AD 2001-22-06

final rule
Data completeness: 60%

Airworthiness Directives; Boeing Model B-17E, F, and G Airplanes

AD Number
2001-22-06
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. 95-NM-15-AD
FR Citation
66 FR 54111

Applicability

TypeManufacturerModelDetails
aircraft Boeing B-17E Airworthiness Directives; Boeing Model B-17E, F, and G Airplanes

Unsafe Condition

Cracking and corrosion of the wing spar chords, bolts and bolt holes of the spar chords, and wing terminals may reduce structural integrity of the wing.

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

Required Actions

Inspect to detect cracking and corrosion of the wing spar chords, bolts, bolt holes, and wing terminals. Correct any discrepancies found during inspections.

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

Boeing Model B-17E, F, and G airplanes

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.