PTZ-AD 2006

Številka PTZReferenčna PTZDatum efektiveRok izvršitveProizvajalecVsebina PTZReferenčni SB
001-06 PTZFAA-2005-25-08.pdf23.1.2006As indicated in ADShadin; ADC-2000 air data computers (may be installed in Cessna 172,206G,208,210L, Piper PA-28-181,31-350,32-300,34-200T)Certain ADC-2000 units may display incorrect altitude info on the EFIS. Upgrade of Air Data Computer (see AD for p/n) is required.Shadin Service Bulletin SB28-05-002,Rev C, dated June 29, 2005
002-06 PTZFAA-2005-26-10.pdf31.1.2006Superseeded by 052-06 PTZ (N-2006-12-07)Lycoming engines; models 320,360,540 series with certain Engine Components Inc. (ECi) cylinder assemblies installedReported failures of the ECi cylinder assemblies. Removal & Replacement of certain cylinder assemblies from service.ECi Service Bulletin No. 05-08, dated September 1, 2005
003-06 PTZF-2006-011R1.pdf14.1.2006REVISEDAirbus SAS; A318, A319, A320, A321 AircraftEngine pylon spar box ribs; identify and repair ribs, that might not have been heat-treated in productionAirbus All Operators Telex A320-54A1015, dated December 14, 2005 or any later approved revision
004-06 PTZF-2006-007.pdf4.1.2006before the next flightCessna 182 and Reims F182, equipped with SMA SR305-230 engineEngine operation in cold conditionsSMA service Bulletin SB-C182-71-002, dated November 24, 2005
005-06 PTZI-2006-001.htm10.1.2006 Agusta; A109A & A109AII helicoptersInspection for cracks of tail rotor blades, P/N 109-0132-02-11/-15/-121Agusta Bolletino Tecnico 109-110 rev.A, dated December 12, 2005
109-110_3.pdf
006-06 PTZFAA-2005-24-10.pdf17.1.2006As indicated in ADBellanca (Champion) Aircraft Corp., 7GCBC Citabria and others, see listingPartial loss of Aileron control due to incorrectly swaged cable sleeve. 
087-04R2 PTZA-2004-004R2.pdf12.1.2006Not later than August 31, 2006Rotax; 912 A/F/S,914 F series enginesReplacement of coolant/Reduction of Cylinder Head Temperature Limits. This AD replaces AD A-2004-004 R1 (087-04R1 PTZ) 
007-06 PTZCF-2005-41.pdf15.2.2006When indicated, unless already accomplishedBombardier Inc. Model CL-600-2B19Shear Pin Failure in Pitch Feel Simulator Input Lever This AD Superseedes and cancels AD CF-2003-26Bombardier Alert SB A601R-27-144, dated September 15 2005, or later approved
008-06 PTZEASA-2005-0035.pdf30.12.2005See AD for detailsPiper Aircraft Inc., (The New); PA-28 and PA-32Repetitive Inspections on MLG casted oleo housing for cracks.The New Piper Aircraft, Inc. Service Bulletin 1131
093-05 R1 PTZEASA-2005-0023R2.pdf1.11.2005RevisedLycoming EnginesSame as original issue, prolonged period before initial inspection in order to allow more time to obtain the required tooling 
003-06 R1 PTZEU-2006-0136.pdf14.1.2006Superseeded by EU-2006-0136Airbus SAS; A318, A319, A320, A321 AircraftEngine pylon spar box ribs; identify and repair ribs, that might not have been heat-treated in production Airbus All Operators Telex A320-54A1015, dated December 14, 2005 or any later approved revision
009-06 PTZF-2006-040.pdf27.1.2006Upon receipt from January 27, 2006EUROCOPTER; EC 120 B helicoptersCertain s/n Spherical thrust bearings prohibition for flight (expecting correction)EC 120B Eurocopter Alert Telex No 04A006 or later approved revision of the same
010-06 PTZEASA-2005-021.pdf1.8.20051.may 2006Honeywell;Aicrafts, equipped with RCZ-83() and RCZ-85() Comm UnitsCorrection of the design deficiency- Incorporation of SB's on affected units.Honeywell SB A21-3851-005, A24-3851-002
011-06 PTZFAA-2006-03-08.pdf10.3.2006within 100 hours time-in-service (TIS) or the next 12 calendar months, whichever occurs firstAero Advantage; ADV200 series vacuum pumpsVacuum pumps removal from service. May be installed in Champion 7GCBC, Cessna 172M,N,P,182G,TU206G,U206B, Commander 112TC, Piper PA-18-150, PA-25-235,PA-28-140,PA-28-161, PA-28-181,PA-28R-200,PA-28R-201T,PA-31-350,PA-32-300, SOCATA MS 893A,MS893E, RALLYE 150 ST, TB 9 and others 
017-03R1CF-2003-05R1.pdf31.3.2006As indicated, unless already accomplishedBombardier Inc. Model CL-600-2B19; s/n 7003 and subsequentAmended aircraft applicability of the bulkhead inspectionASB A601R-21-054, Revisions A,B,C or later; ASB A601R-21-053, Revision A or later
012-06 PTZF-1997-144-038R1.pdf11.2.2006Effective date the original issue July 12,1997EUROCOPTER; SA 341/342 helicoptersupdated referenced Alert Service BulletinEUROCOPTER SA 341/342 ASB No. 05.32 R1
013-06 PTZ2006-04-10.pdf24.3.2006Within 100 flight hours or latest by may 23,2006Cessna Aircraft Company; Model 500,550,S550,560,560XL and 750 airplanesInstallation of identification sleeves on the wires of Fire extinguishing BottlesSee AD text
014-06 PTZ2006-04-12.pdf30.3.2006Within the compliance times specified in this AD unless the actions have already been doneGeneral Electric Company (GE); CF34-3A1 and -3B1 series turbofan enginesAdditional population of stage 5 and 6 LPT disks with possibility of Low-cycle-fatique (LCF) failure GE Alert Service Bulletin (ASB) No. CF34-AL S/B 72-A0173, Revision 05
015-06 PTZ2006-05-04.pdf7.4.2006Within the compliance times specified unless the actions have already been doneGeneral Electric Company (GE); CF34-1A,-3A,-3A1, -3A2,-3B and -3B1 series turbofan enginesRemoval of Certain Fan Disks From Service This AD supersedes AD 2001-10-03GE ASB CF34-BJ 72-A0088, Revision 1 and GE ASB CF34-AL 72-A0103
093-05 R2 PTZEASA-2005-0023R2.pdf   This Ad is superseded by EASA 2005-0023 R3 (PTZ 043-07 PTZ)1.11.2005As indicated in ADLycoming EnginesInspection of exhaust valves and guides in accordance with Lycoming SB 388C - Hi-Crome exhaust valves and guides exclusionLycoming Service Bulletin & Service Instruction
SB388C.pdf
SI1485A.pdf
016-06 PTZN-2006-06-03.pdf20.4.2006Within the compliance times specified unless the actions have already been doneCessna Aircraft Company; Model 500 and 501,550 and 551,S550,560 airplanesChafed Electrical wiring harness inside the fuel tankSee Table 2 for applicable service bulletin
017-06 PTZN-2006-06-16.pdf27.4.2006Within 50 hours Time-In-Service (TIS) or 6 months after the effective date of this ADLycoming Engines; AEIO-360, IO-360, O-360, LIO-360, and LO-360 Series Reciprocating EnginesRetirement of certain S/N crankshaftsLycoming engines MSB 566 supp.1
SB566S-1.pdf
018-06 PTZEU-2006-044.pdf28.2.2006Immediately after the effective date of this ADThielert Aircraft Engines; TAE 125-01Revision of Chapter 5 of the MM; Added new exchange interval for the LP fuel pumpThielert Service Bulletin
2005-152-Thielert-TM-TAE-125-0010.pdf
019-06 PTZEU-2006-0065.pdf6.4.2006Within the next 1000 hours Time-in-Service (TiS) or within 2 years after the effective date of this ADRobinson Helicopter Company; All Robinson R22 HelicoptersInstallation of landing skid extensions and shoes 
020-06R1 PTZEU-2006-0069-E-R1.pdf7.4.2006Within eight days of aircraft operation following the effective date of this ADAirbus; A318, A319, A320 and A321 aircraftThe forward lugs of MLG rib 5 fittings inspection and repairSee AD for details
021-06 PTZN-2006-07-06.pdf11.5.2006Within eight days of aircraft operation following the effective date of this ADCirrus Design Corporation; SR20 and SR22Inspection of the fuel line, installation of parts to protect the fuel lineCirrus Design Corporation Service Bulletin
SB2X-28-04R1.pdf
022-06 PTZCF-2006-04.pdf28.4.2006Within 60 days of the effective date of this ADBombardier Inc.; Model CL-600-2B19, all serial numbersBacklash wear limits in aileron PCUsSee AD for details
023-06 PTZEU-2006-0093.pdf5.5.2006Within 110 Flying hours or within 4 months- first limit reachedEurocopter, EC 120 helicoptersEngine controls- Collective levers twist grip assembly- bonding between the drive tube and the control pinionEUROCOPTER EC 120 Alert Service Bulletin No. 76A006
024-06 PTZCF-2006-07.pdf25.4.2006Within 90 days of the effective date of this directiveBombardier Inc. Model CL-600-2B19AC service Bus Contractor wiring modificationBombardier Alert SB A601R-24-121, dated April 18 2006, or later approved
025-06 PTZEU-2006-0106-E.pdf2.5.2006Immediately from the effective date of this ADAirbus; A318, A319, A320, A321 AircraftFuel - Main Fuel Pump System / Fuel Pumps Airworthiness Limitation AIRBUS AFM TR 4.03.00/28
026-06 PTZEU-2006-0092.pdf8.5.2006Within 50 hours Time-In-Service (TIS) from the effective date of this AD, see AD for detailsHartzell Propeller Inc.; Hartzel Propellers ( )HC-( )2Y( )-( ), installed on Lycoming ( )-360 series enginesHub cracks in Hartzell two blade "compact" series aluminum hub propellersSB227-R04.pdf
SB269-R00.pdf
027-06 PTZEU-2006-0108.pdf15.5.2006See AD for detailsAirbus; A318, A319, A320, A321 AircraftTemporary loss of all display unitsA315/319/320/321 Flight Manual Temporary Revision 4.02.00/22, AIRBUS Service Bulletin A320-31A1220 or latter approved revisions
028-06 PTZN-2006-10-21.pdf22.6.2006Within the compliance times specified in this AD unless the actions have already been doneLycoming Engines; 360 and 540 series with Engine Components Incorporated (ECi) Reciprocating Engine Connecting RodsTo prevent fatigue failure of the connecting rod. 
029-06 PTZEU-2006-0135.pdf5.6.2006Operational Limitation is mandatory from the effective date of this ADAirbus; A318, A319, A320 and A321 AircraftSpeed Limitation to 250 IAS with RAT (Ram Air Turbine) deployed - Valid During Flight Tests OnlyAFM TR 2.05.00/67 or later approved revisions
003-06 R2 PTZEU-2006-0136R2.pdf5.6.2006As indicated in ADAirbus; A318, A319, A320 and A321 AircraftNacelles/Pylons - Engine Pylon Spar Box RibsAOT A320-54A1015 Rev.2, dated May 18, 2006 or latter approved revisions
030-06 PTZCF-2006-12.pdf5.7.2006No later than 3 months from the effective dateBell Helicopter Textron Canada; Model 206A/B helicoptersVertical stabilizer (fin) supports One time inspection and recurring torque checkAlert Service Bulletin (ASB) 206-06-107 or later approved Revisions
031-06 PTZEU-2006-0153.pdf9.6.2006As indicated in ADAirbus; A318, A319, A320 and A321 AircraftAuxiliary Power Unit (APU)- Starter Motor and Air Intake System- Inspection/CleaningAIRBUS Service Bulletin A320-49-1068 rev. 1
032-06 PTZEU-2006-0112.pdf26.5.2006As indicated, unless already accomplishedAirbus; A318, A319, A320 and A321 AircraftMain Landing Gear Door ActuatorAIRBUS Service Bulletin A320-32-1309, any later approved revision and FAA AD 2007-06-18
033-06 PTZEU-2006-0150-2.pdf12.6.2006June 30th, 2006GROB Luft- und Raumfahrt; Astir CSElevator Spherical Attachment Bolt ReplacementGROB Service Bulletin
MSB_306-38-1.pdf
034-06 PTZEU-2006-0140-E.pdf25.5.2006As indicated in ADCTT Systems AB; Bombardier CL-600-2B19 with STC LBA.21E2.TA0270 zonal dryer installedZonal Drying System DeactivationLufthansa Technik AG SIL LHT 06-001
035-06 PTZCF-2006-11.pdf19.6.2006As indicated, unless already accomplishedBombardier Inc.; Model CL-600-2B19Inspection of Chemical Oxygen Generator for Improper Installation of Release PinBombardier Service Bulletins, listed in AD
036-06 PTZEU-2006-0162.pdf22.6.2006As indicated in ADAirbus; A318, A319, A320 and A321 AircraftSafe life Airworthiness Limitation Items- ALS Part 1 (Supersedes 012-04 PTZ (F-2004-032))A318/A319/A320/A321 MPD section 9-1 revision 06, approved June 13, 2003 and A318/A319/A320/A321 ALS Part 1, approved February 28, 2006
037-06 PTZEU-2006-0165.pdf16.6.2006June 30th, 2006Airbus; A318, A319, A320 and A321 AircraftAirworthiness Limitation Items (ALI)- Structural Maintenance- Superseedes 006-04PTZAirbus AI/SE-M4/95A.0252/96 issue 6, 7 or later approved revisions
038-06 PTZEU-2006-0166.pdf28.6.2006Within the next 1000 hours time-in-service (TIS) or within 2 years, whichever comes firstRobinson Helicopter Company, R44 HelicoptersDoors- Cotter pins installation 
039-06 PTZEU-2006-0167.pdf28.6.2006Within the next 1000 hours time-in-service (TIS) or within 2 years, whichever comes firstRobinson Helicopter Company; Model R22 helicopterDoors- Hinges Modification 
040-06 PTZEU-2006-0171.pdf3.7.2006Within the next 1000 hours time-in-service (TIS) or within 2 years, whichever comes firstSchweizer Aircraft Corporation; Model 269A, 269A-1, 269B, 269C, 269C-1 and 269D helicoptersFuel Vent Modification; to prevent release of fuel in the event of a roll-overSchweizer Service Letter L-168
041-06 PTZEU-2006-0172.pdf3.7.2006Before further flight, after the effective date of this DirectiveEnstrom Helicopter Corporation; F-28A and 280 series helicopters fitted with certain blade gripsInspection and rework of the tail rotor blade assy Service Directive Bulletin 0067
042-06 PTZEU-2006-0173.pdf3.7.2006Not later than May 31, 2007Bell Helicopter Textron Inc.; Bell 212 series helicopters with Sperry Helipilot automatic flight control systemRelocation of the Helipilot disconnect switch 
043-06 PTZN-2006-13-10.pdf7.8.2006See Original AD for detailsRaytheon Aircraft Company (Beech); C90ARudder trim tab-moisture drainage provisions- added serial numbers to FAA AD N-92-07-05SB55-2365, Revision 2
044-06 PTZN-2006-13-06.pdf26.7.2006Within the compliance times specified unless the actions have already been doneRolls-Royce Corporation (formerly Allison); model 250 turboshaft and turboprop enginesRemoval from service of certain P/N gas producer rotor assembly tie boltsVarious RRC Commercial Engine Bulletins
045-06 PTZEU-2006-0174.pdf5.7.2006As indicated in ADAirbus; A318, A319, A320 and A321 AircraftSupersedure of AD F-2005-191 (Si-099-05 PTZ), extended applicability and introduced a repetitive boroscopic inspection See AD text
046-06 PTZEU-2006-0176.pdf10.7.2006See AD for detailsAirbus; A318, A319, A320 and A321 AircraftSupersedes AD F-2005-028 (Si-019-05 PTZ) and mandates new, revised SB; see also FAA 2007-07-09AIRBUS Service Bulletin A320-28-1104 revision 03
047-06 PTZEU-2006-0184.pdf17.7.2006Within 36 months from the effective date of this ADAirbus; A319, A320, A321 AircraftSemi automatic cargo loading-Modification of fixed YZ latchesAIRBUS Service Bulletin A320-25-1294 Revision 1 or later
048-06 PTZEU-2006-0141.pdf9.6.2006As indicated in ADTurbomeca; Arrius 2F enginesSupersedes AD F-2005-122 (Si-068-05 PTZ), introduces revised SBTurbomeca Alert SB A319 79 4802, Update No 1
049-06 PTZN-2006-14-03.pdf9.8.2006Within the compliance times specified unless the actions have already been doneHoneywell International Inc. (formerly Garret); model TPE331 turboprop and TSE331 turboshaft enginesNew flight cycle counting method for first, second, and third-stage turbine rotors used in aircraft that make multiple takeoffs and landings without an engine shutdown, and removing turbine rotors from service that have reached or exceeded their cycle life limits.See AD text
050-06 PTZCF-2006-17.pdf   This AD is superseded by CF-2006-17R1 (068-07 PTZ)17.7.2006Within four months or prior to accumulating 800 hours air time from the effective date of this AD, whichever reached first, unless already accomplishedBombardier Inc. Model CL-600-2B19AC Contactor Failure - Ultem 2200 Terminal base plate SealingBombardier SB 601R-24-122, dated 27 June 2006 or later approved revisions
051-06 PTZEU-2006-0203.pdf19.7.2006See AD for detailsAirbus; A318, A319, A320 and A321 AircraftFuel Airworthiness Limitations; changes in maintenance/inspection tasks and operator internal documentation amendmentA320 Fuel Airworthiness Limitations, 95A.1931/05 Issue 1, or later approved revisions
052-06 PTZN-2006-12-07.pdf11.7.2006Within the compliance times specified unless the actions have already been doneLycoming engines; models 320,360,540 series with certain Engine Components Inc. (ECi) cylinder assemblies installedApplicability errors were found in Si-002-06 PTZ (AD N-2005-26-10). ECi Service Bulletin No. 05-08, Revision 2,dated February 28, 2006
05-8.pdf
053-06 PTZEU-2006-0220.pdf31.7.2006Within the next 8 weeks from the effective date of this ADRecaro Aircraft Seating GmbH;Passanger Seats Type 3410,3510,4400,4420 and 6510, delivered between 1.nov.2005 and 5.may 06Visual inspection of the seat shackleVarious Recaro Service Bulletins, listed in AD
054-06 PTZN-2006-15-08.pdf24.8.2006At the next scheduled inspection of the fuel control drive, but within 1,000 hours-in-serviceHoneywell International Inc., formerly Garrett; TPE331 Turboprop Engines With Affected Woodward FCU AssembliesInitial and Repetitive Inspection of Affected Woodward FCU AssembliesHoneywell Alert Service Bulletin (ASB) No. TPE331-A73-0271, -0262, -0254
055-06 PTZEU-2006-0221.pdf31.7.2006Unless already accomplished, listed actions must be performed within 3 months from effective date of ADSaab AB, Saab Aerosystems; SAAB SF340A and 340B all serial numbersFuel System Airworthiness Limitations (comprising maintenance/inspection tasks and Critical Design Control Configuration Limitations (CDCCL)SAAB Fuel Airworthiness Limitations Document No 340LKS 9033 or later
056-06 PTZEU-2006-0223.pdf7.8.2006See AD for detailsAIRBUS; A318, A319, A320 and A321; all certified models, all manufactured S/NFlight controls – Trimmable Horizontal Stabilizer Actuator- InspectionsAIRBUS Service Bulletin (SB) A320-27-1164 Revision 2, 3, 4
057-06 PTZCF-2006-19.pdf25.8.2006Within 1500 hours air time after the effective date of this AD, Repeat the inspection not to exceed 1500 hours air time, Within 4000 hours air time replace the existing engine exhaust nozzle attachment hardwareBombardier Inc. CL600-2B19 Regional Jet (CRJ), aircraft serial numbers 7003 through 7067, and 7069 through 7947.Engine Exhaust Nozzle In-Flight Loss INSPECTION and REPLACEMENT of the hardware attaching the engine nozzle to the engine flange.Bombardier service bulletin (SB) 601R-78-021
058-06 PTZEU-2006-0228-E.pdf28.7.2006EMERGENCY AD Upon receipt of this AD and before next flightAgusta S.p.a. A109A, AII, C, K2, E, S, LUHTail Rotor - Tail Rotor Pitch Control Link Assy P/N 109-0130-05-117 INSPECTIONAgusta - Agusta Alert SB 109-122, 109K-47, 109EP-70, 109S-5, 109L-001, 119-15
059-06 PTZEU-2006-0222.pdf31.7.2006See AD for detailsAIRBUS; A318, A319, A320 and A321 aircraft, all certified models, all S/N that are equipped with fuel pumps manufactured by Eaton Aerospace Limited (formerly FR-HITEMP limited) part number (PN) 568-1-27202-005 with a S/N from 6137 and above.Fuel - Main Fuel Pump System/Fuel PumpsSB A320-28-1152 and A320-28-1153
060-06 PTZN-2006-16-01.pdf15.8.2006within 60 days after the effective date of this AD, unless the actions have already been doneHamilton Sundstrand Propellers, Model 14RF-19 with propeller system actuator yoke arms, P/N 810436-2, which might be installed in actuator assemblies P/N790199-6. These propellers are installed on, but not limited to, SAAB 340 airplanes.To prevent actuator yoke arms breaking during flight, which could cause high propeller vibration and contribute to reduced controllability of the airplane. Replacement of all actuator yoke arms, P/N 810436-2, with improved actuator yoke arms, P/N 810436-3.Mark newly installed actuators. Do not install any actuator yoke arms, P/N 810436-2, into any propeller assembly.Hamilton Sundstrand Service Bulletin 14RF-19-61-113, Revision 1
061-06 PTZN-2006-16-04.pdf7.9.2006See AD for details (For fuel nozzles with a P/N listed in Table 3 within 50 operating hours after the effective date; P/N listed in Table 4 within 150 operating hours after January 5, 2005).Rolls-Royce Corporation (formerly Allison Engine Company, Allison Gas Turbine Division, and Detroit Diesel Allison) (RRC) 250-B and 250-C series turboshaft and turboprop engines; Engines Installed on, But Not Limited To- see table 2 (BELL 206)Minimizing the risk of sudden loss of engine power and uncommanded shutdown of the engine due to fuel contamination and collapse of the screen in the FUEL NOZZLE.Rolls-Royce Corporation Alert Commercial Engine Bulletins (CEBs); all at Revision 1, all dated August 30, 2004, listed in the Table 5 of this AD.
062-06 PTZEU-2006-0234.pdf24.8.2006Within the next 50 hours TIS after the effective date of this AD,unless accomplished previously, verify the installation of the forward plugs and stops of the seat railsCostruzioni Aeronautiche TECNAM; All models P92-J, P92-JS and P2002-JF aeroplanes, certified in any categoryEquipment & Furnishings - Seat Rail Stops - Inspection; Tecnam MANDATORY SB 001-CS dated 24th March 2006 or later approved revisions.
MSB_001-CS.pdf
063-06 PTZN-2006-16-07.pdf9.8.2006Within 800 flight hours or four months after the effective date of this AD, whichever occurs first, unless the actions have already been done in accordance with Bombardier SB 601R-24-122,dated June 27, 2006.Bombardier, Inc. (Formerly Canadair):Bombardier Model CL-600-2B19 (Regional Jet Series 100 & 440) airplanes, certificated in any category, S/N 7003 through 7990 inclusive and 8000 and subsequent.Prevention of short circuit failures of certain AC contactors, which could result in arcing and consequent smoke or fire.Instructions of Bombardier SB 601R-24-122, Rev A, dated July 13, 2006.
064-06 PTZEU-2006-0235-E.pdf   This AD is superseded by EASA EAD 2007-0138-E (PTZ 057-07)10.8.2006Mandatory measures from the effective date of this AD. At each check after the last flight of the day without exceeding 10 flying hours between two successive checks, visually check for absence of cracks in the blade pressure face and blade suction face.EUROCOPTER; AS 350 and AS 355 helicoptersEMERGENCY AD Tail Rotor - Tail Rotor Blade Skin - CheckEUROCOPTER AS 350 Alert Service Bulletin No. 05.00.40 Revision 1 and AS 355 Alert Service Bulletin No. 05.00.38 Revision 1 or later approved revisions.
065-06 PTZEU-006-0261-E.pdf28.8.2006Before the next flightEUROCOPTER (formerly EUROCOPTER-FRANCE, AEROSPATIALE,SUD-AVIATION)Emergency AD Oxygen - Oxygen Cylinders – Removal/Emptying AS 350 B3 and SA 315 B helicopters, all serial numbers with certain Oxygen Cylinders PN´sEUROCOPTER AS 350 Alert Service Bulletin No. 05.00.54,EUROCOPTER SA 315 Alert Service Bulletin No. 05.42, or any subsequent approved revision.
066-06 PTZCF-2006-20.pdf29.8.2006Within seven days, from the effective date of this directive.Bombardier Inc. Model CL-600-2B19, serial number 7003 thru 7990 and 8000 and subsequentHorizontal Stabilizer Trim – Uncommanded Motion  
067-06 PTZCF-2006-21.pdf29.8.2006Within seven days, from the effective date of this directive.Bombardier Inc. Model CL-600-2B16 (CL-604), serial number 5301 and subsequent.Horizontal Stabilizer Trim – Uncommanded Motion 
068-06 PTZEU-2006-0236.pdf24.8.2006See AD for compliance detailsAIRBUS (formerly AIRBUS INDUSTRIE); AIRBUS A319-100 series and A320-200 series, see AD for AC S/NFuel, Wings - Fuel system – Labels in Fuel TankSee AD for details
069-06 PTZEU-2006-0248.pdf1.9.2006The following measure is mandatory as from June 11, 2004, the effective date of DGAC AD No. F-2004-085EUROCOPTER, AS 350 HelicoptersEquipment and Furnishings – Emergency All-Up Operating Weight LimitationEUROCOPTER AS 350 Alert Service Bulletin No. 01.00.55 R1 or later approved revisions.
