AD 61-09-01

Active

Elevator Hydraulic Damper Housing

Key Information
61-09-01
Active
April 07, 1961
Not specified
Unknown
N/A
Applicability
["Aircraft"]
["Large Airplane"]
Lockheed Martin Corporation
188A 188C
Regulatory Text

61-09-01 LOCKHEED: Amdt. 279 Part 507 Federal Register April 28, 1961. Applies to All 188 Series Aircraft Which Incorporate Hydraulic Damper Housing P/N's 840655-1 and 475645-1 (rudder, elevator, and aileron control systems) Installed Per Lockheed Service Bulletin 88/SB-524 and 88/SB-532.

Compliance required not later than the next 50 hours' time in service.

As a result of an incident involving elevator booster hydraulic damper malfunction, hydraulic damper housing P/N 840655-1 and P/N 475645-1 not identified with blue anodized color must be replaced with new parts identified with blue anodized color as received from the manufacturer or reworked to the following dimensions:

(a) Length of skirt 0.312 inch plus or minus 0.010 inch.

(b) Bore of body 1.3800-1.3817 inches.

(c) Clearance between piston and damper housing 0.0015-0.0040 inch.

(d) Identify the reworked housing with blue dye or blue paint.

The reinstallation of new or reworked damper housings mustbe accomplished in accordance with instructions in Lockheed Service Letter FS/251702-L dated February 14, 1961.

(Lockheed Service Wire to all operators dated April 7, 1961, applies to this same subject.)

This directive becomes effective upon publication in the Federal Register for all persons except those to whom it was made effective immediately by telegram dated April 7, 1961.

AD Assistant

Get AI-powered answers about this AD, check applicability, and find compliance steps.

Sign Up to Unlock
References
This information is not available.
--- - Part 39
FAA Documents