PTZ AD 2012

Številka PTZReferenčna PTZDatum efektiveRok izvršitveProizvajalecVsebina PTZReferenčni SB
001-12 PTZEASA EMERGENCY AD 2012-0019-E27.01.2012Within 4 flight hours or 30 days, whichever occurs first after the effective date of this AD;
See Required Action(s)
And Compliance
Time(s) for Details
BRP-Powertrain GmbH & Co. KG Rotax 912 S2, 912 S3 and 914 F2 enginesEngine Oil – Oil Pump and Attachment Bolts – Inspection BRP-Powertrain ASB-912-060 and ASB-914-043 (same document), dated 26 January 2012
002-12 PTZEASA EMERGENCY AD 2012-0041-E14.03.2012Before the first flight of the day after the effective date of this AD and thereafter, before each first flight of the day; See Required Action(s)
And Compliance
Time(s) for Details
Eurocopter Deutschland GmbH (ECD), Eurocopter España S.A., Eurocopter S.A.   EC 135 and EC 635 helicoptersMain Rotor System – Main Rotor Hub – Inspection / ReplacementEurocopter Deutschland ASB No. EC135-62A-029 dated 08 March 2012
003-12 PTZEASA EMERGENCY AD 2012-0075-E02.05.2012Before next flight after the effective date of this AD;
See Required Action(s)
And Compliance
Time(s) for Details
Société de Motorisations Aéronautiques
SMA SR305-230 engine installation
Cessna Model 182M, 182N, 182P, 182Q, 182R, and (Reims-manufactured)
F182P and F182Q aeroplanes, all serial numbers, if modified in accordance
with STC 10013975 (formerly EASA.A.S.00774) (SMA SR305-230 engine
installation)
Powerplant – Turbocharger and Intercooler Hoses – Replacement SMA SB n° SB-C182-71-007 origina l issue dated 26 April 2012
004-12 PTZEASA EMERGENCY AD 2012-0077-E04.05.2012Before next flight after the effective date of this AD;
See Required Action(s)
And Compliance
Time(s) for Details
AgustaWestland S.p.A. AB412 and AB412EP helicoptersEquipment & Furnishings – Hoist Hook – InspectionAgustaWestland BT 412-132 original issue dated 02 May 2012
005-12 PTZFAA EMERGENCY AD 2012-10-52This Emergency AD is effective upon receiptBefore further flight, see AD compliance for detailsCessna 206, 207, and 210 airplanes with Hartzell Engine Technologies (HET) turbochargers, part
numbers (P/Ns) 406610-0005 and 406610-9005, installed.   These turbochargers are installed on, but not limited to, Cessna 206, 207, and 210 airplanes
with Continental Motors, Inc TSIO-520-C, -G, -H, -M, and –R reciprocating engines installed
Turbocharger incorrectly located oil passages in the center housing, causing insufficient oil flow to the bearings.HET Alert Service Bulletin No. 047, dated May 8, 2012
006-12 PTZEASA EMERGENCY AD 2012-0085-E   This AD supersedes EASA AD 2012-0041R1 dated 15 March 20118.05.2012Within 3 days after the effective date of this AD and thereafter, before
each flight;
See Required Action(s)
And Compliance
Time(s) for Details
Eurocopter Deutschland GmbH (ECD), Eurocopter España S.A., Eurocopter S.A. EC 135 P1(CDS), EC 135 P1(CPDS), EC 135 P2(CPDS), EC 135 P2+,
EC 135 T1(CDS), EC 135 T1(CPDS), EC 135 T2(CPDS), EC 135 T2+,
EC 635 T1(CPDS), EC 635 P2+ and EC 635 T2+ helicopters, all S/N
Main Rotor System – Main Rotor Hub – Inspection / ReplacementEurocopter Deutschland ASB No. EC135-62A-029 Revision 1, dated 16 May 2012
007-12 PTZEASA EMERGENCY AD 2012-0086-E   This AD supersedes EASA AD 2012-0077-E dated 03 May 201219.05.2012See Required Action(s)
And Compliance
Time(s) for Details
AgustaWestland S.p.A (formerly Agusta S.p.A.), AgustaWestland Philadelphia
Corporation (formerly Agusta Aerospace Corporation) AB412 and AB412EP helicopters, all serial numbers
Equipment & Furnishings – Hoist Hook – InspectionAgustaWestland BT 412-132 original issue dated 02 May 2012   AgustaWestland BT 412-133 original issue dated 17 May 2012
008-12 PTZEASA EMERGENCY AD 2012-0093-E   This AD is superseded with EASA AD 2012-0097-E28.05.2012From the effective date of this AD, before next flight;
See Required Action(s)
And Compliance
Time(s) for Details
BRP-Powertrain GmbH & Co. KG, BRP-Rotax GmbH & Co. KG; Bombardier-
Rotax GmbH & Co. KG; Bombardier-Rotax GmbH Rotax 912 series engines
Engine - Fuel and Control – Fuel Pump – ReplacementBRP-Powertrain ASB-912-061, dated 26 May 2012
009-12 PTZEASA EMERGENCY AD 2012-0097-E   This AD supersedes EASA Emergency AD 2012-0093-E dated 26 May 2012 and is suerseded with EASA AD 2012-0097R101.06.2012From the effective date of this AD, before next flight;
See Required Action(s)
And Compliance
Time(s) for Details
BRP-Powertrain GmbH & Co. KG, BRP-Rotax GmbH & Co. KG; Bombardier-
Rotax GmbH & Co. KG; Bombardier-Rotax GmbH   Rotax 912 series engines
Engine - Fuel and Control – Fuel Pump – ReplacementBRP-Powertrain ASB-912-061R1, dated 31 May 2012
010-12 PTZEASA AD 2012-0097R1   This AD revises EASA Emergency AD 2012-0097-E dated 31 May 2012, which superseded EASA Emergency AD 2012-0093-E dated 26 May 201201.06.2012From the effective date of this AD, before next flight;
See Required Action(s)
And Compliance
Time(s) for Details
BRP-Powertrain GmbH & Co. KG, BRP-Rotax GmbH & Co. KG; Bombardier-
Rotax GmbH & Co. KG; Bombardier-Rotax GmbH   Rotax 912 series engines
Engine - Fuel and Control – Fuel Pump – ReplacementBRP-Powertrain ASB-912-061R1, dated 31 May 2012
011-12 PTZFAA EMERGENCY AD 2012-10-5226.06.2012Before further flight, remove from service the turbochargers identified in paragraph (c) of this
emergency AD, unless already done
Hartzell Engine Technologies (HET) turbochargers various P/N´s and S/N´s- see AD Applicability for details.   These turbochargers are installed on, but not limited to, Cessna 206, 207, and 210 airplanes with Continental Motors, Inc TSIO-520-C, -G, -H, -M, and -R reciprocating engines installed.Turbocharger bearing seizure, failed
turbocharger components, and damage to the airplane
Hartzell Engine Technologies Alert Service Bulletin No. 047, dated May 8, 2012
012-12 PTZEASA EMERGENCY AD 2012-0195-E   Corrected 25.09.12 EASA EAD 2012-0195-E  27.09.2012Within 5 Flight Hours (FH) after the effective date of this AD
See Required Action(s) And Compliance Time(s) for Details
AgustaWestland S.p.A (formerly Agusta S.p.A.).   A109E helicopters, serial numbers (S/N) from 11002 to 11807, except 11796;  A109LUH, all S/N; A109S, all S/N; AW109SP, S/N from 22202 to 22278, except 22239, 22264, 22266, 22272, 22273, 22275 and 22277;
A109C helicopters, all S/N;  and A109K2 helicopters, all S/N
Tail Rotor – Tail Rotor Duplex Bearing Ring Nut – InspectionSee Ref. Publications for list
013-12 PTZEASA EMERGENCY AD 2012-0232-E02.11.2012Within 10 days or 50 flight hours, whichever occurs first after the effective date of this AD. See Required Action(s)
And Compliance
Time(s) for Details
Airbus (formerly Airbus Industrie)
A300-600 and A310 aeroplanes
Equipment / Furnishings – Portable Oxygen Cylinder in Overhead Stowage – Inspection / ReplacementAirbus AOT A25W003-12, dated 31 October 2012
014-12 PTZEASA EMERGENCY AD 2012-0257-E07.12.2012During the next ALF check after the effective date of this AD, and thereafter, during each ALF check, without exceeding 10 flight hours between two consecutive inspections. See Required Action(s)
And Compliance
Time(s) for Details
EUROCOPTER (formerly Eurocopter France, Aerospatiale)
AS 350 and AS 355 helicopters

Tail Rotor – Laminated Half-Bearings – Inspection / Replacement
Eurocopter AS350 EASB No. 05.00.71 Revision 1 dated 26 November 2012 Eurocopter AS355 EASB No. 05.00.63 Revision 1 dated 26 November 2012
015-12 PTZEASA EMERGENCY AD 2012-0264-E This AD is superseded with EASA AD 2013-002222.12.2012Before next flight after the effective date of this AD See Required Action(s)
And Compliance
Time(s) for Details

AIRBUS (formerly Airbus Industrie) A318, A319, A320 and A321 aeroplanes
Airplane Flight Manual – Blocked Angle of Attack Sensor – Operational Procedure Airbus AFM A320 TR286 “AOA Blocked” issue 1.0 dated 17 December 2012