AD 75-16-19

final rule

Airworthiness Directives; Flug-und Fahrzeugwerke A.G. Model Diamant HBV and Diamant 16.5 Gliders

AD Number
75-16-19
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 Flug- und Fahrzeugwerke Ag Diamant 16.5 Airworthiness Directives; Flug-und Fahrzeugwerke A.G. Model Diamant HBV and Diamant 16.5 Gliders
aircraft Flug- und Fahrzeugwerke Ag HBV Diamant Airworthiness Directives; Flug-und Fahrzeugwerke A.G. Model Diamant HBV and Diamant 16.5 Gliders

Unsafe Condition

Rudder jamming due to insufficient fin fairing overlap of the rudder nose.

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

Required Actions

Visually inspect and measure the fin fairing overlap of the rudder nose for right full rudder to ensure an overlap of more than 0.4 in. (10 mm). If overlap is insufficient, modify the rudder nose by bonding fiberglass strips in accordance with Service Bulletin No.2 or FAA-approved equivalent.

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

Compliance Time

within 25 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

Flug-und Fahrzeugwerke A.G. Diamant HBV gliders (all serial numbers) and Diamant 16.5 gliders (S/N 011 through 069 except 030, 031, 036, 058, 067, and 068)

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

Federal Register Abstract

Rudder Jamming

Applicability Source Text

Show captured applicability text from the source AD
AD Final Rules - DRS_75-16-19.html
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AD Number:
75-16-19
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; Flug-und Fahrzeugwerke A.G. Model Diamant HBV and Diamant 16.5 Gliders
Subject:
Rudder Jamming
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
08/12/1975
Make:
Flug- und Fahrzeugwerke Ag
Model:
Diamant 16.5 | HBV Diamant
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Superseded AD: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Superseded By: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: 75-16-19
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-2293

AD NUMBER:   75-16-19

SUBJECT HEADING:   Airworthiness Directives; Flug-und Fahrzeugwerke A.G. Model Diamant HBV and Diamant 16.5 Gliders

ACTION:  

SUMMARY:  

DATES:   Effective August 12, 1975.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
75-16-19 FLUG-und FAHRZEUGWERKE A.G.: Amendment 39-2293. Applies to Diamant HBV gliders, all serial numbers, and Diamant 16.5 gliders, S/N 011 through 069, except 030, 031, 036, 058, 067, and 068, certificated in all categories.

Compliance is required within 25 hours' time in service after the effective date of this AD, unless already accomplished.

To prevent jamming of the rudder, accomplish the following:

(a) Visually inspect and measure the fin fairing overlap of the rudder nose for right full rudder to assure an overlap of more than 0.4 inc. (10 mm) in accordance with Flug-und Fahrzeugwerke A.G. Service Bulletin No.2, dated May 15, 1970, or an FAA-approved equivalent.

(b) If fin fairing overlap measured in accordance with paragraph (a) of this AD is less than 0.4 in. (10 mm), modify (lengthen) the rudder nose by bonding fiberglass strips to the nose in accordance with Flug-und Fahrzeugwerke A.G. Service Bulletin No.2, dated May 15, 1970, or an FAA-approved equivalent.

This amendment becomes effective August 12, 1975.

FOOTER:

Document Text

Show stored source text (verify against official source)
AD Final Rules - DRS_75-16-19.html
Copy URL
Print/Save as PDF
Document Versions
 Feedback
Details
AD Number:
75-16-19
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; Flug-und Fahrzeugwerke A.G. Model Diamant HBV and Diamant 16.5 Gliders
Subject:
Rudder Jamming
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
08/12/1975
Make:
Flug- und Fahrzeugwerke Ag
Model:
Diamant 16.5 | HBV Diamant
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: 75-16-19
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-2293

AD NUMBER:   75-16-19

SUBJECT HEADING:   Airworthiness Directives; Flug-und Fahrzeugwerke A.G. Model Diamant HBV and Diamant 16.5 Gliders

ACTION:  

SUMMARY:  

DATES:   Effective August 12, 1975.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
75-16-19 FLUG-und FAHRZEUGWERKE A.G.: Amendment 39-2293. Applies to Diamant HBV gliders, all serial numbers, and Diamant 16.5 gliders, S/N 011 through 069, except 030, 031, 036, 058, 067, and 068, certificated in all categories.

Compliance is required within 25 hours' time in service after the effective date of this AD, unless already accomplished.

To prevent jamming of the rudder, accomplish the following:

(a) Visually inspect and measure the fin fairing overlap of the rudder nose for right full rudder to assure an overlap of more than 0.4 inc. (10 mm) in accordance with Flug-und Fahrzeugwerke A.G. Service Bulletin No.2, dated May 15, 1970, or an FAA-approved equivalent.

(b) If fin fairing overlap measured in accordance with paragraph (a) of this AD is less than 0.4 in. (10 mm), modify (lengthen) the rudder nose by bonding fiberglass strips to the nose in accordance with Flug-und Fahrzeugwerke A.G. Service Bulletin No.2, dated May 15, 1970, or an FAA-approved equivalent.

This amendment becomes effective August 12, 1975.

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.