Garmin Cessna Caravan G1000 파일럿 매뉴얼 - 페이지 15
{카테고리_이름} Garmin Cessna Caravan G1000에 대한 파일럿 매뉴얼을 온라인으로 검색하거나 PDF를 다운로드하세요. Garmin Cessna Caravan G1000 16 페이지. Integrated flight deck
Garmin Cessna Caravan G1000에 대해서도 마찬가지입니다: 파일럿 매뉴얼 (6 페이지), 파일럿 매뉴얼 (32 페이지), 파일럿 매뉴얼 (25 페이지), 파일럿 매뉴얼 (34 페이지), 파일럿 매뉴얼 (21 페이지), 비행기 비행 매뉴얼 보충 자료 (33 페이지), 파일럿 매뉴얼 (22 페이지)
페이지 인쇄
A
AC 120-80
10
AC 23-17B
10
AC 43.13-1B
10
ADC
3, 4, 8, 9, 10
ADM
7
AFMS
7
AFS-600
7, 10
AHRS
3, 4, 7, 8, 9, 10
AIM
7
Airborne traffic
5
Aircraft manufacturer
7, 8
Approach procedure
7
APV
7
Areas of Operation IV
7, 8
Cessna Nav III
10
Areas of Operation VII-D
7, 10
ARINC 429
3
Audio panel
2, 3, 5, 8
Autopilot
7, 8, 9, 10
B
Backup
7, 8, 9, 10
Backup instruments
7, 8
C
Cessna Nav III aircraft
10
CFII
1
CFIT
7
Check-ride
1
CHT
5
Circuit breakers
1, 8, 9, 10
Class B
4, 9
Class C
4, 9
COM/MIC buttons
5
COM/NAV/GPS
4
COM/NAV frequencies
4
Components
1, 2, 3
COM radio
5
Configuration modules
3
Copyright
i
Cross-track
10
D
Databus
3
Dimming controls
8
Direct-to navigation
7
DISPLAY BACKUP button
3, 5, 8, 10
DPE
1
E
E6B calculations
4
EGT
5
EIS
3, 5
Emergency mode
5
190-00368-02 Rev. A
INDEX
Engine/airframe interface
Engine instrumentation
ENT key
8, 10
F
FAA-S-8081-4D
1, 7
Failure indications
6
Failure mode
1, 3, 4, 5, 7
Flight plan
7
FMS
7, 8, 10
Frequencies
9
Fuel
5
Full component failure
Full panel
8
G
G1000 system
2
GDC 74A (ADC)
4
GDL-69/69A (weather datalink)
GDU 1040 (display)
GEA 71 (engine/airframe)
GIA 63 (IAU)
3, 4
GMA 1347 (audio panel)
GMU 44 (magnetometer)
GPS navigation
4
GRS 77 (AHRS)
4
GTX 32 (transponder)
GTX 33 (transponder)
Gyro
4
H
Hardware
3
HDG
9
HMI
4
I
Index
11
Intercom system
5
L
LCD
2
Lightning detection
List of figures
ii
LRU
2
M
Magnetometer
4
Marker beacon
5
MENU key
8, 10
MFD
3, 8, 10
Mode A
4, 9
Mode C
5
Mode C veil
9
Mode S
4, 5, 7
Moving map
3, 9, 10
Garmin G1000 Guide for Designated Pilot Examiners & Certified Flight Instructors
N
3, 4, 5
1, 5
NAV/COM audio
NAV button
NAV mode
NAV radio
O
OAT
Oil pressure
Oil temperature
P
4
Partial failure
Partial panel
PFD
POH
Practical examination
Precision approach
7
Primary flight instruments
3, 5
PTS
4, 5
R
5, 8
4
Reversionary mode
RM
Roll mode
5
RPM
4, 5, 7
RS-232
RS-485
S
Setup Menu window
SRM
System architecture
T
Table of contents
TAS
Task D
Technical support
Terrain awareness
TIS
7
Trademark
Transponder
TSO C-146
Turn-rate
V
Vacuum system
VOR/LOC/GS
W
WAAS
Weather datalink
5
5
9
5
4
5
5
4
8
3, 4, 5, 8, 9, 10
7
7
10
8, 9
1, 7, 8, 10
3, 5, 6, 8, 10
7
9, 10
5
3
3
8
7
1
ii
4
10
1
7
5, 7
i
3, 4, 5, 7, 9
7
4
5
4
7
7
11