AD 83-24-04

final rule

Airworthiness Directives; BRITISH AEROSPACE Model BAC 1-11 200 and 400 Series Airplanes

AD Number
83-24-04
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 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).

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

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.

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

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.

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

Affected Aircraft

British Aerospace Model BAC 1-11 200 and 400 Series airplanes, all serial numbers, certificated in all categories.

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

Federal Register Abstract

Nose Landing Gear

Applicability Source Text

Show captured applicability text from the source AD
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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

Show stored source text (verify against official source)
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:

Source: Official FAA Source ↗

Retrieved: Apr 8, 2026

Rights: U.S. Government Public Domain

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