Zap. številka | Oznaka | Aplikativnost | Naslov- vsebina | Referenčni dokumenti |
1. | EASA SIN 2008-01 | LINDSTRAND supplied burner hoses manufactured by Flexquip as
identified in LHAB Service Bulletin (SB) No. 11 | LINDSTRAND Hot Air Balloons (LHAB) – Replacement of defective
fuel hoses | United Kingdom CAA Emergency Airworthiness Directive G-2008-0001 |
2. | EASA SIN
2008-02 | The New Piper Aircraft, Inc. (Piper) airplanes (seeTable 1) | Potential failure of hydraulic hose
part number (P/N) 17766-02 (465-138) | FAA Special Airworthiness Information Bulletin (SAIB) CE-08-11, dated 9
January 2008 |
3. | EASA SIN 2008-03 | All gas cylinders supplied by CBL which have a CB-0824-0001 R
EGO
Type Cylinder Liquid Valve fitted which is date stamped between 12/05
and 08/06 | CAMERON BALLOONS LIMITED (CBL) – Fuel Cylinders fitted with a
CB-0824-0001 liquid valve | United Kingdom CAA Emergency Airworthiness Directive G-2008-0002 |
4. | EASA SIN 2008-04 | Pratt & Whitney JT8D Series Engines Rotating Group Components; see
attachment to this SIN for affected Parts | Pratt & Whitney JT8D Series Engines Rotating Group Components –
Notification of Unapproved Parts due to Theft | None |
5. | EASA SIN 2008-05 | Propeller Electronic Controller, Part Number 699018002, Serial numbers
as listed in the attached UK CAA Emergency AD G-2008-0003 | DOWTY PROPELLERS – Propeller Electronic Controller (PEC)
Identification and Removal from Service | United Kingdom Civil Aviation Authority (UK CAA) Emergency
Airworthiness Directive G-2008-0003 and Dowty Propellers Alert Service
Bulletin D8400-61-A77 |
6. | EASA SIN 2008-06 | Individual Honeywell IVA-81A units as identified in the attached SAIB;
these are known to be installed on, but not limited to, transport category
aircraft | Unapproved Parts – Installed in Honeywell IVA-81A TCAS II Vertical
Speed Indicators | FAA Special Airworthiness Information Bulletin (SAIB) NM-08-12 |
7. | EASA SIN 2008-07 | Pratt & Whitney Canada PW305A and PW305B engines, serial numbers
as specified in Transport Canada AD CF-2008-08 | Low Pressure (LP) Compressor Fan Blades - Identification and
Removal from Service | Transport Canada Airworthiness Directive (AD) CF-2008-08; and Pratt &
Whitney Canada Alert Service Bulletin A24588 Revision 2 |
8. | EASA SIN 2008-08 | All aircraft, certificated in any category, fitted with upward-facing (wing- or
fuselage installed) or side-facing (fuselage) fuel filler opening(s) and fuel
filler neck area | Failure of Fuel Filler Cap, resulting in Fuel Contamination | United Kingdom Aircraft Accident Investigation Board (AAIB)
bulletin EW/C2005/10/04 |
9. | EASA SIN 2008-09 | Embraer EMB-135( ) and EMB-145( ) aircraft | Non-compliance with Airworthiness Directive (AD) Requirements | FAA AD 2008-03-03; ANAC (Brazil) AD 2002-01-01 R3; and
Embraer Alert Service Bulletin (ASB) 145-27-A106 |
10. | EASA SIN 2008-10 | All A318, A319, A320 and A321 aircraft | Airbus A318/A319/A320/A321 Standard Operating Procedures –
Ground Spoilers do not Deploy Automatically After Landing | Airbus FCOM Temporary Revision No. 137-1 |
11. | EASA SIN 2008-11 | All Agusta AB412 and AB412EP helicopters having installed (and/or
stored as spare parts) the rescue hoist P/N BL 10300-60 or
P/N 412-8800-01-315 equipped respectively with hook P/N S6150-
61090-1 or P/N 412-8800-05-101 | Rescue Hoist P/N BL-10300-60 and P/N 412-8800-01-315 – Inspection of
Hook P/N S6150-61090-1 and P/N 412-8800-05-101 | ENAC EAD 2008-62
Alert BT Agusta 412-124 |
12. | FAA SAIB NM-08-12 | Honeywell IVA-81A Traffic Alert and Collision Avoidance System (TCAS II) Traffic Advisory/ Vertical Speed Indicators (TCAS/IVSI) | Navigation - Traffic Alert and Collision Avoidance System (TCAS II) | none |
13. | EASA SIN 2008-12 | Bombardier, Inc. Model CL-600-2C10, CL-600-2D15 and CL-600-2D24 aircraft, serial numbers as specified in Transport Canada AD CF-2008-14 | Air Driven Generator Power Centre Contactors - Identification and Removal from Service | Transport Canada Airworthiness Directive (AD) CF-2008-14; and Bombardier Aerospace Service Bulletin 670BA-24-021 Revision A, dated 11 December 2006 |
14. | EASA SIN 2008-14 | See SAIB intoduction for details | Turbochargers and related control components overhauled by Statesville AeroTech Services.
