AD Amdt-39-10450

Recurring final rule
Data completeness: 70%

Airworthiness Directives; Fokker Model F28 Mark 0070 and Mark 0100 Series Airplanes

AD Number
Amdt-39-10450
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. 97-NM-249-AD
FR Citation
63 FR 17318

Applicability

TypeManufacturerModelDetails
aircraft Fokker F28 Mark 0070 and Mark 0100 Airworthiness Directives; Fokker Model F28 Mark 0070 and Mark 0100 Series Airplanes

Unsafe Condition

Leakage of hot air from the corrujoint seals of the low- and high-pressure check valves located in the stubwings could result in heat damage to the fuselage skin and stubwing structure, leading to reduced structural integrity.

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

Required Actions

Perform a one-time visual inspection to detect heat damage of the fuselage skin and stubwing structure. Conduct repetitive leak tests of the seals of the bleed air system or repair heat-damaged structure as necessary. Replace corrujoint seals with new improved seals.

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

Compliance Time

Before further flight

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

Affected Aircraft

Fokker Model F28 Mark 0070 and Mark 0100 series airplanes subject to mandatory continuing airworthiness information by a foreign civil airworthiness authority.

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

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