Revision:
1
Date: Nov 12, 2008
DEPARTMENT OF TRANSPORTATION
FEDERAL AVIATION ADMINISTRATION
WASHINGTON, D.C.
MASTER MINIMUM EQUIPMENT LIST
GULFSTREAM G150
APPROVED BY:
STEPHEN L. FORD, CHAIRMAN
FLIGHT OPERATIONS EVALUATION BOARD
Federal Aviation Administration
Flight Standards Division
Aircraft Evaluation Group, LGB-AEG
3960 Paramount Blvd, Suite 100
Lakewood, CA 90712-4137
Telephone: (562)-627-5279
FAX: (562)-627-5281
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT:
REVISION: 1
GULFSTREAM G150
DATE: 11/12/2008
TABLE OF CONTENTS
SYSTEM NO.
SYSTEM
-Table of Contents
-Log of Revisions
-Control Pages
-Highlights of Change
-Definitions
-Preamble
21
Air Conditioning
21
Air Conditioning
22
Auto Flight
23
Communications
23
Communications
24
Electrical Power
25
Equipment/Furnishings
25
Equipment/Furnishings
26
Fire Protection
27
Flight Controls
28
Fuel
29
Hydraulic Power
30
Ice and Rain Protection
31
Indicating/Recording Systems
32
Landing Gear
33
Lights
34
Navigation
34
Navigation
34
Navigation
35
Oxygen
38
Water / Waste
45
Central Maintenance Computer
46
Information Systems
49
Airborne Auxiliary Power
52
Doors
71
Powerplant
73
Engine Fuel & Control
74
Ignition
76
Engine Controls
77
Engine Indicating
78
Engine Exhaust
79
Engine Oil
80
Starting
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PAGE NO.
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II
III thru V
VI
VII thru XV
XVI thru XVII
21-1, 2, 3, 4, 5, 6,
21-7
22-1, 2, 3, 4, 5, 6
23-1, 2, 3, 4, 5, 6
23-7, 8
24-1, 2, 3
25-1, 2, 3, 4, 5, 6
25-7, 8, 9
26-1, 2
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28-1, 2, 3, 4, 5
29-1, 2, 3
30-1, 2, 3, 4,5
31-1, 2, 3
32-1, 2
33-1, 2, 3, 4
34-1, 2, 3, 4, 5, 6
34-7, 8, 9, 10, 11
34-12, 13, 14,15
35-1, 2
38-1, 2
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46-1, 2
49-1
52-1, 2
71-1
73-1
74-1
76-1
77-1
78-1
79-1
80-1
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT:
REVISION: 1
GULFSTREAM G150
DATE: 11/12/2008
Log of Revisions
Rev. No.
Date
Page Numbers
ORIGINAL
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Initials
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT:
REVISION: 1
GULFSTREAM G150
DATE: 11/12/2008
Control Page
System
Page No.
Cover Page
Table of Contents
I
Log of Revisions
II
Control Page
III
IV
V
Highlights of Change
VI
Definitions
VII
VIII
IX
X
XI
XII
XIII
XIV
XV
Preamble
XVI
XVII
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Current Date
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U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT:
REVISION: 1
GULFSTREAM G150
DATE: 11/12/2008
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U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT:
REVISION: 1
GULFSTREAM G150
DATE: 11/12/2008
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U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT:
REVISION: 1
GULFSTREAM G150
DATE: 11/12/2008
HIGHLIGHTS OF CHANGE
1
PAGE NO.
VI
This is Revision 1 to the Master Minimum Equipment list (MMEL). It is the
result of a public Flight Operations Evaluation Board (FOEB) meeting held
on April 23 - 24, 2008 to consider approximately 234 items proposed by
GAC for inclusion in the MMEL. The majority of those items were accepted
by the FOEB.
FAA Policy Letters 1-122 were also incorporated in this revision. For a
complete listing of FAA Policy Letters visit “www. opspecs.com”.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT:
REVISION: 14
GULFSTREAM G150
DATE: 08/26/2008
DEFINITIONS
PAGE NO:
VII
1. System Definitions.
System numbers are based on the Air Transport Association (ATA) Specification
Number 100 and items are numbered sequentially.
a. "Item" (Column 1) means the equipment, system, component, or function listed in the
"Item" column. Repair interval categories (A, B, C, and D) are listed on right side of
column 1. Repair intervals are described in definition 22.
b. "Number Installed" (Column 2) is the number (quantity) of items normally installed in
the aircraft. This number represents the aircraft configuration considered in developing
this MMEL. Should the number be a variable (e.g., passenger cabin items) a number is
not required.
c. "Number Required for Dispatch" (Column 3) is the minimum number (quantity) of
items required for operation provided the conditions specified in Column 4 are met.
NOTE: Where the MMEL shows a variable number required for dispatch, the MEL must
reflect the actual number required for dispatch or an alternate means of configuration
control approved by the Administrator.
d. "Remarks or Exceptions" (Column 4) in this column includes a statement either
prohibiting or permitting operation with a specific number of items inoperative, provisos
(conditions and limitations) for such operation, and appropriate notes.
e. A vertical bar (change bar) in the margin indicates a change, addition or deletion in
the adjacent text for the current revision of that page only. The change bar is dropped at
the next revision of that page.
2. "Airplane/Rotorcraft Flight Manual" (AFM/RFM) is the document required for type
certification and approved by the responsible FAA Aircraft Certification Office. The FAA
approved AFM/RFM for the specific aircraft is listed on the applicable Type Certificate
Data Sheet.
3. "As required by FAR" means that the listed item is subject to certain provisions
(restrictive or permissive) expressed in the Federal Aviation Regulations operating rules.
The number of items required by the FAR must be operative. When the listed item is not
required by FAR it may be inoperative for time specified by repair category. The term “14
CFR” may be substituted for “FAR” in MMELs or operator MELs.
4. Each inoperative item must be placarded to inform and remind the crewmembers and
maintenance personnel of the equipment condition.
U. S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT:
REVISION: 14
GULFSTREAM G150
DATE: 08/26/2008
DEFINITIONS
PAGE NO:
VIII
NOTE: To the extent practical, placards should be located adjacent to the control or
indicator for the item affected; however, unless otherwise specified, placard wording and
location will be determined by the operator.
5."-" symbol in Column 2 and/or Column 3 indicates a variable number (quantity) of the
item installed.
6. "Deleted" in the remarks column after a sequence item indicates that the item was
previously listed but is now required to be operative if installed in the aircraft.
7. As used in MMELs, "ER" refers to Extended Operations (ETOPS) of an airplane with
operational approval to conduct ETOPS in accordance with the applicable regulations.
8. "Federal Aviation Regulations" (FAR) means the applicable portions of the Federal
Aviation Act and Federal Aviation Regulations.
9. "Flight Day" means a 24 hour period (from midnight to midnight) either Universal
Coordinated Time (UCT) or local time, as established by the operator, during which at
least one flight is initiated for the affected aircraft.
10. "Icing Conditions" means an atmospheric environment that may cause ice to form on
the aircraft (structural) or in the engine(s) (induction).
11. Alphabetical symbol in Column 4 indicates a proviso (condition or limitation) that
must be complied with for operation with the listed item inoperative.
12. ”Inoperative" means a system and/or component malfunction to the extent that it
does not accomplish its intended purpose and/or is not consistently functioning normally
within its approved operating limit(s) or tolerance(s).
13. ”Notes:" in Column 4 provides additional information for crewmember or
maintenance consideration. Notes are used to identify applicable material which is
intended to assist with compliance, but do not relieve the operator of the responsibility
for compliance with all applicable requirements. Notes are not a part of the provisos.
14. Inoperative components of an inoperative system: Inoperative items which are
components of a system which is inoperative are usually considered components
directly associated with and having no other function than to support that system.
(Warning/caution systems associated with the inoperative system must be operative
unless relief is specifically authorized per the MMEL).
U. S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT:
REVISION: 14
GULFSTREAM G150
DATE: 08/26/2008
DEFINITIONS
PAGE NO:
IX
15."(M)" symbol indicates a requirement for a specific maintenance procedure which
must be accomplished prior to operation with the listed item inoperative. Normally these
procedures are accomplished by maintenance personnel; however, other personnel may
be qualified and authorized to perform certain functions. Procedures requiring
specialized knowledge or skill, or requiring the use of tools or test equipment should be
accomplished by maintenance personnel. The satisfactory accomplishment of all
maintenance procedures, regardless of who performs them, is the responsibility of the
operator. Appropriate procedures are required to be published as part of the operator's
manual or MEL.
16."(O)" symbol indicates a requirement for a specific operations procedure which must
be accomplished in planning for and/or operating with the listed item inoperative.
Normally these procedures are accomplished by the flight crew; however, other
personnel may be qualified and authorized to perform certain functions. The satisfactory
accomplishment of all procedures, regardless of who performs them, is the responsibility
of the operator. Appropriate procedures are required to be published as a part of the
operator's manual or MEL.
NOTE: The (M) and (O) symbols are required in the operator's MEL unless otherwise
authorized by the Administrator.
17. "Deactivated" and "Secured" means that the specified component must be put into
an acceptable condition for safe flight. An acceptable method of securing or deactivating
will be established by the operator.
18. "Visual Flight Rules" (VFR) is as defined in FAR Part 91. This precludes a pilot from
filing an Instrument Flight Rules (IFR) flight plan.
19. "Visual Meteorological Conditions" (VMC) means the atmospheric environment is
such that would allow a flight to proceed under the visual flight rules applicable to the
flight. This does not preclude operating under Instrument Flight Rules.
20. "Visible Moisture" means an atmospheric environment containing water in any form
that can be seen in natural or artificial light; for example, clouds, fog, rain, sleet, hail, or
snow.
21. "Passenger Convenience Items" means those items related to passenger
convenience, comfort or entertainment such as, but not limited to, galley equipment,
movie equipment, ash trays, stereo equipment, overhead reading lamps, etc.
U. S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT:
REVISION: 14
GULFSTREAM G150
DATE: 08/26/2008
DEFINITIONS
PAGE NO:
X
22. Repair Intervals: All users of an MEL approved under FAR 121, 125, 129 and 135
must effect repairs of inoperative systems or components, deferred in accordance with
the MEL, at or prior to the repair times established by the following letter designators:
Category A. Items in this category shall be repaired within the time interval specified in
the remarks column of the operator's approved MEL. For time intervals specified in
"flight days," the day the malfunction was recorded in the aircraft maintenance
record/logbook is excluded. For all other time intervals (flights, flight legs, cycles, hours,
etc), repair tracking begins at the point when the malfunction is deferred in accordance
with the operator's approved MEL.
Category B. Items in this category shall be repaired within three (3) consecutive calendar
days (72 hours), excluding the day the malfunction was recorded in the aircraft
maintenance record/logbook. For example, if it were recorded at 10 a.m. on January
26th, the three day interval would begin at midnight the 26th and end at midnight the
29th.
Category C. Items in this category shall be repaired within ten (10) consecutive calendar
days (240 hours), excluding the day the malfunction was recorded in the aircraft
maintenance record/logbook. For example, if it were recorded at 10 a.m. on January
26th, the 10 day interval would begin at midnight the 26th and end at midnight February
5th.
Category D. Items in this category shall be repaired within one hundred and twenty (120)
consecutive calendar days (2880 hours), excluding the day the malfunction was
recorded in the aircraft maintenance log and/or record. The letter designators are
inserted adjacent to Column 2.
An operator who has the authorization to use an MEL also has the authority to approve
extensions to the maximum repair interval for category B and C items provided the
responsible Flight Standards District Office (FSDO) is notified within 24 hours of the MEL
extension. The operator is not authorized to extend A and D items in the MEL. Misuse
of the MEL extension authority may result in the operators OpSpecs/Mspecs being
amended by removing the authority for the operator to use the MEL extension authority
and/or use an MEL.
