PTZ-AD 2008

Številka PTZReferenčna PTZDatum efektiveRok izvršitveProizvajalecVsebina PTZReferenčni SB
001-08 PTZCF-2008-0124.01.2008Within 4500 hours air time after the effective date of this directive, modify the fuel tank climb vent loop pipes; See AD for detailsBombardier Inc. Model CL-600-2C10 aircraft, serial numbers 10003 through 10169 and CL-600-2D24 aircraft, serial numbers 15001 through 15025Fuel System Safety - Fuel Tank Climb Vent Loop Fuel Leak onto Anti-Ice DuctBombardier Service Bulletin (SB) 670BA-28-011, Revision B, dated 4 July 2007
002-08 PTZCF-2008-0224.01.2008Within 4500 hours air time after the effective date of this directive; See AD for detailsBombardier Inc. Model CL-600-2C10 aircraft, serial numbers 10003 through 10169 and CL-600-2D24 aircraft, serial numbers 15001 through 15025Fuel System Safety -Insufficient Electrical Bonding Between Fuel Tubes and Insufficient Lightning Current Capability of Fuel Tube CouplingsBombardier SB 670BA-28-014, Revision A, dated 7 May 2007
003-08 PTZFAA 2007-26-1218.01.2008Within 10 hours time-in-service (TIS), unless accomplished previously; Before further flight, replace any unairworthy blade with an airworthy Robinson Helicopter Company Model R22, R22 Alpha, R22 Beta, R22 Mariner helicopters, serial numbers 0002 through 4100; R44 helicopters, serial numbers 0001 through 1670; and R44 II helicopters, serial numbers 10001through 11570, certificated in any categoryDetect main rotor blade skin debond and prevent blade failure and subsequent loss ofcontrol of the helicopterRobinson R22 Service Letter SL-56 and R44 Service Letter SL-32and ADDITIONAL INFORMATION REGARDING MAIN ROTOR BLADE SKIN DEBONDING
004-08 PTZUK G-2008-0001-E Emergency AD12.01.2008Before further flight; See AD compliance for detailsLINDSTRAND HOT AIR BALLOONS LTD (LHAB)  ALL LINDSTRAND HOT AIR BALLOONS with  Burner hoses manufactured by FlexquipFUEL HOSES - REPLACEMENT OF DEFECTIVE HOSESLHAB Service Bulletin No 11.
005-08 PTZEASA Emergency AD 2007-0306-E18.12.2007See AD compliance for detailsAgusta S.p.A.  A109E, A109K2 and A109C HelicoptersRotor - Main Rotor Blade Tip Cap p/n 709-0103-29-109 –InspectionAgusta - Alert Service Bulletins 109EP-85, 109K-48 and 109-25
006-08 PTZUK G-2008-0002Emergency AD16.01.2008Before further flight; See AD compliance for detailsCAMERON BALLOONS LIMITED (CBL)   All Cameron Balloons with gas cylinders supplied by CBL balloons which have a CB-0824-0001 Rego Type Cylinder Liquid Valve fitted which is date stamped between 12/05 and 08/06Defective inlet self seal valvesCameron Balloons Service Bulletin 16 and Service Bulletin 17
007-08 PTZEASA 2007 - 0067R127.03.2007See AD compliance for detailsAIRBUS SAS A319 and A320 series aircraftWings – Centre and Outer Wing Box at level of Rib 1 Junction – InspectionSee AD Ref. Publications for list
008-08 PTZCF-2007-3410.01.2008See AD compliance for detailsBombardier Inc. Model CL-600-2B19 aircraft, serial numbers 7003 through 7067, and 7069 through 7929Fuel System Safety - Insufficient Electrical Bonding for Lightning Protection Inside Fuel TanksBombardier Service Bulletin (SB) 601R-28-055, Revision D
009-08 PTZCF-2007-3510.01.2008See AD compliance for detailsBombardier Inc. Model CL-600-2B19 aircraft, all serial numbersFuel System Safety - Introduction of Critical Design Configuration Control LimitationsSee AD for details
010-08 PTZCF-2007-3611.01.2008Within 10,000 hours air time after the effective date of this AD; See AD compliance for detailsBombardier Inc. Model CL-600-2B19 aircraft, serial numbers 7003 through 7067, 7069 through 7982Fuel System Safety - Chafing of Fuel Quantity Gauging System WiringBombardier Service Bulletin (SB) 601R-28-059, Rev E
011-08 PTZCF-2007-24R1Supersedes Airworthiness Directive (AD) CF-2007-2410.01.2008See AD compliance for detailsPratt & Whitney Canada PW206 and PW207 Compressor Turbine (CT) DiskPW 200 Compressor Turbine Disk Inspection and Retaining Nut ReplacementAlert Service bulletin PW200-72-A28280 R4
012-08 PTZEASA 2008-001605.02.2008Within the next 110 Flight Hours (FH) or 6 months or during the next scheduled maintenance, whichever occurs first after the effective date ofthis AD; See AD Thielert Aircraft Engines TAE125-01 engines, all serial numbers   These engines are known to be installed on, but not limited to, Cessna 172 and (Reims-built) F172 series (EASA STC Nr. EASA.A.S.01527); Piper PA-28 series (EASA STC Nr. EASA.A.S.01632), APEX (Robin) DR 400 series (EASA STCNr. EASA.A.S.01380); and Diamond DA40 and DA42 Engine Oil System – Piston Cooling Nozzles – InspectionThielert Service Bulletin TM TAE125-0017
013-08 PTZEASA 2008-001807.02.2008See AD compliance for detailsTURBOMECA ARRIUS 2B1, ARRIUS 2B1A, ARRIUS 2B2, ARRIUS 2K1 and ARRIUS 2K2 engines, all serial numbersThese engines are known to be installed on, but not limited to, Eurocopter Deutschland EC135 and Agusta A109 twin-engine helicoptersEngine Fuel & Control – Electronic Engine Control (EEC) Unit –Identification / ModificationTURBOMECA Service Bulletin N° 319 73 2835, Update No.1
014-08 PTZFAA 2008-02-0626.02.2008See AD compliance for detailsGARMIN International   GSM 85 servo gearbox units These units are installed in, but notlimited to: Cessna Aircraft Company 182T, T182T, 206H, and T206H Hawker Beechcraft Corporation G36 and G58 Diamond Aircraft Industries GmbH DA40 and DA40F Columbia Aircraft Manufacturing 350 and 400Mooney Airplane Company, Inc. M20M and M20RDetect and correct defectiveGARMIN GSM 85 servo gearbox units, which could result in jamming of the servo gearboxGARMIN International, Inc. Service Bulletin No. 0713, Revision A, B, C, D   CessnaAircraft Company Single Engine Service Bulletin SB07-22-01
015-08 PTZFAA 2008-02-1828.02.2008Within the next 25 hours time-in-service afterFebruary 28, 2008; See AD compliance for detailsCessna Aircraft Company: Cessna 172 Models Cessna 182 Models equipped with: BRS-172 Parachute System installed via STC No. SA01679CH, orBRS-182 Parachute System installed via STC No. SA01999CHPrevent premature separation of the collar. Thiscondition could result in the parachute failing to successfully deploy.For Cessna 172 series airplanes follow BRS SB 07-01   For Cessna 182 series airplanes, followBRS SB 07-02
016-08 PTZUK G-2008-000318.01.2008See AD compliance for detailsDowty PropellersPropeller Electronic Controller Part No. 699018002PROPELLER ELECTRONIC CONTROLLER - UNIT REMOVALDowty Propellers Alert Service Bulletin D8400-61-A77
017-08 PTZCF-2008-0715.02.2008Within 60 days after the effective date of this directive; See AD compliance for detailsBombardier Inc. Model CL-600-2C10, CL-600-2D15 and CL-600-2D24 aircraft, all serial numbersFuel System Safety - Introduction of Critical Design Configuration Control LimitationsSee AD for details
018-08 PTZEASA 2008-002212.02.2008Within 30 days after the effective date of this AD; See AD compliance for detailsSaab AB, Saab Aerosystems (formerly Saab Aircraft AB) Model SF340A and 340B [including variant 340B (WT)] aircraft, all serial numbersIce & Rain Protection – Flight in Icing Conditions /Airplane Flight Manual – AmendmentSAAB SF340A Airplane Flight Manuals Doc.No: AFM 340A 000, AFM 340A 001, AFM 340A 003   SAAB 340B Airplane Flight Manuals Doc.No: AFM 340B 000, AFM 340B 001, AFM 340B 003, AFM 340B 010
019-08 PTZFAA 2008-03-0206.03.2008Within the next 100 hours time-in-service (TIS) after March 6, 2008 or within the next 12 months after March 6,2008, whichever occurs first; See AD compliance for detailsCessna Aircraft Company   172R172SDetect and correct chafing of the fuel return line assembly, which could resultin fuel leaking under the cabin floor and fuel vapors entering the cabin. This condition could lead to fire under the floor or in the cabin areaCessna Service Bulletin SB07-28-01, datedJune 18, 2007
020-08 PTZFAA 2008-03-0910.03.2008See AD compliance for detailsCFM International, S.A.   CFM56-7B18, -7B20, -7B22, -7B24, -7B26, - 7B27, -7B22/B1, -7B24/B1, -7B26/B1, -7B27/B1, -7B22/B2, -7B26/B2, -7B27/B3 turbofan engines with turbine rear frame (TRF), part numbers 340-166-205-0, 340-166-206-0, 340-166-207-0, 340-166-208-0, 340-166-209-0, and 340-166-210-0, installed. These engines are installed on, but not limited to, Boeing 737 series airplanesPrevent failure of the TRF from low-cycle fatigue cracks. Failure of the TRF could result in engine separation fromthe airplane, which could lead to loss of control of the airplaneCFM International Service Bulletin CFM56-7B S/B 72-0579, Rev 1
021-08 PTZFAA 2008-03-1011.03.2008Within the next 90 days after March 11, 2008 (the effectivedate of this AD); See AD compliance for detailsCessna Aircraft CompanyModels 525, 525A and 525BDetect and correct any damage from corrosion on the airplane structure. Corrosion of the airplane structure could cause structural degradation and lead to structuralfailure of the airplane with consequent loss of control.See Table 2 for list of SB´s
022-08 PTZFAA 2008-03-1211.03.2008See AD compliance for detailsMcDonnell Douglas Model DC-8-11, DC-8-12, DC-8-21, DC-8-31, DC-8-32, DC-8-33, DC-8-41, DC-8-42, and DC-8-43 Airplanes; Model DC-8F-54 and DC-8F-55 Airplanes; Model DC-8-50, -60, -60F, -70, and -70F Series Airplanes; Model DC-9-10, -20, -30, - 40, and -50 Series Airplanes; Model DC-9-81 (MD-81), DC-9-82 (MD-82), DC-9-83 (MD-83),and DC-9-87 (MD-87) Airplanes; and Model MD-88 AirplanesPrevent failure of the rudder pedal bracket assembly, which could result in the loss of rudder and brakingcontrol at either the captain's or first officer's positionSee Table 2
023-08 PTZFAA 2008-03-1611.03.2008See AD compliance for detailsCirrus Design Corporation   Model SR20 airplanes, serial numbers (SN) 1005 through 1861, and Model SR22 airplanes, SN 0002 through 2333, SN 2335 through 2419, and SN 2421 through 2437,that are certificated in any categoryPrevent the possibility of jamming of the rudder-aileroninterconnect system, which may result in loss of rudder and aileron flight controlsCirrus Service Bulletin No. SB 2X-27-14 R3, Revised:October 10, 2007
024-08 PTZFAA 2008-02-1906.03.2008See AD compliance for detailsHoneywell International Inc. (formerly AlliedSignal Inc. and Garrett Turbine Engine Co.) TFE731-2C, -3B, -3BR, -3C, - 3CR, -3D, -3DR, -4R, -5AR, -5BR, -5R, -20R, -20AR, -20BR, -40, -40AR, -40R, and -60 series turbofan engines with certain high pressure (HP) turbine rotor discs part numbers and serial numbers These engines are installed on, but not limited to the airplanes listed in AD applicabilityPrevent uncontained failure of the HP turbine rotor assembly, which could result indamage to the airplaneHoneywell Alert SB No. TFE731-A72-5185, dated July 5, 2006, andSB No. TFE731-72-3720, dated July 5, 2006
025-08 PTZFAA 2008-03-2017.03.2008Within 60 months after the effective date of this AD, modify the door-mounted escape system of the forward right side door slide compartment, in accordance with the AccomplishmentInstructions of Boeing Special Attention Service Bulletin 737-25-1567, dated March 21, 2007; See AD for detailsBoeing Model 737-300, -400, and -500 series airplanesPrevent the escape slide from being unusable during an emergency evacuation and consequentinjury to passengers or crewmembersBoeing Special Attention Service Bulletin 737-25-1567, dated March 21, 2007
026-08 PTZCF-2008-0807.02.2008See AD for detailsPratt & Whitney Canada (P&WC) - PW305A and PW305B engines certain serial numbersEngine Fan Blade FractureAlert Service Bulletin (ASB) No. A24588 Special Instructions (SI) No.37-2007. ASB No. A24588R2Service Bulletin (SB) No. 24595
027-08 PTZCF-2008-0918.02.2008See AD for detailsBombardier Inc. Model: CL-600-2B19 – Serial numbers 7305 through 7990 and 8000 and subsequentAir-Driven Generator – Internal WiringBombardier Aerospace Service Bulletin 601R-24-113, original issue, dated 22 April 2004, or Revision A, dated 11 August 2005
028-08 PTZCF-2008-1019.02.2008See AD for detailsBombardier Inc. Models: CL-600-2C10 – Serial numbers 10004 and subsequent. CL-600-2D15 and CL-600-2D24 – Serial numbers 15002 and subsequentAir-Driven Generator – Internal WiringBombardier Aerospace Service Bulletin 670BA-24-015, dated 17 May 2004, or Revision A, dated 18 December 2006
029-08 PTZCF-2008-1225.02.2008Within 30 days of the effective date of this AD; See AD for detailsBombardier Inc. CL-600-1A11 (CL-600) CL-600-2A12 (CL-601) CL-600-2B16 (CL-601-3A/3R)CL-600-2B16 (CL-604)Stick Pusher Capstan Shaft FailureSee AD
030-08 PTZEASA Emergency AD 2008-0027-E13.02.2008Total Engine Time below 20h: before achieving 30 hours total engine time or at the next engine inspection, whichever occurs first   Total Engine Time above 20h: within the next 10 flight hours or at the next engine inspection, whichever occurs first;See AD for detailsThielert Aircraft Engines   TAE125-02-99 (CENTURION 2.0) engines   These engines are known to be installed on, but not limited to, Cessna 172and (Reims-built) F172 series Piper PA-28 series, APEX (Robin) DR 400 series and Diamond DA40 and DA42 aircraftEngine Fuel Injection System – High-Pressure Fuel Line Bracket – InstallationThielert Aircraft Engines Service Bulletin TM TAE 125-1005 P1, Revision 1dated 11 February 2008
031-08 PTZCF-2007-25R1 Supersedes Airworthiness Directive CF-2007-25 (132-07 PTZ)29.10.2007See AD CorrectiveActions for detailsPratt & Whitney Canada (P&WC) PW305A and PW305B Engine High Pressure Compressor (HPC) Drum Rotor CracksPW305A and PW305B Engine High Pressure Compressor (HPC) Drum Rotor CracksSB PW300-72-24462; SB PW300-72-24376; SIL PW300-093 andPW305-MM-05-20-00 requirements
032-08 PTZEASA Emergency AD 2008-0028-E15.02.2008Within the next 25 Flight Hours (FH) or within 30 days after the effective date of this AD, whichever occurs first. Repeat thereafter,inspections at intervals not to exceed 100 FH. See AD compliance for detailsCostruzioni Aeronautiche TECNAM S.r.l. Model P92-JS; from serial number (s/n) 013 up to s/n 068 inclusiveStabilizers – Vertical Fin Spar - InspectionCostruzioni Aeronautiche TECNAM S.r.l. SB 006-CS
033-08 PTZEASA 2008-003304.03.2008At the next scheduled 1600 Flight Hours (FH) aircraft check after the effective date of this AD, or after any blade accumulates 15 000 FH time inservice, whichever occurs later, and thereafter at intervals not to exceed 1600 FH, inspect the blade outer sleeves for cracks; See AD compliance for detailsDowty Propellers (part of GE Aviation Systems) R354, R375, R389 and R390 propellersThese propellers are known to be installed on Saab SF340A and 340B aircraftPropellers – Blade Outer Sleeve - InspectionDowty Propellers Alert Service Bulletin No. SF340-61-A106
034-08 PTZEASA 2008-003405.03.2008Before 31 May 2009; See AD compliance for detailsAIRBUS (formerly AIRBUS INDUSTRIE)A318, A319, A320 and A321 aircraftHydraulic Power – Auxiliary Hydraulic Power – Ram AirTurbine (RAT) Gerotor Pump - ReplacementAIRBUS Service Bulletin A320-29-1122 original issue
035-08 PTZCF-2008-1410.03.2008See AD compliance for detailsBombardier Inc. Models CL-600-2C10 – Serial numbers 10004 and subsequent. CL-600-2D15 and CL-600-2D24 – Serial numbers 15002 and subsequentAir Driven Generator Power Centre - ContactorsBombardier Aerospace Service Bulletin 670BA-24-021
036-08 PTZEASA 2008-003206.03.2008See AD compliance for detailsAIRBUSA318, A319, A320 and A321 aircraftIndicating Systems- Electronic Instrument System (EIS) – Display Management Computer (DMC) Software EIS2 StandardS7 / InstallationAIRBUS Service Bulletin A320-31A1220 AIRBUS Service Bulletin A320-31-1263AIRBUS Service Bulletin A320-31-1276
037-08 PTZENAC Emergency AD 2008-6220.20.2008Before the next flight of the helicopter with the rescue hoist installed or before the installation on the helicopter of the rescue hoists and/or for the hooks stored as spare parts, after the effective date of this AD inspect the hook of the rescue hoist in accordance with the instructions of the Agusta Alert BT 412-124.However the inspection of spare parts must be done not later then 31.March.2008Agusta S.p.A.AB412 (series) and AB412EPRescue hoist P/N BL-10300-60 and P/N 412-8800-01-315 – inspection of hook P/N S6150-61090-1and P/N 412-8800-05-101Alert BT Agusta 412-124
038-08 PTZEASA 2008-0016 R1This AD revises and replaces AD 2008-0016 (012-08 PTZ)05.02.2008Within the next 110 Flight Hours (FH) or 6 months or during the next scheduled maintenance, whichever occurs first after the effective date ofthis AD; Thereafter, at intervals not to exceed 100 FH (+/- 10 FH); See AD compliance for detailsThielert Aircraft EnginesTAE125-01 enginesEngine Oil System – Piston Cooling Nozzles – InspectionThielert Service Bulletin TM TAE125-0017 dated 14 December 2007
039-08 PTZFAA 2008-05-0103.04.2008Within 2,200 flight hours after the effective date of this AD, but not to exceed 24 months after the effective date of thisAD; See AD compliance for detailsGeneral Electric Company (GE) CF34-8C1/-8C5/-8C5B1/-8E5/-8E5A1 turbofan engines GE CF34-10E series turbofan engines This engines are installed on, but not limited to, BombardierInc. Model CL-600-2C10 (CRJ-700 & -701), and CL-600-2D24/-2D15 (CRJ-900) airplanes; Embraer ERJ 170- 100/ -200 series airplanes and Embraer ERJ 190-100/- 200 series airplanesPrevent the engine from failing to shutdown during an overspeed which may lead to uncontained engine failureSee Table 1- Incorporation by Reference
040-08 PTZFAA 2008-05-0908.04.2008Within the next 50 hours time-inservice after April 8, 2008 or within the next 6 months after April 8,2008 whichever occurs firstCessna Aircraft CompanyCertain S/N of Models: 172R, 172S, 182T, T182T, 206H, T206H Prevent failure of the seat base/back attach brackets, which could result in the seats collapsing backwards during flight with consequent loss of controlCessna Aircraft Company Service Bulletin SB07-25-04, dated April 23,2007
041-08 PTZFAA 2008-05-0208.04.2008See AD compliance for detailsEmpresa Brasileira de Aeronautica S.A. (EMBRAER) Model EMB-135BJ, -135ER, -135KE, -135KL, -135LR, -145, -145ER, -145MR, -145LR, -145XR, -145MP, and -145EP airplanes; certificated in any categoryPrevent failure of multiple hinge fittings, which could result in severe vibration, and to prevent failure of the rudder control rods, which could result in jamming of the rudder II; and possible structuralfailure and reduced controllability of the airplaneSee Table 1 and Table 2
042-08 PTZFAA 2008-04-2103.04.2008Before the accumulation of 20,000 total flight hours, or within 7,000 flight cycles after theeffective date of this AD, whichever occurs later; See AD compliance for detailsBoeing Model 737-300, -400, and -500 series airplanes, certificated in anycategory; as identified in Boeing Service Bulletin 737-57-1210, Revision 2, dated June 13, 2007Prevent failure of the main deck floor beams at certain body stations due tofatigue cracking, which could result in rapid decompression of the airplaneBoeing Service Bulletin 737-57-1210, Revision 2, dated June 13, 2007
043-08 PTZFAA 2008-05-0608.04.2008See AD compliance for detailsBoeing Model 737-100, -200, -300, -400, and -500 series airplanes, certificated in any category; as identified in Boeing Service Bulletin 737-57-1296, dated June 13, 2007Detect and correct fatigue cracking of the upper and lower chords and web of the longitudinal floor beams, which could result in rapidloss of cabin pressureBoeing Service Bulletin 737-57-1296, dated June 13, 2007
044-08 PTZEASA 2008-003812.03.2008See AD compliance for detailsMoravan Aviation s.r.o. (formerly Moravan n.p, Moravan a.s, MORAVAN - AEROPLANES a.s) Z 143L aircraft variant, all serial numbers, certificated in any categoryCarburettor Heating System - Vortex Inserts in the Heat Exchanger -Inspection / ReplacementMoravan Aviation Mandatory Service Bulletin Z143L/31a original issue;Revision No. 9 to Airplane Maintenance Manual, Doc. No. 005.022.1 (English Version)
045-08 PTZEASA 2008- 004412.03.2008See AD compliance for detailsEUROCOPTER (formerly EUROCOPTER-FRANCE, AEROSPATIALE)AS 350 and AS 355 helicoptersEquipment / Furnishings - Rear Bench Seat and Sliding Doors -Limitation / Removal / ModificationEUROCOPTER AS 350 Service Bulletin No. 25.00.70 original issue;EUROCOPTER AS 355 Service Bulletin No. 25.00.66 original issue
046-08 PTZEASA 2008-004613.03.2008Before further flight after the effective date of this AD, modify the AFM; See AD compliance for detailsMoravan Aviation s.r.o (formerly Moravan n.p, Moravan a.s, Moravan –Aeroplanes a.s)Z 43 and Z 143L aeroplanes, all serial numbersAirworthiness Limitations - Permissible Aerobatic manoeuvres inUtility category - ModificationMORAVAN Aviation Mandatory Service Bulletins Z43/46a initial issue and Z143L/29a initial issue
047-08 PTZEASA 2008- 004813.03.2008Before 30 September 2009; See AD compliance for details Before 30 September 2009; See AD compliance for details Landing Gear – Braking and Steering Control Unit (BSCU) –Modification / ReplacementAIRBUS Service Bulletin A320-32-1336 original issue
048-08 PTZEASA 2008-003921.03.2008See AD compliance for detailsCentre Est Aéronautique, Avions Pierre ROBIN, Constructions Aéronautiques de Bourgogne (CAB), APEX INDUSTRIESAPEX AIRCRAFT DR400DC generation - Voltage regulator and IFR & Night-VFR operations -Modification / RestrictionsAPEX AIRCRAFT SB No.070306 Revision 1
049-08 PTZEASA 2008- 005119.03.2008No later than 31 December 2009; See AD compliance for detailsAIRBUS (formerly AIRBUS INDUSTRIE)A318, A319, A320 and A321 aircraftFuel / Electrical Power - Prevention of Fuel Tank ExplosionRisks - Electrical Cables - ModificationAIRBUS Service Bulletin A320-24-1062 Revision 6
050-08 PTZEASA 2008-005419.03.2008Within the next 6 months after the effective date of this AD, and thereafter atintervals not to exceed 2 years; See AD compliance for detailsSaab AB, Saab AerosystemsSAAB SF340A and 340B aircraftLanding Gear – Emergency Extension Valve – Functional CheckSAAB SB 340-32-136 dated 9 January 2008; andSAAB 340 Maintenance Review Board (MRB) Report, Section F, Revision 6
051-08 PTZEASA 2008-0056-E   This AD is superseded by EASA Emergency AD 2008-0056R1-E (PTZ 054-08)10.03.2008Before next flight;See AD compliance for detailsThielert Aircraft Engines TAE125-02-99 engines   These engines are known to be installed on, but not limited to, Cessna 172and (Reims-built) F172 series (EASA STC Nr. EASA.A.S.01527); Piper PA-28 series (EASA STC Nr. EASA.A.S.01632), APEX (Robin) DR 400 series (EASA STC Nr. EASA.A.S.01380); and Diamond DA40 and DA42 aircraftEngine Fuel Injection System – High-Pressure Fuel Line Bracket –InstallationThielert Aircraft Engines Service Bulletin TM TAE 125-1005 P1, Revision 2dated 06 March 2008
052-08 PTZCF-2008-15TRANSPORT CANADA EMERGENCY AD10.03.2008See AD CorrectiveActions for detailsAll Bombardier Inc. Model CL-600-2B19 “Regional Jet” aircraftEnhancement to Takeoff Operational Safety MarginsAircraft Flight Manual (AFM) Temporary Revision (TR)RJ/155-2, dated 07 March 2008
053-08 PTZCF-2008-16TRANSPORT CANADA EMERGENCY AD12.03.2008See AD CorrectiveActions for detailsAll Bombardier Inc. CL-600-1A11, CL-600-2A12 and CL-600-2B16 aircraftEnhancement to Takeoff Operational Safety MarginsSee AD CorrectiveActions for details
054-08 PTZEASA Emergency AD 2008-0056R1-E  This AD supersedes EASA AD 2008-0027-E (051-08 PTZ)10.03.2008Before next flight; See AD compliance for detailsThielert Aircraft Engines TAE125-02-99 engines   These engines are known to be installed on, but not limited to, Cessna 172 and (Reims-built) F172 series, Piper PA-28 series, APEX (Robin) DR 400 series, and Diamond DA40 and DA42Engine Fuel Injection System – High-Pressure Fuel Line Bracket –InstallationThielert Aircraft Engines Service Bulletin TM TAE 125-1005 P1, Rev. 1 and Thielert Aircraft Engines Service Bulletin TM TAE 125-1005 P1, Rev. 2
055-08 PTZSwedish Civil Aviation Authority AD 1-20101.03.2008To be performed within three months from the effective date of this ADFOLA Airsafe life vests type A-190 or A-290Inspection of the zipper on the life vest valiseFOLA Airsafe Service Bulletin 9-387 rev. A or later revision
056-08 PTZEASA 2006-0316 R1 This AD revises and replaces EASA Emergency AD 2006-0316-E (PTZ 103-06)17.10.2006See AD compliance for detailsBRP-Rotax GmbH & Co. KG; Bombardier-Rotax GmbH & Co. KG; Bombardier- Rotax GmbHRotax 912 and 914 series enginesEngine – Magnetic Plug – InspectionsBRP-Rotax Alert Service Bulletin ASB-912-051 and ASB-914-034 andBRP-Rotax Service Bulletin SB-912-051 and SB-914-034
057-08 PTZFAA Emergency AD 2008-06-51   EASA Notification for FAA 2008-06-5112.03.2008Before furtherflight, unless the actions have already been done; See AD compliance for detailsLycoming Engines IO, (L)IO, TIO, (L)TIO, AEIO, AIO, IGO, IVO, and HIO series reciprocating engines, Teledyne Continental Motors (TCM) TSIO-360-RB reciprocating engines, and Superior Air Parts, Inc. IO-360 series reciprocating engines with certain Precision Airmotive LLC RSA-5 and RSA-10 series fuel injection servos Substantial loss of engine power andsubsequent loss of control of the airplanePrecision Airmotive LLC Mandatory Service Bulletin (MSB) No. PRS-107, Revision 1, dated March 6, 2008
058-08 PTZCF-2008-08R1 This AD Supersedes CF-2008-08 07.02.2008See AD for detailsPratt & Whitney Canada (P&WC) - PW305A and PW305B enginesEngine Fan Blade FractureAlert Service Bulletin (ASB) No. A24588 Special Instructions (SI) No.37-2007. ASB No. A24588R2Service Bulletin (SB) No. 24595
059-08 PTZFAA 2008-06-2423.04.2008Within 60 months after the effective date of this AD; See AD compliance for detailsBoeing Model 737-300, -400, and -500 series airplanesPrevent the in-line flow indicators of the passenger oxygen masks from fracturing and separating, which could inhibit oxygen flow to the masks and consequently result in exposure of the passengers and cabin attendantsto hypoxia following a depressurization eventBoeing Special Attention Service Bulletin 737-35-1099, dated April 9, 2007; B/E Aerospace ServiceBulletin 174080-35-01, dated February 6, 2006; and Revision 1, dated May 1, 2006
060-08 PTZFAA 2008-06-2728.04.2008See AD compliance for detailsGoodrich (Formerly BFGoodrich)Goodrich evacuation systems approved under Technical Standard Orders (TSOs) TSO-C69, TSO-C69a, and TSO-C69b, installed on certain Boeing airplanes, McDonnell Douglas airplanes and Airbus airplanes certificated in any category, as listed in Table 1-3 of this ADPrevent failure ofan evacuation system, which could impede an emergency evacuation and increase the chance of injury to passengers and flightcrew during the evacuationGoodrich Service Bulletin 25-343, Revision 3, dated January 12, 2007   Goodrich Service Bulletin25-344, Revision 2, dated October 11, 2006
061-08 PTZFAA 2008-06-2908.04.2008See AD compliance for detailsBoeing Model 737-300, -400, and -500 series airplanes, certificated in any categoryDetect and correct loose or missing parts from the main slat track downstop assemblies, which could puncture the slat can and result in a fuel leak and consequent fireBoeing Alert Service Bulletin737-57A1301, dated February 5, 2008
062-08 PTZFAA 2008-06-2810.04.2008See AD compliance for detailsAvidyne Corporation (Avidyne) Primary Flight Displays (PFDs) certain Part Numbers (P/Ns) that are installed on, but not limited to the following airplanes: Adam Aircraft, Cessna Aircraft; Cirrus Design Corporation; Diamond Aircraft Industries; Hawker Beechcraft Corporation; Hawker Beechcraft Corporation; Piper Aircraft.See AD for models.Prevent certain conditions from existing when PFDs display incorrect attitude, altitude, and airspeed information. This could result in airspeed/altitude mismanagement or spatial disorientation of the pilot with consequent loss of airplane control,inadequate traffic separation, or controlled flight into terrain.See AD
063-08 PTZEASA 2008-0064This AD supersedes EASA AD 2007-031318.04.2008See AD compliance for detailsEUROCOPTER DEUTSCHLAND GmbH EC135 and EC635 series helicopters, all models, all serial numbers, if equipped with Control rod Part Number (P/N) L672M2005207, Ball pivot P/N 92-201-00and/or Ball pivot P/N 92-207-00Rotor Flight Controls – Tail Rotor Control Rod and Ball Pivot – Inspection / ReplacementEUROCOPTER EC 135 Alert Service Bulletin No. EC135-67A-017 Revision 2dated 17 March 2008
064-08 PTZEASA 2008-006925.04.2008See AD compliance for detailsSaab AB, Saab Aerosystems SAAB SF340A Serial No’s 004 thru 159 and SAAB 340B Serial No’s 160 thru 459Power Plant – Forward Engine Cowl Door – Inspection / ReportingSAAB Service Bulletin SB-340-71-060, dated 08 Feb. 2008
065-08 PTZFAA 2008-0628R110.04.2008See AD compliance for detailsAvidyne Corporation (Avidyne) Primary Flight Displays (PFDs) certain P/N that are installed on, but not limited to the following airplanes: Adam Aircraft, Cessna Aircraft, Cirrus Design Corporation, Diamond Aircraft, Hawker Beechcraft, Piper AircraftPrevent certain conditions from existing when PFDs display incorrect attitude, altitude, and airspeed information. This could result in airspeed/altitude mismanagement or spatial disorientation of the pilot with consequent loss ofairplane control, inadequate traffic separation, or controlled flight into terrainAvidyne Service Alert No. SA-08-001, dated February 12, 2008
066-08 PTZFAA 2008-08-1429.04.2008Before further flight, unless the actions have already been done; see AD compliance for details Repetitive Inspections- At every engine oil change or within every 50 hours of engine run time, whichever occursFirst.Precision Airmotive LLC This AD applies to the reciprocating engines (Lycoming Engines, Teledyne Continental Motors, Superior Air Parts) with an installed Precision AirmotiveLLC, RSA-5 or RSA-10 series fuel injection servo, having a servo plug gasket, part number (P/N) 365533, installed under the fuel injection servo plug, P/N 383493Prevent a lean running engine, which could result in a substantial loss of engine power and subsequent loss of control of the airplanePrecision Airmotive LLC Mandatory Service Bulletin No. PRS-107, Revision 1
067-08 PTZFAA 2008-08-1019.05.2008See AD compliance for detailsBoeing 737-100, -200, -200C, -300, -400, and -500 series airplanes, certificated in any categoryDetect and correct that cracking, which could result in disconnection of the MLG actuator from the rear spar and support beam, consequent damage to the hydraulic system, and possible loss ofthe ''A'' and ''B'' hydraulic systems and damage or jamming of the flight control cablesBoeing Alert Service Bulletin 737-57A1266, Revision 1, dated January 3, 2007
068-08 PTZEASA 2008-007029.04.2008See AD compliance for detailsPILATUS AIRCRAFT Ltd.PC-6Landing Gear - Locking plate attachment screw -ReplacementPILATUS PC-6 Service Bulletin No. 32-001
069-08 PTZEASA 2008-0064 R118.04.2008See AD compliance for detailsEUROCOPTER DEUTSCHLAND GmbH EC135 and EC635 helicopters if equipped with Control rod Part Number (P/N) L672M2005207, Ball pivot P/N 92-201-00and/or Ball pivot P/N 92-207-00Rotor Flight Controls – Tail Rotor Control Rod and Ball Pivot –Inspection / ReplacementEUROCOPTER EC135 Alert Service Bulletin No. EC135-67A-017 Revision 2dated 17 March 2008
070-08 PTZFAA 2008-08-1706.05.2008Within 10 hours time-in-service or at the next regular inspection interval, whichever occurs first, unless the actionshave already been doneKelly Aerospace Power Systems turbochargers referenced in paragraphs (c)(1) through (c)(15)(vi) ofthis AD installed on Lycoming Engines, Teledyne Continental Motors. See AD Applicability for details Prevent hazardous amounts of carbon monoxide from entering the cabin, an increase in under-cowl temperatures hampering engine and accessory function, and loss of tailpipe retention, which could lead to an in-flight fire and loss of control of theairplaneSee table 1
071-08 PTZEASA 2008-007713.05.2008No later than 30 Sept. 2009; See AD compliance for detailsTURBOMECA ARRIEL 2B turboshaft engines ARRIEL 2B, 2B1 and 2B1A turboshaft engines, all serial numbers. These engines are known to be installed on, but not limited to:Eurocopter AS 350 B3 and EC 130 B4 helicopters.Engine Fuel & Control – Hydro Mechanical Unit (HMU) – Low FuelPressure Switch – Inspection/ReplacementTurboméca Mandatory Service Bulletin 292 73 2826
072-08 PTZEASA 2008-007808.05.2008See AD compliance for detailsSociété de Motorisations Aéronautiques (SMA)Cessna Model 182M, 182N, 182P, 182Q, 182R, and (Reims-manufactured) F182P and F182Q aircraft, all serial numbers, if modified in accordance with STC EASA.A.S.00774 (SMA SR305-230 engine installation)Engine Air – Air Inlet Manifold Hose Clamps – InspectionSMA SB N° SB-C182-75-002 Revision 2
073-08 PTZEASA 2008-008209.05.2008See AD compliance for detailsEUROCOPTER DEUTSCHLAND GmbHEC135 and EC635 series helicopters, all models, all serial numbersMain Rotor Drive – Main Gearbox (MGB) Oil Sampling & AnalysisProgram – IntroductionEurocopter EC 135 Alert Service Bulletin No. EC135-63A-012 Revision 02
074-08 PTZFAA 2008-10-0212.05.2008See AD compliance for detailsCessna Aircraft CompanySee Table 1 and Table 2 for list of types and S/NPrevent erroneousindications from the altimeter, airspeed, and vertical speed indicators, which could cause the pilot to react to incorrect flight information and possibly result in loss of controlnone
075-08 PTZFAA 2008-10-0321.05.2008See AD compliance for detailsBell Helicopter Textron 204B, 205A, 205A-1, 212, 412, 412CF, and 412EP205B, 210To detect any damage in a T/R blade, prevent cracking of a T/R blade leading to failure fromstatic overload, and subsequent loss of control of the helicopternone
076-08 PTZFAA 2008-09-1306.06.2008See AD compliance for detailsBoeing Model 737-300, -400, and -500 series airplanes, certificated inany categoryTo maintain the continued structural integrity of the entire fleet of Model 737-300, -400, and -500series airplanesBoeing Document D6-82669, ''Supplemental Structural Inspection DocumentModels 737-300/400/500 Airplanes,'' Original Release, dated May 2007
077-08 PTZFAA 2008-09-1506.06.2008See AD compliance for detailsBoeing Model 737-100, -200, -200C, -300, -400, and -500 series airplanes, certificated in any categoryDetect and correct cracking in the vinyl interlayer or damage to the structural inner glass panes of the flight deck No. 2, No. 4, and No. 5 windows, which could result in loss of a window and rapid loss of cabin pressure. Loss of cabin pressure could cause crewcommunication difficulties or crew incapacitationBoeing Alert Service Bulletin 737-56A1023, dated May 24, 2007
078-08 PTZEASA 2008-008319.05.2008Within 12 calendar months after the effective date of this AD; See AD compliance for detailsPILATUS AIRCRAFT Ltd.All PC-6 series aircraft models, from Manufacturer Serial Number (MSN) 101 through MSN 949 inclusive and all PC-6 series aircraft models, manufactured by Fairchild, from MSN 2001 through MSN 2092 inclusiveFuselage - Self-locking Stop Nuts - ReplacementPILATUS PC-6 Service Bulletin No. 53-002 Rev. 2
079-08 PTZCF-2008-1828.05.2008See AD CorrectiveAction for detailsBombardier Inc. Models CL-600-1A11 CL-600-2A12 CL-600-2B16 CL-600-2B16 Wing Anti-Ice Piccolo DuctsSee AD for list
080-08 PTZCF-2008-1928.05.2008Within 450 hours air time after the effective date of this AD; See AD CorrectiveAction for detailsBombardier Inc. Models:   CL-600-2C10 CL-600-2D15 CL-600-2D24Water Ingress into the CockpitBombardier Aerospace Alert Service Bulletin, A670BA-56-002, Revision “A”, dated26 Feb 2008
081-08 PTZFAA 2008-10-0912.06.2008See AD for detailsBoeing Model 737-100, -200, -200C, -300, -400, and -500 series airplanesPotential for ignition sources inside fuel tanks caused by latent failures, alterations,repairs, or maintenance actions, which, in combination with flammable fuel vapors, could result in a fuel tank explosion and consequent loss of the airplaneBoeing 737-100/200/200C/300/400/500 Airworthiness Limitations (AWLs)and Certification Maintenance Requirements (CMRs), D6-38278-CMR, Revision March 2008
082-08 PTZCF-2007-13R1Supersedes AD CF-2007-1328.05.2008See AD CorrectiveAction for detailsBell Helicopter Textron Canada (BHTC) Model 206B series helicoptersPower Turbine RPM Steady State Operation AvoidanceAlert Service Bulletin (ASB) 206-07-115 Rev B or206L-07-146 Rev A
083-08 PTZEASA 2008-008627.05.2008Within the next 200 flight hours after the effective date of this AD; See AD for detailsDiamond Aircraft Industries GmbH   DA 42 and DA 42 M aircraft, all S/N, if aileron bellcranks P/N DA4-2717-50-00 are installedFlight Controls – Aileron Bellcrank and Rod Ends – ReplacementDiamond Aircraft Industries GmbH MSB-42-043 orMSB-42-043/1
084-08 PTZEASA 2008-0082R1 This AD revises and replaces EASA AD 2008-008209.05.2008See AD compliance for detailsEurocopter Deutschland GmbH  EC135 and EC635 series helicopters, all models, all serial numbersMain Rotor Drive – Main Gearbox (MGB) Oil Sampling & AnalysisProgram – IntroductionEurocopter EC 135 Alert Service Bulletin No. EC135-63A-012 Rev. 02
085-08 PTZFAA 2008-11-0425.06.2008See AD compliance for detailsBoeing Model 737-100, -200, -200C, -300, -400, and -500 series airplanes, certificated in any categoryReports of cracks found in the skin, bearstrap, and/or frame outer chord in the hinge cutout areas of the forward entry and forward galley service doorways. We are issuing this AD to detect and correct such cracking, which could result in rapid decompression ofthe airplaneBoeing Alert Service Bulletin 737-53A1200, dated April 13, 2006
086-08 PTZEASA Emergency AD 2008-0100-E This AD is superseded by EASA Emergency AD 2008-0106-E (090-08 PTZ)27.05.2008See AD Required action(s) and ComplianceTime(s)Thielert Aircraft Engines GmbH TAE125-02-99 (commercial designation Centurion 2.0) engines, all serialnumbers, except those with clutch Part Number (P/N) 05-7211-K006001 installedEngine – Clutch Assembly – Inspection / ReplacementThielert Aircraft Engines GmbH SB TM TAE 125-1006 P1
087-08 PTZLBA D-2008-17831.05.2008Within the next 50 fh after publication of this AD, but not later than June 30, 2008. The inspection must be repeated together with the periodical inspection or with the 12-month inspection (whatevercomes first)EUROCOPTER Deutschland EC135 all modelsEC635 all modelsImpair of the controls’ freedom of movement by incorrect fixed bearings in the main rotor and tail rotor flight controls due to a production discrepancyEUROCOPTER Alert Service Bulletin EC135-67A-019 dated April 28, 2008
088-08 PTZCF-1996-24R1Cancels Airworthiness Directive (AD) CF-96-2413.06.2008See AD CorrectiveAction for detailsPratt & Whitney Canada (P&WC) PT6A Series enginesCompressor Bleed-off Valve Cover Assembly Inspection/Replacementnone
089-08 PTZFAA 2008-11-1503.06.2008See AD compliance for detailsMcDonnell Douglas airplanesModel 717-200; Model DC-9-11, DC-9-12, DC-9-13, DC-9-14, DC-9-15, and DC-9-15F; DC-9-21; DC-9-31, DC-9-32, DC-9-32 (VC-9C), DC-9-32F, DC-9-33F, DC-9-34, DC-9-34F, and DC-9-32F (C-9A, C-9B); DC-9-41; DC-9-51; DC-9-81 (MD-81), DC-9-82 (MD-82), DC-9-83 (MD-83), DC-9-87 (MD-87); MD-88; MD-90-30 airplanes; certificated in any categoryPotential for ignition sources inside fuel tanks caused by latent failures, alterations,repairs, or maintenance actions, which, in combination with flammable fuel vapors, could result in a fuel tank explosion and consequent loss of the airplaneBoeing Twinjet Special Compliance Items Report, MDC-92K9145,Revision G
090-08 PTZEASA Emergency AD 2008-0106-E This AD supersedes AD 2008-0100-E (086-08 PTZ )dated 23 May 200803.06.2008See AD required action(s) and ComplianceTime(s) section for detailsThielert Aircraft Engines GmbH All TAE125-02-99 (commercial designation Centurion 2.0) engines having the clutch assembly P/N 05-7211-K000304 installed. These engines are known to be installed on, but not limited to, Cessna 172 and (Reims-built) F172 series, Piper PA-28 series,APEX (Robin) DR 400 series  and Diamond DA40 and DA42 aircraftEngine - Clutch Assembly - ReplacementThielert Aircraft Engines GmbH SB TM TAE 125-1006 P1 Rev. 1
091-08 PTZFAA 2008-11-1807.07.2008See AD compliance for detailsCirrus Design CorporationModel SR20 airplanes, serial numbers 1005 through 1815Detect and correct leaks in the exhaustsystem, which could result in exhaust gases leaking into the cabin heating system. This condition could lead to carbon monoxide in the cabin and incapacitation of the pilot.Cirrus Service Bulletin SB 2X-78-07
R1, Rev 1
092-08 PTZFAA 2008-12-0309.07.2008See AD compliance for detailsThis AD applies to airplanes, certificated in any category and equipped with auxiliary fuel tanks installed in accordance with specified Supplemental Type Certificates (STCs), as identified in Table 1 of this AD (Boeing, British Aerospace, McDonnell Douglas).Prevent the potential of ignition sources inside fuel tanks, which, in combination with flammable fuel vapors, could result in fuel tank explosions and consequent loss of the airplaneSee AD
093-08 PTZEASA Emergency AD 2008-0116-E19.06.2008See AD Required action(s) and ComplianceTime(s) for detailsEurocopter Deutschland GmbH  EC135 and EC635 helicoptersMain Rotor Drive – Main Gearbox (MGB) Oil Sampling & AnalysisProgram – AmendmentEurocopter EC135 Alert Service Bulletin No.
EC135-63A-012
Revision 03
094-08 PTZHB-2008-242 EMERGENCY04.07.2008Before the next flight after the effective date of this AD; see AD COMPLIANCE/ ACTION for detailsPilatus – PC-6FLAP OPERATING MECHANISM – LEAF SPRINGS – Inspection, ReplacementPILATUS PC-6 Service Bulletin No. 27-002 PILATUS PC-6 Service Bulletin No. 27-003
095-08 PTZD-2008-222 This AD is supersedes by AD D-2008-222R1 The AD D-2008-222 has been cancelled23.06.2008See AD compliance for detailsRolls-Royce Deutschland, Dahlewitz, Germany BR700-710BR700-710 - Re-use of Potentially Damaged Engine MaterialRRD Worldwide Communication WW/20209/1/30 May 08, which is also covered by EASA Safety Information Bulletin SIB 2008-49
096-08 PTZEASA 2007-0241R207.09.2007See AD compliance for detailsPilatus Aircraft Ltd. PC-6 series aircraftWing – Wing Strut Fitting – Inspection / ReplacementPilatus Aircraft Ltd.
PC-6 SB
No. 57-005 dated
30 August 2007, Rev. 1 dated 19 Nov. 2007
and Rev 2 dated
19 May 2008
097-08 PTZEASA 2008-011324.06.2008See AD compliance for detailsEurocopter Deutschland GmbH EC135 and EC635 series helicopters and MBB-BK 117 C-2 helicoptersRotors Flight Control – Cyclic-Stick Locking Device – ModificationEurocopter Deutschland GmbH ASB MBB
BK117C-2-67A-008 and ASB EC135-67A-015,
both dated 14 April 2008
098-08 PTZCF-2008-2030.06.2008See AD Corrective Action for detailsBombardier Inc. Model CL-600-2B19 aircraftFuel System Safety - Insufficient Electrical Bonding at the Refuel/Defuel Shutoff ValvesBombardier SB 601R-28-053, Revision C, dated 14 March 2006
099-08 PTZCF-2008-2130.06.2008See AD Corrective Action for detailsBombardier Inc. CL-600-2B19 AircraftCracking of Main Landing Gear Trunnion Fitting WebTemporary Revision (TR) 2B-2136 of the Canadair Regional Jet Maintenance Requirement Manual (MRM), Appendix B, “Airworthiness Limitations”
100-08 PTZEASA 2008- 012111.07.2008See AD compliance for detailsEUROCOPTER AS 350 helicoptersStabilizers – Upper and Lower Fin Attachment Fitting - ModificationEUROCOPTER AS 350
ALERT SERVICE
BULLETIN No. 55.00.16
Rev 0 dated 28 February 2008
101-08 PTZEASA 2008-0127R122.07.2008See AD compliance for detailsSaab AB, Saab Aerosystems SF340A and 340B aircraftFuel System – Refuel/Defuel Panel Illuminated Placard – Inspection / ReplacementSAAB Service Bulletin SB-340-28-027
102-08 PTZEASA 2008-012823.07.2008See AD compliance for detailsThielert Aircraft Engines GmbH TAE 125-01, all serial numbersTime Limits / Maintenance Checks – Airworthiness Limitations – ImplementationThielert Aircraft Engines GmbH Operation & Maintenance Manual
TAE 125-01 OM-02-01, Chapter 5 at
Issue 3 Rev 5
103-08 PTZD-2008-23211.07.2008See AD compliance for detailsGrob Aerospace, Germany Grob G103 Twin AstirBolt cracking in the airbrake control system as a result of exceeding bolt torque and / or irregular adjustment of the airbrake systemGROB Service Bulletin NO. MSB 315-76/1
104-08 PTZFAA 2008-12-0116.06.2008See AD compliance for detailsCessna Aircraft Company Model 525 airplanes, serial numbers 525-0600 through 525-0662Detect and correct missing firewall sealant between the aft firewall assembly and seal assembly, which could result in failure of the fire extinguishing system to prevent the spread of fire through the firewall gapCessna Aircraft Company Citation Service Letter SL525-71-05
105-08 PTZFAA 2008-13-2817.07.2008See AD compliance for detailsHartzell Propeller Inc. left-hand rotating ( )HC-( )(2,3)Y(K,R)-2 two- and three-bladed, aluminum hub, ''compact'' series propellers; These propellers are installed on Lycoming Engines LIO-360 series and LO-360 series reciprocating engines, installed on Piper Aircraft, Inc. Seneca PA-34-200 and Seminole PA-44-180, and Hawker Beechcraft Corporation Model 76 Duchess, airplanesPrevent failure of the propeller hub, which could result in blade separation and loss of control of the airplaneHartzell Propeller Inc.
Alert Service Bulletin (ASB) No. HC-ASB-61-297, Rev 1
106-08 PTZCF-2008-2318.07.2008See AD Corrective Action for detailsPratt & Whitney Canada (P&WC) JT15D-5 enginesEngine Flameout in IcingP&WC ASB number A7611 Rev. No. 1
107-08 PTZFAA 2006-16-18 R118.07.2008See AD compliance for detailsSandel Avionics Incorporated Model ST3400 terrain awareness warning system/radio magnetic indicator (TAWS/RMI) units; installed on various small and transport category airplanes, certificated in any category, including, but not limited, to the airplane models listed in Table 1 of this AD (Airbus A300; Boeing 737; Cessna 208, 208B, 421C; 501, 525, 550, 560, 650, S550; Piper PA-31T2…)Prevent a bearing error, which could lead to an airplane departing from its scheduled flight path, which could result in a reduction in separation from, and a possible collision with, other aircraft or terrainSandel ST3400 Service Bulletin SB3400-01, Revision B
108-08 PTZEASA 2008-0136   This AD is revised and replaced by EASA AD 2008-0136R105.08.2008See AD compliance for detailsDiamond Aircraft Industries GmbH DA 42 and DA 42 M aircraft, all serial numbersAirplane Flight Manual – Lightning Strike Procedures – AmendmentDiamond Aircraft Industries GmbH Temporary Revision TR-MÄM-42-270 dated 31 May 2008;   Diamond Aircraft Industries GmbH DA 42 Aircraft Maintenance Manual, Chapter 05-50, paragraph 5.D post-lightning strike inspection
109-08 PTZCF-2008-2423.07.2008See AD Corrective Action for detailsBombardier Inc. Model CL-600-2C10 aircraft, serial numbers 10003 through 10169 and CL-600-2D24 aircraft, serial numbers 15001 through 15030Fuel System Safety - Chafing of Fuel System Wiring with High Power Wiring at Centre Fuel Tank Front SparBombardier Service Bulletin (SB) 670BA-24-012, Revision B, dated 25 July 2007
110-08 PTZCF-2008-2523.07.2008See AD Corrective Action for detailsBombardier Inc. Model CL-600-2C10 aircraft, serial numbers 10003 through 10169 and CL-600-2D24 aircraft, serial numbers 15001 through 15030Fuel System Safety - Chafing of Fuel System Wiring with High Power Wiring along FuselageBombardier Service Bulletin (SB) 670BA-24-011, Revision C, dated 28 November 2005
111-08 PTZEASA 2008-013029.07.2008See AD compliance for detailsThielert Aircraft Engines GmbH TAE125-01 engines, all serial numbers, if installed on Diamond Aircraft Industries Model DA 42 aircraftPropellers – Propeller Control Valve – Replacement (Life Limit)Thielert Service Bulletin TM TAE125-0018 dated 19 June 2008
112-08 PTZEASA 2008-013431.07.2008See AD compliance 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
113-08 PTZEASA Emergency AD 2008-0142-E01.08.2008See Required Action(s) And ComplianceTime(s) for detailsAgusta S.p.AAB412 helicoptersTime Limits / Maintenance Checks – Rescue Hoist Cable AssemblyRetirement Life Limitation – IntroductionAgusta Alert Bollettino Tecnico 412-126
114-08 PTZEASA 2008-014919.08.2008See Required Action(s) And Compliance Time(s) for detailsAIRBUS (formerly AIRBUS INDUSTRIE) A318, A319, A320 and A321 aircraftFlight Controls – Elevator Servo-Control Rod Eye-end – InspectionAIRBUS All Operators Telex (AOT) A320-27A1186 Original issue dated 23 June 2008
115-08 PTZFAA 2008-15-0505.08.2008See AD compliance for detailsBoeing Model 737-300, -400, and -500 series airplanes, certificated in any categoryDetect and correct corrosion of the carriage spindle, which could result in fracture. Fracture of both the inboard and outboard carriage spindles, in the forward ends through the large diameters, on a single flap, could adversely affect the airplane's continued safe flight and landing.Boeing Alert Service Bulletin 737-57A1304, dated June 2, 2008   Boeing Alert Service Bulletin 737-57A1277, Revision 1, dated November 25, 2003
116-08 PTZEASA 2008-013907.08.2008See Required Action(s) And Compliance Time(s) for DetailsDiamond Aircraft Industries GmbH DA 42 aircraft, all serial numbers, if Thielert TAE125-01 engines are installedPower Plant – Rear Engine Support Bracket Mounting Bolts – Inspection / ReplacementDiamond Aircraft Industries GmbH Mandatory Service Bulletin MSB-42-058 and Work Instruction WI-MSB-42-058
117-08 PTZFAA 2008-13-1212.08.2008See AD compliance for detailsBoeing Model 737-100, -200, -200C, -300, -400, and -500 series airplanes, certificated in any categoryDetect and correct fatigue cracking of the upper frame to side frame splice of the fuselage, which could result in reduced structural integrity of the frame and adjacent lap jointBoeing Alert Service Bulletin 737-53A1261
118-08 PTZFAA 2008-13-2912.08.2008See AD compliance for detailsMcDonnell Douglas Model DC-9-81 (MD-81), DC-9-82 (MD-82), DC-9-83 (MD-83), DC-9-87 (MD-87), and MD-88 airplanes, certificated in any categoryDetect and correct cracked overwing frames which could sever the frame, increase the loading of adjacent frames, and result in damage to adjacent structure and loss of overall structural integrity of the airplaneBoeing Alert Service Bulletin MD80-53A301, Revision 1
119-08 PTZFAA 2008-14-0714.08.2008See AD compliance for detailsLycoming Engines (formerly Textron Lycoming Division, AVCO Corporation) fuel injected reciprocating engines manufactured by Lycoming Engines that incorporate externally mounted fuel injection lines (engines with an ''I'' in the prefix of the engine model designation) as listed in the Table 1. Engine models in Table 1 are installed on, but not limited to, Piper PA-24 Comanche, PA-30 and PA- 39 Twin Comanche, PA-28 Arrow, and PA-23 Aztec; Beech 23 Musketeer; Mooney 20, and Cessna 177 Cardinal airplanesPrevent failure of the fuel injector fuel lines that would allow fuel to spray into the engine compartment, resulting in an engine fireLycoming Engines Mandatory Service Bulletin No. 342E
120-08 PTZFAA 2008-14-1314.08.2008See AD compliance for detailsCirrus Design Corporation SR20 S/N 1423 through 1906 SR22 S/N 0795 and 0820 through 2912In-flight failure of the cabin door, which could result in door separation from the airplaneCirrus Design Corporation Service Bulletin SB 2X-52-07 R4
121-08 PTZEASA 2008-014515.08.2008See Required Action(s) And Compliance Time(s) for DetailsThielert Aircraft Engines GmbH TAE125-01 and TAE125-02-99 engines, all serial numbers, if installed on Diamond Aircraft Industries Model DA 42 aircraftPropellers – Propeller Control Valve – Replacement (Life Limit)Thielert Aircraft Engines SB TM TAE125-0018 and TM TAE125-1007 P1
122-08 PTZEASA 2008-014615.08.2008See Required Action(s) And Compliance Time(s) for DetailsSaab AB, Saab Aerosystems (formerly Saab Aircraft AB) SF340A and 340B aircraftHydraulic System – Hydraulic Accumulators – ReplacementSAAB Service Bulletin SB-340-29-023
123-08 PTZEASA 2008-015019.08.2008See Required Action(s) And Compliance Time(s) for DetailsAIRBUS (formerly AIRBUS INDUSTRIE)   A318, A319, A320 and A321 aircraftFlight Controls – Trimmable Horizontal Stabilizer Actuator (THSA) – InspectionAIRBUS Service Bulletin A320-27-1164 Rev 6
124-08 PTZEASA 2008-015119.08.2008See Required Action(s) And Compliance Time(s) for DetailsAIRBUS (formerly AIRBUS INDUSTRIE)   A318, A319, A320 and A321 aircraftEquipment / Furnishings – Cockpit Door Latch / Striker Assembly – Modification / ReplacementAIRBUS SB A320-25-1444
125-08 PTZFAA 2008-14-1520.08.2008See AD compliance for detailsInternational Aero Engines AG (IAE) IAE V2500-A1, V2522-A5, V2524-A5, V2527-A5, V2527E-A5, V2527M-A5, V2530-A5, V2533-A5, V2525-D5, and V2528-D5 turbofan enginesPrevent heat damage to high-pressure turbine (HPT) and low-pressure turbine (LPT) critical life limited hardware such as the HPT stage 1-2 airseal. Damage to the HPT stage 1-2 airseal could cause uncontained engine failure and damage to the airplaneInternational Aero Engines Service Bulletin No. V2500-ENG-72-0541, Revision 4
126-08 PTZEASA 2006–0140R125.05.2006See 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 Ref. Publications
127-08 PTZCF-2007-10R125.08.2008See AD compliance for detailsBombardier Inc. Model CL-600-2B19, serial number 7003 thru 7990 and 8000 and subsequentFlaps FailureSee AD
128-08 PTZEASA 2008-015804.09.2008See Required Action(s) And Compliance Time(s) for DetailsFunkwerk Avionics GmbH   TRT600, TRT800, TRT800A and TRT800H Mode-S Transponders, all part numbers, all serial numbersNavigation – Mode-S Transponders – LimitationNone
129-08 PTZCF-2008-16R103.09.2008See AD compliance for detailsBombardier Inc. CL-600-1A11, CL-600-2A12 and CL-600-2B16 aircraftEnhancement to Takeoff Operational Safety MarginsSee AD
130-08 PTZCF-2008-15R103.09.2008See AD compliance for detailsBombardier Inc. Model CL-600-2B19 aircraftEnhancement to Takeoff Operational Safety MarginsSee AD
131-08 PTZEASA 2008-015908.09.2008See Required Action(s) And Compliance Time(s) for DetailsHoneywell International Inc.   MST-67A Mode-S TranspondersNavigation Systems – Mode-S Transponder – Modification / ReplacementHoneywell Service Bulletin MST 67A-34-56 Honeywell Software Bulletin MST 67A-SW5
132-08 PTZFAA 2008-17-0523.09.2008See AD compliance for detailsEmpresa Brasileira De Aeronautica S.A. EMBRAER Model EMB-135ER, -135KE, -135KL, -135LR, and - 135BJ airplanes; and all Model EMB-145, -145ER, -145MR, -145LR, -145XR, -145MP, and -145EP airplanes; certificated in any categoryPrevent an ignition source inside the fuel tank that could ignite fuel vapor and cause a fuel tank explosion and loss of the airplaneSee table 2
133-08 PTZFAA 2008-17-0323.09.2008See AD compliance for detailsBoeing Model 737-100, -200,  -200C -300, -400, and -500 seriesDetect and correct such cracking, which could prevent the left forward entry door from sealing correctly, and could cause in-flight decompression of the airplaneBoeing Alert Service Bulletin- 737-53A1197 and 737-53A1188
134-08 PTZEASA 2008-0164 This AD is superseded by EASA 2008-017110.09.2008See Required Action(s) And Compliance Time(s) for DetailsPilatus Aircraft Ltd.   PC-6 aircraft, all models, all serial numbersLanding Gear - Movement of Brake Pedals- Check/ModificationPILATUS PC-6 Service Bulletin No. 32-002 Rev 2
135-08 PTZFAA Emergency AD 2008-19-51Issued 08.09.2008 effective upon receiptSee AD compliance for detailsRolls- Royce Corporation (RRC) AE 3007A series turbofan engines installed on, but not limited to Empresa Brasileira de Aeronautica S. A. (EMBRAER) EMB-135 and EMB-145 airplanesCracked high-pressure turbine (HPT) stage 2 wheelsRRC Alert Service Bulletin (ASB) AE 3007A-A-72-367, dated September 5, 2008
136-08 PTZEASA 2008-0171This AD supersedes EASA 2008-016423.09.2008See Required Action(s) And ComplianceTime(s) for DetailsPilatus Aircraft Ltd. PC-6Landing Gear - Movement of Brake Pedals- Check/ModificationPILATUS PC-6 Service Bulletin No. 32-002 Rev 2
137-08 PTZEASA Emergency AD 2008-0175-E18.09.2008See Required Action(s) And ComplianceTime(s) for DetailsEurocopter Deutschland GmbHEC 135 and EC 635 helicoptersMain Rotor Drive – Main Transmission Mast Bearing Retainer Bolts– Inspection / ModificationEurocopter Deutschland EC135 Alert Service Bulletin No. EC135-63A-013Rev 02
138-08 PTZEASA Emergency AD 2008-0177-E19.09.2008Before next flight after the effective date of this AD; See Required Action(s) And ComplianceTime(s) for DetailsEUROCOPTER  EC 120 B helicoptersEquipment & Furnishings – Emergency Floatation Gear Lighting and Ancillary Control Unit (LACU) Pushbutton – In-Flight Check /ReplacementEurocopter Alert Service Bulletin N° 04A007
139-08 PTZEASA 2008-0136R1 This AD revises and replaces EASA AD 2008-013605.08.2008See Required Action(s) and Compliance Time(s)Diamond Aircraft Industries GmbH (Austria) Diamond Aircraft Industries DA 42 and DA 42 M aircraft, all serial numbersAirplane Flight Manual – Lightning Strike Procedures – AmendmentDiamond Aircraft Industries Temporary Revision TR-MÄM-42-270   Diamond Aircraft Industries DA 42 Aircraft Maintenance Manual, Chapter 05-50, para 5.D post-lightning strike inspection
140-08 PTZEASA 2008-017417.09.2008Within 15 days after the effective date of this AD; See Required Action(s) And Compliance Time(s) for DetailsSPEKON Sächsische Spezialkonfektionen   RE-5L Emergency ParachutesEmergency Parachute - Replacement of the Drogue ParachuteSPEKON Sicherheitsmitteilung (Safety Bulletin) No. 01/2008 Issue 2
141-08 PTZFAA 2008-19-0520.10.2008See AD compliance for detailsLycoming Engines (formerly Textron Lycoming) models 320, 360, and 540 series, ''Parallel Valve'', reciprocating engines listed in Table 1 of this AD, with ECi cylinder assembly, P/N AEL65102 series ''Titan'', and with cylinder head, P/N AEL85099, installedPrevent loss of engine power due to cracks at the head-to-barrel interfacein the cylinder assemblies and possible engine failure caused by separation of a cylinder head, which could result in loss of control of the aircraftECi Mandatory Service Bulletin No. 08-1, Rev 3
142-08 PTZFAA 2008-19-12 27.10.2008See AD compliance for detailsHoneywell International Inc. (formerly AlliedSignal Inc., formerly Garret Turbine Engine Company)TFE731-4, -4R, -5, -5AR, -5BR, and -5R series turbofan enginesUncontainment of turbine blades and fragments of the LPT nozzle assembly, which could result in damage to the airplaneHoneywell International Inc. Service Bulletin (SB) No. TFE731-72-3727 and SB No. TFE731-72-3728
143-08 PTZD-2008-222R1 This AD supersedes the AD D-2008-222The AD D-2008-222 has been cancelled with immediate effect25.09.2008See AD compliance for detailsRolls-Royce DeutschlandAircraft Engine BR700-710BR700-710 - Re-use of Potentially Damaged Engine MaterialRolls-Royce Deutschland Worldwide Communication WW/20209/1/30
144-08 PTZEASA 2008-017009.10.2008No later than 31 May 2009; See Required Action(s) And ComplianceTime(s) for DetailsTURBOMECA ARRIUS 2F turbo-shaft engine These engines are known to be installed on, but not limited to,Eurocopter EC120B helicoptersEngine Fuel & Control - Lubrication Unit - ModificationTURBOMECA Service Bulletin n° 319 79 4075
145-08 PTZEASA 2008-016611.09.2008See Required Action(s) And ComplianceTime(s) for DetailsAIRBUS (formerly AIRBUS INDUSTRIE)A300, A310, A300-600 and A300-600ST aircraftFire Protection / Hydraulic Power - Air Pressurisation Check Valves– Identification / ReplacementAIRBUS Service Bulletins A300-29-0124 original issue, A310-29-2097 original issue; A300-29-6060 original issue; A300-29-9009 original issue
146-08 PTZEASA Emergency AD 2008-0190-E15.10.2008Before next flight after the effective date of this AD; See Required Action(s) And Compliance Time(s) for DetailsEurocopter Deutschland GmbH EC135 and EC635 helicoptersFuselage – Rear Structure / Tail Boom – InspectionEurocopter Deutschland ASB EC135-53A-022 dated 13 October 2008
147-08 PTZEASA 2008-018115.10.2008See Required Action(s) And Compliance Time(s) for DetailsAIRBUS SAS A300, A310 and A300-600 aircraftNacelles / Pylons – Pylon Side Panels at Rib 8 – InspectionAIRBUS Service Bulletin A300-54-0075 Rev 02   Service Bulletin A310-54-2018 Rev 02   Service Bulletin A300-54-6015 Rev 02
148-08 PTZEASA 2006–0140R225.05.2006See 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 SystemAir Conditioning - Zonal Drying System DeactivationSee Ref. Publications for list
149-08 PTZEASA 2008-018522.10.2008See Required Action(s) And Compliance Time(s) for DetailsEUROCOPTER EC 120 helicoptersEngine Controls – Twist Grip Drive Tube – Replacement /InspectionEUROCOPTER EC 120 Alert Service Bulletin 76A005 Rev 1;   EUROCOPTER EC 120 Alert Service Bulletin 76A006 Rev 2
150-08 PTZEASA 2008-018824.10.2008See Required Action(s) And Compliance Time(s) for DetailsAIRBUS SAS   A300 aircraftElectrical Power – Fuel Pump Wiring – Modification [Prevention against Fuel Tank Explosion Risks]AIRBUS Service Bulletin A300-24-0103 Rev 02
151-08 PTZEASA 2008–018924.10.2008See Required Action(s) And Compliance Time(s) for DetailsEUROCOPTER AS350 helicoptersEquipment and Furnishings - Emergency Flotation Gear – ReplacementEUROCOPTER Alert Service Bulletin No. 25.01.02 Rev. 0 dated 24 Sept 2008
152-08 PTZCF-2008-3003.11.2008See Corrective Action for DetailsBombardier Inc. Model CL-600-2B19Wing Anti-Ice Piccolo Ducts (Piccolo Tubes)See AD
153-08 PTZFAA 2008-15-0602.09.2008See AD compliance for detailsCessna Aircraft Company Model 175 and175ACracks in the engine mounting bracketsCessna Single Engine Service Bulletin SEB07-2, Rev 2
154-08 PTZFAA 2008-19-0316.10.2008See AD compliance for detailsBoeing Model 737-300, -400, and -500 series airplanesFatigue cracking of the fuselage skin panels at the chem-mill stepsBoeing Alert Service Bulletin 737-53A1293, dated August 13, 2008
155-08 PTZFAA 2008-17-1305.11.2008See AD compliance for detailsBoeing Model 737-100, -200, -200C, -300, -400, and -500 series airplanesWater leak into the flight deck ceilingBoeing Alert Service Bulletin 737-38A1054, dated August 23, 2007
156-08 PTZFAA 2008-21-0313.11.2008See AD compliance for detailsBoeing Model 737-300, -400, and -500 series airplanesDamage of the fuse pins of the inboard and outboard midspar fittings of the nacelle strutBoeing Special Attention Service Bulletin 737-54-1044, dated December 10, 2007
157-08 PTZEASA 2006-0112R1   This AD revises and replaces EASA AD 2006-011223.05.2006See Required Action(s) And Compliance Time(s) for DetailsAIRBUS (formerly AIRBUS INDUSTRIE) A318, A319, A320 and A321 aircraftLanding Gear - Main Landing Gear (MLG) - Door Actuator – InspectionAIRBUS Service Bulletin A320-32-1309 original issue   AIRBUS Service Bulletin A320-32-1338 original issue
158-08 PTZAGÊNCIA NACIONAL DE AVIAÇÃO CIVIL – BRAZIL   ANAC 2008-10-0221.10.2008See AD compliance for details   Within the next 1500 flight hours or 6 months after the effective date of this AD, whichever occurs firstEmbraer EMB-145, EMB-145ER, EMB-145EU, EMB-145EP, EMB-145LR, EMB-145LU, EMB-145MR, EMB-145MP, EMB-145MK, EMB-145XR, EMB-135ER, EMB-135LR, EMB-135KE, EMB-135KL and EMB-135BJ aircraft modelsCorrosion on the Auxiliary Power Unit (APU) mounting rodsEmbraer Service Bulletins Nos. 145-49-0034 original issue or 145LEG-49-0008 original issue
159-08 PTZEASA 2008-0158R1   This AD revises and replaces EASA AD 2008-015804.09.2008See Required Action(s) And Compliance Time(s) for DetailsFunkwerk Avionics GmbH, Filser Electronic GmbH   TRT600, TRT800A, and TRT800H Mode-S Transponders, all part numbers, all serial numbersNavigation – Mode-S Transponders – LimitationEASA Safety Information Bulletin 2008-84
160-08 PTZEASA Emergency AD 2008-0191-E21.10.2008Within 7 days after the effective date of this AD; See Required Action(s) And Compliance Time(s) for DetailsAIRBUS (formerly AIRBUS INDUSTRIE)   A319, A320 and A321 aircraftPower Plant – Rear Engine Mount Barrel Nuts – Inspection / ReplacementAIRBUS All Operator Telex A320-71A1045, dated 17 Oct 2008
161-08 PTZFAA 2008-22-0126.11.2008See AD compliance for detailsAirplanes equipped with auxiliary fuel tanks installed in accordance with specified STC´s, as identified in Table 1 of this AD (Boeing, Bombardier, McDonnell Douglas)Potential of ignition sources inside fuel tanksnone
162-08 PTZFAA 2008-21-1128.11.2008See AD compliance for detailsGeneral Electric Company (GE) CF6-80C2 and CF6-80E1 engines installed on, but not limited to, Airbus A300, A310, and A330 series airplanes, Boeing 747 and 767 series airplanes, and McDonnell Douglas MD11 series airplanesUncontained release of engine debris and loss of the structural integrity of the mount system that supports the engineSee AD
163-08 PTZEASA 2007-0299R225.10.2007See Required Action(s) And Compliance Time(s) for DetailsAIRBUS   A300 aircraftWings – Centre Flap Inner Tab Hinge Bracket – Inspection /ReplacementAirbus SB A300-57-0250 original issue or rev 01 Airbus SB A300-57-0252 Airbus SB A300-57-0205
164-08 PTZEASA AD CANCELLATION NOTICE 2008-0166-CN Corrected by 166-08 PTZ29.10.2008Not applicableAIRBUS   A300, A310, A300-600 and A300-600ST aircraftFire Protection / Hydraulic Power - Air Pressurisation Check Valves – Identification / ReplacementAirbus Service Bulletins: A300-29-0124 A310-29-2097 A300-29-6060 A300-29-9009
165-08 PTZEASA 2008-019712.11.2008Within 15 days after the effective date of this AD; See Required Action(s) And Compliance Time(s) for DetailsMcDonnell Douglas Corporation   DC-9-10, -20, -30, -40, and -50 Series, DC-9-81/82/83/87, MD-88, MD-90, and 717 airplanesCentral Aural Warning System – Airplane Flight Manual and Pre- Start Check of the Take-off Warning System – IntroductionNot applicable
