Airworthiness Directive E7-10758

one-time
AD E7-10758 · 2007-06-11 · airframe

Airworthiness Directives; Hawker Beechcraft Corporation (Type Certificate (TC) No. 3A20 and TC No. A24CE Formerly Held by Raytheon Aircraft Corporation and Beech) Models C90A, B200, B200C, B300, and B300C Airplanes

What this AD requires

We are adopting a new airworthiness directive (AD) that supersedes AD 2006-23-02, which applies to certain Hawker Beechcraft Corporation (HBC) (Type Certificate (TC) No. 3A20 and TC No. A24CE formerly held by Raytheon Aircraft Corporation and Beech) Models C90A, B200, B200C, B300, and B300C airplanes. AD 2006-23-02 currently requires you to inspect the flight controls for improper assembly or damage, and if any improperly assembled or damaged flight controls are found, take corrective action. Since we issued AD 2006-23-02, we have determined the need to add airplane serial numbers that were not previously included in the applicability. Consequently, this AD retains the actions of AD 2006-23-02 and adds airplane serial numbers to the applicability. We are issuing this AD to detect and correct improperly assembled or damaged flight controls, which could result in an unsafe condition by reducing capabilities of the flight controls and lead to loss of control.

Which aircraft AD E7-10758 applies to

MakesHawker Beechcraft CorporationRaytheon Aircraft CorporationBeech
ModelsC90A, B200, B200C, B300, B300C
Serial-conditional — narrows to serials LJ-1697–LJ-1726, LJ-1728–LJ-1728, LJ-1729–LJ-1729, LJ-1731–LJ-1739, BB-1827–BB-1912, BL-148–BL-148, BL-149–BL-149, FL-379–FL-423, FL-426–FL-426, FL-428–FL-450, FL-452–FL-452, FM-11–FM-11, LJ-1741–LJ-1743.

Group 1 (C90A, B200, B200C, B300, B300C) maintains actions from AD 2006-23-02; Group 2 (C90A, S/N LJ-1741 through LJ-1743) is newly added applicability.

Whether AD E7-10758 actually applies to your aircraft (by serial and installed parts) and whether it’s already complied with comes from that aircraft’s records.

Supersession

Supersedes AD 2006-23-02.

How AD compliance is recorded

A valid compliance record (14 CFR 43.9) states:

Method of complianceThe specific action taken (inspected, replaced, modified) and to what revision.
DateWhen the work was done.
Aircraft timeTotal time in service / tach at compliance — how recurring next-due is computed.
Signature & certificateThe A&P/IA who returned it to service, with certificate number.
Is AD E7-10758 complied with on your aircraft?

Tailplate reads a tail number’s logbooks and matches every applicable AD — including this one — to its compliance evidence, with recurring next-due dates computed.

Look up a tail number →Read the full directive (Federal Register)

Applicability is derived from the FAA directive corpus and is advisory, not a legal airworthiness determination. Compliance is established only from an aircraft’s actual records.