23. Electronic fault alerting system – General
New generation aircraft display system fault indications to the flight crew by use of
computerized display systems. Each aircraft manufacturer has incorporated individual
design philosophies in determining the data that would be represented. The following are
customized definitions (specific to each manufacturer) to help determine the level of
messages affecting the aircraft's dispatch status .When preparing the MEL document,
operators are to select the proper Definition No. 23 for their aircraft, if appropriate.
U. S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT:
REVISION: 14
GULFSTREAM G150
DATE: 08/26/2008
DEFINITIONS
a.
PAGE:
XI
BOEING (B-747-400, 757, 767, 777, 787)
Boeing airplanes equipped with Engine Indicating and Crew Alerting Systems (EICAS),
provide different priority levels of system messages (WARNING, CAUTION, ADVISORY,
STATUS and MAINTENANCE).Any messages that affects airplane dispatch status will
be displayed at a STATUS message level or higher. The absence of an EICAS STATUS
or higher level (WARNING, CAUTION, ADVISORY) indicates that the
system/component is operating within its approved operating limits or tolerances.
System conditions that result only in a maintenance level message, i.e. no correlation
with a higher level EICAS message, do not affect dispatch and do not require action
other than as addressed within an operator’s standard maintenance program.
b.
BOEING (B-717, MD-10, MD-11)
These aircraft are equipped with an alerting function which is a subsystem within the
Electronic Instrument System (EIS). The alerting function provides various levels of
system condition alerts (WARNING, CAUTION, ADVISORY, MAINTENANCE and
STATUS). Alerts that affect aircraft dispatch will include WARNING, CAUTION,
STATUS or MAINTENANCE level. MAINTENANCE alerts are displayed on the status
page of the EIS display panel under the maintenance heading. A MAINTENANCE alert
on the EIS indicates the presence of a system fault which can be identified by the
Central Fault Display System (CFDS) interrogation. The systems are
designed to be fault tolerant, however, for any MAINTENANCE alert, the MEL must be
verified for dispatch purposes.
c.
AIRBUS (A-300-600, A-310, A-318/319/320/321, A-330, A-340)
Airbus aircraft equipped with Electronic Centralized Aircraft Monitoring (ECAM) provide
different levels of system condition messages (WARNING, CAUTION, STATUS, and
ADVISORY). A-318/319/320/321, A-330, and A-340 also provide MAINTENANCE status
messages. Any message that effects airplane dispatchability will normally be at the
WARNING, CAUTION or STATUS level. MAINTENANCE messages (A318/319/320/321, A-330, and A-340 only) are also indicated on ECAM Status Page
below the white Maintenance label. A MAINTENANCE status (Class II) message on
ECAM indicates the presence of a system fault which can be identified by CFDS (A318/319/320/321) or CMS (A-330/A-340) interrogation. The systems are designed to be
fault tolerant. For A-318/319/320/321, MAINTENENACE status (Class II) do not affect
dispatch but are listed in the MMEL. Dispatch is allowed without specific conditions
except for:
BLUE RSVR MAINTENANCE status: If applicable, and
AIR BLEED MAINTENANCE status: As applicable.
For the A-330 and A-340, MAINTENANCE status messages do not affect dispatch.
U. S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT:
REVISION: 14
GULFSTREAM G150
DATE: 08/26/2008
DEFINITIONS
d.
PAGE:
XII
FOKKER (FK-100)
Fokker aircraft are equipped with Multi Function Display System (MFDS) which provides
electronic message referring to the different priority levels of system information
(WARNING (red), CAUTION (amber), AWARENESS (cyan) AND STATUS (white). Any
messages that affects aircraft dispatch will be at the WARNING, CAUTION or
AWARENESS level. In these cases the MEL must be verified for dispatch capability and
maintenance may be required. System conditions that only require maintenance are not
presented on the flight deck. These maintenance indications/messages may be
presented on the Maintenance & Test Panel (MAP) or the Centralized Fault Display Unit
(CFDU) and by dedicated Built In Test Evaluation (BITE) of systems.
e.
CANADAIR (CL-65, CL-604)
Canadair aircraft equipped with Engine Indication and Crew Alerting Systems (EICAS)
provide four classes of messages (WARNING, CAUTION, ADVISORY, and STATUS).
Any message that affects aircraft dispatch will be at the WARNING, CAUTION, or
STATUS level. System conditions that only require maintenance are not visible to the
flight crew. These maintenance indications/messages are only activated by maintenance
personnel using the Maintenance Diagnostics Computer.
f.
EMBRAER (EMB-135/145, ERJ-170 Series)
The EMB-135/145 and ERJ-170/190 are equipped with an Engine Indicating and Crew
Alerting System (EICAS) that provides three different message levels: WARNING,
CAUTION, and ADVISORY. The ERJ-170/190 Series add STATUS messages. Failures
that effect dispatchability are presented to the flight crew at one of these levels. Other
failures may be presented only to the maintenance personnel on the Multi Function
Display (MFD) maintenance pages or through the download of the Central Maintenance
Computer (CMC). System conditions that result only in a maintenance level message,
i.e. no correlation with a higher level EICAS message, do not affect dispatch and do not
require action other than as addressed within an operator's standard maintenance
program.
g.
GULFSTREAM (G-IV, G-V, GV-SP, GIV-X, G-150 and G200)
Gulfstream airplanes equipped with EICAS provide different priority levels of system
messages: WARNING (red), CAUTION (amber), ADVISORY, STATUS and
MAINTENANCE (cyan or blue). Any WARNING or CAUTION message affects airplane
dispatch status and requires that the Airplane Flight Manual or the MEL be used to
determine dispatch capability. STATUS messages which indicate a system failure
U. S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT:
REVISION: 14
GULFSTREAM G150
DATE: 08/26/2008
DEFINITIONS
PAGE:
XIII
(e.g., FMS 1 fail) require that the Airplane Flight Manual or the MEL be used to
determine dispatch capability. MAINTENANCE messages do not affect airplane
dispatch status. They indicate the presence of a system fault which can be identified by
Maintenance Data Acquisition Unit (MDAU on the G-V) interrogation, Central
Maintenance Computer (CMC on the GV-SP/GIV-X) interrogation or by reference to the
Airplane Flight Manual.
