AD 71-08-02

final rule

Airworthiness Directives; MCDONNELL DOUGLAS DC-9 Airplanes

AD Number
71-08-02
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Unknown
FR Citation
This information is not available.
Technical illustration of an aircraft landing gear and wheel assembly
Problem area Landing gear

Applicability

TypeManufacturerModelDetails
aircraft The Boeing Company DC-9-11 Airworthiness Directives; MCDONNELL DOUGLAS DC-9 Airplanes
aircraft The Boeing Company DC-9-12 Airworthiness Directives; MCDONNELL DOUGLAS DC-9 Airplanes
aircraft The Boeing Company DC-9-13 Airworthiness Directives; MCDONNELL DOUGLAS DC-9 Airplanes
aircraft The Boeing Company DC-9-14 Airworthiness Directives; MCDONNELL DOUGLAS DC-9 Airplanes
aircraft The Boeing Company DC-9-15 Airworthiness Directives; MCDONNELL DOUGLAS DC-9 Airplanes
aircraft The Boeing Company DC-9-15F Airworthiness Directives; MCDONNELL DOUGLAS DC-9 Airplanes
aircraft The Boeing Company DC-9-21 Airworthiness Directives; MCDONNELL DOUGLAS DC-9 Airplanes
aircraft The Boeing Company DC-9-31 Airworthiness Directives; MCDONNELL DOUGLAS DC-9 Airplanes
aircraft The Boeing Company DC-9-32 Airworthiness Directives; MCDONNELL DOUGLAS DC-9 Airplanes
aircraft The Boeing Company DC-9-32 (VC-9C) Airworthiness Directives; MCDONNELL DOUGLAS DC-9 Airplanes
aircraft The Boeing Company DC-9-32F Airworthiness Directives; MCDONNELL DOUGLAS DC-9 Airplanes
aircraft The Boeing Company DC-9-32F (C-9A) Airworthiness Directives; MCDONNELL DOUGLAS DC-9 Airplanes
aircraft The Boeing Company DC-9-32F (C-9B) Airworthiness Directives; MCDONNELL DOUGLAS DC-9 Airplanes
aircraft The Boeing Company DC-9-33F Airworthiness Directives; MCDONNELL DOUGLAS DC-9 Airplanes
aircraft The Boeing Company DC-9-34 Airworthiness Directives; MCDONNELL DOUGLAS DC-9 Airplanes
aircraft The Boeing Company DC-9-34F Airworthiness Directives; MCDONNELL DOUGLAS DC-9 Airplanes
aircraft The Boeing Company DC-9-41 Airworthiness Directives; MCDONNELL DOUGLAS DC-9 Airplanes
aircraft The Boeing Company DC-9-51 Airworthiness Directives; MCDONNELL DOUGLAS DC-9 Airplanes
aircraft The Boeing Company DC-9-81 (MD-81) Airworthiness Directives; MCDONNELL DOUGLAS DC-9 Airplanes
aircraft The Boeing Company DC-9-82 (MD-82) Airworthiness Directives; MCDONNELL DOUGLAS DC-9 Airplanes
aircraft The Boeing Company DC-9-83 (MD-83) Airworthiness Directives; MCDONNELL DOUGLAS DC-9 Airplanes
aircraft The Boeing Company DC-9-87 (MD-87) Airworthiness Directives; MCDONNELL DOUGLAS DC-9 Airplanes

Unsafe Condition

Failure to control speed brake retraction and inflight deployment of ground spoilers could result in loss of airplane control.

AI-generated summary from the source AD text. Verify against the official source before acting.

Required Actions

Affix cockpit placards stating 'DO NOT EXTEND GEAR WITH SPEED BRAKES DEPLOYED' and 'DO NOT ARM GROUND SPOILERS PRIOR TO GEAR EXTENSION', or install interlock switch per McDonnell Douglas Service Bulletin 32-128 and amend AFM limitations section with the same statements. Previously installed placards may be removed if the interlock switch is installed.

AI-generated summary from the source AD text. Verify against the official source before acting.

Compliance Time

within the next 50 hours' time in service after effective date of this AD

AI-generated summary from the source AD text. Verify against the official source before acting.

Affected Aircraft

MCDONNELL DOUGLAS DC-9 airplanes certificated in all categories, including models DC-9-11, DC-9-12, DC-9-13, DC-9-14, DC-9-15, DC-9-15F, DC-9-21, DC-9-31, DC-9-32, and others as listed.

