AD 46-13-05

AD Final Rules - DRS_46-13-05.html
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AD Number:
46-13-05
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
DOUGLAS Model DC3 Aircraft
Subject:
Control Boot Assemblies
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
Make:
The Boeing Company
Model:
DC3-G102 | DC3-G102A | DC3-G103A | DC3-G202A | DC3A-S1C3G | DC3A-S1CG | DC3A-S4C4G | DC3A-SC3G | DC3...Show more
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Superseded AD: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Superseded By: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: 46-13-05
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:  

AD NUMBER:   46-13-05

SUBJECT HEADING:   DOUGLAS Model DC3 Aircraft

ACTION:  

SUMMARY:  

DATES:  

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
46-13-05 DOUGLAS: (Was Mandatory Note 10 of AD-618-3 and Mandatory Note 12 of AD-669-3.) Applies to All DC3 Aircraft.

To be accomplished not later than April 1, 1947.

Replace all canvas control boot assemblies either with the new rubber control column boot assemblies of the same part number (No. 5035184-16 and -17), as called for on Douglas Service Bulletin No. 231, or with the following boot assemblies:

(a) Thompson Co. (H.I. Thompson Co., 1733 Cordova St., Los Angeles 7, Calif.), No. 11-21001, change B, for Models DC3-C/C-47 and DC-3-D/C117A.

(b) Thompson Co. No. 11-21002, change A, for Model DC3.

(c) American Airlines Drawing No. CDS-6132.

Pending replacement, the canvas boots should be inspected prior to each flight to determine that the top of the boot is tight around the control assembly and the pocket around the base is eliminated.


FOOTER: