Številka PTZ | Referenčna PTZ | Datum efektive | Rok izvršitve | Proizvajalec | Vsebina PTZ | Referenčni SB |
001-09 PTZ | FAA 2009-01-01 | 31.12.2008 | Within 14 days of the effective date of this AD; See AD compliance for details | CFM International, S. A
CFM56-5B1, -5B2, -5B4, -5B5, -5B6, -5B7, -5B1/P, -5B2/P, -5B3/P, -5B3/P1, -5B4/P, -5B5/P, -5B6/P, -5B7/P, -5B8/P, -5B9/P, -5B1/2P, -5B2/2P, -5B3/2P, -5B3/2P1, -5B4/2P, -5B6/2P, -5B4/P1, -5B4/2P1, and -5B9/2P turbofan engines.
These engines are installed on, but not limited to, Airbus A318, A319, A320, and A321 series airplanes | High-pressure compressor (HPC) stalls during climb out after takeoff | EASA Airworthiness Directive 2008-0227-E
CFM International, S. A. SB No. CFM56-5B S/B 72-0722 |
002-09 PTZ | AGÊNCIA NACIONAL DE AVIAÇÃO CIVIL – BRAZIL
ANAC 2009-01-01 | 08.01.2009 | Within the next 12 months after the effective date of this AD; See AD compliance for details | Embraer EMB-135BJ, EMB-135ER,
EMB-135KE, EMB-135KL, EMB-135LR, EMB-145, EMB-145EP, EMB-145ER, EMB-145EU, EMB-145LR,
EMB-145LU, EMB-145MK, EMB-145MP, EMB-145MR, EMB-145XR and EMB-145LR | Landing Gear Electronic Unit (LGEU) - Replacement | Embraer Service Bulletins No. 145-32-0120 or No. 145LEG-32-0032 |
003-09 PTZ | EASA 2009-0002 | 21.01.2009 | No later than 28 February 2011; See Required Action(s)
And Compliance
Time(s) for Details | TURBOMECA
Arriel 1B, 1D and 1D1 turboshaft engines, all serial numbers.
These engines are known to be installed on, but not limited to, Eurocopter
AS 350 B, AS 350 BA, AS 350 B1 and AS 350 B2 helicopters. | Engine – Reduction Gear Box Intermediate Pinion – Modification | Turboméca, S.A. Mandatory Service Bulletin No. 292 72 0276 Version B |
004-09 PTZ | EASA 2009-0005
This AD supersedes CAA UK AD 006-10-99 | 22.01.2009 | See Required Action(s)
And Compliance
Time(s) for Details | Dowty Aerospace Propellers
R389 and R390 propellers
These propellers are known to be installed on Saab SF340A and 340B aircraft | Propellers – Hub Assembly – Inspection | Dowty Propellers ASB SF340-61-95 Rev 5
Dowty Propellers SB SF340-61-105 original issue or Rev 1 |
005-09 PTZ | CF- 2008-33R1 | 09.02.2009 | See AD Corrective
Actions for Details | Bombardier Inc. CL-600-2B19 Aircraft | Inboard Flap Actuator | See AD |
006-09 PTZ | EASA 2007–0138R1
This AD revises and replaces EASA AD 2007-0138-E | 18.05.2007 | See Required Action(s)
And Compliance
Time(s) for Details | EUROCOPTER
AS 350 and AS 355 helicopters | Tail Rotor - Tail Rotor Blades Skin- Inspection / Repair | See AD Ref. Publications for details |
007-09 PTZ | EASA 2009–0004 | 26.01.2009 | See Required Action(s)
And Compliance
Time(s) for Details | EUROCOPTER
AS 350 and EC 130 helicopters | Engine Starting - Starter-generator Damping Assembly –
Inspection / Adjustment | See AD Ref. Publications for details |
008-09 PTZ | EASA 2009-0009 | 28.01.2009 | See Required Action(s)
And Compliance
Time(s) for Details | CFM International SA
CFM56-7B turbofan engines
These engines are known to be installed on, but not limited to, Boeing 737series aeroplanes | Time Limits – Low Pressure Turbine Rear Frame – Life Limit /
Mandatory Inspection | See AD Ref. Publications for details |
009-09 PTZ | CF-2009-02 | 19.02.2009 | Within 24 months after the effective date of this directive | Bombardier Inc. Model CL-600-2B19 | Overwing Emergency Exit Placards | Bombardier Service Bulletin (SB) 601R-11-088, dated 25 June 2008 |
010-09 PTZ | FAA 2009-02-03 | 09.02.2009 | See AD compliance for details | Lycoming Engines
Teledyne Continental Motors
Superior Air Parts, Inc.
