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EASA Flight Controls - Rudder Control Pedal Torque Tubes - Inspection / Replacement

F 406 aeroplanes, serial numbers from 0001 to 0098 inclusive
N/A
N/A

ASI Aviation SB F406-104 original issue dated 28 July 2015.
The use of later approved revisions of this document is acceptable for compliance with the requirements of this AD.
EASA Fin Forward Pickup - Inspection
Model PAL 750XL aircraft, S/N all through to 193, 195 and 197.
NZCAA AD DCA/750XL/16A
N/A

Pacific Aerospace Limited Mandatory Service Bulletin (MSB)PACSB/XL/068
EASA Fuel Control - Fuel Control Unit Bellow Leak
Pratt and Whitney Canada (P&WC) - Engine models as listed in the AD
N/A
N/A

P&WC SB 14389
P&WC SB 13473
EASA Propellers - Rear Half Hub Dowel Holes - Inspection / Replacement
Model R352/6-123-F/1, R352/6-123-F/2 and R410/6-123-F35 propellers, all serial numbers.
These propellers are known to be installed on, but not limited to, Fokker F27 Mk 050, F27 Mk 0502 and F27 Mk 0604 aeroplanes.
N/A
N/A

Dowty Propellers SB F50-61-165 initial issue dated 19 November 2012, or ASB F50-61-A165 Revision 1 dated 12 May 2015.
The use of later approved revisions of this document is acceptable for compliance with the requirements of this AD
EASA Doors - Jettisoning System of the Pilot and Co-pilot Doors - Functional Check
EC 155 B1 helicopters, all serial numbers delivered after manufacturing before 30 June 2015, and equipped with pilot or co-pilot doors jettisoning system in accordance with Airbus Helicopters modification POST MOD 0752C05, except helicopters on which Aircraft Maintenance Manual (AMM) task 52-11-00-712 was accomplished on both pilot and co-pilot doors since last crew door installation.
N/A
N/A

Airbus Helicopters ASB EC155-52A032 revision 0, dated 22 July 2015.
The use of later approved revisions of this document is acceptable for compliance with the requirements of this AD.
EASA Doors - Cabin Sliding Plug Doors / Emergency Jettisoning System - Inspection
AS 332 C, AS 332 C1, AS 332 L, AS 332 L1 and AS 332 L2 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 0725870.
EC 225 LP helicopters, all manufacturer serial numbers with a manufacturing date before 14 July 2014 and equipped with cabin sliding plug doors.
EASA AD 2014-0263R1
N/A

Airbus Helicopters ASB AS332-53.01.86, dated 18 August 2014 or Revision 1 dated 29 June 2015.
Airbus Helicopters ASB EC225-53A048, dated 18 August 2014.
The use of later approved revisions of these documents is acceptable for compliance with the requirements of this AD.
EASA Engine - Front Support Pins - Inspection / Replacement
ARRIEL 1E2 turbo-shaft engines, all serial numbers.
These engines are known to be installed on, but not limited to, Airbus Helicopters Deutschland (formerly Eurocopter Deutschland) MBB-BK117-C1 and MBB-BK117-C2 helicopters.
N/A
N/A

Turboméca MSB 292 72 0842 version A dated 25 March 2015 or version B dated 08 July 2015.
The use of later approved revisions of this document is acceptable for compliance with the requirements of this AD.
EASA Fuselage - Missing Shims Between Longerons and Longeron Joint Fittings
Bombardier Inc. model DHC-8-400, -401 and -402 aeroplanes, serial numbers 4156 through 4453, 4456 and 4457.
N/A
N/A

Bombardier Service Bulletin (SB) 84-53-65
EASA Ice and Rain Protection- Full Ice Protection System Tail Rotor Slip Ring - Inspection / Replacement
AB139 and AW139 helicopters, all serial numbers (S/N), if equipped with Full Icing Protection System (FIPS).
Note 1: Helicopters equipped with FIPS and have one of the kits "Partial Removal Arrangement" with Part Number (P/N) from 4G3000F00311 to P/N 4G3000F00319 inclusive are affected by the requirements of this AD.
N/A
N/A

AgustaWestland BT 139-404 original issue dated 22 December 2014.
The use of later approved revisions of this document is acceptable for compliance with the requirements of this AD.
EASA Air - Carburettor Heated Air Intake Box - Modification
DR 400/100, DR 400/120 and DR 400/120D aeroplanes, all serial numbers, if modified in accordance with STC EASA.A.S.01266 (renumbered EASA STC 10014147) at original issue.
N/A
N/A

Atelier Chabord SB BS-DR420-12-01 Revision A dated 10 December 2012.
The use of later approved revisions of this document is acceptable for compliance with the requirements of this AD.
EASA Equipment and Furnishings - VHF Antenna for Emergency Flotation Gear Protection - Installation
EC 225 LP helicopters, all serial numbers, if equipped with an emergency flotation gear and having no antenna installed on the bottom structure, as described in Figure 1 of Alert Service Bulletin (ASB) No EC225-25A086, except helicopters modified in accordance with Airbus Helicopters modification (MOD) 0726840
N/A
N/A

Airbus Helicopters (formerly Eurocopter) ASB N° EC225-25A086, dated 11 July 2011.
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
 
EASA AD 2015-0103 (including correction)
N/A

Rolls-Royce Alert NMSB RB.211-72-AH972 Revision 2 dated 20 July 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 Doors - Aft Cargo Door Frame Forks - Inspection
Airbus A300F4-605R and A300F4-622R aeroplanes, all manufacturer serial numbers (MSN) on which Airbus modification (MOD) 12046 has been embodied in production.
Note: Airbus MOD 12046 has been embodied in production on MSN 0805 and above, except MSN 0836, 0837 and 0838.
N/A
N/A

Airbus AOT A52W011-15 original issue dated 23 July 2015.
The use of later approved revisions of this document is acceptable for compliance with the requirements of this AD.
EASA Tail Rotor - Rotor Blades - Inspection
AS 332 C, AS 332 C1, AS 332 L, and AS 332 L1 helicopters, equipped with tail rotor de-icing installation unit Part Number (P/N) 204ZP01Y01 and tail rotor blade P/N 332A12-0055-XX (where XX represents any dash number) (type A10).
N/A
N/A

Airbus Helicopters ASB AS332-05.01.02 original issue, dated 22 July 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 - Damage Tolerant Airworthiness Limitation Items - ALS Part 2 - Amendment
Airbus A380-841 and A380-842 aeroplanes, all manufacturer serial numbers (MSN).
N/A
N/A

Airbus A380 ALS Part 2 variation 4.6 (00L050H152E/C01 Issue 01), approved on 01 July 2015.
The use of later approved revisions of this document is acceptable for compliance with the requirements of this AD.
EASA Equipment / Furnishings - Portable Oxygen Cylinder in Overhead Stowage - Inspection / Replacement
A300-600 and A310 passenger aeroplanes, all models, all serial numbers (except all-cargo aeroplanes), if equipped with one-frame overhead stowage compartments (OHSC).
EASA AD 2012-0245-E
N/A

Airbus AOT A25W003-12 Revision 1 dated 14 November 2012.
Airbus SB A300-25-6222 original issue dated 25 February 2015.
Airbus SB A310-25-2210 original issue dated 25 February 2015.
The use of later approved revisions of these documents is acceptable for compliance with the requirements of this AD.
EASA Windows - Cabin Windows / Jettisoning System - Inspection
AS 332 and EC 225 LP helicopters, all manufacturer serial numbers equipped with an extraction tape fitted with press-studs on the windows.
N/A
N/A

Airbus Helicopters ASB EC225-56A008 original issue, dated 16 July 2015.
Airbus Helicopters ASB AS332-56.00.10 original issue, dated 16 July 2015.
The use of later approved revisions of these documents is acceptable for compliance with the requirements of this AD.
EASA Fuselage - Aft Cargo Door Sill Beam Area - Inspection
Airbus A300-600 and A310 aeroplanes, all certified models, all manufacturer serial numbers on which Airbus modification (mod) 05438 has been embodied in production, except aeroplanes on which Airbus mod 12046 has also been embodied in production.
EASA AD 2014-0097-E
N/A

Airbus AOT A53W005-14 original issue dated 22 April 2014 or Revision 01 dated 29 April 2014.
Airbus SB A300-53-6179 original issue dated 12 December 2014.
Airbus SB A310-53-2139 original issue dated 12 December 2014.
The use of later approved revisions of these documents is acceptable for compliance with the requirements of this AD.
EASA Aircraft Flight Manual - All Engine Operative Rate of Climb Performance - Revision
P.68R aeroplanes, all serial numbers (s/n) up to s/n 480 inclusive.
N/A
N/A

Vulcanair S.p.A. SB No. 244 dated 27 April 2015.
Vulcanair S.p.A. AFM NOR10.707-30, rev. 2, dated 23 April 2015.
Vulcanair S.p.A. AFM NOR10.707-30B, rev. 19, dated 23 April 2015.
Vulcanair S.p.A. AFM NOR10.707-30C, rev. 27, dated 23 April 2015.
The use of later approved revisions of these documents is acceptable for compliance with the requirements of this AD.
EASA Wiring / Harness - Collective Lever Wiring Harness - Inspection
MBB-BK117 C-2 helicopters, all serial numbers (s/n) up to s/n 9708 inclusive.
N/A
N/A

AHD ASB MBB-BK117 C-2-88A-010 Revision 1 dated 16 April 2015.
The use of later approved revisions of this document is acceptable for compliance with the requirements of this AD.
EASA Flight Controls - Elevator Control System - Corrosion of the Elevator Control Rod and Elevator Actuating Lever on the Control Column
Viking Air Ltd. (formerly Bombardier Inc.) model DHC-2 Mk. I, DHC-2 Mk. II and DHC-2 Mk. III aeroplanes, all serial numbers
N/A
N/A

Viking Air Ltd. Service Bulletin (SB) V2/0005
EASA Ice and Rain Protection - Engine Air Inlet Anti-Ice System - Aircraft Flight Manual - Amendment
Falcon 2000EX aeroplanes, all manufacturer serial numbers.
N/A
N/A

None
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