AD 67-31-03

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AD Number:
67-31-03
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; BRITISH AIRCRAFT Model BAC 1-11 200 and 400 Series Airplanes
Subject:
Reversal Of Rudder Feel Function
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
11/30/1967
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Superseded AD: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Superseded By: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: 67-31-03
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-519

AD NUMBER:   67-31-03

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

ACTION:  

SUMMARY:  

DATES:   Effective November 30, 1967.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
67-31-03 BRITISH AIRCRAFT: Amdt. 39-519, Part 39, Federal Register November 30, 1967. Applies to Model BAC 1-11 200 and 400 Series Airplanes.

Compliance required as indicated, unless already accomplished.

To prevent reversal of the rudder feel function, within the next 500 hours' time in service after the effective date of this AD, accomplish the following:

(a) Replace the paired links located in the rudder feel simulator linkage, Hobson P/N CH 504-071 or CH 504-280 with redesigned Hobson slotted links, P/N CH 504-446 in accordance with British Aircraft Corporation on BAC 1-11 Alert Service Bulletin PM 3290, or later ARB-approved issue, or an equivalent approved by the Chief, Aircraft Certification Staff, FAA, Europe, Africa, and Middle East Region.

(b) Attach Hobson slotted links P/N CH 504-446 with bolts P/N CH 127803-25 (NAS 1108-25) and CH-127803-22 (NAS 1108-22), or self-retained bolt P/N CH 127800 (NAS 1108-27-SR) and rivet P/N CH 524-129-3. If bolts P/N CH 127803-25 (NAS 1108-25) and CH 127803-22 (NAS 1108-22) are used, replace these bolts with self-retained bolt P/N CH 127800 (NAS 1108-27-SR) and rivet P/N CH-524-129-3 during the next overhaul of the rudder feel simulator units.

This amendment effective November 30, 1967.

FOOTER: