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93-22-03: Inspect Rudder Pedal Assemblies

FAA order 93-22-03 is an airworthiness directive in force since December 16, 1993. The FAA's subject line: Inspect Rudder Pedal Assemblies. System: flight controls.

What it applies to as the FAA lists it

Kind of product
Aircraft
Makes
—
Models
F.28 Mark 0100

Dates and paperwork

In force since
December 16, 1993
Docket
93-NM-78-AD
Status
Current
The FAA's document
Read the order on the FAA's site

The order itself the regulatory text, as published

Show the full text (2,620 characters)
93-22-03 FOKKER: Amendment 39-8728. Docket 93-NM-78-AD. Applicability: Model F28 Mark 0100 series airplanes; serial numbers 11244 through 11407, inclusive, 11409, and 11410; certificated in any category. Compliance: Required as indicated, unless accomplished previously. To prevent reduced braking authority and reduced directional control of the airplane while it is on the ground, accomplish the following: (a) Within 30 days after the effective date of this AD, conduct an inspection of the rudder (brake) pedal assemblies, to verify installation of retainer rings, part number (P/N) MS16624-1075, in accordance with Fokker Service Bulletin SBF100-27-047, Revision 1, dated February 9, 1993. (1) If all of the retainer rings are installed correctly, no further action is required by this AD. (2) If any retainer ring is not installed, or is not installed correctly, prior to further flight, install retainer ring, P/N MS16624-1075, in accordance with the service bulletin. (b) An alternative method of compliance or adjustment of the compliance time that provides an acceptable level of safety may be used if approved by the Manager, Standardization Branch, ANM-113, FAA, Transport Airplane Directorate. Operators shall submit their requests through an appropriate FAA Principal Maintenance Inspector, who may add comments and then send it to the Manager, Standardization Branch, ANM-113. NOTE: Information concerning the existence of approved alternative methods of compliance with this AD, if any, may be obtained from the Standardization Branch, ANM-113. (c) Special flight permits may be issued in accordance with FAR 21.197 and 21.199 to operate the airplane to a location where the requirements of this AD can be accomplished. (d) The inspection and necessary installation shall be done in accordance with Fokker Service Bulletin SBF100-27-047, Revision 1, dated February 9, 1993, which contains the following list of effective pages: Page Number Revision Level Shown on Page Date Shown on Page 1 1 February 9, 1993 2-4 Original August 28, 1992 This incorporation by reference was approved by the Director of the Federal Register in accordance with 5 U.S.C. 552(a) and 1 CFR Part 51. Copies may be obtained from Fokker Aircraft USA, Inc., 1199 North Fairfax Street, Alexandria, Virginia 22314. Copies may be inspected at the FAA, Transport Airplane Directorate, 1601 Lind Avenue, SW., Renton, Washington; or at the Office of the Federal Register, 800 North Capitol Street, NW., suite 700, Washington, DC. (e) This amendment becomes effective on December 16, 1993.

Source: FAA Dynamic Regulatory System, airworthiness directives. The FAA's document is the authority; the register counts are this site's, from the FAA register of November 6, 2026. Connections as data: /graph/directive/93-22-03.json · aircraft systems.