Airworthiness Directive · Amendment 39-15084 · 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
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
This AD applies to the following airplane models and serial numbers that are certificated in any category:
(1) Group 1 Airplanes (maintains the actions from AD 2006-23-02):
| Model | Serial No. |
|---|---|
| (i) C90A | LJ-1697 through LJ-1726, LJ-1728, LJ-1729, and LJ-1731 through LJ-1739. |
| (ii) B200 | BB-1827 through BB-1912. |
| (iii) B200C | BL-148 and BL-149. |
| (iv) B300 | FL-379 through FL-423, FL-426, FL-428 through FL-450, and FL-452. |
| (v) B300C | FM-11. |
(2) Group 2 Airplanes: Model C90A, serial numbers LJ-1741 through LJ-1743.
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.
To address this problem, you must do the following, unless already done:
| Actions | Compliance | Procedures |
|---|---|---|
| (1) Inspect the entire flight control system for improper assembly and any damage | (i) For Group 1 Airplanes: At whichever of the following occurs first: (A) Within the next 100 hours time-in-service (TIS) after December 13, 2006 (the effective date of AD 2006-23-02); or (B) At the next annual inspection that occurs at least 30 days after December 13, 2006 (the effective date of AD 2006-23-02) (ii) For Group 2 Airplanes: At whichever of the following occurs first: (A) Within the next 100 hours TIS after July 16, 2007 (the effective date of this AD); or (B) At the next annual inspection that occurs at least 30 days after July 16, 2007 (the effective date of this AD). | Follow Raytheon Aircraft Company Mandatory Service Bulletin Number SB 27-3761, Issued: February 2006; or Raytheon Aircraft Company Mandatory Service Bulletin Number SB 27-3761, Rev. 1, Dated December 2006. |
| (2) If you find any improperly assembled or damaged flight controls as a result of the inspection required by paragraph (e)(1) of this AD, take corrective action as specified in the service information | Before further flight after the inspection required by paragraph (e)(1) of this AD | Follow Raytheon Aircraft Company Mandatory Service Bulletin Number SB 27-3761, Issued: February 2006; or Raytheon Aircraft Company Mandatory Service Bulletin Number SB 27-3761, Rev. 1, Dated December 2006. |
The aircraft, engines and makers this AD names, by the model designations in its text. A model listed here may still be outside the AD's serial ranges.
