AD 68-06-03
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Textron Aviation Inc. | DH.125 Series 1A | Airworthiness Directives; HAWKER SIDDELEY Model DH. 125 Airplanes |
| aircraft | Textron Aviation Inc. | DH.125 Series 1A-522 | Airworthiness Directives; HAWKER SIDDELEY Model DH. 125 Airplanes |
| aircraft | Textron Aviation Inc. | DH.125 Series 3A | Airworthiness Directives; HAWKER SIDDELEY Model DH. 125 Airplanes |
Unsafe Condition
A fully asymmetric flap condition in the lift dump position
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Replace the flap center hinge bolt with a self-retaining bolt P/N 3110-7681 in accordance with Hawker Siddeley Service Bulletin 27-49-(1894) Revision 2 or later ARB-approved revision.
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Compliance Time
within the next 150 hours' time in service after the effective date of this AD
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Affected Aircraft
HAWKER SIDDELEY Model DH.125 airplanes, Series 1A, 1A/522 and 3A
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Source: Official FAA Source ↗
Retrieved: Apr 8, 2026
Rights: U.S. Government Public Domain
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