PTZ-AD 2014

Številka PTZReferenčna PTZDatum efektiveRok izvršitveProizvajalecVsebina PTZReferenčni SB
001-14 PTZEASA EMERGENCY AD  2014-0040-E21.02.2014Within 5 flight hours (FH) after the effective date of this AD, and, thereafter, at intervals not to exceed 100 FH See Required Action(s)
And Compliance
Time(s) for Details
AGUSTAWESTLAND S.p.A.
AB 412 and AB 412 EP helicopters
Tail Rotor Drive – Flanged Adapter – Inspection / ReplacementAgustaWestland BT 412-139 original issue, dated 19 February 2014
002-14 PTZEASA EMERGENCY AD  2014-0063-E14.03.2014Within 10 flight hours (FH) after the effective date of this AD and, thereafter, at intervals not to exceed 25 FH See Required Action(s)
And Compliance
Time(s) for Details
AGUSTAWESTLAND S.p.A. AB 412 helicoptersEquipment / Furnishings – Utility Hydraulic System / Pressure Line Pump and Filter – Inspection / ReplacementAgustaWestland BT 412-140 original issue, dated 11 March 2014
003-14 PTZEASA EMERGENCY AD  2014-0076-E27.03.2014Within the compliance time as defined in Table 1 of this AD, and, thereafter, at intervals not to exceed 10 flight hours (FH); See AD Required Action(s)
And Compliance
Time(s) for Details
Airbus Helicopters (formerly Eurocopter, Eurocopter France, Aerospatiale) AS 350 B, BA, BB, B1, B2, B3 and D helicopters, and AS 355 E, F, F1, F2, N and NP helicopters, all serial numbersFuselage – Rear Structure Junction Frame Reinforcement Angles – InspectionAirbus Helicopters Emergency ASB AS350 05.00.70 dated 24 March 2014 Airbus Helicopters Emergency ASB AS355 05.00.62 dated 24 March 2014
004-14 PTZEASA EMERGENCY AD  2014-0097-E25.04.2014See AD Required Action(s)
And Compliance
Time(s) for Details
Fuselage – Aft Cargo Door Sill Beam Area – InspectionAirbus (formerly Airbus Industrie) A300-600 and A310 aeroplanesAirbus AOT A53W005-14 dated 22 April 2014
005-14 PTZEASA EMERGENCY AD  2014-0102-E06.05.2014Within 10 flight hours (FH) after the effective date of this AD and, thereafter, at intervals not to exceed 25 FH See AD Required Action(s)
And Compliance
Time(s) for Details
Tail Rotor – Tail Rotor Drive Shaft Line Nuts – Inspection / ReplacementAgusta S.p.A. (formerly Costruzioni Aeronautiche G. Agusta S.p.A.) AB 206 A and AB 206 B helicopters, all serial numbersAgustaWestland BT 206-250 dated 30 April 2014
006-14 PTZEASA EMERGENCY AD 2014-0113-E09.05.2014Within the compliance time defined in Table 1 of this AD, as applicable depending on helicopter model, and, thereafter, at intervals not to exceed 25 flight hours (FH)
See AD Required Action(s)
And Compliance
Time(s) for Details
Main Rotor Drive – Engine-to-Transmission Drive Shaft Line Nuts – Inspection / ReplacementAgustaWestland S.p.A. (formerly Agusta S.p.A) AgustaWestland AB 212, AB 412 and AB 412EP helicopters, all serial numbers (s/n)AgustaWestland BT 212-205 original issue dated 28 April 2014 AgustaWestland BT 412-138 original issue dated 13 December 2013
007-14 PTZFAA EMERGENCY AD 2014-12-52This Emergency AD is effective upon receipt Before further flight See AD Compliance for Details2nd stage low-pressure turbine (LPT2) blade separations Honeywell International Inc.
(Type Certificate previously held by AlliedSignal Inc.,
Garrett Turbine Engine Company) TFE731-4, -4R, -5AR, -5BR, -5R, -20R, -20AR, -20BR, -40, -40AR, -40R, -40BR, -50R, and
-60 turbofan engines
Alert Service Bulletins
ASB No. TFE731-72-A3792, dated June 5, 2014 ASB No. TFE731-72-A5242, dated June 5, 2014 and ASB No. TFE731-72-A5243, dated June 5, 2014
008-14 PTZTRANSPORT CANADA EMERGENCY AD CF-2014-1717.06.2014Within 24 hours from the effective date of this AD, unless already accomplished See AD  Corrective Actions for DetailsAdditional limitation for landing/taxi light operations on ground due to potential fuel leakageBombardier Inc. model CL-600-2B16 (604 Variant) aeroplanes, serial numbers 5301 through 5665, and 5701 and subsequentAircraft Flight Manual (AFM) Temporary Revisions (TRs) 604/38 and 605/20
009-14 PTZTRANSPORT CANADA EMERGENCY AD CF-2014-1920.06.2014Within 24 hours from the effective date of this AD, unless already accomplished See AD  Corrective Actions for DetailsEngine Exhaust - Engine Thrust Reverser Actuator Attachment Structure FailureBombardier Inc. model CL-600-1A11 aeroplanes, serial numbers 1004 to 1085Aircraft Flight Manual (AFM)
Temporary Revisions (TR) 600/29, 600/30, 600-1/24 and 600-1/26 Bombardier Inc. Alert service bulletin (ASB) A600-0769
010-14 PTZTRANSPORT CANADA EMERGENCY AD CF-2014-2110.07.2014Within 25 hours air time from the effective date of this AD and at intervals not exceeding 8 hours air time thereafter See AD  Corrective Actions for DetailsFuel - Fuel Leak From the Auxiliary Power Unit Fuel Boost Pump Electrical Conduit in the Right Landing Light CompartmentBombardier Inc. model CL−600−2B16 aeroplanes, serial numbers 5906, 5910, 5912, 5917, 5919 to 5932, 5934, 5935, 5939, 5940, 5942 and 5948 Alert Service Bulletin (ASB) A605-28-008 Revision 2, dated 9 July 2014, or later revisions approved
011-14 PTZTRANSPORT CANADA EMERGENCY AD CF-2014-2715.08.2014See AD  Corrective Actions for DetailsWings - Inboard Flap Hinge Box – Missing Fastener Head on Forward Attachment FittingBombardier Inc. model CL-600-2B16 (604 Variant) aeroplanes, serial numbers 5301 through 5665 and 5701 through 5920Bombardier Alert Service Bulletin (ASB):
A604-57-006 Rev.2;
A605-57-004 Rev.2
012-14 PTZEASA EMERGENCY AD 2014-0238-E04.11.2014Within 5 flight hours (FH) after the effective date of this AD See AD Required Action(s)
And Compliance
Time(s) for Details
Main Rotor Drive – Main Gear Box Support Assembly Nuts – Inspection / ReplacementAGUSTAWESTLAND S.p.A. A109, AW109, A119 and AW119 helicoptersSee AD Reference Publications for list
013-14 PTZEASA EMERGENCY AD 2014-0266-E11.12.2014Before next flight after the effective date of this AD See AD Required Action(s)
And Compliance
Time(s) for Details
Airplane Flight Manual – Undue Activation of Alpha Protection – Emergency ProcedureAIRBUS A318, A319, A320 and A321 aeroplanesAirbus AFM A320 TR 502 issue 1, EASA approved 05 December 2014
014-14 PTZEASA EMERGENCY AD 2014-0270-E  Superseded by EASA AD 2014-0270R115.12.2014See AD Required Action(s)
And Compliance
Time(s) for Details
Wings – Wing Bottom Skin at Main Landing Gear Rib 5 – InspectionAIRBUS A319 and A320 aeroplanesAOT A57N006-14 original issue dated 04 December 2014
015-14 PTZTRANSPORT CANADA EMERGENCY AD CF-2013-39R212.12.2014See AD  Corrective Actions for DetailsWings - Inboard Flap Hinge Box – Incorrectly Oriented (Hi-LOK/Hi-LITE) Fastener on Forward Attachment FittingBombardier Inc. Model CL-600-1A11 (600) aeroplanes; Model CL-600-2A12 (601 Variant) aeroplanes; Model CL-600-2B16 (601-3A/3R Variant) aeroplanes
Bombardier A600-0763 Rev. 2 A601-0627 Rev. 2