EASA Biweekly AD Report 05-2015

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EASA No subject

This Airworthiness Directive (AD) applies to Embraer S.A. model ERJ 190-100 STD, ERJ 190-100 LR, ERJ 190-100 IGW, ERJ 190-100 SR, ERJ 190-200 STD, ERJ 190-200 LR and ERJ 190-200 IGW airplanes; all serial numbers.
ANAC ADs 2015-02-01 and 2014-02-01
N/A

Embraer SB 190-36-0023
Embraer SB 190-36-0023
Embraer SB 190-21-0041
EASA Tail Rotor - Pitch Control Link Assembly - Inspection / Replacement
A109A, A109AII, A109C, A109E, A109K2, A109LUH, A109S, AW109SP, A119 and AW119MKII helicopters, all serial numbers
N/A
N/A

AgustaWestland BT 109-145 Rev. A, dated 27 February 2015.
AgustaWestland BT 109EP-141 Rev. A, dated 27 February 2015.
AgustaWestland BT 109K-65 Rev. A, dated 27 February 2015.
AgustaWestland BT 109L-079 Rev. A, dated 27 February 2015.
AgustaWestland BT 109S-065 Rev. A, dated 27 February 2015.
AgustaWestland BT 109SP-087 Rev. A, dated 27 February 2015.
AgustaWestland BT 119-072 Rev. A, dated 27 February 2015.
The use of later approved revisions of these documents is acceptable for compliance with the requirements of this AD.
EASA Flight Controls - Aileron, Speed Brake and Flap Control Systems - Modification
TSA-M powered sailplanes, S6 and S6-RT models, all manufacturer serial numbers (MSN); and
ASP Model S15-1 aeroplanes, all MSN.
N/A
N/A

None
EASA Wings - Fixed Wing Leading Edge and Front Spar Structure - Inspection / Repair
BAe 146 and AVRO 146-RJ aeroplanes, all models, all serial numbers.
EASA AD 2009-0014
N/A

BAE Systems (Operations) Ltd ISB.57-072 Initial Issue dated 22 February 2008, or Revision 1 dated 25 September 2008, or Revision 2 dated 29 April 2010, or Revision 3 dated 31 August 2010.
The use of later approved revisions of this document is acceptable for compliance with the requirements of this AD.
EASA Auto Flight / Instruments - Stop Rudder Input Warning - Installation / Activation
Airbus A318-111, A318-112, A318-121, A318-122, A319-111, A319-112, A319-113, A319-114, A319-115, A319-131, A319-132, A319-133, A320-211, A320-212, A320-214, A320-215, A320-216, A320-231, A320-232, A320-233, A321-111, A321-112, A321-131, A321-211, A321-212, A321-213, A321-231 and A321-232 aeroplanes, all manufacturer serial numbers.
N/A
N/A

Airbus SB A320-22-1375 original issue dated 15 January 2014.
Airbus SB A320-22-1427 original issue dated 25 January 2013.
Airbus SB A320-22-1447 original issue dated 18 October 2013.
Airbus SB A320-22-1461 original issue dated 31 October 2013.
Airbus SB A320-22-1480 original issue dated 09 July 2014.
Airbus SB A320-22-1454 original issue dated 12 February 2014.
Airbus SB A320-22-1502 original issue dated 14 November 2014.
Airbus SB A320-31-1414 original issue dated 19 December 2012.
The use of later approved revisions of these documents is acceptable for compliance with the requirements of this AD.
EASA Time Limits / Maintenance Checks - ALS Part 3 - Fuel Airworthiness Limitations - Implementation
F28 Mark 0070 and Mark 0100 aeroplanes, all serial numbers
N/A
N/A

Fokker 70/100 Instructions for Continued Airworthiness, ALS Part 3, Fokker Services Engineering Report SE-672 issue 5, release date 11 December 2014.
The use of later approved revisions of this report is acceptable for compliance with the requirements of this AD.
EASA Time Limits / Maintenance Checks - ALS Part 3 - Fuel Airworthiness Limitations - Implementation
F27 Mark 050, Mark 0502 and Mark 0604 aeroplanes, all serial numbers
N/A
N/A

Fokker 50/60 Instructions for Continued Airworthiness, ALS Part 3, Fokker Services Engineering Report SE-671 issue 7, release date 11 December 2014.
The use of later approved revisions of this report is acceptable for compliance with the requirements of this AD.
EASA Fuselage - Tail Boom / Fenestron Junction Frame - Inspection
EC 130 B4 and EC 130 T2 helicopters, all serial numbers.
EASA AD 2014-0145R1
N/A

Airbus Helicopters EC130 Emergency ASB No. 05A017 original issue, dated 06 June 2014, or Revision 1 dated 13 June 2014, or Revision 2 dated 20 February 2015.
Airbus Helicopters SB EC130-53-029 dated 20 February 2015.
The use of later approved revisions of these documents is acceptable for compliance with the requirements of this AD.
EASA Fuel - Fuel Airworthiness Limitations - Implementation
F27 Mark 200, 300, 400, 500, 600 and 700 aeroplanes, all serial numbers
EASA AD 2014-0105
N/A

Fokker Services SBF27-28-070 original issue dated 30 June 2006, Revision 1 dated 8 January 2008, Revision 2 dated 09 January 2014, and Revision 3 dated 11 December 2014.
The use of later approved revisions of this document is acceptable for compliance with the requirements of this AD.
EASA Fuel - Fuel Airworthiness Limitations - Implementation
F28 Mark 1000, 2000, 3000 and 4000 series aeroplanes, all serial numbers.
EASA AD 2014-0110
N/A

Fokker Services SBF28-28-050 original issue dated 30 June 2006, Revision 1 dated 8 January 2008, Revision 2 dated 09 January 2014, and Revision 3 dated 11 December 2014.
The use of later approved revisions of this document is acceptable for compliance with the requirements of this AD.
EASA Doors - Potable Water Service Panel Access Door Latching Mechanism - Modification
Airbus A330-201, A330-202, A330-203, A330-223, A330-243, A330-301, A330-302, A330-303, A330-321, A330-322, A330-323, A330-341, A330-342, and A330-343 aeroplanes, all Manufacturer Serial Number (MSN), except those on which:
Airbus modification (Mod) 201715 has been embodied in production, or
Airbus Mod 201796 has been embodied in production.
Airbus A340-211, A340-212, A340-213, A340-311, A340-312, A340-313, A340-541, A340-542, A340-642 and A340-643 aeroplanes, all MSN.
N/A
N/A

Airbus SB A330-52-3086 original issue dated 27 April 2012, or Revision 01 dated 25 April 2014.
Airbus SB A340-52-4094 original issue dated 27 April 2012, or Revision 01 dated 25 April 2014.
Airbus SB A340-52-5019 original issue dated 29 May 2012, or Revision 01 dated 25 April 2014.
The use of later approved revisions of these documents is acceptable for compliance with the requirements of this AD.
EASA Engine - Fan Case Low Pressure Fuel Tubes and Clips - Inspection / Replacement
RB211 Trent 895-17, 892-17, 892B-17, 884-17, 884B-17, 877-17 and 875-17 engines, all serial numbers, except those that have embodied RR modification (Mod.) 73-H814 in production, or have been modified in service through RR Service Bulletin (SB) RB211-73-H814.
These engines are known to be installed on, but not limited to, Boeing 777 series aeroplanes.
N/A
N/A

