AD 61-18-01

final rule
Data completeness: 70%

BOEING 707 Series and Boeing 720 Series Aircraft

AD Number
61-18-01
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Unknown
FR Citation
This information is not available.

Applicability

TypeManufacturerModelDetails
aircraft The Boeing Company 707-100 Long Body BOEING 707 Series and Boeing 720 Series Aircraft
aircraft The Boeing Company 707-100B Long Body BOEING 707 Series and Boeing 720 Series Aircraft
aircraft The Boeing Company 707-100B Short Body BOEING 707 Series and Boeing 720 Series Aircraft
aircraft The Boeing Company 707-200 BOEING 707 Series and Boeing 720 Series Aircraft
aircraft The Boeing Company 707-300 Series BOEING 707 Series and Boeing 720 Series Aircraft
aircraft The Boeing Company 707-300B Series BOEING 707 Series and Boeing 720 Series Aircraft
aircraft The Boeing Company 707-300C Series BOEING 707 Series and Boeing 720 Series Aircraft
aircraft The Boeing Company 707-400 Series BOEING 707 Series and Boeing 720 Series Aircraft
aircraft The Boeing Company 720 Series BOEING 707 Series and Boeing 720 Series Aircraft
aircraft The Boeing Company 720B Series BOEING 707 Series and Boeing 720 Series Aircraft

Unsafe Condition

Failure in the main landing gear trunnion support due to cracks in the web, chord areas, flanges, and fittings of the trunnion support rib and bearings.

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

Required Actions

Inspect and clean specified areas of the main landing gear trunnion support for cracks at intervals of 200, 35, 350, 420, 840, and 5,000 hours' time in service. Stop drill cracks under allowable lengths per Boeing Service Bulletin 859 (R-2 or later) and replace or repair components with FAA-approved procedures if cracks exceed limits. Conduct detailed inspections and rework per Service Bulletin 874 within 3,500 hours' time in service.

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

Compliance Time

Compliance required within the specified intervals (e.g., 200 hours' time in service for initial inspections, 3,500 hours' time in service for rework).

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

Affected Aircraft

Boeing 707 Series Aircraft Serial Nos. 17586-17652, 17658-17690, 17692-17712, 17718-17724, 17903-17906, 17918-17919, 17925-17930, 18012 and 18054 and Boeing 720 Series Aircraft Serial Nos. 17907-17917, 18013-18020, 18023, and 18041.

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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