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2007-03-04 Airbus A330-200 and A330-300 series
2007-03-05 Gulfstream Aerospace LP Model Gulfstream 100 airplanes; and Model Astra SPX and 1125
Westwind Astra
2007-03-07 S 2002-20-07 Boeing 737-100, -200, -200C, -300, -400, -500, -600, -700, -700C, -800
and -900 series
LARGE AIRCRAFT
AD No. Information Manufacturer Applicability
Info: E - Emergency; COR - Correction; S - Supersedes; R - Revision; FR - Final Rule of Emergency
5
Biweekly 2007-04
2007-03-09 Airbus A300 Airplanes; Model A300 B4-601, B4-603, B4-620, B4-622,
B4-605R, B4-622R, F4-605R, F4-622R, and C4-605R Variant F
Airplanes (Collectively Called A300-600 Series Airplanes); and
Model A310 Airplanes
2007-03-10 Airbus A300 airplanes; A300 B4-601, B4-603, B4-620, B4-622, B4-605R,
B4-622R, A300 F4-605R, F4-622R, and C4-605R Variant F
airplanes; and A310
2007-03-11 Bombardier, Inc CL-600-2B19 (Regional Jet Series 100 & 440)
2007-03-13 Rolls-Royce Deutschland Ltd Engine: 528, 529, 532, 535, 542, and 552
2007-03-15 S 2003-02-04 CFM International Engine: CFM56-5 and 5B series
2007-03-18 Airbus A300 and A300-600
2007-03-19 S 2004-14-16 Bombardier, Inc CL-600-2B19 (Regional Jet Series 100 & 440)
2007-04-03 S 2006-04-02 Embraer EMB-135BJ, -135ER, -135KE, -135KL, and -135LR airplanes;
and Model EMB-145, -145ER, -145MR, -145LR, -145XR, -
145MP, and -145EP
2007-04-04 BAE Systems BAE 146-100A, -200A, and -300A series airplanes; and Avro 146-
RJ70A, 146-RJ85A, and 146-RJ100A
2007-04-05 S 2005-13-33 Airbus A300
2007-04-06 McDonnell Douglas DC-8-62 and DC-8-63
2007-04-07 Bombardier, Inc. DHC-8-400
2007-04-09 Embraer EMB-135BJ, -135ER, -135KE, -135KL, and -135LR airplanes;
and Model EMB-145, -145ER, -145MR, -145LR, -145XR, -
145MP, and -145EP
2007-04-10 S 96-24-03 Boeing 747-400
2007-04-15 Sicma Aero Seat Appliance: Passenger seat assemblies
2007-04-16 Boeing 767
2007-04-17 McDonnell Douglas DC-10-10, DC-10-10F, DC-10-15, DC-10-30, and DC-10-30F
(KC-10A and KDC-10), DC-10-40 and DC-10-40F, MD-10-10F
and MD-10-30F
2007-04-18 Learjet 23, 24, 24A, 24B,, 24-B-A, 24 C, 24D, 24D-A, 24E, 24F, 24F-A,
25, 25A, 254B, 25C, 25D, 25F, 28, 29, 31, 31A, 35, 35A (C-21A,
36, 36. 36A, 55, 55B and 55C
6 BW 2007-04
FAA
Aircraft Certification Service
AIRWORTHINESS DIRECTIVE
www.faa.gov/aircraft/safety/alerts/
www.gpoaccess.gov/fr/advanced.html
2007-03-09 Airbus: Amendment 39-14920. Docket 2003-NM-123-AD.
Applicability: All Model A300 airplanes; Model A300 B4-601, B4-603, B4-620, B4-622, B4-
605R, B4-622R, F4-605R, F4-622R, and C4-605R Variant F airplanes; and Model A310 airplanes;
certificated in any category.
Compliance: Required as indicated, unless accomplished previously.
To prevent failure of the ram air turbine (RAT) yoke fitting, which could result in the loss of
RAT function and possible loss of critical flight control in the event of certain emergency situations,
accomplish the following:
Detailed Inspection and Replacement
(a) For Model A300-600 series airplanes, and Model A310 airplanes: Within 1,300 flight hours
or 6 months after the effective date of this AD, whichever occurs first, do a detailed inspection for
breaks of the bottom flange fitting of the yoke fitting for the RAT swivel coupling in accordance with
the applicable all operators telex (AOT) in paragraph (a)(1) or (a)(2) of this AD. If the flange fitting
is broken, before further flight, replace the flange fitting with a new flange fitting in accordance with
the applicable AOT. For airplanes equipped with Hamilton Sundstrand RATs, verify the adjustment
of the ejection jack, and correct the adjustment as applicable.
(1) For Model A300-600 series airplanes: Airbus A300-600 AOT 57A6096, Revision 01, dated
April 11, 2005.
(2) For Model A310 airplanes: Airbus A310 AOT 57A2085, Revision 01, dated April 11, 2005.
Note 1: For the purposes of this AD, a detailed inspection is defined as: “An intensive visual
examination of a specific structural area, system, installation, or assembly to detect damage, failure,
or irregularity. Available lighting is normally supplemented with a direct source of good lighting at
intensity deemed appropriate by the inspector. Inspection aids such as mirror, magnifying lenses, etc.,
may be used. Surface cleaning and elaborate access procedures may be required.”
(b) For Model A300 airplanes, Model A300-600 series airplanes, and Model A310 airplanes
equipped with Dowty Rotol RATs, except airplanes on which Airbus Modification 12986 has been
done: Within 12 months after the effective date of this AD, replace the RAT swivel coupling fork
fitting with a new steel fitting, in accordance with the Accomplishment Instructions of Airbus Service
　
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