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EXCEPTIONS
27. FLIGHT CONTROLS
1. Flap/Stabilizer C
Warning System
1 0 (O) May be inoperative provided
Flap/Stabilizer position indicator is
monitored to observe proper Flap/Stabilizer
position.
None required. Flight crew will ensure
Flap/Stabilizer Position
Indicator is operating
properly during flap /
stabilizer movement. AFM ,
Normal Procedures .
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
2. Rudder Limit C
Warning Light System
1 0 May be inoperative provided Single Rudder
Limit Warning Light System is operative.
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. Single Rudder Limit C
Warning Light System
1 0 May be inoperative provided Rudder Limit
Warning Light System is operative.
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.
4. Automatic Ground C
Spoiler System
1 0 (O) May be inoperative provided airplane is
operated in accordance with AFM
Limitations
None required. Flight crew will ensure
Ground Spoiler switch
remains "OFF" and airplane
is operated in accordance with
AFM Limitations .
An Inoperative Placard will
be placed next to Ground
Spoiler Arming Switch and
will be noted on ADLS.
27-2
GULFSTREAM AEROSPACE CORPORATION PAGE NUMBER: 27-2
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
27. FLIGHT CONTROLS
5. Electric Elevator C
Trim System
1 0 (O) May be inoperative provided:
a) Electric Pitch Trim remains OFF,
and
b) Airplane is operated accordance
with AFM Limitations.
None required. Flight crew will ensure
Electric Pitch Trim switch
remains "OFF" and airplane
is operated in accordance with
AFM Limitations ,
(Maximum Operating Limit
Speed).
An Inoperative Placard will
be placed next to Pitch Trim
Switch and will be noted on
ADLS.
28-1
GULFSTREAM AEROSPACE CORPORATION PAGE NUMBER: 28-1
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
28. FUEL
1. Fuel Tank C
Temperature
System
1 0 (O) May be inoperative provided:
a) Total Air Temperature is used as
an indication of fuel temperature,
and
b) Airplane is operated in
accordance with AFM
Limitations.
None required. Flight crew will ensure Total
Air Temperature (TAT) is
not less than -40°C for more
than one hour and airplane is
operated in accordance with
AFM, Limitations .
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
2. Fuel Quantity Indicating
Systems
1) EICAS or Standby C 1 0 (M) O) May be partially or completely
inoperative provided the associated Standby
Fuel Quantity Indicating System or EICAS
Fuel Quantity Indicating System is
operative.
Maintenance personnel will
ensure tanks are filled using
Standby Fuel Quantity
Indicating System or EICAS
Fuel Quantity Indicating
System.
Flight crew will ensure
associated Standby Fuel
Quantity Indicating System
or EICAS Fuel Quantity
Indicating System is
operative.
An Inoperative Placard will
be displayed in a prominent
position to be seen by flight
crew and will be noted on
ADLS.
C 1 0 (M) (O) Either Left or Right Fuel Quantity
Display may be inoperative provided:
a) Both tanks are completely filled
using overwing refueling,
b) Both fuel flow meters are
operative,
c) After takeoff, power is set by
matching fuel flow indications on
both engines, and
　
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