AD 47-33-03

final rule

Airworthiness Directives; Beech Models AT-11 and C18S Airplanes

AD Number
47-33-03
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Unknown
FR Citation
This information is not available.
Technical illustration of a riveted aircraft structural panel and frame
Problem area Airframe structure

Applicability

TypeManufacturerModelDetails
aircraft Textron Aviation Inc. Army AT-11 Airworthiness Directives; Beech Models AT-11 and C18S Airplanes
aircraft Textron Aviation Inc. C18S Airworthiness Directives; Beech Models AT-11 and C18S Airplanes

Unsafe Condition

The absence of proper drain holes in the tail cone and fuselage bulkhead No. 15 may lead to inadequate drainage, potentially causing corrosion or structural damage.

AI-generated summary from the source AD text. Verify against the official source before acting.

Required Actions

Add two drain holes in the tail cone and two 1/4-inch drain holes in fuselage bulkhead No. 15 as specified in Figure 2. Compliance with Beech Service Bulletin No. C18-7 is acceptable.

AI-generated summary from the source AD text. Verify against the official source before acting.

Compliance Time

prior to certification or, if certificated, on next periodic inspection but not later than November 1, 1947

AI-generated summary from the source AD text. Verify against the official source before acting.

Affected Aircraft

Textron Aviation Inc. Models AT-11 and C18S

AI-generated summary from the source AD text. Verify against the official source before acting.

Federal Register Abstract

Tail Cone Drain Holes

Applicability Source Text

Show captured applicability text from the source AD
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Details
AD Number:
47-33-03
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; Beech Models AT-11 and C18S Airplanes
Subject:
Tail Cone Drain Holes
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
Make:
Textron Aviation Inc.
Model:
Army AT-11 | C18S
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Superseded AD: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Superseded By: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: 47-33-03
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:  

AD NUMBER:   47-33-03

SUBJECT HEADING:   Airworthiness Directives; Beech Models AT-11 and C18S Airplanes

ACTION:  

SUMMARY:  

DATES:  

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
47-33-03 BEECH: (Was Mandatory Note 5 of AD-757-2 and Mandatory Note 4 of AD- 582-2.) Applies to AT-11 and C18S Aircraft.

To be accomplished prior to certification or, if certificated, on next periodic inspection but not later than November 1, 1947.

In order to provide better tail cone drainage, add two drain holes in the tail cone and two 1/4-inch drain holes in the fuselage bulkhead No. 15 as shown in Figure 2.



(Beech Service Bulletin No. C18-7 covers this same subject.)

FOOTER:

Document Text

Show stored source text (verify against official source)
AD Final Rules - DRS_47-33-03.html
Copy URL
Print/Save as PDF
Document Versions
 Feedback
Details
AD Number:
47-33-03
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; Beech Models AT-11 and C18S Airplanes
Subject:
Tail Cone Drain Holes
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
Make:
Textron Aviation Inc.
Model:
Army AT-11 | C18S
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: 47-33-03
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:  

AD NUMBER:   47-33-03

SUBJECT HEADING:   Airworthiness Directives; Beech Models AT-11 and C18S Airplanes

ACTION:  

SUMMARY:  

DATES:  

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
47-33-03 BEECH: (Was Mandatory Note 5 of AD-757-2 and Mandatory Note 4 of AD- 582-2.) Applies to AT-11 and C18S Aircraft.

To be accomplished prior to certification or, if certificated, on next periodic inspection but not later than November 1, 1947.

In order to provide better tail cone drainage, add two drain holes in the tail cone and two 1/4-inch drain holes in the fuselage bulkhead No. 15 as shown in Figure 2.



(Beech Service Bulletin No. C18-7 covers this same subject.)

FOOTER:

Source: Official FAA Source ↗

Retrieved: Apr 8, 2026

Rights: U.S. Government Public Domain

This site is not affiliated with or endorsed by the FAA. Always verify with official sources.