AD 86-26-04 SUPERSEDED

86-26-04 CESSNA: Amendment 39-5503. Applies to the following airplanes certificated in any category:

MODELS
SERIAL NUMBERS
120, 140
All
140A
All
150
17001 thru 17,999; 59001 thru 59018
150A, 150B, 150C, 150D
150E, 150F, 150G, 150H
150J, 150K, 150L

15059019 thru 15072003
F150F, F150G, F150H
F150-0001 thru F150-0529
F150K
F15000530 thru F15000658
170, 170A, 170B
All
172, 172A
28,000 thru 29,999
36,000 thru 36,999
46,001 thru 47,746
172B, 172C, 172D, 172E,
172F, 172G, 172H,
172I, 172K

17247747 thru 17259223
F172D, Fl72E, F172F, F172G
F172-0001 thru Fl72-0654
F172H
F17200655 thru F17200754
FR172E, FR172F, FR172G
FR1720000l thru FR17200225
P172D
All
175, 175A, 175B, 175C
All
177, 177A, 177B
17700001 thru 17701530
180, 180A
30000 thru 32999
180A, 180B, 180C,

50,000 thru 50911
180D, 180E, 180F, 180G, 180H
18050912 thru 18052175
182, 182A, 182B,
33,000 thru 34999
182C
51,001 thru 53,007
182D, 182E, 182F
182G, 182H, 182J
182K, 182L, 182M, 182N

18253008 thru 18260445
185, 185A, 185B, 185C
185D, 185E, A185E

185-0001 thru 185-1599
A185E
18501600 thru 18501832
190, 195, 195A, 195B
All
205, 205A
All
206
All
U206, U206A, U206B, U206C, U206D, TU206A, TU206B, TU206C, TU206D

206-0276 thru 206-1444
U206E, TU206E
20601445 thru 20601587
P206, P206A, P206B,
P206C, P206D, TP206A,
TP206B, TP206C, TP206D

P206-0001 thru P206-0603
P206E, TP206E
P20600604 thru P20600647
207, T207
2070001 thru 20700190
210
57001 thru 57575
210A, 210B, 210C, 210D
210E, 210F, 210G, 210H,
210J, 210K, T210K

21057576 thru 21059351
T210G, T210H, T210J
All
336
All
337, 337A, 337B, 337C
337D, 337E, T337B,
T337C, T337, T337E

33700001 thru 33701316

Compliance: Required within the next 25 hours time-in-service (TIS) after the effective date of this AD, unless already accomplished.

To prevent slippage of the pilot/co-pilot shoulder harnesses, accomplish the following on airplanes which have had the shoulder harnesses installed by any of the following Cessna Accessory Kits (AK):

AK140-10
AK182-75
AK210-172
AK150-7
AK195-10
AK210-173
AK150-121
AK210-77
AK210-174
AK170-10
AK210-93
AK336-32
AK177-10
AK210-171
AK336-36

AK336-103

(a) Inspect the upper shoulder harness adjuster in accordance with Cessna Single Engine Service Bulletin, SEB86-8 or Cessna Multi-Engine Service Bulletin, MEB86-22, as appropriate, for the presence of a retainer spring. If installed, prior to further flight, remove the spring and stamp out the -401 identification number in accordance with the service bulletin instructions.

NOTE: There are two adjusters in each shoulder harness assembly. This AD applies only to the upper adjuster.

(b) Airplanes may be flown in accordance with FAR 21.197 to a location where this AD may be accomplished.

(c) The holder of a pilot certificate issued under Part 61 of the Federal Aviation Regulations (FAR) on any airplane owned or operated by him may conduct the inspections and modifications required by this AD on any airplane not used in air carrier service. The person accomplishing this AD must make the appropriate maintenance record entry as prescribed by FAR 91.173.

(d) Any equivalent method of compliance with this AD, if used, must be approved by the Manager, Wichita Aircraft Certification Office, Federal Aviation Administration, 1801 Airport Road, Room 100, Wichita, Kansas 67209; Telephone (316) 946-4400.

All persons affected by this directive may obtain copies of the documents referred to herein upon request to Cessna Aircraft Company, Customer Service, P.O. Box 1521, Wichita, Kansas 67201; or FAA, Office of the Regional Counsel, Room 1558, 601 East 12th Street, Kansas City, Missouri 64106.

This amendment becomes effective January 6, 1987.