EASA biweekly AD report 2015-08

Get EASA and FAA biweekly AD reports emailed free from

EASA Flight Controls - Aileron Control System / Tab Counter Balance Weight - Replacement

PC-12/47 and PC-12/47E aeroplanes, all manufacturer serial numbers (MSN).
Note: Aeroplanes from MSN 1521 on are delivered with Pilatus Aircraft Ltd. Service Bulletin (SB) 27-021 already embodied in production
N/A
N/A

Pilatus Aircraft Ltd SB No. 27-021 initial issue, dated 20 January 2015.
The use of later approved revisions of this document is acceptable for compliance with the requirements of this AD.
EASA Flight Controls - Improperly Formulated Task in the Aircraft Maintenance Manual for the Flight Control Unit Back-up Module
Bombardier Inc. model BD-700-A10 and BD-700-A11 aeroplanes, serial numbers 9002 and subsequent
N/A
N/A

Aircraft Maintenance Manual (AMM) Task 27-61-05-710-801
Certification Maintenance Requirement (CMR) task number 27-61-05-201
EASA Air - Inlet Guide Vane / Variable Stator Vane Actuator / Clevis Pin - Inspection / Re-Installation
RTM 322-01/9 and RTM 322-01/9A engines, all serial numbers.
These engines are known to be installed on, but not limited to, NH Industries NH90 (military) helicopters
N/A
N/A

Turboméca MSB MSBP-M3-A-75-31-10-05A-A-A Issue 1 dated 18 February 2015.
The use of later approved revisions of this document is acceptable for compliance with the requirements of this AD.
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
N/A
N/A

Rolls Royce plc WW/11174/2, dated 22 January 2015
EASA Main Rotor - Main Rotor Blade Vibration Absorber - Modification
MBB-BK 117 C-2 and MBB-BK 117 D-2 helicopters, all serial numbers
N/A
N/A

AHD ASB MBB-BK117 C-2-62A-009 original issue dated 20 January 2015.
AHD ASB MBB-BK117 D-2-62A-001 original issue dated 20 January 2015.
The use of later approved revisions of these documents is acceptable for compliance with the requirements of this AD.
EASA CANCELATION
Apex and Alpha R2000 aircraft
N/A
N/A

None
EASA Oil - Nozzle Bonding on Ejector Assembly - Inspection
ARRIUS 2F engines, all serial numbers.
These engines are known to be installed on, but not limited to, Airbus Helicopters (formerly Eurocopter, Eurocopter France) EC 120 B helicopters.
EASA AD 2013-0243
N/A

Turbomeca SB 319 79 4835 original issue A dated 22 May 2013, or Version B dated 12 February 2015. The use of later approved revisions of this document is acceptable for compliance with the requirements of this AD.
EASA Engine - High Pressure Turbine Stage 1 Disc - Cyclic Life Limit Reduction
Tay 650-15 and Tay 651-54 engines, all variants, all serial numbers.
These engines are known to be installed on, but not limited to, Fokker F28 Mark 0100 and Boeing 727 series aeroplanes.
EASA AD 2007-0086
N/A

RRD NMSB TAY-72-A1821 Revision 01 dated 26 March 2015.
The use of later approved revisions of this document is acceptable for compliance with the requirements of this AD.
EASA Fuselage - Fuselage Skin Repairs - Inspection
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 numbe
N/A
N/A

Airbus AOT A53N007-14 original issue, dated 22 July 2014.
The use of later approved revisions of this document is acceptable for compliance with the requirements of this AD.
EASA Starting - Software Mapping / Start Phase Monitoring System - Installation
TAE 125-02-99 (commercial designation CD-135, formerly Centurion 2.0) and TAE 125-02-114 (commercial designation CD-155, formerly Centurion 2.0S) engines, all serial numbers (S/N), if a Dual Mass Flywheel is installed, and if the engine is installed on one of the following aeroplane types:
- Cessna 172 and (Reims-built) F172 series with engine installed through Supplemental Type Certificate (STC) EASA 10014287.
- Piper PA-28 series with engine installed through STC EASA 10014364.
- CEAPR (APEX, Robin) DR 400 series with engine installed through STC EASA.A.S.01380 or STC EASA 10014219, all aeroplane S/N up to 2674 (included), with STC installed before December 2014.
-Diamond (DAI) DA 40 D model, S/N D4.001 through D4.399 and S/N 40.DS001 through 40.DS135 (engine installed during aeroplane manufacture), or any other S/N with engine installed through STC EASA 10036328.
- DAI DA 42 and DA42 M models, S/N 42.004 through 42.427, S/N 42.AC001 through 42.AC151 and S/N 42.M001 through 42.M027 (engine installed during aeroplane manufacture), or any other S/N with engine installed through STC EASA 10048730.
Engines having a Dual Mass Flywheel installed can be identified by marking on the fuel rail (sticker "Dual Mass Flywheel installed"), or record in the engine log book ("Dual Mass Flywheel" listed as engine component on page 4 "Main Engine Components").
N/A
N/A

TMG SB TM TAE 125-1018 P1 Revision 1, dated 05 February 2015.
TMG SB TM TAE 000-0007 Revision 28, dated 05 February 2015.
TMG Installation Manual IM-02-02, Chapter 13.08.16, Issue 4, Revision 1, dated 02 December 2014.
TMG SB TMG 601-1007 P1 Revision 3, dated 05 February 2015.
TMG SB TMG 651-1004 P1 Revision 2, dated 05 February 2015.
TMG SB TMG 691-1002 P1 Revision 2, dated 05 February 2015.
CEAPR SB n° 141201 Revision 1, dated 05 February 2015.
DAI MSB D4-097/2 (Issue 2), dated 04 February 2015.
DAI MSB 42-109/1 (Issue 1), dated 04 February 2015.
The use of later approved revisions of these documents is acceptable for compliance with the requirements of this AD.
TAGS: Europe
Hide comments

Comments

  • Allowed HTML tags: <em> <strong> <blockquote> <br> <p>

Plain text

  • No HTML tags allowed.
  • Web page addresses and e-mail addresses turn into links automatically.
  • Lines and paragraphs break automatically.
Publish