| CAA-2011-06-014 |
2011/07/01 |
FAA |
2011-13-03 |
This AD applies to the Lycoming Engines and TCM turbocharged reciprocating engines listed in, but not limited to, Table 1 of this AD, with the following Hartzell Engine Technologies, LLC (HET) turbocharger models TA3601, TAO401, TAO402, TAO411, TAO413, T1879, T18A21, T18A44, THO867, and TEO659, installed:
(1) Newly manufactured turbochargers (otherwise known as the -0000 series) before serial number H-NJL00003, or rebuilt (otherwise known as the -9000 series) before serial number H-NJR00002; and
(2) With less than 50 hours time-in-service (TIS) on the effective date of this AD; and
(3) With a part number listed in Table 2 or Table 3 of this AD; and
(4) With a ''slanted A'' foundry mark located on the center housing and rotating assembly (CHRA).
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| CAA-2011-06-013(已有後續修訂版) |
2011/07/01 |
EASA |
2011-0120 |
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 A321-232 aeroplane models, manufacturer serial numbers: 3339, 3340, 3350, 3355, 3360, 3367, 3369, 3372, 3380, 3382, 3385, 3387, 3388, 3390, 3393, 3395, 3397 to 3508 inclusive, 3510 to 3519 inclusive,
3522, 3523, 3525, 3527, 3529, 3530, 3537, 3539, 3542, 3544, 3546, 3548, 3552 and 3555.
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| CAA-2011-06-012(已有後續修訂版) |
2011/07/01 |
EASA |
2011-0121 |
Airbus A318-111, A318-112, A318-121, A318-122, 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 A321-232 aeroplane models, manufacturer serial numbers: 3359, 3361, 3362, 3365, 3366, 3368, 3370 to 3508 inclusive, 3510 to 3519
inclusive, 3522, 3523, 3525, 3527, 3529, 3530, 3533 to 3534 inclusive, 3537, 3539, 3542, 3544, 3546, 3548, 3552, and 3555.
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| CAA-2011-06-011 |
2011/06/30 |
EASA |
2011-0122-E |
Airbus A330 aeroplanes, models -301, -321, -322, -341 and -342, all
manufacturer serial numbers if equipped with MLG Bogie Beam Part Number (P/N) 201272300 or P/N 201272305.and Airbus A340 aeroplanes, models -211, -212, -213, -311, -312 and -313, all
manufacturer serial numbers if equipped with MLG Bogie Beam P/N
201272300 or P/N 201272305.
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| CAA-2011-06-010 |
2011/06/30 |
EASA |
2011-0117 |
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-2011-06-008 |
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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