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AD 92-18-06 ACTIVE

Braking and Directional Control
Key Information
AD Number 92-18-06 Status Active
Effective Date October 08, 1992 Issue Date Not specified
Docket Number 92-NM-46-AD Amendment 39-8350
Product Type ["Aircraft"] Product Subtype ["Large Airplane"]
CFR Part --- - Part 39 CFR Section N/A
Citation This information is not available.
Applicability
Manufacturer(s) BAE Systems (Operations) Limited
Model(s) BAe 146-100A BAe 146-200A BAe 146-300A
Regulatory Text

92-18-06 BRITISH AEROSPACE: Amendment 39-8350. Docket No. 92-NM-46-AD.
Applicability: Model BAe 146-100A, -200A, and -300A series airplanes, equipped with Dunlop hydraulic fuses, part number ACM29100; certificated in any category.

Compliance: Required as indicated, unless accomplished previously.

To prevent potential loss of airplane braking and directional control, accomplish the following:

(a) Prior to the accumulation of 4,000 landings since installation of Dunlop hydraulic fuses having part number ACM29100 (Mod. states 1 or 2), or within 60 days after the effective date of this AD, whichever occurs later, remove green and yellow hydraulic systems Dunlop hydraulic fuses having part number ACM29100 (Mod. states 1 or 2) and install new hydraulic fuses having part number ACM30506 (Mod. 1), in accordance with British Aerospace Modification Service Bulletin SB.32-130-70295C, dated September 27, 1991.

(b) 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, FAA, Transport Airplane Directorate. 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: Information concerning the existence of approved alternative methods of compliance with this AD, if any, may be obtained from the Standardization Branch.

(c) Special flight permits may be issued in accordance with FAR 21.197 and 21.199 to operate the airplane to a location where the requirements of this AD can be accomplished.

(d) The removal and installation shall be done in accordance with British Aerospace Modification Service Bulletin SB.32-130-70295C, dated September 27, 1991. 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 British Aerospace, PLC, Librarian for Service Bulletins, P.O. Box 17414, Dulles International Airport, Washington, DC. 20041-0414. 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.

(e) This amendment becomes effective on October 8, 1992.