AD 2002-23-01 Airworthiness Directives; Gulfstream Aerospace LP Model Galaxy and Gulfstream 200 Airplanes

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

Model Galaxy airplanes, having serial numbers 004 through 056 inclusive; and Gulfstream 200 airplanes, having serial numbers 057 through 073 inclusive; 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 detect and correct damage to the forward engine cross spar assembly, which could result in the reduced structural integrity of the forward engine cross spar assembly, accomplish the following: Inspection and Corrective Action, If Necessary (a) Within 20 flight cycles after the effective date of this AD, perform a one-time detailed inspection to detect evidence of damage ( i.e. , drill marks) to the forward engine cross spar assembly at fuselage station 582.000, per the Accomplishment Instructions of Gulfstream 200 Service Bulletin 200-53-128, dated September 18, 2002. Note 2: 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.” (1) If no evidence of damage is found, no further action is required by this paragraph. (2) If any damage is found, prior to further flight, repair in accordance with a method approved by the Manager, International Branch, ANM-116, FAA, Transport Airplane Directorate; or the Civil Aviation Administration of Israel (or its delegated agent). Reporting Requirement (b) Submit a report of inspection findings (both positive and negative) to Gulfstream Aerospace Corporation, P.O. Box 2206, Mail Station D25, Savannah, Georgia 31402; fax (912) 965-3598; at the applicable time specified in paragraph (b)(1) or (b)(2) of this AD. The report must include the inspection results, a description of any discrepancy found, the airplane serial number, and the number of landings and flight hours on the airplane. Information collection requirements contained in this AD have been approved by the Office of Management and Budget (OMB) under the provisions of the Paperwork Reduction Act of 1980 (44 U.S.C. 3501 et seq. ) and have been assigned OMB Control Number 2120-0056. (1) For airplanes on which the inspection is accomplished after the effective date of this AD: Submit the report within 60 days after performing the inspection required by paragraph (a) of this AD. (2) For airplanes on which the inspection has been accomplished prior to the effective date of this AD: Submit the report within 60 days after the effective date of this AD. Alternative Methods of Compliance (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, International Branch, ANM-116. Operators shall submit their requests through an appropriate FAA Principal Maintenance Inspector, who may add comments and then send it to the Manager, International Branch, ANM-116. Note 3: Information concerning the existence of approved alternative methods of compliance with this AD, if any, may be obtained from the International Branch, ANM-116. Special Flight Permits (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. Incorporation by Reference (e) Unless otherwise specified in this AD, the actions shall be done in accordance with Gulfstream 200 Service Bulletin 200-53-128, dated September 18, 2002, including a Service Reply Card. 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 Gulfstream Aerospace Corporation, P.O. Box 2206, Mail Station D25, Savannah, Georgia 31402. 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. Note 4: The subject of this AD is addressed in Israeli airworthiness directive 53-02-08-08, dated September 10, 2002. Effective Date (f) This amendment becomes effective on November 29, 2002. Issued in Renton, Washington, on November 5, 2002. Kalene C. Yanamura, Acting Manager, Transport Airplane Directorate, Aircraft Certification Service. [FR Doc. 02-28613 Filed 11-12-02; 8:45 am] BILLING CODE 4910-13-P