AD 88-05-02
Unsafe Condition
Fatigue cracking in the airplane structure at the flap outboard hinge fitting and fuselage skin beneath the canopy blister, which could result in the inability of the structure to meet required loads.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Visually inspect the wing bottom skin for cracks at the flap outboard hinge fitting and fuselage skin beneath the canopy blister in accordance with specified service bulletins. Repair detected cracks prior to further flight using FAA approved methods.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Prior to the accumulation of 12,000 flights or within 8 months after the effective date of this AD, whichever occurs later for some serial numbers; prior to 7,500 flights or within 6 months after the effective date, whichever occurs later for others.
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
BRITISH AEROSPACE (BAe) PLC Model DH/BH/HS 125 series airplanes listed in BAe 125 Service Bulletins 57-67 and 53-63, dated February 27, 1987.
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.