-265-30
      • NA-265-40
      • NA-265-60
      • NA-265-65
      • NA-265-70
      • NA-265-80
  • TEXTRON AVIATION INC.
    • 400 (Beechjet)
      • 400
      • 400A
      • 400T
    • 4000 (Horizon)
    • 500/550 (Citation)
      • 550 (Citation Bravo)
      • 550 (Citation II)
      • S550 (Citation S/II)
    • 560/560XL
      • 560 (Citation Encore)
      • 560 (Citation Encore+)
      • 560 (Citation Ultra)
      • 560 (Citation V)
      • 560XL (Citation XLS)
      • 560XL (Citation XLS+)
      • 560XL (Excel)
    • 650
    • 680
    • 750 (Citation X)
    • BAe/BH/DH/HS.125
      • BAe.125 Series 1000A
      • BAe.125 Series 1000B
      • BAe.125 Series 800A
      • BAe.125 Series 800B
      • BH.125 Series 400A
      • BH.125 Series 600A
      • DH.125 Series 1A
      • DH.125 Series 1A-522
      • DH.125 Series 1A/R-522
      • DH.125 Series 1A/S-522
      • DH.125 Series 3A
      • DH.125 Series 3A/R
      • DH.125 Series 3A/RA
      • DH.125 Series 400A
      • HS.125 Series 1B
      • HS.125 Series 1B-522
      • HS.125 Series 1B/R-522
      • HS.125 Series 1B/S-522
      • HS.125 Series 3B
      • HS.125 Series 3B/R
      • HS.125 Series 3B/RA
      • HS.125 Series 3B/RB
      • HS.125 Series 3B/RC
      • HS.125 Series 400A
      • HS.125 Series 400B
      • HS.125 Series 400B/1
      • HS.125 Series 401B
      • HS.125 Series 403A(C)
      • HS.125 Series 403B
      • HS.125 Series 600A
      • HS.125 Series 600B
      • HS.125 Series 600B/1
      • HS.125 Series 600B/2
      • HS.125 Series 600B/3
      • HS.125 Series 700A
      • HS.125 Series 700B
      • HS.125 Series F3B
      • HS.125 Series F3B/RA
      • HS.125 Series F400B
      • HS.125 Series F403B
      • HS.125 Series F600B
    • Hawker
      • Hawker 1000
      • Hawker 750
      • Hawker 800
      • Hawker 800XP
      • Hawker 850XP
      • Hawker 900XP
    • MU-300 (Diamond)
      • MU-300 (Diamond I)
      • MU-300 (Diamond IA)
      • MU-300-10 (Diamond II)
Revision This AD revises FAA AD 2012-11-09, dated June 26, 2012, to clarify a certain restriction by providing a broader method of compliance.
Correction Not applicable
Supersedure The original issue of this AD superseded FAA AD 2011-04-09, dated 8 March 2011.
Publication(s) and related information None
Remarks Following EASA review of FAA AD 2012-11-09R1, EASA has determined that the measure required by the subject FAA AD is not within the scope of Regulation (EC) No 216/2008. In addition, in view of the applicability of the AD, specified as ‘Various Transport Category Airplanes’, the AD cannot be clearly recognised as a ‘State of Design’ AD. For these two reasons, this AD does not fall within the scope of ED Decision 02/2003 and cannot be considered for adoption. No corresponding EASA AD is expected to be issued on the same subject for aeroplanes registered or operating in Europe within the scope of Regulation (EC) No 216/2008. In case you need further information, please contact the Safety Information Section, Certification Directorate, EASA. E-mail ADs[at]easa[dot]europa[dot]eu.