PTZ-AD 2009

Številka PTZReferenčna PTZDatum efektiveRok izvršitveProizvajalecVsebina PTZReferenčni SB
001-09 PTZFAA 2009-01-0131.12.2008Within 14 days of the effective date of this AD; See AD compliance for detailsCFM International, S. A CFM56-5B1, -5B2, -5B4, -5B5, -5B6, -5B7, -5B1/P, -5B2/P, -5B3/P, -5B3/P1, -5B4/P, -5B5/P, -5B6/P, -5B7/P, -5B8/P, -5B9/P, -5B1/2P, -5B2/2P, -5B3/2P, -5B3/2P1, -5B4/2P, -5B6/2P, -5B4/P1, -5B4/2P1, and -5B9/2P turbofan engines. These engines are installed on, but not limited to, Airbus A318, A319, A320, and A321 series airplanesHigh-pressure compressor (HPC) stalls during climb out after takeoffEASA Airworthiness Directive 2008-0227-E   CFM International, S. A. SB No. CFM56-5B S/B 72-0722
002-09 PTZAGÊNCIA NACIONAL DE AVIAÇÃO CIVIL – BRAZIL ANAC 2009-01-0108.01.2009Within the next 12 months after the effective date of this AD; See AD compliance for detailsEmbraer EMB-135BJ, EMB-135ER, EMB-135KE, EMB-135KL, EMB-135LR, EMB-145, EMB-145EP, EMB-145ER, EMB-145EU, EMB-145LR, EMB-145LU, EMB-145MK, EMB-145MP, EMB-145MR, EMB-145XR and EMB-145LRLanding Gear Electronic Unit (LGEU) - ReplacementEmbraer Service Bulletins No. 145-32-0120 or No. 145LEG-32-0032
003-09 PTZEASA 2009-000221.01.2009No later than 28 February 2011; See Required Action(s) And Compliance Time(s) for DetailsTURBOMECA Arriel 1B, 1D and 1D1 turboshaft engines, all serial numbers. These engines are known to be installed on, but not limited to, Eurocopter AS 350 B, AS 350 BA, AS 350 B1 and AS 350 B2 helicopters.Engine – Reduction Gear Box Intermediate Pinion – ModificationTurboméca, S.A. Mandatory Service Bulletin No. 292 72 0276 Version B
004-09 PTZEASA 2009-0005   This AD supersedes CAA UK AD 006-10-9922.01.2009See Required Action(s) And Compliance Time(s) for DetailsDowty Aerospace Propellers R389 and R390 propellers   These propellers are known to be installed on Saab SF340A and 340B aircraftPropellers – Hub Assembly – InspectionDowty Propellers ASB SF340-61-95 Rev 5   Dowty Propellers SB SF340-61-105 original issue or Rev 1
005-09 PTZCF- 2008-33R109.02.2009See AD Corrective Actions for DetailsBombardier Inc. CL-600-2B19 AircraftInboard Flap ActuatorSee AD
006-09 PTZEASA 2007–0138R1 This AD revises and replaces EASA AD 2007-0138-E18.05.2007See Required Action(s) And Compliance Time(s) for DetailsEUROCOPTER   AS 350 and AS 355 helicoptersTail Rotor - Tail Rotor Blades Skin- Inspection / RepairSee AD Ref. Publications for details
007-09 PTZEASA 2009–000426.01.2009See Required Action(s) And Compliance Time(s) for DetailsEUROCOPTER   AS 350 and EC 130 helicoptersEngine Starting - Starter-generator Damping Assembly – Inspection / AdjustmentSee AD Ref. Publications for details
008-09 PTZEASA 2009-000928.01.2009See Required Action(s) And Compliance Time(s) for DetailsCFM International SA CFM56-7B turbofan engines These engines are known to be installed on, but not limited to, Boeing 737series aeroplanesTime Limits – Low Pressure Turbine Rear Frame – Life Limit / Mandatory InspectionSee AD Ref. Publications for details
009-09 PTZCF-2009-0219.02.2009Within 24 months after the effective date of this directiveBombardier Inc. Model CL-600-2B19Overwing Emergency Exit PlacardsBombardier Service Bulletin (SB) 601R-11-088, dated 25 June 2008
010-09 PTZFAA 2009-02-0309.02.2009See AD compliance for detailsLycoming Engines Teledyne Continental Motors Superior Air Parts, Inc. with a Precision Airmotive LLC, RSA-5 or RSA-10 series, or Bendix, RSA-5 or RSA-10 series, fuel injection servo, having a servo plug gasket, P/N 365533, that was installed under the fuel injection servo plug, P/N 383493, on or after August 22, 2006Lean running engineSee AD
011-09 PTZFAA 2009-04-0324.03.2009See AD compliance for detailsRolls-Royce Corporation (Formerly Allison Engine Company, Inc.) AE 3007A1E and AE 1107C turbofan/turboshaft enginesLow-cycle-fatigue failure of the partsSee AD Related Information
