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AIRWORTHINESS DIRECTIVES FINAL RULES: 86-24-07
CITATION: This information is not available.
PAGE NUMBER:
DOCKET NUMBER: Unknown
AMENDMENT: 39-5475
AD NUMBER: 86-24-07
SUBJECT HEADING: Airworthiness Directives; Cessna Models 150C thru 150M, A150K thru A150M,
152, A152, 172D thru 172N, R172K, P172D, 177 thru 177B, 177RG, 180F thru 180K, 182F thru 182Q,
R182, 185B thru 185E, A185E, A185F, 188, A188, A188A, 188B, A188B, 205, 205A, 206, U206, U206A
thru U206G, TU206A thru TU206G, P206, P206A thru P206E, TP206A thru TP206E, 207, 207A, T207,
T207A, 210C thru 210M, T210K thru T210M, T210F thru T210J, P210N, F150F thru F150M, FA150K,
FA150L, FRA150L, FRA150M, F152, FA152, FP172, F172D thru F172N, FR172E thru FR172K, F177RG,
F182P, F182Q, FR182, R172E thru R172H
ACTION:
SUMMARY:
DATES: Effective January 7, 1987.
ADDRESSES:
FOR FURTHER INFORMATION CONTACT:
SUPPLEMENTARY INFORMATION:
REGULATORY TEXT:
86-24-07 CESSNA: Amendment 39-5475. Applies to the following model and serial number single-engine
airplanes certificated in any category manufactured thru Model year 1978 equipped with ball type rod ends
on the engine controls.
MODELS SERIAL NUMBERS
150C thru 150M S/N 15059701 thru 15079405
A150K thru A150M S/N A1500001 thru A1500734
152 S/N 15279406 thru 15282031
A152 S/N A1520735 thru A1520808
172D thru 172N S/N 17249545 thru 17271034
R172K S/N R1722000 thru R1722929
P172D S/N P17257120 thru P17257188
177 thru 177B S/N 17700001 thru 17702752
177RG S/N 177RG0001 thru 177RG1366
180F thru 180K S/N 18051184 thru 18053000
182F thru 182Q S/N 18254424 thru 18266590
R182 S/N R18200001 thru R18200583
185B thru 185E S/N 185-0513 thru 185-1599
A185E, A185F S/N 18501600 thru 18503683
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188, A188 S/N 188-0001 thru 188-0572
A188A, 188B S/N 18800573 thru 18803296
A188B S/N 18800967T thru 18803296T
205, 205A S/N 205-0001 thru 205-0577
206, U206 S/N 206-0001 thru 206-0275
U206A thru U206G S/N U206-0276 thru U206-1444
TU206A thru TU206G S/N U20601445 thru U20604649
P206, P206A thru P206E S/N P206-0001 thru P206-0603
TP206A thru TP206E S/N P20600604 thru P20600647
207, 207A, T207, T207A S/N 20700001 thru 20700482
210C thru 210M and S/N 21058086 thru 21062954
T210K thru T210M
T210F thru T210J S/N T210-0001 thru T210-0454
P210N S/N P21000001 thru P21000150
F150F thru F150M S/N F150-0001 thru F150-0529
S/N F15000530 thru F15001428
FA150K, FA150L S/N FA1500001 thru FA1500120
FRA150L, FRA150M S/N FRA1500121 thru FRA1500336
F152 S/N F15201429 thru F15201528
FA152 S/N FA1520337 thru FA1520347
FP172 S/N FP172-0001 thru FP172-0003
F172D thru F172N S/N F172-0001 thru F172-0654
S/N F17200655 thru F17201749
FR172E thru FR172K S/N FR17200001 thru FR17200630
F177RG S/N F177RG0001 thru F177RG0177
F182P, F182Q S/N F18200001 thru F18200094
FR182 S/N FR18200001 thru FR18200020
R172E thru R172H S/N R172-0001 thru R172-0409
S/N R1720410 thru R1720625
Compliance: Required within the next 100 hours time-in-service after the effective date of this AD, unless
already accomplished.
To prevent engine power interruption due to loss of attachment of the engine controls, accomplish the
following:
(a) Modify the engine controls installation by installing a drilled steel bolt, AN3l0 type castellated nut and a
steel cotter pin in accordance with Cessna Single-Engine Customer Care Service Information Letter SE79-6.
(b) Airplanes may be flown in accordance with FAR 21.197 to a location where this AD can be
accomplished.
(c) An equivalent means of compliance with this AD may be used if approved by the Manager, Wichita
Aircraft Certification Office, Federal Aviation Administration, 1801 Airport Road, Room 100, Mid-Continent
Airport, Wichita, Kansas 67209.
All persons affected by this directive may obtain copies of the document(s) referred to herein upon request to
Cessna Aircraft Company, Customer Services, Post Office Box 1521, Wichita, Kansas 67201; or the FAA,
Rules Docket, Office of the Regional Counsel, Room 1558, 601 East 12th Street, Kansas City, Missouri
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64106.
This amendment becomes effective on January 7, 1987.
FOOTER:
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