AD 82-13-06

AD Final Rules - DRS_82-13-06.html
Copy URL
Print/Save as PDF
Document Versions
 Feedback
Details
AD Number:
82-13-06
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; SCHWEIZER (GULFSTREAM AMERICAN-GRUMMAN) Models G-164B, G-164C, and G164D Airplanes
Subject:
Aileron Bellcrank Inspection
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
07/05/1982
Make:
Allied Ag Cat Productions, Inc.
Model:
G-164B | G-164B-15T | G-164B-20T | G-164B-34T | G-164B (with 73 inch wing gap) | G-164C | G-164D | G...Show more
Product Type:
Aircraft
Product Subtype:
Small 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Superseded AD: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Superseded By: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: 82-13-06
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-4410

AD NUMBER:   82-13-06

SUBJECT HEADING:   Airworthiness Directives; SCHWEIZER (GULFSTREAM AMERICAN-GRUMMAN) Models G-164B, G-164C, and
G164D Airplanes

ACTION:  

SUMMARY:  

DATES:   Effective July 5, 1982.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
82-13-06 SCHWEIZER (GULFSTREAM AMERICAN-GRUMMAN): Amendment 39-4410. Applies to Models G-164B (S/N 1B thru 656B), G-164C (S/N 1C thru 44C), and G164D (S/N 1D thru 16D) airplanes certificated in any category.

COMPLIANCE: Required as indicated unless already accomplished.

To detect elongation of the aileron cable attach holes and to eliminate the possibility of P/N A1450-281 bushings becoming dislodged from the aileron bellcrank, accomplish the following:

a) Within 25 hours time-in-service after the effective date of this AD and every 12 months thereafter, on airplanes not modified in accordance with Gulfstream American Service Bulletin No. 75 (either original issuance or Revision "A" dated January 25, 1980), visually inspect the aileron bellcrank for elongation of the aileron cable attach holes per Part A of the revised service bulletin. If excessive elongation is found, prior to further flight, modify or replace the aileron bellcrank in accordance with Parts B and C of the revised service bulletin.

b) Within 25 hours time-in-service after the effective date of this AD, on airplanes that have been modified in accordance with the original issue of Gulfstream American AG-CAT Service Bulletin No. 75, visually inspect the aileron bellcranks and if the bushings are loose or have less than .230 inch edge distance, replace the aileron bellcrank in accordance with Part D of Revision "A" of the Service Bulletin dated January 25, 1980.

c) The repetitive inspections required by paragraph a) of this AD may be discontinued upon accomplishing the modifications described in Parts B and C of Gulfstream American AG-CAT Service Bulletin No. 75, Revision "A", dated January 25, 1980.

d) Upon request, with substantiating data submitted through an FAA Maintenance Inspector, the compliance times specified in this AD may be adjusted by the Chief, New York Aircraft Certification Office, FAA, JFK International Airport, Jamaica, New York 11430.

e) Aircraft may be flown in accordance with FAR 21.197 to a location where this AD may be accomplished.

f) An equivalent method of compliance with this AD may be used if approved by the Chief, New York Aircraft Certification Office, FAA, JFK International Airport, Jamaica, New York 11430.

This amendment supersedes Amendment 39-3882 (44 FR 11034) AD 80-17-08, effective August 15, 1980.
This Amendment becomes effective on July 5, 1982.

FOOTER: