AD 81-04-51 R1

Airworthiness directive · Autothrottle Disengage · Boeing DC-9-81 (MD-81), DC-9-82 (MD-82), DC-9-83 (MD-83) and 1 more

Effective
December 28, 1981
Models
DC-9-81 (MD-81), DC-9-82 (MD-82), DC-9-83 (MD-83), DC-9-87 (MD-87)
Data sheet
TCDSA6WE
Registered aircraft
86 matched by model
Product
Aircraft · Large airplane
Amendment
39-4281

Unofficial copy of the text in the FAA’s Dynamic Regulatory System. The FAA’s own copy is the authoritative one. DRS record last changed May 30, 2024.

On this page

The airworthiness directive

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.

Affected TCDS · 1

The type certificate data sheets for the models this AD names, matched by model and maker.

Registered aircraft · 86

Registered aircraft whose airframe or engine model this AD names. Matched by model only, so check each against the AD’s applicability.

By aircraft maker
  • Mcdonnell Douglas85 aircraft
  • Douglas1 aircraft
By year built
19821999
Registered aircraft by year built: 76 aircraft
19821
19861
19875
19884
19893
19903
199123
19925
19931
19941
19961
19976
19986
199916

10 with no year recorded

By model

Aircraft

See all 86 aircraft