012-09 PTZFAA 2009-04-0527.03.2009See AD compliance for detailsCessna Aircraft Company Models 182Q and 182R airplanes that are equipped with Societé de Motorisations Aéronautiques (SMA) aircraft diesel engineImproper intercooler hose assembly installationSee AD
013-09 PTZFAA 2009-04-1030.03.2009See AD compliance for detailsGeneral Electric Company CF6-80A, CF6-80C2, and CF6-80E1 series turbofan engines. These engines are installed on, but not limited to, Airbus A300, A310, and A330 series, Boeing 747 and 767 series, and McDonnell Douglas MD-11 series airplanesCritical life-limited rotating engine part failureSee AD
014-09 PTZEASA 2009-001111.02.2009See Required Action(s) And Compliance Time(s) for DetailsEUROCOPTER (formerly EUROCOPTER FRANCE, AEROSPATIALE) AS 350B, BA, BB, B1, B2, B3 and EC 130B4 helicopters, all serial numbersTime Limits/Maintenance Checks – Airworthiness Limitation - RevisionSee AD Ref. Publications for details
015-09 PTZEASA 2009-001917.02.2009See Required Action(s) And Compliance Time(s) for DetailsEUROCOPTER   AS350 helicoptersRotors Flight Control - Collective Pitch Lever Locking Stud – Inspection / RepairSee AD Ref. Publications for details
016-09 PTZEASA 2009-003905.03.2009See Required Action(s) And Compliance Time(s) for DetailsEUROCOPTER   AS 350 and AS 355 helicoptersTail Rotor - Tail Rotor Blades Skin - Inspection / RepairSee AD Ref. Publications for details
017-09 PTZEASA 2009-0022-E09.02.2009Within the next 5 flight hours after the effective date of this directive but no later than 15 February 2009, whichever occurs first; See Required Action(s) And Compliance Time(s) for DetailsAgusta S.p.A.   AB206 helicoptersEngine – Power Turbine Speed – Operational LimitationAgusta Alert Bollettino Tecnico 206-244 dated 05 February 2009
018-09 PTZEASA 2009-002524.02.2009See Required Action(s) And Compliance Time(s) for DetailsAIRBUS A318, A319, A320 and A321 aircraftWings – Flap Track No.1 Pendulum Assembly – Inspection / ReplacementAIRBUS SB A320-57-1144 or SB A320-57-1144 AIRBUS SB A320-57A1146
019-09 PTZEASA 2009-003026.02.2009See Required Action(s) And Compliance Time(s) for DetailsEUROCOPTER   AS 350 helicoptersStabilizers – Upper and Lower Fin Attachment Fitting - Inspection / Modification / ReplacementSee AD Ref. Publications for details
020-09 PTZEASA 2008-0134R131.06.2008See Required Action(s) And Compliance Time(s) for DetailsTURBOMÉCA ARRIUS 2F turbo-shaft engine These engines are known to be installed on, but not limited to, Eurocopter EC120B helicoptersEngine Fuel & Control - P3 Air Pipe -Inspection/ModificationTurboméca Service Bulletin N° 319 75 4810 original issue
021-09 PTZEASA 2009-002704.03.2009See Required Action(s) And Compliance Time(s) for DetailsEUROCOPTER   AS 350 and EC 130 helicoptersEngine Starting – Starter-Generator Damping Assembly – AdjustmentEUROCOPTER AS350 ASB No. 80.00.07 Rev 1   EUROCOPTER EC130 ASB No. 80A003
022-09 PTZEASA 2006–0140R325.05.2006See Required Action(s) And Compliance Time(s) for DetailsLufthansa Technik AG; SR Technics; Jet Aviation Basel, AG; CTT Systems AB   CTT Systems AB Zonal Drying System, P/N´s as listed in the Applicability of this directiveAir Conditioning - Zonal Drying System DeactivationSee AD Ref. Publications for details
023-09 PTZEASA 2009-003606.03.2009See Required Action(s) And Compliance Time(s) for DetailsCFM International SA (CFM)   CFM56-3 turbofan enginesEngine – Fan Blades with 25 Degree Mid-span Shrouds – InspectionsCFM service bulletin CFM56-3/3B/3C S/B 72-1067, original issue
024-09 PTZANAC 2009-02-0112.02.2009Within the next 2500 flight hours or 24 months after the effective date of this AD, whichever occurs first; See AD compliance for detailsEmbraer model EMB-135BJ, EMB-135ER, EMB-135KE, EMB-135KL, EMB-135LR, EMB-145, EMB-145EP, EMB-145ER, EMB-145EU, EMB-145LR, EMB-145LU, EMB-145MK, EMB-145MP, EMB-145MR and EMB-145XR airplanesMain landing gear (MLG) trailing arm pins - Inspection/Replacement; MLG auxiliary door mounting support - ModificationEmbraer Service Bulletin Nos. 145-32-0122 and 145-52-0047, or 145LEG-32-0033 and 145LEG-52-0014
