| CAA-2011-06-008 |
2011/06/24 |
FAA |
2011-12-12 |
To The Boeing Company Model MD-90-30 airplanes, certificated in any category, as identified in Boeing Alert Service Bulletin MD90-55A014, dated June 24, 2010.
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| CAA-2011-06-007(已有後續修訂版) |
2011/06/24 |
FAA |
2011-12-10 |
Model R22, R22 Alpha, R22 Beta, and R22 Mariner helicopters, with main rotor blade (blade), part number (P/N) A016-4; and Model R44 and R44 II helicopters, with blade, P/N C016-2 or C016-5, certificated in any category.
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| CAA-2011-06-006(已有後續修訂版) |
2011/06/24 |
FAA |
2011-12-13 |
To The Boeing Company Model 737-600, -700, -700C, -800, -900, and -900ER series airplanes, certificated in any category; as identified in Boeing Service Bulletin 737-27-1289, dated April 7, 2010.
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| CAA-2010-10-004修訂 |
2011/06/12 |
EASA |
2010-0204Correction |
Rockwell Collins Mode S Transponders identified by type and Part Number (P/N) as follows:
Type P/N (all serial numbers)
TDR-94 622-9352-007, 622-9352-207, 622-9352-008, 622-9352-108, 622-9352-308, 622-9352-309, 622-9352-408, 622-9352-409 TDR-94D 622-9210-007, 622-9210-207, 622-9210-008, 622-9210-108, 622-9210-308, 622-9210-309, 622-9210-408, 622-9210-409 when installed in combination with certain Rockwell Collins Air Data Computers (ADC) as specified below, and the Rockwell Collins Commercial Standard Digital Bus (CSDB) databus is being used to transfer altitude information between the ADC and the transponder(s). ADC Type P/N (all suffixes, all serial numbers) ADC-81A 622-4401-XXX
ADC-82A 622-6475-XXX
ADC-82C 622-8329-XXX
ADC-82L 622-8105-XXX
ADC-85 622-8051-XXX
ADC-85A 822-0370-XXX
For fixed-wing aeroplanes to which this AD applies, refer to Rockwell-Collins, Inc. Service Information Letter 08-1 to identify whether an installation is affected. Additionally, Rockwell-Collins, Inc. Service Information Letter 2-85 details the part numbers assigned for aeroplanes certified with the ADS-81/82 Air Data System.
This AD applies only to fixed-wing aeroplanes with the affected transponders installed and operating under Instrument Flight Rules (IFR) in the designated
Enhanced Surveillance (EHS) airspace in Europe.
These transponders, in combination with CDSB altitude information transfer, are known to be installed on, but not limited to:
- Hawker Beechcraft 200 (King Air) series and 1900D aeroplanes,
- Dassault Aviation Mystère-Falcon 20 and Mystère-Falcon 50 eroplanes,
and - SAAB SF340A and 340B aeroplanes. For more information regarding Mode-S EHS, please consult the
EUROCONTROL website and local Aeronautical Information Circulars (AIC).
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| CAA-2011-06-005 |
2011/06/10 |
Transport Canada Civil Aviation |
CF- 2011-12 |
Bombardier Inc. DHC-8 Aeroplanes: Models 102, 103, 106, 201, 202, 301, 311, 314 and 315, Serial Numbers 003 through 672 Models 400, 401 and 402, Serial Numbers 4001 through 4343.
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| CAA-2011-06-004(已有後續修訂版) |
2011/06/03 |
EASA |
2011-0098 |
Airbus A310 and A300-600, all certified models; Airbus A318, models -111, -112, -121 and -122,
Airbus A319, models -111, -112, -113, -114, -115, -131, -132 and -133, Airbus A320, models -111, -211, -212, -214, -215, -216, -231, -232 and -233, Airbus A321, models -111, -112, -131, -211, -212, -213, -231 and -232;
Airbus A330, models -201, -202, -203, -223, -243, -301, -302, -303, -321, -322, -323, -341, -342 and -343; Airbus A340, models -211, -212, -213, -311, -312, -313, -541, -542, -642 and -643;
Boeing 717-200 Series;
Boeing 737-100, -200, -200C, -300, -400, -500, -600, -700, -700C, -800, -900 and -900ER Series;
Boeing 747-100, -100B, -100B SUD, -200B, -200C, -300, -400, -400D,
-400F SR, and SP Series;
Boeing 757 200, -200CB, and -300 Series; Boeing 767-200, -300 and -400ER Series; Boeing 777-200; -200LR, -300, -300ER, and 777F Series; McDonnell Douglas MD-11 and MD-11F; McDonnell Douglas DC-9 Series, MD-88 and MD-90-30;
Fokker F27 Marks 100, 200, 300, 400, 500, 600, 700, 050, 0502, and 0604, if equipped with any passenger seats manufactured by Koito Industries, including all seats modified by third party after the initial delivery, unless a complete certification programme to show that the seats and their installation fully comply with the appropriate certification basis is successfully conducted.
