AD 99-24-02
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | The Boeing Company | 767-200 Series | Airworthiness Directives; BOEING Model 767-200 and -300 Series Airplanes |
| aircraft | The Boeing Company | 767-300 Series | Airworthiness Directives; BOEING Model 767-200 and -300 Series Airplanes |
| aircraft | The Boeing Company | 767-300F Series | Airworthiness Directives; BOEING Model 767-200 and -300 Series Airplanes |
Unsafe Condition
Fracture of the lower drag strut of the nose landing gear (NLG) caused by a thin wall thickness condition during manufacturing, which could result in NLG collapse.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Perform a one-time visual inspection to determine the part and serial numbers of the lower drag strut. If serial number prefix is HM or FRG, conduct an ultrasonic inspection to measure wall thickness. Depending on thickness, either no further action, overhaul within 5 years, or replace prior to further flight.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Within 90 days after effective date for visual inspection; prior to further flight for ultrasonic inspection and replacement if needed; overhaul within 5 years if thickness is within certain limits.
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
Boeing Model 767-200, -300, and -300F series airplanes listed in Boeing Alert Service Bulletin 767-32A0185.
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.