AD 81-04-51 R1

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AD Number:
81-04-51 R1
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; MCDONNELL DOUGLAS DC-9-80 Series Airplanes
Subject:
Autothrottle Disengage
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
12/28/1981
Make:
The Boeing Company
Model:
DC-9-81 (MD-81) | DC-9-82 (MD-82) | DC-9-83 (MD-83) | DC-9-87 (MD-87)
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Superseded AD: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Superseded By: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: 81-04-51 R1
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-4281

AD NUMBER:   81-04-51 R1

SUBJECT HEADING:   Airworthiness Directives; MCDONNELL DOUGLAS DC-9-80 Series Airplanes

ACTION:  

SUMMARY:  

DATES:   Effective December 28, 1981.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
81-04-51 R1 MCDONNELL DOUGLAS: Amendment 39-4107 as amended by amendment 39-4281. Applies to McDonnell Douglas Model DC-9-80 series airplanes, fuselage numbers 924 through 1017 inclusive, certificated in all categories. Compliance required as noted in the body of this AD, unless already accomplished. To prevent unscheduled deployment of the thrust reversers during approach prior to touchdown, accomplish the following:

A. Effective immediately after the effective date of this AD, the flight crew shall disengage the autothrottle during approach prior to reaching 50 feet AGL.

B. Within 48 hours calendar time after receipt of this AD, unless already accomplished:

1. Placard each aircraft in clear view of each pilot with the following wording: "Disengage ATS on approach before reaching 50 feet AGL."

2. The FAA-approved Airplane Flight Manual shall be revised to add the following in the limitations section:

AUTOTHROTTLES: The autothrottles must be disengaged during approach before reaching 50 feet AGL.

C. Alternate means of compliance or other actions which provide an equivalent level of safety may be used when approved by the Chief, Los Angeles Area Aircraft Certification Office, FAA Northwest Region.

D. Incorporation of the modifications in accordance with Part 2, Accomplishment Instructions, of McDonnell Douglas DC-9 Super 80 Service Bulletin 78-47 dated August 4, 1981, or later revisions approved by the Chief, Los Angeles Area Aircraft Certification Office, FAA Northwest Mountain Region, constitutes terminating action. Following such modification, both the placard and the Airplane Flight Manual limitation required by A. and B. above may be removed.

The manufacturer's specifications and procedures identified and described in this directive are incorporated herein and made a part hereof pursuant to 5 U.S.C. 552(a)(1).

All persons affected by this directive who have not already received these documents from the manufacturer may obtain copies upon request to McDonnell Douglas Corporation, 3855 Lakewood Boulevard, Long Beach, California 90846, Attention: Director, Publications and Training, C1-750 (54-60). This document also may be examined at FAA Northwest Mountain Region, 9010 East Marginal Way South, Seattle, Washington 98108; or the Los Angeles Area Aircraft Certification Office, 4344 Donald Douglas Drive, Long Beach, California 90808.

Amendment 39-4107 became effective May 14, 1981, to all persons, except to whom it was made immediately effective by telegram dated February 9, 1981.

This amendment 39-4281 becomes effective December 28, 1981.


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