AD 93-22-03

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AD Number:
93-22-03
Document Type:
AD Final Rules
Docket Number:
93-NM-78-AD
Subject Heading:
Airworthiness Directives; FOKKER Model F28 Mark 0100 Series Airplanes
Subject:
Inspect Rudder Pedal Assemblies
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
12/16/1993
Make:
Model:
F.28 Mark 0100
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Superseded AD: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Superseded By: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: 93-22-03
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   93-NM-78-AD

AMENDMENT:   39-8728

AD NUMBER:   93-22-03

SUBJECT HEADING:   Airworthiness Directives; FOKKER Model F28 Mark 0100 Series Airplanes

ACTION:  

SUMMARY:  

DATES:   Effective December 16, 1993.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
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.

FOOTER: