AD 71-24-10
final rule
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Textron Aviation Inc. | 35-C33 | Airworthiness Directives; BEECH Models 35-C33, E33, F33, 35-C33A, E33A, F33A, E33C, F33C, V35, V35TC, V35, V35A-TC, V35B, V35B-TC, 36, A36, 95-B55, 95-B55A, 95-C55, D55, E55, 56TC, A56TC, 58, D95A, E95 |
| aircraft | Textron Aviation Inc. | 35-C33A | Airworthiness Directives; BEECH Models 35-C33, E33, F33, 35-C33A, E33A, F33A, E33C, F33C, V35, V35TC, V35, V35A-TC, V35B, V35B-TC, 36, A36, 95-B55, 95-B55A, 95-C55, D55, E55, 56TC, A56TC, 58, D95A, E95 |
| aircraft | Textron Aviation Inc. | 36 | Airworthiness Directives; BEECH Models 35-C33, E33, F33, 35-C33A, E33A, F33A, E33C, F33C, V35, V35TC, V35, V35A-TC, V35B, V35B-TC, 36, A36, 95-B55, 95-B55A, 95-C55, D55, E55, 56TC, A56TC, 58, D95A, E95 |
| aircraft | Textron Aviation Inc. | 56TC | Airworthiness Directives; BEECH Models 35-C33, E33, F33, 35-C33A, E33A, F33A, E33C, F33C, V35, V35TC, V35, V35A-TC, V35B, V35B-TC, 36, A36, 95-B55, 95-B55A, 95-C55, D55, E55, 56TC, A56TC, 58, D95A, E95 |
| aircraft | Textron Aviation Inc. | 58 | Airworthiness Directives; BEECH Models 35-C33, E33, F33, 35-C33A, E33A, F33A, E33C, F33C, V35, V35TC, V35, V35A-TC, V35B, V35B-TC, 36, A36, 95-B55, 95-B55A, 95-C55, D55, E55, 56TC, A56TC, 58, D95A, E95 |
| aircraft | Textron Aviation Inc. | 95-B55 | Airworthiness Directives; BEECH Models 35-C33, E33, F33, 35-C33A, E33A, F33A, E33C, F33C, V35, V35TC, V35, V35A-TC, V35B, V35B-TC, 36, A36, 95-B55, 95-B55A, 95-C55, D55, E55, 56TC, A56TC, 58, D95A, E95 |
| aircraft | Textron Aviation Inc. | 95-B55A | Airworthiness Directives; BEECH Models 35-C33, E33, F33, 35-C33A, E33A, F33A, E33C, F33C, V35, V35TC, V35, V35A-TC, V35B, V35B-TC, 36, A36, 95-B55, 95-B55A, 95-C55, D55, E55, 56TC, A56TC, 58, D95A, E95 |
| aircraft | Textron Aviation Inc. | 95-C55 | Airworthiness Directives; BEECH Models 35-C33, E33, F33, 35-C33A, E33A, F33A, E33C, F33C, V35, V35TC, V35, V35A-TC, V35B, V35B-TC, 36, A36, 95-B55, 95-B55A, 95-C55, D55, E55, 56TC, A56TC, 58, D95A, E95 |
| aircraft | Textron Aviation Inc. | 95-C55A | Airworthiness Directives; BEECH Models 35-C33, E33, F33, 35-C33A, E33A, F33A, E33C, F33C, V35, V35TC, V35, V35A-TC, V35B, V35B-TC, 36, A36, 95-B55, 95-B55A, 95-C55, D55, E55, 56TC, A56TC, 58, D95A, E95 |
| aircraft | Textron Aviation Inc. | A36 | Airworthiness Directives; BEECH Models 35-C33, E33, F33, 35-C33A, E33A, F33A, E33C, F33C, V35, V35TC, V35, V35A-TC, V35B, V35B-TC, 36, A36, 95-B55, 95-B55A, 95-C55, D55, E55, 56TC, A56TC, 58, D95A, E95 |
| aircraft | Textron Aviation Inc. | A56TC | Airworthiness Directives; BEECH Models 35-C33, E33, F33, 35-C33A, E33A, F33A, E33C, F33C, V35, V35TC, V35, V35A-TC, V35B, V35B-TC, 36, A36, 95-B55, 95-B55A, 95-C55, D55, E55, 56TC, A56TC, 58, D95A, E95 |
| aircraft | Textron Aviation Inc. | D55 | Airworthiness Directives; BEECH Models 35-C33, E33, F33, 35-C33A, E33A, F33A, E33C, F33C, V35, V35TC, V35, V35A-TC, V35B, V35B-TC, 36, A36, 95-B55, 95-B55A, 95-C55, D55, E55, 56TC, A56TC, 58, D95A, E95 |
| aircraft | Textron Aviation Inc. | D95A | Airworthiness Directives; BEECH Models 35-C33, E33, F33, 35-C33A, E33A, F33A, E33C, F33C, V35, V35TC, V35, V35A-TC, V35B, V35B-TC, 36, A36, 95-B55, 95-B55A, 95-C55, D55, E55, 56TC, A56TC, 58, D95A, E95 |
| aircraft | Textron Aviation Inc. | E33 | Airworthiness Directives; BEECH Models 35-C33, E33, F33, 35-C33A, E33A, F33A, E33C, F33C, V35, V35TC, V35, V35A-TC, V35B, V35B-TC, 36, A36, 95-B55, 95-B55A, 95-C55, D55, E55, 56TC, A56TC, 58, D95A, E95 |
