PTZ-AD 2005

Številka PTZReferenčna PTZDatum efektiveRok izvršitveProizvajalecVsebina PTZReferenčni SB
001-05 PTZENAC_2004-522.pdf30.12.2004Within 30 days as of the effective date of this AD, unless already accomplished.Vulcanair (former Partenavia); all P68 airplane variantsCarry out the operational checks/inspections/modifications.MSB No.128, dated 12. October 2004
002-04 PTZF-2004-192_(A).pdf1.1.2005Before January 31, 2006.TURBOMECA; ARRIEL 2 turboshaft enginesCheck the torque measurements made by the production Digital Engine Control Unit (DECU) which is installed on the engineMandatory Service Bulletin A 292 73 2816 original issue or later approved revision.
104-04 R1 PTZF-2004-189_(B)_R1.pdf15.1.2005Within the compliance times specified in this AD.AIRBUS SAS; A319, A320 and A321 aircraftInspection of the uppermost fastener holes.AIRBUS Service Bulletin A320-53A1135 Revision 3, A320-53-1140 Revision 2, A320-53-1148, A320-53-1149, A320-53-1160, A320-53-1158
003-05 PTZF-2005-010_(A).pdf5.1.2005No later than within the next 25 flying hours, then at intervals of no more than 100 flying hours.EUROCOPTER; AS 350 helicoptersCheck the spar of the upper and lower vertical fins for absence of cracks.EUROCOPTER AS 350 Alert Telex No. 05.00.46
004-05 PTZF-2004-196_(A).pdf28.12.2004No later than within the next 50 flying hours from the effective date of this ADEUROCOPTER; AS 350 helicoptersCheck of the tail servo-control.Alert Telex EUROCOPTER AS 350 No 67.00.30.
005-05 PTZF-2005-013_(B).pdf29.1.200529.01.2005AIRBUS SAS; A320 aircraftInsert in the Minimum Equipment List (MEL) of the aircraft, the Temporary Revision (TR) TR No 01-27/01H issue 01 of the Master Minimum Equipment List (MMEL)AIRBUS Service Bulletin A320-27-1149, MMEL A318/A319/A320/A321 TR No 01-27/01H issue 01 approved by JAA on November 3, 2004.
006-05 PTZFAA_AD_2004-26-02.pdf26.1.2005at the first piece-part exposure after 6,000 cycles-since-new (CSN), but no later than 20,000 CSN.GE Aircraft Engines (GE); CF34-3A, CF34-3A2, CF34-1A, CF34-3A1, CF34-3B, and CF34-3B1 Series Turbofan EnginesHPC Spool Replacement After the effective date of this AD: (1) Do not install any HPC forward spool, P/N 6078T56P03; (2) Do not install any HPC forward spool, P/N 6078T56P04, with more than 0 CSN. 
007-05 PTZCF-2005-03.pdf8.2.2005Within 14 days of the effective date of this directive.Bombardier Inc.; Model CL-600-1A11 (600), CL-600-2A12 (601 Variant), CL-600-2B16 (601-3A Variant), CL-600-2B16 (601-3R Variant), CL-600-2B16 (604 Variant)Amend all copies of the AFM by incorporating the applicable Temporary Revision (TR) and advise all flight crews on the changes introduced through the AFM TR. 
008-05 PTZCF-2005-01.pdf2.2.2005Within 14 days after the effective date of this directive.Bombardier Inc.; Model CL-600-2B19 Regional Jet Series 100 and 440 aircraftAmend the AFM by inserting Temporary Revision (TR) RJ/149-1 dated 1 February 2005 and advise all flight crews on the changes introduced through the AFM TR. 
009-05 PTZCF-2005-02.pdf2.2.2005Within 14 days after the effective date of this directive:Bombardier Inc.; CL-600-2C10 Regional Jet Series 700 and 701, and CL-600-2D24 Regional Jet Series 900 aircraft.Amend all copies of the AFM by incorporating the applicable Temporary Revision (TR) and dvise all flight crews on the changes introduced through the AFM TR. 
010-05 PTZCF-2004-27.pdf28.5.2004At the next annual inspection, but not later than 31 January 2005, unless already accomplished.Bell Helicopter Textron Canada (BHTC); Model 206B helicopters, Serial Number 3567 through 4577 and 5101 through 5284.Inspect the inside door handle assembly.BHTC ASB 206-04-102, dated 24 September 2004
011-05 PTZFOCA_AD_HB-2004-491.pdf30.12.2005Within the next 60 days after 30 December 2004.PILATUS AIRCRAFT LTD; All Model B4-PC 11, B4-PC 11A and B4-PC 11AF gliders.Inspect the control-column support P/N 112.35.11.072 for cracks. If during the inspection in paragraph 3.1.1. cracks are found; before further flight, replace the support P/N 112.35.11.072 with a new part. This AD superseded 027-03 R1 PTZ (FOCA AD HB-2003-199R1)PILATUS B4-PC 11 Service Bulletin No. 1005 REV No. 2, dated 22 April 2004.
012-05 PTZFAA_AD_98-20-38R1.pdf18.2.2005Within 30 days after November 4, 1998Raytheon Aircraft Company; Beech 200 Series AirplanesRevise the FAA-approved Airplane Flight Manual (AFM) by incorporating the following into the Limitations Section of the AFM. This may be accomplished by inserting a copy of this AD in the AFM. 
013-05 PTZFAA_AD_2005-01-18.pdf1.3.2005Within the compliance times specified in this AD.Raytheon Aircraft Company; Beech 100, 200, and 300 Series AirplanesDetect and correct any cracked fuselage stringers in the rear pressure bulkhead area, which could result in structural damage to the fuselage.Raytheon Mandatory Service Bulletin SB 53-2472, Rev. 4, Issued: June, 1993, Revised: July, 2003.
014-05 PTZEASA_V2500_PAD_2005_001.pdf17.1.2005Within 500 flight hours but no later than December 31, 2005 or at the next removal of the FuelInternational Aero Engines (IAE); V2500-A5 series enginesInspect the area of the fuel filter cover of the Fuel Cooled Oil Cooler (FCOC). If fuel leakage is observed. This AD supersedes EASA member state AD number: France
DGAC_2003-355(B)_R2.pdf
Service Bulletin IAE 79-0085, Service Bulletin IAE 79-0086
015-05 PTZG-2005-0004.pdf30.1.2005Before further flight.SLINGSBY AVIATION LTD; Model T67 all Series aeroplanes.Thereafter, inspect the tailplane support brackets. Cracked tailplane support brackets must be replaced. Repetitive inspection of tailplane support brackets for aircraft where the brackets have previously been replaced.SLINGSBY_No__179_R3.pdf
090-02 R2 PTZCF-2002-35R2.pdf30.1.2005Within 60 days of the effective date of this directive,Bombardier Inc.; Model CL-600-2B19 AirplaneAileron Control Checks. Amend the Transport Canada approved maintenance schedule 
016-05 PTZFAA_AD_2005-01-19.pdf23.2.2005Within 180 days after effective date of this ADGARMIN International Inc.; GTX 33, GTX 33D, GTX 330, and GTXSoftware UpgradeMandatory Software Service Bulletin No.: 0304, Rev B, dated June 12, 2003 or No.: 0409, dated July 19, 2004
017-05 PTZFAA_AD_2005-01-04.pdf22.2.2005Within the compliance times specified in this AD.Raytheon Aircraft Company; 90, 99, 100, 200, and 300 SeriesDocumented compliance with AD 98–15–13 or follow PART II of the ACCOMPLISHMENT INSTRUCTIONS section in Raytheon Aircraft Mandatory Service Bulletin SB 2718, Revision 1, dated June 1997; or Revision 2, dated April 2000.Mandatory Service Bulletin SB 2718, Revision 1, dated June 1997; or Revision 2, dated April 2000.
