Airworthiness Directive

AD 2011-15-05 76 FR 41667 Active

Federal Aviation Administration · 14 CFR part 39

FR document
2011-17567
Amendment
39-16752
Published
2011-07-15
Effective
2011-08-19
Models covered
1
Last live check
2026-10-01
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AD

2011-15-05

FR doc 2011-17567 · 76 FR 41667

AD 2011-15-05Published 2011-07-15Effective 2011-08-19

FAA rule - 14 CFR 39

FAA rule. Compliance with an applicable AD is required under 14 CFR 39.7. Check its effective date, applicability, compliance times and current status.

Requires a correction to the published data in the airplane flight manual and the pilot's operating handbook to ensure it corresponds with the published data in the pilot's checklist.

Full official abstract

We are adopting a new airworthiness directive (AD) for certain Hawker Beechcraft Corporation Models B300 and B300C (C-12W) airplanes. This AD was prompted by an error found in the take-off speeds and field lengths published in the FAA-approved airplane flight manual. This AD requires a correction to the published data in the airplane flight manual and the pilot's operating handbook to ensure it corresponds with the published data in the pilot's checklist. This condition, if not corrected, could result in a pilot taking off from shorter runways than required by the airplane if the airplane loses an engine after takeoff decision speed (V<INF>1</INF>). This could result in the airplane running out of runway before take-off can be accomplished. We are issuing this AD to correct the unsafe condition on these products.

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All Beechcraft King Air 300/350 directives

Applies to 1 model in our index