AD 93-17-11

final rule
Data completeness: 70%

Airworthiness Directives; De Havilland Models DHC-8-100 Series and DHC-8-300 Series Airplanes

AD Number
93-17-11
Status
final_rule
Effective Date
Product Category
aircraft
Docket
93-NM-41-AD
FR Citation
This information is not available.

Applicability

TypeManufacturerModelDetails
aircraft Bombardier Inc. DHC-8-101 Airworthiness Directives; De Havilland Models DHC-8-100 Series and DHC-8-300 Series Airplanes
aircraft Bombardier Inc. DHC-8-102 Airworthiness Directives; De Havilland Models DHC-8-100 Series and DHC-8-300 Series Airplanes
aircraft Bombardier Inc. DHC-8-103 Airworthiness Directives; De Havilland Models DHC-8-100 Series and DHC-8-300 Series Airplanes
aircraft Bombardier Inc. DHC-8-106 Airworthiness Directives; De Havilland Models DHC-8-100 Series and DHC-8-300 Series Airplanes
aircraft Bombardier Inc. DHC-8-301 Airworthiness Directives; De Havilland Models DHC-8-100 Series and DHC-8-300 Series Airplanes
aircraft Bombardier Inc. DHC-8-311 Airworthiness Directives; De Havilland Models DHC-8-100 Series and DHC-8-300 Series Airplanes
aircraft Bombardier Inc. DHC-8-315 Airworthiness Directives; De Havilland Models DHC-8-100 Series and DHC-8-300 Series Airplanes

Unsafe Condition

Reduced strength and fail-safe capability of the structural attachment of the horizontal stabilizer to the airplane due to cracks at the radius transition between the bolt head and shank of the horizontal stabilizer midspar attachment bolts.

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

Required Actions

Within 250 landings after the effective date, perform a one-time magnetic particle inspection of the horizontal stabilizer midspar attachment bolts. If any crack is found, replace both bolts with serviceable ones prior to further flight. Additionally, ensure all bolts installed after the effective date are inspected using magnetic particle techniques before installation.

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

Compliance Time

Within 250 landings after the effective date of this AD

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

Affected Aircraft

De Havilland Models DHC-8-100 series (serial numbers 003 through 315 inclusive, 317 through 344 inclusive, and 346 through 349 inclusive) and DHC-8-300 series (serial numbers 100 through 319 inclusive, 321 through 337 inclusive, 339, 341, and 342).

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.