AD 83-17-06

Airworthiness directive · Aileron Balance Weights · Flap actuated aileron droop system (Sierra Industries STC SA1382WE or 5 others)

Effective
September 1, 1983
Models
150D, 150E, 150F, 150G, 150H, 150J and 56 more
Registered aircraft
37,488 matched by model
Product
Aircraft · Small airplane
Amendment
39-4716

Unofficial copy of the text in the FAA’s Dynamic Regulatory System. The FAA’s own copy is the authoritative one. DRS record last changed May 30, 2024.

On this page

The airworthiness directive

83-17-06 CESSNA: Amendment 39-4716. Applies to Models 180 through 180H, 180J and 180K airplanes, modified per Robertson STC SA1435WE; 150D through 150L airplanes, modified per Robertson STC SA2191WE; 150D through 150L airplanes, modified per Robertson STC SA2192WE; 185, 185A through 185E, A185E and A185F airplanes, modified per Robertson STC SA1441WE; 182 through 182R, R182, T182 and TR182 airplanes, modified per Robertson STC SA1382WE; and 172, 172A through 172P airplanes, modified per Robertson STC SA1689WE airplanes certificated in any category.

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

To prevent possible destructive aileron flutter, accomplish the following:

a) Check the permanent aircraft records of the airplane to determine if it has been modified per the applicable STC at Robertson Aircraft Corporation Repair Station No. 415-23 prior to August 1, 1983. If not, no furtheraction is necessary. If, modified at this facility before this date, inspect and, if necessary, correct the aileron balance weight installation in accordance with paragraph b) of this AD.

b) Measure the height of all aileron balance weights. If the measured height of all weights is approximately 3/4 inch, the weights are correctly installed and no further action is necessary. If the measured height of any weight is approximately 1/2 inch, prior to further flight, install new balance weights of the appropriate part number in accordance with the applicable STC data or Robertson Service Bulletin No. 20. Rebalance the ailerons within the limits specified by the Cessna Aircraft Company Service Manual for the airplane involved.

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

d) An equivalent method of compliance with this AD may be used if approved by the Manager, Seattle Aircraft Certification Office, FAA, NorthwestMountain Region, 9010 East Marginal Way South, Seattle, Washington 98168.

This amendment becomes effective on September 1, 1983.

Affected TCDS · 5

The type certificate data sheets for the models this AD names, matched by model and maker.

Registered aircraft · 37,488

Registered aircraft whose airframe or engine model this AD names. Matched by model only, so check each against the AD’s applicability.

By aircraft maker
  • Cessna37,485 aircraft
  • Cessna Wren3 aircraft
By year built
19412012
Registered aircraft by year built: 31,742 aircraft
19411
19431
19471
19511
19522
1953236
1954230
1955429
19561,084
1957745
1958736
1959745
1960666
1961648
1962686
1963815
19641,197
19651,568
19662,184
19671,332
19681,595
19691,357
1970691
1971750
19721,189
19731,649
19741,276
19751,587
19761,592
19771,415
19781,606
19791,502
1980681
1981712
1982259
1983120
1984143
1985214
198691
19881
19931
19971
20091
20122

5,746 with no year recorded

By model

See all 65 models

Aircraft

See all 37,488 aircraft