070-06 PTZEU-2006-0252.pdf1.9.200631.12.2006; See AD for detailsEUROCOPTER; SA 330, AS 332, SA 341/342, AS 350, AS 355, SA 360, SA 365, AS 365,EC 155, SE 3160 and SA 316/319 helicoptersEquipment and Furnishings – Hoist Operator’s Belt Snap HookEUROCOPTER Alert Service Bulletins: See AD for details
071-06 PTZEU-2006-0247.pdf1.9.2006See AD for compliance detailsEUROCOPTER (formerly EUROCOPTER-FRANCE, AEROSPATIALE); AS 350 HelicoptersRotor Flight Controls – Tail Servo-ControlEUROCOPTER AS 350 Alert Service Bulletin No. 67.00.30 or later approved revisions
072-06 PTZEU-2006-0249.pdf1.9.2006See AD for compliance detailsEUROCOPTER (formerly EUROCOPTER-FRANCE, AEROSPATIALE); AS 350 and AS 355 HelicoptersDoors – Sliding Door – Wear on Rollers and RailsEUROCOPTER AS 350 ASB No. 05.00.41 Rev 2;EUROCOPTER AS 355 ASB No. 05.00.39 Rev 2, as applicable, or later approved revisions.
073-06 PTZEU-2006-0262.pdf8.9.2006Within 9,000 Flight Cycles (FC) or 12,000 Flight Hours (FH), or 60 months,whichever occurs first after the effective date of this ADAIRBUS (formerly AIRBUS INDUSTRIE); A320 aircraftStabilizers – Rudder Actuator Fittings – ReplacementAIRBUS Service Bulletin A320-55-1030 original issue or later approved revisions and FAA AD 2007-06-17
074-06 PTZEU-2006-0263.pdf12.9.2006Within 8,000 flight cycles since the last MLG overhaul, or within 1,500 flight cycles or 6 months after the effective date of this directive, whichever occurs laterSaab AB, Saab Aerosystems (Saab Aircraft AB); SAAB SF340A and SAAB 340BLanding Gear – MLG Shock Strut & Axle Adaptors – Inspection/ModificationSAAB SB 340-32-133; and APPH Ltd. SB AIR83022-32-32 or AIR83064-32-12, as applicable, or later approved revisions.
075-06 PTZEU-2006-0251R1.pdf1.9.2006See AD for compliance detailsEUROCOPTER (formerly EUROCOPTER FRANCE, AEROSPATIALE); AS 350 AND AS 355 HelicoptersDoors – Sliding Door Rear Roller Support Shaft and Rear FittingEUROCOPTER AS 350 Alert Service Bulletins No. 05.00.47 and No. 52.00.30; or EUROCOPTER AS 355 Alert Service Bulletins No. 05.00.45 and No. 52.00.23, as applicable, or later approved revisions
076-06 PTZEU-2006-0264.pdf13.9.2006Within 18 months after the effective date of this directiveAVIOINTERIORS S.p.A.; Passengers Seats, various Part Numbers.Equipment & Furnishings – Passenger Seats Rear Fitting Assembly Attachment – Replacement The affected seats are known to be installed on, but not limited to, the following aircraft: Airbus A319, A320 and A321 series; Boeing 737, 747 and 777 series;McDonnell Douglas DC-9, DC-10 and MD90 series.Aviointeriors Service Bulletin 180/A84-01 Rev. 1 or later approved revisions.
077-06 PTZEU-2006-0267.pdf14.9.2006Unless accomplished previously, within 100 hours time-in-service (TIS) after the effective date of this AD, and thereafter at intervals not to exceed 100 hours TISReims Aviation, S.A.; F150, FA150, FRA150, F152 and FA152 seriesStabilizers – Horizontal and Vertical Stabilizer Attachment– Inspection/ReplacementReims Aviation SB 24, Revision n°1 or later approved revisions; or Cessna Single Engine Service Information Letter SE79-49, Revision # 1,dated April 28, 1980 or later approved revisions.
078-06 PTZEU-2006-0269.pdf14.9.2006Within the next 15 days after the effective date of this directive,unless previously accomplished; See AD for detailsHoneywell International Inc., MST 67A Mode S transponder; known to be installed in various aircraft- See AD for details (SAAB SF340A and 340B)Navigation Systems – Mode S Transponder - Modification Honeywell Software Bulletin SWB MST 67A–SW2
079-06 PTZN-2006-16-14.pdf22.9.2006Within 6,000 flight hours or 24 months after the effective date of this AD, whichever is first.AIRBUS; Model A318, A319, A320, and A321 airplanes, certificated in any category, except airplanes having manufacturer serial numbers (MSN) 2155 and subsequentTo ensure that, in the event of an engine fire, the valve actuator functions will properly block the fuel flow to the engine and prevent an uncontrollable fire.Airbus SB A320-28-1122, Rev 01, including Appendix 01; FRHiTEMP Service Bulletin HTE190001-28-003, dated March 30, 2004.
080-06 PTZN-2006-17-04.pdf1.9.2006Within the next 5 hours TIS after the effective date of this AD on airplanes that have not had a 100-hour or annual inspection of the engine installation fuel hoses for security and tightness of the end fittingsCessna Aircraft Company; Models: 172R, 172S, 182T,T182T, 206H and T206H (see S/N´s)Inspection of the two end fittings on each of the flexible fuel hoses located in the engine compartment for the correct torque valuesCessna Service Bulletin No. SB06-71-02, dated June 19, 2006
081-06 PTZN-2006-16-18.pdf25.9.2006Within 14 days and within 90 days after the effective date of this AD (see AD for compliance details)Sandel Avionics Incorporated; (Sandel) Model ST3400 terrain awareness warning system/radio magnetic indicator (TAWS/RMI) unitsInstallation of warning placard on the TAWS/RMI and revising the Limitations section of the airplane flight manual (AFM) as result of in-flight bearing error. Units installed on various small and transport category airplanes see table 1 foe details (for example- Cessna 208, 208B, 421C; 501, 525, 550, 560, 650, S550)Sandel ST3400 Service Bulletin SB3400-01,Rev B, dated Sept. 15, 2004
082-06 PTZN-2006-17-13.pdf27.9.2006You are responsible for having the actions required by this AD performed within 60 days after the effective date of this AD, unless the actions have already been done.RECARO Aircraft Seats GmbH & Co; (RECARO) Model 3410 302, 303, 306, 307, 314, 316, 317, 791, 792, and 795 series seats.Replacing the existing attachment bolts for the seat belts with longer attachment bolts. These seats are installed on, but not limited to, Boeing 737, 747, 777 and Airbus A319-100 series, A320-200 series, and A321-200 series airplanes.RECARO service bulletin SB-No.: 3410-25MR477, Rev 3, dated May 17, 2004
083-06 PTZEU-2006-0273.pdf14.9.2006See AD for compliance detailsEUROCOPTER (formerly EUROCOPTER-FRANCE, AEROSPATIALE); AS 350 and AS 355 HelicoptersFuselage – RH Cabin Vibration Damper & Blade – Inspection /Replacement / ModificationEUROCOPTER AS 350 Alert Service Bulletin (ASB) No. 05.00.48 and 53.00.34; and EUROCOPTER AS 355 ASB No. 05.00.46 and No.53.00.22, as applicable, or later approved revisions.
