AD 88-24-12

final rule
Data completeness: 70%

Airworthiness Directives; BOEING Model 727 Series Airplane

AD Number
88-24-12
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 Airworthiness Directives; BOEING Model 727 Series Airplane
aircraft The Boeing Company 727-100C Series Airworthiness Directives; BOEING Model 727 Series Airplane
aircraft The Boeing Company 727-200 Series Airworthiness Directives; BOEING Model 727 Series Airplane
aircraft The Boeing Company 727-200F Series Airworthiness Directives; BOEING Model 727 Series Airplane
aircraft The Boeing Company 727 Series Airworthiness Directives; BOEING Model 727 Series Airplane
aircraft The Boeing Company 727C Series Airworthiness Directives; BOEING Model 727 Series Airplane

Unsafe Condition

Failure of the main landing gear (MLG) to extend as a result of loosening of the self-locking nut at the attachment of the downlock forward pushrod assembly to the downlock torque shaft.

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

Required Actions

Install the bolt, washer, nut, and cotter pin as specified in Boeing Service Bulletins 727-32-0237 (item 5 of Figure 5) and 727-32-0353. An alternate means of compliance or adjustment may be approved by the FAA Manager, Seattle Aircraft Certification Office.

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

Compliance Time

within the next 3,500 flight cycles after the effective date of this AD

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Affected Aircraft

All Model 727 series airplanes prior to line number 1620, not equipped with the safety bar modification described in Boeing Service Bulletin 727-32-275, Revision 2.

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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