025-09 PTZFAA 2009-05-0231.03.2009See AD compliance for detailsGeneral Electric Company CF6-80C2 and CF6-80E1 turbofan engineFuel leaksSee AD
026-09 PTZFAA 2009-04-1502.04.2009See AD compliance for detailsBoeing Model 737-100, -200, -200C, -300, -400, and -500 series airplanesMultiple adjacent cracked stringer tie clips and damaged skin and framesBoeing Special Attention Service Bulletin 737-53-1268
027-09 PTZFAA 2009-04-1702.04.2009See AD compliance for detailsGeneral Electric Company (GE) CF6-45A, CF6-45A2, CF6-50A, CF6-50C, CF6-50CA, CF6-50C1, CF6-50C2, CF6-50C2B, CF6-50C2D, CF6-50E, CF6-50E1, CF6-50E2, and CF6-50E2B series turbofan engines These engines are installed on, but not limited to, Airbus A300 series, Boeing 747 series, McDonnell Douglas DC-10 series, and DC-10-30F airplanesSeparation of LFCEN assembly forward and aft centerbodies due to high imbalance engine conditionsAccomplishment Instructions, Section 3, of GE SB No. CF6-50 S/B 78-0244, Rev 1, CF6-50 S/B 78-0244, or CF6-50 S/B 78-0242
028-09 PTZFAA 2009-05-0503.04.2009Prior to further flight after April 3, 2009 (the effective date of this AD); See AD compliance for more detailsAvidyne Corporation (Avidyne) Primary Flight Displays (PFDs), part numbers (P/Ns) 700-00006-000, 700-00006-001, 700-00006-002, 700-00006-003, and 700-00006-100   PFDs that are installed on, but not limited to the airplanes below that are certificated in any category: Adam Aircraft, Cessna Aircraft Company, Cirrus Design Corporation, Diamond Aircraft Industries, Hawker Beechcraft Corporation, Piper Aircraft, Inc.Avidyne PFDs (Primary Flight Displays ) displaying incorrect altitude and airspeed informationAvidyne Service Bulletin No. 601-00006-096, Rev 1
029-09 PTZEASA 2009-004513.03.2009See Required Action(s) And Compliance Time(s) for DetailsAIRBUS A310 and A300-600 aeroplanesEquipment / Furnishings – IPECO Pilot and Co-pilot Seats – Inspection / Modification / ReplacementASB A310-25A2199 ASB A300-25A6210 SB A310-25-2202 SB A300-25-6214   Airbus Operator Engineering Bulletin N°160-1 and N°121-1
030-09 PTZEASA 2009-005527.03.2009See Required Action(s) And Compliance Time(s) for DetailsAIRBUS SAS A310, A300-600 and A300-600ST aeroplanesElectrical Power – Engine Feeder Harness – Inspection & Nacelles/Pylons – GE CF6-80C2 Pylon Forward Pyramid – InspectionSee AD Ref. Publications for details
031-09 PTZEASA 2009-005925.03.2009See Required Action(s) And Compliance Time(s) for DetailsAvia Propeller Ltd Model V410, V500A, V503, V503A, V503AP, V503P, V506 and V520 propellers which have been manufactured before 6 Nov. 2002   These propellers are known to be installed on, but not limited to, the following aircraft: Zlin Z-42M, Z-42MU, Z-142, Z-43, Z-50M, Let Kunovice Ae 45, Ae-145, Z-37, Z-37A, L-200A, L-200D, Orličan L-40Propeller - Repetitive Inspections of the Propeller BladesAvia Propeller Service Bulletins No.1 issue G and No.6 issue D and issue E
032-09 PTZEASA 2009-006527.03.2009See Required Action(s) And Compliance Time(s) for DetailsEurocopter Deutschland GmbH   EC 135 and EC 635 helicoptersFuselage – Rear Structure / Tail Boom – Pre-Flight Check / InspectionEurocopter Deutschland ASB EC135-53A-022 Rev 1
033-09 PTZFAA 2009-02-0615.04.2009See AD compliance for detailsBoeing Model 737-300, -400, and -500 series airplanes, certificated in any categoryCracking in the fuselage frames and frame reinforcementsBoeing Alert Service Bulletin 737-53A1279
034-09 PTZCF-2009-0809.04.2009See AD compliance for detailsBombardier Inc. Models: CL-600-2C10,  CL-600-2D15 and CL-600-2D24Pressurization System: Cabin Pressure Control (CPC) Units and Cabin Pressure Control Panel (CPCP) DeficiencyBombardier Alert Service Bulletin (ASB) A670BA-21-022, dated 3 August 2006
035-09 PTZCF-2009-0930.03.2009See AD Corrective Actions for DetailsBombardier Inc. Model CL-600-2C10 aircraft, and CL-600-2D15/CL-600-2D24 aircraftFuel System Safety - Hydraulic System Overheat Inside the Fuel TankBombardier Service Bulletin (SB) 670BA-29-005, dated 29 January 2009
036-09 PTZCF-2009-10 EMERGENCY AD12.03.2009See AD Corrective Actions for DetailsBell Helicopter Textron Canada (BHTC) Models: 206A all S/N; 206B series all S/N including those converted from Model 206A; 206L series, all S/N; 407 and 427 all S/NCyclic Control Lever Assembly InstallationAlert Service Bulletin´s: 206-09-121 206L-09-155 407-09-85 427-09-23
037-09 PTZFAA 2009-05-0820.04.2009See AD compliance for detailsTrimble or FreeFlight Systems 2101 I/O Approach Plus global positioning system (GPS) navigation system (2101 I/O Approach Plus system)Erroneous information provided by the 2101 I/O Approach Plus systemNone
038-09 PTZEASA 2007- 0071R1   This directive revises AD 2007-007130.03.2007See Required Action(s) And Compliance Time(s) for DetailsAPEX AIRCRAFT   DR 400 series aeroplanesWings - Main spar and fabric covering - Reinforcement / Modification / InspectionAPEX AIRCRAFT Technical Instruction No 1001047 issue H   APEX AIRCRAFT Technical Instructions No.1000851 issue D and No.1001846 issue F
039-09 PTZEASA Emergency AD 2006-0067-E21.03.2009Within 5 flight hours after the effective date of this directive and no later than 27 March 2009, whichever occurs first; See Required Action(s) And Compliance Time(s) for DetailsAgusta S.p.A.   AB206 helicoptersMain Rotor – Pitch Horn Trunnion Bearing – Inspection /ReplacementAgusta Alert Bollettino Tecnico 206-245 dated 20 March 2009
040-09 PTZEASA 2006–0334R114.11.2006See Required Action(s) And Compliance Time(s) for DetailsTHALES COMMUNICATIONS VHF Data Radio, Part Numbers EVR716-11-0300A EVR716-11-0350A EVR716-01-0100A EVR716-01-0200A EVR750-03-0100A known to be installed on, but not limited to, the following aircraft: - Bombardier DHC-8-400 (all models); - Airbus A318, A319, A320, A321, A330, A340 (all models); - Boeing 717, 727, 737, 747, 757, 767, 777 (all models)Communications - Thales Communications VHF Data Radio - ModificationThales Communications Service Bulletins: EVR716-23-015   EVR716-23-012 Initial Issue or Rev. 01   EVR7-23-05 Initial Issue or Rev. 01
041-09 PTZEASA Emergency AD 2009-0068-E27.03.2009See Required Action(s) And Compliance Time(s) for DetailsTURBOMECA ARRIEL 1 and ARRIEL 2 series turboshaft enginesEngine - Module M04 (Power Turbine) Power Turbine Blades - Life Limit / ReplacementTurboméca Mandatory Service Bulletin (MSB) A292 72 0827 - version A and MSB A292 72 2833 - version A
042-09 PTZFAA 2009-07-0330.04.2009See AD compliance for detailsGeneral Electric Company (GE) CF6-80C2 and CF6-80E1 series turbofan enginesCracked HPCR spool shaft stage 14 disk websCF6-80C2 S/B 72-A1122 CF6-80E1 S/B 72-A0258
043-09 PTZFAA 2009-07-0805.05.2009See AD compliance for detailsPiper Aircraft, Inc. PA-46-350P and PA-46R-350TIncorrectly installed current limitersPiper Aircraft, Inc. Service Bulletin No. 2000
044-09 PTZCF-2009-1326.04.2009See AD Corrective Actions for DetailsBombardier Inc Model CL-600-2B19 aircraftFlap Actuator Pinion Gear – Non ConformanceNone
045-09 PTZFAA 2009-07-1207.05.2009See AD compliance for detailsGeneral Electric Company (GE) CF34-1A, -3A, -3A1, -3A2, -3B, and - 3B1 turbofan engines These engines are installed on, but not limited to, Bombardier, Inc. Airplane models CL-600-2A12, -2B16, and -2B19Inability to restart both engines after flameout due to excessive friction of the 4-step sealGE Service Bulletin (SB) No. CF34-AL S/B 72-0238 (CL-600-2B19), and SB No.CF34-BJ S/B 72-0217 (CL-600-2A12 and CL-600-2B16)
