AD 63-03-01

final rule
Data completeness: 70%

Airworthiness Directives; BOEING Models 707-100B, 707-300B, 720-000B Series and DOUGLAS DC-8-50 Series Aircraft

AD Number
63-03-01
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Unknown
FR Citation
(Federal Register: February 5, 1963)

Applicability

TypeManufacturerModelDetails
aircraft The Boeing Company 707-100B Long Body Airworthiness Directives; BOEING Models 707-100B, 707-300B, 720-000B Series and DOUGLAS DC-8-50 Series Aircraft
aircraft The Boeing Company 707-100B Short Body Airworthiness Directives; BOEING Models 707-100B, 707-300B, 720-000B Series and DOUGLAS DC-8-50 Series Aircraft
aircraft The Boeing Company 707-300B Series Airworthiness Directives; BOEING Models 707-100B, 707-300B, 720-000B Series and DOUGLAS DC-8-50 Series Aircraft
aircraft The Boeing Company 720 Series Airworthiness Directives; BOEING Models 707-100B, 707-300B, 720-000B Series and DOUGLAS DC-8-50 Series Aircraft
aircraft The Boeing Company 720B Series Airworthiness Directives; BOEING Models 707-100B, 707-300B, 720-000B Series and DOUGLAS DC-8-50 Series Aircraft
aircraft The Boeing Company DC-8-51 Airworthiness Directives; BOEING Models 707-100B, 707-300B, 720-000B Series and DOUGLAS DC-8-50 Series Aircraft
aircraft The Boeing Company DC-8-52 Airworthiness Directives; BOEING Models 707-100B, 707-300B, 720-000B Series and DOUGLAS DC-8-50 Series Aircraft
aircraft The Boeing Company DC-8-53 Airworthiness Directives; BOEING Models 707-100B, 707-300B, 720-000B Series and DOUGLAS DC-8-50 Series Aircraft
aircraft The Boeing Company DC-8-55 Airworthiness Directives; BOEING Models 707-100B, 707-300B, 720-000B Series and DOUGLAS DC-8-50 Series Aircraft

Unsafe Condition

Clogging of engine main oil filters by foreign matter has caused lubrication system malfunctions which have resulted in engine mechanical failures affecting safety of flight.

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

Required Actions

Modify the engine oil filter assembly to install a differential pressure switch and an additional spring in the bypass valve per Service Bulletin No. 327. Install a pressure switch across the engine main oil system filter set to actuate at approximately 50 p.s.i., following Boeing Service Bulletin No. 1586 or Douglas Service Bulletin No. 79-11. Provide cockpit indications for the pressure switch actuation as per respective service bulletins.

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

Compliance Time

within the next 4,000 hours' time in service after the effective date of this AD

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Affected Aircraft

Boeing Models 707-100B, 707-300B, 720-000B Series and Douglas DC-8-50 Series Aircraft with Pratt & Whitney JT3D Series engines, as listed in respective service bulletins.

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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