AD 69-24-01
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 Model M.100S and Carmam Model M.200 Gliders |
| aircraft | Aer-Pegaso S.p.A. | Societe C.A.R.M.A.M. | M-200 | Airworthiness Directives; Aer-Pegaso Model M.100S and Carmam Model M.200 Gliders |
Unsafe Condition
Improper installation of the horizontal stabilizer to the glider.
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Required Actions
Install an inspection window on the left side of the dorsal fin and paint the elevator control transmission fork plates per Aer-Pegaso Technical Bulletin N.10/M-100S or FAA-approved equivalent. Install a placard in the cockpit instructing the pilot to visually confirm the elevator control lever engagement before first flight after tailplane rigging.
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Compliance Time
within the next 25 hours' time in service after the effective date of this AD
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Affected Aircraft
Aer-Pegaso Model M.100S and Carmam Model M.200 gliders
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Federal Register Abstract
Horizontal Stabilizer
Applicability Source Text
Show captured applicability text from the source AD
AD Final Rules - DRS_69-24-01.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 69-24-01 Document Type: AD Final Rules Docket Number: Unknown Subject Heading: Airworthiness Directives; Aer-Pegaso Model M.100S and Carmam Model M.200 Gliders Subject: Horizontal Stabilizer Status: Current Citation: This information is not available. Citation Publish Date: Effective Date: 11/23/1969 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S.p.A. | Societe C.A.R.M.A.M. Model: M-100 S | M-200 Product Type: Aircraft Product Subtype: Glider Affected AD: Superseded AD: Affected By: Superseded By: Service/Office: Office of Primary Responsibility: CFR Part Reference: Part 39 Comments: AIRWORTHINESS DIRECTIVES FINAL RULES: 69-24-01 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: Unknown AMENDMENT: 39-877 AD NUMBER: 69-24-01 SUBJECT HEADING: Airworthiness Directives; Aer-Pegaso Model M.100S and Carmam Model M.200 Gliders ACTION: SUMMARY: DATES: Effective November 23, 1969. ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 69-24-01 AER PEGASO C.A.R.M.A.M.: Amdt. 39-877. Applies to Aer-Pegaso Model M.100S and C.A.R.M.A.M. Model M.200 gliders. Compliance is required within the next 25 hours' time in service after the effective date of this AD, unless already accomplished. To detect improper installation of the horizontal stabilizer to the glider, accomplish the following: (a) Install an inspection window on the left side of the dorsal fin to allow visual confirmation of the elevator "quick disconnect" attachment and paint the two plates of the elevator control transmission fork in accordance with Aer-Pegaso Technical Bulletin N.10/M- 100S, dated September 26, 1969, or an FAA-approved equivalent. (b) Install the following placard in the cockpit in clear view of the pilot: "Before the first flight after rigging the tailplane to the fuselage, look through the inspection window located on the left side of the dorsal fin and visually confirm that the end (ball bearing) of the elevator control lever is correctly engaged in the corresponding fork of the elevator control transmission. To do this, it may be necessary to move the control stick in the longitudinal direction in order to bring the lever end into view through the window. If the rigging is correct, the ball bearing will appear between the fork sides." This amendment becomes effective November 23, 1969. FOOTER:
Document Text
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AD Final Rules - DRS_69-24-01.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 69-24-01 Document Type: AD Final Rules Docket Number: Unknown Subject Heading: Airworthiness Directives; Aer-Pegaso Model M.100S and Carmam Model M.200 Gliders Subject: Horizontal Stabilizer Status: Current Citation: This information is not available. Citation Publish Date: Effective Date: 11/23/1969 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: 69-24-01 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: Unknown AMENDMENT: 39-877 AD NUMBER: 69-24-01 SUBJECT HEADING: Airworthiness Directives; Aer-Pegaso Model M.100S and Carmam Model M.200 Gliders ACTION: SUMMARY: DATES: Effective November 23, 1969. ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 69-24-01 AER PEGASO C.A.R.M.A.M.: Amdt. 39-877. Applies to Aer-Pegaso Model M.100S and C.A.R.M.A.M. Model M.200 gliders. Compliance is required within the next 25 hours' time in service after the effective date of this AD, unless already accomplished. To detect improper installation of the horizontal stabilizer to the glider, accomplish the following: (a) Install an inspection window on the left side of the dorsal fin to allow visual confirmation of the elevator "quick disconnect" attachment and paint the two plates of the elevator control transmission fork in accordance with Aer-Pegaso Technical Bulletin N.10/M- 100S, dated September 26, 1969, or an FAA-approved equivalent. (b) Install the following placard in the cockpit in clear view of the pilot: "Before the first flight after rigging the tailplane to the fuselage, look through the inspection window located on the left side of the dorsal fin and visually confirm that the end (ball bearing) of the elevator control lever is correctly engaged in the corresponding fork of the elevator control transmission. To do this, it may be necessary to move the control stick in the longitudinal direction in order to bring the lever end into view through the window. If the rigging is correct, the ball bearing will appear between the fork sides." This amendment becomes effective November 23, 1969. FOOTER:
Source: Official FAA Source ↗
Retrieved: Apr 8, 2026
Rights: U.S. Government Public Domain
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