AD 2017-19-02

Recurring final rule
Data completeness: 70%

Airworthiness Directives; The Boeing Company Airplanes

AD Number
2017-19-02
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. FAA-2016-9184
FR Citation
82 FR 43171

Applicability

TypeManufacturerModelDetails
aircraft Boeing Company Airworthiness Directives; The Boeing Company Airplanes

Unsafe Condition

Cracking of the cam support assemblies of the main cargo door (MCD) could result in reduced structural integrity of the MCD and consequent rapid decompression of the airplane.

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

Required Actions

Repetitive ultrasonic inspections for cracking of the cam support assemblies of the MCD are required, with replacement if necessary. Completion of the initial inspection and all applicable replacements terminates all requirements of AD 80-08-10 R1 for that airplane.

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

Compliance Time

Before the accumulation of 18,000 door flight cycles. If the door flight cycles are not known, use total airplane flight cycles.

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

Affected Aircraft

The Boeing Company Model 727 series airplanes equipped with a main cargo door (MCD).

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

Source: Official FAA Source ↗

Retrieved: Apr 6, 2026

Rights: U.S. Government Public Domain

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