EASA Biweeky AD Report 03-2015

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EASA AD 2013-0196R1 - Electric and Electronic Common Installation - Harness at Door 3 Area - 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 numbers (MSN) on which Airbus Modification (Mod) 48825 is embodied in production, except those on which one of the following Mods is embodied:
40161, 49289, 50201, 50412, 52485, 55680, 56070, 56250, 57023, 58230, 58470, 58870, 58990, 200467, 201669
Airbus A340-211, A340-212, A340-213, A340-311, A340-312 and A340-313 aeroplanes, all MSN on which Airbus Mod No 48825 is embodied in production, except those on which Mod 55606 or Mod 57400 or Mod 40161 is embodied.
Supersedes: N/A
Relates to: N/A
Ref. Publications
Airbus SB A330-92-3098 original issue dated 11 January 2013.
Airbus SB A340-92-4084 original issue dated 11 January 2013.
The use of later approved revisions of these documents is acceptable for compliance with the requirements of this AD.
EASA AD 2013-0281R1 - Lights - Position Strobe Light - Inspection / Deactivation / Modification
AS 350 B, AS 350 BA, AS 350 BB, AS 350 B1, AS 350 B2, AS 350 B3 and AS 350 D helicopters, all serial numbers (s/n), and AS 355 E, AS 355 F, AS 355 F1, AS 355 F2, AS 355 N and AS 355 NP helicopters, all s/n, if modified in production with (optional) modification OP0811 and equipped with a Grimes-Honeywell power supply unit, Part Number (P/N) 60-1431-3, in the baggage compartment as part of that optional modification, except helicopters that have embodied at least one of the modifications as listed in Appendix1 of this AD.
Supersedes: EASA AD 2011-0244-E
Relates to: N/A
Ref. Publications
Eurocopter AS350 ASB No. 05.00.66, dated 22 December 2011, or Revision 1, dated 20 November 2013, or Airbus Helicopters AS350 ASB No. 05.00.66, Revision 2 dated 17 November 2014.
Eurocopter AS355 ASB No. 05.00.60, dated 22 December 2011, or Revision 1, dated 20 November 2013 or, Airbus Helicopters AS355 ASB No. 05.00.60 Revision 2 dated 17 November 2014.
Eurocopter AS350 ASB No. 33.00.33, dated 20 November 2013, or Airbus Helicopters AS350 ASB No. 33.00.33 Revision 1 dated 17 November 2014.
Eurocopter AS355 ASB No. 33.00.20, dated 20 November 2013, or Airbus Helicopters AS350 ASB No. 33.00.20 Revision 1 dated 17 November 2014.
The use of later approved revisions of these documents is acceptable for compliance with the requirements of this AD.
EASA AD 2014-0175-CN --- This Notice cancels EASA AD 2014-0175 - Powerplant - Engine Reduction Gear Box Bearings - Inspection / Replacement
A119 and AW119MK II helicopters, all serial numbers (S/N), if equipped with a Pratt & Whitney Canada (PWC) PT6B-37A engine having a S/N as listed in Transport Canada Civil Aviation (TCCA) AD CF-2015-01.
Supersedes: N/A
Relates to: N/A
Ref. Publications
AgustaWestland BT No. 119-066 rev. A dated 27 January 2015.
EASA AD 2015-0013 - Fuel - Internal Auxiliary Fuel System - Modification
S-92A helicopters, if equipped with a Zodiac Aerosafety System (ASY) IAFS forward auxiliary fuel tank, Part Number (P/N) 508687 series
Supersedes: N/A
Relates to: N/A
Ref. Publications
Zodiac Aerosafety Systems SB n° 508687-28-002 original issue, dated 07 January 2015.
The use of later approved revisions of this document is acceptable for compliance with the requirements of this AD.
EASA AD 2015-0014 - Engine - Reduction Gear Box Quill Shaft and Supporting Cone - Inspection
M601D, M601D-1, M601D-11NZ, M601E, M601E-11, M601E-11A, M601E-21 and M601F engines with a serial number (s/n) as listed in Appendix 1 of this AD.
These engines are known to be installed on, but not limited to, Aircraft Industries L-410 aeroplanes.
Supersedes: N/A
Relates to: N/A
Ref. Publications
GE Aviation Czech SB M601D/44 original issue dated 27 June 2014, or Revision 01 dated 23 December 2014, or Revision 02 dated 23 January 2015.
The use of later approved revisions of this document is acceptable for compliance with the requirements of this AD.
EASA AD 2015-0016 - Rotor(s) - Main Rotor Blade Attachment Pin - Inspection
AS 332 L2 helicopters, all manufacturer serial numbers (MSN), if equipped with Main Rotor Blade (MRB) Attachment Pin Part Number (P/N) 332A31-2123-00 or P/N 332A31-2115-20, and
EC 225 LP helicopters, all MSN, if equipped with MRB Attachment Pin P/N 332A31-3204-20.
Supersedes: N/A
Relates to: N/A
Ref. Publications
Airbus Helicopters ASB EC225-05A040 dated 22 December 2014,
Airbus Helicopters ASB AS332-05.00.99 dated 22 December 2014.
The use of later approved revisions of these documents is acceptable for compliance with the requirements of this AD.
TC AD CF-2015-01 - Engine Indicating - Incorrect Engine Torque Indication
Pratt & Whitney Canada (P&WC) model PT6B-37A engines with pre-Service Bulletin (SB) 39092 configuration and serial numbers:
PCE-PU0001, PU0004, PU0006, PU0008, PU0009, PU0010, PU0015, PU0016, PU0023, PU0025, PU0033, PU0034, PU0036 thru PU0055, PU0058 thru PU0063, PU0066, PU0068, PU0069, PU0070, PU0072 thru PU0087, PU0092, PU0096, PU0098, PU0099, PU0100, PU0101, PU0102, PU0105 thru PU0113, PU0121, PU0122, PU0125 thru PU0142, PU0144, PU0147 thru PU0161, PU0163 thru PU0167, PU0169 thru PU0209, PU0212, PU0213, PU0214, PU0216, PU0219 and PU0220.
Supersedes: N/A
Relates to: EASA AD 2014-0175 (CANCELLED)
Ref. Publications
P&WC SB 39092
P&WC SB 39095
EASA AD 2015-0015 - Engine - Gas Generator Turbine Blades - Replacement
M601D-1, M601E, M601E-11, M601E-11A, M601E-21, M601F, M601FS, M601F-22, M601F-32, M601T and M601Z engines with a serial number (s/n) as listed in Appendix 1 of this AD.
These engines are known to be installed on, but not limited to,
- Thrush S2R aeroplanes
- PZL "Kruk" aeroplanes
- Dornier DO 28 aeroplanes
Supersedes: N/A
Relates to: N/A
Ref. Publications
GE Aviation Czech SB M601D-1_31 dated 23 December 2014.
GE Aviation Czech SB M601D-1_32 dated 23 December 2014.
The use of later approved revisions of these documents is acceptable for compliance with the requirements of this AD.
TC AD CF-2015-02 - Doors - Airstair Door Jammed due to Deformed Handrail Stowage Hardware
Bombardier Inc. model DHC-8-400, -401, and -402 aeroplanes, serial numbers 4001 through 4473, equipped with Jetway Compatible Passenger Airstair Door Modsum 4-422100 or Modsum 4-458687
Supersedes: N/A
Relates to: N/A
Ref. Publications
Bombardier SB 84-52-79
EASA AD 2014-0171R1 - Doors - Body Landing Gear Centre Door Hinge Fitting - Inspection
Airbus A380-841, A380-842 and A380-861 aeroplanes, all manufacturer serial numbers.
Supersedes: N/A
Relates to: N/A
Ref. Publications
Airbus SB A380-52-8076 original issue, dated 03 July 2014.
Airbus SB A380-52-8070 original issue, dated 05 November 2014.
The use of later approved revisions of these documents is acceptable for compliance with the requirements of this AD.
Airbus TD TD_G1_S4_05971_2014 Issue A, dated 20 January 2014.
EASA AD 2015-0011 - Fire Protection - Engine Fire Extinguishing / Detection System - Modification
CN-235-200 and CN-235-300 aeroplanes, manufacturer serial numbers from C-018 to C-211, inclusive
Supersedes: N/A
Relates to: N/A
Ref. Publications
EADS-CASA SB235-26-0006 original issue, dated 08 July 2014.
The use of later approved revisions of this document is acceptable for compliance with the requirements of this AD.
EASA AD 2014-0263R1 - Doors - Cabin Sliding Plug Doors / Emergency Jettisoning System - Inspection
AS 332 C, AS 332 C1, AS 332 L, and AS 332 L1 helicopters, all manufacturer serial numbers with a manufacturing date before 14 July 2014 and equipped with cabin sliding plug doors modified in accordance with Airbus Helicopters modification (mod) AL25612 or mod 0723047.
AS 332 L2 and EC 225 LP helicopters, all manufacturer serial numbers with a manufacturing date before 14 July 2014 and equipped with cabin sliding plug doors.
Supersedes: N/A
Relates to: N/A
Ref. Publications
Airbus Helicopters ASB AS332-53.01.86, dated 18 August 2014,
Airbus Helicopters ASB EC225-53A048, dated 18 August 2014.
The use of later approved revisions of this document is acceptable for compliance with the requirements of this AD.
EASA AD 2014-0275R1 - Oxygen - Passenger Chemical Oxygen Generators - Replacement
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).
Supersedes: N/A
Relates to: N/A
Ref. Publications
Airbus AOT A35N006-14 dated 10 December 2014.
B/E Aerospace SB 117042-35-001 original issue dated 10 December 2014.
The use of later approved revisions of these documents is acceptable for compliance with the requirements of this AD.
B/E Aerospace SIL D1019-01 Revision 1, dated 03 January 2000, provides instructions for the activation and the disposal of a removed generator.
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