with a Precision Airmotive LLC, RSA-5 or RSA-10 series, or Bendix, RSA-5 or RSA-10 series, fuel injection servo, having a servo plug gasket, P/N 365533, that was installed under the fuel injection servo plug, P/N 383493, on or after August 22, 2006 | Lean running engine | See AD |
011-09 PTZ | FAA 2009-04-03 | 24.03.2009 | See AD compliance for details | Rolls-Royce Corporation (Formerly Allison Engine Company, Inc.) AE 3007A1E and AE 1107C turbofan/turboshaft engines | Low-cycle-fatigue failure of the parts | See AD Related Information |
012-09 PTZ | FAA 2009-04-05 | 27.03.2009 | See AD compliance for details | Cessna Aircraft Company
Models 182Q and 182R airplanes that are equipped with Societé de Motorisations Aéronautiques (SMA) aircraft diesel engine | Improper intercooler hose assembly installation | See AD |
013-09 PTZ | FAA 2009-04-10 | 30.03.2009 | See AD compliance for details | General Electric Company CF6-80A, CF6-80C2, and CF6-80E1 series
turbofan engines. These engines are installed on, but not limited to, Airbus A300, A310, and A330
series, Boeing 747 and 767 series, and McDonnell Douglas MD-11 series airplanes | Critical life-limited rotating engine part failure | See AD |
014-09 PTZ | EASA 2009-0011 | 11.02.2009 | See Required Action(s)
And Compliance
Time(s) for Details | EUROCOPTER (formerly EUROCOPTER FRANCE, AEROSPATIALE) AS 350B, BA, BB, B1, B2, B3 and EC 130B4 helicopters, all serial numbers | Time Limits/Maintenance Checks – Airworthiness Limitation -
Revision | See AD Ref. Publications for details |
015-09 PTZ | EASA 2009-0019 | 17.02.2009 | See Required Action(s)
And Compliance
Time(s) for Details | EUROCOPTER
AS350 helicopters | Rotors Flight Control - Collective Pitch Lever Locking Stud –
Inspection / Repair | See AD Ref. Publications for details |
016-09 PTZ | EASA 2009-0039 | 05.03.2009 | See Required Action(s)
And Compliance
Time(s) for Details | EUROCOPTER
AS 350 and AS 355 helicopters | Tail Rotor - Tail Rotor Blades Skin - Inspection / Repair | See AD Ref. Publications for details |
017-09 PTZ | EASA 2009-0022-E | 09.02.2009 | Within the next 5 flight hours after the effective date of this directive but no
later than 15 February 2009, whichever occurs first;
See Required Action(s)
And Compliance
Time(s) for Details | Agusta S.p.A.
AB206 helicopters | Engine – Power Turbine Speed – Operational Limitation | Agusta Alert Bollettino Tecnico 206-244 dated 05 February 2009 |
018-09 PTZ | EASA 2009-0025 | 24.02.2009 | See Required Action(s)
And Compliance
Time(s) for Details | AIRBUS A318, A319, A320 and A321 aircraft | Wings – Flap Track No.1 Pendulum Assembly – Inspection /
Replacement | AIRBUS SB A320-57-1144 or SB A320-57-1144
AIRBUS SB A320-57A1146 |
019-09 PTZ | EASA 2009-0030 | 26.02.2009 | See Required Action(s)
And Compliance
Time(s) for Details | EUROCOPTER
AS 350 helicopters | Stabilizers – Upper and Lower Fin Attachment Fitting -
Inspection / Modification / Replacement | See AD Ref. Publications for details |
020-09 PTZ | EASA 2008-0134R1 | 31.06.2008 | See Required Action(s)
And Compliance
Time(s) for Details | TURBOMÉCA
ARRIUS 2F turbo-shaft engine
These engines are known to be installed on, but not limited to,
Eurocopter EC120B helicopters | Engine Fuel & Control - P3 Air Pipe -Inspection/Modification | Turboméca Service Bulletin N° 319 75 4810 original issue |
021-09 PTZ | EASA 2009-0027 | 04.03.2009 | See Required Action(s)
And Compliance
Time(s) for Details | EUROCOPTER
AS 350 and EC 130 helicopters | Engine Starting – Starter-Generator Damping Assembly – Adjustment | EUROCOPTER AS350 ASB No. 80.00.07 Rev 1
EUROCOPTER EC130 ASB No. 80A003 |
022-09 PTZ | EASA 2006–0140R3 | 25.05.2006 | See Required Action(s)
And Compliance
Time(s) for Details | Lufthansa Technik AG;
SR Technics;
Jet Aviation Basel, AG;
CTT Systems AB
CTT Systems AB Zonal Drying System, P/N´s as listed in the Applicability of this directive | Air Conditioning - Zonal Drying System Deactivation | See AD Ref. Publications for details |
023-09 PTZ | EASA 2009-0036 | 06.03.2009 | See Required Action(s)
And Compliance
Time(s) for Details | CFM International SA (CFM)
CFM56-3 turbofan engines | Engine – Fan Blades with 25 Degree Mid-span Shrouds –
Inspections | CFM service bulletin CFM56-3/3B/3C S/B 72-1067, original issue |
024-09 PTZ | ANAC 2009-02-01 | 12.02.2009 | Within the next 2500 flight hours or 24 months after the effective date of this AD,
whichever occurs first; See AD compliance for details | Embraer model EMB-135BJ, EMB-135ER, EMB-135KE, EMB-135KL, EMB-135LR, EMB-145, EMB-145EP, EMB-145ER, EMB-145EU, EMB-145LR, EMB-145LU, EMB-145MK, EMB-145MP, EMB-145MR and EMB-145XR airplanes | Main landing gear (MLG) trailing arm pins - Inspection/Replacement; MLG auxiliary door mounting support - Modification | Embraer Service Bulletin Nos. 145-32-0122 and 145-52-0047, or
145LEG-32-0033 and 145LEG-52-0014 |
025-09 PTZ | FAA 2009-05-02 | 31.03.2009 | See AD compliance for details | General Electric Company
CF6-80C2 and CF6-80E1 turbofan engine | Fuel leaks | See AD |
026-09 PTZ | FAA 2009-04-15 | 02.04.2009 | See AD compliance for details | Boeing Model 737-100, -200, -200C, -300, -400, and -500 series airplanes | Multiple adjacent cracked stringer tie clips and damaged skin and frames | Boeing Special Attention Service Bulletin 737-53-1268 |
027-09 PTZ | FAA 2009-04-17 | 02.04.2009 | See AD compliance for details | General Electric Company (GE) CF6-45A, CF6-45A2, CF6-50A, CF6-50C, CF6-50CA, CF6-50C1, CF6-50C2, CF6-50C2B, CF6-50C2D, CF6-50E, CF6-50E1, CF6-50E2, and CF6-50E2B series turbofan engines
These engines are installed on, but not limited to, Airbus A300 series, Boeing 747 series, McDonnell Douglas DC-10 series, and DC-10-30F airplanes | Separation of LFCEN assembly forward and aft centerbodies
due to high imbalance engine conditions | Accomplishment Instructions, Section 3, of GE SB No. CF6-50 S/B 78-0244, Rev 1,
CF6-50 S/B 78-0244, or
CF6-50 S/B 78-0242 |
028-09 PTZ | FAA 2009-05-05 | 03.04.2009 | Prior to further
flight after
April 3, 2009
(the effective
date of this
AD); See AD compliance for more details | Avidyne Corporation (Avidyne) Primary Flight Displays (PFDs), part
numbers (P/Ns) 700-00006-000, 700-00006-001, 700-00006-002, 700-00006-003, and 700-00006-100
PFDs that are installed on, but
not limited to the airplanes below that are certificated in any category: Adam Aircraft, Cessna Aircraft Company, Cirrus Design Corporation, Diamond Aircraft Industries, Hawker Beechcraft Corporation, Piper Aircraft, Inc. | Avidyne PFDs (Primary Flight Displays ) displaying incorrect altitude and
airspeed information | Avidyne Service Bulletin No. 601-00006-096, Rev 1 |
029-09 PTZ | EASA 2009-0045 | 13.03.2009 | See Required Action(s)
And Compliance
Time(s) for Details | AIRBUS
A310 and A300-600 aeroplanes | Equipment / Furnishings – IPECO Pilot and Co-pilot Seats –
Inspection / Modification / Replacement | ASB A310-25A2199
ASB A300-25A6210
SB A310-25-2202
SB A300-25-6214
Airbus Operator Engineering Bulletin N°160-1 and N°121-1 |
030-09 PTZ | EASA 2009-0055 | 27.03.2009 | See Required Action(s)
And Compliance
Time(s) for Details | AIRBUS SAS
A310, A300-600 and A300-600ST aeroplanes | Electrical Power – Engine Feeder Harness – Inspection
&
Nacelles/Pylons – GE CF6-80C2 Pylon Forward Pyramid –
Inspection | See AD Ref. Publications for details |
031-09 PTZ | EASA 2009-0059 | 25.03.2009 | See Required Action(s)
And Compliance
Time(s) for Details | Avia Propeller Ltd
Model V410, V500A, V503, V503A, V503AP, V503P, V506 and V520 propellers which have been manufactured before 6 Nov. 2002
These propellers are known to be installed on, but not limited to, the following aircraft: Zlin Z-42M, Z-42MU, Z-142, Z-43, Z-50M, Let Kunovice Ae 45, Ae-145, Z-37, Z-37A, L-200A, L-200D, Orličan L-40 | Propeller - Repetitive Inspections of the Propeller Blades | Avia Propeller Service Bulletins No.1 issue G and No.6 issue D and issue E |
032-09 PTZ | EASA 2009-0065 | 27.03.2009 | See Required Action(s)
And Compliance
Time(s) for Details | Eurocopter Deutschland GmbH
EC 135 and EC 635 helicopters | Fuselage – Rear Structure / Tail Boom – Pre-Flight Check /
Inspection | Eurocopter Deutschland ASB EC135-53A-022 Rev 1 |
033-09 PTZ | FAA 2009-02-06 | 15.04.2009 | See AD compliance for details | Boeing Model 737-300, -400, and -500 series airplanes, certificated in any category | Cracking in the fuselage frames and frame
reinforcements | Boeing Alert Service Bulletin 737-53A1279 |
034-09 PTZ | CF-2009-08 | 09.04.2009 | See AD compliance for details | Bombardier Inc. Models:
CL-600-2C10, CL-600-2D15 and CL-600-2D24 | Pressurization System: Cabin Pressure Control (CPC) Units and Cabin Pressure Control Panel (CPCP) Deficiency | Bombardier Alert Service Bulletin (ASB) A670BA-21-022, dated 3 August 2006 |
035-09 PTZ | CF-2009-09 | 30.03.2009 | See AD Corrective
Actions for Details | Bombardier Inc. Model
CL-600-2C10 aircraft, and CL-600-2D15/CL-600-2D24 aircraft | Fuel System Safety - Hydraulic System Overheat Inside the Fuel Tank | Bombardier Service Bulletin (SB) 670BA-29-005, dated 29 January 2009 |
036-09 PTZ | CF-2009-10 EMERGENCY AD | 12.03.2009 | See AD Corrective
Actions for Details | Bell Helicopter Textron Canada (BHTC) Models:
206A all S/N; 206B series all S/N including those converted from Model 206A; 206L series, all S/N;
407 and 427 all S/N | Cyclic Control Lever Assembly Installation | Alert Service Bulletin´s:
206-09-121
206L-09-155
407-09-85
427-09-23 |
037-09 PTZ | FAA 2009-05-08 | 20.04.2009 | See AD compliance for details | Trimble or FreeFlight Systems 2101 I/O Approach Plus global positioning
system (GPS) navigation system (2101 I/O Approach Plus system) | Erroneous information provided by
the 2101 I/O Approach Plus system | None |
038-09 PTZ | EASA 2007- 0071R1
This directive revises AD 2007-0071 | 30.03.2007 | See Required Action(s)
And Compliance
Time(s) for Details | APEX AIRCRAFT
DR 400 series aeroplanes | Wings - Main spar and fabric covering -
Reinforcement / Modification / Inspection | APEX AIRCRAFT Technical Instruction No 1001047 issue H
APEX AIRCRAFT Technical Instructions No.1000851 issue D and No.1001846
issue F |
039-09 PTZ | EASA Emergency AD 2006-0067-E | 21.03.2009 | Within 5 flight hours after the effective date of this directive and no
later than 27 March 2009, whichever occurs first; See Required Action(s)
And Compliance
Time(s) for Details | Agusta S.p.A.
AB206 helicopters | Main Rotor – Pitch Horn Trunnion Bearing – Inspection /Replacement | Agusta Alert Bollettino Tecnico 206-245 dated 20 March 2009 |
040-09 PTZ | EASA 2006–0334R1 | 14.11.2006 | See Required Action(s)
And Compliance
Time(s) for Details | THALES COMMUNICATIONS
VHF Data Radio, Part Numbers
EVR716-11-0300A
EVR716-11-0350A
EVR716-01-0100A
EVR716-01-0200A
EVR750-03-0100A
known to be installed on, but not limited to, the following aircraft:
- Bombardier DHC-8-400 (all models);
- Airbus A318, A319, A320, A321, A330, A340 (all models);
- Boeing 717, 727, 737, 747, 757, 767, 777 (all models) | Communications - Thales Communications VHF Data Radio -
Modification | Thales Communications Service Bulletins:
EVR716-23-015
EVR716-23-012 Initial Issue or Rev. 01
EVR7-23-05 Initial Issue or Rev. 01 |
041-09 PTZ | EASA Emergency AD 2009-0068-E | 27.03.2009 | See Required Action(s)
And Compliance
Time(s) for Details | TURBOMECA
ARRIEL 1 and ARRIEL 2 series turboshaft engines | Engine - Module M04 (Power Turbine) Power Turbine Blades -
Life Limit / Replacement | Turboméca Mandatory Service Bulletin (MSB) A292 72 0827 - version A
and
MSB A292 72 2833 - version A |
042-09 PTZ | FAA 2009-07-03 | 30.04.2009 | See AD compliance for details | General Electric Company (GE) CF6-80C2 and CF6-80E1 series turbofan
engines | Cracked HPCR spool shaft stage 14 disk webs | CF6-80C2 S/B 72-A1122
CF6-80E1 S/B 72-A0258 |
043-09 PTZ | FAA 2009-07-08 | 05.05.2009 | See AD compliance for details | Piper Aircraft, Inc.
PA-46-350P and PA-46R-350T | Incorrectly installed current limiters | Piper Aircraft, Inc. Service
Bulletin No. 2000 |
044-09 PTZ | CF-2009-13 | 26.04.2009 | See AD Corrective
Actions for Details | Bombardier Inc Model CL-600-2B19 aircraft | Flap Actuator Pinion Gear – Non Conformance | None |
045-09 PTZ | FAA 2009-07-12 | 07.05.2009 | See AD compliance for details | General Electric Company (GE) CF34-1A, -3A, -3A1, -3A2, -3B, and - 3B1 turbofan engines
These engines are installed on, but not limited to, Bombardier, Inc. Airplane models CL-600-2A12, -2B16, and -2B19 | Inability to restart both engines after
flameout due to excessive friction of the 4-step seal | GE Service Bulletin (SB) No. CF34-AL S/B 72-0238 (CL-600-2B19), and
SB No.CF34-BJ S/B 72-0217 (CL-600-2A12 and CL-600-2B16) |
046-09 PTZ | EASA 2009-0081 | 20.04.2009 | See Required Action(s)
And Compliance
Time(s) for Details | AIRBUS
A300 and A300-600 aeroplanes | Wings – Main Landing Gear (MLG) Rib 5 Attachment Fitting Lower
Flange – Inspection / Repair | A300-57-0235 original issue up to rev 05
A300-57-6088 original issue up to rev 04
A300-57A0246 Rev 03
A300-57A6101 Rev 03 |
047-09 PTZ | CF-2009-18 | 19.05.2009 | Within 26 months after the effective date of this directive | Bombardier Inc. Models
CL-600-1A11
CL-600-2A12
CL-600-2B16 | Air Driven Generator (ADG) Power Feeder Harness - Wire Chafing | Bombardier Service Bulletin (SB) 600-0737 or 601-0591 |
048-09 PTZ | CF- 2009-19 | 19.05.2009 | Within 1600 hours air time or within 18 months after the effective date of this directive, whichever comes first | Bombardier Inc. Model CL-600-2B19 | Nose Landing Gear Selector Valve and Nose Landing Gear Door Selector Valve End Caps – Incorrect Assembly | None |
049-09 PTZ | CF-2009-20 | 25.05.2009 | See AD Corrective
Actions for Details | Bombardier Inc. Models
CL-600-2C10
CL-600-2D15 and
CL-600-2D24 | Main Landing Gear Torque Link Apex Pin Disengagement | Bombardier Aerospace Service Bulletin (SB) 670BA-32-019, Rev A |
050-09 PTZ | CF- 2009-21R1 Supersedes and cancels Airworthiness Directives (AD) CF-2006-16R1
and CF-2009-21 | 26.05.2009 | Within 250 hours air time or within 6 months after the effective date of this directive | Bombardier Inc. Models
CL-600-1A11
CL-600-2A12
CL-600-2B16
CL-600-2B16 | Nose Landing Gear Selector Valve and Nose Gear Door Selector Valve End Caps – Incorrect
Assembly | SB 600-0721
SB 601-0558
SB 601-0558
SB 604-32-021 |
051-09 PTZ | CF-2009-22 | 08.06.2009 | See AD Corrective
Actions for Details | Bombardier Inc. Models
CL-600-2C10
CL-600-2D15 and
CL-600-2D24 | Landing Gear Alternate Extension System (AES) – Valve Clevis Damage | Alert Service Bulletin (ASB) A670BA-32-022, Revision A |
052-09 PTZ | CF-2009-23 | 08.06.2009 | Prior to 15000 hours air time, or within the next 5000 hours air time after the effective date of this AD , whichever comes later | Bombardier Inc. Models
CL-600-2B19
CL-600-2C10
CL-600-2D15 and
CL-600-2D24 | Passenger Door Corrosion | See AD |
053-09 PTZ | CF-2009-24 | 08.06.2009 | See AD Corrective
Actions | Bombardier Inc. Model CL-600-2B16 | Air Driven Generator (ADG) – Strut Cracking | See AD |
054-09 PTZ | FAA 2009-08-01 | 14.05.2009 | See AD compliance for details | Honeywell NZ-2000 navigation computers and Honeywell IC-800 or
IC-800E integrated avionics computers; including but not limited to the airplanes identified in Table 1 of AD (Bombardier, Dassault, Gulfstream, Lockheed, Hawker Beechcraft) | Shift in the FMS computed position | See AD |
055-09 PTZ | FAA 2009-09-06 | 11.06.2009 | See AD compliance for details | Boeing Model 737-100, -200, -200C, -300, -400, and -500 series airplanes | Fatigue
cracking of the backup intercostals and upper sill web of the forward airstair doorway | See AD |
056-09 PTZ | FAA 2009-09-07 | 11.06.2009 | See AD compliance for details | Boeing Model 737-100, -200, -200C, -300, -400, and -500 series
airplanes | Broken retract actuator beams of the MLG | See AD |
057-09 PTZ | FAA 2009-08-51 Emergency AD | 27.05.2009 | See AD compliance for details | Rolls-Royce Corporation (RRC) (Formerly Allison Engine Company) | Uncontained failure of the HPT stage 2 wheel | See AD |
058-09 PTZ | FAA 2009-10-09 | 17.06.2009 | See AD compliance for details | Cessna Aircraft Company
See AD Applicability for models | Rudder traveling past the normal travel limit | See AD |
059-09 PTZ | FAA 2009-10-01 | 09.06.2009 | See AD compliance for details | Pratt & Whitney (PW) JT9D-7R4G2, -7R4E1, -7R4E4, and -7R4H1 series turbofan engines. These engines are installed on, but not limited to, Boeing 747-200, -300, 767-200, and Airbus A300-600 and A310-300 series airplanes | Uncontained
failure of the 2nd stage high-pressure turbine (HPT) air seal assembly | See AD |
060-09 PTZ | FAA 2009-11-02 | 23.06.2009 | See AD compliance for details | CFM International S.A. CFM56-2, CFM56-3, CFM56-5A, CFM56-5B,CFM56-5C, and CFM56-7B series turbofan engines.
