AD 88-05-04
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Fokker Services | F.28 Mark 0070 | Airworthiness Directives; FOKKER AIRCRAFT Model F-28 Series Airplanes |
| aircraft | Fokker Services | F.28 Mark 0100 | Airworthiness Directives; FOKKER AIRCRAFT Model F-28 Series Airplanes |
| aircraft | Fokker Services | F.28 Mark 1000 | Airworthiness Directives; FOKKER AIRCRAFT Model F-28 Series Airplanes |
| aircraft | Fokker Services | F.28 Mark 2000 | Airworthiness Directives; FOKKER AIRCRAFT Model F-28 Series Airplanes |
| aircraft | Fokker Services | F.28 Mark 3000 | Airworthiness Directives; FOKKER AIRCRAFT Model F-28 Series Airplanes |
| aircraft | Fokker Services | F.28 Mark 4000 | Airworthiness Directives; FOKKER AIRCRAFT Model F-28 Series Airplanes |
Unsafe Condition
Reduced directional control capability due to insufficient stops in the rudder pedal mechanism.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Install stops in the rudder pedal mechanism per Fokker Service Bulletin F28/27-158 within six months after the effective date. Alternate means of compliance may be approved by the Manager, Standardization Branch, ANM-113.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Within six months after the effective date of this AD
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
Fokker Aircraft Model F-28 series airplanes, Serial Numbers 11003 to 11231 inclusive, 11991 and 11992
AI-generated summary from the source AD text. Verify against the official source before acting.
Federal Register Abstract
Rudder Pedal
Applicability Source Text
Show captured applicability text from the source AD
AD Final Rules - DRS_88-05-04.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 88-05-04 Document Type: AD Final Rules Docket Number: Unknown Subject Heading: Airworthiness Directives; FOKKER AIRCRAFT Model F-28 Series Airplanes Subject: Rudder Pedal Status: Current Citation: This information is not available. Citation Publish Date: Effective Date: 04/08/1988 Make: Fokker Services Model: F.28 Mark 0070 | F.28 Mark 0100 | F.28 Mark 1000 | F.28 Mark 2000 | F.28 Mark 3000 | F.28 Mark 4000 Product Type: Aircraft Product Subtype: Large Airplane Affected AD: Superseded AD: Affected By: Superseded By: Service/Office: Office of Primary Responsibility: CFR Part Reference: Part 39 Comments: AIRWORTHINESS DIRECTIVES FINAL RULES: 88-05-04 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: Unknown AMENDMENT: 39-5862 AD NUMBER: 88-05-04 SUBJECT HEADING: Airworthiness Directives; FOKKER AIRCRAFT Model F-28 Series Airplanes ACTION: SUMMARY: DATES: Effective April 8, 1988. ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 88-05-04 FOKKER AIRCRAFT: Amendment 39-5862. Applies to Model F-28 series airplanes, Serial Numbers 11003 to 11231 inclusive, 11991 and 11992, certificated in any category. Compliance required as indicated, unless previously accomplished. To prevent reduced directional control capability, accomplish the following: A. Within the next six months after the effective date of this AD, install stops in the rudder pedal mechanism in accordance with Fokker Service Bulletin F28/27-158, dated November 15, 1985. B. An alternate means of compliance or adjustment of compliance time, which provides an acceptable level of safety, may be used when approved by the Manager, Standardization Branch, ANM-113, FAA, Northwest Mountain Region. C. Special flight permits may be issued in accordance with FAR 21.197 and 21.199 to operate airplanes to a base for the accomplishment of inspections and/or modifications required by this AD. All persons affected by this directive who have not already received the appropriate service documents from the manufacturer may obtain copies upon request to Fokker Aircraft USA, 1199 N. Fairfax St., Alexandria, Virginia 22314. These documents may be examined at the FAA, Northwest Mountain Region, 17900 Pacific Highway South, Seattle, Washington, or at the Seattle Aircraft Certification Office, 9010 East Marginal Way South, Seattle, Washington. This amendment becomes effective April 8, 1988. FOOTER:
Document Text
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AD Final Rules - DRS_88-05-04.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 88-05-04 Document Type: AD Final Rules Docket Number: Unknown Subject Heading: Airworthiness Directives; FOKKER AIRCRAFT Model F-28 Series Airplanes Subject: Rudder Pedal Status: Current Citation: This information is not available. Citation Publish Date: Effective Date: 04/08/1988 Make: Fokker Services Model: F.28 Mark 0070 | F.28 Mark 0100 | F.28 Mark 1000 | F.28 Mark 2000 | F.28 Mark 3000 | F.28 Mark 4000 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: 88-05-04 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: Unknown AMENDMENT: 39-5862 AD NUMBER: 88-05-04 SUBJECT HEADING: Airworthiness Directives; FOKKER AIRCRAFT Model F-28 Series Airplanes ACTION: SUMMARY: DATES: Effective April 8, 1988. ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 88-05-04 FOKKER AIRCRAFT: Amendment 39-5862. Applies to Model F-28 series airplanes, Serial Numbers 11003 to 11231 inclusive, 11991 and 11992, certificated in any category. Compliance required as indicated, unless previously accomplished. To prevent reduced directional control capability, accomplish the following: A. Within the next six months after the effective date of this AD, install stops in the rudder pedal mechanism in accordance with Fokker Service Bulletin F28/27-158, dated November 15, 1985. B. An alternate means of compliance or adjustment of compliance time, which provides an acceptable level of safety, may be used when approved by the Manager, Standardization Branch, ANM-113, FAA, Northwest Mountain Region. C. Special flight permits may be issued in accordance with FAR 21.197 and 21.199 to operate airplanes to a base for the accomplishment of inspections and/or modifications required by this AD. All persons affected by this directive who have not already received the appropriate service documents from the manufacturer may obtain copies upon request to Fokker Aircraft USA, 1199 N. Fairfax St., Alexandria, Virginia 22314. These documents may be examined at the FAA, Northwest Mountain Region, 17900 Pacific Highway South, Seattle, Washington, or at the Seattle Aircraft Certification Office, 9010 East Marginal Way South, Seattle, Washington. This amendment becomes effective April 8, 1988. FOOTER:
Source: Official FAA Source ↗
Retrieved: Apr 8, 2026
Rights: U.S. Government Public Domain
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