018-05 PTZFAA_AD_2005-01-10.pdf22.2.2005Within the next 100 hours TIS after effective date of this AD), unless already done.The New Piper Aircraft, Inc.; Models PA-23-235, PA-23-250, and PAE23-250 AirplanesReplace any oil reservoir and installed oil reservoir hoses.The New Piper Aircraft, Inc. Vendor Service Publication No. 166, dated August 20, 2004, and the procedures in Garrett Aviation Service Bulletin No. 1002143, Revision A, dated June 18, 2004.
050-03 R1 PTZCF-2003-14R1.pdf26.2.2005Within the compliance times specified in this AD.Bombardier Inc.; Model CL-600-2B19 AirplaneA. Inspection and Repair of Electrical Harnesses B. Modification of Routing and Support of Electrical HarnessesRevision A of ASB A601R-27-101 or the original issue of ASB A601R-27-133
018-05 PTZFAA_AD_2005-05-53_Emergency.pdf5.3.2005Prior to further flightCessna Aircraft Company (Cessna); Models 172R, 172S, 182T, and T182T AirplanesFollow Chapter 5 TIME LIMITS/ MAINTENANCE CHECKS of whichever of the following applies: • Model 172 Maintenance Manual using the List of Effective Pages, dated June 7, 2004. • Model 182/T182 Maintenance Manual using the List of Effective Pages, dated March 1, 2004. 
019-05 PTZF-2005-028_(B).pdf26.2.2005Superseded by EU-2006-0176 (Si-046-06 PTZ)AIRBUS SAS; A318, A319, A320 and A321 aircraftFuel system - Prevention against explosion risks - In tank bondingService Bulletin AIRBUS A320-28-1104.
020-05 PTZF-2005-031_(B).pdf16.2.2005Before December 31st, 2009,AIRBUS SAS; A320 aircraftFuel system - Fuel pumps - Prevention against explosion risksAIRBUS Service Bulletin A320-28-1008 Revision 1 and A320-28-1054
021-05 PTZF-2005-032_(A).pdf16.2.2005Within the compliance times specified in this AD.EUROCOPTER; AS 350 helicoptersDoors - Pin of the sliding door rear fittingEUROCOPTER AS 350 Alert Telex No. 05.00.47
142-02 PTZF-2002-606_(A).pdf12.3.2005No later than within 110 flying hours or 3 months following the effective date of the original issue of this ADEUROCOPTER; EC 120 helicoptersRotor flight controls - Collective pitch leverEUROCOPTER EC120 Alert Service Bulletin No. 67A009
022-05 PTZF-2005-035_(B).pdf12.3.2005Unless already accomplished, before 750 flight cycles, 600 flight hours or 100 daysAIRBUS SAS; A319, A320 and A321 aircraftOuter wing - Inspection of the main landing gear support rib 5AIRBUS Alert Service Bulletin A320-57A1136
023-05 PTZF-2005-040_(B).pdf12.3.2005Not later than December 31, 2009,AIRBUS SAS; A300, A310, A300-600, A319, A320, A321, A330,Equipment/Furnishings - Non Textile Floor (NTF) replacementAMM AIRBUS 25-28-12/42 PB 401
024-05 PTZFAA_AD_2005-05-15.pdf18.4.2005Within the compliance times specified unless the actions have already been done.Honeywell International Inc. (formerly AlliedSignal Inc. and Garrett Turbine Engine Co.) TFE731-2 and -2C series, and TFE731-3, -3A, -3AR, -3B, -3BR, and -3R series turbofan enginesInitial Inspection for TFE731-2 and -2C Series Engines. Repetitive Inspections for TFE731-2 and -2C Series Engines. Disk Replacement. Honeywell Service Bulletin No. TFE731–72–3369RWK
025-05 PTZF-2005-029_R1_(B).pdf26.3.2005Within one month following the effective date of this AD, except aircraft that have received AIRBUS modification 30650 or 30872 in production or AIRBUS (SB) A320-25-1248 in service.AIRBUS SAS; A318, A319, A320 and A321 aircraftNORTHROP-GRUMMAN (previously LITTON) ADIRU - Modification of shelf supportsAIRBUS Service Bulletin A320-25-1248 Revision 1
026-05 PTZF-2005-046_(B).pdf26.3.2005Within 2400 flight hours, or within 15 months from the effective date of this AD, whichever occurs first,AIRBUS SAS; A319, A320 and A321 aircraftLavatories - DASELL lavatory walls corrosionAIRBUS Service Bulletins A320-25-1365, A320-25-1289 and A320-25-1357
027-05 PTZF-2005-047_(A).pdf26.3.2005Compliance with this AD is required as indicated, unless already done.TURBOMECA; ASTAZOU III turboshaft enginesCivil useTURBOMECA Mandatory Service Bulletin A268 72 0
095-04 R1 PTZF-2004-170_R1_(A).pdf26.3.2005Within the compliance times specified in this AD.EUROCOPTER; AS 350, AS 355, AS 332, SA 341/342 helicoptersEquipment and furnishings - Hoists hooks EUROCOPTER AS 350 Alert Telex No. 01.00.56, AS 355 Alert Telex No. 01.00.50, AS 332 Alert Telex No. 01.00.70 and SA 341/342 Alert SB No. 01.33.
028-05 PTZF-2005-042_(A).pdf26.3.2005Within the compliance times specified in this AD.EUROCOPTER; AS 350Rotor flight controls - Yaw controlEUROCOPTER AS 350 Alert Service Bulletin No. 67.00.26 R1
029-05 PTZF-2005-051_(B).pdf9.4.2005Unless already accomplished, within 20 months since first flight or within 600 flight hours from the.AIRBUS SAS; A318, A319, A320 and A321 aircraftFlight controls - Trimmable horizontal stabilizer actuatorAIRBUS Service Bulletin A320-27-1164 Revision 2.