084-06 PTZEU-2006-0274.pdf15.9.2006Not later than at the next annual inspection after the effective date of this AD or within 12 months after the last inspection. Thereafter, at intervals not exceeding 12 months, repeat the inspectionCarling Technologies, Inc.; Rocker-type Switches,Part Number (P/N) TA 201TBWElectrical Power – Switches – Inspection/Replacement This switches known to be installed in, but not limited to,aircraft manufactured by the Piper Aircraft Corporation, Cessna Aircraft Company and Grumman American Aviation Corporation, certificated under FAR Part 23.This AD is superseded and canceled by EASA AD 2006-0375
085-06 PTZEU-2006-0279.pdf17.9.2006Prohibited use in flight of the PARACHUTE SHOP equipments with a manufacturing date after 1st Jan 2001. Equipment must be removed from service.PARACHUTE SHOP; Parachute Harnesses and Reserve Canopies (see AD for Applicability)Equipment/Furnishings – Parachute Equipment – Removal from Service.None
086-06 PTZEU-2006-0275.pdf22.9.2006Within the next scheduled 100-hours or annual inspection but no later than three (3) months after the effective date of this AD.Agusta S.p.a.; AB206A and AB206B helicoptersStabilizers - Vertical Fin Supports - InspectionAgusta “Bollettino Tecnico” 206-240 issued on 5 July 2006 or later approved revisions.
087-06 PTZN-2006-18-12.pdf13.10.2006Required as indicated in AD, unless accomplished previously.Saab Aircraft AB; Model SAAB-Fairchild SF340A (SAAB/SF340A) airplanes and SAAB 340B airplanes,To prevent false warning indications to the flightcrew from the hot detection system of the tail pipe harness of the engine nacelles due to discrepancies of the harness.Saab SB 340-26-030, dated Oct 28, 2002; or Saab SB 340-26-018, Rev 02, and 340-26-029, both dated Oct 28, 2002
088-06 PTZN-2006-18-15.pdf25.9.2006Within 50 operating hours time-in-service (TIS) after the effective date of this AD,Within every 100 operating hours TIS after the last propeller hub ECI inspection, or at every annual inspection,perform repetitive ECIs.Hartzell Propeller Inc.; ( )HC-( )2Y( )-( ) series propellers with non-suffix SN propeller hubs installed on Lycoming O-, IO-, LO-, and AEIO-360 series reciprocating engines.Could be installed on different aircraft (see AD).Prevent failure of the propeller hub causing blade separation and subsequent loss of airplane control. Performing Propeller Hub Eddy Current Inspection (ECI).Hartzell Propeller Inc. SB HC-SB-61-227
SB227-R05.pdf
089-06 PTZEU-2006-0280.pdf26.9.2006See AD for compliance detailsAIRBUS (formerly AIRBUS INDUSTRIE); A319, A320 and A321 aircraftElectrical Power, Engine – Integrated Drive Generator connector on IAE V2500 engine – Operational ProcedureAIRBUS SB A320-71-1030 original issue, AIRBUS SB A320-71-1034 original issue or later approved revisions; AIRBUS AFM TR 4.02.00/20
090-06 PTZEU-2006-0281.pdf28.9.2006See AD for compliance detailsEXTRA Flugzeugproduktions- und Vertriebs-GmbH; (former Extra Flugzeugbau GmbH); EA 300 aircraftFuselage –Upper Longeron at Horizontal Stabilizer - Inspection/ModificationEXTRA Service Bulletin No. 300-2-95, Issue F or later approved revisions.
2003-001R1-sb-300-2-95-issue-f.pdf and FAA 2007-02-11
091-06 PTZEU-2006-0171-R1.pdf24.9.2006Within the next 1,000 hours time-in-service after 03 July 2006, but not later than 03 July 2008,whichever occurs first.Schweizer Aircraft Corporation; Hughes Helicopters, Inc.; Schweizer (Hughes) 269 SeriesFuel – Fuel Vent System – ModificationSchweizer Service Letter L-169 dated 10 August 2000
092-06 PTZCF-2006-10-_R2.pdf10.10.2006As indicated in AD, unless already accomplished.Bell Helicopter Textron Canada (BHTC), Model 206 A/B series helicoptersFuel Distribution SystemAlert Service Bulletin (ASB) 206-05-103, Revision A, dated 12 July 2006
ASB_206-05-103_Rev_A.pdf
093-06 PTZN-2006-19-04.pdf17.10.2006See AD for compliance detailsHoneywell International, Inc.: certain Communication (COM) units and Mode S transponder- See AD for detailsTo prevent the transponder of the COM unit from going into standby mode, which could increase the workload on the flightcrew and result in improper functioning of the traffic alert and collision avoidance system. Installed in- see AD for details: Bombardier, Cessna (Model 550 and 560 and 650), Dassault (Falcon), EMBRAER, Learjet, Lockheed, Raytheon, certificated in any category.Different Honeywell Alert Service Bulletins- See Table 1 in AD
094-06 PTZN-2006-19-10.pdf24.10.2006Within 50 hours time-in-service or within 180 days,whichever occurs first after the effective date of this ADCirrus Design Corporation; airplane models SR20 and SR22To prevent the crew seats from folding forward during emergency landing dynamic loads with consequent occupant injury.Cirrus Design Corporation SB SB 2X-25-17 R1, Issued:December 15, 2005, Revised: January 20, 2006
SB2X-25-17R1.pdf
095-06 PTZzacasna_odredba.pdf3.10.2006Takoj, velja do preklicaVsi batni letalski motorjiPrepoved uporabe avtomobilskega bencina (čisti bencin ali mešanica z letalskim bencinom 100LL) za batne letalske motorje, razen v primerih, če je proizvajalec letalskega motorja drugače določil, kar se dokaže z originalnim priročnikom za uporabo letalskega motorja, ki je za tip in serijsko številko letalskega motorja potrjen s strani proizvajalca.SI1070N.pdf
096-06 PTZEU-2006-0286-E-Corr.2.pdf25.9.2006Required as indicated, unless accomplished previously in accordance with EAD 2006-0261-E, See AD for detailsINTERTECHNIQUE, Zodiac Aircraft Systems; Oxygen Reserve CylindersOxygen - Oxygen Reserve Cylinders – Removal/Emptying Which are known to be installed on,but not limited to Airbus A300, Dassault Aviation Mystère-Falcon 20, Mystère-Falcon 50, Falcon 200 and Falcon 900 aircraft; Pilatus aircraft; Eurocopter SA 315 B and AS 350 B3 helicopters;and Hindustan Aeronautics Limited helicopters.INTERTECHNIQUE SB GLD/GLF-35-150; EUROCOPTER AS 350 Alert Service Bulletin No. 05.00.54; EUROCOPTER SA 315 Alert Service Bulletin No. 05.42, or any subsequent approved revision.