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| CAA-2011-06-003(已有後續修訂版) |
2011/06/03 |
FAA |
2011-12-01 |
To Koito Industries, Ltd., seats and seating systems having a model number identified in table 1 of this AD that are approved under technical standard order (TSO) TSO-C39b, TSO-C39c, or TSO-C127a, and installed on, but not limited to, airplanes of the manufacturers identified in table 2 of this AD, all type certificated models in any category.Table 1–Seat Models
Model Numbers
AFS-105, AFS-136,
AFS-235, AFS-315,
ARS-183, ARS-189, ARS-190,
ARS-200, ARS-242, ARS-242-TA, ARS-254, ARS-255, ARS-263, ARS-276, ARS-277, ARS-281, ARS-289,
ARS-29, ARS-29-03, ARS-304, ARS-308, ARS-311, ARS-311-A, ARS-311-B, ARS-336, ARS-339, ARS-341, ARS-347, ARS-352, ARS-354, ARS-357, ARS-360, ARS-384, ARS-385, ARS-392, ARS-397, ARS-398,
ARS-415, ARS-417, ARS-418, ARS-419, ARS-423, ARS-424, ARS-425, ARS-427, ARS-431, ARS-437, ARS-446, ARS-447, ARS-448, ARS-451, ARS-452, ARS-465, ARS-478, ARS-480, ARS-482, ARS-483, ARS-493, ARS-494, ARS-507, ARS-510, ARS-511, ARS-514, ARS-516, ARS-518, ARS-527, ARS-542, ARS-543, ARS-550, ARS-552, ARS-553, ARS-554, ARS-571, ARS-574, ARS-577, ARS-588, ARS-589, ARS-591, ARS-592, ARS-593, ARS-594, ARS-595, ARS-596, ARS-597, ARS-598, ARS-599,ARS-600, ARS-601, ARS-604, ARS-605, ARS-607, ARS-610, ARS-611, ARS-613, ARS-615, ARS-616, ARS-617, ARS-620, ARS-626, ARS-627, ARS-629, ARS-636, ARS-641, ARS-642, ARS-643, ARS-644, ARS-646, ARS-647, ARS-649, ARS-651, ARS-652, ARS-657, ARS-658, ARS-659, ARS-667, ARS-668, ARS-669, ARS-670, ARS-671, ARS-672, ARS-673, ARS-674, ARS-694, ARS-697,
ARS-704, ARS-707, ARS-709, ARS-710,
ARS-813, ARS-814, ARS-815, ARS-823, ARS-831, ARS-832, ARS-833, ARS-835, ARS-836, ARS-837, ARS-838, ARS-840, ARS-841, ARS-843, ARS-844, ARS-846, ARS-847, ARS-849, ARS-851, ARS-852, ARS-853, ARS-857, ARS-858, ARS-859, ARS-861, ARS-862, ARS-869, ASS-197D,
ASS-215, ASS-30, ASS-30-1, B-317,
F11M11, F44A33, P11B31, P11B33, P11M93, P21B33, P21B35, P21B73,
P22A23, P32B73, P52B41, P56B63,
PB7-2001, T-316,Y11B31, Y11B33, Y11B73, Y15B73, Y21A23, Y21B73,
Y27B73, YE1B35, YG7B35, YH1B73,
YK2B73
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| CAA-2011-06-002 |
2011/06/03 |
FAA |
2011-11-05 |
To all The Boeing Company Model DC-10-10, DC-10-10F, DC-10-15, DC-10-30, DC-10-30F (KC-10A and KDC-10), DC-10-40, DC-10-40F, MD-10-10F, MD-10-30F, MD-11, and MD-11F airplanes, certificated in any category.
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| CAA-2011-06-001 |
2011/06/03 |
EASA |
2011-0105 |
SA 365 N1, AS 365 N2, AS 365 N3, SA 366 G1, EC 155 B and EC 155 B1
helicopters, all serial numbers.
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| CAA-2011-05-011 |
2011/05/31 |
EASA |
2011-0103 |
Tri-Band ELT antennas, Part Number (P/N) 21-41 ( ) series, all serial numbers (s/n) up to 12999 inclusive, which are used in combination with a large variety of ELT units; see also Note below.
Chelton P/N 21-41 ( ) series antennas installed in combination with the following ELT units are not affected by this AD:
Chelton Avionics, Inc DBA Wulsberg Electronics (formerly ARTEX) ELT model C406-N HM, P/N 453-5061,
Chelton Avionics, INC DBA Wulsberg Electronics (formerly ARTEX) ELT model C406-N, P/N 453-5060, and
ELTA ELT model ADT406²AF/AP-H, P/N 01N65901 rev. (x)
The affected antennas are known to be installed on, but not limited to, Eurocopter (formerly Eurocopter France, Aerospatiale) AS 350, EC 155 and AS 332 series helicopters. It is also possible that the antenna is installed on fixed wing aircraft.
Note: For the definition of ELT, refer to the types of ELT in EUROCAE ED-62A paragraph 1.2 or in RTCA DO-204 paragraph 2.1. The definition includes all four basic types: ELT (AF) - Automatic Fixed, ELT (AP) - Automatic Portable, ELT (S) - Survival, and ELT (AD) - Automatic Deployable.
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