EASA Biweekly AD Report 2015-12

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EASA Engine - Critical Parts - Identification / Replacement
RB211-535E4-37, RB211-535E4-B-37 and RB211-535E4-C-37 engines, all serial numbers (s/n). These engines are known to be installed on, but not limited to, Boeing 757 series aeroplanes
EASA AD 2015-0058
N/A

Rolls-Royce Alert NMSB RB.211-72-AH792 Revision 1 dated 05 June 2015.
The use of later approved revisions of this document is acceptable for compliance with the requirements of this AD.
RR Worldwide (WW) Communication WW/11174/2, dated 22 January 2015. RR WW/11196/1 dated 01 May 2015
EASA Wings - Wing Rear Spar - Inspection / Repair
Jetstream 4100 aeroplanes, all models, all serial numbers
EASA AD 2011-0096
N/A

BAE Systems (Operations) Ltd SB J41-A57-029 Revision 3 dated 08 April 2014.
The use of later approved revisions of this document is acceptable for compliance with the requirements of this AD.
EASA Fuselage - Skin and Structure / Allowable Damage Limits - Records Check / Repair
Airbus A330-201, A330-202, A330-203, A330-223, A330-243, A330-223F, A330-243F, A330-301, A330-302, A330-303, A330-321, A330-322, A330-323, A330-341, A330-342 and A330-343 aeroplanes,
Airbus A340-211, A340-212, A340-213, A340-311, A340-312 and A340-313 aeroplanes,
all manufacturer serial numbers (MSN) up to MSN 1 600 inclusive.
N/A
N/A

Airbus SB A330-53-3232 original issue dated 04 November 2014.
Airbus SB A340-53-4222 original issue dated 25 November 2014.
Airbus SB A330-53-3233 original issue dated 26 September 2014.
Airbus SB A340-53-4223 original issue dated 26 September 2014.
Airbus SB A330-53-3234 original issue dated 08 December 2014.
Airbus SB A340-53-4224 original issue dated 15 December 2014
Airbus SB A330-53-3235 Revision 01 dated 14 January 2015.
Airbus SB A340-53-4225 Revision 01 dated 14 January 2015.
Airbus SRM dated April 2013.
Airbus SRM TR 53-001 dated 28 November 2014.
The use of later approved revisions of these documents is acceptable for compliance with the requirements of this AD.
EASA Flight Controls - Elevator Trim Circuit - Inspection / Modification
Jetstream 4100 aeroplanes, all models, all serial numbers
N/A
N/A

BAE Systems (Operations) Ltd, ISB J41-27-068 original issue dated 21 January 2014.
The use of later approved revisions of these documents is acceptable for compliance with the requirements of this AD.
EASA Flight Controls - Elevator Aileron Computers - Replacement / Software Update
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 (MSN).
DGAC France AD 95-203-072 and 2001-508
N/A

