AD 65-14-03

final rule

BOEING Models 707 and 720 Series Aircraft

AD Number
65-14-03
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 707-100 Long Body BOEING Models 707 and 720 Series Aircraft
aircraft The Boeing Company 707-100B Long Body BOEING Models 707 and 720 Series Aircraft
aircraft The Boeing Company 707-100B Short Body BOEING Models 707 and 720 Series Aircraft
aircraft The Boeing Company 707-200 BOEING Models 707 and 720 Series Aircraft
aircraft The Boeing Company 707-300 Series BOEING Models 707 and 720 Series Aircraft
aircraft The Boeing Company 707-300B Series BOEING Models 707 and 720 Series Aircraft
aircraft The Boeing Company 707-300C Series BOEING Models 707 and 720 Series Aircraft
aircraft The Boeing Company 707-400 Series BOEING Models 707 and 720 Series Aircraft
aircraft The Boeing Company 720 Series BOEING Models 707 and 720 Series Aircraft
aircraft The Boeing Company 720B Series BOEING Models 707 and 720 Series Aircraft

Unsafe Condition

Failure of the nose gear drag brace lock rod upper attachment bolt P/N BAC B30ABP6-37 due to fatigue, which could result in the nose gear remaining retracted during landing.

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

Required Actions

Replace bolt P/N BAC B30ABP6-37 with a new bolt of the same part number or approved substitutes (Standard Pressed Steel Company SFH 22-6-35, Voi-Shan Mfg. Co. VS 2545H6F35T) within specified timeframes. Repetitive replacement required every 6,000 hours' time in service unless using approved substitutes.

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

Compliance Time

Within 600 hours' time in service after the effective date (July 23, 1965) for bolts with 5,400+ hours' time in service on the effective date; prior to 6,000 hours' time in service for bolts with less than 5,400 hours' time in service on the effective date.

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

Affected Aircraft

Boeing Models 707 and 720 Series Aircraft noted in Boeing Service Bulletin No. 2073(R-1)

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

Federal Register Abstract

Nose Gear Drag Brace Lock Rod Upper Attachment Bolt

Applicability Source Text

Show captured applicability text from the source AD
AD Final Rules - DRS_65-14-03.html
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AD Number:
65-14-03
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
BOEING Models 707 and 720 Series Aircraft
Subject:
Nose Gear Drag Brace Lock Rod Upper Attachment Bolt
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
07/23/1965
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: 65-14-03
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-90

AD NUMBER:   65-14-03

SUBJECT HEADING:   BOEING Models 707 and 720 Series Aircraft

ACTION:  

SUMMARY:  

DATES:   Effective July 23, 1965.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
65-14-03 BOEING: Amdt. 39-90 Part 39 Federal Register June 23, 1965. Applies to Models 707 and 720 Series Aircraft Noted in Boeing Service Bulletin No. 2073(R-1).

Compliance required as indicated.

Investigation of a recent failure of the nose gear drag brace lock rod upper attachment bolt, which resulted in the affected aircraft landing with the nose gear retracted, indicates that this bolt is susceptible to fatigue failures and requires replacement.

(a) Bolt P/N BAC B30ABP6-37 shall be replaced as follows:

(1) Bolts having 5,400 or more hours' time in service on the effective date of this AD shall be replaced in accordance with paragraph (3) within 600 hours' time in service after the effective date of this AD.

(2) Bolts having less than 5,400 hours' time in service on the effective date of this AD shall be replaced in accordance with paragraph (3) prior to the accumulation of 6,000 hours' time in service.

(3) Replace nose gear drag brace lock rod upper attachment bolts P/N BAC B30ABP6-37 with a new bolt of the same part number or with Standard Pressed Steel Company bolt SFH 22-6-35, Voi-Shan Mfg. Co. bolt VS 2545H6F35T, or a bolt approved by the Chief, Aircraft Engineering Division, FAA Western Region.

(4) Bolts P/N BAC B30ABP6-37 installed in accordance with (3) shall be repetitively replaced thereafter within each 6,000 hours' time in service from the last replacement unless they are replaced with Standard Pressed Steel Co., bolt SFH 22-6-35, Voi-Shan Mfg. Co. bolt VS 2545H6F35T, or a bolt approved by the Chief, Aircraft Engineering Division, FAA Western Region.

(b) Operators who have not kept records of hours' time in service on nose gear drag brace lock rod upper attachment bolts shall substitute airplane hours' time in service in lieu thereof.

(Boeing Service Bulletin No. 2073 (R-1) covers this same subject.)

This directive effective July 23, 1965.

FOOTER:

Document Text

Show stored source text (verify against official source)
AD Final Rules - DRS_65-14-03.html
Copy URL
Print/Save as PDF
Document Versions
 Feedback
Details
AD Number:
65-14-03
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
BOEING Models 707 and 720 Series Aircraft
Subject:
Nose Gear Drag Brace Lock Rod Upper Attachment Bolt
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
07/23/1965
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: 65-14-03
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-90

AD NUMBER:   65-14-03

SUBJECT HEADING:   BOEING Models 707 and 720 Series Aircraft

ACTION:  

SUMMARY:  

DATES:   Effective July 23, 1965.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
65-14-03 BOEING: Amdt. 39-90 Part 39 Federal Register June 23, 1965. Applies to Models 707 and 720 Series Aircraft Noted in Boeing Service Bulletin No. 2073(R-1).

Compliance required as indicated.

Investigation of a recent failure of the nose gear drag brace lock rod upper attachment bolt, which resulted in the affected aircraft landing with the nose gear retracted, indicates that this bolt is susceptible to fatigue failures and requires replacement.

(a) Bolt P/N BAC B30ABP6-37 shall be replaced as follows:

(1) Bolts having 5,400 or more hours' time in service on the effective date of this AD shall be replaced in accordance with paragraph (3) within 600 hours' time in service after the effective date of this AD.

(2) Bolts having less than 5,400 hours' time in service on the effective date of this AD shall be replaced in accordance with paragraph (3) prior to the accumulation of 6,000 hours' time in service.

(3) Replace nose gear drag brace lock rod upper attachment bolts P/N BAC B30ABP6-37 with a new bolt of the same part number or with Standard Pressed Steel Company bolt SFH 22-6-35, Voi-Shan Mfg. Co. bolt VS 2545H6F35T, or a bolt approved by the Chief, Aircraft Engineering Division, FAA Western Region.

(4) Bolts P/N BAC B30ABP6-37 installed in accordance with (3) shall be repetitively replaced thereafter within each 6,000 hours' time in service from the last replacement unless they are replaced with Standard Pressed Steel Co., bolt SFH 22-6-35, Voi-Shan Mfg. Co. bolt VS 2545H6F35T, or a bolt approved by the Chief, Aircraft Engineering Division, FAA Western Region.

(b) Operators who have not kept records of hours' time in service on nose gear drag brace lock rod upper attachment bolts shall substitute airplane hours' time in service in lieu thereof.

(Boeing Service Bulletin No. 2073 (R-1) covers this same subject.)

This directive effective July 23, 1965.

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.