AD 92-18-08

Airworthiness directive · Flight Control Systems · Piper PA-46-310P and PA-46-350P

Effective
October 2, 1992
Published
August 17, 1992
Issued
August 10, 1992
Models
PA-46-310P, PA-46-350P
Data sheet
TCDSA25SO
Registered aircraft
897 matched by model
Product
Appliance
Amendment
39-8352
Docket
92-CE-07-AD

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 November 21, 2025.

On this page

The airworthiness directive

92-18-08 BENDIX/KING: Amendment 39-8352. Docket No. 92-CE-07-AD.

Applicability: KAP 150/KFC 150 Flight Control Systems installed on Piper Models PA-46-310P and PA-46-350P airplanes, certificated in any category.

Compliance: Required within the next 90 calendar days after the effective date of this AD, unless already accomplished.

To prevent moisture from entering the electronic circuit board through the pitch servo, which could possibly lead to undesired movement of the elevator, accomplish the following:

(a) Install a pitch servo cover kit, part number 050-03007-0000, in accordance with the instructions in Bendix/King Installation Bulletin No. 312, dated March 19, 1990.

NOTE 1: Installation of the yaw servo cover kit, part number 050-03006-0000, which is referenced in Bendix/King Installation Bulletin No. 312, is not required by this AD action.

(b) Special flight permits may be issued in accordance with FAR 21.197 and 21.199 to operate airplanes to a location where the requirements of this AD can be accomplished.

(c) An alternative method of compliance or adjustment of the compliance time that provides an equivalent level of safety may be approved by the Manager, Wichita Aircraft Certification Office, 1801 Airport Road, Room 100, Mid-Continent Airport, Wichita, Kansas 67209. The request shall be forwarded through an appropriate FAA Maintenance Inspector, who may add comments and then send it to the Manager, Wichita Aircraft Certification Office.

NOTE 2: Information concerning the existence of approved alternative methods of compliance with this AD, if any, may be obtained from the Wichita Aircraft Certification Office.

(d) The installation required by this AD shall be done in accordance with Bendix/King Installation Bulletin No. 312, dated March 19, 1990. This incorporation by reference was approved by the Director of the Federal Register in accordance with 5 U.S.C. 552(a) and 1 CFR Part 51. Copies may be obtained from Bendix/King, Product Support Department, 400 N. Rogers Road, Olathe, Kansas 66062-0212. Copies may be inspected at the FAA, Central Region, Office of the Assistant Chief Counsel, Room 1558, 601 E. 12th Street, Kansas City, Missouri, or at the Office of the Federal Register, 800 North Capitol Street, NW, suite 700, Washington, DC.

(e) This amendment becomes effective on October 2, 1992.

Affected TCDS · 1

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

Registered aircraft · 897

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
  • Piper880 aircraft
  • New Piper17 aircraft
By year built
19772026
Registered aircraft by year built: 820 aircraft
19771
19835
198444
198546
198647
198726
198819
198935
199013
19911
19922
19938
199412
199520
199633
199730
199825
199939
200036
20013
200212
20034
20047
20057
200612
200715
20087
20092
201021
201124
201236
201332
201427
201527
201621
20173
201815
201917
20207
202114
202211
202317
202418
202513
20266

77 with no year recorded

By model

Aircraft

See all 897 aircraft