166-08 PTZEASA AD CANCELLATION NOTICE 2008-0166-CN Corrected29.10.2008Not applicableAIRBUS   A300, A310, A300-600 and A300-600ST aircraftFire Protection / Hydraulic Power - Air Pressurisation Check Valves – Identification / ReplacementAirbus Service Bulletins: A300-29-0124 A310-29-2097 A300-29-6060 A300-29-9009
167-08 PTZEASA 2008-019818.11.2008See Required Action(s) And Compliance Time(s) for DetailsAIRBUS   A319, A320 and A321 aircraftInstruments – Electronic Instrument System (EIS) Display Management Computer (DMC) Software Update – IntroductionAIRBUS Service Bulletin A320-31-1286
168-08 PTZFAA 2008-22-1809.12.2008Within the next 25 hours time-in-service after Dec 9, 2008; See AD compliance for detailsCessna Aircraft Company Models 150, 150A, 150B, 150C, 150D, 150E, 150F, 150G, 150H, 150J, 150K, A150K, 150L, A150L, 150M, A150M, 152, and A152 airplanes that Have a BRS-150 Parachute System InstalledPrevent premature separation of the collar. This condition could result in the parachute failing to successfully deployBRS Service Bulletin SB 2008-04-01 R1, issued April 24, 2008
169-08 PTZEASA 2008-019919.11.2008Within 12 months after the effective date of this AD; See Required Action(s) And Compliance Time(s) for DetailsAIRBUS   A318, A319, A320 and A321 aircraftHydraulic Power – Auxiliary Hydraulic Power - Ram Air Turbine (RAT) Ejection Jack - ReplacementAIRBUS Service Bulletin A320-29-1136 original issue
170-08 PTZCF-2008-3315.12.2008Within 30 days after the effective date of this AD; See AD Corrective Actions for DetailsBombardier Inc. CL-600-2B19 AircraftInboard Flap ActuatorSee AD
171-08 PTZCF-2008-32 Superseded by CF-2008-32R115.12.2008Within 30 days after the effective date of this AD; See AD Corrective Actions for DetailsBombardier CL-600-2A12 (CL601) and CL-600-2B16 (601-3A, 601-3R & CL604) AircraftEngine Throttle Control Gearbox wear InspectionSee AD
172-08 PTZCF-2008-32R1 Supersedes Airworthiness Directive (AD) 2008-3215.12.2008Within 30 days after the effective date of this AD; See AD Corrective Actions for DetailsBombardier CL-600-2A12 (CL601) and CL-600-2B16 (601-3A, 601-3R & CL604) AircraftEngine Throttle Control Gearbox wear InspectionSee AD
173-08 PTZEASA 2008-0158R204.09.2008See Required Action(s) And Compliance Time(s) for DetailsFunkwerk Avionics GmbH   TRT600 transpondersNavigation – Mode-S Transponders – LimitationEASA Safety Information Bulletin 2008-84R1
174-08 PTZEASA 2008-018319.11.2008See Required Action(s) And Compliance Time(s) for DetailsFunkwerk Avionics GmbH   TRT800A and TRT800H TranspondersNavigation – Mode-S Transponders – ReplacementFunkwerk Avionics SB TRT800-A-H-1 Revision 1
175-08 PTZFAA 2008-23-0725.11.2008See AD compliance for detailsBoeing Model 737-100, -200, -200C, -300, -400, -500, -600, -700, -700C, -800, -900, and -900ER series airplanes, certificated in any categoryFailure of the flightcrew to recognize and react to a valid cabin altitude warning hornSee AD
176-08 PTZFAA 2008-13-12R101.12.2008See AD compliance for detailsBoeing Model 737-100, -200, -200C, -300, -400, and -500 series airplanes, certificated in any categoryFatigue cracking of the upper frame to side frame splice of the fuselageSee AD
177-08 PTZFAA 2008-23-0915.12.2008See AD compliance for detailsBoeing airplanes, certificated in any category, specified in paragraphs (c)(1) and (c)(2) of this ADInsulation blankets constructed of AN-26 are removed from the fuselageSee AD
178-08 PTZFAA 2008-22-0126.11.2008See AD compliance for detailsVarious Transport Category Airplanes (Boeing, Bombardier, McDonnell Douglas)Potential of ignition sources inside fuel tanksSee AD
179-08 PTZFAA 2008-24-0230.12.2008Before the next time the elevator control cable is disconnected for any reason or within the next 12 calendar months after Dec 30, 2008 (the effective date of this AD), whichever occurs firstMaule Aerospace Technology   M-4, M-5, M-6, M-7, M-8, MT-7, MX-7, MXT-7- See AD Applicability for detailed listMechanic rigging the elevator controls backwardsMaule Aerospace Technology, Inc. Mandatory Service Bulletin No. 30
180-08 PTZFAA 2008-24-0530.12.2008See AD compliance for detailsBoeing   Model 737-400 and -500 series airplanes Model 737-600, -700, -700C, -800, and -900 series airplanesFailure of the windshield wipers in wet weatherBoeing Alert Service Bulletin 737-30A1059 and Boeing Service Bulletin 737-30A1057
181-08 PTZCF-2008-32R215.12.2008Within 30 days after the effective date of this directive; See AD Corrective Actions for DetailsBombardier CL-600-2A12 (CL601) and CL-600-2B16 (601-3A, 601-3R & CL604) AircraftEngine Throttle Control Gearbox wear InspectionSee AD
182-08 PTZEASA 2008-0205-E04.12.2008See Required Action(s) And Compliance Time(s) for DetailsEUROCOPTER (formerly EUROCOPTER FRANCE, AEROSPATIALE)   All AS350 B, BA, BB, B1, B2, B3, D helicoptersRotors Flight Control - Collective Pitch Lever Locking Stud – Inspection / RepairEUROCOPTER Emergency Alert Service Bulletin No. 05.00.58 Rev. 0
183-08 PTZEASA 2008-020709.12.2008See Required Action(s) And Compliance Time(s) for DetailsAIRBUS (formerly AIRBUS INDUSTRIE) A310 and A300-600 aircraftFuel System – Auxiliary Central Tank (ACT) – Modification / Re-Identification [Prevention against Fuel Tank Explosion Risks]Airbus Service Bulletin A310-28-2149 original issue, Rev 01 and Rev 02   Airbus Service Bulletin A300-28-6073 original issue, Rev 01, Rev 02 and Rev 03
184-08 PTZEASA 2008-020809.12.2008See Required Action(s) And Compliance Time(s) for DetailsAIRBUS (formerly AIRBUS INDUSTRIE) A300, A310 and A300-600 aircraftWings – Centre Wing Bottom Skin at Rib 1 – InspectionAIRBUS SB A300-57-0204 Rev 01   AIRBUS SB A310-57-2061 Rev 01   AIRBUS SB A300-57-6047 Rev 05
185-08 PTZEASA 2008-021519.12.2008See Required Action(s) And Compliance Time(s) for DetailsThielert Aircraft Engines GmbH TAE 125-02-99 enginesReplacement of Rail Pressure Control Valve – Modification of VRail Plug - Time Limits / Maintenance Checks – Airworthiness Limitations – ImplementationThielert Service Bulletin TAE SB TM 125-1008 P1 R1   Thielert Aircraft Engines GmbH Operation & Maintenance Manual TAE 125-02-99 OM-02-02, Chapter 5 at Issue 1 Revision 2
186-08 PTZCF-2008-3422.12.2008See AD Corrective Actions for DetailsBombardier Inc. Models CL-600-2C10, S/N 10112–10199, 10201–10206   CL-600-2D15 and CL-600-2D24, S/N 1500 –15026, 15030, 15031Inspection and Replacement of the Fuse Blocks in the APU Start Contactor AssemblyBombardier Aerospace Service Bulletin (SB) 670BA-49-012, original revision
187-08 PTZCF-2007-19R131.12.2008See AD Corrective Actions for DetailsEurocopter AS 350 Series Helicopters equipped with a Honeywell Control UnitHydraulic Test Switch ProtectionEurocopter Service Bulletin (SB) 67.00.32 rev 1
188-08 PTZEASA 2008–0214-E10.12.2008See Required Action(s) And Compliance Time(s) for DetailsEUROCOPTER (formerly EUROCOPTER FRANCE, AEROSPATIALE) AS350 B, BA and D helicopters, all serial numbers equipped with the emergency flotation gear installationEquipment & Furnishing – Emergency Flotation Gear – Inspection / Limitation / ReplacementEUROCOPTER Emergency Alert Service Bulletin No. 01.00.59 Rev. 0
189-08 PTZEASA 2008-0208R1 This AD revises and replaces EASA AD 2008-020809.12.2008See Required Action(s) And Compliance Time(s) for DetailsAIRBUS (formerly AIRBUS INDUSTRIE) A300, A310 and A300-600 aircraftWings – Centre Wing Bottom Skin at Rib 1 – InspectionAIRBUS SBA300-57-0204 Rev 01 AIRBUS SBA310-57-2061 Rev 01 AIRBUS SBA300-57-6047 Rev 05
190-08 PTZEASA 2008-022602.01.2009See Required Action(s) And Compliance Time(s) for DetailsAirbus (formerly Airbus Industrie) A310 and A300-600 aircraftEngine Exhaust – Centre Latch of Thrust Reverser Door Opening Mechanism – Replacement / InspectionSee Ref. Publications for list
191-08 PTZEASA Emergency AD 2008-0227-E   This AD is superseded by EASA Emergency AD 2008-0228-E24.12.2008See Required Action(s) And Compliance Time(s) for DetailsCFM International SA (CFM) CFM56-5B turbofan engines   These engines are known to be installed on but not limited to Airbus A318/A319/A320/A321 aircraftEngine – High Pressure Compressor (HPC) Stall Event– Inspection/ReplacementCFM56-5B S/B 72-0722, dated 22 December 2008
192-08 PTZCF-2008-3505.01.2009See AD Corrective Actions for DetailsBombardier Inc. Model CL-600-2B19, serial number 7003 and subsequent equipped with Thales AOA transducersAngle of Attack Transducer – Heating Element Degradation and Inaccurate CalibrationBombardier SB 601R-27-153 dated 17 Oct 2008 Bombardier SB 601R-27-154 dated 1 Dec 2008
193-08 PTZEASA Emergency AD 2008-0228-E This AD supersedes EASA AD 2008-0227-E27.12.2008See Required Action(s) And Compliance Time(s) for DetailsAIRBUS   A318, A319, A320 and A321 aircraft models, all serial numbers with CFM56-5B engines installedEngine – High Pressure Compressor (HPC) Stall Event– Inspection/ReplacementCFM56-5B S/B 72-0722   Airbus OIT/FOT 999.0109 /08 rev1   A318/A319/A320/A321 AMM Task 71-00-00-710-040
194-08 PTZFAA 2008-26-0428.01.2009See AD compliance for detailsCessna Aircraft Company Model 560 airplanes, certificated in any category, serial numbers (S/Ns) 560-0001 through -0538 inclusiveInadvertent stall due to the inadequate stall warning margin provided by an improperly adjusted stall warning systemSee AD
195-08 PTZFAA 2008-26-0608.01.2009See AD compliance for detailsRolls-Royce Corporation (RRC) AE 3007A series turbofan engines These engines are installed on, but not limited to, Empresa Brasileira de Aeronautica S. A. (EMBRAER) EMB-135 and EMB-145 airplanesCracks in the HPT stage 2 wheelRolls-Royce Corporation ASB AE 3007A-A-72-367
196-08 PTZFAA 2008-26-1005.01.2009See AD compliance for detailsCessna Aircraft Company All serial numbers (S/Ns) of the airplanes listed in Table 1 of this AD (172, F172, 182, F182, 185, T210,…)Erroneous indications from the altimeter, airspeed, and vertical speed indicatorsSee AD
197-08 PTZFAA 2008-26-1128.01.2009See AD compliance for detailsPiper Aircraft, Inc. PA-46-350P PA-46R-350T PA-46-500TPIce  forming on the stall vaneSee AD