These components might also be included in overhauled turbocharged engines distributed by Triad Aviation, Incorporated. | FAA Special Airworthiness Information Bulletin SAIB NE-07-42R1 |
15. | EASA SIN 2008-15 | See FAA UPN | Improper Maintenance Performed on Aircraft Appliances | FAA Unapproved Parts Notification (UPN) No. 2007-00045 |
16. | EASA SIN 2008-16 | Any aircraft and/or engines, as applicable, which have auxiliary power
units and component parts installed, as identified in the attached FAA UPN. | Auxiliary Power Units (APU’s) and component parts that have been improperly returned to service | FAA Unapproved Parts Notification (UPN) No. S2007-00727004 |
17. | EASA SIN
2008-17 | Any aircraft and/or engines, as applicable, which have engine rotating
group parts and components installed, as identified in the attached FAA UPN | Engine rotating group parts and components that have been improperly maintained and returned to service | FAA Unapproved Parts Notification (UPN) No. 2008- S20071128005 |
18. | EASA SIN 2008-18 | Components that have been released to service on an invalid release document | Validity of Form 1 Approval Certificates issued by JAR 145 organisations located in JAA Member States which are not EU or EFTA Member States | Commission Regulation (EC) No 2042/2003 Annex II (EASA Part-145) |
19. | EASA SIN 2008-20 | Affected aircraft as indicated in the respective FAA SAIB documents
Cirrus Design Corporation;
Piper Aircraft, Inc.; Diamond | Failure of Transient Voltage Suppressors | FAA SAIB CE-08-12, CE-08-13 and CE-08-14; and
Cirrus Design Corporation Service
Advisory (SA) 07-17,
Piper Aircraft, Inc. Service Bulletin 1187, and Garmin Mandatory Service Bulletin No. 0738 Revision B |
20. | Transport Canada AV-2008-02 | Diamond Aircraft (DA) model DA20-C1 powered by the Teledyne Continental Motors (TCM) IO-240-B series engine | Teledyne Continental Motors
IO-240 fuel system contamination | TCM Service Bulletin SB07-9 and Service Information Directive SID07-10
Diamond Aircraft MSB DAC1-73-05 Rev 1
Transport Canada CF-2007-27R1
DA20-C1 Aircraft Flight Manual Rev 23 |
21. | EASA SIN 2008-21 | FOLA Airsafe Life Vests Type A-190 or A-290 | Inspection of the zipper on the life vest valise | Swedish Civil Aviation Authority) Airworthiness
Directive 1-201
FOLA Airsafe Service Bulletin 9-387 rev. A |
22. | EASA SIN 2008-22 | Any aircraft which have accessories and/or wheel and brake assemblies installed, as identified in the attached FAA UPN | Wheel and brake assemblies and aircraft accessories that have been improperly maintained and returned to service | FAA Unapproved Parts Notification (UPN) No. 2007-00139 |
23. | EASA SIN 2008-23 | Any aircraft which have cabin controllers and/or outflow valves installed, as identified in the attached FAA UPN | Cabin Controllers and Outflow Valves that have been improperly maintained and returned to service | FAA Unapproved Parts Notification (UPN) No. 2008-S200708310320 |
