AD 82-27-01

AD Final Rules - DRS_82-27-01.html
Copy URL
Print/Save as PDF
Document Versions
 Feedback
Details
AD Number:
82-27-01
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
McCAULEY ACCESSORY DIVISION Model 1A170/FFA Propellers
Subject:
Hub
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
12/30/1982
Make:
McCauley Propeller Systems
Model:
1A170
Product Type:
Propeller
Product Subtype:
Affected AD:
Superseded AD:
Affected By:
Superseded By:
Service/Office:
Office of Primary Responsibility:
CFR Part Reference:
Part 39
Comments:
AIRWORTHINESS DIRECTIVES FINAL RULES: 82-27-01
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-4520

AD NUMBER:   82-27-01

SUBJECT HEADING:   McCAULEY ACCESSORY DIVISION Model 1A170/FFA Propellers

ACTION:  

SUMMARY:  

DATES:   Effective December 30, 1982.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
82-27-01 McCAULEY ACCESSORY DIVISION: Amendment 39-4520. Applies to all McCauley Accessory Division Model 1A170/FFA fixed pitch propellers installed on, but not limited to, Gulfstream Aerospace Model AA-5B aircraft certificated in all categories.

Compliance is required as indicated, unless already accomplished.

To prevent propeller failure, accomplish the following:

(a) For propellers with 190 or more hours time in service since new or since last dye penetrant type inspection, inspect in accordance with paragraph (c) within the next 10 hours time in service and every 200 hours time in service thereafter.

(b) For propellers with less than 190 hours time in service since new or since last dye penetrant type inspection, inspect in accordance with paragraph (c) prior to the accumulation of 200 hours time in service and every 200 hours time in service thereafter.

(c) Inspection procedure:

(1) Remove propeller from the aircraft and remove spacer from the propeller.

(2) Thoroughly remove and clean all paint material down to the anodize surface and inspect the center relief bore (hole), all mounting bolt holes, and all external surfaces in the entire propeller hub area (faces and sides) for cracks using dye penetrant inspection methods.

(3) If a crack is found, replace the propeller with a serviceable propeller before further flight.

(d) A special flight permit may be issued in accordance with Federal Aviation Regulations (FARs) 21.197 and 21.199 to operate the aircraft to a base where this AD can be accomplished.

(e) Upon request of the operator, an equivalent means of compliance with the requirements of this AD may be approved by the Manager, Chicago Aircraft Certification Office, FAA, 2300 East Devon Avenue, Des Plaines, Illinois 60018.

This AD supersedes Amendment 39-3689 (45 FR 8947), AD 80-04-05.

This amendment becomes effective December 30, 1982.

FOOTER: