AD 77-10-12

final rule

Airworthiness Directives; MCDONNELL DOUGLAS DC-8 Series Airplanes

AD Number
77-10-12
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Unknown
FR Citation
This information is not available.
Technical illustration of an aircraft flight control surface and actuator
Problem area Flight controls

Applicability

TypeManufacturerModelDetails
aircraft The Boeing Company DC-8-11 Airworthiness Directives; MCDONNELL DOUGLAS DC-8 Series Airplanes
aircraft The Boeing Company DC-8-12 Airworthiness Directives; MCDONNELL DOUGLAS DC-8 Series Airplanes
aircraft The Boeing Company DC-8-21 Airworthiness Directives; MCDONNELL DOUGLAS DC-8 Series Airplanes
aircraft The Boeing Company DC-8-31 Airworthiness Directives; MCDONNELL DOUGLAS DC-8 Series Airplanes
aircraft The Boeing Company DC-8-32 Airworthiness Directives; MCDONNELL DOUGLAS DC-8 Series Airplanes
aircraft The Boeing Company DC-8-33 Airworthiness Directives; MCDONNELL DOUGLAS DC-8 Series Airplanes
aircraft The Boeing Company DC-8-41 Airworthiness Directives; MCDONNELL DOUGLAS DC-8 Series Airplanes
aircraft The Boeing Company DC-8-42 Airworthiness Directives; MCDONNELL DOUGLAS DC-8 Series Airplanes
aircraft The Boeing Company DC-8-43 Airworthiness Directives; MCDONNELL DOUGLAS DC-8 Series Airplanes
aircraft The Boeing Company DC-8-51 Airworthiness Directives; MCDONNELL DOUGLAS DC-8 Series Airplanes
aircraft The Boeing Company DC-8-52 Airworthiness Directives; MCDONNELL DOUGLAS DC-8 Series Airplanes
aircraft The Boeing Company DC-8-53 Airworthiness Directives; MCDONNELL DOUGLAS DC-8 Series Airplanes
aircraft The Boeing Company DC-8-55 Airworthiness Directives; MCDONNELL DOUGLAS DC-8 Series Airplanes
aircraft The Boeing Company DC-8-61 Airworthiness Directives; MCDONNELL DOUGLAS DC-8 Series Airplanes
aircraft The Boeing Company DC-8-61F Airworthiness Directives; MCDONNELL DOUGLAS DC-8 Series Airplanes
aircraft The Boeing Company DC-8-62 Airworthiness Directives; MCDONNELL DOUGLAS DC-8 Series Airplanes
aircraft The Boeing Company DC-8-62F Airworthiness Directives; MCDONNELL DOUGLAS DC-8 Series Airplanes
aircraft The Boeing Company DC-8-63 Airworthiness Directives; MCDONNELL DOUGLAS DC-8 Series Airplanes
aircraft The Boeing Company DC-8-63F Airworthiness Directives; MCDONNELL DOUGLAS DC-8 Series Airplanes
aircraft The Boeing Company DC-8-71 Airworthiness Directives; MCDONNELL DOUGLAS DC-8 Series Airplanes
aircraft The Boeing Company DC-8-71F Airworthiness Directives; MCDONNELL DOUGLAS DC-8 Series Airplanes
aircraft The Boeing Company DC-8-72 Airworthiness Directives; MCDONNELL DOUGLAS DC-8 Series Airplanes
aircraft The Boeing Company DC-8-72F Airworthiness Directives; MCDONNELL DOUGLAS DC-8 Series Airplanes
aircraft The Boeing Company DC-8-73 Airworthiness Directives; MCDONNELL DOUGLAS DC-8 Series Airplanes
aircraft The Boeing Company DC-8-73F Airworthiness Directives; MCDONNELL DOUGLAS DC-8 Series Airplanes
aircraft The Boeing Company DC-8F-54 Airworthiness Directives; MCDONNELL DOUGLAS DC-8 Series Airplanes
aircraft The Boeing Company DC-8F-55 Airworthiness Directives; MCDONNELL DOUGLAS DC-8 Series Airplanes

Unsafe Condition

Cracks and failure or jamming of the elevator geared tab crank arm and gust lock assemblies could occur, leading to reduced elevator control effectiveness.

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

Required Actions

Visually inspect both left and right side inboard and outboard elevator geared tab crank arm assemblies (P/N 4710541 and 4710542) and gust lock assembly (P/N 5644178) for cracks and failure. Replace failed or cracked parts with serviceable ones before further flight. Verify clearance between crank assemblies and box section throughout elevator travel.

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

Compliance Time

within the next 300 hours time in service or 30 days after the effective date of this AD, whichever comes first, unless already accomplished within the past 30 days

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

Affected Aircraft

McDonnell Douglas DC-8 Series airplanes, including models DC-8-11, DC-8-12, DC-8-21, DC-8-31, DC-8-32, DC-8-33, DC-8-41, DC-8-42, DC-8-43, DC-8-51, and others as listed, certificated in all categories.

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

Federal Register Abstract

Crank Arm Assembly

Applicability Source Text

Show captured applicability text from the source AD
AD Final Rules - DRS_77-10-12.html
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Details
AD Number:
77-10-12
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; MCDONNELL DOUGLAS DC-8 Series Airplanes
Subject:
Crank Arm Assembly
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
05/26/1977
Make:
The Boeing Company
Model:
DC-8-11 | DC-8-12 | DC-8-21 | DC-8-31 | DC-8-32 | DC-8-33 | DC-8-41 | DC-8-42 | DC-8-43 | DC-8-51 | ...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: 77-10-12
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-2906

AD NUMBER:   77-10-12

SUBJECT HEADING:   Airworthiness Directives; MCDONNELL DOUGLAS DC-8 Series Airplanes

ACTION:  

SUMMARY:  

DATES:   Effective May 26, 1977.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
77-10-12 MCDONNELL DOUGLAS: Amendment 39-2906. Applies to Model DC-8 Series airplanes, certificated in all categories.

Compliance required within the next 300 hours time in service or 30 days after the effective date of this AD, whichever comes first, unless already accomplished within the past 30 days.

To detect cracks and prevent failure or jamming of the elevator geared tab crank arm and gust lock assemblies, comply with the following:

(a) Visually inspect both the left and right side inboard and outboard elevator geared tab crank arm assemblies, P/N's 4710541 and 4710542 for failure and/or cracks.

(b) Visually inspect the P/N 5644178 gust lock assembly, and specifically, the torque tube section of the P/N 4644181 crank assembly, for failure and/or cracks.

(c) Failed or cracked parts must be replaced with like serviceable parts before further flight.

(d) Verify that clearance exists between the crank assemblies, P/N 4710541 and 4710542, and the box section for all positions along elevator travel.

Note: McDonnell Douglas DC-8 Alert Service Bulletin A27-262, dated April 28, 1977, covers the same subject.

(e) Special flight permits may be issued in accordance with FAR's 21.197 and 21.199 to authorize operation of an airplane to a base to perform the inspections required by this AD.

This amendment becomes effective May 26, 1977.


FOOTER:

Document Text

Show stored source text (verify against official source)
AD Final Rules - DRS_77-10-12.html
Copy URL
Print/Save as PDF
Document Versions
 Feedback
Details
AD Number:
77-10-12
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; MCDONNELL DOUGLAS DC-8 Series Airplanes
Subject:
Crank Arm Assembly
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
05/26/1977
Make:
The Boeing Company
Model:
DC-8-11 | DC-8-12 | DC-8-21 | DC-8-31 | DC-8-32 | DC-8-33 | DC-8-41 | DC-8-42 | DC-8-43 | DC-8-51 | ...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: 77-10-12
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-2906

AD NUMBER:   77-10-12

SUBJECT HEADING:   Airworthiness Directives; MCDONNELL DOUGLAS DC-8 Series Airplanes

ACTION:  

SUMMARY:  

DATES:   Effective May 26, 1977.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
77-10-12 MCDONNELL DOUGLAS: Amendment 39-2906. Applies to Model DC-8 Series airplanes, certificated in all categories.

Compliance required within the next 300 hours time in service or 30 days after the effective date of this AD, whichever comes first, unless already accomplished within the past 30 days.

To detect cracks and prevent failure or jamming of the elevator geared tab crank arm and gust lock assemblies, comply with the following:

(a) Visually inspect both the left and right side inboard and outboard elevator geared tab crank arm assemblies, P/N's 4710541 and 4710542 for failure and/or cracks.

(b) Visually inspect the P/N 5644178 gust lock assembly, and specifically, the torque tube section of the P/N 4644181 crank assembly, for failure and/or cracks.

(c) Failed or cracked parts must be replaced with like serviceable parts before further flight.

(d) Verify that clearance exists between the crank assemblies, P/N 4710541 and 4710542, and the box section for all positions along elevator travel.

Note: McDonnell Douglas DC-8 Alert Service Bulletin A27-262, dated April 28, 1977, covers the same subject.

(e) Special flight permits may be issued in accordance with FAR's 21.197 and 21.199 to authorize operation of an airplane to a base to perform the inspections required by this AD.

This amendment becomes effective May 26, 1977.


FOOTER:

Source: Official FAA Source ↗

Retrieved: Apr 8, 2026

Rights: U.S. Government Public Domain

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