AD 56-16-02

final rule
Data completeness: 60%

LOCKHEED All Models 49, 149, 649, 749, and 1049 Series

AD Number
56-16-02
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Unknown
FR Citation
This information is not available.

Applicability

TypeManufacturerModelDetails
aircraft Lockheed Aircraft Corporation 1049-54 LOCKHEED All Models 49, 149, 649, 749, and 1049 Series
aircraft Lockheed Aircraft Corporation 1049B-55 (Navy R7V-1) LOCKHEED All Models 49, 149, 649, 749, and 1049 Series
aircraft Lockheed Aircraft Corporation 1049C-55 LOCKHEED All Models 49, 149, 649, 749, and 1049 Series
aircraft Lockheed Aircraft Corporation 1049D-55 LOCKHEED All Models 49, 149, 649, 749, and 1049 Series
aircraft Lockheed Aircraft Corporation 1049E-55 LOCKHEED All Models 49, 149, 649, 749, and 1049 Series
aircraft Lockheed Aircraft Corporation 1049F-55 (USAF C-121C) LOCKHEED All Models 49, 149, 649, 749, and 1049 Series
aircraft Lockheed Aircraft Corporation 1049G-82 LOCKHEED All Models 49, 149, 649, 749, and 1049 Series
aircraft Lockheed Aircraft Corporation 1049H-82 LOCKHEED All Models 49, 149, 649, 749, and 1049 Series
aircraft Lockheed Aircraft Corporation 149-46 LOCKHEED All Models 49, 149, 649, 749, and 1049 Series
aircraft Lockheed Aircraft Corporation 49-46 LOCKHEED All Models 49, 149, 649, 749, and 1049 Series

Unsafe Condition

Fatigue failures in the side webs of the Bendix Eclipse-Pioneer Type DQ-15 Series servo disconnect mounting brackets in the primary flight control system could disable the flight control system.

AI-generated summary from the source AD text. Verify against the official source before acting.

Required Actions

Inspect rudder and elevator servo disconnect mounting brackets by dye penetrant or equivalent method every 125 hours until item 2 is done. Discard defective brackets. Install secondary servo support brackets as soon as possible but not exceeding next overhaul period after parts are available.

AI-generated summary from the source AD text. Verify against the official source before acting.

Compliance Time

At 125-hour intervals until item 2 is accomplished. Item 2 must be done as soon as possible but not to exceed next overhaul period after parts become available.

AI-generated summary from the source AD text. Verify against the official source before acting.

Affected Aircraft

Lockheed Aircraft Corporation models 49, 149, 649, 749, and 1049 Series equipped with Bendix Eclipse-Pioneer Type PB-10 Series automatic pilot installations.

AI-generated summary from the source AD text. Verify against the official source before acting.

Source: Official FAA Source ↗

Retrieved: Apr 8, 2026

Rights: U.S. Government Public Domain

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