曝光臺(tái) 注意防騙 網(wǎng)曝天貓店富美金盛家居專營(yíng)店坑蒙拐騙欺詐消費(fèi)者

This supplement is part of, and must be placed in, the basic FAA Approved Airplane Flight Manual
for Brazilian Registered Airplanes. The information contained herein supplements the information of
the basic FAA Approved Airplane Flight Manual. For limitations, procedures and performance
information not contained in this supplement, consult the basic FAA Approved Airplane Flight
Manual.
OPERATING LIMITATIONS
GARMIN G1000 AVIONICS SYSTEM - LIMITATIONS
TIS is not operational on Brazilian airplanes.
GARMIN G1000 GPS NAVIGATION SYSTEM - LIMITATIONS
1. Manual entry of approach waypoints is prohibited.
2. The pilot must review the complete transition-approach, comparing the waypoints and
altitudes displayed on the FMS flight plan with those on the published procedure prior to
activation, to insure that the correct procedure and transition are selected.
3. FMS/GPS approaches must be performed with a pictorial situational awareness system
(moving map) available to the pilot.
4. FMS/GPS approaches must be performed with autopilot or flight director engaged.
5. If “RAIM” becomes not available in terminal area phase of flight, GPS-based navigation
should be reverted to another IFR-approved navigation system.
6. IF “RAIM” becomes not available in enroute phase of flight, continue to navigate using the
GPS equipment or revert to an alternate means of navigation other than GPS appropriate to
the route and phase of flight. When continuing to use GPS navigation, position must be
verified every 15 minutes using another IFR-approved navigation system.
510FM-S8-01 S8-AA S8-5
SECTION V - SUPPLEMENTS MODEL 510
SUPPLEMENT 8
FAA APPROVED
U.S. Configuration
OPERATING PROCEDURES
The operating procedures are the same as those in the basic FAA Approved Airplane Flight Manual
except as follows:
EMERGENCY PROCEDURES
􀂄 TAILCONE BLEED LEAK
(RED TAIL CONE BLD LK CAS MESSAGE)
Indicates that the tail cone temperature sensor has detected a tail cone temperature over 82ºC
(180ºF) which may indicate a bleed air leak or fire in the tailcone.
• IF CAS MESSAGE EXTINGUISHES
(INDICATES POSSIBLE BLEED LEAK FROM IDLE ENGINE)
3. Throttle - MAINTAIN REDUCED POWER to keep message extinguished.
4. Land as soon as practical.
Procedure Completed
• IF MESSAGE DOES NOT CLEAR
3. Throttle (idle engine) - AS REQUIRED.
4. Throttle (opposite engine) - IDLE.
􀀀 IF CAS MESSAGE CLEARS
(INDICATES POSSIBLE BLEED LEAK FROM IDLE ENGINE)
5. Throttle - MAINTAIN REDUCED POWER to keep message extinguished.
6. Land as soon as practical.
Procedure Completed
􀀀 IF CAS MESSAGE STILL DOES NOT CLEAR
(INDICATES POSSIBLE TAILCONE / BAGGAGE FIRE OR MAJOR
BLEED LEAK)
5. Use minimum symmetric power as required for descent and landing. Consider the
potential of baggage or tailcone fire and subsequent need for emergency evacuation
after landing.
6. Land as soon as possible.
Procedure Completed
1. L and R Engine ITT - NOTE.
2. Throttle (engine with highest ITT) - IDLE. (If unable to determine a higher ITT, start
procedure by retarding the left engine to IDLE.)
S8-6 S8-AA 510FM-S8-00
MODEL 510 SECTION V - SUPPLEMENTS
SUPPLEMENT 8
FAA APPROVED
Configuration U.S.
ABNORMAL PROCEDURES
No change.
NORMAL PROCEDURES
No change.
PERFORMANCE
No change.
DESCRIPTION
No change.
510FM-S8-00 S8-AA S8-7/S8-8

MODEL 510 SECTION V - SUPPLEMENTS
SUPPLEMENT 8
FAA APPROVED
Configuration U.S.
LOG OF ANAC ACCEPTED SUPPLEMENTS
The following list contains ANAC accepted supplements. Refer to Log of Approved Supplements in
the basic FAA Approved Airplane Flight Manual for revision status.
SUPPLEMENT
NUMBER
NAME EQUIPMENT
INSTALLED
1 Garmin FlightCharts or Jeppesen Chartview
System
2 Steep Approach Operations
3 Citation Performance Calculator (CPCalc)
7 Traffic Advisory System
8 Brazilian Registered Airplanes
9 Honeywell KHF1050 HF Transceiver with PS440
Control Display Unit
10 Iridium Satcom Antenna
510FM-S8-00 S8-AA S8-9/S8-10

U.S.
MODEL 510
510-0001 AND ON
SUPPLEMENT 9
HONEYWELL KHF 1050 HF TRANSCEIVER WITH
PS440 CONTROL DISPLAY UNIT
24 AUGUST 2007
S9-1
COPYRIGHT © 2007
CESSNA AIRCRAFT COMPANY
WICHITA, KANSAS, USA
510FM-S9-00
SECTION V - SUPPLEMENTS MODEL 510
SUPPLEMENT 9
FAA APPROVED
U.S. Configuration
SUPPLEMENT 9
HONEYWELL KHF 1050 HF TRANSCEIVER WITH PS440
CONTROL DISPLAY UNIT
Use the Log of Effective Pages to determine the current status of this supplement. Pages affected by
　
中國(guó)航空網(wǎng) www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：Citation Mustang airplane flight manual 3(12)