AD 97-19-02 Airworthiness Directives; British Aerospace (Jetstream) Model 4101 Airplanes

Models named: Jetstream 4101. Read the applicability below — it usually turns on serial or part numbers too.

All Model Jetstream 4101 airplanes, certificated in any category. Note 1: This AD applies to each airplane identified in the preceding applicability provision, regardless of whether it has been modified, altered, or repaired in the area subject to the requirements of this AD. For airplanes that have been modified, altered, or repaired so that the performance of the requirements of this AD is affected, the owner/operator must request approval for an alternative method of compliance in accordance with paragraph (c) of this AD. The request should include an assessment of the effect of the modification, alteration, or repair on the unsafe condition addressed by this AD; and, if the unsafe condition has not been eliminated, the request should include specific proposed actions to address it.

Required as indicated, unless accomplished previously. To prevent inability of the main entrance door to open, which could delay or impede passengers exiting the airplane, or rescue personnel from entering the airplane during an emergency, accomplish the following: (a) Within 30 days after the effective date of this AD, perform a functional test to verify proper operation of the main entrance door (including the ``G'' lock system) and the ``speed'' lock system of the main entrance door, in accordance with Section 52-10-05 of BAe Jetstream Series 4101 Maintenance Manual (MM). (1) If the ``speed'' lock and the ``G'' lock function satisfactorily: Within 60 days after the effective date of the AD, perform the actions specified in paragraphs (a)(1)(i) and (a)(1)(ii) of this AD. (i) Clean (remove existing contaminents and lubricant) and re- lubricate (with a dry lubricant) the ``speed'' lock and main entrance door ``G'' lock systems in accordance with Jetstream Service Bulletin J41-52-058, dated July 14, 1997. And, (ii) Following accomplishment of paragraph (a)(1)(i) of this AD, and prior to further flight, repeat the functional test specified in paragraph (a) of this AD. (A) If the ``G'' lock and the ``speed'' lock function satisfactorily in the functional test required by paragraph (a)(1)(ii) of this AD, accomplish the requirements of paragraph (b) of this AD. (B) If the ``G'' lock and the ``speed'' lock do not function satisfactorily in the functional test required by paragraph (a)(1)(ii) of this AD: Prior to further flight, repair the ``G'' lock and the ``speed'' lock in accordance with a method approved by the Manager, Standardization Branch, ANM-113, FAA, Transport Airplane Directorate. (2) If either the ``speed'' lock and/or the ``G'' lock do not function correctly: Prior to further flight, perform the actions specified [[Page 47364]] in paragraphs (a)(2)(i) and (a)(2)(ii) of this AD. (i) Clean (remove existing contaminents and lubricant) and re- lubricate (with a dry lubricant) the main entrance door ``speed'' lock and ``G'' lock systems in accordance with Jetstream Service Bulletin J41-52-058, dated July 14, 1997. And, (ii) Following accomplishment of paragraph (a)(2)(i) of this AD, and prior to further flight, repeat the functional test of the main entrance door (including the ``G'' lock system) and the ``speed'' lock system, in accordance with the MM. (A) If the ``G'' lock and speed lock function satisfactorily in the functional test required by paragraph (a)(2) of this AD, accomplish the requirements of paragraph (b) of this AD. (B) If the ``G'' lock and speed lock do not function satisfactorily in the functional tests required by paragraph (a)(2) of this AD: Prior to further flight, repair the ``G'' lock and speed lock in accordance with a method approved by the Manager, Standardization Branch, ANM-113. (b) Perform the actions specified in paragraphs (b)(1) and (b)(2) of this AD within 1,500 hours time-in-service following accomplishment of the initial functional test of the main entrance door required by paragraph (a) of this AD. Repeat the actions specified in paragraphs (b)(1) and (b)(2) of this AD, thereafter, at intervals not to exceed 1,500 hours time-in-service. (1) Clean (remove contaminents and dry lubricant) and re- lubricate (with dry lubricant) the main entrance door ``speed'' lock and ``G'' lock systems in accordance with Jetstream Service Bulletin J41-52-058, dated July 14, 1997. (2) Following accomplishment of paragraph (b)(1) of this AD and prior to further flight, perform a functional test of the main entrance door (including the ``G'' lock system) and the ``speed'' lock system, in accordance with the MM. If the ``G'' lock or ``speed'' lock system do not perform satisfactorily: Prior to further flight, repair the ``G'' lock or ``speed'' lock system in accordance with a method approved by the Manager, Standardization Branch, ANM-113. (c) An alternative method of compliance or adjustment of the compliance time that provides an acceptable level of safety may be used if approved by the Manager, Standardization Branch, ANM-113. Operators shall submit their requests through an appropriate FAA Principal Maintenance Inspector, who may add comments and then send it to the Manager, Standardization Branch, ANM-113. Note 2: Information concerning the existence of approved alternative methods of compliance with this AD, if any, may be obtained from the Standardization Branch, ANM-113. (d) Special flight permits may be issued in accordance with sections 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. (e) Certain actions shall be done in accordance with Jetstream Service Bulletin J41-52-058, dated July 14, 1997. This incorporation by reference was approved by the Director of the Federal Register in accordance with 5 U.S.C. 552(a) and 1 CFR part 51. Copies may be obtained from AI(R) American Support, Inc., 13850 Mclearen Road, Herndon, Virginia 20171. Copies may be inspected at the FAA, Transport Airplane Directorate, 1601 Lind Avenue, SW., Renton, Washington; or at the Office of the Federal Register, 800 North Capitol Street, NW., suite 700, Washington, DC. (f) This amendment becomes effective on September 24, 1997. Issued in Renton, Washington, on September 3, 1997. Darrell M. Pederson, Acting Manager, Transport Airplane Directorate, Aircraft Certification Service. [FR Doc. 97-23861 Filed 9-8-97; 8:45 am] BILLING CODE 4910-13-U