曝光臺 注意防騙 網曝天貓店富美金盛家居專營店坑蒙拐騙欺詐消費者

(SAT) is below +8° C and visible moisture, precipitation, or wet runway are present. Engine
operation of 85% LP for one (1) minute is recommended just prior to takeoff and at intervals of
not more than sixty (60) minutes under these temperature and moisture conditions.
Depart icing conditions if COWL PRESSURE LOW message illuminates and Cowl Anti-Ice
Pressure cannot be maintained at or above 4 psi.
NOTE: The Cowl Pressure Low message illuminates at 4 psi SN 1190 and subs. and SN 1000
thru 1189 with ASC 243, and at 10 psi for SN 1000 thru 1189 without ASC 243. Cowl
anti-ice is effective at 4 psi or greater.
Use of Cowl Anti-Icing System is required in flight as indicated on TEMPERATURE RANGE
FOR COWL ANTI-ICING figure, when visible moisture or precipitation is present or when signs
of icing are observed. Ice accretion may be observed on wings or windshield edges.
GULFSTREAM AEROSPACE
GIV AIRPLANE FLIGHT MANUAL
SECTION 1
LIMITATIONS
1-32 FAA APPROVED
31 May 2000
Figure 1-8: Temperature Range for Cowl Anti-Icing
GULFSTREAM AEROSPACE
GIV AIRPLANE FLIGHT MANUAL
SECTION 1
LIMITATIONS
FAA APPROVED 1-33
31 May 2000
1-31-00: INDICATING/RECORDING
1-31-10: Electronic Checklist:
Electronic Checklist Document Number 1159AV41201-20 corresponds to this revision of
Airplane Flight Manual for SPZ 8000 equipped airplanes.
Electronic Checklist Document Number 1159AV41202-20 corresponds to this revision of
Airplane Flight Manual for SPZ 8400 equipped airplanes.
Electronic Checklist Document Number 1159AV41201-8 and 1159AV41202-10 are acceptable
for use until the checklist modules can be updated.
Checklist version can be verified by selecting TITLE PAGE of Electronic Checklist.
GULFSTREAM AEROSPACE
GIV AIRPLANE FLIGHT MANUAL
SECTION 1
LIMITATIONS
1-34 FAA APPROVED
31 May 2000
1-32-00: LANDING GEAR
1-32-10: Brake System:
Takeoff is prohibited with BRAKE FAIL or BRAKE PEDAL message displayed.
1-32-20: Anti-Skid System:
Takeoff is permitted with Anti-Skid inoperative, provided Ground Spoilers are operative, 20°
flaps are used, and the cowl and wing anti-icing systems are not used.
1-32-40: Landing Lights:
Ground operation of landing lights is limited to five (5) minutes.
GULFSTREAM AEROSPACE
GIV AIRPLANE FLIGHT MANUAL
SECTION 1
LIMITATIONS
FAA APPROVED 1-35
30 May 2002
1-34-00: NAVIGATION
1-34-10: Airborne Weather Radar:
When operating weather radar on the ground, the following limitations apply:
Do NOT operate radar during refueling of the airplane nor when within 300 ft (92 meters) of
other refueling operations.
Do NOT operate radar within 49 ft (15 meters) of ground personnel with 24” antenna installed.
Do NOT operate radar within 33 ft (10 meters) of ground personnel with 18” antenna installed.
1-34-20: Inertial Reference System (IRS):
When operating in "ATT-REF" mode, do NOT use IRS heading information unless airplane
heading is manually entered via the ISDU or the appropriate IRS status page on the FMS CDU.
NOTE: For SPZ 8000 equipped airplanes, heading will appear as 000° when the IRS is selected
to "ATT-REF".
For SPZ 8400 equipped airplanes:
NOTE: HDG FAIL will appear on the HSI until a valid airplane heading is manually entered via
the ISDU or IRS status page on the FMS CDU.
Honeywell HG1075AE Series IRS equipment installed in Gulfstream IV has been certified for
alignment to 78° Latitudes. For alignment between 70° and 78° Latitude, fifteen (15) minute
alignment time is required. For flight above 73° N and 60° S Latitude, EFIS heading information
must be switched from MAG to TRUE due to loss of valid MAG heading from the IRS. Above
73° N and 60° S Latitude with TRUE heading information displayed, ILS, MLS, TCN, and VOR
navigation capability is unavailable unless special procedures in GIV Operating Manual are
followed.
GULFSTREAM AEROSPACE
GIV AIRPLANE FLIGHT MANUAL
SECTION 1
LIMITATIONS
1-36 FAA APPROVED
30 May 2002
1-34-30: Pilot’s Manuals:
For SPZ-8000 equipped airplanes, the Honeywell SPZ-8000 Digital Integrated Flight Control
System (Phase II) Pilot’s Manual for the Gulfstream IV, Honeywell Publication Number A28-
1146-064, Revision 5, dated October 1999 (or later approved revision) is to be immediately
available to the flight crew.
For SPZ-8400 equipped airplanes, the Honeywell SPZ-8400 Digital Automatic Flight Control
System Pilot’s Manual for the Gulfstream IV, Honeywell Publication Number A28-1146-097,
Revision 2, dated October 1999 (or later approved revision) is to be immediately available to the
　
中國航空網 www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：灣4飛機飛行手冊AFM Gulfstream IV AIRPLANE FLIGHT MANUAL 1(21)