- Effective
- December 17, 1986
- Model
- Lake Model 250
- Data sheet
- TCDS1A13
- Product
- Aircraft · Small airplane
- Amendment
- 39-5461
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.
Copies of the files this page was built from, with their SHA-256. Retrieved October 18, 2026.
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|---|---|---|---|
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On this page
The airworthiness directive
86-23-05 CONSOLIDATED AERONAUTICS INCORPORATED: Amendment 39-5461. Applies to Consolidated Aeronautics Incorporated, Lake Model 250 Airplanes, Serial Numbers 2 through 17, equipped with fuel shutoff valve mounting plate part number 3-6572-17, certificated in any category.
Compliance: Required within the next 100 hours time-in-service after the effective date of this AD, unless already accomplished.
To prevent the possible contact of the fuel shutoff valve handle hardware and the cabin rear upholstery panel, accomplish the following: (a) Modify the fuel shutoff valve mounting plate in accordance with instructions in Lake Aircraft Division Consolidated Aeronautics Incorporated Service Bulletin No. B-66 dated May 31, 1985.
(b) Airplanes may be flown in accordance with FAR 21.197 to a location where this AD can be accomplished.
(c) An equivalent means of compliance with this AD may be used if approved by the Manager, Federal Aviation Administration, Boston Aircraft Certification Office, ANE-150, 12 New England Executive Park, Burlington, Massachusetts 01803.
All persons affected by this directive may obtain copies of the documents referred to herein upon request to Lake Aircraft, Laconia Airport, Laconia, New Hampshire 03646; or Federal Aviation Administration, Office of the Regional Counsel, Room 158, 601 East 12th Street, Kansas City, Missouri 64106.
This amendment becomes effective on December 17, 1986.
Affected TCDS · 1
The type certificate data sheets for the models this AD names, matched by model and maker.