026-02 R1 PTZF-2002-125_(B).pdf26.2.2005 AIRBUS SAS; A319, A320 and A321 aircraftCANCELLATION NOTICE 
011-02 R1 PTZF-2002-075_R1_(B).pdf26.3.2005Within the compliance times specified in this AD.AIRBUS SAS; A319, A320 and A321 aircraftMain Landing Gear side-stay cuff lugAIRBUS Service Bulletin A320-32A1224 and A320-32-1223
030-05 PTZF-2005-052_(B).pdf9.4.2005Unless already accomplished, within 600 flight hours from the effective date of this ADAIRBUS SAS; A318, A319, A320 and A321 aircraft103VU panel - Hinge pin inspectionAIRBUS AOT 25A1440 dated February 15, 2005
060-04 R4 PTZLBA_D-2004-352R4.pdf10.4.2005Within the compliance times specified in this AD.Hoffmann Propeller GmbH&Co. KG; HO-V343 propellers1. Examination of the propeller blade shake. 2. Examination of the blade retention nut preload torque. 3. Ultrasonic inspection of the propeller hub. 4. Eddy current inspection of the propeller hub, if ultrasonic inspection shows any signs of damages. 5. Exchange or repair of the propeller if any blade shake or signs of cracks or damages of the propeller hub outside serviceable limits have been detected during the inspection.SB_Hoffmann_E-015-B.pdf
SI_Hoffmann_61-10-05_SI_E_4D.pdf
031-05 PTZCF-2005-04.pdf7.3.2005Within 30 days after the effective date of this directiveBombardier Inc.; Model CL-600-2B19 Airplane, Serial Number 7003 and subsequent.Horizontal Stabilizer Trim Actuator (HSTA) Secondary Load Path Indicator InspectionBombardier Alert Service Bulletin A601R-27-128
032-05 PTZCF-2005-05.pdf8.3.2005Within 30 days after the effective date of this directiveBombardier Inc.; Model CL-600-2B19 Airplane, Serial Numbers 7003 and subsequent, that have not incorporated Modsum TC601R16421 or its subsequent revisions.Revision of Structural Inspection Program 
033-05 PTZFAA_AD_83-08-01R2.pdf11.5.2005Compliance with this AD is required as indicated, unless already done.Hartzell Propeller Inc. (Formerly TRW Hartzell Propeller); HC-B3TN-2, HC-B3TN-3, HC-B3TN-5, HC-B4TN-3, HC-B4TN-5, HC-B4MN-5, HC-B5MP-3a) Install all new propellers and serviceable propellers, as follows, before further flight or b) Within the next 300 hours time-in-service after the effective date of this AD, do the following on all applicable turbopropellers presently installed with P/N A-2047 attaching bolts 
030-05 R1 PTZF-2005-052_R1_(B).pdf9.4.2005Unless already accomplished, within 600 flight hours from the effective date of this AD at original issueAIRBUS SAS; A318, A319, A320 and A321 aircraft103VU panel - Hinge pin inspectionAIRBUS AOT 25A1440 dated February 15, 2005
096-04 R1 PTZF-2004-172_R1_(B).pdf23.4.2005Before December 31, 2005AIRBUS SAS; A318, A319, A320 and A321 aircraftFire protection - Cargo compartment water drain valveAIRBUS Service Bulletin A320-52-1124
034-05 PTZF-2005-058_(B).pdf23.4.2005Before December 31st, 2009AIRBUS SAS; A320 and A321 aircraftFuel system - Prevention against explosion risks - In tank bondingAIRBUS Service Bulletin A320-28-1055 Revision 1
035-05 PTZF-2005-057_(B).pdf23.4.2005Within the compliance times specified in this AD.AIRBUS SAS; A319, A320 and A321 aircraftPassenger door - Slide raft telescopic girt barAIRBUS All Operator Telex A320-52A1111, A320-52-1112 Revision 05
036-05 PTZF-2005-056_(B).pdf23.4.2005Before December 31st, 2009.AIRBUS SAS; A320 aircraftFuel system - Prevention against explosion risks - In tank bondingAIRBUS Service Bulletin A320-28-1067 Revision 2.
037-05 PTZUF-2005-073_R1_(A).pdf
F-2005-073_(A)_R1.pdf
29.4.2005Effective date of this ADTURBOMECA; ARRIUS 2F turboshaft enginesModule 2 replacement Alert Fax TURBOMECA No 057/05/DSO/TM dated April 26, 2005.
038-05 PTZCF-2005-10.pdf2.5.2005Within the next 100 hours air time, but no later than 10 June 2005 fort Part 1 and At the first occasion when aircraft is defueled, but not later than 01 December 2005 for Part 2Bell Helicopter Textron Canada (BHTC); Model 206 A/B series helicopters:Fuel Distribution System Superseeded by 038-05R1 PTZ
CF-2005-10R1.pdf
ASB 206-05-103, dated 11 February 2005
009-04 R1 PTZCF-2004-01R1.pdf20.2.2004Within 1000 hours air time, after the effective date of this directive. Repeat the inspection at intervals not to exceed 1000 hours air time.Bombardier Inc.; Model CL-600-2B19, serial numbers 7003 through 7067, 7069 throughEngine Throttle Control GearboxBombardier SB 601R-76-019
039-05 PTZFAA_AD_2005-10-12.pdf2.6.2005Required as indicated, unless accomplished previously.Schweizer Aircraft Corporation; Model 269C, C-1, and D HelicoptersTo prevent separation of the inner spring tube from the lateral trim control housing, the associated loss of trim control, increased local resistance to right cyclic stick movement, and subsequent emergency landing or loss of control of the helicopter.Schweizer Service Bulletins B-283.1 and C1B-017.1, both dated March 4,2005 and DB-012, dated February 8, 2005,
040-05 PTZUF-2005-087.pdf31.5.2005Within the compliance times specified in this AD.EUROCOPTER; AS 350 and AS 355 helicoptersUntimely firing of squibs on GOODRICH electric hoists.EUROCOPTER Alert Telex AS 350 n° 25.00.94 and AS 355 n° 25.00.84
041-05 PTZFAA_AD_2004-25-16_R1.pdf20.6.2005Within the compliance times specified in this AD.Kelly Aerospace Power Systems (formerly owned by ElectroSystems, JanAero Devices, Janitrol, C&D Airmotive Products, FL Aerospace, and Midland-Ross Corporation)Fuel regulator shutoff valveKelly Aerospace Power Systems Service Bulletin No. A–107A
042-05 PTZF-2005-076_(A).pdf11.5.2005Within the compliance times specified in this AD.EUROCOPTER; EC 120 helicoptersTail rotor drive shaft - Rear drive shaft friction ringEUROCOPTER EC 120 Alert Telex No. 05A006.
043-05 PTZCF-2005-13.pdf6.6.2005Compliance is required as indicated unless already accomplished.Bombardier Inc.; CL-600-2B19Cracking of Aft Pressure Bulkhead Web Superseded by 043-05 R1 PTZ
CF-2005-13R1.pdf
 
044-05 PTZFAA_AD_2005-12-06.pdf19.7.2005Within the compliance times specified in this AD.Teledyne Continental Motors (Formerly Bendix) S-20, S-1200, D-2000, and D-3000 Series MagnetosInitial Inspections of Impulse Coupling Assemblies. Repetitive Inspections of Impulse Coupling Assemblies.TCM SB No. 639, dated March 1993, TCM Service Information Letter No. SIL648, dated October 18, 1994.
045-05 PTZFAA_AD_2005-13-16.pdf8.8.2005Within the compliance times specified in this AD.The New Piper Aircraft, Inc.: PA-34-200, PA-34-200T, and PA-34-220T airplanes,The actions specified in this AD are intended to detect, correct, and prevent failure in certain components of the NLG, lack of cleanliness of the NLG due to inadequate maintenance, or lack of lubricant in the NLG or NLG components. This failure of the NLG could lead to loss of control of the airplane during take-off, landing, or taxiing operations. This AD supersedes AD 93-24-14.Service Bulletin No. 1123A, dated November 30, 2004.
046-05 PTZFAA_AD_2005-13-10.pdf9.8.2005Within the next 30 days after August 9, 2005Cessna Aircraft Company: 172R, 172S, 182T, T182T, 206H and T206H AirplanesReplace any incorrect amp circuit breaker with the required 40-amp circuit breaker.Cessna Service Bulletin No. SB05–24–01, January 31, 2005.
047-05 PTZFAA_AD_2005-10-13.pdf22.6.2005At the next time the gas producer turbine rotor is disassembled for any reason, or within 1,750 hours time-since-lastoverhaul, inspection after the effective date of this AD, whichever occurs first, but no later than October 31, 2011, unless already done.Rolls-Royce Corporation (Formerly Allison Engine Company) 250-B17B, -B17C, -B17D, -B17E, -C20, -C20B, -C20F, -C20J, -C20S, and -C20W Turboprop and Turboshaft EnginesInstall a turbine energy absorbing ringRolls-Royce Corporation Alert Commercial Engine Bulletin No. CEB-A-1255, Revision 4, dated September 29, 2004
014-04 R1 PTZCF-2004-05R2.pdf30.6.2005Before next flightBell Helicopter Textron Canada: Models 206A, 206B, 206L SeriesRevision 1 of this directive introduced terminating action requiring affected blades to be inspected for acceptable tail rotor blade skin thickness.ASB 206-04-100 Rev. C in ASB 206L-04-127 Rev. C
048-05 PTZFAA_AD_2005-11-05.pdf18.7.2005Within compliance times specified unless the action have already been done.Precise Flight, Inc.: Models SVS I and SVS IA Standby Vacuum SystemsIncorporate the airplane flight manual supplement (AFMS) in the airplane flight manual with the appropriate revision, install placards described in the AFMS and upgrade the Model SVS I or SVS IA SVS to the Model VI SVS. 
049-05 PTZFAA_AD_2005-13-07.pdf27.7.2005Within compliance times specified unless the action have already been done.Honeywell International Inc. (Formerly AlliedSignal Inc. and Garrett Turbine Engine Co.) TFE731-2 and -3 Series Turbofan EnginesReplace discsHoneywell International, Inc. Service Bulletin No. TFE731-72-3682, dated November 26, 2002
050-05 PTZF-2003-001_(B)_R2.pdf18.6.2005Within the compliance times specified in this AD.CFM INTERNATIONAL; CFM56-5 and CFM56-5B enginesEngine indicating - EGT harnesses and couplingsCFM56-5 SB 77-0020 Revision 3 (or any subsequent approved issue), CFM56-5B SB 77-0008 Revision 3 (or any subsequent approved issue).
051-05 PTZF-2005-086_(A).pdf18.6.2005Within the compliance times specified in this AD.EUROCOPTER; EC 120 helicoptersRotor flight controls - Collective torque tube assemblyEUROCOPTER EC 120 Alert Service Bulletin No. 67A014
052-05 PTZF-2005-088_(A).pdf8.6.2005within 25 engine operating hours and at the latest by July 31st, 2005.TURBOMECA; ARRIUS 2F turboshaft enginesFuel system and controls - Check of correct position of adjusted FCU fuel filterMandatory Alert Service Bulletin No A319 73 4823 (or any subsequent approved issue), ARRIUS 2F Maintenance Manual Ref X 319 L6 301 2.
053-05 PTZCF-2005-18.pdf11.7.2005Compliance is required as indicated unless already accomplished.Bombardier Inc.; CL-600-2B19 aircraftMissing Restrictor on Refuel / Defuel Shut-Off ValvesBombardier Alert Service Bulletin A601R-28-064, dated 21 April 2005,
054-05 PTZLTA_2005-196.pdf14.6.2005Immediately after the effective date of this airworthiness directive.DG-Flugzeugbau, DG-300, DG-300 ELAN, DG-300 ELAN ACRO, DG-300 CLUB ELAN, DG-300 CLUB ELAN ACROIncrease of service life and revision of the appropriate maintenance manual.DG-Flugzeugbau Technical Note No. 359/23 of 3 February 2005.
LTA_2005-196-TN-359-23.pdf
055-05 PTZF-2005-101_(B).pdf2.7.2005From September 02, 2005, it is mandatory to strictly adhere to the requirements of the AIRBUS A318/A319/A320/A321 CMR document at issue 22.AIRBUS SAS; A318, A319, A320 and A321 aircraftCertified limitations - MPD Section 9-3AIRBUS A318/A319/A320/A321 CMR document reference AI/ST4/993.436/88 (Section 9-3 of the MPD), issue 22 approved on May 03, 2005
078-04 R1 PTZF-2004-123_(B)_R1.pdf2.7.2005Before May 31, 2007AIRBUS SAS; A319, A320 and A321 aircraftEnvironmental/Air conditioning - Cargo compartment - Heating temperature sensorAIRBUS Service Bulletin A320-21-1141
056-05 PTZF-2005-087_(A).pdf30.5.2005Within the compliance times specified in this AD.EUROCOPTER; AS 350 and AS 355 helicoptersEquipment/Furnishings - Untimely firing of squibs on GOODRICH electric hoistsEUROCOPTER Alert Telex AS 350 n° 25.00.94 and AS 355 n° 25.00.84
057-05 PTZEASA_AD_05_0019_Robinson_R22.pdf5.7.2005Before 01 December 2005.Robinson Helicopter Company; R22/ All modelsRotor Blades - ReplacementR22 Service Bulletin SB-94, dated 14.12.2004.