AI-generated summary from the source AD text. Verify against the official source before acting.

Federal Register Abstract

Control Of Speed Brake

Applicability Source Text

Show captured applicability text from the source AD
AD Final Rules - DRS_71-08-02.html
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Details
AD Number:
71-08-02
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; MCDONNELL DOUGLAS DC-9 Airplanes
Subject:
Control Of Speed Brake
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
11/30/1971
Make:
The Boeing Company
Model:
DC-9-11 | DC-9-12 | DC-9-13 | DC-9-14 | DC-9-15 | DC-9-15F | DC-9-21 | DC-9-31 | DC-9-32 | DC-9-32 (...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: 71-08-02
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-1346

AD NUMBER:   71-08-02

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

ACTION:  

SUMMARY:  

DATES:   Effective November 30, 1971.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
71-08-02 MCDONNELL DOUGLAS: Amend 39-1189 as amended by amendment 39-1346. Applies to DC-9 airplanes certificated in all categories.

Compliance required within the next 50 hours' time in service after effective date of this AD, unless already accomplished.

To ensure pilot control of speed brake retraction and to prevent inflight deployment of ground spoilers, accomplish one of the following:

1. Affix a placard(s) in the cockpit in plain view of both crew members stating:

DO NOT EXTEND GEAR WITH SPEED BRAKES DEPLOYED

DO NOT ARM GROUND SPOILERS PRIOR TO GEAR EXTENSION

2. a. Install the interlock switch per McDonnell Douglas DC-9 Service Bulletin No. 32-128, dated November 17, 1971, or later FAA approved revisions, or an equivalent modification approved by the Chief, Aircraft Engineering Division, FAA Western Region and

b. Amend the Limitations Section, FAA Approved Airplane Flight Manual, to include the statements:

Do not extend gear with speed brakes deployed.

Do not arm ground spoilers prior to gear extension.

NOTE: Placards previously installed per Step 1. may be removed if step 2 is accomplished.

Amendment 39-1189 became effective April 13, 1971.

This amendment 39-1346 becomes effective November 30, 1971.


FOOTER:

Document Text

Show stored source text (verify against official source)
AD Final Rules - DRS_71-08-02.html
Copy URL
Print/Save as PDF
Document Versions
 Feedback
Details
AD Number:
71-08-02
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; MCDONNELL DOUGLAS DC-9 Airplanes
Subject:
Control Of Speed Brake
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
11/30/1971
Make:
The Boeing Company
Model:
DC-9-11 | DC-9-12 | DC-9-13 | DC-9-14 | DC-9-15 | DC-9-15F | DC-9-21 | DC-9-31 | DC-9-32 | DC-9-32 (...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: 71-08-02
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-1346

AD NUMBER:   71-08-02

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

ACTION:  

SUMMARY:  

DATES:   Effective November 30, 1971.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
71-08-02 MCDONNELL DOUGLAS: Amend 39-1189 as amended by amendment 39-1346. Applies to DC-9 airplanes certificated in all categories.

Compliance required within the next 50 hours' time in service after effective date of this AD, unless already accomplished.

To ensure pilot control of speed brake retraction and to prevent inflight deployment of ground spoilers, accomplish one of the following:

1. Affix a placard(s) in the cockpit in plain view of both crew members stating:

DO NOT EXTEND GEAR WITH SPEED BRAKES DEPLOYED

DO NOT ARM GROUND SPOILERS PRIOR TO GEAR EXTENSION

2. a. Install the interlock switch per McDonnell Douglas DC-9 Service Bulletin No. 32-128, dated November 17, 1971, or later FAA approved revisions, or an equivalent modification approved by the Chief, Aircraft Engineering Division, FAA Western Region and

b. Amend the Limitations Section, FAA Approved Airplane Flight Manual, to include the statements:

Do not extend gear with speed brakes deployed.

Do not arm ground spoilers prior to gear extension.

NOTE: Placards previously installed per Step 1. may be removed if step 2 is accomplished.

Amendment 39-1189 became effective April 13, 1971.

This amendment 39-1346 becomes effective November 30, 1971.


FOOTER:

Source: Official FAA Source ↗

Retrieved: Apr 8, 2026

Rights: U.S. Government Public Domain

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