AD 75-23-02
final rule
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Aer-Pegaso S.p.A. | Societe C.A.R.M.A.M. | M-100 S | Airworthiness Directives; Aer Pegaso M100S and Carmam M200 Gliders |
| aircraft | Aer-Pegaso S.p.A. | Societe C.A.R.M.A.M. | M-200 | Airworthiness Directives; Aer Pegaso M100S and Carmam M200 Gliders |
Unsafe Condition
Possible structural failure of aileron spars due to cracks in the spar to the right of the central hinge.
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Required Actions
Within 10 hours' time in service after the effective date, inspect aileron spar to the right of the central hinge for cracks every 20 hours' time in service. If cracks are found, reinforce with 1.5 mm thick birch plywood plates per Carmam Drawing dated April 12, 1968, before further flight.
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Compliance Time
Within the Next 10 hours' time in service after the effective date, and thereafter at intervals not to exceed 20 hours' time in service from the last inspection
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Affected Aircraft
Aer-Pegaso S.p.A. M-100 S gliders, all serial numbers; Carmam M-200 gliders except serial number 45 and subsequent
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Federal Register Abstract
Aileron Spars
Applicability Source Text
Show captured applicability text from the source AD
AD Final Rules - DRS_75-23-02.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 75-23-02 Document Type: AD Final Rules Docket Number: Unknown Subject Heading: Airworthiness Directives; Aer Pegaso M100S and Carmam M200 Gliders Subject: Aileron Spars Status: Current Citation: This information is not available. Citation Publish Date: Effective Date: 11/14/1975 Make: Aer-Pegaso S.p.A. | Societe C.A.R.M.A.M. Model: M-100 S | M-200 Product Type: Aircraft Product Subtype: Glider Affected AD: Superseded AD: Affected By: Superseded By: Service/Office: Office of Primary Responsibility: CFR Part Reference: Part 39 Comments: AIRWORTHINESS DIRECTIVES FINAL RULES: 75-23-02 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: Unknown AMENDMENT: 39-2413 AD NUMBER: 75-23-02 SUBJECT HEADING: Airworthiness Directives; Aer Pegaso M100S and Carmam M200 Gliders ACTION: SUMMARY: DATES: Effective November 14, 1975. ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 75-23-02 AER PEGASO and CARMAM: Amendment 39-2413. Applies to Aer Pegaso M100S gliders, all serial numbers, and Carmam M200 gliders, except serial number 45 and subsequent, certificated in all categories. Compliance is required as indicated, unless already accomplished. To prevent possible structural failure of aileron spars accomplish the following: (a) Within the Next 10 hours' time in service after the effective date of this AD, and, thereafter, at intervals not to exceed 20 hours' time in service from the last inspection, visually inspect the aileron spar to the right of the central hinge for cracks. (b) If a crack is found during an inspection required by paragraph (a) of this AD, before further flight, reinforce the affected area with plates made of 1.5 mm thick birch plywood of aeronautical quality in accordance with Carmam Drawing, titled "Modification Aileron Central Part" dated April 12, 1968, or an FAA- approved equivalent. (c) Upon incorporation of the reinforcement specified in paragraph (b) of this AD, the inspections required by paragraph (a) of this AD may be discontinued. This amendment becomes effective November 14, 1975. FOOTER:
Document Text
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AD Final Rules - DRS_75-23-02.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 75-23-02 Document Type: AD Final Rules Docket Number: Unknown Subject Heading: Airworthiness Directives; Aer Pegaso M100S and Carmam M200 Gliders Subject: Aileron Spars Status: Current Citation: This information is not available. Citation Publish Date: Effective Date: 11/14/1975 Make: Aer-Pegaso S.p.A. | Societe C.A.R.M.A.M. Model: M-100 S | M-200 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: 75-23-02 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: Unknown AMENDMENT: 39-2413 AD NUMBER: 75-23-02 SUBJECT HEADING: Airworthiness Directives; Aer Pegaso M100S and Carmam M200 Gliders ACTION: SUMMARY: DATES: Effective November 14, 1975. ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 75-23-02 AER PEGASO and CARMAM: Amendment 39-2413. Applies to Aer Pegaso M100S gliders, all serial numbers, and Carmam M200 gliders, except serial number 45 and subsequent, certificated in all categories. Compliance is required as indicated, unless already accomplished. To prevent possible structural failure of aileron spars accomplish the following: (a) Within the Next 10 hours' time in service after the effective date of this AD, and, thereafter, at intervals not to exceed 20 hours' time in service from the last inspection, visually inspect the aileron spar to the right of the central hinge for cracks. (b) If a crack is found during an inspection required by paragraph (a) of this AD, before further flight, reinforce the affected area with plates made of 1.5 mm thick birch plywood of aeronautical quality in accordance with Carmam Drawing, titled "Modification Aileron Central Part" dated April 12, 1968, or an FAA- approved equivalent. (c) Upon incorporation of the reinforcement specified in paragraph (b) of this AD, the inspections required by paragraph (a) of this AD may be discontinued. This amendment becomes effective November 14, 1975. FOOTER:
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Retrieved: Apr 8, 2026
Rights: U.S. Government Public Domain
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