Gulfstream mid-cabin airplanes (G-150, G-200) equipped with EICAS provide different
priority levels of system messages: WARNING (red), CAUTION (amber), ADVISORY
(green), and STATUS (white). The Airplane Flight Manual prohibits take off with any
WARNING message displayed. CAUTION, ADVISORY and STATUS messages may
affect airplane dispatch status and requires the Airplane Flight Manual or the MEL be
used to determine dispatch capability. The airplane may dispatch with CAUTION,
ADVISORY and STATUS messages that indicate proper system operation and are not
illuminated due to a system failure (i.e. FUEL STBY PUMP ON when the pump is
selected ON, GND A/B OUT with LAND selected on the ground, or APU GEN OFF with
the switch OFF). MAINTENANCE and MAINTENANCE DATA STATUS messages do
not affect airplane dispatch status. They indicate the presence of a system fault which
can be retrieved from the Maintenance Diagnostics Computer. In all cases, the Airplane
Flight Manual must be referenced and procedures compiled with for the displayed
message prior to applying MEL dispatch relief.
h.
De-HAVILLAND (DASH 8 SERIES 400)
Series 400 aircraft are equipped with a Caution/Warning Panel that annunciates all
cautions and warnings. Advisory messages are displayed by the Electronic Indication
System (EIS) or individual advisory lights supplied in the cockpit. "Class 1 failures" are
failures that prevent continued operation of a specific Line Replacement Unit or channel
and are annunciated via advisory messages: caution, warning or advisory lights in the
flight compartment. Dispatch with such posted failures are to be in accordance with the
MMEL. "Class 2 failures" are failures which do not prevent continued system function.
These faults will not be annunciated to the flight crew and the absence of the higher
level alert (warning, caution, advisory) indicates that the system/component is operating
within its approved operating limits or tolerances. Such faults would be evident during
maintenance interrogation performed during maintenance activities. Class 2 faults do not
affect dispatch and will be listed in the Fault Isolation Manual (FIM). Class 2 faults will be
left to the discretion of the operators when these faults are to be rectified.
U. S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT:
REVISION: 14
GULFSTREAM G150
DATE: 08/26/2008
DEFINITIONS
PAGE:
XIV
24. "Administrative control item" means an item listed by the operator in the MEL for
tracking and informational purposes. It may be added to an operator's MEL by approval
of the Principal Operations Inspector provided no relief is granted, or provided conditions
and limitations are contained in an approved document (i.e. Structural Repair Manual,
airworthiness directive, etc.). If relief other than that granted by an approved document is
sought for an administrative control item, a request must be submitted to the
Administrator. If the request results in review and approval by the FOEB, the item
becomes an MMEL item rather than an administrative control item.
25."***" symbol in Column 1 indicates an item which is not required by regulation but
which may have been installed on some models of aircraft covered by this MMEL. This
item may be included on the operator's MEL after the approving office has determined
that the item has been installed on one or more of the operator's aircraft. The symbol,
however, shall not be carried forward into the operator's MEL. It should be noted that
neither this policy nor the use of this symbol provide authority to install or remove an
item from an aircraft.
26. "Excess Items" means those items that have been installed that are redundant to the
requirements of the FARs.
27. "Day of Discovery" is the calendar day an equipment/instrument malfunction was
recorded in the aircraft maintenance log and or record. This day is excluded from the
calendar days or flight days specified in the MMEL for the repair of an inoperative item of
equipment. This provision is applicable to all MMEL items, i.e., categories "A, B, C, and
D."
28. “Considered Inoperative”, as used in the provisos means that item must be treated
for dispatch, taxi and flight purposes as though it were inoperative. The item shall not be
used or operated until the original deferred item is repaired. Additional actions include:
documenting the item on the dispatch release (if applicable), placarding, and complying
with all remarks, exceptions, and related MMEL provisions, including any (M) and (O)
procedures and observing the repair category.
29. “ Is not used” in the provisos, remarks or exceptions for an MMEL item may specify
that another item relieved in the MMEL “is not used.” In such cases, crewmembers
should not activate, actuate, or otherwise utilize that component or system under normal
operations. It is not necessary for the operators to accomplish the (M) procedures
associated with the item. However, operational requirements must be complied with,
and an additional placard must be affixed, to the extent practical, adjacent to the control
or indicator for the item that is not used to inform crewmembers that a component or
system is not to be used under normal operations.
U. S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT:
REVISION: 14
GULFSTREAM G150
DATE: 08/26/2008
DEFINITIONS
PAGE:
XV
30. Nonessential equipment and furnishings (NEF) are those items installed on the
aircraft as part of the original type certification, supplemental type certificate, or other
form of alteration that have no effect on the safe operation of flight and would not be
required by the applicable certification rules or operational rules. They are those items
that if inoperative, damaged or missing have no effect on the aircraft’s ability to be
operated safely under all operational conditions. These nonessential items may be
installed in areas including, but not limited to, the passenger compartment, flight deck
area, service areas, cargo areas, crew rest areas, lavatories, and galley areas. NEF
items are not items already identified in the MEL or CDL of the applicable aircraft. They
do not include items that are functionally required to meet the certification rule or for
compliance with any operational rule. Operator’s NEF process shall not provide for
deferral of items within serviceable limits identified in the manufacture’s maintenance
manual or operator’s approved maintenance program such as wear limits, fuel/hydraulic
leak rates, oil consumption, etc. Cosmetic items that are fully serviceable but worn or
soiled may be deferred under an operator’s NEF process.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT:
REVISION: 2
GULFSTREAM G150
DATE: 06/14/1989
PREAMBLE
(06/14/1989)
PAGE NO:
XVI
The following is applicable for authorized certificate holders operating under Federal
Aviation Regulations (FAR) Parts 121, 125, 129, 135: The FAR require that all
equipment installed on an aircraft in compliance with the Airworthiness Standards and
the Operating Rules must be operative. However, the Rules also permit the publication
of a Minimum Equipment List (MEL) where compliance with certain equipment
requirements is not necessary in the interests of safety under all operating conditions.
Experience has shown that with the various levels of redundancy designed into aircraft,
operation of every system or installed component may not be necessary when the
remaining operative equipment can provide an acceptable level of safety. A Master
Minimum Equipment List (MMEL) is developed by the FAA, with participation by the
aviation industry, to improve aircraft utilization and thereby provide more convenient and
economic air transportation for the public. The FAA approved MMEL includes those
items of equipment related to airworthiness and operating regulations and other items of
equipment which the Administrator finds may be inoperative and yet maintain an
acceptable level of safety by appropriate conditions and limitations; it does not contain
obviously required items such as wings, flaps, and rudders. The MMEL is the basis for
development of individual operator MELs which take into consideration the operator's
particular aircraft equipment configuration and operational conditions. Operator MELs,
for administrative control, may include items not contained in the MMEL; however, relief
for administrative control items must be approved by the Administrator. An operator's
MEL may differ in format from the MMEL, but cannot be less restrictive than the MMEL.
The individual operator's MEL, when approved and authorized, permits operation of the
aircraft with inoperative equipment.
Equipment not required by the operation being conducted and equipment in excess of
FAR requirements are included in the MEL with appropriate conditions and limitations.
The MEL must not deviate from the Aircraft Flight Manual Limitations, Emergency
Procedures or with Airworthiness Directives. It is important to remember that all
equipment related to the airworthiness and the operating regulations of the aircraft not
listed on the MMEL must be operative.
Suitable conditions and limitations in the form of placards, maintenance procedures,
crew operating procedures and other restrictions as necessary are specified in the MEL
to ensure that an acceptable level of safety is maintained.
The MEL is intended to permit operation with inoperative items of equipment for a period
of time until repairs can be accomplished. It is important that repairs be accomplished at
the earliest opportunity. In order to maintain an acceptable level of safety and reliability
the MMEL establishes limitations on the duration of and conditions for operation with
inoperative equipment.
U. S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT:
REVISION: 2
GULFSTREAM G150
DATE: 06/14/1989
PREAMBLE
(06/14/1989)
PAGE NO:
XVII
The MEL provides for release of the aircraft for flight with inoperative equipment. When
an item of equipment is discovered to be inoperative, it is reported by making an entry in
the Aircraft Maintenance Record/Logbook as prescribed by FAR. The item is then either
repaired or may be deferred per the MEL or other approved means acceptable to the
Administrator prior to further operation. MEL conditions and limitations, do not relieve the
operator from determining that the aircraft is in condition for safe operation with items of
equipment inoperative.
When these requirements are met, an Airworthiness Release, Aircraft Maintenance
Record/Logbook entry, or other approved documentation is issued as prescribed by
FAR. Such documentation is required prior to operation with any item of equipment
inoperative.
Operators are responsible for exercising the necessary operational control to ensure that
an acceptable level of safety is maintained. When operating with multiple inoperative
items, the interrelationships between those items and the effect on aircraft operation and
crew workload will be considered.
Operators are to establish a controlled and sound repair program including the parts,
personnel, facilities, procedures, and schedules to ensure timely repair.
WHEN USING THE MEL, COMPLIANCE WITH THE STATED INTENT OF THE
PREAMBLE, DEFINITIONS, AND THE CONDITIONS AND LIMITATIONS SPECIFIED
IN THE MEL IS REQUIRED
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT:
REVISION NO: 1
PAGE NO:
GULFSTREAM G150
DATE: 11/12/2008
21-1
1. SYSTEM,
REPAIR CATEGORY
SEQUENCE NUMBERS &
2. NUMBER INSTALLED
ITEM
3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
21 AIR CONDITIONING
1. Bleed Switching Valves
C
C
2
2
1
0
(M) One may be inoperative provided
airplane is operated at or below FL250.
|
(M) May be inoperative provided:
a) Affected valves are CLOSED, and
b) Environment Control System
|
(ECS) Selector is in RAM.
|
NOTE: Cabin pressurization and
Temperature control are not available
with Environmental Control System (ECS)
Selector in RAM.
|
|
|
|
|
|
|
|
2. HP Bleed Air Duct Blow
Out Discs
C
2
0
(M) One or both disks may be missing
provided no airflow from respective
port(s) is verified with respective
engine(s) running before each takeoff.
3. Ram Air Check Valve
C
1
0
(O) May be inoperative in OPEN position |
provided airplane is operated
|
unpressurized.
|
4. Automatic Temperature
Control Cabin
C
1
0
May be inoperative provided Manual
Temperature Control Cabin is operative.
C
1
0
(O) May be inoperative provided airplane |
is operated unpressurized.
|
NOTE: When operating without either
automatic or manual temperature control,
it is possible to heat cabin/cockpit using
emergency bleed air from right engine by
moving ECS Selector to EMERG (reduce
right engine thrust to avoid display of
DUCT TEMP HI warning message).
|
|
|
|
|
|
|
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT:
REVISION NO: 1
PAGE NO:
GULFSTREAM G150
DATE: 11/12/2008
21-2
1. SYSTEM,
REPAIR CATEGORY
SEQUENCE NUMBERS &
2. NUMBER INSTALLED
ITEM
3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
21 AIR CONDITIONING
5. Manual Temperature
Control Cabin
6. Air Conditioning Unit
C
1
0
May be inoperative provided Automatic
Temperature Control Cabin is operative.
C
1
0
(O) May be inoperative provided airplane |
is operated unpressurized.
|
C
1
0
NOTE: When operating without either
automatic or manual temperature control,
it is possible to heat cabin/cockpit using
emergency bleed air from right engine by
moving ECS Selector to EMERG (reduce
right engine thrust to avoid display of
DUCT TEMP HI warning message).
|
|
|
|
|
|
|
May be inoperative provided airplane is
operated with Environment Control
System (ECS) Selector in RAM.
|
|
NOTE: Cabin pressurization and
Temperature control are not available
with Environmental Control System (ECS)
Selector in RAM.
|
|
|
|
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT:
REVISION NO: 1
PAGE NO:
GULFSTREAM G150
DATE: 11/12/2008
21-3
1. SYSTEM,
REPAIR CATEGORY
SEQUENCE NUMBERS &
2. NUMBER INSTALLED
ITEM
3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
21 AIR CONDITIONING
7. Cabin Pressurization
Control System
1) Automatic Mode
2) Manual Mode
B
1
0
May be inoperative provided:
a) Manual Mode is operative, and
b) CABIN DOOR UNLOCK message |
is operative.
B
1
0
May be inoperative provided airplane is
operated with Environment Control
System (ECS) Selector in RAM.
|
|
NOTE: Cabin pressurization and
Temperature control are not available
with Environmental Control System (ECS)
Selector in RAM.
|
|
|
|
B
1
0
May be inoperative provided Automatic
Mode is operative.
B
1
0
May be inoperative provided airplane is
operated with Environment Control
System (ECS) Selector in RAM.
|
|
NOTE: Cabin pressurization and
Temperature control are not available
with Environmental Control System (ECS)
Selector in RAM.
|
|
|
|
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT:
REVISION NO: 1
PAGE NO:
GULFSTREAM G150
DATE: 11/12/2008
21-4
1. SYSTEM,
REPAIR CATEGORY
SEQUENCE NUMBERS &
2. NUMBER INSTALLED
ITEM
3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
21 AIR CONDITIONING
8. Valves
|
1) Outflow Valve
C
1
0
(M) May be inoperative provided:
a) Extended overwater operations
are not conducted,
b) Outflow valve is secured OPEN,
and
c) Airplane is operated
unpressurized.
|
|
|
|
|
|
|
2) Safety Valve
C
1
0
(O) May be inoperative provided airplane |
is operated unpressurized.
|
9. Cabin Altitude Rate of
Climb Indicator
C
1
0
May be inoperative provided:
a) Cabin Altitude Indicator is
operative,
b) Automatic and Manual Mode of
Cabin Pressurization Control
System (CPCS) is operative.
|
|
|
|
|
C
1
0
May be inoperative provided:
a) Cabin Differential Pressure
Indication is operative,
b) A chart to convert cabin differential
pressure to cabin altitude is
provided to crew, and
|
c) Automatic and Manual Mode of
Cabin Pressurization Control
|
System (CPCS) is operative.
C
1
0
(O) May be inoperative provided airplane |
is operated unpressurized.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT:
REVISION NO: 1
PAGE NO:
GULFSTREAM G150
DATE: 11/12/2008
21-5
1. SYSTEM,
REPAIR CATEGORY
SEQUENCE NUMBERS &
2. NUMBER INSTALLED
ITEM
3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
21 AIR CONDITIONING
10. Cabin Altitude Indicator
C
1
0
May be inoperative provided:
a) Cabin Differential Pressure
Indicator is operative,
b) A chart to convert cabin differential
pressure to cabin altitude is
provided to crew, and
|
c) Cabin Altitude is monitored during
flight by crewmember.
C
1
0
(O) May be inoperative provided airplane |
is operated unpressurized.
C
1
0
May be inoperative provided:
a) Cabin Altitude Indicator is
operative,
b) A chart to convert cabin altitude to
cabin differential pressure is
provided to crew, and
c) Cabin Altitude is monitored during
flight by crewmembers.
C
1
0
(O) May be inoperative provided airplane |
is operated unpressurized.
12. Nose Cooling Fans
C
2
1
One may be inoperative provided AFM
procedures are followed for each flight
13. Bleed Pressure/
Temperature HI Warning
System
C
1
0
May be inoperative provided airplane is
operated with Environment Control
System (ECS) Selector in RAM.
|
|
|
NOTE: Cabin pressurization and
Temperature control are not available
with Environmental Control System (ECS)
Selector in RAM.
|
|
|
|
11. Cabin Differential
Pressure Indicator
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT:
REVISION NO: 1
PAGE NO:
GULFSTREAM G150
DATE: 11/12/2008
21-6
1. SYSTEM,
REPAIR CATEGORY
SEQUENCE NUMBERS &
2. NUMBER INSTALLED
ITEM
3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
21 AIR CONDITIONING
14. Duct Temp HI Warning
System
C
1
0
15. Cockpit Duct Temp HI
Warning System
May be inoperative provided airplane is
operated with Environment Control
System (ECS) Selector in RAM.
|
|
|
NOTE: Cabin pressurization and
Temperature control are not available
with Environmental Control System (ECS)
Selector in RAM.
|
|
|
|
Deleted in Revision 1.
|
16. Overhead Airflow Vents
(Wemacs/Gaspers)
D
-
-
|
|
17. Cabin Altitude High
Warning System
C
1
0
(O) May be inoperative provided airplane |
is operated unpressurized.
|
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT:
REVISION NO: 1
PAGE NO:
GULFSTREAM G150
DATE: 11/12/2008
21-7
1. SYSTEM,
REPAIR CATEGORY
SEQUENCE NUMBERS &
2. NUMBER INSTALLED
ITEM
3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
21 AIR CONDITIONING
18. Cabin Pressurization
System
C
1
0
May be inoperative provided airplane is
operated unpressurized.
19. Cabin Temperature
Indicator
C
1
0
May be inoperative provided Automatic or |
Manual Temperature Control System is
|
operative.
|
20. Windshield Defog
System
C
1
0
May be inoperative provided windshield
heating system is operative.
21. APU Airflow HI Flow
Pushbutton
D
1
0
|
|
22. Cabin Temperature
Remote Controllers
D
-
-
|
|
23. Emergency
Pressurization System
C
1
0
(O) May be inoperative provided airplane |
is operated unpressurized.
|
24. Ditch Pushbutton
C
1
0
May be inoperative provided outflow valve |
can be controlled by Manual Cabin
|
Pressure operation.
|
25. Dump Pushbutton
C
1
0
May be inoperative provided outflow valve |
can be controlled by Manual Cabin
|
Pressure operation.
|
|
|
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT:
REVISION NO: 1
PAGE NO:
GULFSTREAM G150
DATE: 11/12/2008
22-1
1. SYSTEM,
REPAIR CATEGORY
SEQUENCE NUMBERS &
2. NUMBER INSTALLED
ITEM
3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
22 AUTO FLIGHT
1. Flight Director Systems
C
2
0
May be inoperative provided enroute or
approach minimums do not require its
use.
2. Autopilot System
B
1
0
(M) May be inoperative except where
enroute operations, RVSM operations, or
approach minimums require its use
provided AFM Limitations are observed.
NOTE: Airplane must be operated at or
below FL310 when both autopilot and
yaw damper are inoperative.
|
|
|
|
|
|
|
|
|
3. Yaw Damper System
C
1
0
May be inoperative provided:
a) Autopilot and Yaw Damper are
disengaged by placing YD/AP
DISC bar in DOWN position, and
b) Airplane is operated at or below
FL310.
4. MACH Trim
C
1
0
May be inoperative provided airplane is
operated in accordance with AFM
Limitations.
5. Control Wheel Autopilot
Disconnect Buttons
|
|
NOTE: Airplane must be operated at or
below 0.78 Mach with autopilot
disengaged and Mach Trim inoperative.
|
|
|
C
2
1
One may be inoperative provided:
a) Autopilot is not used below 1500
feet AGL, and
b) Approach minimums do not
require use of autopilot.
|
|
|
|
|
B
2
0
May be inoperative provided autopilot is
not used.
|
|
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT:
REVISION NO: 1
PAGE NO:
GULFSTREAM G150
DATE: 11/12/2008
22-2
1. SYSTEM,
REPAIR CATEGORY
SEQUENCE NUMBERS &
2. NUMBER INSTALLED
ITEM
3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
22 AUTO FLIGHT
6. Takeoff/Go-Around
(TOGA) Buttons
7. Flight Control Computers
(FCC)
C
2
1
May be inoperative provided airplane is
piloted from side with operative button
when autopilot is used for coupled
approaches.
|
|
|
|
C
2
0
(O) May be inoperative provided autopilot
is not utilized for coupled approaches and
alternate procedures are established and
used.
|
|
|
|
NOTE: Flight Director Takeoff and GoAround Guidance are not available with
both TOGA buttons inoperative.
|
|
|
One or both may be inoperative provided:
a) Automatic Cabin Pressurization
System is operative,
b) Contingency planned flight time
with one engine inoperative does
not exceed one hour at cruise
from a suitable airport,
c) Landing weather minimums are
not dependent upon its use,
d) Airplane is operated at or below
FL280,
e) Airplane is operated in accordance
with AFM Limitations for Autopilot,
Mach Trim and Yaw Damper, and
f) Repairs are made within one (1)
flight day.
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
NOTE: Loss of a single FCC results in
loss of mach trim compensation,
automatic stabilizer trim, yaw damper,
autopilot and flight director functions.
|
|
|
|
A
2
0
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT:
REVISION NO: 1
PAGE NO:
GULFSTREAM G150
DATE: 11/12/2008
22-3
1. SYSTEM,
REPAIR CATEGORY
SEQUENCE NUMBERS &
2. NUMBER INSTALLED
ITEM
3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
22 AUTO FLIGHT
8. Pitch Synchronization
Pushbutton
C
2
0
9. FMS V-Speed
Calculation and Upload
System
C
1
0
|
|
May be inoperative provided V-speeds
are manually input and crosschecked
between each pilot station.
10. Autopilot Coupler
1) Left Selection
2) Right Selection
(continued)
|
|
|
|
C
C
1
1
0
0
May be inoperative provided:
a) Contingency planned flight time
with one engine inoperative does
not exceed one hour from a
suitable airport, and
b) All autopilot functions are
operative.
|
|
|
|
|
|
|
NOTE: If autopilot will not engage
consider FCC inoperative.
|
|
May be inoperative provided:
a) Contingency planned flight time
with one engine inoperative does
not exceed one hour from a
suitable airport, and
b) All autopilot functions are
operative.
|
|
|
|
|
|
|
NOTE: If autopilot will not engage
consider FCC inoperative.
|
|
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT:
REVISION NO: 1
PAGE NO:
GULFSTREAM G150
DATE: 11/12/2008
22-4
1. SYSTEM,
REPAIR CATEGORY
SEQUENCE NUMBERS &
2. NUMBER INSTALLED
ITEM
3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
22 AUTO FLIGHT
10. Autopilot Coupler
(continued)
3) Left and Right Selections
|
A
2
0
Both may be inoperative provided:
a) Automatic Cabin Pressurization
System is operative,
b) Contingency planned flight time
with one engine inoperative does
not exceed one hour at cruise
from a suitable airport,
c) Landing weather minimums are
not dependent upon its use,
d) Airplane is operated at or below
FL280,
e) Airplane is operated in accordance
with AFM Limitations for Autopilot,
Mach Trim and Yaw Damper, and
f) Repairs are made within one (1)
flight day.
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
NOTE: Expect loss of mach trim
compensation, automatic stabilizer trim,
yaw damper, autopilot, and flight director
functions.
|
|
|
|
11. Flight Control Panel,
Vertical Guidance Modes
|
|
1) Vertical Navigation
(VNAV) Mode Selector
Switch
C
1
0
May be inoperative provided vertical
navigation mode is considered
inoperative and not used during autopilot
operations.
