Airworthiness directives › 2013-05-07
AD 2013-05-07 Airworthiness Directives; The Boeing Company Airplanes
Models named: 767-200, -300, -300F, -400ER series. Read the applicability below — it usually turns on serial or part numbers too.
Applicability*9
This AD applies to The Boeing Company Model 767-200, -300, -300F, and -400ER series airplanes, certificated in any category; as identified in the service information specified in paragraphs (c)(1), (c)(2), (c)(3), (c)(4), (c)(5), and (c)(6) of this AD. (1) Boeing Service Bulletin 767-27A0224, Revision 1, dated December 16, 2011. (2) Boeing Service Bulletin 767-49A0035, Revision 2, dated June 2, 2006. (3) Boeing Service Bulletin 767-27-0204, Revision 2, dated August 16, 2011. (4) Boeing Service Bulletin 767-27-0205, Revision 2, dated August 30, 2011. (5) Boeing Service Bulletins 767-51A0027, Revision 1, dated October 12, 2006. (6) Boeing Service Bulletin 767-51A0028, Revision 1, dated October 12, 2006.
Compliance
Comply with this AD within the compliance times specified, unless already done.
Required actions
For airplanes identified in Boeing Service Bulletin 767-27-0204, Revision 2, dated August 16, 2011; and Boeing Service Bulletin 767-27-0205, Revision 2, dated August 30, 2011: At the applicable time specified in paragraph (g)(1) or (g)(2) of this AD, do a general visual inspection for dirt, loose particles, and blockage of the flanged tube and drain hole for the E1A and E1B elevator control cable aft pressure seals, and all applicable corrective actions, in accordance with the Accomplishment Instructions of Boeing Service Bulletin 767-27-0204, Revision 2, dated August 16, 2011 (for Model 767-200, -300, and -300F series airplanes); or Boeing Service Bulletin 767-27-0205, Revision 2, dated August 30, 2011 (for Model 767-400ER series airplanes). Do all applicable corrective actions before further flight. Repeat the inspection thereafter at intervals not to exceed 24 months. (1) For airplanes on which Boeing Service Bulletin 767-27A0219 has been done as of the effective date of this AD: Within 24 months after the effective date of this AD. (2) For airplanes on which Boeing Service Bulletin 767-27A0219 has not been done as of the effective date of this AD: Do the inspection at the time specified in paragraph (g)(2)(i) or (g)(2)(ii) of this AD, whichever occurs later. (i) Within 24 months after the effective date of this AD. (ii) Within 24 months since the date of issuance of the original airworthiness certificate or the date of issuance of the original export certificate of airworthiness.
Unsafe condition
This AD was prompted by reports of stiff operation of the elevator pitch control system and jammed elevator controls. We are issuing this AD to prevent moisture from collecting and freezing on the elevator control system components, which could limit the ability of the flightcrew to make elevator control inputs and result in reduced controllability of the airplane.
Affected ADs
None.
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The directive text above is reproduced from the Federal Register, a work of the United States government and in the public domain. The separation into applicability, compliance and required actions is TrackAD's.*1