24. | EASA SIN 2008-19 | All large aeroplanes equipped with carbon brakes and operated to/from airports where runway icing conditions are possible | Catalytic Oxidation of Aircraft Carbon Brakes due to Runway De-Icing (RDI) Fluids | Aerospace Industry Report 2007 – Society of Automotive Engineers (SAE G-12 Fluids Committee - Catalytic Oxidation Working Group) – Aircraft Carbon Brake Oxidation related to Runway / Pavement De-Icing fluids (RDI) |
25. | EASA SIN 2008-26 | The Nichols Airborne F7-51 series electronic controller. The Nichols Airborne F7-51 controller is asubcomponent of Nichols 1H85 airborne ambient and bleed air flow control systems installed on Beech Super King Air | Nichols Airborne F7-51 series Electronic Controllers that have been improperly maintained and returned to service | FAA Unapproved Parts Notification (UPN) No. 2008-200700130 |
26. | FAA SAIB NM-08-15
EASA SIN 2008-27 | EMBRAER Model EMB-135/145 airplanes | Instruments: Contamination of the Attitude Heading Reference System (AHRS) Computers | Embraer Service Bulletin 145-21-0036 and 145LEG-21-0006 |
27. | FAA SW-08-16 | Robinson Helicopter Company (Robinson) Model R44 II helicopters thru serial number 12167 | Air conditioning wiring | Robinson Service Bulletin SB-65, dated February 22, 2008 See www.robinsonheli.com/servelib.htm |
28. | CASA AWB 32-011 | Diamond DA42 aircraft | Undercarriage
pin circlips part number DIN471-08-2P are subject to fatigue failures which may lead to undercarriage failures | none |
29. | CASA AWB 02-029 | Tecnam P2002JF series aircraft | Possibility of substandard hardware in critical areas, typically, flight controls, powerplant and landing gear | none |
30. | EASA SIN 2008-29 | Aircraft operations during known or expected icing conditions prior to flight and Maint. Org. | Ground De- / Anti-Icing of Aeroplanes; Intake / Fan-blade
Icing and effects of fluid residues on flight controls – replacing EASA SIN No. 2006-09 issued 26 September 2006 | EASA Safety Information Notice No. 2006-09 issued 26 Sept. 2006 |
31. | EASA SIN 2008-30 | Robinson R44 II rotorcraft, all S/N up to and including 12167 | Electrical Short in the Air Conditioning Wiring | FAA Special Airworthiness Information Bulletin (SAIB) SW-08-16 dated 2 April 2008 |
32. | EASA SIN 2008-31 | Honeywell Model IVA-81A TCAS display indicators held as spares
and identified in the attached FAA UPN; and any Transport Category
aircraft which have Honeywell Model IVA-81A TCAS display indicators, as identified in the attached FAA UPN, installed | Honeywell Model IVA-81A TCAS Display Indicators that have been improperly overhauled and returned to service | FAA Unapproved Parts Notification (UPN) No. 2008-200600159 |
33. | CAA New Zealand CAN 32-001 | Tecnam aircraft | Tecnam Main Wheel Inner Tubes | None |
34. | CAA NZ CAN 29-001 | All Piper PA-34 Seneca aircraft fitted with an Oildyne hydraulic power pack | Piper PA-34 Seneca Aircraft Hydraulic Pumps | None |
35. | CAA NZ CAN 27-001 | Cessna and Reims Aviation 172, 180 and 185 series aircraft with S/N listed in Cessna Service Bulletin (SB) SEB01-3 | Cessna 172, 180 and 185 Primary Flight Control Yoke Inspection | Cessna Service Bulletin (SB) No. SEB01-3 |
36. | CAA NZ CAN 28-003 | All Cirrus Design Corporation SR20 and SR22 aircraft | Cirrus SR20 and SR22 Aircraft Fuel System | None |
37. | CAA NZ CAN 28-004 | All aircraft fitted with upward facing or side facing fuel filler openings | Fuel Contamination due to Fuel Filler Cap Failure | EASA SIN No. 2008-08 dated 07 February 2008 and UK Aircraft Accident Investigation Board (AAIB) Bulletin No. EW/C2005/10/04 |
38. | CAA NZ CAN 72-001 | All normally aspirated piston engines with a constant speed propeller | Normally Aspirated Engine Power Checks – Reference RPM | None |
39. | EASA SIB 2008-44 | All Robinson R44 Raven I helicopters, and any piston powered helicopter
using a carburettor incorporating an accelerator pump in the fuel delivery circuit | Malfunctioning of the Carburettor Accelerator Pump in the Fuel System of Piston Engine Powered Helicopters | Australia AWB 73-004 |
40. | EASA SIB 2008-35 Rev 1 | Engine parts held as spares and identified in the attached FAA SAIB | Critical Parts for CFM56 series engines that may have been improperly repaired and approved for return to service | FAA SAIB NE-08-17 R1 |
41. | EASA SIB 2008-47 | Boeing 737-600, 737-700, 737-800 and 737-900 series aircraft | Failure of certain Potable Water Couplers during Freezing Weather Conditions | FAA SAIB NM-08-24 |
42. | Australia AWB 32-014 | all CESSNA C208 Aircraft | Tight Main Landing Gear Attachment Pins in CESSNA C208 Aircraft | none |
43. | Australia AWB 51-006 | all CESSNA aircraft which have Flat Steel Spring Undercarriage Struts | Corrosion and Cracking of Main Landing Gear Assemblies on CESSNA Aircraft | none |
44. | FAA NE-08-18 | Effect of Engine Dampers on Propeller Life | Potential for propeller failure due to high vibratory stress induced by worn or improper engine crankshaft dampers | none |
45. | FAA SAIB NE-08-19 | Propeller Installations on Experimental Aircraft | Potential propeller failures, aircraft
damage, and potential loss of aircraft control for certain untested propellers installed on experimental aircraft | none |
46. | EASA SIB 2008-37 | Propellers (type designs) owned and/or manufactured by the companies identified in the attached FAA SAIB | Possible failures of variable pitch propellers due to inadequate propeller maintenance | FAA SAIB NE-08-20 |
47. | EASA SIB 2008-38 | Propellers (type designs) owned and/or manufactured by the companies identified in the attached FAA SAIB | Potential for propeller failures on piston engine aircraft due to
prolonged operation in a restricted RPM (revolutions per minute) range | FAA SAIB NE-08-21 |
48. | EASA SIB 2008-39 | Propellers (type designs) owned and/or manufactured by the companies identified in the attached FAA SAIB | Procedures for a “propeller search inspection” or “general visual inspection” and performance of “cosmetic repairs” | FAA SAIB NE-08-22 |
49. | FAA SAIB NE-08-26 | Lycoming four, six, and eight cylinder reciprocating engines with a
Teledyne Continental Motors (TCM) (formerly Bendix) Series D2000 and D3000 Dual Magneto
(2 magnetos with a single drive).
These engines can be identified by the letter “D” in the 4th or 5th character in the engine model’s suffix. | Dual Magnetos | Lycoming Service Instruction (SI) 1508B |
50. | EASA SIB 2008-33 | Bell Helicopter Textron, Inc. -Models to include: 204, 205, 206, 209, 212, 222, 412, and possibly other models | Parts produced and sold without an FAA production approval | FAA Unapproved Parts Notification (UPN) No. 2008-200500151 |
51. | FAA SAIB NM-08-27 | Transport Category Airplanes equipped with carbon brakes and operated to/from airports where runway de-icing (RDI) fluids are used | Landing gear: Catalytic Oxidation of Aircraft Carbon Brakes due to Runway De-icing (RDI) Fluids | EASA Safety Information Notice No. 2008-19 |
52. | Australia AWB 62-005 | All Robinson Helicopter Company (RHC) R22 and R44 Model helicopters | Painting R22 and R44 Main Rotor Blades | RHC R22 Service Letter SL-56 and R44 Service Letter SL-32 |
53. | Australia AWB 73-005 | All aircraft fitted with Precision Airmotive/Facet/Marvel-Schebler Float Carburettors | Precision Airmotive Carburettors - Floats | Precision Airmotive Mandatory Service Bulletin (MSB) MSA-13 |
54. | EASA SIB 2008-49 | BR700-710 engine
BR700-710 engines are known to be installed on, but not limited
to, Bombardier Inc. BD-700 ‘Global Express’ and Gulfstream
Aerospace Corporation GV and GV-SP (including the commercial designation G500 and G550 variants) series aircraft | Rolls-Royce Deutschland BR700-710 series engines – Re-use of Potentially Damaged Engine Parts and Components | Rolls-Royce Deutschland Ltd & Co KG Worldwide Communication Ref. WW/20209/1 dated 30 May 2008 |
55. | EASA SIB 2008-24 | Aeroplanes with a Maximum Takeoff Weight of less than 5 670 kg and 9
Passenger Seats or less | Passenger Restraint System on Normal, Utility and Aerobatic Category | UK Air Accident Investigation Branch - Safety Recommendations 2001-40
& 2006-101 |
56. | EASA SIB 2008-55R1 | Piper Model PA-23, PA-31, and PA-42 series aircraft | Forward Baggage Door Locking Mechanism Components –
Inspection / Lubrication / Replacement | FAA Safety Alert for Operators SAFO 08013 dated 29 May 2008
Piper Aircraft Inc. SB 1194 |
57. | FAA SAIB NE-08-36 | BRP Rotax
(Rotax) 912 A, 912 F, 912 S, and 914 F series reciprocating engines | Possible abnormal
camshaft and hydraulic valve tappet wear | EASA published AD 2006-0316R1 |
58. | FAA SAIB NE-08-26R1 | Lycoming four, six, and eight cylinder reciprocating engines with a
Teledyne Continental Motors (TCM) (formerly Bendix) Series D2000 and D3000 Dual Magneto
(2 magnetos with a single drive) | Separation of the
magneto from the engine, which will result in the loss of power | Lycoming Service Instruction No. 1508B |
59. | EASA SIB 2008-50 | Parts held as spares and identified in the FAA UPN; and
any aircraft which have the affected parts, as identified in the
FAA UPN, installed | Aircraft Parts with Fraudulently Produced Documents that
include FAA Airworthiness Tags and traceability documents | FAA Unapproved Parts Notification (UPN) No. 2008-200700111 |
60. | EASA SIB 2008-53 | Rolls-Royce Corporation P/N 23079946 impeller wheels held as
spares or installed on an engine, with serial numbers as identified in the FAA UPN | Rolls-Royce Corporation Engine Impeller Wheels Part Number
(P/N) 23079946 unapproved and declared un-airworthy by the manufacturer due to incomplete manufacturing processes | FAA Unapproved Parts Notification (UPN) No. 2008-S20071123008 |
61. | EASA SIB 2008-54 | All Cessna single-engine aircraft, including those manufactured by
Reims Aviation and for which Cessna is now the Type Certificate
holder, as identified in Cessna Single Engine Service Bulletin
SEB03-3 | Voltage Regulator VR600A with insufficient over-voltage
protection | FAA SAIB CE-04-72R1
Cessna Single Engine Service Bulletin SEB03-3
Cessna Owner Advisory SEB03-3A and
Service Kit SK210-170 instructions |
62. | EASA SIB 2008-57 | All aircraft powered by reciprocating engines | Fuel System Icing – Suspended Water in Fuel | Transport Canada Civil Aviation (TCCA) Service Difficulty Advisory AV-2008-03
Lycoming Service Letter L172C
Teledyne Continental Service Information Letter SIL99-2B |
63. | EASA SIB 2008-58 | All aircraft that have Garmin non-WAAS GNS 400 Series (GPS
400, GNC 420, GNC 420A, GNS 430, GNS 430A) units
installed with main software version 5.03, and all aircraft that
have Garmin non-WAAS GNS 500 Series (GPS 500, GPS 500
TAWS, GNS 530, GNS 530 TAWS, GNS 530A, GNS 530A
TAWS) units installed with Main Software Version 6.03. | Unintended 8.33 kHz / 25 kHz Channel Spacing Switching | Garmin Service Advisory No.:0822 |
