AD 83-24-04
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Airbus SAS | BAC 1-11 200 Series | Airworthiness Directives; BRITISH AEROSPACE Model BAC 1-11 200 and 400 Series Airplanes |
| aircraft | Airbus SAS | BAC 1-11 400 Series | Airworthiness Directives; BRITISH AEROSPACE Model BAC 1-11 200 and 400 Series Airplanes |
Unsafe Condition
Collapse of the nose landing gear due to failure of Tonks spring discs (P/N AK43-1283), Terry discs (P/N AB43-2579), and Spring Master discs (P/N AB43-2745).
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Required Actions
Replace Tonks spring discs prior to specified landing limits. Functionally test discs in accordance with Service Bulletin 32-A-PM5191. Replace Terry and Spring Master discs before their respective landing limits. Conduct recurring functional tests at intervals not exceeding 500 landings until replacement. Incorporate helical coil springs via BAe Modification 32-PM5191 to terminate AD.
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Compliance Time
Accomplish actions prior to specified landing limits or within 500 landings after January 9, 1984, whichever comes later. Testing must occur prior to specified landing milestones or within 500 landings after the effective date, whichever comes later.
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Affected Aircraft
British Aerospace Model BAC 1-11 200 and 400 Series airplanes, all serial numbers, certificated in all categories.
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Federal Register Abstract
Nose Landing Gear
Applicability Source Text
Show captured applicability text from the source AD
AD Final Rules - DRS_83-24-04.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 83-24-04 Document Type: AD Final Rules Docket Number: Unknown Subject Heading: Airworthiness Directives; BRITISH AEROSPACE Model BAC 1-11 200 and 400 Series Airplanes Subject: Nose Landing Gear Status: Current Citation: This information is not available. Citation Publish Date: Effective Date: 01/09/1984 Make: Airbus SAS Model: BAC 1-11 200 Series | BAC 1-11 400 Series Product Type: Aircraft Product Subtype: Large Airplane Affected AD: Superseded AD: Affected By: Superseded By: Service/Office: Office of Primary Responsibility: CFR Part Reference: Part 39 Comments: AIRWORTHINESS DIRECTIVES FINAL RULES: 83-24-04 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: Unknown AMENDMENT: 39-4776 AD NUMBER: 83-24-04 SUBJECT HEADING: Airworthiness Directives; BRITISH AEROSPACE Model BAC 1-11 200 and 400 Series Airplanes ACTION: SUMMARY: DATES: Effective January 9, 1984. ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 83-24-04 BRITISH AEROSPACE: Amendment 39-4776. Applies to Model BAC 1-11 200 and 400 series airplanes, certificated in all categories. To prevent collapse of the nose landing gear, accomplish the following, unless previously accomplished: A. For pre-modification PM5766 up/down lock jacks: (1) Tonks spring discs - P/N AK43-1283. (i) Must be replaced prior to the accumulation of 4,000 landings or within 500 landings after the effective date of this AD, whichever comes later. (ii) Must be functionally tested in accordance with paragraphs 2.3 and 2.4 of Service Bulletin 32-A-PM5191, Issue 5, dated May 15, 1981, prior to the accumulation of 4,000 landings or within 100 landings after the effective date of this AD, whichever comes later. (2) Terry discs - P/N AB43-2579 and Spring Master discs - P/N AB43-2745: (i) Must be replaced prior to the accumulation of 8,000 landings or within 500 landings after the effective date of this AD, whichever comes later. (ii) Must be functionally tested in accordance with paragraphs 2.3 and 2.4 of the service bulletin prior to the accumulation of 6,000 landings or within 500 landings after the effective date of this AD, whichever comes later; and thereafter at intervals not to exceed 500 landings, until replaced in accordance with paragraph A(2)(i), above. B. For post-modification PM5766 up/down lock jacks: (1) Tonks spring discs - P/N AK43-1283. (i) Must be replaced prior to the accumulation of 8,000 landings or within 500 landings after the effective date of this AD, whichever comes later. (ii) Must be functionally tested in accordance with paragraphs 2.3 and 2.4 of the service bulletin prior to the accumulation of 4,000 landings or within 500 landings after the effective date of this AD, whichever comes later; and thereafter at intervals not to exceed 500 landings, until replaced in accordance with paragraph B(1)(i), above. (2) Terry discs - P/N AB43-2579 and Spring Master Discs - P/N AB43- 2745. (i) Must be replaced prior to the accumulation of 10,000 landings or within 500 landings after the effective date of this AD, whichever comes later. (ii) Must be functionally tested in accordance with paragraphs 2.3 and 2.4 of the service bulletin prior to the accumulation of 8,000 landings or within 500 landings after the effective date of this AD, whichever comes later; and thereafter at intervals not to exceed 500 landings, until replaced in accordance with paragraph B(2)(i), above. C. Terminating action for this AD is accomplished by incorporation of helical coil springs into the up/down lock jack, BAe Modification 32-PM5191. D. For the purpose of complying with this AD, subject to acceptance by the assigned FAA maintenance inspector, the number of landings may be determined by dividing each airplane's hours time in service by the operator's fleet average time from takeoff to landing for the airplane type. E. Alternate means of compliance which provide an equivalent level of safety may be used when approved by the Manager, Seattle Aircraft Certification Office, FAA, Northwest Mountain Region. F. Special flight permits may be issued in accordance with FAR 21.197 and 21.199 to operate airplanes to a base for the accomplishment of inspections and/or modifications required by this AD. This amendment becomes effective January 9, 1984. FOOTER:
Document Text
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AD Final Rules - DRS_83-24-04.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 83-24-04 Document Type: AD Final Rules Docket Number: Unknown Subject Heading: Airworthiness Directives; BRITISH AEROSPACE Model BAC 1-11 200 and 400 Series Airplanes Subject: Nose Landing Gear Status: Current Citation: This information is not available. Citation Publish Date: Effective Date: 01/09/1984 Make: Airbus SAS Model: BAC 1-11 200 Series | BAC 1-11 400 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: 83-24-04 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: Unknown AMENDMENT: 39-4776 AD NUMBER: 83-24-04 SUBJECT HEADING: Airworthiness Directives; BRITISH AEROSPACE Model BAC 1-11 200 and 400 Series Airplanes ACTION: SUMMARY: DATES: Effective January 9, 1984. ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 83-24-04 BRITISH AEROSPACE: Amendment 39-4776. Applies to Model BAC 1-11 200 and 400 series airplanes, certificated in all categories. To prevent collapse of the nose landing gear, accomplish the following, unless previously accomplished: A. For pre-modification PM5766 up/down lock jacks: (1) Tonks spring discs - P/N AK43-1283. (i) Must be replaced prior to the accumulation of 4,000 landings or within 500 landings after the effective date of this AD, whichever comes later. (ii) Must be functionally tested in accordance with paragraphs 2.3 and 2.4 of Service Bulletin 32-A-PM5191, Issue 5, dated May 15, 1981, prior to the accumulation of 4,000 landings or within 100 landings after the effective date of this AD, whichever comes later. (2) Terry discs - P/N AB43-2579 and Spring Master discs - P/N AB43-2745: (i) Must be replaced prior to the accumulation of 8,000 landings or within 500 landings after the effective date of this AD, whichever comes later. (ii) Must be functionally tested in accordance with paragraphs 2.3 and 2.4 of the service bulletin prior to the accumulation of 6,000 landings or within 500 landings after the effective date of this AD, whichever comes later; and thereafter at intervals not to exceed 500 landings, until replaced in accordance with paragraph A(2)(i), above. B. For post-modification PM5766 up/down lock jacks: (1) Tonks spring discs - P/N AK43-1283. (i) Must be replaced prior to the accumulation of 8,000 landings or within 500 landings after the effective date of this AD, whichever comes later. (ii) Must be functionally tested in accordance with paragraphs 2.3 and 2.4 of the service bulletin prior to the accumulation of 4,000 landings or within 500 landings after the effective date of this AD, whichever comes later; and thereafter at intervals not to exceed 500 landings, until replaced in accordance with paragraph B(1)(i), above. (2) Terry discs - P/N AB43-2579 and Spring Master Discs - P/N AB43- 2745. (i) Must be replaced prior to the accumulation of 10,000 landings or within 500 landings after the effective date of this AD, whichever comes later. (ii) Must be functionally tested in accordance with paragraphs 2.3 and 2.4 of the service bulletin prior to the accumulation of 8,000 landings or within 500 landings after the effective date of this AD, whichever comes later; and thereafter at intervals not to exceed 500 landings, until replaced in accordance with paragraph B(2)(i), above. C. Terminating action for this AD is accomplished by incorporation of helical coil springs into the up/down lock jack, BAe Modification 32-PM5191. D. For the purpose of complying with this AD, subject to acceptance by the assigned FAA maintenance inspector, the number of landings may be determined by dividing each airplane's hours time in service by the operator's fleet average time from takeoff to landing for the airplane type. E. Alternate means of compliance which provide an equivalent level of safety may be used when approved by the Manager, Seattle Aircraft Certification Office, FAA, Northwest Mountain Region. F. Special flight permits may be issued in accordance with FAR 21.197 and 21.199 to operate airplanes to a base for the accomplishment of inspections and/or modifications required by this AD. This amendment becomes effective January 9, 1984. FOOTER:
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