046-09 PTZEASA 2009-008120.04.2009See Required Action(s) And Compliance Time(s) for DetailsAIRBUS   A300 and A300-600 aeroplanesWings – Main Landing Gear (MLG) Rib 5 Attachment Fitting Lower Flange – Inspection / RepairA300-57-0235 original issue up to rev 05   A300-57-6088 original issue up to rev 04   A300-57A0246 Rev 03   A300-57A6101 Rev 03
047-09 PTZCF-2009-1819.05.2009Within 26 months after the effective date of this directiveBombardier Inc. Models CL-600-1A11 CL-600-2A12 CL-600-2B16Air Driven Generator (ADG) Power Feeder Harness - Wire ChafingBombardier Service Bulletin (SB) 600-0737 or 601-0591
048-09 PTZCF- 2009-1919.05.2009Within 1600 hours air time or within 18 months after the effective date of this directive, whichever comes firstBombardier Inc. Model CL-600-2B19Nose Landing Gear Selector Valve and Nose Landing Gear Door Selector Valve End Caps – Incorrect AssemblyNone
049-09 PTZCF-2009-2025.05.2009See AD Corrective Actions for DetailsBombardier Inc. Models CL-600-2C10 CL-600-2D15 and CL-600-2D24Main Landing Gear Torque Link Apex Pin DisengagementBombardier Aerospace Service Bulletin (SB) 670BA-32-019, Rev A
050-09 PTZCF- 2009-21R1 Supersedes and cancels Airworthiness Directives (AD) CF-2006-16R1 and CF-2009-2126.05.2009Within 250 hours air time or within 6 months after the effective date of this directiveBombardier Inc. Models CL-600-1A11 CL-600-2A12 CL-600-2B16 CL-600-2B16 Nose Landing Gear Selector Valve and Nose Gear Door Selector Valve End Caps – Incorrect AssemblySB 600-0721 SB 601-0558 SB 601-0558 SB 604-32-021
051-09 PTZCF-2009-2208.06.2009See AD Corrective Actions for DetailsBombardier Inc. Models CL-600-2C10 CL-600-2D15  and CL-600-2D24Landing Gear Alternate Extension System (AES) – Valve Clevis DamageAlert Service Bulletin (ASB) A670BA-32-022, Revision A
052-09 PTZCF-2009-2308.06.2009Prior to 15000 hours air time, or within the next 5000 hours air time after the effective date of this AD , whichever comes laterBombardier Inc. Models CL-600-2B19 CL-600-2C10 CL-600-2D15 and CL-600-2D24 Passenger Door CorrosionSee AD
053-09 PTZCF-2009-2408.06.2009See AD Corrective Actions Bombardier Inc. Model CL-600-2B16 Air Driven Generator (ADG) – Strut CrackingSee AD
054-09 PTZFAA 2009-08-0114.05.2009See AD compliance for detailsHoneywell NZ-2000 navigation computers and Honeywell IC-800 or IC-800E integrated avionics computers; including but not limited to the airplanes identified in Table 1 of AD (Bombardier, Dassault, Gulfstream, Lockheed, Hawker Beechcraft)Shift in the FMS computed positionSee AD
055-09 PTZFAA 2009-09-0611.06.2009See AD compliance for detailsBoeing Model 737-100, -200, -200C, -300, -400, and -500 series airplanesFatigue cracking of the backup intercostals and upper sill web of the forward airstair doorwaySee AD
056-09 PTZFAA 2009-09-0711.06.2009See AD compliance for detailsBoeing Model 737-100, -200, -200C, -300, -400, and -500 series airplanesBroken retract actuator beams of the MLGSee AD
057-09 PTZFAA 2009-08-51 Emergency AD27.05.2009See AD compliance for detailsRolls-Royce Corporation (RRC) (Formerly Allison Engine Company)Uncontained failure of the HPT stage 2 wheelSee AD
058-09 PTZFAA 2009-10-0917.06.2009See AD compliance for detailsCessna Aircraft Company See AD Applicability for modelsRudder traveling past the normal travel limitSee AD
059-09 PTZFAA 2009-10-0109.06.2009See AD compliance for detailsPratt & Whitney (PW) JT9D-7R4G2, -7R4E1, -7R4E4, and -7R4H1 series turbofan engines. These engines are installed on, but not limited to, Boeing 747-200, -300, 767-200, and Airbus A300-600 and A310-300 series airplanesUncontained failure of the 2nd stage high-pressure turbine (HPT) air seal assemblySee AD
060-09 PTZFAA 2009-11-0223.06.2009See AD compliance for detailsCFM International S.A. CFM56-2, CFM56-3, CFM56-5A, CFM56-5B,CFM56-5C, and CFM56-7B series turbofan engines. These engines are installed on, but not limited to, Airbus A319, A320, and A340 airplanes and Boeing 737 airplanesCracking of the HPC 4-9 spoolSee AD
061-09 PTZFAA 2009-10-1404.06.2009See AD compliance for detailsHartzell Propeller Inc. steel hub turbine propellers listed in Table 1 of AD. These propellers are installed on, but not limited to, the airplanes listed in Table 1 of ADSeparation of the propeller blade counterweight slugSee AD
062-09 PTZFAA 2009-07-1114.05.2009See AD compliance for detailsBoeing Model 737-300, -400, and -500 series airplanesDiscrepancies of the fuselage skinSee AD
063-09 PTZFAA 2009-12-0516.06.2009See AD compliance for detailsBoeing Model 737-300, -400, and -500 series airplanesLoss of all attitude indications from both the standby indicator and EFIS displaysSee AD
064-09 PTZFAA 2009-12-0616.06.2009See AD compliance for detailsBoeing Model 737-300, -400, and -500 series airplanes Model 737-600, -700, -700C, -800, and -900 series airplanesElectrical power to IFE systems and other nonessential electrical systems through a switch in the flight compartmentSee AD
065-09 PTZFAA 2009-13-0624.06.2009See AD compliance for detailsPiper Aircraft, Inc. PA-23, PA-31, and PA-42 Series AirplanesDamaged, worn, corroded, or non-conforming nose baggage door componentsSee AD
066-09 PTZFAA 2009-14-0412.08.2009See AD compliance for detailsBoeing Model 737-100, -200, -200C, -300, -400, and -500 series airplanesHot short between the outboard landing light and fuel shutoff valve circuitsSee AD
067-09 PTZEASA 2009-008423.04.2009See AD compliance for detailsAIRBUS SAS A310, A300-600 and A300-600ST aeroplanesEquipment / Furnishings – Pilot and Co-pilot Seats – Deactivation of Powered MovementSee AD
068-09 PTZEASA 2008-0146R1 This AD revises and replaces EASA AD 2008-014615.08.2009See AD compliance for detailsSaab AB, Saab Aerosystems SF340A and 340B aeroplanesHydraulic System – Hydraulic Accumulators – ReplacementSee AD
069-09 PTZEASA 2009-0093-E21.04.2009See Required Action(s) And Compliance Time(s) for DetailsEurocopter Deutschland GmbH EC135 and EC635 series helicopters, and MBB-BK 117 C-2 helicoptersOptional Equipment – External Mounted Hoist System – Visual Check / ReplacementSee AD
070-09 PTZEASA 2006–0140R425.05.2006See Required Action(s) And Compliance Time(s) for DetailsLufthansa Technik AG; SR Technics; Jet Aviation Basel, AG; CTT Systems AB   CTT Systems AB Zonal Drying System, Part Numbers (P/N) as listed in the Applicability of this directiveAir Conditioning - Zonal Drying System DeactivationSee AD
071-09 PTZEASA 2009-009706.05.2009See Required Action(s) And Compliance Time(s) for DetailsRockwell Collins Inc. TDR-94 and TDR-94D transpondersNavigation – Mode S Transponder – Check / ModificationSee AD
072-09 PTZEASA 2009-0088R108.05.2009See Required Action(s) And Compliance Time(s) for DetailsCFM International SA (CFM)   CFM56-5B turbofan enginesEngine – High Pressure Compressor (HPC) – Inspection / ReplacementSee AD
073-09 PTZEASA 2009-0055R127.03.2009See Required Action(s) And Compliance Time(s) for DetailsAIRBUS SAS   A310, A300-600 and A300-600ST aeroplanesElectrical Power – Engine Feeder Harness – Inspection & Nacelles/Pylons – GE CF6-80C2 Pylon Forward Pyramid – InspectionSee AD
074-09 PTZEASA 2009-0106-E02.05.2009See Required Action(s) And Compliance Time(s) for DetailsEurocopter Deutschland GmbH EC135 and EC635 helicoptersMain Rotor Drive – Main Gearbox (MGB) Oil Sampling & Analysis Program – AmendmentSee AD
075-09 PTZEASA 2007-0241R307.09.2007See Required Action(s) And Compliance Time(s) for DetailsPilatus Aircraft Ltd. PC-6 series aeroplanesWing – Wing Strut Fitting – Inspection / ReplacementSee AD
076-09 PTZEASA 2009-011021.05.2009See Required Action(s) And Compliance Time(s) for DetailsCFM International SA   CFM56-5B turbofan enginesTime Limits – Low Pressure Turbine Rear Frame – Life Limit / Mandatory InspectionSee AD
