AD 76-07-11

final rule

Airworthiness Directives; Alexander Schleicher Model ASW-17 Gliders

AD Number
76-07-11
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Unknown
FR Citation
This information is not available.
Technical illustration of an aircraft flight control surface and actuator
Problem area Flight controls

Applicability

TypeManufacturerModelDetails
aircraft Alexander Schleicher GmbH & Co. ASW 17 Airworthiness Directives; Alexander Schleicher Model ASW-17 Gliders

Unsafe Condition

Water ballast system control leakage into the fuselage area could result in a loss of elevator control.

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

Required Actions

Install a placard prohibiting water ballast system use before further flight. Within 10 hours time in service, install 25 mm hose clamps on PVC hoses securing them to brass tubes, inspect clamps by exerting a 10 pound pull, and replace any loose clamps with new ones followed by re-inspection.

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

Compliance Time

Before further flight and within the next 10 hours time in service after the effective date of this AD.

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

Affected Aircraft

Alexander Schleicher GmbH & Co. Model ASW 17 gliders, Serial Numbers 17001 through 17043.

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

Federal Register Abstract

Water Ballast System Control

Applicability Source Text

Show captured applicability text from the source AD
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Details
AD Number:
76-07-11
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; Alexander Schleicher Model ASW-17 Gliders
Subject:
Water Ballast System Control
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
04/22/1976
Make:
Alexander Schleicher GmbH & Co.
Model:
ASW 17
Product Type:
Aircraft
Product Subtype:
Glider
Affected AD:
Superseded AD:
Affected By:
Superseded By:
Service/Office:
Office of Primary Responsibility:
CFR Part Reference:
Part 39
Comments:
AIRWORTHINESS DIRECTIVES FINAL RULES: 76-07-11
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-2572

AD NUMBER:   76-07-11

SUBJECT HEADING:   Airworthiness Directives; Alexander Schleicher Model ASW-17 Gliders

ACTION:  

SUMMARY:  

DATES:   Effective April 22, 1976.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:   76-07-11 ALEXANDER SCHLEICHER: Amendment 39-2572. Applies to Model ASW-17 gliders, Serial Numbers 17001 through 17043, certificated in all categories.

Compliance is required as indicated.

To prevent water ballast from leaking into the fuselage area which could result in a loss of elevator control, accomplish the following:

(a) Before further flight, install a placard in the vicinity of the water ballast system control to read as follows: "USE OF WATER BALLAST SYSTEM PROHIBITED."

(b) Within the next 10 hours time in service after the effective date of this AD, unless already accomplished, comply with the following:

(1) Install a standard 25 mm (1 inch) diameter hose clamp on each of the two polyvinylchloride (PVC) hoses to secure the two PVC hoses to the brass tubes that feed the water ballast exhausts which are located at the bottom of the fuselage behind the landing gear.

(2) Inspect for clamp security by exerting a 10 pound pull on each PVC hose after securing clamps.

(3) Install new clamps in place of those clamps which come loose following the inspection required by paragraph (b)(2) of this AD and inspect the replacement clamps in accordance with paragraph (b)(2) of this AD.

(c) Upon compliance with paragraph (b) of this AD, the placard required by paragraph (a) of this AD may be removed.

This amendment becomes effective April 22, 1976.

FOOTER:

Document Text

Show stored source text (verify against official source)
AD Final Rules - DRS_76-07-11.html
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Print/Save as PDF
Document Versions
 Feedback
Details
AD Number:
76-07-11
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; Alexander Schleicher Model ASW-17 Gliders
Subject:
Water Ballast System Control
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
04/22/1976
Make:
Alexander Schleicher GmbH & Co.
Model:
ASW 17
Product Type:
Aircraft
Product Subtype:
Glider
Affected AD:
Superseded AD:
Affected By:
Superseded By:
Service/Office:
Office of Primary Responsibility:
CFR Part Reference:
Part 39
Comments:
AIRWORTHINESS DIRECTIVES FINAL RULES: 76-07-11
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-2572

AD NUMBER:   76-07-11

SUBJECT HEADING:   Airworthiness Directives; Alexander Schleicher Model ASW-17 Gliders

ACTION:  

SUMMARY:  

DATES:   Effective April 22, 1976.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:   76-07-11 ALEXANDER SCHLEICHER: Amendment 39-2572. Applies to Model ASW-17 gliders, Serial Numbers 17001 through 17043, certificated in all categories.

Compliance is required as indicated.

To prevent water ballast from leaking into the fuselage area which could result in a loss of elevator control, accomplish the following:

(a) Before further flight, install a placard in the vicinity of the water ballast system control to read as follows: "USE OF WATER BALLAST SYSTEM PROHIBITED."

(b) Within the next 10 hours time in service after the effective date of this AD, unless already accomplished, comply with the following:

(1) Install a standard 25 mm (1 inch) diameter hose clamp on each of the two polyvinylchloride (PVC) hoses to secure the two PVC hoses to the brass tubes that feed the water ballast exhausts which are located at the bottom of the fuselage behind the landing gear.

(2) Inspect for clamp security by exerting a 10 pound pull on each PVC hose after securing clamps.

(3) Install new clamps in place of those clamps which come loose following the inspection required by paragraph (b)(2) of this AD and inspect the replacement clamps in accordance with paragraph (b)(2) of this AD.

(c) Upon compliance with paragraph (b) of this AD, the placard required by paragraph (a) of this AD may be removed.

This amendment becomes effective April 22, 1976.

FOOTER:

Source: Official FAA Source ↗

Retrieved: Apr 8, 2026

Rights: U.S. Government Public Domain

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