These engines are installed on, but not limited to, Airbus A319, A320, and A340 airplanes and Boeing 737 airplanes | Cracking of
the HPC 4-9 spool | See AD |
061-09 PTZ | FAA 2009-10-14 | 04.06.2009 | See AD compliance for details | Hartzell Propeller Inc. steel hub turbine propellers listed in Table 1 of AD.
These propellers are installed on, but not limited to, the airplanes listed in Table 1 of AD | Separation of the propeller blade counterweight slug | See AD |
062-09 PTZ | FAA 2009-07-11 | 14.05.2009 | See AD compliance for details | Boeing Model 737-300, -400, and -500 series airplanes | Discrepancies of the fuselage skin | See AD |
063-09 PTZ | FAA 2009-12-05 | 16.06.2009 | See AD compliance for details | Boeing Model 737-300, -400, and -500 series airplanes | Loss of all attitude indications from both the standby indicator and EFIS displays | See AD |
064-09 PTZ | FAA 2009-12-06 | 16.06.2009 | See AD compliance for details | Boeing Model 737-300, -400, and -500 series airplanes
Model 737-600, -700, -700C, -800, and -900 series airplanes | Electrical power to IFE systems and other nonessential
electrical systems through a switch in the flight compartment | See AD |
065-09 PTZ | FAA 2009-13-06 | 24.06.2009 | See AD compliance for details | Piper Aircraft, Inc. PA-23, PA-31, and PA-42 Series Airplanes | Damaged, worn, corroded, or non-conforming nose
baggage door components | See AD |
066-09 PTZ | FAA 2009-14-04 | 12.08.2009 | See AD compliance for details | Boeing Model 737-100, -200, -200C, -300, -400, and -500 series airplanes | Hot short between the outboard landing light and fuel shutoff valve circuits | See AD |
067-09 PTZ | EASA 2009-0084 | 23.04.2009 | See AD compliance for details | AIRBUS SAS
A310, A300-600 and A300-600ST aeroplanes | Equipment / Furnishings – Pilot and Co-pilot Seats – Deactivation
of Powered Movement | See AD |
068-09 PTZ | EASA 2008-0146R1
This AD revises and replaces EASA AD 2008-0146 | 15.08.2009 | See AD compliance for details | Saab AB, Saab Aerosystems
SF340A and 340B aeroplanes | Hydraulic System – Hydraulic Accumulators – Replacement | See AD |
069-09 PTZ | EASA 2009-0093-E | 21.04.2009 | See Required Action(s)
And Compliance
Time(s) for Details | Eurocopter Deutschland GmbH
EC135 and EC635 series helicopters, and
MBB-BK 117 C-2 helicopters | Optional Equipment – External Mounted Hoist System – Visual
Check / Replacement | See AD |
070-09 PTZ | EASA 2006–0140R4 | 25.05.2006 | See Required Action(s)
And Compliance
Time(s) for Details | Lufthansa Technik AG;
SR Technics;
Jet Aviation Basel, AG;
CTT Systems AB
CTT Systems AB Zonal Drying System,
Part Numbers (P/N) as listed in the Applicability of this directive | Air Conditioning - Zonal Drying System Deactivation | See AD |
071-09 PTZ | EASA 2009-0097 | 06.05.2009 | See Required Action(s)
And Compliance
Time(s) for Details | Rockwell Collins Inc.
TDR-94 and TDR-94D transponders | Navigation – Mode S Transponder – Check / Modification | See AD |
072-09 PTZ | EASA 2009-0088R1 | 08.05.2009 | See Required Action(s)
And Compliance
Time(s) for Details | CFM International SA (CFM)
CFM56-5B turbofan engines | Engine – High Pressure Compressor (HPC) – Inspection /
Replacement | See AD |
073-09 PTZ | EASA 2009-0055R1 | 27.03.2009 | See Required Action(s)
And Compliance
Time(s) for Details | AIRBUS SAS
A310, A300-600 and A300-600ST aeroplanes | Electrical Power – Engine Feeder Harness – Inspection
&
Nacelles/Pylons – GE CF6-80C2 Pylon Forward Pyramid –
Inspection | See AD |
074-09 PTZ | EASA 2009-0106-E | 02.05.2009 | See Required Action(s)
And Compliance
Time(s) for Details | Eurocopter Deutschland GmbH
EC135 and EC635 helicopters | Main Rotor Drive – Main Gearbox (MGB) Oil Sampling &
Analysis Program – Amendment | See AD |
075-09 PTZ | EASA 2007-0241R3 | 07.09.2007 | See Required Action(s)
And Compliance
Time(s) for Details | Pilatus Aircraft Ltd.
PC-6 series aeroplanes | Wing – Wing Strut Fitting – Inspection / Replacement | See AD |
076-09 PTZ | EASA 2009-0110 | 21.05.2009 | See Required Action(s)
And Compliance
Time(s) for Details | CFM International SA
CFM56-5B turbofan engines | Time Limits – Low Pressure Turbine Rear Frame – Life Limit /
Mandatory Inspection | See AD |
077-09 PTZ | EASA 2009-0111 | 27.05.2009 | See Required Action(s)
And Compliance
Time(s) for Details | AIRBUS
A300 aeroplanes | Flight Controls – Trimmable Horizontal Stabilizer Actuator (THSA) –
Check / Replacement | See AD |
078-09 PTZ | EASA 2009-0094 | 05.05.2009 | See Required Action(s)
And Compliance
Time(s) for Details | AIRBUS
A300 and A300-600 aeroplanes | Fuselage / Wings – Frame 40 Forward Fitting between Stringers 32
and 33 – Inspection / Repair | See AD |
079-09 PTZ | EASA 2009-0137 | 07.07.2009 | See Required Action(s)
And Compliance
Time(s) for Details | Agusta S.p.A.