058-05 PTZFAA_AD_2005-13-36.pdf9.8.2005Within 100 flight hours, or 90 days after the effective date of this AD, whichever occurs firstLearjet Inc.; Model 23, 24, 24A, 24B, 24B-A, 24C, 24D, 24D-A, 24E, 24F, 24F-A, 25, 25A, 25B, 25C, 25D, 25F, 28, 29, 31, 31A, 35, 35A (C-21A), and 36 AirplanesDo a detailed inspection of the center ball of the aileron control cable or cables for a defective swage.Bombardier alert service bulletins A23/24/25–27–17 December 23, 2002, A23/24/25–27–17 December 23, 2002, A31–27–25 December 23, 2002 and A35/36–27–42 December 23, 2002.
059-05 PTZFAA_AD_2005-14-11.pdf17.8.2005Within 10 hours time-in-service after the effective date of this AD.Hartzell Propeller, Inc., McCauley Propeller Systems, and Sensenich Propeller Manufacturing Company, Inc. PropellersThis AD requires maintenance actions amounting to an overhaul of the affected propellers.Special Airworthiness Information Bulletin No. NE-01-19, dated March 20, 2001,
060-05 PTZFAA_AD_2005-14-12.pdf29.7.2005Within the compliance times specified unless the actions have already been done.Hartzell Propeller Inc.; Models HC-B3TN-2, HC-B3TN-3, HC-B3TN-5, HC-B3MN-3, HC-B4TN-3, HC-B4TN-5, HC-B4MN-5, HC-B4MP-3, HC-B4MP-5, and HCB5MP-3 PropellersVisual Inspections and Torque ChecksAD 2004-21-01, Amendment 39-13822 (69 FR 60952) also pertains to the subject of this AD.
061-05 PTZFAA_AD_2005-15-10.pdf26.8.2005Within the compliance times specified in this AD.The New Piper Aircraft, Inc. Models PA-34-200T, PA-34-220T, PA-44-180, and PA-44-180T AirplanesVisually inspect any installed aircraft heater fuel pump for leakage.The New Piper Aircraft, Inc. Service Bulletin No. 1127, dated February 26, 2003 and No. 1127B, dated April 18, 2005; Kelly Aerospace Power Systems Service Information Letter Bulletin No. A-110A, dated March 6, 2003 and No. A-110B, dated December 20, 2004.
062-05 PTZUF-2005-161_(A).pdf16.9.2005At the latest before the next hoisting operation,EUROCOPTER; SA 341/342 HELICOPTERSEquipment/Furnishings – Untimely firing of squibs on GOODRICH electric hoists.EUROCOPTER SA 341/342 Alert Telex No. 25.12.
063-05 PTZF-2005-108_(B).pdf16.7.2005Before December 31, 2010 or within 6500 Flight Hours from this AD effective date, whichever occurs first.AIRBUS SAS; A318, A319, A320 and A321 aircraftFuel system - Magnetic fuel level indicator (MFLI)AIRBUS Service Bulletin A320-28-1138
064-05 PTZF-2005-115_(B).pdf16.7.2005Within the compliance times specified in this AD.AIRBUS SAS; A318, A319, A320 and A321 aircraftMain landing gear (MLG) - Shock absorber sliding tube cracksAIRBUS Service Bulletin A320-32A1273 Revision 2
054-04 R1 PTZF-2004-065_(B)_R1.pdf16.7.2005 AIRBUS, A318, A319, A320 and A321 aircraftMain landing gear (MLG) - Shock absorber sliding tube. This Revision 1 cancels Airworthiness Directive (AD)
DGAC_F-2004-065(B).pdf
 
065-05 PTZCF-2005-26.pdf18.7.2005Within the compliance times specified in this AD.Bombardier Inc.; CL-600-2B19 aircraftSuperseded by 065-05R1 PTZ
CF-2005-26R1.pdf
Bombardier Service Bulletin 601R-30-029, Revision A, dated 7 July 2005,
066-05 PTZLTA_2005-248.pdf12.7.2005As of the effective date of this AD,Personal Parachute OMEGA ( ) / QUICK ( )----- THE USE OF ALL THE OMEGA ( ) / QUICK ( ) PERSONAL PARACHUTES IS PROHIBITED ------- None –
105-04 R1 PTZCF-2004-23R1.pdf18.8.2005Within 5500 flight hours of the effective date of this directive, unless already accomplished.Bombardier Inc.; CL-600-2B19 aircraftCamloc Fasteners On Center Pedestal.Bombardier Aerospace Service Bulletin (SB) 601R-31-030, Revision D, dated 16 June 2005.
067-05 PTZF-2005-121_(B).pdf30.7.2005Within the compliance times specified in this AD.AIRBUS SAS; A319 and A320 aircraftFuel system - Labels in fuel tanksAIRBUS Service Bulletin A320-28-1102 Revision 1, A320-57-1117 Revision 1 and A318/319/320/321 MMEL (Master Minimum Equipment List) No 01-28/01Z issue 01.
068-05 PTZF-2005-122_(A).pdf30.7.2005Superseded by EU-2006-0141 (Si-048-06 PTZ)TURBOMECA; ARRIUS 2F turboshaft enginesOil - Replacement of check-valve piston o-ringMandatory Alert Service Bulletin No A319 79 4802
113-03 R2 PTZF-2003-465_(A)_R2.pdf30.7.2005Within the compliance times specified in this AD.EUROCOPTER; EC 120 helicoptersTail rotor drive - Tail rotor drive shaft damperEUROCOPTER EC 120 B Alert Service Bulletin No. 65A004
066-05 R1 PTZLTA_2005-248_R1.pdf21.7.2005As indicated, unless already accomplished:Personal Parachute OMEGA ( ) / QUICK ( )Personnel Parachute OMEGA ( ) / QUICK ( ) - OMEGA Container-System - Modification of Flap-No. 3, Visual Inspection of Bartecs, and Equipment Handbook Change.Performance Variable Service Bulletin SB-O-200501, dated 18 July 2005. Performance Variable Equipment Handbook (German Version) EH-O-Q01, Revision 4, dated 01 July 2005.
LTA_2005-248_R1-SB-O-200501.pdf
069-05 PTZF-2005-102_(A)_R1.pdf13.8.2005Within the compliance times specified in this AD.EUROCOPTER; AS 350 and AS 355 helicoptersFuselage - RH cabin vibration damperEUROCOPTER AS 350 Alert Telex No. 05.00.48 R1 and EUROCOPTER AS 355 Alert Telex No. 05.00.46 R1
070-05 PTZF-2005-136_(A).pdf3.8.2005Within the compliance times specified in this AD.EUROCOPTER; AS 350 and AS 355 helicoptersDoors - Sliding door rear roller support shaft and rear fitting.EUROCOPTER AS 350 Alert Telex No. 05.00.47 R1 and EUROCOPTER AS 355 Alert Telex No. 05.00.45 R1
021-05 R1 PTZF-2005-032_(A)_R1.pdf3.8.2005 EUROCOPTER; AS 350 helicoptersDoors - Pin of the sliding door rear fitting. This Revision 1 cancels Airworthiness Directive (AD) F-2005-032, which is replaced by AD F-2005-136.
F-2005-032_(A).pdf
 
071-05 PTZFAA_AD_2005-16-04.pdf12.9.2005Required as indicated, unless accomplished previously.Bell Helicopter Textron; Model 206A and 206B HelicoptersDetect a crack in the crosstube, which could lead to failure of the crosstube, collapse of the landing gear, and subsequent loss of control of the helicopter.Aeronautical Accessories, Inc. Alert Service Bulletin No. AA-03121, dated October 25, 2004
072-05 PTZFAA_AD_2005-16-05.pdf26.8.2005Required as indicated, unless accomplished previously.Robinson Helicopter Company; Model R-22 Series HelicoptersTo prevent separation of a door window or door assembly from the helicopter, which could damage the tail rotor during flight and result in loss of control of the helicopter.Tech-Tool Plastics, Inc. Service Bulletin No. TTP2005-01, Revision A, dated February 1, 2005
073-05 PTZFAA_AD_2005-16-09.pdf13.9.2005Within the compliance times specified, unless the actions have already been done.Learjet; Model 23, 24, 25, 35, and 36 AirplanesPerform an inspection to detect deterioration (such as cracks, cuts, breaks, splits, or warpage) of both flappers of the tip tank in each wing.Learjet Service Bulletin SB 23/24/25-28-2, dated October 6, 1995 (for Model 23, 24, and 25 airplanes); or SB 35/36-28-10, dated October 6, 1995 (for Model 35 and 36 airplanes)
074-05 PTZFAA_AD_2005-17-11.pdf7.10.2005Within the compliance times specified in this AD.The Cessna Aircraft Company; Models 525, 525A, and 525BInstall identification sleeves on the wires for both engine fire extinguisher bottles. Reconnect the wires to both engine fire extinguisher bottles. Test the wires for correct installationCessna Citation Service Bulletins SB525-26-01, SB525A-26-02 and SB525B-26-01, all dated April 5, 2005
075-05 PTZF-2005-128_(B).pdf13.7.2005Unless already accomplished, within 500 flight hours from July 08, 2005AIRBUS SAS; A320 aircraftLanding gear - Main Landing Gear (MLG) axle nut separation. Inspect the locking bolts, nuts, washers and cotter pins of each MLG wheel and apply corrective actions if necessary in accordance with AOT A320-32A1303.AIRBUS AOT A320-32A1303 dated July 04, 2005
076-05 PTZF-2005-143_(A)_R1.pdf31.8.2005At the latest by February 28, 2006.TURBOMECA; ARRIUS 2F turboshaft enginesFuel control unit - ReplacementTURBOMECA Mandatory Alert Service Bulletin No. A319 73 4825, first issue dated August 2005
077-05 PTZFAA_AD_2005-17-19.pdf13.10.2005Within 50 hours TIS or within 180 days, whichever occurs first after October 13, 2005Cirrus Design Corporation; Models SR20 and SR22 AirplanesThis AD is the result of discovering that the crew seats, under emergency landing dynamic loads, may fold forward at less than 26 g required by the regulations, 14 Code of Federal Regulations (CFR) Section 23.562(b)(2). The actions specified in this AD are intended to prevent the crew seats from folding forward during emergency landing dynamic loads with consequent occupant injury.Cirrus Design Corporation Alert Service Bulletin SB A2X-25-08, dated June 22, 2004 and SB 2X-25-06 R4, revised May 5, 2005.
078-05 PTZFAA_AD_2005-18-12.pdf14.10.2005Within the compliance times specified unless the actions have already been done.Hartzell Propeller Inc. PropellersPerform visual and nondestructive inspections of propeller components for cracks, corrosion or pits, nicks, scratches, wear, blade minimum dimensions, and damage in the blade balance hole.Hartzell Service Bulletin No. HC-SB-61-136, Revision I, dated April 25, 2003.
079-05 PTZFAA_AD_2005-18-20.pdf14.10.2005Within 10 hours after the effective date of this ADGoodrich De-icing and Specialty Systems; ''FASTprop'' Propeller DeicersThis AD results from reports of Goodrich ''FASTprop'' propeller de-icers becoming loose or debonded, and detaching from propeller blades during operation. We are issuing this AD to prevent Goodrich ''FASTprop'' propeller de-icers from detaching from the propeller blade, resulting in damage to the airplane, and possible injury to passengers and crewmembers.Goodrich De-icing and Specialty Systems Alert Service Bulletin (ASB) No. 30-60-00-1, dated November 15, 2004
080-05 PTZFAA_AD_2005-19-11.pdf21.10.2005Within 50 hours time-in-service or 6 months after the effective date of this AD, whichever is earlier, unless the actions have already been done.Lycoming Engines (Formerly TextronLycoming); AEIO-360, IO-360, O-360, LIO-360, LO-360, AEIO-540, IO-540, O-540, and TIO-540 Series Reciprocating EnginesVerify the crankshaft SN. After the effective date of this AD, do not install any crankshaft that has a SN listed in Table 4 of Lycoming MSB No. 566, dated July 11, 2005, into any engine.Lycoming Mandatory Service Bulletin No. 566, dated July 11, 2005,
SB566.pdf
SB566S-1.pdf
customer_letter_nov_30.pdf
081-05 PTZF-2005-117_(B).pdf29.6.2005Within 5 days from the effective date of this ADAIRBUS SAS; A319, A320 and A321 aircraftperform a detailed inspection of the forward engine mount primary load path components and apply all necessary corrective actionsAIRBUS AOT A320-71A1036 Revision 1 dated June 28, 2005
046-02 R3 PTZF-2001-499_R4_(B).pdf31.8.2005Within 10 days following June 26, 2002 [effective date of this AD at Revision 3]AIRBUS SAS; A319, A320GOODRICH carbon brake - Reduction of performances.AIRBUS Service Bulletin A320-32-1247 Revision 2
082-05 PTZF-2005-159_(A).pdf24.9.2005Replaced by EU-2006-0142TURBOMECA; ARRIUS 2B and 2K turboshaft enginesOil - Replacement of check-valve piston o-ringMandatory Alert Service Bulletin No A319 79 2832 and No A319 79 2833
083-05 PTZF-2005-158_(A).pdf
F-2005-158.pdf
1.10.2005Every 110 flying hours, comply with the maintenance operations specified in the referenced revisions,EUROCOPTER; AS 350, EC 130 helicoptersTail rotor drive - Tail rotor drive shaft 
022-02 R1 PTZF-2002-027_R1_(A).pdf24.9.2005Before the next hoisting missionEUROCOPTER; AS 350 helicoptersEquipment / Furnishings - BREEZE 450-lb electric hoistEUROCOPTER AS 350 Alert Service Bulletin No. 25.00.73.
084-05 PTZFAA_AD_2005-18-16.pdf13.10.2005Before exceeding the life limit of 6,000 cycles-since-new.General Electric Company; CF34-3A1 Turbofan Enginesto prevent LCF cracking and failure of those components, which could result in uncontained engine failure and damage to the airplane.GE Temporary Revision No. 05-0073, and Temporary Revision No. 05-0074, for CF34 Engine Manual, SEI-756.
085-05 PTZFAA_AD_2005-19-20.pdf4.11.2005At the next 100-hour or annual inspection that occurs following 30 days after November 4, 2005 (the effective date of this AD), whichever occurs first.The New Piper Aircraft, Inc.; Models PA-28-160, PA-28-161, PA-28-180, and PA-28-181 AirplanesReplace the two AN894–6–4 bushing screw thread expanders on the two AN826–6 tees (one on the gascolator and the other one attached to a bushing (AN912–2J) attached to the inlet on the top of the top fuel pump) with NAS1564–6–4J reducers and AN818–6 nuts. Bulletin No. SB 05-2, dated April 12, 2005.
086-05 PTZFAA_AD_2005-20-04.pdf This AD is superseded by FAA 2007-05-15 (035-07 PTZ)
EASA-2004-0006R1.pdf
1.11.2005Within the compliance times specified in this AD.Teledyne Continental Motors; GTSIO-520 Series Reciprocating EnginesInstallation of TCM Service Kit, EQ6642RTeledyne Continental Motors
MSB94-4G.pdf
087-05 PTZCF-2005-35.pdf3.10.2005Prior to accumulating 5500 hours air time from the effective date of this directive or 36 months after the effective date of this directive, whichever is reached first, unless already accomplished.Bombardier Inc. Model CL-600-2B19; s/n 7003 and subsequentJunction Boxes - Leach TDH-Series Relays MalfunctionBombardier Service Bulletin (SB) 601R-24-118, Revision A, dated 08 August 2005
036-05-R1 PTZF-2005-056-R1.pdf8.10.2005Cancellation NoticeAirbus SAS; A 320 AircraftThis Revision 1 cancels 036-05 PTZ, and is replaced by 019-05 PTZ already included in AIRBUS Service Bulletin A320-28-1104
022-03-R1 PTZF-2003-119-R1.pdf8.10.2005Cancellation NoticeAirbus SAS; A319,A320, A321 AircraftThis Revision 1 cancels 022-03 PTZ, and is replaced by 089-05 PTZ  
088-05 PTZF-2005-164.pdf8.10.2005No later than May 31, 2010Airbus SAS; A318, A319, A320, A321, A330, A340 AircraftUnwanted horizontal movements on EADS SOGERMA Services Pilot and co-pilot seats EADS SOGERMA-SERVICES Service Bulletin TAAI1-25-617 dated February 01, 2005.
089-05 PTZF-2005-165.pdf8.10.2005Measures are rendered mandatory from the effective date of this ADAirbus SAS; A318, A319, A320, A321 AircraftFuel leak procedure; Inserting Temporary Revision in the flight manual of the aircraft. The crew is required to strictly follow that procedure. 
014-05-R1 PTZEASA-2005-0012R1.pdf1.5.2005See EASA AD; 1. Inspect the area within 500 Fl. hours after the effective date; and 2. Apply modifications no later than July 31, 2007International Aero Engines; V2500-A1,-A5 (Airbus A319, A320 & A321)Retaining of Fuel filter cover on the FCOC. Loosen helicoil inserts possibility. Inspection and modification.IAE SB 79-0085 or 79-0086 as applicable; All Operators Wire AOW 1048
090-05 PTZFAA-2005-20-25.pdf9.11.2005Within the next 200 hours time-in-service (TIS), the next 12 months, or at the next scheduled inspection, after November 9, whichever occurs first.The Cessna Aircraft Company Models 401, 401A, 401B, 402, 402A, 402B, 402C, 404, 411, 411A, 414, 414A, 421, 421A, 421B, 421C, 425, and 441 AirplanesDetermining date code of certain avionics bus circuit breaker switch, also imposes a 1.000-hour safe limit for date code earlier than 0434.Models 425 and 441 airplanes, procedures in Cessna Conquest SB CQB05–2, all other affected models Multi-engine SB MEB05-1, dated February 21, 2005, and the applicable maintenance manual.
21-01R2 PTZCF-1999-32R3.pdf25.10.2002Replace MLG main fittings by June 30, 2007Bombardier Inc. Model CL-600-2B19; -3 and -4 MLG main fittingsRetrofiting of all aircrafts with the (-83/-84) main fittings to terminate the need to comply with Parts I, II, III, IV and V of this directive as well as with the requirements of 063-04R1 PTZ (AD CF-2004-18R1).Bombardier SB 601R-32-093 Original issue, Rev A, B or later revisions
037-03R1 PTZCF-2003-09R1.pdf6.6.2003Replace MLG main fittings by December 31, 2008Bombardier Inc. Model CL-600-2B19; P/N 601R85001-81/-82 MLG main fittingsRetrofiting of the aircraft with the redesigned (-83/-84) main fitting to terminate the need to comply with Parts I, II, III, IV and V of this directive. Bombardier SB 601R-32-093 Original issue, Rev A, B or later revisions
063-04R1 PTZCF-2004-18R1.pdf16.9.2004Replace MLG main fittings by June 30, 2007Bombardier Inc. Model CL-600-2B19; -3 and -4 MLG main fittingsRetrofiting of the aircraft with the redesigned (-83/-84) main fitting to terminate the need to comply with Parts I, II, III of this directive, as well as with the requirements of 21-01R2 PTZ (AD CF-1999-32R3). Bombardier SB 601R-32-093 Original issue, Rev A, B or later revisions
065-05R1 PTZCF-2005-26R1.pdf17.10.2005Within the compliance times specified in this AD.Bombardier Inc.; certain Models CL-600-2B19Piccolo tubes; Revision 1 of this directive is issued to revise the aircraft serial number applicability. This revision does not introduce additional mandatory action.Bombardier Service Bulletin 601R-30-029, Revision B, dated 29 August 2005,
043-05R1 PTZCF-2005-13R1.pdf7.11.2005Compliance is required as indicated unless already accomplished.Bombardier Inc.; CL-600-2B19Cracking of Aft Pressure Bulkhead Web; Revision 1 mandates new inspection threshold and updates A/c serial numbers 
091-05 PTZEASA-2004-0009R1.pdf3.2.2005As indicated in AD(former Allison Engine Company) Rolls Royce Corp; Model 250 Series Engines, installed in single/twin engined helicoptersThe 'B'-nut torque values Superseded by 091-05R1 PTZ
EASA-2004-0009R2.pdf
 
092-05 PTZF-2005-161.pdf16.9.2005Before the next hoisting operationEUROCOPTER;SA 341 G and SA 342 J helicopters, equipped with GOODRICH electric hoist 76370-XXXPotential risk of untimely squib firing, which would cause the cable to be cut.EUROCOPTER SA 341/342 Alert Telex n° 25.12