077-09 PTZEASA 2009-011127.05.2009See Required Action(s) And Compliance Time(s) for DetailsAIRBUS   A300 aeroplanesFlight Controls – Trimmable Horizontal Stabilizer Actuator (THSA) – Check / ReplacementSee AD
078-09 PTZEASA 2009-009405.05.2009See Required Action(s) And Compliance Time(s) for DetailsAIRBUS A300 and A300-600 aeroplanesFuselage / Wings – Frame 40 Forward Fitting between Stringers 32 and 33 – Inspection / RepairSee AD
079-09 PTZEASA 2009-013707.07.2009See Required Action(s) And Compliance Time(s) for DetailsAgusta S.p.A.   A109E helicoptersElectrical Power – Battery Bus (BATT BUS) Circuit Breaker – ModificationSee AD
080-09 PTZEASA 2009-012224.06.2009See Required Action(s) And Compliance Time(s) for DetailsEUROCOPTER   EC 120, AS 350, EC 130, AS 355, AS 365, EC 155, SA 330, AS 332 and EC 225 HelicoptersEquipment / Furnishings –Load Release Units – Inspection / Modification / LimitationSee AD
081-09 PTZEASA 2009-013607.07.2009See Required Action(s) And Compliance Time(s) for DetailsTurboméca   ASTAZOU XIV turboshaft enginesEngine Rotating Assembly – Third Stage Turbine Wheel – Inspection / RemovalSee AD
082-09 PTZEASA 2009-014116.07.2009See Required Action(s) And Compliance Time(s) for DetailsAIRBUS   A318, A319, A320 and A321 aeroplanesStabilizers – Rudder Side Shell Skin – InspectionSee AD
083-09 PTZEASA 2009-0148-E11.07.2009See Required Action(s) And Compliance Time(s) for DetailsAgusta S.p.A, Eurocopter, Eurocopter Deutschland GmbH, Sikorsky Aircraft Corporation   A109 series and AB139/ AW139, AS332, AS350 and AS355 series, EC225, SA330, SA365, AS365 and EC155 series, SA360, EC135, MBB-BK 117, BO 105 series, S-61 helicoptersEquipment / Furnishings – D-Lok Hook of the Rescue Hoist – Inspection / Removal from Service / ReplacementSee AD
084-09 PTZEASA 2009-015124.07.2009See Required Action(s) And Compliance Time(s) for DetailsThielert Aircraft Engines GmbH   TAE125-02-99 enginesEngine/Propeller – Constant Speed Unit – Propeller Control Valve – Vibration IsolatorSee AD
085-09 PTZEASA 2009-0154-E17.07.2009See Required Action(s) And Compliance Time(s) for DetailsCFM International SA   CFM56-5B turbofan enginesEngine Fuel and Control - Hydromechanical Unit (HMU) – Inspection/ReplacementSee AD
086-09 PTZEASA 2009-015731.07.2009See Required Action(s) And Compliance Time(s) for DetailsAIRBUS   A300 aeroplanesElectrical Power – Fuel Pump Wiring – Modification [Prevention against Fuel Tank Explosion Risks]See AD
087-09 PTZEASA 2009-015531.07.2009See Required Action(s) And Compliance Time(s) for DetailsAIRBUS SAS   A300, A310 and A300-600 aeroplanesTime Limits / Maintenance Checks – Damage Tolerant Airworthiness Limitation Items – ALS Part 2 – AmendmentSee AD
088-09 PTZEASA 2009-015731.07.2009See Required Action(s) And Compliance Time(s) for DetailsAIRBUS   A300 aeroplanesElectrical Power – Fuel Pump Wiring – Modification [Prevention against Fuel Tank Explosion Risks]See AD
089-09 PTZEASA 2009-016028.07.2009See Required Action(s) And Compliance Time(s) for DetailsExtra Flugzeugproduktions- und Vertriebs- GmbH EA 300 aeroplanesFuselage Structure – Tail Spring Support – Inspection / ModificationSee AD
090-09 PTZEASA 2008-0145R115.08.2008See Required Action(s) And Compliance Time(s) for DetailsThielert Aircraft Engines GmbH   TAE125 enginesPropellers – Propeller Control Valve – Replacement (Life Limit)See AD
091-09 PTZEASA Emergency AD 2009-0163-E31.07.2009See Required Action(s) And Compliance Time(s) for DetailsDG Flugzeugbau GmbH   DG-100 series sailplanesFlight Controls - Elevator Control Bearing Stand – Inspection / ModificationSee AD
092-09 PTZEASA Emergency AD 2009-0167-E03.08.2009See Required Action(s) And Compliance Time(s) for DetailsDG Flugzeugbau GmbH   DG-100 series and DG-200 series sailplanesFlight Controls - Control Column Rod End -Inspection / ReplacementSee AD
093-09 PTZEASA Emergency AD 2009-0169-E03.08.2009See Required Action(s) And Compliance Time(s) for DetailsDG Flugzeugbau GmbH   DG-500 MB and DG-800 B Powered SailplanesStarting - Zinc Coated Starter Ring Gears - Inspections / ReplacementSee AD
094-09 PTZEASA 2009-014311.08.2009See Required Action(s) And Compliance Time(s) for DetailsAIRBUS SAS   A300-600 aeroplanesFuel System – Fuel Tank Electrical Bonding – Inspection / Modification [Fuel Tank Safety]See AD
095-09 PTZEASA 2009-016514.08.2009See Required Action(s) And Compliance Time(s) for DetailsAIRBUS SAS   A300, A310 and A300-600 aeroplanesFuselage – Frame (FR) 15A Nose Landing Gear (NLG) Crossbeam – Inspection/RepairSee AD
096-09 PTZEASA 2009-016614.08.2009See Required Action(s) And Compliance Time(s) for DetailsAIRBUS   A310 and A300-600 aeroplanesStabilizers – Rudder Side Shell Skin – InspectionSee AD
097-09 PTZEASA 2009-017319.08.2009See Required Action(s) And Compliance Time(s) for DetailsRockwell Collins Inc.   TDR-94 and TDR-94D transpondersNavigation – Mode S Transponder – Modification / ReplacementSee AD
098-09 PTZCF-2009-2729.07.2009See AD Corrective ActionsBombardier Inc. Models CL-600-2B19 CL-600-2C10 CL-600-2D15 CL-600-2D24Air Driven Generator (ADG) – Strut CrackingSee AD
099-09 PTZCF-2009-2820.07.2009Within 6000 hours air time after the effective date of this directiveBombardier Inc. Models CL-600-2C10 CL-600-2D15 CL-600-2D24Elevator Oscillation Due To Elevator Control Rod DisconnectSee AD Corrective Actions
100-09 PTZCF-2009-3027.07.2009Within 5 000 hours air-time after the effective date of this directiveBombardier Inc. Models CL-600-2C10 CL-600-2D15 CL-600-2D24Aft Baggage Cargo Compartment – Blowout Panel Protective Cages DamageBombardier Service Bulletin (SB) 670BA-25-071, dated 15 May 2009
101-09 PTZCF-2009-3129.07.2009Within 60 days after the effective date of this directiveBombardier Inc. Model CL-600-2B19Bulkhead Check Valves – Periodic Discard TaskSee AD Corrective Actions
102-09 PTZCF-2003-05R2 Supersedes AD CF-2003-05R1 issued 7 February 200629.07.2009See AD Corrective ActionsBombardier Inc. Model CL-600-2B19Air Supply Ducts and Bulkhead Check Valve – InspectionsSee AD Corrective Actions
103-09 PTZCF-2009-3210.08.2009Within the next 10 flight hours, but not later than 30 calendar days from the effective day of this directiveBell Helicopter Textron Canada (BHTC) Helicopter Models: 206A, 206B, 206L, 206L-1, 206L-3, 206L-4, 222, 222B, 222U, 230, 407, 427, 430Bearings in Flight ControlsSee AD Corrective Actions for list
104-09 PTZCF-2009-3318.08.2009Within 5000 hours air time or 24 months after the effective date of this directive, whichever comes first, See AD Corrective ActionsBombardier Inc. Models CL-600-2C10 CL-600-2D15 CL-600-2D24Thrust Reverser – Transcowl Assembly CrackingSee AD Corrective Actions
105-09 PTZFAA 2009-16-0309.09.2009See AD compliance for detailsTeledyne Continental Motors (TCM) IO-520, TSIO-520, and IO-550 series reciprocating engines with SAP investment cast cylinder assemblies, certain part numbers (P/Ns) installed. These engines are installed on, but not limited to, the airplanes listed in Table 1 of this AD(Cessna, Rockwell, Beechcraft, Bellanca)Separation of the cylinder headTeledyne Continental Service Bulletin No. SB03-3
106-09 PTZFAA 2009-16-1409.09.2009See AD compliance for detailsBoeing Model 737-100, -200, -200C, -300, -400, and -500 series airplanesFatigue cracking of the intercostals on the forward and aft sides of the forward entry doorBoeing Alert Service Bulletin 737-53A1204, Rev 1
107-09 PTZEASA 2009-017119.08.2009See Required Action(s) And Compliance Time(s) for DetailsAIRBUS A300, A310, A300-600 and A300-600ST aeroplanesFire Protection / Hydraulic Power - Air Pressurisation Check Valves – Identification / ReplacementAIRBUS Service Bulletins: A300-29-0124 Rev 02 A310-29-2097 Rev 01 A300-29-6060 Rev 01 A300-29-9009 Rev 02