AD 75-26-04

AD Final Rules - DRS_75-26-04.html
Copy URL
Print/Save as PDF
Document Versions
 Feedback
Details
AD Number:
75-26-04
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Beech Model 200 Airplanes
Subject:
Fuel Transfer System
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
12/19/1975
Make:
Textron Aviation Inc.
Model:
200
Product Type:
Aircraft
Product Subtype:
Small/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Superseded AD: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Superseded By: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: 75-26-04
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-2458

AD NUMBER:   75-26-04

SUBJECT HEADING:   Beech Model 200 Airplanes

ACTION:  

SUMMARY:  

DATES:   Effective December 19, 1975.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
75-26-04 BEECH: Amendment 39-2458. Applies to Model 200 (BB-2 through BB-71) airplanes.

Compliance: Required as indicated, unless already accomplished.

To prevent malfunction of the fuel transfer system, within the next 50 hours' time in service after the effective date of this AD, accomplish the following:

A) Inspect the P/N 100-920067-1 fuel vent float valve for opening and operation in accordance with the criteria set forth in Beechcraft Service Instruction No. 0772-295 or later FAA-approved revision. (P/N 101-320035-1 baffle, if installed, must be removed to perform this inspection.)

B) Replace any fuel vent float valve assembly that does not meet the criteria set forth in Beechcraft Service Instruction No. 0772-295 or later FAA-approved revision with new P/N 100-920067-1 fuel vent float valve assembly.

C) Any equivalent method of compliance with this AD must be approved by the Chief, Engineering and Manufacturing Branch, FAA, Central Region.

This amendment becomes effective December 19, 1975.

FOOTER: