Garmin SA01535Wi_D- User Manual

Garmin SA01535Wi_D

Garmin SA01535Wi_D– User Manual, read for free online in PDF format. We hope this helps you resolve any issues you may have. If you have further questions, please contact us through the contact form.

1 Page 1
2 Page 2
3 Page 3
4 Page 4
5 Page 5
6 Page 6
7 Page 7
8 Page 8
9 Page 9
10 Page 10
11 Page 11
12 Page 12
13 Page 13
14 Page 14
15 Page 15
16 Page 16
17 Page 17
18 Page 18
19 Page 19
20 Page 20
21 Page 21
22 Page 22
23 Page 23
24 Page 24
25 Page 25
26 Page 26
27 Page 27
28 Page 28
29 Page 29
30 Page 30
31 Page 31
32 Page 32
33 Page 33
34 Page 34
35 Page 35
36 Page 36
37 Page 37
38 Page 38
39 Page 39
40 Page 40
41 Page 41
42 Page 42
43 Page 43
44 Page 44
45 Page 45
46 Page 46
47 Page 47
48 Page 48
49 Page 49
50 Page 50
51 Page 51
52 Page 52
53 Page 53
54 Page 54
55 Page 55
56 Page 56
57 Page 57
58 Page 58
59 Page 59
60 Page 60
61 Page 61
62 Page 62
63 Page 63
64 Page 64
65 Page 65
66 Page 66
67 Page 67
68 Page 68
69 Page 69
70 Page 70
71 Page 71
72 Page 72
73 Page 73
74 Page 74
75 Page 75
76 Page 76
77 Page 77
78 Page 78
79 Page 79
80 Page 80
81 Page 81
82 Page 82
83 Page 83
84 Page 84
85 Page 85
86 Page 86
87 Page 87
88 Page 88
89 Page 89
90 Page 90
91 Page 91
92 Page 92
93 Page 93
94 Page 94
95 Page 95
96 Page 96
97 Page 97
98 Page 98
99 Page 99
100 Page 100
101 Page 101
102 Page 102
103 Page 103
104 Page 104
105 Page 105
106 Page 106
107 Page 107
108 Page 108
109 Page 109
110 Page 110
111 Page 111
112 Page 112
113 Page 113
114 Page 114
115 Page 115
116 Page 116
117 Page 117
118 Page 118
119 Page 119
120 Page 120
121 Page 121
122 Page 122
123 Page 123
124 Page 124
125 Page 125
126 Page 126
127 Page 127
128 Page 128
129 Page 129
130 Page 130
131 Page 131
132 Page 132
133 Page 133
134 Page 134
135 Page 135
136 Page 136
137 Page 137
Page: / 137

Table of Contents:

  • Page 2 – Street
  • Page 3 – Supplement for; See Cover
  • Page 4 – This page intentionally left blank.
  • Page 5 – FAA APPROVED; Table of Contents
  • Page 7 – USE OF THE HANDBOOK
  • Page 8 – OPERATIONAL APPROVALS
  • Page 9 – Navigation information is referenced to WGS-84 reference system.; ELECTRONIC FLIGHT BAG
  • Page 10 – ABBREVIATIONS AND TERMINOLOGY; Aeronautical Information Regulation And Control
  • Page 15 – Section 2 - Limitations; INTRODUCTION
  • Page 16 – POWER PLANT LIMITATIONS AND INDICATOR MARKINGS; NOTE; load and/or increasing N
  • Page 17 – MANEUVER LIMITS; AND
  • Page 18 – Limitations are in bolded text for this section only; If the AIRAC cycle will; In the event of a predicted continuous loss of
  • Page 19 – In the event of a predicted; Pilots
  • Page 21 – AHRS AREAS OF OPERATION
  • Page 22 – Figure 1, GRS 77 Geographic Limits
  • Page 23 – AUTOPILOT OPERATION LIMITS; Do not use autopilot or yaw damper during takeoff and landing.; Do not use autopilot below the following altitudes:; SYNTHETIC VISION AND PATHWAYS LIMITS
  • Page 24 – The TAWS databases have an area of coverage as detailed below:
  • Page 25 – OPTIONAL L3 COMMUNICATIONS AVIONICS SYSTEM WX-500 STORMSCOPE; On Instrument Panel above the Standby Attitude Indicator:
  • Page 26 – KINDS OF OPERATION LIMITS; Day; KINDS OF OPERATIONS EQUIPMENT LIST
  • Page 31 – Section 3 - Emergency Procedures
  • Page 32 – AUTOMATIC FLIGHT CONTROL SYSTEM; AUTOPILOT MALFUNCTION / PITCH TRIM RUNAWAY; (Be prepared for possible high elevator control forces)
  • Page 33 – Boost; If Condition Persists:
  • Page 34 – MANUAL AUTOPILOT DISCONNECT; Attitude
  • Page 35 – AUTOPILOT FAILURE; Advise ATC of loss of autopilot system.; Record each altimeter reading for contingency procedure use; the loss of automatic altitude hold capability.
  • Page 37 – PITCH TRIM FAILURE; If Red
  • Page 38 – AUTOPILOT OVERSPEED RECOVERY; annunciation on PFD); Levers; After underspeed condition is corrected:
  • Page 39 – ELECTRICAL SYSTEM; If Neither Generator Will Reset:
  • Page 40 – LOAD MANAGEMENT TABLE; EQUIPMENT
  • Page 41 – TAWS AND GPWS; TAWS OR GPWS WARNING; MAXIMUM; After Warning Ceases:; TCAS II; TCAS II RESOLUTION ADVISORY; (Red on PFD and aural resolution advisory)
  • Page 42 – WINDSHEAR ENCOUNTER; (To prevent automatic autopilot; After Exiting Windshear:; ESP ENGAGEMENT; Refer to Section 7 – Systems Description, “Electronic
  • Page 43 – Section 3A - Abnormal Procedures
  • Page 45 – or; In RVSM Airspace and Autopilot Inoperative:
  • Page 46 – ELECTRIC PITCH TRIM INOPERATIVE; If still inoperative:
  • Page 49 – FLASHING AMBER MODE ANNUNCIATION
  • Page 50 – YAW AXIS FAILURE (Amber; If the amber; ELECTRONIC STABILITY AND PROTECTION; MANUAL ESP DISENGAGEMENT
  • Page 51 – G1000 INTEGRATED AVIONICS SYSTEM; ALTITUDE MISCOMPARE; If Pilot and Standby
  • Page 52 – If Copilot and Standby Altimeter Agree (Pilot Altimeter Differs):
  • Page 53 – If Able to Identify Accurate Altitude Source:; If Unable to Identify Accurate Altitude Source:; WARNING
  • Page 54 – AIRSPEED MISCOMPARE; Softkey
  • Page 55 – If Pilot’s and Copilot’s Altitude Agree:; PITCH MISCOMPARE
  • Page 56 – HEADING MISCOMPARE
  • Page 57 – If a loss of altitude error correction advisory is received:; DISPLAY UNIT FAILURE; PFD FAILURE; SELECT operating transponder
  • Page 58 – MFD FAILURE; Panel; LOSS OF GPS/SBAS NAVIGATION DATA; USE ALTERNATE SOURCES
  • Page 59 – If No Alternate Navigation Sources Are Available:; ALL INFORMATION NORMALLY DERIVED FROM GPS TURNS AMBER. ALL OF THIS; TAWS is inoperative.; GPS APPROACH ALARM LIMITS EXCEEDED
  • Page 60 – ILS DATABASE FREQUENCY AND/OR COURSE MISMATCH; Prior to Turning Inbound on the Final Approach Course; LOSS OF RADIO TUNING FUNCTIONS; Frequency
  • Page 61 – LOSS OF ALTITUDE ALERTER IN RVSM AIRSPACE
  • Page 62 – FAILED ATTITUDE AND/OR HEADING; If in RVSM airspace:
  • Page 63 – If in RVSM airspace and autopilot inoperative:
  • Page 64 – ENGINE INDICATION SYSTEM (EIS) FAILURE; If All Engine Gauges on One Engine Red ‘X’:; LOSS OF NAVIGATION DATA; INACCURATE FLIGHT DIRECTOR DISPLAY; CROSSCHECK BOTH PFDs with the Standby Attitude Indicator; ENGAGE AS DESIRED if flight director commands are appropriate
  • Page 65 – BOTH ON ADC1, BOTH ON ADC2; BOTH ON AHRS 1, BOTH ON AHRS 2; Displays; BOTH ON GPS 1, BOTH ON GPS 2; Status
  • Page 66 – USING ADC1 or ADC2; SYNTHETIC VISION; If G1000 operation in display backup mode is required:
  • Page 67 – TAWS or GPWS CAUTION; To Inhibit TAWS
  • Page 68 – To Enable GPWS if Inhibited:; To Override Flap Altering:
  • Page 69 – To Inhibit Glideslope or Glidepath Alerting:
  • Page 71 – Section 4 - Normal Procedures
  • Page 73 – COM RADIO COMMUNICATIONS BEFORE STARTING ENGINES; To obtain an ATC clearance before starting the engines:; PREFLIGHT INSPECTION; RIGHT AFT FUSELAGE
  • Page 74 – Figure 2, RVSM Critical Region
  • Page 75 – BEFORE ENGINE STARTING; Autopilot
  • Page 76 – BEFORE TAXI
  • Page 78 – With Elevator Tab Wheel in Motion,; TAKEOFF; Maximum Difference: 200 Feet
  • Page 79 – IN FLIGHT; SHUTDOWN AND SECURING; OTHER PROCEDURES
  • Page 80 – VERTICAL MODES; ‘ALT’
  • Page 81 – to the vertical clearance limit.; Vertical DIRECT TO; To descend from the present position to a waypoint:
  • Page 82 – LATERAL MODES
  • Page 83 – ILS
  • Page 84 – If Flying Full Approach Including Transition:; Or
  • Page 89 – VOR APPROACH
  • Page 91 – IF Flying Full Approach Including Transition:
  • Page 92 – At An Appropriate Safe Altitude:
  • Page 93 – nose; alternate before leaving the missed approach holding fix):
  • Page 94 – Recommended Procedures Following a Missed Approach:
  • Page 95 – Use of Pathways; Departure
  • Page 96 – Approach
  • Page 99 – Section 5 – Performance
  • Page 101 – Section 6 - Weight and Balance
  • Page 103 – Section 7 - Systems Description
  • Page 104 – GENERAL; SYSTEM OVERVIEW
  • Page 105 – Figure 3, Instrument Panel
  • Page 107 – Figure 5, Copilot's Control Wheel With Trim Switches
  • Page 108 – Figure 6, Copilot's Control Wheel Without Trim Switches
  • Page 109 – Figure 7, Overhead Panel
  • Page 110 – Figure 8, Right Side Circuit Breaker Panel
  • Page 111 – Figure 9, Pedestal Configuration
  • Page 112 – Figure 10, GFC 700 System Interface
  • Page 113 – FLIGHT CONTROLS; AFCS, AUTOPILOT, FLIGHT DIRECTOR AND RUDDER BOOST
  • Page 115 – AFCS VERTICAL MODES
  • Page 116 – AFCS LATERAL MODES
  • Page 117 – ELECTRIC ELEVATOR TRIM
  • Page 120 – Figure 13 – Engagement Limit Indications Upon ESP Activation
  • Page 121 – Autopilot Underspeed Protection
  • Page 122 – FLIGHT INSTRUMENTS; STANDBY FLIGHT INSTRUMENTS; Standby attitude indicator; Figure 15, Standby Flight Instruments
  • Page 123 – ENGINE INSTRUMENTATION; ) operation is monitored by the gas
  • Page 124 – PROPELLER SYNCHROPHASER; INVERTERS
  • Page 126 – TRIPLE FED BUS
  • Page 127 – Surface Deice
  • Page 128 – STANDBY BATTERY POWER SUPPLY; OFF
  • Page 129 – LIGHTING SYSTEMS; COCKPIT; PITOT AND STATIC SYSTEM; PITOT
  • Page 130 – STATIC; GROUND COMMUNICATIONS
  • Page 131 – General
  • Page 132 – Obstacle and Terrain Alerts and Warnings
  • Page 134 – Airport Signs and runway highlight
  • Page 135 – VCO Description
  • Page 137 – Section 8 – Handling, Service, and Maintenance
Loading the manual

"Loading the manual" means you need to wait until the file loads and becomes available for online reading. Some manuals are very large, and the time they take to appear depends on your internet speed.

Summary

Page 2 - Street

Hawker Beechcraft King Air 300/300LW 190-00716-02 Rev. 1 Page 2 of 137 © Copyright 2012 GARMIN Ltd. or its subsidiaries All Rights Reserved Except as expressly provided herein, no part of this manual may be reproduced, copied, transmitted, disseminated, downloaded or stored in any storage medium, fo...

Page 3 - Supplement for; See Cover

190-00716-02 Rev. 1 Hawker Beechcraft King Air 300/300LW Page 3 of 137 GARMIN International, Inc Log of Revisions Pilot’s Operating Handbook and FAA Approved Airplane Flight Manual Supplement for G1000 Integrated Avionics System and GFC 700 AFCS In Hawker Beechcraft King Air 300/300LW Aircraft REV N...

Page 4 - This page intentionally left blank.

Hawker Beechcraft King Air 300/300LW 190-00716-02 Rev. 1 Page 4 of 137 This page intentionally left blank.

Other Garmin Models