AD 75-16-15

final rule

Airworthiness Directives; BRITISH AIRCRAFT CORPORATION Model BAC 1-11, 200 and 400 Series Airplanes

AD Number
75-16-15
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Unknown
FR Citation
This information is not available.

Applicability

TypeManufacturerModelDetails
aircraft Airbus SAS BAC 1-11 200 Series Airworthiness Directives; BRITISH AIRCRAFT CORPORATION Model BAC 1-11, 200 and 400 Series Airplanes
aircraft Airbus SAS BAC 1-11 400 Series Airworthiness Directives; BRITISH AIRCRAFT CORPORATION Model BAC 1-11, 200 and 400 Series Airplanes

Unsafe Condition

Failure of the handbrake control valve filter housing, P/N ACM.23102, due to hydraulic fluid leakage and distortion.

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

Required Actions

Inspect the filter housing for hydraulic fluid leakage and distortion at specified intervals. Remove the handbrake control valve from service if leakage or distortion is found. Replace with serviceable valves meeting specified landing limits or modified with strengthened filter housing P/N ACM.27656.

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

Compliance Time

Prior to the accumulation of 7,000 total landings, or within the next 25 landings after the effective date of this AD, whichever occurs later. For unmodified valves, prior to 9,500 total landings or within 500 landings after the effective date. For modified valves, prior to 12,000 total landings or within 500 landings after the effective date.

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

Affected Aircraft

BRITISH AIRCRAFT CORPORATION Model BAC 1-11 200 and 400 Series airplanes except those modified with Dunlop Modification C.1559 part (b) incorporating filter housing P/N ACM.27656.

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

Federal Register Abstract

Handbrake Control Valves

Applicability Source Text

Show captured applicability text from the source AD
AD Final Rules - DRS_75-16-15.html
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AD Number:
75-16-15
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; BRITISH AIRCRAFT CORPORATION Model BAC 1-11, 200 and 400 Series Airplanes
Subject:
Handbrake Control Valves
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
08/28/1975
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: 75-16-15
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-2288

AD NUMBER:   75-16-15

SUBJECT HEADING:   Airworthiness Directives; BRITISH AIRCRAFT CORPORATION Model BAC 1-11, 200 and 400 Series Airplanes

ACTION:  

SUMMARY:  

DATES:   Effective August 28, 1975.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
75-16-15 BRITISH AIRCRAFT CORPORATION: Amendment 39-2288. Applies to BAC Model 1-11, 200 and 400 Series airplanes, except those which have been modified in accordance with Dunlop Modification C.1559, part (b) to incorporate the strengthened filter housing, P/N ACM.27656.

Compliance is required as indicated.

To prevent failure of the handbrake control valve filter housing, accomplish the following:

(a) For handbrake control valves, P/N AC 61772, prior to the accumulation of 7,000 total landings, or within the next 25 landings after the effective date of this AD, whichever occurs later, unless already accomplished within the last 350 landings -

(1) Clean the filter housing on the handbrake control valve, P/N AC 61772;

(2) With the No 2 hydraulic system pressurized to 3,000 psi, inspect the face of the filter housing, P/N ACM. 23102 for hydraulic fluid leakage and distortion; and

(3) If leakage or distortion is found, before further flight, remove the handbrake control valve from service and comply with paragraph (d).

(b) For handbrake control valves, P/N AC 61772, except those which have been modified in accordance with Dunlop Modification C.1559, part (a), prior to the accumulation of 9,500 total landings, or within the next 500 landings after the effective date of this AD, whichever occurs later, remove the handbrake control valve from service, and comply with paragraph (d).

(c) For handbrake control valves, P/N AC 61772, which have been modified in accordance with Dunlop Modification C.1559, part (a), prior to the accumulation of 12,000 total landings (including landings before modification), or within the next 500 landings after the effective date of this AD, whichever occurs later, remove the handbrake control valve from service, and comply with paragraph (d).

(d) Replace handbrake control valves removed as a result of the action required by paragraphs (a)(3), (b), or (c) of this AD with any of the following:

(1) Serviceable handbrake control valves, P/N AC 61772, which have accumulated less than 9,500 landings since new and continue to comply with paragraphs (a) and (b);

(2) Serviceable handbrake control valves, P/N AC 61772, which have been modified in accordance with Dunlop Modification C.1559, part (a) and have accumulated less than 12,000 landings since new and continue to comply with paragraphs (a) and (c); or

(3) Serviceable handbrake control valves, P/N AC 61772, which have had the old type filter housing, P/N ACM. 23102 replaced with the new strengthened filter housing, P/N ACM. 27656 in accordance with Dunlop Modification C.1559, part (b).

(e) 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 BAC 1-11 airplane.

(Dunlop Alert Service Bulletin No. 29-A131, dated December 16, 1971, Dunlop Service Bulletin No. 29-131, dated December 20, 1971; and Revision 1, dated January 7, 1972; and BAC 1-11 Alert Service Bulletin No. 32-A-PM 5102, dated July 14, 1972, cover this same subject).

This amendment becomes effective August 28, 1975.

FOOTER:

Document Text

Show stored source text (verify against official source)
AD Final Rules - DRS_75-16-15.html
Copy URL
Print/Save as PDF
Document Versions
 Feedback
Details
AD Number:
75-16-15
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; BRITISH AIRCRAFT CORPORATION Model BAC 1-11, 200 and 400 Series Airplanes
Subject:
Handbrake Control Valves
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
08/28/1975
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: 75-16-15
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-2288

AD NUMBER:   75-16-15

SUBJECT HEADING:   Airworthiness Directives; BRITISH AIRCRAFT CORPORATION Model BAC 1-11, 200 and 400 Series Airplanes

ACTION:  

SUMMARY:  

DATES:   Effective August 28, 1975.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
75-16-15 BRITISH AIRCRAFT CORPORATION: Amendment 39-2288. Applies to BAC Model 1-11, 200 and 400 Series airplanes, except those which have been modified in accordance with Dunlop Modification C.1559, part (b) to incorporate the strengthened filter housing, P/N ACM.27656.

Compliance is required as indicated.

To prevent failure of the handbrake control valve filter housing, accomplish the following:

(a) For handbrake control valves, P/N AC 61772, prior to the accumulation of 7,000 total landings, or within the next 25 landings after the effective date of this AD, whichever occurs later, unless already accomplished within the last 350 landings -

(1) Clean the filter housing on the handbrake control valve, P/N AC 61772;

(2) With the No 2 hydraulic system pressurized to 3,000 psi, inspect the face of the filter housing, P/N ACM. 23102 for hydraulic fluid leakage and distortion; and

(3) If leakage or distortion is found, before further flight, remove the handbrake control valve from service and comply with paragraph (d).

(b) For handbrake control valves, P/N AC 61772, except those which have been modified in accordance with Dunlop Modification C.1559, part (a), prior to the accumulation of 9,500 total landings, or within the next 500 landings after the effective date of this AD, whichever occurs later, remove the handbrake control valve from service, and comply with paragraph (d).

(c) For handbrake control valves, P/N AC 61772, which have been modified in accordance with Dunlop Modification C.1559, part (a), prior to the accumulation of 12,000 total landings (including landings before modification), or within the next 500 landings after the effective date of this AD, whichever occurs later, remove the handbrake control valve from service, and comply with paragraph (d).

(d) Replace handbrake control valves removed as a result of the action required by paragraphs (a)(3), (b), or (c) of this AD with any of the following:

(1) Serviceable handbrake control valves, P/N AC 61772, which have accumulated less than 9,500 landings since new and continue to comply with paragraphs (a) and (b);

(2) Serviceable handbrake control valves, P/N AC 61772, which have been modified in accordance with Dunlop Modification C.1559, part (a) and have accumulated less than 12,000 landings since new and continue to comply with paragraphs (a) and (c); or

(3) Serviceable handbrake control valves, P/N AC 61772, which have had the old type filter housing, P/N ACM. 23102 replaced with the new strengthened filter housing, P/N ACM. 27656 in accordance with Dunlop Modification C.1559, part (b).

(e) 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 BAC 1-11 airplane.

(Dunlop Alert Service Bulletin No. 29-A131, dated December 16, 1971, Dunlop Service Bulletin No. 29-131, dated December 20, 1971; and Revision 1, dated January 7, 1972; and BAC 1-11 Alert Service Bulletin No. 32-A-PM 5102, dated July 14, 1972, cover this same subject).

This amendment becomes effective August 28, 1975.

FOOTER:

Source: Official FAA Source ↗

Retrieved: Apr 8, 2026

Rights: U.S. Government Public Domain

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