AD 64-16-03
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Maryland Air Industries, Inc. | F-27 | Airworthiness Directives; FAIRCHILD Model F-27 Series Aircraft |
| aircraft | Maryland Air Industries, Inc. | F-27A | Airworthiness Directives; FAIRCHILD Model F-27 Series Aircraft |
| aircraft | Maryland Air Industries, Inc. | F-27B | Airworthiness Directives; FAIRCHILD Model F-27 Series Aircraft |
| aircraft | Maryland Air Industries, Inc. | F-27F | Airworthiness Directives; FAIRCHILD Model F-27 Series Aircraft |
| aircraft | Maryland Air Industries, Inc. | F-27G | Airworthiness Directives; FAIRCHILD Model F-27 Series Aircraft |
| aircraft | Maryland Air Industries, Inc. | F-27J | Airworthiness Directives; FAIRCHILD Model F-27 Series Aircraft |
| aircraft | Maryland Air Industries, Inc. | F-27M | Airworthiness Directives; FAIRCHILD Model F-27 Series Aircraft |
Unsafe Condition
The rudder may become unbalanced, leading to improper control forces and degraded handling characteristics.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Rebalance the rudder following Fairchild Service Bulletin 27-38 or an equivalent approved method.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
within 300 hours' time in service after the effective date of this AD
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
Maryland Air Industries, Inc. Model F-27, F-27A, F-27B, F-27F, F-27G, F-27J, F-27M aircraft
AI-generated summary from the source AD text. Verify against the official source before acting.
Federal Register Abstract
Rudder
Applicability Source Text
Show captured applicability text from the source AD
AD Final Rules - DRS_64-16-03.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 64-16-03 Document Type: AD Final Rules Docket Number: Unknown Subject Heading: Airworthiness Directives; FAIRCHILD Model F-27 Series Aircraft Subject: Rudder Status: Current Citation: This information is not available. Citation Publish Date: Effective Date: 07/23/1964 Make: Maryland Air Industries, Inc. Model: F-27 | F-27A | F-27B | F-27F | F-27G | F-27J | F-27M Product Type: Aircraft Product Subtype: Large Airplane Affected AD: Superseded AD: Affected By: Superseded By: Service/Office: Office of Primary Responsibility: CFR Part Reference: Part 39 Comments: AIRWORTHINESS DIRECTIVES FINAL RULES: 64-16-03 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: Unknown AMENDMENT: AD NUMBER: 64-16-03 SUBJECT HEADING: Airworthiness Directives; FAIRCHILD Model F-27 Series Aircraft ACTION: SUMMARY: DATES: Effective July 23, 1964. ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 64-16-03 FAIRCHILD: Amdt. 771 Part 507 Federal Register July 23, 1964. Applies to Model F-27 Series Aircraft. Compliance required within 300 hours' time in service after the effective date of this AD, unless already accomplished. Rebalance the rudder in accordance with the procedures specified in Section 2, "Accomplishment Instructions", of Fairchild Service Bulletin 27-38, or an equivalent approved by the Engineering and Manufacturing Branch, FAA Eastern Region. (Fairchild Service Bulletin 27-38 dated May 4, 1964, covers this same subject.) This directive effective July 23, 1964. FOOTER:
Document Text
Show stored source text (verify against official source)
AD Final Rules - DRS_64-16-03.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 64-16-03 Document Type: AD Final Rules Docket Number: Unknown Subject Heading: Airworthiness Directives; FAIRCHILD Model F-27 Series Aircraft Subject: Rudder Status: Current Citation: This information is not available. Citation Publish Date: Effective Date: 07/23/1964 Make: Maryland Air Industries, Inc. Model: F-27 | F-27A | F-27B | F-27F | F-27G | F-27J | F-27M 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: AIRWORTHINESS DIRECTIVES FINAL RULES: 64-16-03 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: Unknown AMENDMENT: AD NUMBER: 64-16-03 SUBJECT HEADING: Airworthiness Directives; FAIRCHILD Model F-27 Series Aircraft ACTION: SUMMARY: DATES: Effective July 23, 1964. ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 64-16-03 FAIRCHILD: Amdt. 771 Part 507 Federal Register July 23, 1964. Applies to Model F-27 Series Aircraft. Compliance required within 300 hours' time in service after the effective date of this AD, unless already accomplished. Rebalance the rudder in accordance with the procedures specified in Section 2, "Accomplishment Instructions", of Fairchild Service Bulletin 27-38, or an equivalent approved by the Engineering and Manufacturing Branch, FAA Eastern Region. (Fairchild Service Bulletin 27-38 dated May 4, 1964, covers this same subject.) This directive effective July 23, 1964. FOOTER:
Source: Official FAA Source ↗
Retrieved: Apr 8, 2026
Rights: U.S. Government Public Domain
This site is not affiliated with or endorsed by the FAA. Always verify with official sources.
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