AD 64-27-01
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Textron Aviation Inc. | P35 | Airworthiness Directives; Beech Model P35 and S35 Airplanes |
| aircraft | Textron Aviation Inc. | S35 | Airworthiness Directives; Beech Model P35 and S35 Airplanes |
Unsafe Condition
The elevator control column stop fitting may bind between overtrimmed stops or go past the stops and jam the control column in the full aft (up elevator) position.
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Required Actions
Remove the large inspection plate on the left firewall, mark the contact area on the fixed stops using the control column fitting stop as a guide, and if the combined contact area width is less than 3/16 inch, fabricate and install a new elevator control fixed stop in accordance with Beech Service Bulletin No. 64-19 or an FAA-approved equivalent.
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Compliance Time
within 25 hours' time in service after the effective date of this AD
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Affected Aircraft
Beech Model P35 and S35 Airplanes, Serial Numbers D-6842 through D-7630, except Serial Numbers D-7610, D-7615, D-7617, D-7620, and D-7625 through D-7628.
AI-generated summary from the source AD text. Verify against the official source before acting.
Federal Register Abstract
Control Wheel Column Aft Stop
Applicability Source Text
Show captured applicability text from the source AD
AD Final Rules - DRS_64-27-01.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 64-27-01 Document Type: AD Final Rules Docket Number: Unknown Subject Heading: Airworthiness Directives; Beech Model P35 and S35 Airplanes Subject: Control Wheel Column Aft Stop Status: Current Citation: Federal Register: December 1, 1964 Citation Publish Date: 12/01/1964 Effective Date: 12/07/1964 Make: Textron Aviation Inc. Model: P35 | S35 Product Type: Aircraft Product Subtype: Small Airplane Affected AD: Superseded AD: Affected By: Superseded By: Service/Office: Office of Primary Responsibility: CFR Part Reference: Part 39 Comments: AIRWORTHINESS DIRECTIVES FINAL RULES: 64-27-01 CITATION: [Federal Register: December 1, 1964] PAGE NUMBER: DOCKET NUMBER: Unknown AMENDMENT: 39-6 AD NUMBER: 64-27-01 SUBJECT HEADING: Airworthiness Directives; Beech Model P35 and S35 Airplanes ACTION: SUMMARY: DATES: Effective December 7, 1964. ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 64-27-01 BEECH: Amdt. 39-6 Part 39 (New) Federal Register December 1, 1964. Applies to Models P35 and S35 Aircraft, Serial Numbers D-6842 through D-7630, except Serial Numbers D-7610, D-7615, D-7617, D-7620, and D-7625 through D-7628. Compliance required within 25 hours' time in service after the effective date of this AD, unless already accomplished. To prevent the elevator control column stop fitting from binding between overtrimmed stops or going past the stops and jamming the control column in the full aft (up elevator) position, accomplish the following. (a) Remove the large inspection plate on the left firewall. With the control column in the most aft position, mark the contact area on the fixed stops, using the control column fitting stop as a guide. The combined contact area width on the two stops measured in a horizontal plane shall be at least 3/16 inch. (b) Fabricate and install a new elevator control fixed stop on aircraft having less than 3/16 inch combined contact area width on the two stops measured in a horizontal plane in accordance with Beech Service Bulletin No. 64-19, or an FAA-approved equivalent. (Beech Service Bulletin No. 64-19, covers this same subject.) This directive effective December 7, 1964. FOOTER:
Document Text
Show stored source text (verify against official source)
AD Final Rules - DRS_64-27-01.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 64-27-01 Document Type: AD Final Rules Docket Number: Unknown Subject Heading: Airworthiness Directives; Beech Model P35 and S35 Airplanes Subject: Control Wheel Column Aft Stop Status: Current Citation: Federal Register: December 1, 1964 Citation Publish Date: 12/01/1964 Effective Date: 12/07/1964 Make: Textron Aviation Inc. Model: P35 | S35 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: 64-27-01 CITATION: [Federal Register: December 1, 1964] PAGE NUMBER: DOCKET NUMBER: Unknown AMENDMENT: 39-6 AD NUMBER: 64-27-01 SUBJECT HEADING: Airworthiness Directives; Beech Model P35 and S35 Airplanes ACTION: SUMMARY: DATES: Effective December 7, 1964. ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 64-27-01 BEECH: Amdt. 39-6 Part 39 (New) Federal Register December 1, 1964. Applies to Models P35 and S35 Aircraft, Serial Numbers D-6842 through D-7630, except Serial Numbers D-7610, D-7615, D-7617, D-7620, and D-7625 through D-7628. Compliance required within 25 hours' time in service after the effective date of this AD, unless already accomplished. To prevent the elevator control column stop fitting from binding between overtrimmed stops or going past the stops and jamming the control column in the full aft (up elevator) position, accomplish the following. (a) Remove the large inspection plate on the left firewall. With the control column in the most aft position, mark the contact area on the fixed stops, using the control column fitting stop as a guide. The combined contact area width on the two stops measured in a horizontal plane shall be at least 3/16 inch. (b) Fabricate and install a new elevator control fixed stop on aircraft having less than 3/16 inch combined contact area width on the two stops measured in a horizontal plane in accordance with Beech Service Bulletin No. 64-19, or an FAA-approved equivalent. (Beech Service Bulletin No. 64-19, covers this same subject.) This directive effective December 7, 1964. FOOTER:
Source: Official FAA Source ↗
Retrieved: Apr 8, 2026
Rights: U.S. Government Public Domain
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