| aircraft | Textron Aviation Inc. | E33A | Airworthiness Directives; BEECH Models 35-C33, E33, F33, 35-C33A, E33A, F33A, E33C, F33C, V35, V35TC, V35, V35A-TC, V35B, V35B-TC, 36, A36, 95-B55, 95-B55A, 95-C55, D55, E55, 56TC, A56TC, 58, D95A, E95 |
| aircraft | Textron Aviation Inc. | E33C | Airworthiness Directives; BEECH Models 35-C33, E33, F33, 35-C33A, E33A, F33A, E33C, F33C, V35, V35TC, V35, V35A-TC, V35B, V35B-TC, 36, A36, 95-B55, 95-B55A, 95-C55, D55, E55, 56TC, A56TC, 58, D95A, E95 |
| aircraft | Textron Aviation Inc. | E55 | Airworthiness Directives; BEECH Models 35-C33, E33, F33, 35-C33A, E33A, F33A, E33C, F33C, V35, V35TC, V35, V35A-TC, V35B, V35B-TC, 36, A36, 95-B55, 95-B55A, 95-C55, D55, E55, 56TC, A56TC, 58, D95A, E95 |
| aircraft | Textron Aviation Inc. | E95 | Airworthiness Directives; BEECH Models 35-C33, E33, F33, 35-C33A, E33A, F33A, E33C, F33C, V35, V35TC, V35, V35A-TC, V35B, V35B-TC, 36, A36, 95-B55, 95-B55A, 95-C55, D55, E55, 56TC, A56TC, 58, D95A, E95 |
| aircraft | Textron Aviation Inc. | F33 | Airworthiness Directives; BEECH Models 35-C33, E33, F33, 35-C33A, E33A, F33A, E33C, F33C, V35, V35TC, V35, V35A-TC, V35B, V35B-TC, 36, A36, 95-B55, 95-B55A, 95-C55, D55, E55, 56TC, A56TC, 58, D95A, E95 |
| aircraft | Textron Aviation Inc. | F33A | Airworthiness Directives; BEECH Models 35-C33, E33, F33, 35-C33A, E33A, F33A, E33C, F33C, V35, V35TC, V35, V35A-TC, V35B, V35B-TC, 36, A36, 95-B55, 95-B55A, 95-C55, D55, E55, 56TC, A56TC, 58, D95A, E95 |
| aircraft | Textron Aviation Inc. | F33C | Airworthiness Directives; BEECH Models 35-C33, E33, F33, 35-C33A, E33A, F33A, E33C, F33C, V35, V35TC, V35, V35A-TC, V35B, V35B-TC, 36, A36, 95-B55, 95-B55A, 95-C55, D55, E55, 56TC, A56TC, 58, D95A, E95 |
| aircraft | Textron Aviation Inc. | V35 | Airworthiness Directives; BEECH Models 35-C33, E33, F33, 35-C33A, E33A, F33A, E33C, F33C, V35, V35TC, V35, V35A-TC, V35B, V35B-TC, 36, A36, 95-B55, 95-B55A, 95-C55, D55, E55, 56TC, A56TC, 58, D95A, E95 |
| aircraft | Textron Aviation Inc. | V35A | Airworthiness Directives; BEECH Models 35-C33, E33, F33, 35-C33A, E33A, F33A, E33C, F33C, V35, V35TC, V35, V35A-TC, V35B, V35B-TC, 36, A36, 95-B55, 95-B55A, 95-C55, D55, E55, 56TC, A56TC, 58, D95A, E95 |
| aircraft | Textron Aviation Inc. | V35B | Airworthiness Directives; BEECH Models 35-C33, E33, F33, 35-C33A, E33A, F33A, E33C, F33C, V35, V35TC, V35, V35A-TC, V35B, V35B-TC, 36, A36, 95-B55, 95-B55A, 95-C55, D55, E55, 56TC, A56TC, 58, D95A, E95 |
Unsafe Condition
Failure of control wheel adapters not stamped with two Beech inspection stamps could result in control wheel detachment during flight.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Ascertain two Beech inspection stamps on one tip of each control wheel adapter. Replace adapters without stamps with specified part numbers or equivalent approved parts.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
within 50 hours' time in service after August 1, 1973, for airplanes not complying with AD 71-12-04, or within 300 hours' time in service after August 1, 1973, for those that do comply with AD 71-12-04
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
BEECH Models 35-C33, E33, F33, 35-C33A, E33A, F33A, E33C, F33C, V35, V35TC, V35A, V35A-TC, V35B, V35B-TC, 36, A36, 95-B55, 95-B55A, 95-C55, D55, E55, 56TC, A56TC, 58, D95A, E95 with specified serial ranges, and models with P/N 60-524080 series control wheels including clock and light provisions.
AI-generated summary from the source AD text. Verify against the official source before acting.
Federal Register Abstract
Security of Control Wheel
Applicability Source Text
Show captured applicability text from the source AD
AD Final Rules - DRS_71-24-10.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 71-24-10 Document Type: AD Final Rules Docket Number: Unknown Subject Heading: Airworthiness Directives; BEECH Models 35-C33, E33, F33, 35-C33A, E33A, F33A, E33C, F33C, V35, V35T...Show more Subject: Security of Control Wheel Status: Current Citation: This information is not available. Citation Publish Date: Effective Date: 08/01/1973 Make: Textron Aviation Inc. Model: 35-C33 | 35-C33A | 36 | 56TC | 58 | 95-B55 | 95-B55A | 95-C55 | 95-C55A | A36 | A56TC | D55 | D95A |...Show more 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: 71-24-10 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: Unknown AMENDMENT: 39-1693 AD NUMBER: 71-24-10 SUBJECT HEADING: Airworthiness Directives; BEECH Models 35-C33, E33, F33, 35-C33A, E33A, F33A, E33C, F33C, V35, V35TC, V35, V35A-TC, V35B, V35B-TC, 36, A36, 95-B55, 95-B55A, 95-C55, D55, E55, 56TC, A56TC, 58, D95A, E95 ACTION: SUMMARY: DATES: Effective August 1, 1973 ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 71-24-10 BEECH: Amendment 39-1350 as amended by Amendment 39-1693. Applies to the following airplanes: 1) Models Serial Numbers Affected 35-C33, E33, F33 CD-1062 thru CD-1254, except CD- 1237 35-C33A, E33A, F33A CE-118 thru CE-346, except CE-324 E33C, F33C CJ-1 thru CJ-30 V35, V35TC, V35A D-8336 thru D-9285, except V35A-TC, V35B, D-9208, -9279, -9280, -9281, V35B-TC 9282 36, A36 E-1 thru E-275 95-B55, 95-B55A TC-1021 thru TC-1397, except TC- 1395, -1396 95-C55, D55, E55 TE-256 thru TE-845, except TE-836, 837 56TC, A56TC TG-1 thru TG-94 58 TH-1 thru TH-170 except TH-135, - 153, -161 D95A, E95 TD-678 thru TD-721 2) Only applicable if altered in service to incorporate P/N 60-524080 series control wheels which have provisions for a clock and light: Models Serial Numbers Affected 35-C33 CD-814 thru CD-1061 35-C33A CE-1 thru CE-117 V35 D-7977 thru D-8335 95-B55, 95-B55A TC-371 and TC-502 thru TC-1020 95-C55, 95-C55A TC-350 and TE-1 thru TE-255 D95A TD-534 thru TD-677 In order to assure security of control wheels, (1) within 50 hours' time in service after the effective date of this AD, for those airplanes which do not comply with AD 71-12-04, or (2) within 300 hours' time in service after the effective date of this AD, for those airplanes which do comply with AD 71-12-04, unless already accomplished, accomplish the following: Ascertain that two Beech inspection stamps can be seen on one tip of each control wheel adapter. (These tips may be seen while looking toward the forward face of control wheel hubs, without disassembly.) If the stamps cannot be seen on an adapter, replace it with either Beech P/N 96-524029-15 (short) or Beech P/N 96-524029-19 (long) control wheel adapters which have the aforementioned stamps, or in the alternative with Beech P/N 96-524029-31 (short) and 96- 524029-33 (long control wheel adapters, or with any equivalent part approved by the Chief, Engineering and Manufacturing Branch, FAA, Central Region. Beechcraft Service Instruction No. 0254-156, or later revision approved by Chief, Engineering and Manufacturing Branch, FAA, Central Region, pertains to this subject. This AD Amendment 39-1350 supersedes AD 71-12-04. Amendment 39-1350 became effective December 1, 1971. This amendment 39-1693 becomes effective August 1, 1973. FOOTER:
Document Text
Show stored source text (verify against official source)
AD Final Rules - DRS_71-24-10.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 71-24-10 Document Type: AD Final Rules Docket Number: Unknown Subject Heading: Airworthiness Directives; BEECH Models 35-C33, E33, F33, 35-C33A, E33A, F33A, E33C, F33C, V35, V35T...Show more Subject: Security of Control Wheel Status: Current Citation: This information is not available. Citation Publish Date: Effective Date: 08/01/1973 Make: Textron Aviation Inc. Model: 35-C33 | 35-C33A | 36 | 56TC | 58 | 95-B55 | 95-B55A | 95-C55 | 95-C55A | A36 | A56TC | D55 | D95A |...Show more 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: 71-24-10 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: Unknown AMENDMENT: 39-1693 AD NUMBER: 71-24-10 SUBJECT HEADING: Airworthiness Directives; BEECH Models 35-C33, E33, F33, 35-C33A, E33A, F33A, E33C, F33C, V35, V35TC, V35, V35A-TC, V35B, V35B-TC, 36, A36, 95-B55, 95-B55A, 95-C55, D55, E55, 56TC, A56TC, 58, D95A, E95 ACTION: SUMMARY: DATES: Effective August 1, 1973 ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 71-24-10 BEECH: Amendment 39-1350 as amended by Amendment 39-1693. Applies to the following airplanes: 1) Models Serial Numbers Affected 35-C33, E33, F33 CD-1062 thru CD-1254, except CD- 1237 35-C33A, E33A, F33A CE-118 thru CE-346, except CE-324 E33C, F33C CJ-1 thru CJ-30 V35, V35TC, V35A D-8336 thru D-9285, except V35A-TC, V35B, D-9208, -9279, -9280, -9281, V35B-TC 9282 36, A36 E-1 thru E-275 95-B55, 95-B55A TC-1021 thru TC-1397, except TC- 1395, -1396 95-C55, D55, E55 TE-256 thru TE-845, except TE-836, 837 56TC, A56TC TG-1 thru TG-94 58 TH-1 thru TH-170 except TH-135, - 153, -161 D95A, E95 TD-678 thru TD-721 2) Only applicable if altered in service to incorporate P/N 60-524080 series control wheels which have provisions for a clock and light: Models Serial Numbers Affected 35-C33 CD-814 thru CD-1061 35-C33A CE-1 thru CE-117 V35 D-7977 thru D-8335 95-B55, 95-B55A TC-371 and TC-502 thru TC-1020 95-C55, 95-C55A TC-350 and TE-1 thru TE-255 D95A TD-534 thru TD-677 In order to assure security of control wheels, (1) within 50 hours' time in service after the effective date of this AD, for those airplanes which do not comply with AD 71-12-04, or (2) within 300 hours' time in service after the effective date of this AD, for those airplanes which do comply with AD 71-12-04, unless already accomplished, accomplish the following: Ascertain that two Beech inspection stamps can be seen on one tip of each control wheel adapter. (These tips may be seen while looking toward the forward face of control wheel hubs, without disassembly.) If the stamps cannot be seen on an adapter, replace it with either Beech P/N 96-524029-15 (short) or Beech P/N 96-524029-19 (long) control wheel adapters which have the aforementioned stamps, or in the alternative with Beech P/N 96-524029-31 (short) and 96- 524029-33 (long control wheel adapters, or with any equivalent part approved by the Chief, Engineering and Manufacturing Branch, FAA, Central Region. Beechcraft Service Instruction No. 0254-156, or later revision approved by Chief, Engineering and Manufacturing Branch, FAA, Central Region, pertains to this subject. This AD Amendment 39-1350 supersedes AD 71-12-04. Amendment 39-1350 became effective December 1, 1971. This amendment 39-1693 becomes effective August 1, 1973. FOOTER:
Source: Official FAA Source ↗
Retrieved: Apr 8, 2026
Rights: U.S. Government Public Domain
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