Airbus SB A320-27-1135 original issue dated 29 June 2001, or Revision 01 dated 31 August 2001, or Revision 02 dated 18 April 2002.
Airbus SB A320-27-1151 original issue dated 09 March 2004, or Revision 01 dated 19 October 2004.
Airbus SB A320-27-1152 original issue dated 04 June 2004, or Revision 01 dated 19 October 2004, or Revision 02 dated 04 April 2006.
Airbus SB A320-27-1243 original issue dated 17 March 2015.
Airbus SB A320-27-1244 original issue dated 05 March 2015.
The use of later approved revisions of these documents is acceptable for compliance with the requirements of this AD.
EASA EMBRAER S.A. / 39-1394
This Airworthiness Directive (AD) applies to Embraer S.A. model ERJ 170-100 LR, ERJ 170-100 SE, ERJ 170-100 STD, ERJ 170-100 SU, ERJ 170-200 LR, ERJ 170-200 STD and ERJ 170-200 SU airplanes with manufacturer serial number 17000002, 17000004 through 17000013, and 17000015 through 17000453, inclusive.
Note (1): Airplanes with an original airworthiness certificate or original export certificate of airworthiness issued on or after February 23, 2015 must comply with the airworthiness limitations specified as part of the airworthiness certification of those airplanes, or in accordance with operations specifications approved under "Regulamento Brasileiro da Aviacao Civil" (RBAC) 121 or 135, or an inspection program approved under paragraph 91.409(e) of "Regulamento Brasileiro de Homologacao Aeronautica" (RBHA) 91.
Note (2): This AD requires revisions to certain operator maintenance documents to include new inspections or modification to the existing ones and its respective thresholds and intervals. Compliance with these inspections is required by RBHA 91.403(c). For airplanes that have been previously modified, altered, or repaired in the areas addressed by these inspections, the operator may not be able to accomplish the inspections described in the revisions. In this situation, to comply with RBHA 91.403(c), the operator must request approval for an alternative method of compliance according to paragraph (c) of this AD. The request should include a description of changes to the required inspections that will ensure the continued damage tolerance of the affected structure.
ANAC AD 2012-10-01
N/A

You must use the Appendix A, Airworthiness Limitations, of the Embraer 170 and 175 Maintenance Review Board Report, MRB 1621, Revision 10, dated February 23, 2015 to do the actions required by this AD, unless the AD specify otherwise.
EASA Electrical Power - Ground Reference Connection - Retrofit / Rotorcraft Flight Manual - Amendment
MBB-BK117 A-1, MBB-BK117 A-3, MBB-BK117 A-4, MBB-BK117 B-1, MBB-BK117 B-2 and MBB-BK117 C-1 helicopters, all serial numbers.
N/A
N/A

ECD ASB-MBB-BK117-90-118 Revision 02 dated 04 May 2009.
The use of later approved revisions of this document is acceptable for compliance with the requirements of this AD.
BK117 A-3 RFM, TR 9, dated 22 September 2006.
BK117 A-4 RFM, TR 5, dated 22 September 2006.
BK117 B-1 RFM, TR 6, dated 22 September 2006.
BK117 B-2 RFM, TR 1, dated 22 September 2006.
BK117 C-1 RFM, TR 2, dated 22 September 2006.
BK117 C-1C RFM, TR 1, dated 22 September 2006.
EASA Tail Rotor Drive - Slider Assembly Pitch Control - Inspection
A109A and A109AII helicopters, all serial numbers
N/A
N/A

AgustaWestland BT 109-149 original issue dated 29 May 2015.
The use of later approved revisions of this document is acceptable for compliance with the requirements of this AD.
EASA Main Rotor Drive - Cross-Bar - Inspection
AS 350 B, BA, BB, B1, B2, B3 and D helicopters, and
AS 355 E, F, F1, F2, N and NP helicopters, and
EC130 B4 and T2 helicopters, all serial numbers
N/A
N/A

AH ASB AS350-05.00.84 original issue dated 21 May 2015.
AH ASB AS355-05.00.73 original issue dated 21 May 2015.
AH ASB EC130-05A021 original issue dated 21 May 2015.
AH ASB EC130-05A022 original issue dated 21 May 2015.
The use of later approved revisions of these documents is acceptable for compliance with the requirements of this AD.
EASA Main Rotor Drive - Main Gear Box / Gleason Crown - Inspection / Replacement
 
EASA AD 2013-0118
N/A

AgustaWestland BT 109EP-128 Rev. A dated 28 May 2013 or Rev. B dated 20 May 2015 or Rev. C dated 26 May 2015.
AgustaWestland BT 109-K-57 Rev. A dated 28 May 2013 or Rev. B dated 20 May 2015 or Rev. C dated 26 May 2015.
AgustaWestland BT 119-058 Rev. A dated 28 May 2013 or Rev. B dated 20 May 2015 or Rev. C dated 26 May 2015.
The use of later approved revisions of these documents is acceptable for compliance with the requirements of this AD.
EASA Flight Controls - Trimmable Horizontal Stabilizer Actuator - Identification / Replacement
Airbus A330-201, A330-202, A330-203, A330-223, A330-223F, A330-243, A330-243F, A330-301, A330-302, A330-303, A330-321, A330-322, A330-323, A330-341, A330-342 and A330-343 aeroplanes, all manufacturer serial numbers (MSN).
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.
EASA AD 2013-0144R1
N/A

Airbus SB A330-27-3199 dated 15 July 2014.
Airbus SB A340-27-4190 dated 15 July 2014.
Airbus SB A340-27-5062 dated 15 July 2014.
The use of later approved revisions of these documents 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, or Airbus Mod 201796, or Airbus Mod 201938 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 Time Limits / Maintenance Checks - Maintenance Requirements / Airworthiness Limitations - Implementation
Falcon 7X aeroplanes, all serial numbers.
EASA AD 2009-0254 and 2010-0033
N/A

Dassault Aviation Falcon 7X AMM chapter 5-40 DGT 107838 revision 4, dated 02 February 2015.
The use of later approved revisions of this document is acceptable for compliance with the requirements of this AD.
EASA Navigation - Attitude Heading Reference System - Modification / Replacement
Northrop Grumman LITEF GmbH LCR-100 Attitude Heading Reference System (AHRS), Part Number (P/N) 145130-2000, P/N 145130-2001, P/N 145130-7000, P/N 145130-7001 and P/N 145130-7100.
These AHRS units are known to be installed on, but not limited to, Pilatus PC-12, Learjet 31A, Cessna 560XL, RUAG (Dornier) 228 series, and PZL Mielec M28 (Sky Truck) aeroplanes; and Bell Helicopter Textron Inc. 412EP, Bell Helicopter Textron Canada 407, and Sikorsky S-76C helicopters.
N/A
N/A

Northrop Grumman LITEF SB 145130-0017-845, issue C, dated 14 January 2015, or issue D, dated 1 April 2015, which can be downloaded from the NG LITEF GmbH website.
The use of later approved revisions of this document is acceptable for compliance with the requirements of this AD.
EASA Power Plant - Turbocharger Hose - Inspection/Replacement
DA 40 D aeroplanes, all serial numbers (S/N), if equipped with a Thielert TAE 125-02-99 engine
N/A
N/A

DAI MSB D4-088 dated 30 January 2012.
DAI MSB D4-075/1 dated 30 January 2012 with WI MSB D4-075 Revision 1.
The use of later approved revisions of these documents is acceptable for compliance with the requirements of this AD.
EASA Fuselage - Intermediate Gear Box Fairing - Inspection / Replacement
AS 332 C, AS 332 C1, AS 332 L, AS 332 L1, AS 332 L2 and EC 225 LP helicopters, all serial numbers, if equipped with an Intermediate Gear Box (IGB) fairing Part Number (P/N) 332A24-0303-05XX or P/N 332A24-0303-06XX or P/N 332A08-1391-00 or P/N 332A08-1391-01.
EASA AD 2011-0189-E
N/A

Airbus Helicopters AS332 ASB 53.01.47 Revision 5 dated 09 March 2015.
Airbus Helicopters AS332 SB 53.01.78 original issue dated 09 March 2015.
Airbus Helicopters EC225 ASB 53A001 Revision 5 dated 09 March 2015.
Airbus Helicopters EC225 SB 53-041 original issue 09 March 2015.
The use of later approved revisions of these documents is acceptable for compliance with the requirements of this AD.
EASA Flight Controls - Elevator Tension Control Regulator - Inspection
F28 Mark 0070 and Mark 0100 aeroplanes, all serial numbers
N/A
N/A

Fokker Services SBF100-27-095 original issue dated 22 April 2015.
The use of later approved revisions of this document is acceptable for compliance with the requirements of this AD.
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