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Airworthiness directives › 2013-19-08

AD 2013-19-08 Airworthiness Directives; The Boeing Company Airplanes

2013-11-06
2013-10-02
39-17590
FAA-2012-1041
Airframe
—

Models named: 727, 727C, -100, -100C, -200, -200F series, 737-100, -200C series, 747-100, -100B. Read the applicability below — it usually turns on serial or part numbers too.

Applicability*9

This AD applies to The Boeing Company series airplanes, certificated in any category, as specified in paragraphs (c)(1), (c)(2), and (c)(3) of this AD. (1) Model 727, 727C, -100, -100C, -200, and -200F series airplanes, identified in Boeing Special Attention Service Bulletin 727-34-0245, dated June 4, 2008. (2) Model 737-100, -200, and -200C series airplanes, identified in Boeing Special Attention Service Bulletin 737-34-2102, dated June 5, 2008. (3) Model 747-100, -100B, -100B SUD, -200B, -200C, -200F, -300, -400, -400D, -400F, 747SR, and 747SP series airplanes, identified in Boeing Special Attention Service Bulletin 747-34-2925, dated June 4, 2008.

Compliance

Comply with this AD within the compliance times specified, unless already done.

Required actions

Within 36 months after the effective date of this AD: Do a general visual inspection of the left and right angle of attack (AOA) sensor as applicable, to determine if a certain AOA sensor with a paddle type vane is installed, in accordance with the Accomplishment Instructions of the applicable service information specified in paragraph (g)(1), (g)(2), or (g)(3) of this AD. (1) Boeing Special Attention Service Bulletin 727-34-0245, dated June 4, 2008 (for Model 727 airplanes). (2) Boeing Special Attention Service Bulletin 737-34-2102, dated June 5, 2008 (for Model 737-100, -200, and -200C series airplanes). (3) Boeing Special Attention Service Bulletin 747-34-2925, dated June 4, 2008 (for Model 747-100, -100B, -100B SUD, -200B, -200C, -200F, -300, -400, -400D, -400F, 747SR, and 747SP series airplanes).

Unsafe condition

This AD was prompted by a report of an erroneous activation of the control column shaker during takeoff. We are issuing this AD to prevent erroneous activation of the control column shaker during takeoff, which could result in runway overrun, failure to clear terrain or obstacles after takeoff, or reduced controllability of the airplane.

Affected ADs

None.

Read the original on the Federal Register →

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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