Airworthiness directives › 2011-15-05
AD 2011-15-05 Airworthiness Directives; Hawker Beechcraft Corporation Models B300 and B300C (C-12W) Airplanes
Makes named: hawker beechcraft. Read the applicability below — it usually turns on serial or part numbers too.
Applicability*9
(1) This AD applies to Hawker Beechcraft Corporation Models B300 and B300C (C-12W) airplanes, all serial numbers, that: (2) Are certificated in any category; and (3) Are modified per Hawker Beechcraft Drawing 130M000030 or Kit Drawing 130-4014 that incorporate Pilot's Operating Handbook and FAA Approved Flight Manual, part number (P/N) 130-590031-245.
Compliance
Comply with this AD within the compliance times specified, unless already done.
Required actions
Within 14 days after the effective date of this AD, insert Hawker Beechcraft Corporation Log of Temporary Changes, dated February 2011; and Hawker Beechcraft Corporation Temporary Change to the Pilot's Operating Handbook and FAA Approved Airplane Flight Manual, Part Number (P/N) 130-590031-245TC5, dated February 2011; into the airplane's Pilot's Operating Handbook and FAA Approved Flight Manual, P/N 130-590031-245. The actions required by this paragraph may be performed by the owner/operator (pilot) holding at least a private pilot certificate and must be entered into the aircraft records showing compliance with this AD in accordance with 14 CFR 43.9 (a)(1)-(4) and 14 CFR 91.417(a)(2)(v). The record must be maintained as required by 14 CFR 91.417, 121.380, or 135.439.
Unsafe condition
This AD was prompted by an error that was discovered in the take-off speeds and field lengths published in the FAA-approved flight manual. This AD is issued to correct the published data in the airplane flight manual and the pilot's operating handbook and ensure it corresponds with the published data in the pilot's checklist. This condition, if not corrected, could result in taking off from shorter runways than required by the airplane if the airplane loses an engine after takeoff decision speed (V 1 ). This could result in the airplane running out of runway before take-off can be accomplished.
Affected ADs
None.
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The directive text above is reproduced from the Federal Register, a work of the United States government and in the public domain. The separation into applicability, compliance and required actions is TrackAD's.*1