AD 78-11-07

final rule
Data completeness: 70%

BOEING Model 727 Series Airplanes

AD Number
78-11-07
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 jackscrew gimbal support fittings, P/N 65-17435-3 and -4, could result in structural failure of the horizontal stabilizer assembly.

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

Required Actions

Inspect the horizontal stabilizer jackscrew gimbal support fittings for cracks using eddy current or low frequency eddy current methods per Boeing Alert Service Bulletin 727-55-A73 or approved procedures. Repeat inspections at intervals of either 1,500 flight hours or 9 months, or 3,000 flight hours or 18 months if reworked. Replace or repair cracked parts before further flight. Terminate with replacement of fittings with 7075-T73 aluminum alloy P/N 65-17435-5/-6.

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 after the effective date of this AD or prior to November 15, 1978, whichever occurs first, unless accomplished within the last 750 flight hours time-in-service or since January 15, 1978.

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

Affected Aircraft

Boeing Model 727 series airplanes with horizontal stabilizer jackscrew gimbal support fittings P/N 65-17435-3 and -4.

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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