AD 91-05-11

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AD Number:
91-05-11
Document Type:
AD Final Rules
Docket Number:
90-NM-196-AD
Subject Heading:
Airworthiness Directives; BOEING Model 737-300 Series Airplanes
Subject:
AFM Changes - Extended Range
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
03/26/1991
Make:
The Boeing Company
Model:
737-300 Series
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Superseded AD: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Superseded By: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: 91-05-11
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   90-NM-196-AD

AMENDMENT:   39-6909

AD NUMBER:   91-05-11

SUBJECT HEADING:   Airworthiness Directives; BOEING Model 737-300 Series Airplanes

ACTION:  

SUMMARY:  

DATES:   Effective March 26, 1991.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
91-05-11 BOEING: Amendment 39-6909. Docket No. 90-NM-196-AD.

Applicability: Model 737-300 series airplanes, equipped with CFM56-3 series engines, certificated in any category.

Compliance: Required as indicated, unless previously accomplished.

To reduce the risk of total engine thrust loss due to unavoidable severe weather penetration during an ETOPS single engine diversion, accomplish the following:

A. Within the next 30 days after June 12, 1989 (the effective date of Amendment 39-6247), delete from the FAA-approved Airplane Flight Manual (AFM) any reference to approval or suitability of the Model 737-300 airplane for use in extended range operation. This may be accomplished by replacing the existing AFM page(s) containing the Extended Range Operations suitability statement with a page(s) which has that statement deleted. If the existing AFM does not contain such a statement, then no action is necessary.

B. A new AFM ETOPS suitability statement, outlined below, may be inserted into the FAA-approved AFM when the airplane has been configured in accordance with Boeing Document D6-38123, Revision A, dated September 14, 1990, "Configuration, Maintenance and Procedures for Extended Range Operation" (CMP):

EXTENDED RANGE OPERATIONS

The type design reliability and performance of this airplane/engine combination has been evaluated in accordance with FAA Advisory Circular 120-42A and found suitable for extended range operations when configured in accordance with FAA-approved Boeing Document D6- 38123, Revision A, dated September 14, 1990, "Configuration, Maintenance and Procedures for Extended Range (ER) Operation." This finding does not constitute approval to conduct extended range operations.

C. An alternate means of compliance or adjustment of the compliance time, which provides an acceptable level of safety, may be used when approved by the Manager, Seattle Aircraft Certification Office (ACO), FAA, Transport Airplane Directorate.

NOTE: The request should be submitted directly to the Manager, Seattle ACO, and a copy sent to the cognizant FAA Principal Inspector (PI). The PI will then forward comments or concurrence to the Seattle ACO.

D. Special flight permits may be issued in accordance with FAR 21.197 and 21.199 to operate airplanes to a base in order to comply with the requirements of this AD.

All persons affected by this directive who have not already received the appropriate service documents from the manufacturer may obtain copies upon request to Boeing Commercial Airplane Group, P.O. Box 3707, Seattle, Washington 98124. These documents may be examined at the FAA, Northwest Mountain Region, Transport Airplane Directorate, 1601 Lind Avenue SW., Renton, Washington.

Airworthiness Directive 91-05-11 supersedes AD 89-13-06, Amendment 39-6247.
This amendment (39-6909, AD 91-05-11) becomes effective on March 26, 1991.

FOOTER: