AD 91-06-06

final rule
Data completeness: 70%

Airworthiness Directives; BOEING Model 727 Series Airplanes

AD Number
91-06-06
Status
final_rule
Effective Date
Product Category
aircraft
Docket
90-NM-176-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

Cracks in the fuselage skin at lap joints S-4, S-10, S-14, S-19, S-20, and S-26 where the upper skin is less than 0.056 inch thick from body station 259 to 1183 could lead to rapid decompression of the airplane.

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

Required Actions

Perform high frequency eddy current (HFEC) inspections for cracks at specified fuselage lap joints within specified landing intervals and timeframes. Conduct detailed external visual inspections for cracks, corrosion, and delamination at intervals not exceeding 15 or 30 months. Repair detected cracks, corrosion, or delamination prior to further flight. Replace fasteners with protruding head fasteners within 4 or 6 years after August 21, 1989, depending on landing count. Inspect blind fasteners at intervals not exceeding 2,500 landings.

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

Compliance Time

Within the next 2,500 landings or 1 year after August 21, 1989, whichever occurs first, or prior to the accumulation of 28,000 landings, whichever occurs later; thereafter at intervals not to exceed 4,500 landings or 3 years, whichever occurs sooner. For visual inspections: within 6 months after August 21, 1989, unless accomplished within the last 9 months, and thereafter at intervals not to exceed 15 or 30 months. Fastener modifications must be completed within 4 or 6 years after August 21, 1989, depending on landing count.

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

Affected Aircraft

Boeing Model 727 series airplanes listed in Boeing Service Bulletin 727-53-0072, Revision 5, dated June 1, 1989, 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

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