AD 69-19-07
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Aermacchi S.p.A. | S.205 - 22/R | Airworthiness Directives; Siai-Marchetti Model S.205-22/R Airplanes |
Unsafe Condition
Interference between the engine controls and the elevator control column could restrict elevator travel and impair control of the airplane.
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Required Actions
Visually inspect the engine control support console for deformation and check elevator control movement before further flight and at each preflight inspection. If deformation or restricted travel is found, remove the straight type propeller control strut (P/N 205-6-179-01) and install the bent type (P/N 205-6-179-03) per SIAI Service Bulletin 205B22B or FAA-approved equivalent. The modification must be completed within 300 hours' time in service after August 17, 1970, if not already done.
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Compliance Time
Before further flight after the effective date of this AD and thereafter at each preflight inspection. The modification must be accomplished within the next 300 hours' time in service after August 17, 1970.
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Affected Aircraft
Aermacchi S.p.A. Model S.205-22/R airplanes, Serial Numbers 001 through 5-303.
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Federal Register Abstract
Engine and Elevator Controls
Applicability Source Text
Show captured applicability text from the source AD
AD Final Rules - DRS_69-19-07.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 69-19-07 Document Type: AD Final Rules Docket Number: Unknown Subject Heading: Airworthiness Directives; Siai-Marchetti Model S.205-22/R Airplanes Subject: Engine and Elevator Controls Status: Current Citation: This information is not available. Citation Publish Date: Effective Date: 08/17/1970 Make: Aermacchi S.p.A. Model: S.205 - 22/R Product Type: Aircraft Product Subtype: Small Airplane Affected AD: Superseded AD: Affected By: Superseded By: Service/Office: Office of Primary Responsibility: CFR Part Reference: Part 39 Comments: AIRWORTHINESS DIRECTIVES FINAL RULES: 69-19-07 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: Unknown AMENDMENT: 39-1042 AD NUMBER: 69-19-07 SUBJECT HEADING: Airworthiness Directives; Siai-Marchetti Model S.205-22/R Airplanes ACTION: SUMMARY: DATES: Effective August 17, 1970. ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 69-19-07 SIAI-MARCHETTI: Amendment 39-844 as amended by Amendment 39- 1042. Applies to Model S.205-22/R airplanes, Serial Numbers 001 through 5-303. Compliance required as indicated unless already accomplished. To prevent interference between the engine controls located behind the instrument panel and the elevator control column accomplish the following: (a) Before further flight after the effective date of this AD and thereafter at each preflight inspection, visually inspect the engine control support console for deformation and check the elevator control to assure freedom of movement and unrestricted travel. (b) If deformation of the engine control support console or restricted elevator travel is found during the inspections required in paragraph (a), comply with paragraph (d) before further flight. (c) Unless already accomplished in accordance with paragraph (b), comply with paragraph (d) within the next 300 hours' time in service after the effective date of this amendment. (d) Remove straight type propeller control strut (P/N 205-6-179-01) if installed. Install bent type propeller control strut (P/N 205-6-179-03) in accordance with SIAI Service Bulletin No. 205B22B, dated November 19, 1969, or later RAI-approved revision or an FAA- approved equivalent. (e) The repetitive inspections required by paragraph (a) may be discontinued following the incorporation of the modification required by paragraph (d). Amendment 39-844 was effective September 23, 1969. This amendment 39-1042 becomes effective August 17, 1970. FOOTER:
Document Text
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AD Final Rules - DRS_69-19-07.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 69-19-07 Document Type: AD Final Rules Docket Number: Unknown Subject Heading: Airworthiness Directives; Siai-Marchetti Model S.205-22/R Airplanes Subject: Engine and Elevator Controls Status: Current Citation: This information is not available. Citation Publish Date: Effective Date: 08/17/1970 Make: Aermacchi S.p.A. Model: S.205 - 22/R Product Type: Aircraft Product Subtype: Small Airplane Affected AD: Superseded AD: Affected By: Superseded By: Service/Office: Office of Primary Responsibility: CFR Part Reference: Part 39 Comments: AIRWORTHINESS DIRECTIVES FINAL RULES: 69-19-07 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: Unknown AMENDMENT: 39-1042 AD NUMBER: 69-19-07 SUBJECT HEADING: Airworthiness Directives; Siai-Marchetti Model S.205-22/R Airplanes ACTION: SUMMARY: DATES: Effective August 17, 1970. ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 69-19-07 SIAI-MARCHETTI: Amendment 39-844 as amended by Amendment 39- 1042. Applies to Model S.205-22/R airplanes, Serial Numbers 001 through 5-303. Compliance required as indicated unless already accomplished. To prevent interference between the engine controls located behind the instrument panel and the elevator control column accomplish the following: (a) Before further flight after the effective date of this AD and thereafter at each preflight inspection, visually inspect the engine control support console for deformation and check the elevator control to assure freedom of movement and unrestricted travel. (b) If deformation of the engine control support console or restricted elevator travel is found during the inspections required in paragraph (a), comply with paragraph (d) before further flight. (c) Unless already accomplished in accordance with paragraph (b), comply with paragraph (d) within the next 300 hours' time in service after the effective date of this amendment. (d) Remove straight type propeller control strut (P/N 205-6-179-01) if installed. Install bent type propeller control strut (P/N 205-6-179-03) in accordance with SIAI Service Bulletin No. 205B22B, dated November 19, 1969, or later RAI-approved revision or an FAA- approved equivalent. (e) The repetitive inspections required by paragraph (a) may be discontinued following the incorporation of the modification required by paragraph (d). Amendment 39-844 was effective September 23, 1969. This amendment 39-1042 becomes effective August 17, 1970. FOOTER:
Source: Official FAA Source ↗
Retrieved: Apr 8, 2026
Rights: U.S. Government Public Domain
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