AD 71-20-03
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Sud Aviation | Caravelle SE 210 Model VIR | Airworthiness Directives; SUD AVIATION Model SE.210, MK VI-R Airplanes |
Unsafe Condition
Failure of the relay in the elevator servodyne circuit could result in an inoperative jamming warning system for the elevator servodyne.
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Required Actions
Install a holding relay in the elevator servodyne jamming warning circuit in accordance with Sud Service-Caravelle Bulletin No. 27-218 at Revision 4, dated March 27, 1970, or an FAA-approved equivalent.
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Compliance Time
within the next 500 hours' time in service after the effective date of this AD
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Affected Aircraft
Sud Aviation Model SE.210, MK VI-R 'Caravelle' airplanes
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Federal Register Abstract
Relay In Elevator Servodyne Circuit
Applicability Source Text
Show captured applicability text from the source AD
AD Final Rules - DRS_71-20-03.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 71-20-03 Document Type: AD Final Rules Docket Number: Unknown Subject Heading: Airworthiness Directives; SUD AVIATION Model SE.210, MK VI-R Airplanes Subject: Relay In Elevator Servodyne Circuit Status: Current Citation: This information is not available. Citation Publish Date: Effective Date: 10/18/1971 Make: Sud Aviation Model: Caravelle SE 210 Model VIR Product Type: Aircraft Product Subtype: Large Airplane Affected AD: Superseded AD: Affected By: Superseded By: Service/Office: Office of Primary Responsibility: CFR Part Reference: Part 39 Comments: Updated RGL applicability to match AD applicability; CAR C-11-185 AIRWORTHINESS DIRECTIVES FINAL RULES: 71-20-03 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: Unknown AMENDMENT: 39-1296 AD NUMBER: 71-20-03 SUBJECT HEADING: Airworthiness Directives; SUD AVIATION Model SE.210, MK VI-R Airplanes ACTION: SUMMARY: DATES: Effective October 18, 1971. ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 71-20-03 SUD AVIATION: Amendment 39-1296. Applies to Sud Model SE.210, MK VI-R, "Caravelle" airplanes. Within the next 500 hours' time in service after the effective date of this AD, unless already accomplished, incorporate S.A. Modification 1592 by installing a holding relay in the elevator servodyne jamming warning circuit in accordance with Sud Service-Caravelle Bulletin No. 27-218 at Revision 4, dated March 27, 1970, or an FAA-approved equivalent. This amendment becomes effective October 18, 1971. FOOTER:
Document Text
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AD Final Rules - DRS_71-20-03.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 71-20-03 Document Type: AD Final Rules Docket Number: Unknown Subject Heading: Airworthiness Directives; SUD AVIATION Model SE.210, MK VI-R Airplanes Subject: Relay In Elevator Servodyne Circuit Status: Current Citation: This information is not available. Citation Publish Date: Effective Date: 10/18/1971 Make: Sud Aviation Model: Caravelle SE 210 Model VIR Product Type: Aircraft Product Subtype: Large Airplane Affected AD: Superseded AD: Affected By: Superseded By: Service/Office: Office of Primary Responsibility: CFR Part Reference: Part 39 Comments: Updated RGL applicability to match AD applicability; CAR C-11-185 AIRWORTHINESS DIRECTIVES FINAL RULES: 71-20-03 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: Unknown AMENDMENT: 39-1296 AD NUMBER: 71-20-03 SUBJECT HEADING: Airworthiness Directives; SUD AVIATION Model SE.210, MK VI-R Airplanes ACTION: SUMMARY: DATES: Effective October 18, 1971. ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 71-20-03 SUD AVIATION: Amendment 39-1296. Applies to Sud Model SE.210, MK VI-R, "Caravelle" airplanes. Within the next 500 hours' time in service after the effective date of this AD, unless already accomplished, incorporate S.A. Modification 1592 by installing a holding relay in the elevator servodyne jamming warning circuit in accordance with Sud Service-Caravelle Bulletin No. 27-218 at Revision 4, dated March 27, 1970, or an FAA-approved equivalent. This amendment becomes effective October 18, 1971. FOOTER:
Source: Official FAA Source ↗
Retrieved: Apr 8, 2026
Rights: U.S. Government Public Domain
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