AD 62-08-05

final rule

BOEING 707 and 720 Series Aircraft

AD Number
62-08-05
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Unknown
FR Citation
This information is not available.
Technical illustration of an aircraft electrical generator and wiring assembly
Problem area Electrical system

Applicability

TypeManufacturerModelDetails
aircraft The Boeing Company 707-100 Long Body BOEING 707 and 720 Series Aircraft
aircraft The Boeing Company 707-100B Long Body BOEING 707 and 720 Series Aircraft
aircraft The Boeing Company 707-100B Short Body BOEING 707 and 720 Series Aircraft
aircraft The Boeing Company 707-200 BOEING 707 and 720 Series Aircraft
aircraft The Boeing Company 707-300 Series BOEING 707 and 720 Series Aircraft
aircraft The Boeing Company 707-300B Series BOEING 707 and 720 Series Aircraft
aircraft The Boeing Company 707-300C Series BOEING 707 and 720 Series Aircraft
aircraft The Boeing Company 707-400 Series BOEING 707 and 720 Series Aircraft
aircraft The Boeing Company 720 Series BOEING 707 and 720 Series Aircraft
aircraft The Boeing Company 720B Series BOEING 707 and 720 Series Aircraft

Unsafe Condition

Loss of the electrical system and accumulation of dense smoke in the cockpit and cabin due to loose lugs, braided leads, inadequate separation of braid jumpers, overheating wiring, or capacitor issues within the J6 electrical panel.

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

Required Actions

Inspect electrical components and wiring in the J6 panel to ensure lugs and braided leads are tightly secured, braid jumpers are adequately separated, no overheating or capacitor leaks exist. Repair as needed using acceptable maintenance practices.

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

Compliance Time

within the next 25 hours' time in service

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

Affected Aircraft

All 707 and 720 Series Aircraft

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

Federal Register Abstract

Electrical System

Applicability Source Text

Show captured applicability text from the source AD
AD Final Rules - DRS_62-08-05.html
Copy URL
Print/Save as PDF
Document Versions
 Feedback
Details
AD Number:
62-08-05
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
BOEING 707 and 720 Series Aircraft
Subject:
Electrical System
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
Make:
The Boeing Company
Model:
707-100 Long Body | 707-100B Long Body | 707-100B Short Body | 707-200 | 707-300 Series | 707-300B S...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: 62-08-05
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:  

AD NUMBER:   62-08-05

SUBJECT HEADING:   BOEING 707 and 720 Series Aircraft

ACTION:  

SUMMARY:  

DATES:  

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
62-08-05 BOEING: Amdt. 422 Part 507 Federal Register April 17, 1962. Applies to All 707 and 720 Series Aircraft.

As a result of a recent incident involving loss of the electrical system and accumulation of dense smoke in the cockpit and cabin, the following is required:

(a) Unless already accomplished in accordance with recommendations contained in the telegram dated March 23, 1962, issued by Boeing Aircraft Company, within the next 25 hours' time in service, inspect electrical components and wiring within the J6 electrical panel to determine that:

(1) Lugs and braided leads are tightly secured to the contractor studs;

(2) Braid jumpers are adequately separated from adjacent jumpers to prevent contact;

(3) There is no evidence of overheating in wiring and braided leads; and

(4) There is no evidence of capacitor leaks, swelling or overheating.

(b) If any of the foregoing items require corrective action, repair in accordance with acceptable maintenance practices.

This directive effective upon publication in the Federal Register for all persons except those to whom it was made effective immediately by telegram dated March 30, 1962.

FOOTER:

Document Text

Show stored source text (verify against official source)
AD Final Rules - DRS_62-08-05.html
Copy URL
Print/Save as PDF
Document Versions
 Feedback
Details
AD Number:
62-08-05
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
BOEING 707 and 720 Series Aircraft
Subject:
Electrical System
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
Make:
The Boeing Company
Model:
707-100 Long Body | 707-100B Long Body | 707-100B Short Body | 707-200 | 707-300 Series | 707-300B S...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: 62-08-05
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:  

AD NUMBER:   62-08-05

SUBJECT HEADING:   BOEING 707 and 720 Series Aircraft

ACTION:  

SUMMARY:  

DATES:  

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
62-08-05 BOEING: Amdt. 422 Part 507 Federal Register April 17, 1962. Applies to All 707 and 720 Series Aircraft.

As a result of a recent incident involving loss of the electrical system and accumulation of dense smoke in the cockpit and cabin, the following is required:

(a) Unless already accomplished in accordance with recommendations contained in the telegram dated March 23, 1962, issued by Boeing Aircraft Company, within the next 25 hours' time in service, inspect electrical components and wiring within the J6 electrical panel to determine that:

(1) Lugs and braided leads are tightly secured to the contractor studs;

(2) Braid jumpers are adequately separated from adjacent jumpers to prevent contact;

(3) There is no evidence of overheating in wiring and braided leads; and

(4) There is no evidence of capacitor leaks, swelling or overheating.

(b) If any of the foregoing items require corrective action, repair in accordance with acceptable maintenance practices.

This directive effective upon publication in the Federal Register for all persons except those to whom it was made effective immediately by telegram dated March 30, 1962.

FOOTER:

Source: Official FAA Source ↗

Retrieved: Apr 8, 2026

Rights: U.S. Government Public Domain

This site is not affiliated with or endorsed by the FAA. Always verify with official sources.