曝光台 注意防骗
网曝天猫店富美金盛家居专营店坑蒙拐骗欺诈消费者
first departure of each day. If flight time for the day exceeds eight (8)
hours, a second stall barrier check is required prior to the second flight
of the day. This test is performed only on the ground and cannot be
tested in flight.
1. STALL BARRIER Switch............................................................ON
2. Display Controllers (Both).............................SELECT TEST MENU
3. Sea Level (S/L) Line Select Keys (Both) ..........................................
..................................SIMULTANEOUSLY DEPRESS AND HOLD
Continue holding both S/L line select keys until the normalized AOA
indicator pointer slews. Then verify the following:
A. Stall Warning (Control Column Shaker) ......................................
......................................... OCCURS BETWEEN 0.70 AND 0.80
B. Stall Barrier (Control Column Pusher) .........................................
......................................... OCCURS BETWEEN 0.95 AND 1.07
C. A/P DISC (BARR DISC) Button ...................................................
............................OVERRIDES PUSHER WHEN DEPRESSED
Continued on next page
Quick Reference Handbook
NORMAL PROCEDURES REVISION 7
Page NH -10 May 30/02
3. ALT Line Select Keys (Both) ............................................................
.................................. SIMULTANEOUSLY DEPRESS AND HOLD
Continue holding both ALT line select keys until the normalized
AOA indicator pointer slews. Then verify the following:
A. Stall Warning (Control Column Shaker)......................................
.........................................OCCURS BETWEEN 0.54 AND 0.65
B. Stall Barrier (Control Column Pusher).........................................
.........................................OCCURS BETWEEN 0.79 AND 0.90
C. A/P DISC (BARR DISC) Button...................................................
........................... OVERRIDES PUSHER WHEN DEPRESSED
NOTE: Both pilot’s and copilot’s sides have to be tested simultaneously
in order to activate the control column pusher.
NOTE: Another momentary push of the TEST function key may be
required to ensure the AOA indicator is in the normal area prior to
takeoff.
END
Quick Reference Handbook
REVISION 8 NORMAL PROCEDURES
Oct 11/02 Page NI - 1
Guidelines for the Application of SAE Type I, II and IV
De-icing Fluid Mixtures: Minimum Concentrations as a
Function of Outside Air Temperature AFM APPENDIX E
SOURCE DOCUMENTATION: GIV AFM Appendix E, based on FAA
Bulletin No. FSAT 02-05: FAA-Approved Deicing Program (Winter 2002-2003
Update), dated 09/23/02.
SAE Type I De-icing Fluid Mixtures:
SAE Type II and SAE Type IV De-icing Fluid Mixtures:
OAT One Step Process Two Step Process
°C °F De-icing / Anti-icing Step 1: De-icing Step 2: Anti-icing1
-3 and above 27 and above
Water or mix of fluid
and water heated to
60°C (140°F) minimum
at the nozzle.
Below -3 Below 27
Mix of fluid and water
heated to 60°C (140°F)
minimum at the nozzle,
with a freeze point of at
least 10°C (18°F)
below OAT
FP of heated fluid
mixture shall not be
more than 3°C (5°F)
above OAT
Mix of fluid and water
heated to 60°C (140°F)
minimum at the nozzle,
with a freeze point of at
least 10°C (18°F)
below OAT
Note: Upper temperature limit shall not exceed fluid and aircraft manufacturers recommendations.
CAUTION: WING SKIN TEMPERATURES MAY DIFFER AND IN SOME CASES MAY BE LOWER THAN OAT.
A STRONGER MIX (MORE GLYCOL) CAN BE USED UNDER THE LATTER CONDITIONS.
(1) To be applied before first step fluid freezes, typically within 3 minutes.
°C = Degrees Celsius / °F = Degrees Fahrenheit / OAT = Outside Air Temperature / FP = Freezing Point
CAUTION: SAE TYPE I FLUID USED DURING GROUND DE-ICING/ANTI-ICING IS NOT INTENDED FOR AND DOES
NOT PROVIDE PROTECTION DURING FLIGHT.
OAT One Step Process Two Step Process
°C °F De-icing / Anti-icing Step 1: De-icing Step 2: Anti-icing1
-3 and above 27 and above 50/50 Heated2 Type
II/IV
Water heated or a
heated mix of Type I,
II or IV with water
50/50 Type II/IV
Below -3 to -14 Below 27 to 7 75/25 Heated2 Type
II/IV 75/25 Type II/IV
Below -14 to -25 Below 7 to -13 100/0 Heated2 Type
II/IV
Heated suitable mix of
Type I, Type II/IV and
water with FP not
more than 3°C (5°F)
above actual OAT
100/0 Type II/IV
Below -25 Below -13
SAE Type II/IV fluid may be used below -25°C (-13°F) provided that the
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址:
湾流4快速检查单QRH GULFSTREAM IV QUICK REFERENCE HANDBOOK 1(29)