AD 85-03-01

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AD Number:
85-03-01
Document Type:
AD Final Rules
Docket Number:
Unknown
Subject Heading:
Airworthiness Directives; Cessna Model 205, 206, U206, U206A, U206B, U206C, U206D, TU206A, TU206B, T...Show more
Subject:
Throttle and Mixture Controls
Status:
Current
Citation:
This information is not available.
Citation Publish Date:
Effective Date:
03/15/1985
Make:
Cessna Aircraft Company
Model:
206 | 207 | 210-5 (205) | 210B | 210C | 210D | 210E | 210F | 210G | 210H | 210J | P206 | P206A | P20...Show more
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Superseded AD: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Superseded By: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:
Updated RGL applicability to match AD applicability; CAR C-11-185
AIRWORTHINESS DIRECTIVES FINAL RULES: 85-03-01
CITATION:   This information is not available.

PAGE NUMBER:  

DOCKET NUMBER:   Unknown

AMENDMENT:   39-4995

AD NUMBER:   85-03-01

SUBJECT HEADING:   Airworthiness Directives; Cessna Model 205, 206, U206, U206A, U206B, U206C, U206D, TU206A, TU206B, TU206C, TU206D P206, P206A, P206B, P206C, P206D, TP206A, TP206B, TP206C, TP206D, 207, and T207, 210B, 210C, 210D, 210E, 210F, 210G, 210H, 210J, T210F, T210G, T210H and T210J Airplanes

ACTION:  

SUMMARY:  

DATES:   Effective March 15, 1985.

ADDRESSES:  

FOR FURTHER INFORMATION CONTACT:  

SUPPLEMENTARY INFORMATION:  

REGULATORY TEXT:  
85-03-01 CESSNA: Amendment 39-4995. Applies to Models 205 (S/Ns 205-0001 thru 205- 0479); 206, U206, U206A, U206B, U206C, U206D, TU206A, TU206B, TU206C, and TU206D (S/Ns 206-0001 thru U206-1444); P206, P206A, P206B, P206C, P206D, TP206A, TP206B, TP206C, and TP206D (S/Ns P206-0001 thru P206-0603); 207 and T207 (S/Ns 20700001 thru 20700148) 210B, 210C, 210D, 210E, 210F, 210G, 210H, and 210J (S/Ns 21057841 thru 21059199); T210F, T210G, T210H, and T210J (S/Ns T210-O001 thru T210-0454) airplanes certificated in any category.

Compliance: Required within 100 hours time-in-service after the effective date of this AD, unless already accomplished.

To reduce the possibility of engine controls failure and loss of engine power control accomplish the following:

(a) Visually inspect the ends of the engine throttle and mixture control cables to determine if the sleeve and bushing are secured by a drive screw. If so, inspect, modify, and/or replace engine throttle and mixture controls in accordance with Cessna Single-Engine Service Letter SE69-16 dated July 22, 1969.

(b) The airplane may be flown in accordance with FAR 21.197 to a location where this AD may be accomplished provided reduced mixture selection during flight is not performed and the throttle and mixture controls are determined to be functioning properly during preflight inspection of the airplane.

(c) An equivalent means of compliance with this AD may be used if approved by the Manager, Wichita Aircraft Certification Office, FAA, 1801 Airport Road, Room 100, Mid- Continent Airport, Wichita, Kansas 67209; telephone (316) 946-4400.

This amendment becomes effective on March 15, 1985.

FOOTER: