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83-17-06: Aileron Balance Weights

FAA order 83-17-06 is an airworthiness directive in force since September 1, 1983. The FAA's subject line: Aileron Balance Weights. It names Cessna 150, Cessna 172 Skyhawk, Cessna 180 Skywagon, Cessna 182 Skylane, Cessna 185 Skywagon, Cessna A185 Skywagon, Cessna R182 Skylane RG, Cessna T182 Turbo Skylane, Cessna TR182 Turbo Skylane RG: about 46,804 aircraft on the U.S. register today across them, though an order usually covers particular versions or serial numbers rather than every one. System: flight controls.

What it applies to as the FAA lists it

Kind of product
Aircraft
Makes
Cessna Aircraft Company
Models
150D, 150E, 150F, 150G, 150H, 150J, 150K, 150L, 172, 172A, 172B, 172C, 172D, 172E, 172F (USAF T-41A), 172G, 172H (USAF T-41A), 172I, 172K, 172L, 172M, 172N, 172P, 180, 180A, 180B, 180C, 180D, 180E, 180F, 180G, 180H, 180J, 180K, 182, 182A, 182B, 182C, 182D, 182E, 182F, 182G, 182H, 182J, 182K, 182L, 182M, 182N, 182P, 182Q, 182R, 185, 185A, 185B, 185C, 185D, 185E, A185E, A185F, R182, T182, TR182
On this site
Cessna 150 7,995 registered
Cessna 172 Skyhawk 20,670 registered
Cessna 180 Skywagon 2,606 registered
Cessna 182 Skylane 11,828 registered
Cessna 185 Skywagon 227 registered
Cessna A185 Skywagon 1,372 registered
Cessna R182 Skylane RG 706 registered
Cessna T182 Turbo Skylane 935 registered
Cessna TR182 Turbo Skylane RG 465 registered

Dates and paperwork

In force since
September 1, 1983
Docket
Unknown
Status
Current
The FAA's document
Read the order on the FAA's site

The order itself the regulatory text, as published

Show the full text (2,115 characters)
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.

Related safety bulletins advice on the same designs, not orders

2026-03-242026-08 · Floats
2025-07-282025-07 · Reciprocating Engine Supercharger
2022-12-06CE-19-01 R1 · Engine Oil and Airplane Hour Meter; Pressure Switch Failure
2021-08-26AIR-21-16 · FLIGHT COMPARTMENT EQUIPMENT, Cessna Seat Back Attachment Bolt Inspection
2019-02-12CE-19-01 · Engine Oil and Airplane Hour Meter; Pressure Switch Failure

Source: FAA Dynamic Regulatory System, airworthiness directives. The FAA's document is the authority; the register counts are this site's, from the FAA register of October 8, 2026. Connections as data: /graph/directive/83-17-06.json · aircraft systems.