PTZ-AD 2007

Številka PTZReferenčna PTZDatum efektiveRok izvršitveProizvajalecVsebina PTZReferenčni SB
001-07 PTZFAA 2006-26-0103.01.2007See AD compliance for detailsThis AD applies to CFM International CFM56-2 series, -3 series, -5 series, and -7B series engines with certain fuel filters- see AD; These engines are installed on, but not limited to, Airbus A320 and A340 series airplanes, Boeing DC8-71 series, -72 series, and -73 series airplanes, and Boeing 737 series airplanes  To prevent the loss of engine thrust that could result in loss of control during takeoff or landing; This AD requires replacing certain fuel filters- see ADNone
002-07 PTZFAA 2007-01-0613.02.2007See AD compliance for detailsBell Helicopter Textron Canada; Model 206A, B, L, L-1, L-3, and L-4 helicopters, with a tail rotor blade (blade) with the certain (see AD) part number (P/N) and serial number (S/N) installed, certificated in any categoryTo prevent blade failure and subsequent loss of control of the helicopterBell Helicopter Textron Alert Service Bulletin No. 206-04-100 for Model 206A and Band No. 206L-04-127 for Model 206L series, both Rev. C, both dated March 5, 2005
003-07 PTZFAA 2007-01-0716.02.2007See AD compliance for detailsBombardier Model CL-600-2B19 (Regional Jet Series 100 & 440) airplanes, certificated in any category; S/N  7003 through 7067 inclusive, and 7069 through 8999 inclusive; equipped with main landing gear (MLG) main fittings, having P/N 601R85001-3 or -4 (Messier-Dowty P/N 17064-101, -102, -103, or -104)To detect and correct fatigue cracking of the main fitting of the MLG and consequent failure of the main fitting, which could result in the collapse of the MLGCanadian airworthiness directive CF-2004-18R1, dated September 21, 2005
004-07 PTZEASA 2006-0092R1 AD CANCELATTION NOTICE16.01.2007N/AHartzell two blade, aluminum hub, "compact" ( )HC-( )2Y( )-( ) series propellers manufactured before Dec 1991 that do not have an "A" or "B" suffix letter at the end of the hub and propeller S/N and are installed on Lycoming ( )-360 series engines This Notice cancels EASA AD 2006-0092 dated 03 May 2006, including the ‘correction’ dated 07 Sept. 2006. The actions required by the FAA AD 2006-18-15 are almost identical to the ones required by EASA AD 2006- 0092. They are adequate to correct the unsafe condition and therefore that FAA AD is considered ‘accepted’ .Propellers – Propeller Hub – InspectionHartzell Propeller Inc. Service Bulletin HC-SB-61-269, dated April 18, 2005
005-07 PTZFAA 2007-02-1702.03.2007Within 90 days after the effective date of this AD, unless already doneSee AD compliance for detailsTurbomeca Arriel -1A, -1A1, -1A2, -1B, -1B2, -1C, -1C1, -1C2, -1D, - 1D, -1D1, -1K1, -1E, -1E2, -1S, and -1S1 series turboshaft engines. These engines are installed on, but not limited to, Augusta A 109 series, Eurocopter AS 350, AS 365, SA 365, EC 155, and BK 117series, and Sikorsky S-76A and S-76C series helicoptersIdentify and correct an unsafe condition on an aviation productEASA AD 2006-0068
006-07 PTZFAA 2007-02-1601.03.2007See AD compliance for detailsSaab Model SAAB-Fairchild SF340A (SAAB/SF340A) airplanes having S/N 004 through 159 inclusive, and Model SAAB 340B airplanes having S/N160 through 367 inclusive; certificated in any category; on which Saab Modification 2533 has not been implementedTo prevent failure of the starter generator, which could cause a low voltage situation in flight and result in increased pilotworkload and reduced redundancy of the electrical powered systemsSaab Service Bulletin 340-24-035; Saab Service Bulletin 340-24-026and Swedish airworthiness directive 1-197
007-07 PTZEASA 2007-0010 This AD supersedes EASA AD 2006-0353, which superseded ENAC(Italy) PA 2002-59718.12.2006(effective date of EASA 2006-0353See AD compliance for detailsAll Agusta Helicopters A109E where Tail Rotor blades  P/N 109-8132-01-111 are installedTail 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
008-07 PTZEASA 2007-002501.10.2004Effective date of AD A-2004-01From the last inspection date, as requested by AD A-2004-01, repeat thereafter not to exceed 110 hours, TIS,See AD compliance for detailsRotax 912 A, F, S series; Rotax 914 F series and any other Rotax type 912 and 914 series engine whose crankcase assembly has been replaced by a crankcase having a S/N up to S/N 27811 inclusive. These engines are known to be installed on, but not limited to, the following aircraft types: 3-i Sky Arrow, Aeromot, Aircraft Philipp (formerly Alpla-Werke; Nitsche), Diamond, Evektor-Aerotechnik, Grob, Issoire, Reims Aviation, Scheibe, Stemme, Tecnam, W.D. AircraftEngine – Crankcase – InspectionsBRP-Rotax Mandatory Service Bulletins, SB-912-029 R3 and SB-914-018 R3 or later approved revisions
009-07 PTZEASA 2007-002719.02.2007See AD compliance for detailsVulcanair (formerly Partenavia) P68 series aircraft, all models, all serial numbersStructures – Wings & Stabilizers Structural Fatigue Limits –ImplementationVulcanair SB No.120 original issue or Rev. 1 dated 07 June 2006 or later approved rev.
010-07 PTZFAA 2007-03-1915.03.2007See AD compliance for detailsBombardier, Inc. (Formerly Canadair)Bombardier Model CL-600-2B19 (Regional Jet Series 100 & 440) airplanes, S/N  7003 and subsequent; certificated in any category; equipped with main landing gear (MLG) main fittings, certain part numbers (P/N), see AD for detailsDetection and correction of premature cracking of the main fittings of the main landing gears (MLGs)CF-2003-09R1, dated September 21, 2005 (PTZ 037-03); Bombardier Alert Service Bulletin A601R-32-088;Bombardier Service Bulletin 601R-32-093
011-07 PTZFAA 2007-03-1519.03.2007See AD compliance for detailsCFM International CFM56-5 and -5B series turbofan engines- see AD for details;These engines are installed on, but not limited to Airbus Industrie A318, A319, A320, and A321 airplanesPrevention of  unexpected deterioration ofcritical rotating engine parts due to higher than desired engine operating exhaust gas temperature EGTCFM56 Service Bulletin No: CFM56-5B S/B 77-0008 CFM56-5 S/B 77-0020 and DGAC AD F-2003-001 R2  (see 050-05 PTZ)
012-07 PTZEASA EMERGENCY AD 2007-0036-E This AD is superseded by EASA 2007-0036R116.02.2007See AD compliance for detailsAIRBUS  A318, A319, A320 and A321 aircraftPower Plant – Forward Engine Mount Bolts – Inspection /Replacement / RetorqueAIRBUS All Operator Telex (AOT) A320-71A1042 Rev 01; Goodrich All Operator Letter (AOL) CFM56-074 Rev 1
013-07 PTZFAA 2004-23-02 Correction 23.12.2004See AD compliance for detailsRaytheon Aircraft Company aircraft different models- see AD list;including C90, and C90ADetection and correction of  cracks in the NLG fork, which could result in reduced structuralintegrity and inability of the NLG fork to carry design limit and ultimate loadsRaytheon AircraftCompany Mandatory Service Bulletin SB 32-2102, Revision 7, Revised: July, 2003
014-07 PTZFAA 2007-04-1523.03.2007Perform within 600 flight hours after the effective date of this AD, unless the actions have already been done- see AD This AD applies to Sicma Aero Seat, passenger seat assemblies certain P/N- see ADThese seat assemblies are installed on, but not limited to, Airbus A300, A310, A318, A319, A320, A321, A330, and A340 series airplanes Prevent detachment of passenger seat assemblies, especially during emergency conditions, leading to occupant injury Sicma Aero Seat Service Bulletin No. 90-25-005, Issue 2, dated March 31, 1999, and Annex 1, Issue 1, dated March 31, 1999 and Direction Generale de L'Aviation Civile, AD 1994-085(AB) R2, dated July 13, 1999
015-07 PTZFAA Emergency AD 2007-04-51 This AD is superseded by FAA 2007-05-16 (PTZ 033-07 PTZ)Takoj Within 20 engine flight hours after receipt of this emergency ADSee AD for detailsAll owners and operators of General Electric Aircraft Engines (GE) CF34-3A1/-3B/-3B1 turbofan engines installed on Bombardier, Inc. CL-600-2B16 (CL-601-3R Variant), CL-600-2B16 (CL-604 Variant), and CL-600-2B19 (Regional Jet Series 100 and 440) model airplanesAn uncontained fan disk failure during flight operationGE Alert Service Bulletin (ASB) No. CF34-BJ S/B 72-A0213, dated February 15, 2007, and GE ASB No. CF34-AL S/B 72-A0232, dated February 15, 2007
016-07 PTZFAA 2007-04-1823.03.2007See AD compliance for detailsLearjet models identified in the applicable Bombardier service bulletin listed in Table 1 of AD Prevent inadvertent operation, which could result in inadvertent fuel transfer by the left or right wing fuel system and subsequent over-limit fuel imbalance between the left and right wing fuel loads See Table 3 and 4 in AD for details
017-07 PTZEASA 2007-003807.03.2007Within the next 50 flight hours, after the effective date of this AD; Repeat thereafter, at intervals not to exceed 100 flight hours;See AD compliance for detailsA109E Agusta Helicopters up to serial number (s/n) 11158 inclusive and from s/n 11501 to 11510 inclusiveHydraulic Power - Hydraulic Pipes P/N 109-0761-64-103 and 109-0761-65-103 – Inspection / ReplacementAgusta Bollettino Tecnico 109EP-73 original issueor later approved revisions
018-07 PTZEASA 2007-004107.03.2007Within the next 50 operating hours and however within and not later than March 31, 2007; repeat every 300 flight hours or yearly, whichever occurs firstSee AD compliance for detailsAgusta helicopters A109A, A109AII, A109C series, all modelsExhaust – Exhaust Duct Grooved Clamps –Inspection/ReplacementAgusta Bollettino Tecnico 109-123 dated 16 November 2006 or later approved revisions
019-07 PTZEASA 2007-004307.03.2007Within the next 50 hours time in service (TIS) and however within and not later than April 30, 2007; repeated every 100 flight hours or yearly, whichever occurs firstSee AD compliance for detailsAgusta helicopters AB206A and AB206B series, all modelsExhaust – Exhaust Duct Grooved Clamps –Inspection/ReplacementAgusta Bollettino Tecnico 206-242 dated 18 December 2006or later approved revisions
020-07 PTZEASA 2007-004408.03.2007See AD compliance for detailsTURBOMECA Arriel 2B, 2B1 and 2B1A turbo-shaft engines. These engines are known to be installed on, but not limited to, the following helicopters: EurocopterAS 350 B3 and EC 130 B4 helicoptersEngine Fuel and Control - Hydromechanical Metering Unit (HMU) -Visual Inspection of the Drive-Link SplinesTurbomeca, S.A. Mandatory Service Bulletin No. 292 73 2812 - UpdateNo.4
021-07 PTZEASA 2007-004508.03.2007See AD compliance for detailsTURBOMECA  ARRIEL 1A,1A1,1A2,1B, 1C, 1C1, 1C2, 1D, 1D1, 1E2, 1K, 1K1, 1S, 1S1 turboshaft engines originally assembled by TURBOMECA and having previously been used by an operator who is not under the control of a civil Authority (Military, Paramilitary…). These engines are known to beinstalled on, but not limited to, the following helicopters: Eurocopter AS350B/BA/B1/B2, AS365 N/N1/N2/C/C1/C2/C3 and BK117 C1/C2 (EC 145), Agusta A109 K/K2, Sikorsky S76 A+/A++/C helicoptersReturn to Service for Civil Use from an Operator NotControlled by a Civil AuthorityTurbomeca, S.A. Service Bulletin No. A292 72 0806 – Original Issue, orlater approved revisions
