The U.S. aircraft register, updated daily
FAA orders · airworthiness directive · current

92-07-07: Flaps and Ailerons

FAA order 92-07-07 is an airworthiness directive in force since April 30, 1992. The FAA's subject line: Flaps and Ailerons. It names Eiriavion Oy PIK 20: about 56 aircraft on the U.S. register today, 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
Eiriavion Oy
Models
PIK-20, PIK-20B
On this site
Eiriavion Oy PIK 20 56 registered

Dates and paperwork

In force since
April 30, 1992
Docket
91-CE-35-AD
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 (2,697 characters)
92-07-07 EIRIAVION: Amendment 39-8203. Docket No. 91-CE-35-AD. Applicability: Models PIK-20 and PIK-20B sailplanes (all serial numbers) that are equipped with lead mass balance strips on the flaps and ailerons, certificated in any category. Compliance: Required within the next 25 hours time-in-service (TIS) after the effective date of this AD, unless already accomplished, and thereafter at intervals not to exceed 500 hours TIS. To prevent interference to the ailerons that could result in loss of control of the sailplane, accomplish the following: (a) Remove the flaps and ailerons and inspect the lead mass balance strips for cracks using a 10-power magnifying glass. NOTE 1: Particular attention should be given to the attachment rivets during the inspections specified in paragraph (a) of this AD. NOTE 2: If the sailplane is not equipped with mass balance strips on the flaps and ailerons, then no further action is required by this AD. (b) If cracking is detected in accordance with the inspections required by paragraph (a) of this AD, prior to further flight, fabricate and replace the mass balance strips in accordance with the following: (1) Utilize strips made of malleable lead (not brittle or granular) that are the same weight and dimensions. (2) Attach the strips at the same rivet holes as the cracked one and bond the lead in place with epoxy resin. (3) Keep the counter bore holes to the minimum depth in accordance with the applicable service manual. (4) Install washers to the rivets on the glass-reinforced plastic face. (5) Do not increase the diameter of any rivet. (6) Ensure that the final mass balance of each flap and aileron complies with the applicable service manual. (c) Special flight permits may be issued in accordance with FAR 21.197 and 21.199 to operate the sailplane to a location where the requirements of this AD can be accomplished. (d) An alternative method of compliance or adjustment of the compliance time that provides an equivalent level of safety may be approved by the Manager, Brussels Aircraft Certification Staff, Europe, Africa, Middle East office, FAA, c/o American Embassy, 1000 Brussels, Belgium. The request should be forwarded through an FAA Maintenance Inspector, who may add comments and then send it to the Manager, Brussels Aircraft Certification Staff. (e) All persons affected by this directive may examine information that is related to this AD upon request to the FAA, Central Region, Office of the Assistant Chief Counsel, Room 1558, 601 E. 12th Street, Kansas City, Missouri 64106. (f) This amendment (39-8203, AD 92-07-07) becomes effective on April 30, 1992.

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 23, 2026. Connections as data: /graph/directive/92-07-07.json · aircraft systems.