交通部民用航空局

發布日期

2008/04/21

適用性說明

This AD applies to Avidyne Corporation (Avidyne) Primary Flight Displays (PFDs) (Part Numbers (P/Ns) 700-00006-000, 700- 00006-001, 700-00006-002, 700-00006-003, and 700-00006-100) that are installed on, but not limited to the following airplanes that are certificated in any category: (1) Adam Aircraft Model A500; (2) Cessna Aircraft Company Model 441 (STEC Alliant Supplemental Type Certificate (STC) No. SA09547AC-D incorporated); (3) Cessna Aircraft Company Models LC42-550FG and LC41-550FG (Columbia Aircraft Manufacturing and The Lancair Company previously held the type certificate for these airplanes); (4) Cirrus Design Corporation Models SR20 and SR22; (5) Diamond Aircraft Industries GmbH Model DA 40; (6) Hawker Beechcraft Corporation Model E90 (STEC Alliant STC No. SA09545AC-D incorporated); (7) Hawker Beechcraft Corporation Model 200 series (STEC Alliant STC No. SA09543AC-D incorporated); and (8) Piper Aircraft, Inc. Models PA-28-161, PA-28-181, PA-28R- 201, PA-32R-301 (HP), PA-32R-301T, PA-32-301FT, PA-32-301XTC, PA-34- 220T, PA-44-180, PA-46-350P, PA-46R-350T, and PA-46-500TP.

型別

Avidyne Corporation Primary Flight Displays (Part Numbers 700-00006-000, -001, -002, -003, and -100)

民航局AD編號

CAA-2008-03-011A(已有後續修訂版)

原發布國

FAA

原AD編號

2008-06-28R1

生效日期

2008/04/10

主旨摘要

To prevent certain conditions from existing when PFDs display incorrect attitude, altitude, and airspeed information. This could result in airspeed/ altitude mismanagement or spatial disorientation of the pilot with consequent loss of airplane control, inadequate traffic separation, or controlled flight into terrain.

參考資訊（版本/ATA/SB）

Revises AD 2008-06-28(CAA-2008-03-011). Ref. AFM, POH, or AFMS; Avidyne Service Alert No. SA-08-001

存檔序號

97-04-007

專業分項

Avionics

產品類別

Application

備註

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