022-07 PTZEASA 2007-003408.03.2007See AD compliance for detailsEADS SOCATA (formerly SOCATA) TB 9, TB 10 and TB 200 aircraft, all serial numbersTime Limits - Airworthiness Limitations – New Life Limit forEngine and Nose Landing Gear MountsEADS SOCATA TB 9 MM Chapter 4 Revision 18; EADS SOCATA TB 10 MM Chapter 4 Revision 18;EADS SOCATA TB 200 MM Chapter 4 Revision 18
023-07 PTZEASA 2007-004709.03.2007At the next scheduled Inspection, but no later than 15 April 2007;See AD compliance for detailsDiamond Aircraft Industries GmbH; DA 42 airplanes with certain serial numbers- see AD for detailsFuel System – Auxiliary Fuel Tank Venting-Inspection / ModificationDiamond Aircraft Industries Mandatory Service Bulletin MSB 42-032/1 or later approved revisionsand DA 42 Maintenance Manual AMM-TR-OÄM-42-056f Temporary Revision
024-07 PTZFAA 2007-04-1912.03.2007See AD compliance for detailsThis AD applies to Superior Air Parts, Inc. (SAP), cast cylinder assemblies, certain P/N installed in Teledyne Continental Motors (TCM) 470, 520, and 550 series reciprocating engines. This AD also applies to SAP, cast cylinder assemblies certain P/N installed in Lycoming Engines (LE) 320, 360, and 540 series reciprocating engines and Avco Lycoming 540 series reciprocating engines.See AD for details.To prevent cylinder separation that can lead to engine failure, a possible engine compartment fire, and damage to the airplaneSuperior Air Parts, Inc. Mandatory Service Bulletin B06-01, Rev. E, dated January 24, 2007
025-07 PTZEASA 2007-0036R1  This AD supersedes EASA EAD 2007-0036-E16 Februar 2007 (effective date of Emergency AD 2007-0036-E)See AD compliance for detailsAIRBUS Models A318-111 and -112; A319-111, -112, -113, -114 and -115; A320-111, -211, -212, -214, -215 and -216; and A321-111, -112, -211, -212 and -213 aircraft, all serial numbers, which have CFM International CFM56-5A orCFM56-5B series engines installedPower Plant – Forward Engine Mount Bolts – Inspection /Replacement / RetorqueAIRBUS All Operator Telex (AOT) A320-71A1042 Revision 01; and Goodrich All Operator Letter (AOL) CFM56-074 Revision 1; or later approved revisions of these documents
026-07 PTZFAA 2007-04-2403.04.2007See AD compliance for detailsThis AD applies to Bombardier Model CL-600-2B19 (Regional Jet Series 100 & 440) airplanes, certificated in any category; serial numbers (S/Ns) 7003 through 7067 inclusive and S/Ns7069 through 7947 inclusiveTo detect and correct missing or fracturedattachment bolts, which could lead to the loss of an engine exhaust nozzle during flight and consequent structural damage to the airplane and hazard to people or property on the groundCanadian airworthiness directive CF-2006-19, dated July 28, 2006; Bombardier Service Bulletin 601R-78-021, dated June 2, 2006; BombardierService Bulletin CF34-NAC-78-024, Revision 4, dated November 10, 2005
027-07 PTZEASA 2007-005714.03.2007Before April 30th 2008, implement modification Tf12 as per paragraph 2of the Turbomeca Mandatory Service Bulletin no. 319 72 4012TURBOMECA ARRIUS 2F turboshaft engine (installed on EC120B helicopter)Engine - Gas Generator Front Bearing- ModificationTURBOMECA Mandatory Service Bulletin N° 319 72 4012 update N°1 orany approved subsequent issue
028-07 PTZCF-2007-02   This AD is superseded by CF-2007-02R1 (PTZ 106-07)Upon receiptWithin the next 16 hours flight time, but no later than 1 May 2007, unless already accomplishedBell Helicopter Textron Canada (BHTC) Model 206 A and B series helicopters with Transmission Pylon Support Spindle Part Number (P/N) 206-031-554 (Spindle) serial numbers installed- certain S/N See AD for detailsTransmission Pylon Support Spindlenone
029-07 PTZFAA 2007-05-11 This AD supersedes AD 98-13-24 and AD 2006-22-0620.03.2007See AD compliance for detailsThis AD applies to Bombardier Model CL-600-2B16 (CL-604) airplanes, S/N 5301 through 5665 inclusive; and Model CL-600-2B19 (Regional Jet Series 100 & 440) airplanes, S/N  7003 through 7990 inclusive and 8000 through 8066 inclusive; certificated in any categoryTrim problems including uncommanded trim, trim in the opposite direction to that selected, loss of trimposition indication and, in one case, potential loss of trim disconnect capabilityBombardier Service Bulletin S.B. 601R-27-053, Rev B,  Feb 21, 1997. Bombardier Alert Service Bulletin A604-27-029,  Sept 28, 2006 ; or Bombardier Service Bulletin 601R-27-147, Sept 28, 2006 and CF-2006-20R1, CF-2006-21R1
030-07 PTZCF-2007-0105.03.2007Within the next 50 hours air time after the effective date of this directive, See AD compliance for detailsBell Helicopter Textron Canada (BHTC), Models 206A, 206B, 206L, 206L-1, 206L-3 and 206L-4Upper Left Hand Tailboom AttachmentFor 206A/B see ASB 206-06-110   For 206L, L-1, L-3, L-4 see ASB 206L-06-140
031-07 PTZEASA EMERGENCY AD 2007-0060-E09.03.2007At the next maintenance event, or within the next 25 hours of engine operation, but not later than 01 July 2007, whichever occurs first after the effective date of this directive;See AD compliance for detailsBRP-Rotax GmbH & Co. KG; Bombardier-Rotax GmbH & Co. KG; Bombardier-Rotax GmbH; Rotax 912 A series Rotax 912 F seriesRotax 912 S seriesEngine Fuel and Control - Fuel Pump - ReplacementBRP Rotax Alert Service Bulletin ASB-912-053, dated 20 February 2007,or later approved revision
032-07 PTZFAA 2007-05-1011.04.2007See AD compliance for detailsCessna Aircraft Company172R, 172S, 182S, 182T, T182T, 206H, T206H; certain S/N- see AD applicability for detailsTo prevent the crew seat back cylinder lock assembly from bending, cracking, or failingCessna Single Engine Service Bulletin SB04-25-01, Rev 4, Cessna Single Engine Service BulletinSB04-25-02, Rev 1 or Rev 2
033-07 PTZFAA 2007-05-16This AD supersedes emergency AD 2007-04-51 (015-07 PTZ)12.03.2007Within 20 engine flight hours after the effective date of this AD, unless the actions have already been done; See AD compliance for detailsThis AD applies to General Electric Aircraft Engines (GE) CF34-3A1/-3B/-3B1 turbofan engines that have fan disks with S/Ns listed in Table 1 of this AD These engines are installed on, but not limited to, Bombardier, Inc. CL-600-2B16 (CL-601-3R Variant), CL-600-2B16 (CL-604 Variant), and CL-600-2B19 (Regional Jet Series 100 and 440) model airplanesTo prevent an uncontained fan disk failureand airplane damageGE Alert Service Bulletin (ASB) No. CF34-AL S/B 72-A0232 GE ASB No. CF34-BJ S/B 72-A0213 And FAA AD 2006-05-04(see 015-06 PTZ)
034-07 PTZFAA 2007-05-1312.04.2007Within 36 months after the effective date of this AD,See AD compliance for detailsAirbus Model A319, A320, and A321 airplanes identified in paragraphs (c)(1) and (c)(2) of this AD, certificated in any categorysee AD applicability for detailsTo prevent failure of the attachment points of the YZ-latches, which could result in unrestrained cargo causing damage to the fire protection system, hydraulic system, electrical wiring, or other equipment located in the forward and aft cargo compartmentsAirbus Service Bulletin A320-25-1294, Revision 02, dated September 5, 2006 and EASA 2006-0184
035-07 PTZFAA 2007-05-15This AD supersedes AD 2005-20-04 (086-05 PTZ)16.04.2007See AD compliance for detailsThis AD applies to Teledyne Continental Motors (TCM) GTSIO-520 series reciprocating engines. These engines are installed on, but not limited to, Twin Commander (formerly AeroCommander) model 685, Cessna model 404, 411 series, and 421 series, British Aerospace, Aircraft Group, Scottish Division model B.206 series 2 and Aeronautica Macchi model AM-3 airplanesTo prevent failure of the starter adapter assembly and or crankshaft gear, resulting in failure of the engine andpossible forced landingTCM MSB No. MSB94-4G, dated October 31, 2005
036-07 PTZEASA 2007-0064   This AD is revised by EASA 2007 - 0064R1 (122-07 PTZ)27.03.2007Unless already accomplished, within the next 20 months after the effectivedate of this AD, see AD compliance for detailsAIRBUS A319, A320 and A321 aircraft, all certified models, all serial numbers on which zonal tasks ZL-540-02 and ZL-640-02 have already been performed before the effective date of the AD, and for which it cannot be confirmed that access panels 540CZ, 540DZ, 640CZ and640DZ were removed for inspectionWing - Dry Bay Skin - InspectionAIRBUS Service Bulletin A320-57-1121
037-07 PTZEASA 2007-006528.03.2007See AD compliance for detailsAIRBUS A318, A319, A320 and A321 aircraft, all models, all serial numbers; see AD applicability for detailsLanding gear – Normal extension and retraction – Inspection of the selector valves 40GA and 41GAAIRBUS Service Bulletin A320-32-1290 original issue or any later approved revisions
038-07 PTZFAA 2007-06-1523.04.2007See AD compliance for detailsModel AS350B, AS350B1, AS350B2, AS350B3, AS350BA, AS350C, AS350D, and AS350D1; see AD applicability for detailsPrevent in-flight failure of the drive belt or drive shaft, loss of hydraulic power to the flight control system, and subsequent loss of control of helicopterEurocopter Service Bulletin No. 63.00.08, dated May 27, 2002, and No. 29.00.04,Revision 1, date Jan 27, 2004
039-07 PTZFAA 2007-06-02  This AD supersedes AD 2006-07-0919.04.2007See AD compliance for detailsAirbus Model A318, A319, A320, and A321 airplanes, certificated in any categoryDetect and correct failure of the THSA's primary load path, which could result in latent (undetected) loading and eventual failure of the trimmable horizontal stabilizer actuator- THSA's secondary load path and consequent uncontrolled movement of the horizontal stabilizer and loss of control of the airplaneEASA 2006-0223 (056-06 PTZ)
040-07 PTZFAA 2007-06-0530.03.2007See AD compliance for detailsThis AD applies to Airbus Model A318-111 and -112; A319-111, -112, -113, -114, and -115; A320-111, -211, -212, and -214; and A321-111, -112, -211, -212, and -213 airplanes; certificated inany category; all serial numbers, which have CFM International CFM56-5A or CFM56-5B series engines installedApplication of the incorrect torque to the forward engine mount bolts during maintenance couldresult in failure of the forward engine mount and possible separation of the engine from the airplane and damage to the wing or loss of control of the airplane. This AD requires actions that are intended to address the unsafe conditionEASA 2007- 0036R1 (025-07 PTZ); Airbus All Operators Telex A320-71A1042, Rev 01, dated Feb 12, 2007; and Goodrich All Operators Letter CFM56-074, Rev 1, dated Feb 1,2007, for related information.
041-07 PTZEASA 2007-007130.03.2007See AD compliance for detailsAPEX AIRCRAFTDR 400 series aircraft, all models except the DR 400/500, certain S/N- see  for detailsWings - Main spar and fabric covering -Reinforcement / Modification / InspectionAPEX AIRCRAFT Technical Instr. No 1001047 issue H; APEX AIRCRAFT Technical Instr. No.1000851 issue D and No.1001846issue F
042-07 PTZCF-2006-23 R1  This AD supersedes CF-2006-23 (111-06 PTZ) issued on 6 Nov 200619.04.2007At the next scheduled main rotor hub disassembly, but no later than 18 May 2007, see AD for detailsBell Helicopter Textron Canada (BHTC). Models 206 A and 206 B helicopters, up to S/N 3216 (inclusive), having main rotor latch bolts, part numbers 206-010-169-001/-003 and 206-011-122-003Main Rotor Latch Bolts - Removal from ServiceAlert Service Bulletin ASB 206-06-109 dated 25 July 2006, or later revisions
043-07 PTZEASA 2005-0023R3   This AD supersedes EASA 2005-0023R2(PTZ 093-05 R2)01.11.2005See AD compliance for detailsAll Lycoming Piston Engines (Formerly Textron Lycoming)Engine - Exhaust Valve and Guide – InspectionLycoming SB No. 388C dated 22 Nov 2004; Lycoming SI 1485A dated July 2, 2003;or later approved revisions
044-07 PTZEASA 2006-0286R125.09.2006See AD compliance for detailsINTERTECHNIQUE, Zodiac Aircraft Systems Oxygen Reserve Cylinders Oxygen Reserve Cylinders having Part Number (P/N) GLF(XXX)-(X), GLD(XXX)-(X), PC2300 and SLF300, which are known to be installed on, but not limited to Airbus A300 series aircraft; Dassault Aviation (AMD-BA), 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 lim.helicoptersOxygen - Oxygen Reserve Cylinders – Removal/EmptyingINTERTECHNIQUE Service Bulletin GLD/GLF-35-150 ; and EUROCOPTER AS 350 Alert Service Bulletin No. 05.00.54,EUROCOPTER SA 315 Alert Service Bulletin No. 05.42
045-07 PTZCF-2007-0312.04.2007Within the next 100 hours air time but no later than 9 May 2007, See AD compliance for detailsBell Helicopter Textron Canada (BHTC), Models: 206L series and 407Horizontal Stabilizer (Horizontal stabilizers P/N 206-023-119-167 and 407-023-801-109)- Manufacturing Flawsfor 206L series see ASB 206L-06 141   for 407 seeASB 407-06-72
046-07 PTZFAA 2007-04-19R107.05.2007See AD compliance for detailsThis AD applies to Superior Air Parts, Inc. (SAP), cylinder assemblies, manufactured between April 2005 and November 2005, certain part numbers (P/Ns) (See AD for details), installed in Teledyne Continental Motors (TCM) 470, 520, and 550 series reciprocating engines. These P/N cylinder assemblies may be installed in the TCM engine models listed in the Table 1 of this AD. Also can be installed in Lycoming Engines (LE) 320, 360, and 540 series reciprocating engines and Avco Lycoming (AL)540 series reciprocating engines. These P/N cylinder assemblies may be installed in the LE and AL engine models listed in the Table 3.This engines can be installed in diferent aircraft models- see AD for detailsTo prevent cylinder separation that can lead to engine failure, a possible engine compartment fire, and damage to the airplaneSuperior Air Parts, Inc. Mandatory Service Bulletin B06-01, Rev. E, dated January 24, 2007
047-07 PTZEASA 2007-008918.04.2007Within the next 16 hours flight time, but not later than 01 May 2007,whichever occurs first after the effective date of this ADAB 206 A and AB 206 B helicopters, all serial numbers, that have the certain Transmission Pylon Support Spindle Part Number (P/N) 206-031-554 (Spindle) serial numbers installed- see ADMain Rotor Drive – Transmission Pylon Support Spindle –Identification/ReplacementSee CF-2007-02
048-07 PTZFAA 2007-08-01 14.05.2007At the next engine or hot section module shop visit, but before accumulating an additional 6,000 cycles-in-service after the effective date of the AD, unless already done, also see AD compliance for detailsGeneral Electric Company (GE) CT7-5A2/-5A3/-7A/-7A1/-9B/-9B1/-9B2/-9C/-9C3/-9D/-9D2 turboprop engines with stage 2 turbine aft cooling plates, part number (P/N) 6064T07P01, 6064T07P02, 6064T07P05, or 6068T36P01 installed. These engines are installed on, but not limited to, Construcciones Aeronauticas, SA CN-235 series and SAAB Aircraft AB SF340 series airplanes Prevent separation of the stage 2 turbine aft cooling plate, resulting in uncontained engine failure and damage to the airplane General Electric Alert Service Bulletin No. CT7-TP S/B 72-A0464, Revision 04, dated December 12, 2005
049-07 PTZFAA 2007-07-07 This Ad is revised by FAA 2007-07-07 (PTZ 109-07)23.04.2007See AD compliance for detailsThis AD applies to General Electric Company (GE) CF34-1A, -3A, -3A1, -3A2, -3B, and -3B1 turbofan engines, with certain fan disks part numbers (P/Ns) installed. See AD. These engines are installed on, but not limited to, Bombardier Canadair airplane models CL-600-2A12, -2B16, and -2B19 Prevent an uncontained fan disk failure and airplane damage CF34-AL S/B 72-A0231 CF34-AL S/B 72-A0233 CF34-BJ S/B 72-A0212Emergency AD FAA 2007-04-51 and FAA 2007-05-16 also pertain to the subject of this AD
050-07 PTZEASA Emergency AD 2007-0100-E16.04.2007Within 7 days after the effective date of this AD, see AD compliance for detailsDG-Flugzeugbau GmbH Manufacturer(s): Elan Tovarna Elan Flight Ltd Elan Line d.o.o. AMS-Flight d.o.o. Glaser-Dirks Flugzeugbau GmbH Applicable for: DG Flugzeugbau GmbH DG-300 , DG-300 ELAN DG-300 CLUB ELAN DG-300 ELAN ACRODG-300 CLUB ELAN ACROFlight Envelope – Operating Limitations – ModificationDG Flugzeugbau Technical Note No. 359/24   DG-300 and DG-300 ELAN AFM:FM300TN359-24   DG-300 CLUB ELAN AFM:FM300CTN359-24   DG-300 ELAN ACRO AFM:FM300ATN359-24   DG-300 CLUB ELAN ACRO AFM:FM300CATN359-24   List of ADs and SBs applicable for DG-300 series (april 2007)
051-07 PTZFAA 2007-08-0302.05.2007See AD compliance for detailsCessna Aircraft Company: 172R, 172S, 182T, T182T, 206H, T206H. Affected S/N are listed in Table 1 of ADDetect and correct potential loss of fuel flow, which may result in partial or complete loss of engine power and/or uncontrolled engine compartment fire due to fuel leakage forward of the firewallCessna Service Bulletin No. SB07-71-01, Revision 1, dated March 16, 2007
052-07 PTZEASA 2007-0101  This AD supesedes DGAC F-1991-143 R127.04.2007On the next scheduled 100 hour inspection or annual inspection, whicheveroccurs first, Repeat thereafter inspections at intervals not exceeding 110 flight hoursSOCATA, EADS SOCATA TB 9, TB 10, TB 20 and TB 21 aircraft, all serial numbers equipped withaluminium alloy made cabin access door hooksDoors – Cabin Access Door Hooks – Inspection / ReplacementEADS SOCATA Service Bulletin No 10-058 Amdt 2.
053-07 PTZFAA 2007-09-0125.04.2007See AD compliance for detailsCessna Aircraft Company Models 182H, 182J, 182K, 182L, 182M, 182N, 182P, 182Q, and 182R airplanesSee AD applicability for detailsDetect and correct interference between the ground power electrical cable, the fuel strainer cable, and the fuel line between the auxiliary electric fuel pump and the engine-drivenfuel pump. This condition could lead to a fire in the engine compartmentAir Plains Services Corporation Mandatory Service BulletinAPS-07-01-01, date March 5, 2007
054-07 PTZEASA Emergency AD 2007-0060R1-E24.04.2007At the next maintenance event, or within the next 25 hours of engine operation, but not later than 01 July 2007, whichever occurs first after theeffective date of this AD, see AD compliance for detailsAll versions of the engine type Rotax 912 A, 912 F and 912 S all serial numbers if Fuel pump part no. 892230, 892232, 892540 (standard version) or part no. 892235, 892236, 892545 (version including flexible fuel line), are installed. These engines are known to be installed on, but not limited to, the following aircraft types: Skyfox CA-25, CA-25N; Diamond (formerly HOAC) HK-36R Super Dimona, DV 20 Katana; Aeromot AMT-200 Super Ximango; Diamond DA20-A1 Katana; Evektor-Aerotechnik EV-97 Eurostar; Issoire APM-20Lionceau; EIS (Fournier) RF-9; Scheibe SF 36R, SF 25C; Technoflug TFK-2 Carat; WD D4 BK Fascination; III Sky Arrow 650 TC, 650 TCN and 650 TCNS; ABS RF-9 motor glider (Fournier design)Engine Fuel and Control - Fuel Pump - ReplacementBRP Rotax Service Bulletin SB-912-053, dated 13 April 2007, or later approved revision
055-07 PTZEASA Emergency AD 2007- 0110-E25.04.2007Before further flight after the effective date of this AD, see AD compliance for detailsMORAVAN AVIATION s.r.o. (formerly MORAVAN n.p, MORAVAN a.s, MORAVAN AEROPLANES a.s)  MORAVAN Z 42, Z 42M, Z 42MU, Z 142 and Z 142C aircraft, all S/N and MORAVAN Z 242L aircraft S/N 0490, 0541 and from S/N 0651 to 0659 inclusiveAirworthiness Limitations- Permissible Aerobaticmanoeuvres in Utility category - ModificationMORAVAN mandatory Service Bulletins Z 42/54a; Z 142/53a; Z 142C/30a; and Z 242L/49a, all at original issue or later approved revision.     FAA 2007-11-19
056-07 PTZEASA Emergency AD 2007-0135-E16.05.2007Within the next 25 flight hours or 50 flight cycles, or during the next annual inspection, but not later than 31 December 2007, whicheveroccurs first after the effective date of ADGrob Aerospace GmbH [and any predecessor company] G102 "CLUB ASTIR III" G102 "CLUB ASTIR IIIb" G102 STANDARD ASTIR III  Affected S/N are listed in AD applicability section.Flight Controls – Flight Control System Welded Components –Inspection / ReplacementGrob Aerospace Service Bulletin No. MSB 306-35 dated 27 April 2007
057-07 PTZEASA Emergency AD 2007-0138-E   This AD supersedes EASA AD 2006-0235-E(064-06 PTZ)18.05.2007See AD compliance for detailsEUROCOPTER – (formerly EUROCOPTER-FRANCE, AEROSPATIALE)   EUROCOPTER helicopters models: - AS 350 B, BA, BB, B1, B2, B3 and D- AS 355 E, F, F1, F2 and NTail Rotor - Tail rotor blades skin- Inspection / RepairEUROCOPTER AS 350 Alert Service Bulletin No. 05.00.40 Revision 2  EUROCOPTER AS 355 Alert Service Bulletin No. 05.00.38 Revision 2
058-07 PTZEASA Emergency AD 2007- 0139-E18.05.2007See AD compliance for detailsEUROCOPTER (Formerly EUROCOPTER-FRANCE – AEROSPATIALE)   EUROCOPTER AS350 B, BA, BB, B1, B2, B3 and D and EUROCOPTER AS355 E, F, F1, F2 and N helicoptersSee AD applicability for details.Fuselage - Center cross-member under the cabin floor -Inspection / ModificationEUROCOPTER AS 350 ASB No. 53.00.37 initial issue.EUROCOPTER AS 355 ASB No. 53.00.23 initial issue
059-07 PTZFAA 2007-10-1521.06.2007Unless already done, within the next 90 days after the effective date of this AD, see AD compliance for detailsCessna Aircraft Company Models 208 and 208B, all serial numbers, that are certificated in anycategoryTo assure that the pilot has enough information and the necessary equipment to prevent loss ofcontrol of the airplane while in-flight during icing conditionsNone
060-07 PTZEASA Emergency AD 2007- 0141-E23.05.2007Before further flight, verify the Part Number (P/N) and Serial Number(S/N) of the main rotor and tail rotor servo-controls, see AD compliance for detailsEUROCOPTER – (formerly EUROCOPTER-FRANCE, AEROSPATIALE)   EUROCOPTER helicopters models: - AS 350 B, BA, BB, B1, B2, B3 and D - AS 355 E, F, F1, F2 and NSee AD applicability for detailsRotor Flight Controls - Main & Tail Rotors Servo-Controls -Inspection / ReplacementEUROCOPTER AS 350 Alert Service Bulletin No. 01.00.58 Rev.1EUROCOPTER AS 355 Alert Service Bulletin No. 01.00.53 Rev. 1 or any subsequent approved revision
061-07 PTZFAA 2007-11-0626.07.2007As soon as practicable after the effective date of this AD but no later than July 31, 2007, unless the actions havealready been done, see AD compliance for detailsTurbomeca Arrius 2F turboshaft engines with fuel control units (FCUs)not incorporating modification Tf 55. These engines are installed on, but not limited to, Eurocopter EC120B helicoptersPrevent an uncommandedengine in-flight shutdown on a single-engine helicopter, resulting in a forced autorotation landing or an accidentEASA AD 2006-0237 and Turbomeca Mandatory Service Bulletin No. 319 73 4055, Update No. 1, dated March 17, 2006
062-07 PTZFAA 2006-24-08 correction19.12.2006see AD compliance for detailsApplies to Pratt & Whitney Canada (P&WC) PW535A turbofan engines that have fuel manifold, part number (P/N) 3052627-01, installed. These engines are installed on, but notlimited to Cessna Airplane Co. model 560 Citation Ultra Encore airplanesPW535A fuel manifold leakage that could resultin engine fire, in-flight shutdown or damage to the airframeTransport Canada AD CF-2006-22, andP&WC Alert Service Bulletin PW500-72-A30314
063-07 PTZFAA 2007-11-0127.06.2007Within 100 hours time-in-service, unless accomplished previously; see AD compliance for detailsRobinson Helicopter Company Model R44 helicopters, through serial number (S/N) 1576, and Model R44 II helicopters, through S/N 11107, with a seat belt buckle assembly (buckle assembly) part number C628-4, revision M or prior, installed, certificated in any categoryPrevent cracking in the buckle assembly stainless support strap and failure of a seat beltRobinson Helicopter Company ServiceBulletin SB-56, dated March 29, 2006
064-07 PTZFAA 2007-11-1129.06.2007See AD compliance for detailsAIRBUS   Model A318, A319, A320, and A321 airplanes, certificated inany categoryDetect and correct cracking in an MLG sliding tube, which could result in failure of the sliding tube, loss of oneaxle, and consequent reduced controllability of the airplaneAirbus All Operators Telex (AOT) A320-32A1273, Rev.01; Airbus Service Bulletin A320-32A1273, Rev. 02; Messier-Dowty Service Bulletin 201-32-43; Messier-Dowty Service Bulletin 200-32-286, Re.1, and F-2005-115
065-07 PTZEASA 2007- 015512.06.2007Corrective actions have to be performed onaircrafts with affected engines installed until December 31, 2007; See AD compliance for detailsBRP-Rotax GmbH & Co. KG; Bombardier-Rotax GmbH & Co. KG; Bombardier-Rotax GmbH; Rotax 912 A series Rotax 912 F series Rotax 912 S series Rotax 914 F seriesThese engines are known to be installed on different aircraft types- see AD appicability for detailsEngine Fuel and Control – Coolant Specification - ModificationBRP Rotax Service Bulletin SB-912-043 R2 and SB-914-029 R2
066-07 PTZEASA 2007-0156  This AD supersedes and cancels EASA AD 2005-002114.06.2007See AD compliance for detailsHoneywell International, Inc. See AD Applicability for Communication Units and Mode S Transponder Units and P/N   The referenced equipment is known to be installed on, but not limited to the following aeroplanes: BAE Systems Jetstream 4100 series; Bombardier BD-700-1A10 and BD-700-1A11; Cessna Model 525, 550, 560 and 650 series; Dassault Model Falcon 900EX and Falcon 2000EX series; EMBRAER Model EMB-135 and -145 series; Learjet Model 45; Lockheed Model 382G series;Raytheon Model Hawker 800, Hawker 800XP, and Hawker 1000 seriesCommunication – Comm Units & Transponders – Modification /ReplacementHoneywell Technical Newsletter A23-1146-004; Honeywell Alert Service Bulletin (ASB) A21-3851-002; Honeywell ASB A24-3851-005; Honeywell ASB 7510700-23-A0047 Rev.1; Honeywell ASB 7510700-23-A0048; Honeywell ASB 7517400-23-A0017; Honeywell ASB 7517400-23-A6015 Rev.1;Honeywell ASB 7517400-23-A6016
067-07 PTZFAA 2007-11-1706.06.2007See AD compliance for detailsCessna Aircraft Company:Cessna Model 500, 501, 550, 551, S550, 560, 560XL, and 750 airplanesEnsure that the fire extinguishing bottles are activated in the event of an engine or auxiliary power unit (APU) fire, and that flammable fluids are not supplied during a fire, which could result in anunextinguished fire in the nacelle or APUSB500-26-02 SB500-26-02 SB550-26-05 SB560-26-01 SB560XL-26-02 1 SB750-26-05 SBS550-26-02
068-07 PTZCF-2006-17R1   This AD supersedes CF-2006-17 (050-06 PTZ)20.06.2007Within twelve (12) months from the effective date of this directive, unless already accomplishedBombardier Inc. Model CL-600-2B19, serial number 7003 thru 7990 and 8000 thru 8070Short-circuit failures of Tyco Hartman AC contactors – 1K4XD and K4XA - located in the avionics bayBombardier service bulletin (SB) 601R-24-123, Revision B, dated 16 February 2007
069-07 PTZFAA 2007-08-07 18.05.2007Upon accumulating 1,500 hours time-in-service (TIS) or within the next 50 hours TIS after May 18, 2007 (the effective date of this AD), whichever occurs later, See AD compliance for detailsPiper AircraftModels PA-25, PA-25-235, and PA-25-260, all serial numbers up to LA-260-06008, certificated in any category REAR AND FORWARD SUPPORTS OF BOTH HORIZONTAL STABILIZER MODIFICATION  Severe corrosion and cracks in both supports. The probable cause for those failures is the accumulation of steam or application products vapors MCAI Dirección Nacional de Aeronavegabilidad AD No. RA 2006-06-01, Rev. 1 LAVIA S.A., Amendment No. 39/03-041, dated November 17, 2006; and Latinoamericana de Aviación S.A. Service Bulletin No. 25/53/03, dated May 10, 2006
070-07 PTZEASA Emergency AD 2007 – 0160-E11.06.2007Before the next cargo hook operations and however within and not later than August 31, 2007; successively before each single operationof the cargo hook; See AD compliance for detailsAgusta S.p.a. Agusta helicopters A109E, A109LUH, A109S, A119 equipped with thesingle or double Cargo Hook installations with the certain P/NEquipment & Furnishings - Cargo Hook P/N 528-010-01 /Lever P/N 232-028-00 - InspectionAgusta - Alert Service Bulletins 109EP-78; 109L-006; 109S-12; 119-21original issue or later approved revisions.
071-07 PTZEASA 2007-0163This AD Supersedes DGAC AD (CN) 2002-514 R125.06.2007See AD compliance for detailsAIRBUS A318, A319, A320 and A321 aircraft, all certified models, all serial numbersFlight Controls – Elevator Backlash – InspectionAIRBUS AMM task 27.34.00.200.001 issued on February 1997;AIRBUS SB A320-27-1132 Revision 01; and SB A320-27-1114 Revision 05
072-07 PTZEASA 2007-016125.06.2007See AD compliance for detailsAIRBUS A318, A319, A320 and A321 aircraft, all certified models, all serial numbers up to MSN 2850 inclusive, except MSN’s 0115, 0184, 0782, 1151,1190, 2650, 2675, 2706, 2801 and 2837Fuselage - Centre Fuselage - Main Landing Gear Door KeelBeam Hinge and Actuator Fitting - InspectionAIRBUS Service Bulletin A320-53-1195 andAIRBUS Service Bulletin A320-53-1196
073-07 PTZEASA 2007-0065R128.03.2007See AD compliance for detailsAIRBUS A318, A319, A320 and A321 aircraft, all models, all serialnumbersLanding gear – Normal extension and retraction –Inspection of the selector valves 40GA and 41GAAIRBUS Service Bulletin A320-32-1290
074-07 PTZEASA 2006-0153R226.06.2007See AD compliance for detailsA318, A319, A320 and A321 aircraftAuxiliary Power Unit (APU) - Starter Motor and Air Intake System Inspection/CleaningAIRBUS Service Bulletin A320-49-1068; A320-49-1070; A320-49-1075; A320-49-1077
075-07 PTZFAA 2007-12-0616.06.2007See AD compliance for detailsHawker Beechcraft Corporation-Type Certificate formerly held by Raytheon Aircraft Corp. and BeechC90A; B200; B200C; B300; B300CDetect and correct improperlyassembled or damaged flight controlsRaytheon Aircraft Company Mandatory Service Bulletin Number SB 27-3761 orMandatory Service Bulletin Number SB 27-3761
49-2002 R1 PTZ    49-2002 R1 PTZ14.06.2007veljavnost takojVelja za jadralna letala tipa B4-PC 11 za vse tri modele: B4-PC 11, B4-PC 11A ter B4-PC 11AF, proizvajalca PILATUS Flugzeugwerke AG, 6370 Stans, Schweiz, ki so vpisani v Register letal Republike SlovenijePreklic omejitev in zahtev PTZ  49-2002 z dne 09. 05. 2002 (prepoved kakršnegakoli akrobatskega letenja ter zmanjšanje maksimalna dovoljene hitrosti letenja (VNE) na 200 km/h)Referenčni dokument:Poročilo in ugotovitve komisije za preiskovanje vzrokov letalskih nesreč
076-07 PTZEASA 2007-016528.06.2007At the next periodical inspection, but not later than 31 December 2007; See AD compliance for detailsEUROCOPTER DEUTSCHLAND GmbHEC135 and EC635 helicoptersElectrical Power – DC Power Supply Lines – ModificationEurocopter EC135 ASB No. EC135-24A-013 at Rev. 01
077-07 PTZEASA 2007-015614.06.2007See AD compliance for detailsHoneywell International, Inc. Comm Units and Mode S Transponders RCZ-833J part numbers (P/Ns) 7510700-763 and -863; RCZ-833K P/Ns 7510700-765 and -875; RCZ-851J P/N 7510700-813; RCZ-851K P/N 7510700-815; and RCZ-854J P/Ns 7510700-725 and -825 Communication Units; andXS-856A P/Ns 7517400-865 and -885; XS-856B P/Ns 7517400-866 and -886; and XS-857A P/Ns 7517400-876 and -896 Mode S TransponderUnitsCommunication – Comm Units & Transponders – Modification /ReplacementHoneywell Technical Newsletter A23-1146-004; ASB A24-3851-002 [7510700-23-A6046]; Honeywell ASB A21-3851-005 [7510700-23-A0047]; Honeywell ASB 7510700-23-A0047 Rev.1;Honeywell ASB 7510700-23-A0048; Honeywell ASB 7517400-23-A0017;Honeywell ASB 7517400-23-A6015 Rev.1;Honeywell ASB 7517400-23-A6016
078-07 PTZEASA 2007-016829.06.2007Within 72 months from the effective date of this AD; see AD compliance for detailsSaab AB, Saab Aerosystems (Saab Aircraft AB)  SAAB SF340A and SAAB 340BFuel Tank SafetyWing – Fuel Access Door – Improved SealingSAAB Service Bulletin SB-340-57-031
079-07 PTZEASA 2007-016929.06.2007Within 72 months from the effective date of this AD; see AD compliance for detailsSaab AB, Saab Aerosystems (Saab Aircraft AB)  SAAB SF340A and SAAB 340BFuel Tank Safety Fuel - Indicating - Wire separation of Fuel Quantity IndicationSystem (FQIS) Signal Conditioner 28 VDC supply - FuselageSAAB Service Bulletin SB-340-28-025
080-07 PTZEASA 2007-017029.06.2007Within 72 months from the effective date of this AD; see AD compliance for detailsSaab AB, Saab Aerosystems (Saab Aircraft AB)  SAAB SF340A and SAAB 340BFuel Tank Safety Fuel - Indicating - Wire separation of Fuel Quantity IndicationSystem (FQIS) Wiring - WingSAAB Service Bulletin SB-340-28-024
081-07 PTZEASA 2007 - 017806.07.2007Within 600 flight hours or 750 flight cyclesor 100 days after the effective date of this AD, whichever occurs first; see AD compliance for detailsAIRBUS A318, A319, A320 and A321 all certified models, allmanufactured serial numbers (MSN) up to MSN 2860Flight controls – Trimmable Horizontal Stabilizer Actuator -InspectionAIRBUS Service Bulletin A320-27A1179
082-07 PTZEASA Emergency AD 2007-0176-E26.06.2007Before next flight after the effective date of this directive and thereafter atintervals not to exceed 12 months; see AD compliance for detailsDG Flugzeugbau GmbH; Glaser-Dirks Flugzeugbau GmbH; ELAN Flight Ltd (Slovenia); ELAN Line d.o.o. (Slovenia); AMS-Flight d.o.o. (Slovenia)   Sailplanes: DG-500/20 ELAN, all serial numbers; DG-500/22 ELAN, all serial numbers; DG-500 ELAN ORION, all serial numbers; and DG-500 ELAN TRAINER, all serial numbers. Powered Sailplanes: DG-500M, all serial numbers; andDG-500MB, all serial numbersFlight Controls – Bellcrank Bearing Attachment Bolt – Inspection /Re-Torque / Replacement [Life Limitation]DG Flugzeugbau GmbH Technical Note (TN) 348/19 and 843/26 (same document), dated 19 June 2007, including the related working instructionsnumber 1 and number 2
083-07 PTZEASA 2006 – 0251 R2This AD revises AD 2006-0251R101.09.2006see AD compliance for detailsEUROCOPTER (formerly EUROCOPTER FRANCE, AEROSPATIALE) Helicopters: - AS 355 E, F, F1, F2, N - AS 350 B, BA, BB, B1, B2, B3 and D,fitted with sliding door(s) before embodiment of MOD 073298 and/orMOD 073308Doors – Sliding Door Rear Roller Support Shaft and Rear FittingEUROCOPTER AS 350 Alert Service Bulletins No. 05.00.47 and52.00.30; and AS 355 ASB No. 05.00.45 and 52.00.23
084-07 PTZEASA 2007-0182 This AD is revised and replaced by EASA 2007-0182 R1 (PTZ 035-07)  16.07.2007Not later than 31 October 2007, see AD compliance for detailsThielert Aircraft EnginesTAE125-01 and TAE125-02-99 engines, all serial numbers, installed in Diamond Aircraft Industries DA42 aircraftPower Plant – Engine Installation – InspectionTAE Installation Manual IM-02-01 Issue 4, Revision 1, Chapter 13 and TAE Installation Manual IM-02-02 Issue 1, Revision 3, Chapter 13
085-07 PTZEASA 2007-0183 This AD is revised and replaced by EASA 2007-0183 R1(PTZ 110-07)16.07.2007Within the next 100 Flight Hours, whichever occurs first after the effective date ofthis AD, but not later than 31 October 2007, see AD compliance for detailsDiamond Aircraft Industries GmbH   DA 42 airplanes, serial numbers 42.004 through 42.269; and42.AC001 through 42.AC109 (Canadian production line)Engine Controls – Engine Control Unit Back-up Batteries - InstallationDiamond Aircraft Industries (DAI) MSB-42-042; DAI WI-MSB-42-042; DAI SI 42-040; DAI AFM TR-MÄM-42-240 and AMM-TR-MÄM-42-240; TAE Installation Manual IM-02-01 Issue 4, Revision 1, Chapter 13  andTAE Installation Manual IM-02-02 Issue 1, Revision 3, Chapter 13
086-07 PTZEASA 2007-017101.08.2007See AD compliance for detailsAPEX AIRCRAFT  All HR100/200, HR100/200B, DR300 and DR400 equipped with “Avions Robin” nose landing gearNose Landing Gear – Support plate of oleo outer cylinder –Inspection/RepairApex SB  No. 101 revision 5 dated 22 May 2007
087-07 PTZEASA Emergency AD 2007-0192-E17.07.2007Unless already accomplished, within the next 20 flight hours after the effective date of this EAD and not later than Sept 30, 2007See AD compliance for detailsAgusta S.p.a.   A109E, A109S, A109LUHPower Plant - Lower Semichannel assemblies p/n 109-0641- 10-213 OR 109-0642-01-171 of the Forward Firewall –Inspection / ModificationAgusta - Alert Bollettino Tecnico (BT) 109EP-79, 109S-15 and 109L-007
088-07 PTZEASA Emergency AD 2007-0194-E01.08.2007Within the next 25 flight hours or 50 flights, or during the next scheduled 100 hours (or annual) inspection, whichever occurs first after the effective date of this ADSee AD compliance for detailsGROB AEROSPACE GmbH   TWIN ASTIR and G103 Gliders, all variants; andG103C TWIN III SL Powered SailplanesFuselage, Wing & Stabilisers Structure – Inspection/RepairGrob Aerospace Service Bulletin No. MSB 315-74/1, MSB 869-25/1
089-07 PTZEASA Emergency AD 2007-0200-E01.08.2007See AD compliance for detailsMoravan Aviation s.r.o Zlin Z 42, Z 42M, Z 42MU, Z 142, Z 142C and Z 242L aircraft, all serial numberswithout the wing reinforcement modificationIntroduction of new Airworthiness- and Operating LimitationsMORAVAN Mandatory Service Bulletins: Z42/55a for Z42, Z42M and Z42MU aircraft; Z142/54a for Z142 aircraft; Z142C/31a for Z142C aircraft; andZ242L/51a for Z242L aircraft
090-07 PTZCF-2007-1031.07.2007See AD compliance for detailsBombardier Inc. Model CL-600-2B19, serial number 7003 thru 7990 and 8000 and subsequentBombardier Aerospace CL-600- 2B19 Flaps FailureBombardier Service Bulletin (SB) 601R-27-150 and FAA 2007-17-07
091-07 PTZFAA 2007-14-0316.08.2007Within the next 25 hours time-in-service (TIS) after August 16, 2007 or within 60 days after August 16, 2007 whichever occurs firstCirrus Design Corporation Model SR20 airplanes, serial numbers (SN) 1005 through 1798, andModel SR22 airplanes, SN 0002 through 2437Correct pick-up collar support fasteners of the CAPS- Cirrus Airplane Parachute SystemCirrus Alert Service Bulletin No. SB A2X-95-10 R2 or Cirrus Alert Service Bulletin No. SB A2X-95-10 R1
092-07 PTZFAA 2007-16-0115.08.2007Before further flight; See AD compliance for detailsEnstrom Helicopter Corp. Model F-28, F-28A, F-28C, F-28C-2, F-28C-2R, F-28F, F-28F-R, 280, 280C,280F, 280FX, TH-28, 480, and 480B helicoptersPrevent failure of a retention pin, separation of a main rotor blade from the helicopter, andsubsequent loss of control of the helicopterEnstrom Service Directive Bulletin No. T-029 and Enstrom Service Directive Bulletin0102
093-07 PTZEASA 2007- 021020.08.2007Within the next 50 flight hours after the effective date of this AD; See AD compliance for detailsCentre Est Aéronautique, Avions Pierre Robin, Constructions Aéronautiques de Bourgogne, APEX Industries   All DR220 series and DR221series aircraft models; All DR200 and all DR250 series aircraft models; All DR253 series aircraft models; All R3000 series aircraft models; All ATL series aircraft models; All R1180T and R1180TD aircraft; All DR300 series aircraft models, DR315, DR340, DR360 and DR380; All DR400 series aircraft models, except DR400/500, DR400/RP andDR400/200RFuel – Fuel Pump Electrical Grounding – ModificationAPEX SB No 060903
094-07 PTZEASA 2007-021121.08.2007See AD compliance for detailsEUROCOPTER   EC 120 B helicopters, all serial numbers that are fitted with tail rotor drive shafts PartNumber (P/N) C651A3102051 and C651A3102052.Tail Rotor Drive - Rear Drive Shaft Friction Ring - Inspection /ReplacementEUROCOPTER EC120 Alert Service Bulletin No. 05A006
095-07 PTZEASA 2007-021221.08.2007At the next scheduled “A” Type maintenance inspection orwithin the next 3 months after the effective date of this AD, whichever occurs first; See AD compliance for detailsAircraft Industries a.s.; Strojírny první pětiletky n.p.; LET n.p.; and LET a.s. L13 and L13A BLANÍK sailplanes, all serial numbersFlight Controls – Control Sticks and Bridge – Inspection/ReplacementAircraft Industries a.s Mandatory Bulletin No. L13/105a andDocumentation Bulletins No.L13/009d, L13/010d and L13/011d
096-07 PTZEASA 2007-021321.08.2007See AD compliance for detailsAIRBUS A318, A319, A320 and A321 aircraft, all certified models, all serialnumbers (MSN) except aircraft that have received AIRBUS modification 32025 in production or AIRBUS Service Bulletin (SB) A320-57-1118 in serviceWings – Outer Wing Main Landing Gear Support Rib 5 Fitting – Inspection / ModificationAIRBUS Service Bulletin (SB) A320-57-1118 at original issue; and SB A320-57-1138 Revision 01
097-07 PTZEASA 2007-021421.08.2007Before 31March  2009; See AD compliance for detailsAIRBUS models A318-111, A318-112, A319-111, A319-112, A319-113, A319-114, A319-115, A319-131, A319-132, A319-133, A320-111, A320-211, A320-212, A320-214, A320-215, A320-216, A320-231, A320-232, A320-233,A321-111, A321-112, A321-131, A321-211, A321-212, A321-213, A321-231 and A321-232Equipment/Furnishings – 103VU Box – Hinge Pin Stopper –ModificationAIRBUS Service Bulletin (SB) A320 25-1535
098-07 PTZFAA 2007-16-1023.08.2007See AD compliance for detailsTeledyne Continental Motors (TCM) models TSIO-520-BE, TSIO-550-A, TSIO-550-B, TSIO-550-C, TSIO-550-E, and TSIO-550-G These engines are installed on, but not limited to, Adam Aircraft A500, Columbia Aircraft Manufacturing LC41-550FG, Mooney Airplane Company M20TN (Acclaim), andPiper Aircraft Incorporated PA-46-310P (Malibu) airplanesPrevent the turbine rotor from separating from the shaft of the turbocharger due to a machining defect in the turbocharger compressorTeledyne Continental Aircraft Engine Mandatory Service Bulletin (MSB) MSB07-4
099-07 PTZEASA 2007-021723.08.2007See AD compliance for detailsAIRBUS A318, A319, A320 and A321 aircraft, all certified models and all serial numbers equipped with at least one NORTHROP-GRUMMAN (previously LITTON) air data/inertial reference unit (ADIRU)Navigation – NORTHROP-GRUMMAN (previously LITTON)ADIRU – ReplacementSee AD reference publications
100-07 PTZEASA 2007–0218This AD supersedes EASA 2006-0222 (059-06 PTZ)07.09.2007See AD compliance for detailsAIRBUS A318, A319, A320 and A321 aircraft, all certified models, all serial numbers (MSN), except aircraft that have received AIRBUS modification37508 in production or AIRBUS Service Bulletin (SB) A320-28-1159 in serviceFuel – Main Fuel Pump System / Fuel Pumps – AirworthinessLimitations / Inspection / ReplacementAIRBUS SB A320-28-1159 and AIRBUS AFM TR 4.03.00/28 issue 02
101-07 PTZEASA 2007-022127.08.2007See AD compliance for detailsCFM International SA (CFM)CFM56-5B series engines (see AD Aplicability for models) These engines are known to be installed on, but not limited to, Airbus A318, A319, A320 and A321 series aircraftTime Limits – Low Pressure Turbine Rear Frame – Life ReductionCFM56-5B Engine Shop Manual chapter 05, revision 47and CFM56-5B Service Bulletin S/B 72-0620
102-07 PTZEASA 2007- 0018R1This AD revises EASA AD 2007-001829.01.2007See AD compliance for detailsTURBOMECA, S.A. ARRIEL 1 turboshaft engines (see AD Aplicability for models) These engines are known to be installed on, but not limited to: Eurocopter AS 350 B, AS 350 BA, AS 350 B1 and AS 350 B2 helicopters;and Sikorsky S-76C helicoptersEngine - Gas Generator 2nd Stage Turbine -Inspection/ReplacementTurbomeca, S.A. Alert Service Bulletins: A292 72 0807 A292 72 0809 A292 72 0810and Turbomeca Service Bulletin 292 72 0347
103-07 PTZEASA 2007-023106.09.2007See AD compliance for detailsAgusta S.p.a.   A109E and A119 helicoptersHydraulic Power – Hydraulic Pipes P/N’s 109-0761-64-103 and 109-0761-65-103 – Inspection / ReplacementAgusta Bollettino Tecnico 109EP-73 and 119-22 at original issue or later approved revisions
104-07 PTZEASA 2007-023206.09.2007Within the next 50 flight hours after the effective date of this directive, but notlater than 31 October 2007, whichever occurs first; See AD compliance for detailsThielert Aircraft Engines TAE125-01 engines all serial numbers (s/n), up to and including s/n 02-01-1018   These engines are known to be installed on, but not limited to, Cessna 172 and (Reims-built) F172 series, Piper PA-28series), APEX (Robin) DR 400 series and Diamond DA40 and DA42 series aircraft.Engine Oil System - Catchtank (Sump) Filter Adaptor - InstallationThielert Service Bulletin TM TAE 125-0016, Initial Issue or Revision 1 or laterapproved revisions
105-07 PTZCF-2005-10R3This AD supersedes CF-2005-10R2 17.09.2007Within the next 100 hours air time, but no later than 30 November 2007,See AD compliance for detailsBell Helicopter Textron Canada Models 206A and 206BFuel Distribution SystemAlert Service Bulletin (ASB) 206-05-103, Revision A, dated 12 July 2006
106-07 PTZCF-2007-02R1 This AD supersedes CF-2007-02 (PTZ 028-07)14.09.2007Within the next 16 hours flight time, but no later than 15 October 2007, unless already accomplishedBell Helicopter Textron Canada (BHTC) Models 206 A and B series helicopters that have the certain Transmission Pylon Support Spindle Part Number installed- see AD for detailsTransmission Pylon Support Spindlenone
107-07 PTZCF-2007-1317.09.2007See AD compliance for detailsBell Helicopter Textron Canada (BHTC) Model 206B series helicopters including those converted from model 206A, serial numbers up to 4366 and certain 206L helicopters-see ADPower Turbine RPM Steady State Operation AvoidanceAlert Service Bulletin (ASB) 206-07-115 or 206L-07-146, as applicable, dated 21 May 2007, or later revisions
108-07 PTZCF-2007-1617.09.2007As soon as possible, but not later than 25 hours air time or 30 days from the effective date of this directive, See AD compliance for detailsBell Helicopter Textron Canada (BHTC) Model 206 series helicopters S/N up to 4618 and Model 206L series helicopters S/N up to 52340Disc Assemblies –Tail rotor driveshaft (Thomas Couplings)206 series: ASB-206-07-114 dated 28 March 2007206L series: ASB-206L-07-145 dated 28 March 2007
109-07 PTZFAA 2007-07-07 R1 This AD revises FAA 2007-07-07 (PTZ 049-07)  12.09.2007See AD compliance for detailsThis AD applies to General Electric Company (GE) CF34-1A, -3A, -3A1, -3A2, -3B, and - 3B1 turbofan engines, with certain fan disks part numbers- see AD.These engines are installed on, but not limited to, Bombardier Canadair airplane models CL-600- 2A12, -2B16, and -2B19.Prevent an uncontained fan disk failure and airplane damageGE Alert Service Bulletin No. CF34-AL S/B 72-A0231, CF34-AL S/B 72-A0233 andCF34-BJ S/B 72-A0212
110-07 PTZEASA 2007-0183 R1 This AD is revised and replaced with EASA 2007-0183 R2 (PTZ 137-07)16.07.2007Within the next 100 Flight Hours, but not later than 31 October 2007, whicheveroccurs first after the effective date of this AD, See AD compliance for detailsDiamond Aircraft Industries GmbH DA 42 airplanes, serial numbers 42.004, 42.006, 42.009 through 42.156, 42.158 through 42.176, 42.178 through 42.190, 42.192 through 42.233, 42.235 through42.246, 42.248 through 42.254, 42.256 through 42.261, 42.263 through 42.269; and 42.AC001 through 42.AC109Engine Controls – Engine Control Unit Back-up Batteries - InstallationDiamond Aircraft Industries (DAI) Mandatory Service Bulletin MSB-42-042; DAI WI-MSB-42-042; DAI Service Information SI 42-040; DAI AFM TR-MÄM-42-240 and AMM-TR-MÄM-42-240;TAE Installation Manual IM-02-01 Issue 4, Rev 1 and TAE Installation Manual IM-02-02 Issue 1, Rev 3
111-07 PTZFAA 2007-11-0202.10.2007See AD compliance for detailsEnstrom Helicopter Company: Model F-28A, F-28C, and F-28F helicopters, excluding serial number (S/N) 816 and subsequent; Model 280, 280C, 280F, and 280FX helicopters, excluding S/N 2100 and subsequent; and Model TH-28, 480, and 480B helicopters, excluding S/N 5058 and subsequent,certificated in any categoryDetect corrosion and prevent failure of a main rotor push-pull control rod (push-pull rod), and subsequent loss of control of the helicopterEnstrom Helicopter Corporation Service Directive Bulletin No. 0096, No. T-019, Enstrom Helicopter Corporation Service Information Letter No. T-019, No. 0156
112-07 PTZEASA 2007- 0236This AD supersedes EASA AD 2006-0251R214.09.2007See AD compliance for detailsEUROCOPTERAS 350 and AS 355 helicoptersDoors – Sliding Door Rear Roller Support Shaft and Rear FittingInspection/ReplacementEUROCOPTER AS350 ASB No. 05.00.47 initial issue and ASB No. 52.00.30rev 1 or EUROCOPTER AS355 ASB No. 05.00.45 initial issues and ASB No. 52.00.23 rev 1
113-07 PTZFAA 2007-17-1802.10.2007See AD compliance for detailsMcDonnell Douglas Model DC-9-11, DC-9-12, DC-9-13, DC-9-14, DC-9-15, DC-9-15F, DC-9-21, DC-9-31, DC-9-32, DC-9-32 (VC-9C), DC-9-32F, DC-9-33F, DC-9-34, DC-9-34F, DC-9-32F (C-9A, C-9B), DC-9-41, DC-9-51, DC-9-81 (MD-81), DC-9-82 (MD-82), DC-9-83 (MD-83), and DC-9-87 (MD-87) airplanes, and Model MD-88 airplanesPrevent an electrical short of the static port heater from sparking and igniting the insulation blanket adjacent to the static port heater, which could result in smoke and/or fire in the cabin areaBoeing Service Bulletin DC9-30-097, Revision 2, dated May 27, 2005
114-07 PTZEASA 2007-024821.09.2007Within 72 months after the effective date of this directive, see AD compliance for detailsSaab AB, Saab Aerosystems (formerly Saab Aircraft AB)Model SF340A and 340B aircraft, all serial numbersFuel System - Fuel Tank Conduits Wiring Protection – Modification[Fuel Tank Safety]SAAB Service Bulletin SB-340-28-026 original issue or later approved revisions
115-07 PTZCF-2007-1724.09.2007Within 5000 hours air time after the effective date of this directive, unless already accomplishedBombardier Inc. Model CL-600-2B19 aircraft, serial numbers 7003 through 7067 and 7069 through 7924Fuel System Safety - Lack of Sealant on Collector Fuel Tank Bolts and Transfer Ejector PumpsBombardier Service Bulletin (SB) 601R-28-051 rev.A; SB 601R-28-060 rev. A
116-07 PTZCF-2007-1824.09.2007Within 5000 hours air time after the effective date of this directive, see AD compliance for detailsBombardier Inc. Model CL-600-2B19 aircraft, serial numbers 7003 through 7067 and 7069 through 7797Fuel System Safety -Insufficient Electrical Bonding Between Fuel Boost Pump Canister and the Pressure Pick-Up LineBombardier Service Bulletin (SB) 601R-28-057
117-07 PTZEmergency AD CF-2007-21Upon receiptBefore further flight unless already accomplishedBell Helicopter Textron Canada (BHTC) all helicopter Models: 206 series, 222 series, 230, 407, 427 and 430Tail Rotor Blades206 series ASB 206-07-116see AD
118-07 PTZFAA 2007-19-53Upon receiptBefore further flight, replace any affected blade with an airworthy blade with a serialnumber not listed in the applicability section of this AD, see AD compliance for detailsBell Helicopter Textron, Inc. (BHTI) Model 204B, 205A, 205A-1, 205B, 210, 212, 412, 412EP, and 412CF helicopters, certificated in any category, with certain part-numbered and serial-numbered tail rotor blades installedTail rotor blade tip weights slung from the blades during flightSee AD for list of Alert Service Bulletins
119-07 PTZEASA 2007-025702.10.2007Within the next 16 hours flight time, but not later than 15 October 2007,whichever occurs first after the effective date of this directive, see AD compliance for detailsAgusta S.p.A AB 206 A and AB 206 B helicopters, all S/N, that have certain Transmission Pylon Support Spindle Part Number (P/N) 206-031-554 (Spindle) S/N installed, repaired by H-S Tools & Parts Inc.Main Rotor Drive – Transmission Pylon Support Spindle –Identification/ReplacementNone
120-07 PTZEASA 2007 - 025603.10.2007within 30 days after the effective date of this AD; see AD compliance for detailsPacific Scientific Company Restraint Systems: 2000029, 2000067, 2000115  These p/n’s are known to be installed on, but not limited to, EUROCOPTER a/c models AS 350, AS 355, EC120, EC 130, EC 155Equipment and Furnishing - Seat Restraint System Plastic RotaryBuckle Handle - Inspection/ReplacementSB Notice of release   Pacific Scientific SB 25-1111432  Recall Application Form
121-07 PTZENAC EAD 2007-32404.09.2007See AD compliance for detailsAgusta S.p.A.AB206A and AB206B series Helicopters, all serial numbersTail Rotor Driveshaft Disk AssembliesAgusta Alert Mandatory SB 206-243
122-07 PTZEASA 2007 - 0064R1   This AD revises EASA 2007-0064 (036-07 PTZ)05.10.2007Unless already accomplished, before November 27 2008; See AD compliance for detailsAIRBUS  A319, A320 and A321 aircraftWing - Dry Bay Skin – InspectionAIRBUS SB A320-57-1121
123-07 PTZEASA 2007 - 024908.10.2007Unless accomplished previously, within the next 600 Flight Hours after the effective date of this AD; See AD compliance for detailsAIRBUS  A318, A319, A320 and A321 aircraftFire Protection – Cargo Compartment Fire Extinguishing – Inspection of Bottle Wiring Connection – Inspection and ContinuityCheckAIRBUS Service Bulletin A320-26A1068
124-07 PTZEASA 2007- 026116.10.2007At the next scheduled maintenance inspection or within the next 3 months after the effective date of this AD, whicheveroccurs first; see AD compliance for detailsAircraft Industries a.s, LET k.p., LET a.s. and LETECKÉ ZÁVODY a.s.  L 23 SUPER-BLANÍK sailplanes, all serial numbersFlight Controls – Control sticks and bridge – Inspection/ReplacementAircraft Industries a.s Mandatory Bulletin No. L23/050a Rev. 2  Aircraft Industries a.s Documentation Bulletin No.L23/020d original issue
125-07 PTZFAA 2007-21-0515.11.2007See AD compliance for detailsInternational Aero Engines (IAE) model V2500-A1, V2522-A5, V2524- A5, V2527-A5, V2527E-A5, V2527M-A5, V2530-A5, V2533-A5, V2525-D5, and V2528-D5 (see AD for details); These engines areinstalled on, but not limited to, Airbus A319, A320, A321, and Boeing MD-90 airplanesPrevent uncontained failure of the HPT stage 2 air sealIAE Service Bulletin (SB) V2500-ENG-72-0500; IAE SB V2500- ENG-72-0501; IAE SB V2500-ENG-72-0502
126-07 PTZEASA Emergency AD 2007-0274-E23.10.2007See AD compliance for detailsSchweizer Aircraft Corporation269D helicoptersFuselage – Aft Fuselage Assembly and Horizontal StabiliserAttachment – Inspection / Repair / ModificationSchweizer SB DB-018.2
127-07 PTZCF-2007-2301.11.2007Within 5000 hours air time after the effective date of this ADBombardier Inc. Model CL-600-2B19 aircraft, serial numbers 7003 through 7067, and 7069 through 7981Fuel System Safety -Insufficient Electrical Bonding Between Fuel Tubes and Insufficient Lightning Current Capability of Fuel Tube CouplingsBombardier Service Bulletin (SB) 601R-28-054, Revision A, dated 7 August 2006, or later revisions
128-07 PTZCF-2007-2408.11.2007See AD compliance for detailsPratt & Whitney Canada PW 200 Compressor TurbineDisk Inspection and Retaining Nut ReplacementP&WC Alert Service bulletin PW200-72-A28280
129-07 PTZFAA 2007-22-0230.11.2007Within 100 hours time-in-service, unless accomplished previously; See AD compliance for detailsBell Helicopter Textron, Inc.Model 205A, 205A-1, 205B, 212, 412, 412CF, and 412EP helicoptersTo prevent loss of the forward tip weight retention block (tip block) or aft tip closure (tipclosure), loss of the blade, and subsequent loss of control of the helicopterBell Helicopter Textron, Inc. Alert Service Bulletins 205-00-80,205B-00-34, 212-00-111, 412-00-106, and 412CF-00-13
130-07 PTZEASA 2007 - 027609.11.2007See AD compliance for detailsAIRBUS  A318, A319, A320 and A321 aircraftEquipment / Furnishing – 80VU Rack Attachments – Inspection /Repair / ReplacementAIRBUS SB A320-25A1555,  AIRBUS SB A320-25-1557
131-07 PTZAGÊNCIA NACIONAL DE AVIAÇÃO CIVIL – BRAZIL  ANAC 2007-08-0127.09.2007Before 31 Dec. 2008; Within the next 180 days after the effective date of this AD;See AD compliance for detailsEMBRAER  EMB-135BJ aircraft modelThe inclusion of new maintenance tasks in the Critical Design Configuration Control Limitations (CDCCL)and in the Fuel System Limitations (FSL), necessary to preclude ignition sources in the fuel systemnone
132-07 PTZCF-2007-2529.10.2007See AD compliance for detailsPratt & Whitney Canada  PW305A and PW305B EnginePW305A and PW305B Engine High Pressure Compressor (HPC) Drum Rotor CracksSee AD Corrective Actions for details
133-07 PTZAIRWORTHINESS DIRECTIVE CANCELLATION EASA 2006- 0279-CN (PTZ 085-06) is withdrawn and considered superseded by DGAC France AD F-2007-004R1 (PTZ 134-07)08.11.2007See AD for detailsPARACHUTE SHOP  Parachute Harnesses and Reserve CanopiesEquipment/Furnishings – Parachute Equipment –Removal from ServiceDGACFrance AD F-2007-004R1
134-07 PTZDGAC France F-2007-004 R1Upon receipt from August 01, 2007See AD for detailsPARACHUTE SHOPParachute Reserve Canopies and Parachute Harnesses certain types manufactured between January 1, 2001 and March 6, 2007Equipment/Furnishings - Parachute - Reactivation of reserve canopiesand harnessesnone
135-07 PTZEASA 2007-0182 R1 This AD revises and replaces EASA 2007-0182 (PTZ 084-07)16 July 2007Not later than 30 November 2007; See AD compliance for detailsThielert Aircraft EnginesTAE125-01 and TAE125-02-99 engines all serial numbers, installed in Diamond Aircraft Industries DA42 aircraftPower Plant – Engine Installation – InspectionTAE Installation Manual IM-02-01 Issue 4, Revision 1, Chapter 13 and TAE Installation Manual IM-02-02 Issue 1, Revision 3, Chapter 13
136-07 PTZAIRWORTHINESS DIRECTIVE CANCELLATIONEASA F-2005-169See AD for detailsSee AD for detailsPARACHUTE SHOPVEGA 120 type reserve canopyEquipment/Furnishings - Strengthening of assembliesnone
137-07 PTZEASA 2007-0183 R2This AD revises and replaces EASA AD 2007-0182 R1 (PTZ 110-07)16 July 2007Within the next 200 Flight Hours, but not later than 30 November 2007, whicheveroccurs first; See AD compliance for detailsDiamond Aircraft Industries DA 42 certain S/NEngine Controls – Engine Control Unit Back-up Batteries - InstallationSee AD ref. publications for details
138-07 PTZEASA 2007 - 028628.11.2007Unless already accomplished, no later than 27 May 2011; see AD compliance for detailsAIRBUS aircraft A318, A319, A320, A321, all certified models, all S/N, fitted with classical standby instruments installed by AIRBUS modification 20011 or 21999 in production or by AIRBUS Service Bulletin (SB) A320-34-1280 in serviceLights – Instrument & Panel Integral Lighting – EmergencyLighting for Stand-By Instruments - ModificationSB A320-33-1057 SB A320-34-1261 SB A320-34-1280 SB A320-34-1372
139-07 PTZFAA 2007-23-1330.11.2007Within 14 days after the effective date of this ADCessna Aircraft CompanyCessna Model 560 airplanes, certificated in any category, S/N 560-0001 through -0538 inclusivePrevent an inadvertent stall due to the inadequate stall warning margin provided by an improperly adjusted stall warning system, which could result in loss of controllabilityof the airplaneSee AD for reference publications
140-07 PTZCF-2007-2723.11.2007Within 7 days after the effective date of this directive; see AD compliance for detailsDiamond Aircraft Industries Inc. model DA20-C1 aircraft powered by either Teledyne Continental Motors (TCM) IO-240-B13B or IO-240-B17B model enginesIn-Flight Engine ShutdownDA20-C1 AFM DOC No. DA202-C1 Revision 22 dated 2 November 2007
141-07 PTZEASA 2007- 028903.12.2007See AD for detailsEUROCOPTER helicopters models AS 350 B, AS 350 B1, AS 350 D,AS 355 E, AS 355 F, AS 355 F1 and AS 355 F2, all pre MOD 071995Rotor flight controls - Collective lever recess -ModificationEUROCOPTER AS 350 Alert Service Bulletin No. 67.00.16 rev. 2 and AS 355 Alert Service Bulletin No. 67.00.12 rev. 2
142-07 PTZFAA 2007-23-1619.12.2007Within the next 30 days after December 19, 2007; Within the next 10 hours time-in-service afterDecember 19, 2007; whichever occurs first; see AD compliance for detailsCessna Aircraft Company  Model 525B, serial numbers 0001 through 0013 airplanes, that are certificated in any categoryCorrect an incorrect wiring installation and to provide short-circuit protection for all wiring from the aircraft power distribution system. This condition could result in burned wiring and loss ofvarious aircraft electrical systemsCessna Citation Service Bulletin SB525B-24-02, Revision 1, dated October 4,2007
143-07 PTZCF-2007-2910.12.2007See AD Corrective Actions for detailsBombardier Inc. Model CL-600-2B19 aircraft, all serial numbersFuel System Safety - Introduction of Maintenance TasksSee AD Corrective Actions for details
144-07 PTZEASA Emergency AD 2007-0295-E04.12.2007Within the next 5 flight hours but not later than 31 December 2007, whichever occurs first after the effective date of this AD; see AD compliance for detailsAgusta S.p.a.  A109E, A109S, A109LUH and A119 helicopters, all serial numbersFuselage – Pilot & Co-pilot Door Housing Slots – Inspection /ModificationAgusta Alert Bollettino Tecnico (BT) 109EP-83 for A109E, BT 109S-18 for A109S,BT 109L-010 for A109LUH and BT 119-25 for A119
145-07 PTZFAA 2007-24-0502.01.2008See AD compliance for detailsRolls-Royce Corporation (RRC) (formerly Allison Engine Company, Inc.) AE 3007A and AE 3007C series turbofan engines. These engines are installed on, but not limited to, Cessna Aircraft Company 750 series, and Empresa Brasileira de Aeronautica S. A. (EMBRAER) EMB-135 and EMB-145 series airplanesPrevent an in-flight engine shutdown due toloss of engine oil from the starter shaft seal and possible loss of the airplaneSee Table 1 for SB list
146-07 PTZCF-2007-2810.12.2007Within 60 days after the effective date of this directive; See AD compliance for detailsBombardier Inc. Model CL-600-2C10, CL-600-2D15 and CL-600-2D24 aircraft, all serial numbersFuel System Safety - Introduction of Maintenance TasksSee AD for details
147-07 PTZEASA Emergency AD 2007-0301-E14.12.2007Within the next 5 flight hours or 5 days, whichever occurs first after theeffective date of this AD; See AD compliance for detailsEurocopter Deutschland GmbH EC135 and EC635 series helicopters, all models, serial numbers 0005 through 0444, except those equipped with autopilotRotors Flight Control – Tail Rotor Control Rod and Ball Pivot –Inspection/ReplacementEUROCOPTER EC 135 Alert Service Bulletin No. EC135-67A-017
148-07 PTZEASA Emergency AD 2007-0295R1-E04.12.2007Within the next 5 flight hours but not later than 31 December 2007, whicheveroccurs first after the effective date of this AD; See AD compliance for detailsAgusta S.p.a. A109E, A109S, A109LUH and A119 helicopters, all serial numbersFuselage – Pilot & Co-pilot Door Housing Slots – Inspection /ModificationAgusta Alert BT (Alert Service Bulletins) 109EP-83, 109S-18, 109L-010 and 119-25, all dated 29 November 2007
149-07 PTZFAA 2007-25-1614.01.2008See AD compliance for detailsMcDonnell Douglas Model DC-9-81 (MD-81) and DC-9-82 (MD-82) airplanes; certificated in any category; as identified in Boeing Alert Service Bulletin MD80-53A298,dated August 1, 2006Prevent cracking of the fuselage skin at the upper corners of the forward passenger doorjamb, which could lead to loss of overall structuralintegrity of the airplaneBoeing Alert Service Bulletin MD80- 53A298; see AD for details
150-07 PTZCF-2007-27R1 Supersedes AD CF-2007-27 31.12.2007See AD Corrective Actions for detailsDiamond Aircraft Industries Inc. model DA20-C1 aircraft serialnumbers C0001 to C0473 powered by either Teledyne Continental Motors (TCM) IO-240-B13B or IO-240-B17B model enginesIn-Flight Engine ShutdownMandatory Service Bulletin (MSB) DAC1-73-05 Revision 1  Aircraft Fight Manual DA202-C1 Rev. 23
151-07 PTZEASA 2007-031304.01.2008Within the next 5 Flight Hours (FH) or 5 days, whichever occurs first after 14. Dec. 2007; Thereafter, at intervals not to exceed 50 FH; See AD compliance for detailsEurocopter Deutschland GmbH  EC135 and EC635 series helicopters, all models, serial numbers 0005 through 0444, except those equipped with autopilotRotors Flight Control – Tail Rotor Control Rod and Ball Pivot –Inspection/ReplacementEurocopter Deutschland (ECD) EC 135 ASB No. EC135-67A-017 Rev.1
152-07 PTZEASA 2007- 031104.01.2008Within the next 110 Flight Hours but no later than 3 months, after the effectivedate of this AD; See AD compliance for detailsEUROCOPTER  EC 120 B helicopters up to serial number (s/n) 1523 inclusive and all EC130 B4 helicopters PRE Mod 073380, fitted with SICMA Type 159 energy-absorbing seatsEquipment/Furnishings – Energy absorbing seat and Metallisation braid –ModificationEUROCOPTER EC120 Alert Service Bulletin No. 25A023 original issue  EUROCOPTER EC130 Alert Service Bulletin No. 25A025 original issue
153-07 PTZFAA 2007-26-0930.01.2008See AD compliance for detailsHartzell Propeller Inc. models ( )HC-( )( )Y( )-( )( )( ) compact series constant speed or feathering propellers with Hartzell manufactured ''Y'' shank aluminum blades; These propellers are used on, but not limited to, the following airplanes: Aermacchi S.pA. (formerly Siai-Marchetti), Aero, Commander, Aerostar, Beech, Bellanca , Cessna Embraer, Maule, Mooney Pilatus Britten Norman, or Britten, Piper, Pitts, Rockwell; see AD for listPrevent failure of the propeller blade from fatigue cracks in the aluminumblade shank radius, which can result in damage to the airplane and loss of airplane controlSee Table 1 – Incorporation by Reference
154-07 PTZANAC 2007-11-04R1   This AD cancels and supersedes the AD No. 2007-11-04 original issue – Amdt 39-1223,dated 21 Dec. 200721.12.2007Within the next 2500 flight hours or 24 months after the effective date of this AD,whichever occurs first; See AD compliance for detailsEmbraer EMB-145 and EMB-135 aircraft models of serial numbers (S/N) 145002 thru 145362, 145364 thru 145590, and 145592 thru 14500987Occurrence of smoke in the flight deck originated from Pitot 1/2 and TAT 1/2 current sensor relays and yours respective sockets, caused by poor electrical contacts betweenthose relays and their socketsEmbraer Service Bulletins Nos. 145-30-0052 original issue or 145LEG-30-0019 original issue
155-07 PTZF-2007-025   This AD replaces the AD F-2004-015 which is cancelled by its Rev. 1Upon receipt from February 04, 2004 (effective date of AD F-2004-015)See AD for detailsAny reserve canopy manufactured by PARACHUTES DE FRANCE (PdF) between January 1st, 1987 andFebruary 28, 1989 with serial numbers from 87 01 001 up to 89 02 xxxEquipment/Furnishings - Temporary grounding of reserve canopiesService Bulletin PARACHUTES DE FRANCE No. 2/2003
156-07 PTZF-2007-026     This AD replaces EASA AD 2006-0160-E which is cancelled byEASAJune 08, 2006 (effective date of AD EASA 2006-0160-E)Before the next use, as from the effective date of thisAD, unless already accomplished; See AD for detailsPARACHUTES DE FRANCE   TECHNO 240 equipmentsTECHNO 240-B, P/N R 01-240-B - All serial numbers - Reserve ParachuteEquipment/Furnishings - Reserve parachute - Mandatory packingmodifications slider and steering lines replacementPARACHUTE DE FRANCE Service Bulletin BSV-06-001