097-06 PTZEU-2006-0295-E.pdf28.9.2006Inspection as per Diamond MSB 40-048/2 has to be carried before the next flight but not later than 30 November 2006.Diamond Aircraft Industries Inc., Canada; DA 40Engine – Contamination of the Engine Fuel System -InspectionDiamond Aircraft Industries Mandatory Service Bulletin, MSB 40-048/2 or later approved revisions.
098-06 PTZEU-2006-0292.pdf9.10.2006Required as indicated in AD compliance details, unless already accomplished in accordance with CAA UK AD 007-12-83 Revision 1.Enstrom Helicopter Corporation; All Enstrom F-28 and 280 series helicopters.Tail Rotor – Pitch Link & Pitch Arm Plate – Inspection/Replacement 
099-06 PTZEU-2006-0290.pdf9.10.2006After the effective date of this directive, replacement of the listed parts in the AD is required at or before the accumulation of the following times in service.Enstrom Helicopter Corporation; All 480 and 480B HelicoptersTime Limits / Maintenance Checks – Life Limited Components – ReplacementEnstrom Service Information Letter (SIL) T-002
SIL_T-002R4.pdf
100-06 PTZN-2006-20-09.pdf3.11.2006You are responsible for having the actions required by this AD performed within the compliance times specified unless the actions have already been doneLycoming Engines (formerly Textron Lycoming); (L)O-360, (L)IO-360, AEIO-360, O-540, IO-540, AEIO-540, (L)TIO-540, IO-580, and IO-720 series reciprocating engines listed in ADTo prevent failure of the crankshaft, which will result in total engine power loss, in-flight engine failure, and possible loss of the aircraft.You must use the service information specified in Table 1 of this AD to perform the actions required by this AD.
SB569A.pdf
SI1009AS.pdf
101-06 PTZCF-2006-20_R1.pdf16.10.2006Within 14 days and Within 12 months of the effective date of this directive, see AD for detailsBombardier Inc. Model CL-600-2B19, serial numbers 7003 thru 7990 and 8000 thru 8066.Horizontal Stabilizer Trim – Uncommanded MotionAFM Temporary Revision (TR) RJ/152-5 dated 03 Oct 2006; Bombardier In-Service ModSum No. IS601R27410051,Revision C, approved 29 September 2006; Bombardier Service Bulletin (SB) 601R-27-147 dated 28 September 2
102-06 PTZCF-2006-21_R1.pdf16.10.2006Within 14 days and Within 12 months of the effective date of this directive, see AD for detailsBombardier Inc. Model CL-600-2B16 (CL-604), serial numbers 5301 through 5665.Horizontal Stabilizer Trim – Uncommanded MotionAFM Temporary Revision (TR) 604/21-1 dated 03 October 2006; Bombardier Alert Service Bulletin (ASB) A604-27-029 dated 28 September 2006; Bombardier ASB A604-27-029 dated 28 September 2006
103-06 PTZEU-2006-0316-E.pdf17.10.2006EMERGENCY AD; Before the next engine start up from the effective date of this AD,Within 5 hours of operation after the effective date of this AD, see AD for detailsBRP-Rotax GmbH & Co. KG; Bombardier-Rotax GmbH & Co. KG;Bombardier-Rotax GmbH;Engine – Magnetic Plug – Inspections installed on, but not limited to: Sky Arrow, Aeromot, Aircraft Philipp, Aquila, Cessna 150 and A150, Diamond (formerly HOAC) H 36 Dimona, HK 36 series Super Dimona, DV 20 Katana and DA20-A1 Katana;Evektor-Aerotechnik, Grob, Issoire, Reimsn Aviation F150 and FA150 series, Scheibe, Stemme, Tecnam, W.D. Aircraft.BRP-Rotax Alert Service Bulletin, ASB-912-051 and ASB-914-034 or later approved revisions.
ASB-912-051.pdf
104-06 PTZEU-2006-033414.11.2006Not later then 30 months from effective dateThales 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: - Dash 8-400; - Airbus A318, A319, A320, A321, A330, A340 (all series); - Boeing 717, 727, 737, 747, 757, 767, 777 (all series).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 or later approved revisions.
105-06 PTZFAA-2006-22-0501.12.2006See AD for detailsApplies to aircraft, certificated in any category, equipped with a Honeywell Primus II RNZ-850( )/-851( ) integrated navigation unit (INU); including, but not limited to, Jetstream Model 4101; Bombardier Model BD-700-1A10 series airplanes; Model Bombardier CL-215-6B11 (CL-415 variant) series airplanes; Cessna Model 560, 560XL, and 650 airplanes; Dassault Model Mystere-Falcon 50 series airplanes; AvCraft Dornier Model 328-100 and -300 series airplanes; Empresa Brasileira de Aeronautica S.A. (EMBRAER) Model EMB-135 airplanes and Model EMB-145, -145ER, -145MR, -145LR, -145XR, -145MP, and -145EP airplanes; Learjet Model 45 airplanes; Raytheon Model Hawker Inspection to determine wheather certain modifications have been doneHoneywell Tehnical Newsletter A23-3850-001, Rev 1.
