AD 61-06-05

Airworthiness directive · Rudder Boost Piston Locknut · Boeing DC-8-11, DC-8-12, DC-8-21 and 24 more

Effective
March 23, 1961
Published
March 23, 1961
Models
DC-8-11, DC-8-12, DC-8-21, DC-8-31, DC-8-32, DC-8-33 and 21 more
Data sheet
TCDS4A25
Registered aircraft
8 matched by model
Product
Aircraft · Large airplane

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.

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The airworthiness directive

61-06-05 DOUGLAS: Amdt. 270 Part 507 Federal Register March 23, 1961. Applies to All DC-8 Series Aircraft.

Compliance required within the next 20 hours' time in service, unless already accomplished in accordance with Douglas Alert Bulletin dated February 24, 1961.

As a result of reported instances of loosened rudder boost piston end assembly locknut, the following must be accomplished.

Refer to DC-8 Overhaul Manual, Chapter 27-19-2, page 18. Visually inspect for loose locknut P/N NAS 509-16 and proper installation and safetying to locknut of lockwasher P/N NAS 513-16. Insure that lockwasher is not installed backwards and that tang on lockwasher is engaged in notch in piston end and that piston has not rotated out of its proper position. If any discrepancies are found, they must be corrected in accordance with the DC-8 Overhaul Manual and Douglas Alert Bulletin dated February 24, 1961, prior to further flight.

This directive becomes effective upon publicationin the Federal Register for all person except those to whom it was made effective immediately by individual telegrams dated March 8, 1961.

Affected TCDS · 1

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

Registered aircraft · 8

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
  • Douglas5 aircraft
  • Mcdonnell Douglas3 aircraft
By year built
19681972
Registered aircraft by year built: 3 aircraft
19681
19691
19721

5 with no year recorded

By model

Aircraft