AD 77-18-06

final rule
Data completeness: 70%

BOEING Model 727 Series Airplanes

AD Number
77-18-06
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Unknown
FR Citation
This information is not available.

Applicability

TypeManufacturerModelDetails
aircraft The Boeing Company 727-100 Series BOEING Model 727 Series Airplanes
aircraft The Boeing Company 727-100C Series BOEING Model 727 Series Airplanes
aircraft The Boeing Company 727-200 Series BOEING Model 727 Series Airplanes
aircraft The Boeing Company 727-200F Series BOEING Model 727 Series Airplanes
aircraft The Boeing Company 727 Series BOEING Model 727 Series Airplanes
aircraft The Boeing Company 727C Series BOEING Model 727 Series Airplanes

Unsafe Condition

Cracks in the horizontal stabilizer center section front spar junction fittings, P/Ns 65-17448-1 or 65-31273-1, which could lead to structural failure.

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

Required Actions

Inspect the horizontal stabilizer center section front spar junction fittings for cracks using specified methods (eddy current or dye penetrant) with jackscrew support arms removed or installed as per Boeing Service Bulletin. Apply corrosion inhibitor to lugs. Repeat inspections at intervals of 1,500 flight hours or 9 months, or 3,000 flight hours or 18 months if reworked. Replace or repair cracked fittings before further flight. Report cracks within 64 hours. Replace with P/N 65-31273-4 to terminate AD.

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

Compliance Time

Within the next 750 flight hours time-in-service from the effective date (October 3, 1977) or prior to January 1, 1978, whichever occurs first.

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

Affected Aircraft

Boeing Model 727-100 Series, 727-100C Series, 727-200 Series, 727-200F Series, 727 Series, 727C Series with horizontal stabilizer center section front spar junction fittings P/Ns 65-17448-1 or 65-31273-1.

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

This site is not affiliated with or endorsed by the FAA. Always verify with official sources.