106-06 PTZEU-2006-032313.11.2006At the next scheduled maintenance inspection, or at the next annual shopvisit, whichever occurs first after the effective date of this directiveAPEX AIRCRAFT;DR 400/180 and DR400/180R aircraftPower Plant – Air Intake Box – Inspection/ModificationAPEX AIRCRAFT SB 040706 dated June 19th 2006 or later approved revisions1
107-06 PTZFAA-2006-23-0213.12.2006Within 100 hours time-in-service after December 13, 2006 or At the next annual inspection that occurs at least 30 days after December 13, 2006Raytheon Aircraft Company (Formerly Beech); C90A, B200, B200C, B300, B300CTo detect and correct improperly assembled or damaged flight controls Raytheon Aircraft Company Mandatory Service Bulletin Number SB 27-3761, Issued: February 2006
108-06 PTZFAA-2006-23-0428.11.2006Prior to further flight, unless already done, inspect engine fuel system for possible contamination of fuel Diamond Aircraft Industries GmbH: Model DA 40 airplanes equipped with Garmin G1000 supplemental type certificate (STC) SA01254WI Some parts of the installed fuel system indicating system were contaminated with particles from the manufacturing process. Diamond Aircraft Industries GmbH Mandatory Service Bulletin No. MSB-40-048/2, Revision 2, dated September 26, 2006
109-06 PTZEASA 2006 - 034528.11.2006During each pre-flight inspection and “100-hours” inspectionMT-Propeller Entwicklung GmbH; All MT- fixed pitch propellers and MTV- variable pitch propellers MTV-1, MTV-2, MTV-3, MTV-5, MTV-6, MTV-7, MTV-9, MTV-10, MTV-11, MTV-12, MTV-14, MTV-15, MTV-17, MTV-18, MTV-20, MTV-21, MTV-22 and MTV-24 manufactured before 1995 and not overhauled since April 1994. Installed on, but not limited to: René Fournier RF4 Apex ATL Apex DR400 Extra EA-300 EADS Socata RallyePiper PA-46Propeller – Blade Leading Edge Protection – InspectionMT-propeller Service Bulletin No. 8B dated March 8, 2006 or later approved revisions; Operation and Installation Manual E-112, E-118, E-124, E-148, E-309
110-06 PTZEASA EAD 2006-0347-E17.11.2006Before next flight after the effective dateAnd Thereafter, at intervals not to exceed 55 flight hoursAPEX AIRCRAFT; All DR 400 series aircraft, all models except the DR 400/500; see AD for detailsWings – Lower Surface Fabric Covering – Inspection
111-06 PTZCF-2006-23   This AD is superseded by CF-2006-23 R1 (see 042-07 PTZ)04.12.2006At the next scheduled main rotor hub disassembly, but no later than 25 January 2007Bell Helicopter Textron Canada; Model 206 A and Model 206 B certain S/N; see AD for detailsMain Rotor Latch Bolts - Removal from ServiceAlert Service Bulletin (ASB) 206-06-109, or later revisions
112-06 PTZEASA 2006 - 0153 R111.12.2006See AD compliance for detailsAIRBUS, (formerly AIRBUS INDUSTRIE); AIRBUS A318, A319, A320 and A321 aircraftSee AD for detailsAuxiliary Power Unit (APU) - Starter Motor and Air Intake System –Inspection/CleaningAIRBUS Service Bulletin A320-49-1068/ A320-49-1070/ A320-49-1075
113-06 PTZFAA 2006-24-07 03.01.2007See AD compliance for detailsHartzell Propeller Inc. (formerly TRW Hartzell Propeller) and McCauley Propeller Systems (formerly Cessna Aircraft Co.) propellers (certain P/N and S/N- see AD) serviced by Oxford Aviation Limited, doing business as CSE Aviation (UK)CSE Aviation failed to perform some specific inspections and repairs
114-06 PTZFAA 2006-24-0819.12.2006See AD actions and compliance for detailsPratt & Whitney Canada (P&WC) PW535A turbofan engines that have fuel manifold, part number (P/N) 3025267-01, installed.These engines are installed on, but not limited to Cessna Airplane Co. model 560 Citation Ultra Encore airplanes. Unsafe condition as fuel manifold leakage that could result in engine fire, in-flight shutdown or damage to the airframe. Transport Canada Airworthiness Directive CF-2006-22, dated Oct 26, 2006, and P&WC Alert Service Bulletin PW500-72-A30314 dated Sep. 27, 2006
115-06 PTZFAA 2006-25-0108.01.2007See AD compliance for detailsInternational Aero Engines AG (IAE) V2522-A5, V2524-A5, V2527-A5, V2527E-A5, V2527M-A5, V2530-A5, and V2533-A5 turbofan engines Prevention of the No. 3 bearing failure, which could result in an in-flight shutdown (IFSD) and smoke in the cockpit and cabin.IAE SB No. V2500-ENG-72-0452; IAE SB No. V2500-ENG-72-0459 IAE SB No. V2500-ENG-72-0460
116-06 PTZEASA 2006-0353 This AD is superseded by EASA 2007-0010 (see PTZ 007-07)18.12.2006See AD compliance for detailsAll Agusta Helicopters A109E where Tail Rotor blades P/N 109-8132-01-111are installed.Tail Rotor - Tail Rotor Blades P/N 109-8132-01-111 –Inspection/ReplacementAgusta Bollettino Tecnico 109EP-30 Rev. C,Agusta A109E Maintenance Planning Manual Rev. 1
117-06 PTZEASA 2006-0318 R120.10.2006See AD compliance for detailsEUROCOPTER DEUTSCHLAND GmbHEC 135 helicopter, all models, having certain components installed (see AD for details)Rotorcraft Flight Control – T/R Control Linear Transducer(LVDT Collective) Bearing– Inspection/Replacement & Rod and Floor ModificationEurocopter Deutschland EC 135 ASB No. EC135-67A-012 Revision 1 dated 18 October 2006
118-06 PTZEASA Emergency AD 2006-0371-E18.12.2006See AD compliance for detailsAgusta helicopters AB206A and AB206B series having Main Rotorlatch bolts P/N 206-010-169-1/-3 or P/N 206-011-122-3 installedMain Rotor - Main Rotor latch bolts P/N 206-010-169-1/-3 and P/N 206-011-122-3 -ReplacementTransport Canada AD CF-2006-23and Agusta Alert “Bollettino Tecnico” 206-241 original issue
119-06 PTZFAA 2006-25-1519.01.2007Within 90 days after the effective date of this AD, see AD compliance for detailsSicma Aero Seat: third occupant seat assemblies, 133 series, nstalled on, but not limited to, Airbus A319, A320, and A321 series airplanes.Visual inspect the installation of the two headrest bushings and install Mecanindus pins to secure the bushingsDGAC 2000-042(AB), dated January 26, 2000
120-06 PTZEASA 2006-037529.12.2006Not later than at the next annual inspection after 15 September 2006 or within 12 months after the last inspection as previously required by CAA UK Additional AD 001-09-96 or EASA AD 2006-0274, whichever occurs later, visually inspect the affected switches.Thereafter, at intervals not exceeding 12 months, repeat the inspectionCarling Technologies, Inc. Rocker-type Switches, The affected switches are known to be installed on, but not limited to, aircraft manufactured by the Piper Aircraft Corporation, Cessna Aircraft Company and Grumman American Aviation Corporation, certificatedunder FAR Part 23.Electrical Power – Switches – Inspection/ReplacementThis AD supersedes and cancels EASA AD 2006-0274
121-06 PTZFAA AD 2006-23-0213.12.2006See AD compliance for detailsThis AD affects certain  airplane models and S/N that are certificated in any category. Raytheon Aircraft Company (Formerly Beech): C90A, B200, B200C, B300, B300CSee AD for S/NInspect the flight controls for improper assembly or damage, and if any improperly assembled or damaged flight controls are found, take corrective action Raytheon Aircraft Company Mandatory Service Bulletin Number SB 27-3761, Issued: February 2006.