A109E helicopters | Electrical Power – Battery Bus (BATT BUS) Circuit Breaker –
Modification | See AD |
080-09 PTZ | EASA 2009-0122 | 24.06.2009 | See Required Action(s)
And Compliance
Time(s) for Details | EUROCOPTER
EC 120, AS 350, EC 130, AS 355, AS 365, EC 155, SA 330, AS 332 and EC 225 Helicopters | Equipment / Furnishings –Load Release Units – Inspection /
Modification / Limitation | See AD |
081-09 PTZ | EASA 2009-0136 | 07.07.2009 | See Required Action(s)
And Compliance
Time(s) for Details | Turboméca
ASTAZOU XIV turboshaft engines | Engine Rotating Assembly – Third Stage Turbine Wheel –
Inspection / Removal | See AD |
082-09 PTZ | EASA 2009-0141 | 16.07.2009 | See Required Action(s)
And Compliance
Time(s) for Details | AIRBUS
A318, A319, A320 and A321 aeroplanes | Stabilizers – Rudder Side Shell Skin – Inspection | See AD |
083-09 PTZ | EASA 2009-0148-E | 11.07.2009 | See Required Action(s)
And Compliance
Time(s) for Details | Agusta S.p.A,
Eurocopter,
Eurocopter Deutschland GmbH,
Sikorsky Aircraft Corporation
A109 series and AB139/ AW139,
AS332, AS350 and AS355 series, EC225, SA330, SA365, AS365 and EC155 series, SA360, EC135, MBB-BK 117, BO 105 series,
S-61 helicopters | Equipment / Furnishings – D-Lok Hook of the Rescue Hoist –
Inspection / Removal from Service / Replacement | See AD |
084-09 PTZ | EASA 2009-0151 | 24.07.2009 | See Required Action(s)
And Compliance
Time(s) for Details | Thielert Aircraft Engines GmbH
TAE125-02-99 engines | Engine/Propeller – Constant Speed Unit – Propeller Control
Valve – Vibration Isolator | See AD |
085-09 PTZ | EASA 2009-0154-E | 17.07.2009 | See Required Action(s)
And Compliance
Time(s) for Details | CFM International SA
CFM56-5B turbofan engines | Engine Fuel and Control - Hydromechanical Unit (HMU) –
Inspection/Replacement | See AD |
086-09 PTZ | EASA 2009-0157 | 31.07.2009 | See Required Action(s)
And Compliance
Time(s) for Details | AIRBUS
A300 aeroplanes | Electrical Power – Fuel Pump Wiring – Modification [Prevention
against Fuel Tank Explosion Risks] | See AD |
087-09 PTZ | EASA 2009-0155 | 31.07.2009 | See Required Action(s)
And Compliance
Time(s) for Details | AIRBUS SAS
A300, A310 and A300-600 aeroplanes | Time Limits / Maintenance Checks – Damage Tolerant
Airworthiness Limitation Items – ALS Part 2 – Amendment | See AD |
088-09 PTZ | EASA 2009-0157 | 31.07.2009 | See Required Action(s)
And Compliance
Time(s) for Details | AIRBUS
A300 aeroplanes | Electrical Power – Fuel Pump Wiring – Modification [Prevention
against Fuel Tank Explosion Risks] | See AD |
089-09 PTZ | EASA 2009-0160 | 28.07.2009 | See Required Action(s)
And Compliance
Time(s) for Details | Extra Flugzeugproduktions- und Vertriebs- GmbH
EA 300 aeroplanes | Fuselage Structure – Tail Spring Support –
Inspection / Modification | See AD |
090-09 PTZ | EASA 2008-0145R1 | 15.08.2008 | See Required Action(s)
And Compliance
Time(s) for Details | Thielert Aircraft Engines GmbH
TAE125 engines | Propellers – Propeller Control Valve – Replacement (Life Limit) | See AD |
091-09 PTZ | EASA Emergency AD 2009-0163-E | 31.07.2009 | See Required Action(s)
And Compliance
Time(s) for Details | DG Flugzeugbau GmbH
DG-100 series sailplanes | Flight Controls - Elevator Control Bearing Stand –
Inspection / Modification | See AD |
092-09 PTZ | EASA Emergency AD 2009-0167-E | 03.08.2009 | See Required Action(s)
And Compliance
Time(s) for Details | DG Flugzeugbau GmbH
DG-100 series and DG-200 series sailplanes | Flight Controls - Control Column Rod End - Inspection / Replacement | See AD |
093-09 PTZ | EASA Emergency AD 2009-0169-E | 03.08.2009 | See Required Action(s)
And Compliance
Time(s) for Details | DG Flugzeugbau GmbH
DG-500 MB and DG-800 B Powered Sailplanes | Starting - Zinc Coated Starter Ring Gears -
Inspections / Replacement | See AD |
094-09 PTZ | EASA 2009-0143 | 11.08.2009 | See Required Action(s)
And Compliance
Time(s) for Details | AIRBUS SAS
A300-600 aeroplanes | Fuel System – Fuel Tank Electrical Bonding – Inspection /
Modification [Fuel Tank Safety] | See AD |
095-09 PTZ | EASA 2009-0165 | 14.08.2009 | See Required Action(s)
And Compliance
Time(s) for Details | AIRBUS SAS
A300, A310 and A300-600 aeroplanes | Fuselage – Frame (FR) 15A Nose Landing Gear (NLG) Crossbeam –
Inspection/Repair | See AD |
096-09 PTZ | EASA 2009-0166 | 14.08.2009 | See Required Action(s)
And Compliance
Time(s) for Details | AIRBUS
A310 and A300-600 aeroplanes | Stabilizers – Rudder Side Shell Skin – Inspection | See AD |
097-09 PTZ | EASA 2009-0173 | 19.08.2009 | See Required Action(s)
And Compliance
Time(s) for Details | Rockwell Collins Inc.
TDR-94 and TDR-94D transponders | Navigation – Mode S Transponder – Modification / Replacement | See AD |
098-09 PTZ | CF-2009-27 | 29.07.2009 | See AD Corrective
Actions | Bombardier Inc. Models
CL-600-2B19
CL-600-2C10
CL-600-2D15
CL-600-2D24 | Air Driven Generator (ADG) – Strut Cracking | See AD |
099-09 PTZ | CF-2009-28 | 20.07.2009 | Within 6000 hours air time after the effective date of this directive | Bombardier Inc. Models
CL-600-2C10
CL-600-2D15
CL-600-2D24 | Elevator Oscillation Due To Elevator Control Rod Disconnect | See AD Corrective
Actions |
100-09 PTZ | CF-2009-30 | 27.07.2009 | Within 5 000 hours air-time after the effective date of this directive | Bombardier Inc. Models
CL-600-2C10
CL-600-2D15
CL-600-2D24 | Aft Baggage Cargo Compartment – Blowout Panel Protective Cages Damage | Bombardier Service Bulletin (SB) 670BA-25-071, dated 15 May 2009 |
101-09 PTZ | CF-2009-31 | 29.07.2009 | Within 60 days after the effective date of this directive | Bombardier Inc. Model CL-600-2B19 | Bulkhead Check Valves – Periodic Discard Task | See AD Corrective
Actions |
102-09 PTZ | CF-2003-05R2
Supersedes AD CF-2003-05R1 issued 7 February 2006 | 29.07.2009 | See AD Corrective
Actions | Bombardier Inc. Model CL-600-2B19 | Air Supply Ducts and Bulkhead Check Valve – Inspections | See AD Corrective
Actions |
103-09 PTZ | CF-2009-32 | 10.08.2009 | Within the next 10 flight hours, but not later than 30 calendar days from the effective day of
this directive | Bell Helicopter Textron Canada (BHTC) Helicopter Models:
206A, 206B, 206L, 206L-1, 206L-3, 206L-4, 222, 222B, 222U, 230, 407, 427, 430 | Bearings in Flight Controls | See AD Corrective
Actions for list |
104-09 PTZ | CF-2009-33 | 18.08.2009 | Within 5000 hours air time or 24 months after the effective date of this directive, whichever comes first, See AD Corrective
Actions | Bombardier Inc. Models
CL-600-2C10
CL-600-2D15
CL-600-2D24 | Thrust Reverser – Transcowl Assembly Cracking | See AD Corrective
Actions |
105-09 PTZ | FAA 2009-16-03 | 09.09.2009 | See AD compliance for details | Teledyne Continental Motors (TCM) IO-520, TSIO-520, and IO-550 series reciprocating engines with SAP investment cast cylinder assemblies, certain part numbers (P/Ns) installed.
These engines are installed on, but not limited to, the airplanes listed in
Table 1 of this AD(Cessna, Rockwell, Beechcraft, Bellanca) | Separation of the cylinder head | Teledyne Continental Service Bulletin No. SB03-3 |
106-09 PTZ | FAA 2009-16-14 | 09.09.2009 | See AD compliance for details | Boeing Model 737-100, -200, -200C, -300, -400, and -500 series airplanes | Fatigue cracking of the intercostals on the forward and aft sides of the forward entry door | Boeing Alert Service Bulletin 737-53A1204, Rev 1 |
107-09 PTZ | EASA 2009-0171 | 19.08.2009 | See Required Action(s)
And Compliance
Time(s) for Details | AIRBUS
A300, A310, A300-600 and
A300-600ST aeroplanes | Fire Protection / Hydraulic Power - Air Pressurisation Check Valves
– Identification / Replacement | AIRBUS Service Bulletins:
A300-29-0124 Rev 02
A310-29-2097 Rev 01
A300-29-6060 Rev 01
A300-29-9009 Rev 02 |
