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钻石42飞机飞行手册 DA 42 Airplane Flight Manual

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' NOTE ' This airplane flight manual is valid for DA42 airplanes with ' a KAP 140 or no autopilot system installed.
' Refer to the airplane flight manual “DA42 with Garmin ' GFC 700 (O.M 42-102)”, Doc. No. 7.01.06-E for airplanes ' with a Garmin Autopilot system installed.
Page 0 - 0a  Rev. 5  15-Nov-2007  Doc. # 7.01.05-E 


FOREWORD
We congratulate you on the acquisition of your new DIAMOND DA 42 Twin Star.
Skillful operation of an airplane increases both safety and the enjoyment of flying. Please take the time therefore, to familiarize yourself with your new DIAMOND DA 42.
This airplane may only be operated in accordance with the procedures and operating limitations of this Airplane Flight Manual.
Before this airplane is operated for the first time, the pilot must familiarize himself with the complete contents of this Airplane Flight Manual.
In the event that you have obtained your DIAMOND DA 42 second-hand, please let us know your address, so that we can supply you with the publications necessary for the safe operation of your airplane.
This document is protected by copyright. All associated rights, in particular those of translation, reprinting, radio transmission, reproduction by photo-mechanical or similar means and storing in data processing facilities, in whole or part, are reserved.
Copyright . by: DIAMOND AIRCRAFT INDUSTRIES GMBH
N.A. Otto-Strasse 5 A-2700 Wiener Neustadt, Austria Phone : +43-2622-26700 Fax : +43-2622-26780 E-Mail : office@diamond-air.at


0.1 APPROVAL
The content of approved chapters is approved by EASA. All other content is approved by DAI under the authority of EASA DOA No. EASA.21J.052 in accordance with Part 21.

0.2 RECORD OF REVISIONS
All revisions of this manual, with the exception of -
.
Temporary Revisions,

.
updates of the modification level (Section 1.1),

.
updated mass and balance information (Section 6.3),

.
updates of the Equipment Inventory (Section 6.5), and

.
updates of the List of Supplements (Section 9.2) must be recorded in the following table.


The new or amended text is indicated by a vertical black line at the left hand side of the revised page, with the revision number and date appearing at the bottom of the page.
If pages are revised which contain information valid for your particular serial number (modification level of the airplane, weighing data, Equipment Inventory, List of Supplements), then this information must be transferred to the new pages in hand-writing.
The cover pages of Temporary Revisions, if applicable, are inserted behind the cover page of this manual; the following pages of the Temporary Revision are inserted in front of the corresponding pages of this AFM. Temporary Revisions are used to provide information on systems or equipment until the next 'permanent' Revision of the Airplane Flight Manual. When a 'permanent' Revision covers a Mandatory or Optional Design Change Advisory (M.M or O.M), then the corresponding Temporary Revision is superseded. Example: Revision 3 covers O.M 42-053, therefore the Temporary Revision TR-O.M-42-053 is superseded by the 'permanent' Revision 3.
 
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