AD 93-15-06

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AD Number:
93-15-06
Document Type:
AD Final Rules
Docket Number:
93-NM-118-AD
Subject Heading:
Airworthiness Directives; AIRBUS INDUSTRIE Model A300, A310 and A300-600 Series Airplanes
Subject:
Nose Landing Gear Door Uplock Assemblies
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
08/18/1993
Make:
Airbus
Model:
A300 B2-1A | A300 B2-1C | A300 B2-203 | A300 B2K-3C | A300 B4-103 | A300 B4-203 | A300 B4-2C | A300 ...Show more
Product Type:
Aircraft
Product Subtype:
Large Airplane
Affected AD:
Superseded AD:
Affected By:
Superseded By:
Service/Office:
Office of Primary Responsibility:
CFR Part Reference:
Part 39
Comments:
AIRWORTHINESS DIRECTIVES FINAL RULES: 93-15-06
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   93-NM-118-AD

AMENDMENT:   39-8652

AD NUMBER:   93-15-06

SUBJECT HEADING:   Airworthiness Directives; AIRBUS INDUSTRIE Model A300, A310 and A300-600 Series Airplanes

ACTION:  

SUMMARY:  

DATES:   Effective August 18, 1993.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
93-15-06 AIRBUS INDUSTRIE: Amendment 39-8652. Docket 93-NM-118-AD.

Applicability: All Airbus Industrie Model A300, A310 and A300-600 series airplanes; certificated in any category.

Compliance: Required as indicated, unless accomplished previously.

To prevent jamming of the free fall mechanical control mechanism, which could result in the failure of the nose landing gear (NLG) to extend during a gravity free fall, accomplish the following:

(a) Within 30 landings after the effective date of this AD, perform a detailed visual inspection to verify correct installation of the bolts that attach the left- and right-hand NLG door uplock assemblies to the support fittings, and of the bolt connecting the free fall rod to its lever in accordance with Airbus Industrie All Operator Telex (AOT) 32-06, dated March 3, 1993.
(1) If the bolts are installed correctly, no further action is required by paragraph (a) of this AD.
(2) If any bolt is found to have been incorrectly installed, prior to further flight, correct its installation and perform a functional test of the landing gear free fall control and emergency extension systems in accordance with the AOT.

(b) Within 7 days after accomplishing the detailed visual inspection required by paragraph (a) of this AD, submit a report of any inspection findings to Airbus Industrie, in accordance with Airbus Industrie AOT 32-06, dated March 3, 1993. Report all findings, including nil defects to: Airbus Industrie, Product Support Directorate, Attention: Technical Support, AI/ST41, 1 Rond Point Bellonte, 31707 Blagnac Cedex, France. Information collection requirements contained in this regulation 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.

(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, 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, ANM-113.

(d) 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.

(e) The detailed visual inspection, correction, reporting requirement, and functional test shall be done in accordance with Airbus Industrie All Operator Telex (AOT) 32-06, dated March 3, 1993. 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 Airbus Industrie, 1 Rond Point Maurice Bellonte, 31707 Blagnac Cedex, France. 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 August 18, 1993.

FOOTER: