AD 67-14-05
final rule
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Airbus SAS | BAC 1-11 200 Series | Airworthiness Directives; BRITISH AIRCRAFT Model BAC 1-11 200 Series Airplanes |
Unsafe Condition
Fatigue failure of the nose landing gear steering jack cylinder gland nut P/N AB44-229.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Replace aluminum alloy gland nuts P/N AB44-229 with unused aluminum alloy nuts of the same part number or steel nuts P/N AB44-1793, depending on time in service. For nuts with less than 4,900 hours by AD effective date, replace before 5,000 hours. For 4,900+ hours, replace within next 100 hours. Aluminum alloy replacements must be replaced before 5,000 hours.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Before the accumulation of specified hours' time in service as per paragraphs (a) and (b).
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
BRITISH AIRCRAFT Model BAC 1-11 200 Series Airplanes.
AI-generated summary from the source AD text. Verify against the official source before acting.
Federal Register Abstract
Nose Gear Steering Cylinder Gland Nut
Applicability Source Text
Show captured applicability text from the source AD
AD Final Rules - DRS_67-14-05.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 67-14-05 Document Type: AD Final Rules Docket Number: Unknown Subject Heading: Airworthiness Directives; BRITISH AIRCRAFT Model BAC 1-11 200 Series Airplanes Subject: Nose Gear Steering Cylinder Gland Nut Status: Current Citation: This information is not available. Citation Publish Date: Effective Date: 05/14/1967 Make: Airbus SAS Model: BAC 1-11 200 Series Product Type: Aircraft Product Subtype: Large Airplane Affected AD: Superseded AD: Affected By: Superseded By: Service/Office: Office of Primary Responsibility: CFR Part Reference: Part 39 Comments: AIRWORTHINESS DIRECTIVES FINAL RULES: 67-14-05 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: Unknown AMENDMENT: 39-398 AD NUMBER: 67-14-05 SUBJECT HEADING: Airworthiness Directives; BRITISH AIRCRAFT Model BAC 1-11 200 Series Airplanes ACTION: SUMMARY: DATES: Effective May 14, 1967. ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 67-14-05 BRITISH AIRCRAFT: Amdt. 39-398 Part 39 Federal Register April 14, 1967. Applies to Model BAC 1-11 200 Series Airplanes. Compliance required as indicated. To prevent fatigue failure of the nose landing gear steering jack cylinder gland nut, accomplish the following: (a) Replace aluminum alloy gland nuts P/N AB44-229 having less than 4,900 hours' time in service on the effective date of this AD with unused aluminum alloy gland nuts of the same part number or with steel gland nuts P/N AB44-1793, before the accumulation of 5,000 hours' time in service. (b) Replace aluminum alloy gland nuts P/N AB44-229 having 4,900 or more hours' time in service on the effective date of this AD with unused aluminum alloy gland nuts having the same part number or with steel gland nuts P/N AB44-1793, within the next 100 hours' time in service. (c) Aluminum alloy gland nuts P/N AB44-229 installed as replacement parts in complying with either (a) or (b) must be replaced before the accumulation of 5,000 hours' time in service. (British Aircraft Corporation (BAC) One-Eleven Alert Service Bulletin 32-A-PM 2496 pertains to this subject.) This directive effective May 14, 1967. FOOTER:
Document Text
Show stored source text (verify against official source)
AD Final Rules - DRS_67-14-05.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 67-14-05 Document Type: AD Final Rules Docket Number: Unknown Subject Heading: Airworthiness Directives; BRITISH AIRCRAFT Model BAC 1-11 200 Series Airplanes Subject: Nose Gear Steering Cylinder Gland Nut Status: Current Citation: This information is not available. Citation Publish Date: Effective Date: 05/14/1967 Make: Airbus SAS Model: BAC 1-11 200 Series 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: 67-14-05 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: Unknown AMENDMENT: 39-398 AD NUMBER: 67-14-05 SUBJECT HEADING: Airworthiness Directives; BRITISH AIRCRAFT Model BAC 1-11 200 Series Airplanes ACTION: SUMMARY: DATES: Effective May 14, 1967. ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 67-14-05 BRITISH AIRCRAFT: Amdt. 39-398 Part 39 Federal Register April 14, 1967. Applies to Model BAC 1-11 200 Series Airplanes. Compliance required as indicated. To prevent fatigue failure of the nose landing gear steering jack cylinder gland nut, accomplish the following: (a) Replace aluminum alloy gland nuts P/N AB44-229 having less than 4,900 hours' time in service on the effective date of this AD with unused aluminum alloy gland nuts of the same part number or with steel gland nuts P/N AB44-1793, before the accumulation of 5,000 hours' time in service. (b) Replace aluminum alloy gland nuts P/N AB44-229 having 4,900 or more hours' time in service on the effective date of this AD with unused aluminum alloy gland nuts having the same part number or with steel gland nuts P/N AB44-1793, within the next 100 hours' time in service. (c) Aluminum alloy gland nuts P/N AB44-229 installed as replacement parts in complying with either (a) or (b) must be replaced before the accumulation of 5,000 hours' time in service. (British Aircraft Corporation (BAC) One-Eleven Alert Service Bulletin 32-A-PM 2496 pertains to this subject.) This directive effective May 14, 1967. FOOTER:
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