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Airworthiness directives › 2000-22-02

AD 2000-22-02 Airworthiness Directives; Boeing Model 737 Series Airplanes

2000-11-13
2000-11-16
39-11948
2000-NM-325-AD
Airframe
—

Models named: 737 series. Read the applicability below — it usually turns on serial or part numbers too.

Applicability*9

All Model 737 series airplanes, certificated in any category.

Compliance

Required as indicated, unless accomplished previously. To ensure that the flight crew is advised of the procedures necessary to address a condition involving a jammed or restricted rudder, accomplish the following: Restatement of Certain Requirements of AD 96-26-07 (a) Within 30 days after January 17, 1997 (the effective date of AD 96-26-07, amendment 39-9871): Revise the Emergency Procedures Section of the FAA-approved Airplane Flight Manual (AFM) to include the following recall item, which will enable the flight crew to take appropriate action to maintain control of the airplane during an uncommanded yaw or roll condition. This may be accomplished by inserting a copy of this AD in the AFM. “UNCOMMANDED YAW OR ROLL RECALL Maintain control of the airplane with all available flight controls. If roll is uncontrollable, immediately reduce angle of attack and increase airspeed. Do not attempt to maintain altitude until control is recovered. If engaged, disconnect autopilot and autothrottle.” New Requirements of This AD (b) Within 30 days after the effective date of this AD: Revise the Normal Procedures Section of the FAA-approved AFM for Model 737-100 and -200 series airplanes or the Non-Normal Procedures Section of the FAA-approved AFM for Model 737-300, -400, -500, -600, -700, and -800 series airplanes, as applicable, to include the procedure specified in Figure 1 of this AD. This may be accomplished by inserting a copy of this AD in the AFM and removing the existing copy (inserted as required by AD 96-26-07), entitled “Jammed Flight Controls.” ER16NO00.000 (c) It is acceptable to modify the format of the above procedure to reflect the format used by individual carriers. However, the procedural sequence, memory items, and/or associated text may not be modified, except by submitting a request for an alternative method of compliance (AMOC) as specified in paragraph (d) of this AD. Alternative Methods of Compliance (d) An AMOC or adjustment of the compliance time that provides an acceptable level of safety may be used if approved by the Manager, Seattle Aircraft Certification Office (ACO), FAA. Operators shall submit their requests through an appropriate FAA Principal Operations Inspector, who may add comments and then send it to the Manager, Seattle ACO. Note 1: Information concerning the existence of approved alternative methods of compliance with this AD, if any, may be obtained from the Seattle ACO. Special Flight Permits (e) Special flight permits may be issued in accordance with §§ 21.197 and 21.199 of the Federal Aviation Regulations (14 CFR 21.197 and 21.199) to operate the airplane to a location where the requirements of this AD can be accomplished. Effective Date (f) The effective date of this amendment remains November 13, 2000. Issued in Renton, Washington, on November 9, 2000. Donald L. Riggin, Acting Manager, Transport Airplane Directorate, Aircraft Certification Service. [FR Doc. 00-29403 Filed 11-15-00; 8:45 am] BILLING CODE 4910-13-U

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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