AD 63-16-04

final rule
Data completeness: 70%

Airworthiness Directives; GENERAL DYNAMICS Model 22 Aircraft

AD Number
63-16-04
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Unknown
FR Citation
This information is not available.

Applicability

TypeManufacturerModelDetails
aircraft D & R Nevada LLC 22 Airworthiness Directives; GENERAL DYNAMICS Model 22 Aircraft
aircraft D & R Nevada LLC 22M Airworthiness Directives; GENERAL DYNAMICS Model 22 Aircraft

Unsafe Condition

Cracks have been found in foreflaps P/N 22-18600-5/-807.

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

Required Actions

Conduct a close visual inspection for cracks in external clips and entire skin area using dye penetrant or equivalent. Remove and disassemble outboard foreflaps to inspect interior clips via visual, X-ray, or dye penetrant. Replace cracked parts before flight. Repeat inspections within specified intervals and eventually replace foreflaps with modified versions per Service Bulletin 27-65.

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

Compliance Time

Within the next 400 hours' time in service after the effective date of this AD unless already accomplished within the last 400 hours' time in service

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

Affected Aircraft

All Model 22 Aircraft with foreflaps P/N 22-18600-5/-807 not modified per General Dynamics Service Bulletin No. 27-65(1)(a) or B(1)(b)

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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