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crew and will be noted on
ADLS.
22-1
GULFSTREAM AEROSPACE CORPORATION PAGE NUMBER: 22-1
AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-IV MMEL REVISION NO.: 5 MOP REV. NO.: 5
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES MANUAL MMEL DATE: 10/11/01 MOP DATE: 10/11/01
1. 2. NUMBER INSTALLED
SYSTEM & 5. MAINTENANCE 6. OPERATIONAL 7. PLACARDING
SEQUENCE 3. NUMBER REQ’D FOR DISPATCH PROCEDURES PROCEDURES PROCEDURES
NUMBERS 4. MMEL REMARKS OR
EXCEPTIONS
22. AUTO FLIGHT
1. Flight Guidance C
Computers (FGC)
2 1 (O) One may be inoperative provided flight
time with one engine inoperative does not
exceed one hour cruise from a suitable
airport.
NOTE: Each FGC provides mach trim
compensation, electric trim, yaw damper,
autopilot, and flight director functions
independent of the other FGC. Failure of
the second FGC after dispatch would result
in the complete loss of these functions, and
AFM restrictions would apply.
None required. Flight crew will ensure flight
time with one engine
inoperative will NOT exceed
one (1) hour cruise from a
suitable airport. Flight crew
shall be aware failure of
second FGC after dispatch
will result in complete loss of
mach trim compensation,
electric trim, yaw damper,
autopilot, and flight director
functions and AFM
restrictions will apply.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
C 2 0 (O) Both may be inoperative provided:
a) Automatic Cabin Pressurization
System is operative,
b) Flight time with one engine
inoperative does not exceed one
hour cruise from a suitable
airport,
c) Landing weather minimums are
not dependent upon its use,
d) Airplane is operated at or below
FL 390, and
e) Airplane is operated in
accordance with AFM
Limitations for Mach Trim and
Yaw Damper.
None required. Flight crew will ensure:
a) Flight remains at or
below FL 390.
b) Landing Weather
Minimums are not
predicated on use of
FGC’s.
c) Automatic Cabin
Pressurization System is
operative. AFM ,
Normal Procedures .
d) AFM Limitations are
complied with.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
22-2
GULFSTREAM AEROSPACE CORPORATION PAGE NUMBER: 22-2
AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-IV MMEL REVISION NO.: 5 MOP REV. NO.: 5
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES MANUAL MMEL DATE: 10/11/01 MOP DATE: 10/11/01
1. 2. NUMBER INSTALLED
SYSTEM & 5. MAINTENANCE 6. OPERATIONAL 7. PLACARDING
SEQUENCE 3. NUMBER REQ’D FOR DISPATCH PROCEDURES PROCEDURES PROCEDURES
NUMBERS 4. MMEL REMARKS OR
EXCEPTIONS
22. AUTO FLIGHT
2. Auto-throttle D
*** Systems
None required. None required. An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
3. Performance C
*** Computers (PZ)
2 0 None required. Flight crew can expect a
Degradation of following
SPZ-8000 /SPZ-8400 subsystems:
Navigation
Computer, Display
Controller and a loss of
Auto-throttle functions. On
S/N 1183, 1214 & subsequent
Engine Synchronizer will
also be unavailable.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
4. Yaw Damper System C 1 0 (M) May be inoperative provided:
a) Airplane is operated in
accordance with AFM
Limitations, and
b) Procedures are established to
deactivate Yaw Damper System.
Maintenance will, if available,
ensure airplane is properly
fueled and Yaw Damper
System is deactivated utilizing
Yaw Damp Switch.
Flight crew will ensure Yaw
Damp Switch is selected to
Disengaged and airplane is
properly fueled. Airplane is
operated in accordance with
AFM, Limitations , and
Abnormal Procedures .
An Inoperative Placard will
be placed on or below Yaw
Damp Switch and will be
noted on ADLS.
22-3
GULFSTREAM AEROSPACE CORPORATION PAGE NUMBER: 22-3
AIRCRAFT: GULFSTREAM AEROSPACE MODEL G-IV MMEL REVISION NO.: 5 MOP REV. NO.: 5
MAINTENANCE / OPERATIONAL / PLACARDING / PROCEDURES MANUAL MMEL DATE: 10/11/01 MOP DATE: 10/11/01
1. 2. NUMBER INSTALLED
SYSTEM & 5. MAINTENANCE 6. OPERATIONAL 7. PLACARDING
SEQUENCE 3. NUMBER REQ’D FOR DISPATCH PROCEDURES PROCEDURES PROCEDURES
　
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