AD 77-16-08

final rule

Airworthiness Directives; Eiriavion Oy (Formerly Molino Oy) Model PIK-20D Sailplanes

AD Number
77-16-08
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 Eiriavion Oy PIK-20D Airworthiness Directives; Eiriavion Oy (Formerly Molino Oy) Model PIK-20D Sailplanes

Unsafe Condition

Separation of wing upper panel spar cap and wing main spar shear web.

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

Required Actions

Replace wing panels with new serviceable replacements, repair existing panels per appendix 1 of Eiriavion Service Bulletin No. M 17 at an authorized repair facility, or use an approved alternate means of compliance.

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

Compliance Time

before further flight

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

Affected Aircraft

Eiriavion Oy Model PIK-20D sailplanes with serial numbers 20510 through 20532, 20534 through 20540, 20542 through 20544, 20546, 20548, 20552, 20555, and 20556.

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

Federal Register Abstract

Wing Panels

Applicability Source Text

Show captured applicability text from the source AD
AD Final Rules - DRS_77-16-08.html
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AD Number:
77-16-08
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; Eiriavion Oy (Formerly Molino Oy) Model PIK-20D Sailplanes
Subject:
Wing Panels
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
08/08/1977
Make:
Eiriavion Oy
Model:
PIK-20D
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Superseded AD: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Superseded By: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: 77-16-08
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-3005

AD NUMBER:   77-16-08

SUBJECT HEADING:   Airworthiness Directives; Eiriavion Oy (Formerly Molino Oy) Model PIK-20D Sailplanes

ACTION:  

SUMMARY:  

DATES:   Effective August 8, 1977.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
77-16-08 EIRIAVION OY (FORMERLY MOLINO OY): Amendment 39-3005. Applies to Model PIK-20D sailplanes with serial numbers 20510 through 20532, 20534 through 20540, 20542 through 20544, 20546, 20548, 20552, 20555, and 20556.

To prevent separation of wing upper panel spar cap and wing main spar shear web, before further flight, unless already accomplished, comply with paragraph (a), (b), or (c).

(a) Replace wing panels with new wing panels identified by the manufacturer as serviceable replacements.
(b) Repair existing wing panels in accordance with appendix 1 of Eiriavion Service Bulletin No. M 17, dated June 17, 1977, at an FAA certificated repair station that is a manufacturer's authorized repair facility. Following rebonding, visually inspect the affected area to ensure that the new resin forms a continuous bond on both sides of the wing shear web for its full length.

(c) Repair in accordance with an alternate means of compliance which must be approved by the Chief, Aircraft Certification Staff, FAA, Europe, Africa, and Middle East Region, c/o American Embassy, Brussels, Belgium.

NOTE: Copies of the applicable service bulletin are available at the following manufacturer's authorized repair facilities:


Smitty's Soaring Service
Deansboro Road Route 12B
Clinton, New York 13323

Sailplane Repair Service, Inc.
Rich Roberts
216 Commerce Drive
P.O. Box 1462
Fort Collins, Colorado 80522


This amendment is effective August 8, 1977, as to all persons except those persons to whom it was made immediately effective by the telegram dated July 7, 1977, which contained this amendment.

FOOTER:

Document Text

Show stored source text (verify against official source)
AD Final Rules - DRS_77-16-08.html
Copy URL
Print/Save as PDF
Document Versions
 Feedback
Details
AD Number:
77-16-08
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; Eiriavion Oy (Formerly Molino Oy) Model PIK-20D Sailplanes
Subject:
Wing Panels
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
08/08/1977
Make:
Eiriavion Oy
Model:
PIK-20D
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: 77-16-08
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-3005

AD NUMBER:   77-16-08

SUBJECT HEADING:   Airworthiness Directives; Eiriavion Oy (Formerly Molino Oy) Model PIK-20D Sailplanes

ACTION:  

SUMMARY:  

DATES:   Effective August 8, 1977.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
77-16-08 EIRIAVION OY (FORMERLY MOLINO OY): Amendment 39-3005. Applies to Model PIK-20D sailplanes with serial numbers 20510 through 20532, 20534 through 20540, 20542 through 20544, 20546, 20548, 20552, 20555, and 20556.

To prevent separation of wing upper panel spar cap and wing main spar shear web, before further flight, unless already accomplished, comply with paragraph (a), (b), or (c).

(a) Replace wing panels with new wing panels identified by the manufacturer as serviceable replacements.
(b) Repair existing wing panels in accordance with appendix 1 of Eiriavion Service Bulletin No. M 17, dated June 17, 1977, at an FAA certificated repair station that is a manufacturer's authorized repair facility. Following rebonding, visually inspect the affected area to ensure that the new resin forms a continuous bond on both sides of the wing shear web for its full length.

(c) Repair in accordance with an alternate means of compliance which must be approved by the Chief, Aircraft Certification Staff, FAA, Europe, Africa, and Middle East Region, c/o American Embassy, Brussels, Belgium.

NOTE: Copies of the applicable service bulletin are available at the following manufacturer's authorized repair facilities:


Smitty's Soaring Service
Deansboro Road Route 12B
Clinton, New York 13323

Sailplane Repair Service, Inc.
Rich Roberts
216 Commerce Drive
P.O. Box 1462
Fort Collins, Colorado 80522


This amendment is effective August 8, 1977, as to all persons except those persons to whom it was made immediately effective by the telegram dated July 7, 1977, which contained this amendment.

FOOTER:

Source: Official FAA Source ↗

Retrieved: Apr 8, 2026

Rights: U.S. Government Public Domain

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