Rolls-Royce NMSB RB211-73-D685 Revision 3 dated 18 August 2009, or Revision 4 dated 20 January 2010, or Revision 5 dated 18 August 2010, or Revision 6 dated 21 February 2011.
Rolls-Royce SB RB211-73-H814 dated 19 March 2014.
The use of later approved revisions of these documents is acceptable for compliance with the requirements of this AD.
EASA Time Limits / Maintenance Checks - ALS Part 1 - Certification Maintenance Requirements - Implementation
F28 Mark 0070 and Mark 0100 aeroplanes, all serial numbers
N/A
N/A

Fokker 70/100 Instructions for Continued Airworthiness, ALS Part 1, Fokker Services Engineering Report SE-473 issue 11, release date 19 January 2015.
The use of later approved revisions of this report is acceptable for compliance with the requirements of this AD.
EASA Fuselage - Skin Connection Angle and Pressure Bulkhead - Inspection
F28 Mark 0070 and Mark 0100 aeroplanes, all serial numbers
N/A
N/A

Fokker Services SBF100-53-128 original issue dated 12 November 2014.
Fokker Services SBF100-53-129 original issue dated 16 February 2015.
The use of later approved revisions of these documents is acceptable for compliance with the requirements of this AD.
More information on this subject can be found in Fokker Services All Operators Message AOF100.193 and AOF100.193#02.
EASA Wings - Wing Bottom Skin at Main Landing Gear Rib 5 - Inspection
Airbus A319-115, A319-132, A319-133, A320-214, A320-216, A320-232 and A320-233 aeroplanes, manufacturer serial numbers (MSN) 5817, 5826, 5837, 5848, 5855, 5864, 5875, 5886, 5896 and 5910, and MSN 5918 and up.
EASA AD 2014-0270R1
N/A

AOT A57N006-14 original issue dated 04 December 2014, or Revision 01 dated 16 February 2015.
The use of later approved revisions of this document is acceptable for compliance with the requirements of this AD.
EASA Time Limits / Maintenance Checks - Engine Critical Parts - Reduction of Cyclic Life Limits
RB211-535E4-37, RB211-535E4-B-37 and RB211-535E4-C-37 engines, all manufacturer serial numbers.
These engines are known to be installed on, but not limited to, Boeing 757 aeroplanes.
N/A
N/A

RR RB211-535E4-37 TLM 05-10-01-800-000, Revision dated 01 July 2014.
The use of later approved variations or revisions of this document is acceptable for compliance with the requirements of this AD.
EASA Rotor(s) - Main Rotor Blades - Identification / Replacement
A109A helicopters, serial numbers (S/N) from 7154 through 7255 inclusive, and A109AII helicopters, all S/N.
N/A
N/A

AgustaWestland Alert BT 109-142 original issue, dated 17 February 2015.
The use of later approved revisions of this document is acceptable for compliance with the requirements of this AD.
EASA Fuselage - Upper Forward Fuselage Stringers - Inspection / Repair
AS 202 aeroplanes, all models, all serial numbers
N/A
N/A

Gomolzig Flugzeug- und Maschinenbau GmbH SB 2015-1, original issue dated 05 February 2015.
The use of later approved revisions of this document is acceptable for compliance with the requirements of this AD.
EASA SUPERSEDED
This Airworthiness Directive (AD) applies to Embraer S.A. model ERJ 190-100 STD, ERJ 190-100 LR, ERJ 190-100 IGW, ERJ 190-100 SR, ERJ 190-200 STD, ERJ 190-200LR and ERJ 190-200 IGW airplanes; all serial numbers
ANAC AD 2014-02-01
N/A

Embraer SB 190-36-0023
Embraer SB 190-36-0023
Embraer SB 190-21-0041
EASA Time Limits / Maintenance Checks - Airworthiness Limitations - Implementation
AW109SP helicopters, serial number (s/n) 22202, and s/n 22204 through 22213 inclusive.
N/A
N/A

AgustaWestland Publication 0B-C-AMPI-00-P, Change 6, approved by EASA on 29 January 2015.
The use of later approved revisions of this document is acceptable for compliance with the requirements of this AD.
TAGS: Europe
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