AD 93-03-02

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AD Number:
93-03-02
Document Type:
AD Final Rules
Docket Number:
93-CE-09-AD
Subject Heading:
Airworthiness Directives; Beech Models F33A, A36, B36TC and 58 Airplanes
Subject:
Loran Receiver System
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
03/12/1993
Make:
Textron Aviation Inc.
Model:
58 | A36 | B36TC | F33A
Product Type:
Aircraft
Product Subtype:
Small 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Superseded AD: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Superseded By: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: 93-03-02
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   93-CE-09-AD

AMENDMENT:   39-8501

AD NUMBER:   93-03-02

SUBJECT HEADING:   Airworthiness Directives; Beech Models F33A, A36, B36TC and 58 Airplanes

ACTION:  

SUMMARY:  

DATES:   Effective March 12, 1993

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
93-03-02 BEECH AIRCRAFT CORPORATION: Amendment 39-8501; Docket No. 93-CE-09-AD.

Applicability: The following model and serial number airplanes equipped with a Bendix/King KLN-88 Loran receiver system, certificated in any category:


Models	Serial Numbers
F33A	CE-1620, CE-1640, CE-1655, CE-1659,
CE-1662, CE-1680, CE-1682, and CE-1693
A36	E-2563, E-2564, E-2575, E-2582, E-2599,
E-2604, E-2614, E-2631, E-2633, E-2643,
E-2645, E-2650, E-2660, E-2664, E-2673,
E-2675, E-2680, E-2681, E-2688, E-2690,
E-2693, E-2695, E-2698, E-2711, E-2727,
E-2728, E-2737, E-2738, E-2743, E-2746, and E-2752.
B36TC	EA-515, EA-516, EA-519, EA-522, EA-524, and EA-529.
58	TH-1581, TH-1588, TH-1592, TH-1597,
TH-1598, TH-1599, TH-1600, TH-1602,
TH-1612, TH-1616, TH-1621, TH-1623,
TH-1627, TH-1628, TH-1632, TH-1633,
TH-1640, TH-1642, TH-1646, TH-1650,
TH-1651, TH-1653, TH-1661, TH-1663,
TH-1668, TH-1672, and TH-1673.

Compliance: Required within the next 50 hours time-in-service after the effective date of this AD, unless already accomplished.

To prevent the display of a Loran lateral deviation signal when the instrument landing system localizer frequency is selected, which could result in navigational errors, accomplish the following:

(a) Modify the wiring configuration of the switching system between the Bendix/King KLN-88 Loran receiver system and the instrument landing system localizer in accordance with the ACCOMPLISHMENT INSTRUCTIONS section of Beech Service Bulletin No. 2496, dated January 1993.

(b) 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.

(c) An alternative method of compliance or adjustment of the compliance time that provides an equivalent level of safety may be approved by the Manager, Wichita Aircraft Certification Office, FAA, 1801 Airport Road, Room 100, Wichita, Kansas 67209. The request shall be forwarded through an appropriate FAA Maintenance Inspector, who may add comments and send it to the Manager, Wichita Aircraft Certification Office.

NOTE: Information concerning the existence of approved alternative methods of compliance with this AD, if any, may be obtained from the Wichita Aircraft Certification Office.

(d) The modification required by this AD shall be done in accordance with Beech Service Bulletin No. 2496, dated January 1993. 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 the Beech Aircraft Corporation, P.O. Box 85, Wichita, Kansas 67201-0085. Copies may be inspected at the FAA, Central Region, Office of the Assistant Chief Counsel, Room 1558, 601 E. 12th Street, Kansas City, Missouri, or at the Office of the Federal Register, 800 North Capitol Street, NW., suite 700, Washington, DC.

(e) This amendment (39-8501) becomes effective on March 12, 1993.

FOOTER: