AD 89-20-04

final rule
Data completeness: 70%

Airworthiness Directives; BOEING Model 727 Series Airplanes

AD Number
89-20-04
Status
final_rule
Effective Date
Product Category
aircraft
Docket
89-NM-152-AD
FR Citation
This information is not available.

Applicability

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

Unsafe Condition

Rapid decompression of the airplane due to cracks in the fuselage skin at lap joints located at stringer 14L from body station 440 to 720, and at S-14R from body station 440 to 540.

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

Required Actions

Conduct an internal detailed visual inspection for cracks of the fuselage skin at specified lap joints, followed by high or low frequency eddy current inspections within 500 landings or ten days after the AD's effective date, whichever is later. Repeat inspections at intervals of 2,000 landings (HFEC) or 1,000 landings (LFEC). Repair detected cracks prior to further flight using specified Boeing drawings. Modifications per Boeing Drawing 65C35402 terminate repetitive inspections.

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

Compliance Time

Within the next 15 days after receipt of AD T89-14-51, dated June 30, 1989, for the initial inspection. The subsequent inspection must be done within 500 landings after the initial inspection or ten days after the AD's effective date (October 6, 1989), whichever is later. Repeat inspections must be conducted within 2,000 landings (HFEC) or 1,000 landings (LFEC) after the previous inspection.

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

Affected Aircraft

Boeing Model 727 series airplanes, line numbers 001 through 047, certificated in any category.

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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