Hawker Beechcraft Hawker 800XP, Руководство по эксплуатации для пилотов

Страница: 24 / 923

Page 2 of 4
SECTION & PAGES DESCRIPTION
Sub-section 9 - Electrical
Power
Pages 9-1 thru 9-24 Revised headers to Hawker Beechcraft format and footers for
Revision A4.
Page 9-5 Figure 1, removed a green bar connecting the Starter Busbar to
the PS2 Busbar.
Page 9-12 Figure 4, revised APU GEN FAIL annunciator.
Page 9-16 DOUBLE GENERATOR FAILURE, removed XE FAIL
annunciator.
Page 9-17 Figure 6, removed GEN 2 FAIL annunciator.
Page 9-19 Figure 8, removed APU GEN FAIL annunciator.
Sub-section 17 - Avionics
Pages 17-1 thru 17-22 Revised headers to Hawker Beechcraft format and footers for
Revision A4.
Page 17-1 Table of Contents, added "ACP" to "Operation" and revised the
indentation of four entries.
Page 17-10 Incorporated Temporary Change 3.
Page 17-22 MODE 7, revised "WINDHEAR" to "WINDSHEAR".
Section IV - FLIGHT
PLANNING DATA
Sub-section 6 - Single
Engine
Pages 6-1 thru 6-42 Revised headers to Hawker Beechcraft format and footers for
Revision A4.
Page 6-1 Table of Contents, added "SINGLE ENGINE" to "DRIFT
DOWN"; added "SINGLE ENGINE MAXIMUM CONTINUOUS
THRUST FOR DESCENT AND CRUISE".
Page 6-2 Added the following Table of Contents listings: "SINGLE
ENGINE HIGH SPEED DESCENT", "SINGLE ENGINE MAXI-
MUM CONTINUOUS THRUST CRUISE", and tables from
10,000 ft through 27,000 ft.
Page 6-3 Added "SINGLE ENGINE" to "DRIFT DOWN" heading.
Page 6-4 INTRODUCTION, added Single Engine
Maximum Continuous Thrust for Descent and
Cruise heading and text.
Page 6-9 Added Figure number and title to chart.
Pages 6-30 and 6-31 Added Single Engine Maximum Continuous Thrust High Speed
Descent tables.
Pages 6-32 thru 6-42 Added Single Engine Maximum Continuous Thrust Cruise
tables and an intentionally left blank page.
A4