AD 69-19-05
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Dornier Luftfahrt GmbH | Do 28 D-1 | Airworthiness Directives; Dornier International GmbH Model DO-28D-1 Airplanes |
Unsafe Condition
Lateral displacement of the rubber grommet eye on the elevator control bellcrank bushing P/N 28.01.403-040.10 could cause possible jamming of the elevator control.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Visually inspect the elevator control bellcrank for grommet displacement. If displacement is 0.10 inches or more, rework the bushing before further flight. If less than 0.10 inches, rework within the next 100 hours time in service.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
within the next 10 hours time in service after the effective date of this AD
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Affected Aircraft
Dornier International GmbH Model DO-28D-1 airplanes, Serial Numbers 4002 through 4019
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Federal Register Abstract
Elevator Control
Applicability Source Text
Show captured applicability text from the source AD
AD Final Rules - DRS_69-19-05.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 69-19-05 Document Type: AD Final Rules Docket Number: Unknown Subject Heading: Airworthiness Directives; Dornier International GmbH Model DO-28D-1 Airplanes Subject: Elevator Control Status: Current Citation: This information is not available. Citation Publish Date: Effective Date: 09/15/1969 Make: Dornier Luftfahrt GmbH Model: Do 28 D-1 Product Type: Aircraft Product Subtype: Small/Large Airplane Affected AD: Superseded AD: Affected By: Superseded By: Service/Office: Office of Primary Responsibility: CFR Part Reference: Part 39 Comments: AIRWORTHINESS DIRECTIVES FINAL RULES: 69-19-05 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: Unknown AMENDMENT: 39-840 AD NUMBER: 69-19-05 SUBJECT HEADING: Airworthiness Directives; Dornier International GmbH Model DO-28D-1 Airplanes ACTION: SUMMARY: DATES: Effective September 15, 1969. ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 69-19-05 DORNIER INTERNATIONAL GmbH: Amdt. 39-840. Applies to Dornier Model DO-28D-1 airplanes, Serial Numbers 4002 through 4019. To prevent possible jamming of the elevator control, accomplish the following: (a) Within the next 10 hours time in service after the effective date of this AD, unless already accomplished, visually inspect the elevator control bellcrank for lateral displacement of the rubber grommet eye on the bushing, in accordance with Dornier Service Bulletin No. 001-1403 dated 12 May 1969 or an FAA-approved equivalent. (b) If the displacement of rubber grommet eye on the bushing is found to be 0.10 inches or more, before further flight, rework the bushing P/N 28.01.403-040.10 in accordance with Dornier Service Bulletin No. 001-1403, dated 12 May 1969 or an FAA-approved equivalent. (c) If the displacement of rubber grommet eye on the bushing is found to be less than 0.10 inches, within the next 100 hours time in service after the effective date of this AD, unless already accomplished, rework the bushing P/N 28.01.403-040.10 in accordance with Dornier Service Bulletin No. 001-1403, dated 12 May 1969 or an FAA-approved equivalent. This amendment becomes effective September 15, 1969. FOOTER:
Document Text
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AD Final Rules - DRS_69-19-05.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 69-19-05 Document Type: AD Final Rules Docket Number: Unknown Subject Heading: Airworthiness Directives; Dornier International GmbH Model DO-28D-1 Airplanes Subject: Elevator Control Status: Current Citation: This information is not available. Citation Publish Date: Effective Date: 09/15/1969 Make: Dornier Luftfahrt GmbH Model: Do 28 D-1 Product Type: Aircraft Product Subtype: Small/Large 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: 69-19-05 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: Unknown AMENDMENT: 39-840 AD NUMBER: 69-19-05 SUBJECT HEADING: Airworthiness Directives; Dornier International GmbH Model DO-28D-1 Airplanes ACTION: SUMMARY: DATES: Effective September 15, 1969. ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 69-19-05 DORNIER INTERNATIONAL GmbH: Amdt. 39-840. Applies to Dornier Model DO-28D-1 airplanes, Serial Numbers 4002 through 4019. To prevent possible jamming of the elevator control, accomplish the following: (a) Within the next 10 hours time in service after the effective date of this AD, unless already accomplished, visually inspect the elevator control bellcrank for lateral displacement of the rubber grommet eye on the bushing, in accordance with Dornier Service Bulletin No. 001-1403 dated 12 May 1969 or an FAA-approved equivalent. (b) If the displacement of rubber grommet eye on the bushing is found to be 0.10 inches or more, before further flight, rework the bushing P/N 28.01.403-040.10 in accordance with Dornier Service Bulletin No. 001-1403, dated 12 May 1969 or an FAA-approved equivalent. (c) If the displacement of rubber grommet eye on the bushing is found to be less than 0.10 inches, within the next 100 hours time in service after the effective date of this AD, unless already accomplished, rework the bushing P/N 28.01.403-040.10 in accordance with Dornier Service Bulletin No. 001-1403, dated 12 May 1969 or an FAA-approved equivalent. This amendment becomes effective September 15, 1969. FOOTER:
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Retrieved: Apr 8, 2026
Rights: U.S. Government Public Domain
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