093-05 PTZEASA-2005-0023R2.pdf1.11.2005RevisedLycoming Engines; see TCDS No. in EASA ADRevised : 093-05 R2 PTZ (EASA AD No.: 2005-0023R2)Lycoming Service Bulletin & Service Instruction
SB388C.pdf
SI1485A.pdf
094-05 PTZI-2005-345.doc18.9.2005Within the next 50 flying hours, unless already accomplishedCostruzioni Aeronautiche TECNAM; certain s/n P- 92J, P 92-JSInspection of Rudder Pedals, SB P92-J/012Rev.1Costruzioni Aeronautiche TECNAM Service Bulletin
P92-J12-Rev1.pdf
095-05 PTZF-2005-173.pdf5.11.2005Within 20 months following the effective date of this ADAIRBUS SAS; A319 and A320 aircraftPrevention against Explosion Risks, SB A320-28-1059 R6- Modification of wires to the pump control of the center tank Service Bulletin AIRBUS A320-28-1059 Revision 6 or later approved revision
096-05 PTZF-2005-175.pdf5.11.2005See Original AD- depends on p/n of pilot cyclic stickEUROCOPTER; EC 120 B, s/n's up to 1385Preventing sudden restriction of the cyclic stick travel during retrimming; requirements are specified in EUROCOPTER Alert SB 67A011EUROCOPTER EC 120 Alert Service Bulletin (ASB) No. 67A011 R1
097-05 PTZF-2004-059-R1.pdf5.11.2005 EUROCOPTER; EC 120 helicoptersCancellation notice; this AD cancels Airworthiness Directive F-2004-059,dated April 28, 2004, which is replaced by 096-05 PTZ (F-2005-175) 
098-05 PTZF-2005-189.pdf3.12.2005within next 5000 flight hours, but not later than December 03, 2007Airbus SAS; A318, A319, A320, A321 AircraftInspection of certain Twin Motor LP Valve Actuators If necessary apply corrective actionsAIRBUS Service Bulletin A320-28-1122; any later approved revision of that document is also acceptable
099-05 PTZF-2005-191.pdf3.12.2005Superseded by EU-2006-0174 (Si-045-06 PTZ)Airbus SAS; A318, A319, A320, A321 AircraftOperational procedure and maintenance actions, following recent landing on NLG wheel, rotated for 90 degAIRBUS: AMM 12-14-32 and TR issued 13.11.2005, Technical Note 957.1901/05,AFM TR 4.02.00/33,AFM TR 4.02.00/34
038-05 R1 PTZCF-2005-10R1.pdf29.11.2005As indicated, unless already accomplishedBell Helicopter Textron Canada (BHTC); Model 206 A/B series helicoptersFuel Distribution System, grounding of the fuel pumps and solenoid valve and Relocation of Purge Hose- Cancels AD CF-2005-10 (038-05 PTZ)Alert Service Bulletin (ASB) 206-05-103 or later approved Revisions
100-05 PTZI-2005-406.htm14.10.2005As established in Bolletino Tecnico 206-239Agusta; Agusta-Bell AB 206A/BMain rotor blades P/N 206-010-200-all, inspection and rework206-239.pdf
101-05 PTZI-2005-423.htm25.10.2005Within and not later than march 31,2006Agusta; Agusta A 109E, 109K2Replacement of the crushable bumper assembly on all Agusta rescue hoists P/N 109-0900-61 (Breeze-Eastern P/N BL-20200) 109EP-062.pdf
109K-043.pdf
102-05 PTZI-2005-430.htm24.10.2005As established in Bolletino Tecnico 412-111Agusta-Bell; AB 412EPRemoval of cable cut cartridge P/N KT198412-111.pdf
103-05 PTZI-2005-484.htm25.11.2005As established in Bolletino Tecnico 412-112Agusta-Bell; AB 412EPCable Cut Circuit Inspection and Installation of cable cut Cartridge P/N KT198412-112.pdf
104-05 PTZEASA-2005-0027.pdf11.11.2005six months, unless accomplished within the last three yearsApex Aircraft; All Robin DR SeriesInspection for corroded tailplane (stabilator) bearing attachment plates/replacement with new, anodized plates, P/N 34.11.06.000 
105-05 PTZ2005-24-09.pdf15.12.2005Remove affected S/N propeller hubs from service within 10 flight hours or 10 days after the effective dateMc Cauley Propeller Systems;models 2D34C53/74E-X; D2A34C58/90AT-X; 3AF32C87/82NC-X; D3AF32C87/82NC-X;D3A32C88/82NC-X; D3A32C90/82NC-X; and 3AF34C92/90LF-X certain S/NThere was 40 propeller hubs with improperly machined socket retention threads released by the manufacturer.McCauley Propeller Systems Alert Service Bulletin No. ASB251A, dated September 28, 2005
106-05 PTZ1988-028R1-e.pdf12.12.2005As indicated in ADGlasflügel; Club Libelle 205, Mosquito (B), Glasflügel 304(B)Elevator Drive. Revision Corrects an error in the English translation- there were missing two models Mosquito B and Glasflügel 304 B1988-028-TM205-16_20612_303-12_304-3-e.pdf
107-05 PTZEASA-2005-0032.pdf20.12.2005As indicated in ADPiper Aircraft, The New; Pa-28, Pa-32 seriesCorrosion Inspection of Main Spar Behind Fuel TanksPiper Service Bulletin 1006, dated August 15, 1997
108-05 PTZEASA-2005-0034.pdf30.12.2005In next 55 flight hours from the effective date of this AD, repeat interval is 200 Flight HoursPiper Aircraft Corporation, The New; PA-28 and PA-32Inspection of the stabilator balance weight tube for cracks (SB 327, SL 527)Piper Service Bulletin 327
091-05R1 PTZEASA-2004-0009R2.pdf15.12.2004As indicated in AD(former Allison Engine Company) Rolls Royce Corp; Model 250 Series Engines, installed in single/twin engined helicoptersThe 'B'-nut torque valuesRolls Royce Corp. Alert Commercial Service Letter CSL-A-169, A-1166, A-2113, A-3117 and A-4036
094-04R1 PTZF-2004-168R1.pdf31.12.2005 Airbus SAS; A318, A319, A320, A321 AircraftLoss of Integrated Standby Instrument System (ISIS). Revision 1 reduces the scope of effectivitynone
109-05 PTZF-2005-172.pdf31.12.2005Within 200 days following the effective dateAirbus SAS; A319, A320, A321 AircraftEscape slide raft on FWD passenger doors-Girt bar disengagement from the floor fitting Airbus service bulletin A320-25-1394 Revision 1 or later approved revision acceptable
110-05 PTZF-2005-212.pdf31.12.2005Within 600 flight hours following the effective date of this ADAirbus SAS; A319, A320, A321 AircraftRam Air Turbine Carbon Blade-disoriented carbon fibres during manufacturing-one time detailed visual inspectionAirbus Service Bulletin A320-29-1124