2) Vertical Speed (VS)
Mode Selector Switch
C
1
0
May be inoperative provided vertical
|
speed mode is considered inoperative
|
and not used during autopilot operations. |
(continued)
|
|
|
|
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT:
REVISION NO: 1
PAGE NO:
GULFSTREAM G150
DATE: 11/12/2008
22-5
1. SYSTEM,
REPAIR CATEGORY
SEQUENCE NUMBERS &
2. NUMBER INSTALLED
ITEM
3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
22 AUTO FLIGHT
11. Flight Control Panel,
Vertical Guidance Modes
(continued)
|
|
|
3) Flight Level Change
(FLC) Mode Selector
Switch
C
1
0
May be inoperative provided flight level
|
change mode is considered inoperative
|
and not used during autopilot operations. |
4) Pitch Mode (PIT)
C
1
0
May be inoperative provided pitch mode
is considered inoperative and not used
during autopilot operations.
12. Flight Control Panel,
Lateral Guidance Modes
|
|
|
|
|
1) ½ BANK Mode Selector
Switch
C
1
0
May be inoperative provided autopilot
operations do not require ½ bank
selection.
|
|
|
2) Navigation (NAV) Mode
Selector Switch
C
1
0
May be inoperative provided NAV mode
autopilot operations are not required.
|
|
3) Back Course (BC) Mode
Selector Switch
C
1
0
May be inoperative provided Back Course |
operations are not required.
|
4) Approach (APPR) Mode
Selector Switch
C
1
0
May be inoperative provided Approach
Mode Operations are not required.
|
|
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT:
REVISION NO: 1
PAGE NO:
GULFSTREAM G150
DATE: 11/12/2008
22-6
1. SYSTEM,
REPAIR CATEGORY
SEQUENCE NUMBERS &
2. NUMBER INSTALLED
ITEM
3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
22 AUTO FLIGHT
13. Auto Throttle System
***
C
-
0
|
1) Auto Throttle
Engage/Disengage
Switches (on back of
Thrust Lever Knobs)
C
2
1
|
|
|
|
C
2
0
C
2
1
C
2
0
2) Auto Throttle Quick
Disconnect Switches (on
front of Thrust Lever
Knobs)
Both may be inoperative provided Auto
Throttle is not utilized.
|
|
|
|
|
|
Both may be inoperative provided Auto
Throttle is not utilized.
|
|
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT:
REVISION NO: 1
PAGE NO:
GULFSTREAM G150
DATE: 11/12/2008
23-1
1. SYSTEM,
REPAIR CATEGORY
SEQUENCE NUMBERS &
2. NUMBER INSTALLED
ITEM
3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
23 COMMUNICATIONS
1. Communication Systems
(UHF, VHF)
D
-
-
Any in excess of those required by 14
CFR may be inoperative provided it is not
powered by Battery Bus and is not
required for emergency procedures.
|
|
|
|
B
1
0
(O) May be inoperative provided
alternate, normal and emergency
procedures and/or operating restrictions
are established and used.
|
|
|
|
NOTE: Any station function(s) that is
operative may be used.
|
|
2. Passenger Address (PA)
System
1) Passenger Configuration
C
1
0
(O) May be inoperative provided:
a) PA not required by 14 CFR, and |
b) Alternate, normal and emergency
procedures and/or operating
restrictions are established and
used.
NOTE: Any station function(s) that is
operative may be used.
a) Lavatory Speakers
(continued)
C
1
0
(O) May be inoperative provided alternate |
procedures are established and used.
|
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT:
REVISION NO: 1
PAGE NO:
GULFSTREAM G150
DATE: 11/12/2008
23-2
1. SYSTEM,
REPAIR CATEGORY
SEQUENCE NUMBERS &
2. NUMBER INSTALLED
ITEM
3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
23. COMMUNICATIONS
2. Passenger Address (PA)
System (continued)
2) Cargo Configuration
C
1
0
May be inoperative provided alternate,
normal and emergency procedures,
and/or operating restrictions are
established and used.
D
1
0
May be inoperative provided procedures
do not require its use.
C
1
0
(O) May be inoperative provided alternate |
procedures are established and used.
|
D
1
0
May be inoperative provided procedures
do not require its use.
3. Cockpit Speakers
C
2
0
May be inoperative provided affected
|
crewmember(s) has an operative headset |
available.
|
4. Hand Held Microphones
C
-
0
One or more may be inoperative provided
affected cockpit crewmember:
a) Uses a boom microphone,
b) Has an operative Radio Push-toTalk Switch.
|
|
|
|
|
NOTE: Additional Radio Push-to-Talk
(PTT) buttons installed on each side
console and each Display Control Grip
may be used in lieu of each Control
Wheel Push-to-Talk Switch.
|
|
|
|
|
a) Lavatory Speakers
|
|
|
|
|
|
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT:
REVISION NO: 1
PAGE NO:
GULFSTREAM G150
DATE: 11/12/2008
23-3
1. SYSTEM,
REPAIR CATEGORY
SEQUENCE NUMBERS &
2. NUMBER INSTALLED
ITEM
3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
23 COMMUNICATIONS
5. Cockpit Voice Recorder
(CVR) (With Flight Data
Recorder (FDR)
Installed)
A
1
0
May be inoperative provided:
a) Flight Data Recorder (FDR) is
operative, and
b) Repairs are made within three (3)
flight days.
Cockpit Voice Recorder
(CVR) (Without Flight
Data Recorder (FDR)
Installed)
A
1
0
May be inoperative provided repairs are
made within three (3) flight days.
Cockpit Voice Recorder
(CVR) Installed for an
Operator Other Than a
Holder of an Air Carrier
or Commercial Operator
Certificate
A
1
0
May be inoperative provided repairs are
made in accordance with 14 CFR.
6. Selective Call System
*** (SELCAL)
1) Channels
7. Static Discharge Wicks
|
C
-
0
(O) May be inoperative provided alternate |
procedures are established and used.
|
D
-
0
May be inoperative provided procedures
do not require its use.
C
-
0
(O) May be inoperative provided alternate |
procedures are established and used.
|
D
-
0
May be inoperative provided procedures
do not require its use.
C
-
-
Maximum of two (2) may be damaged or
missing provided not more than one (1) is
damaged or missing from each flight
control group surface.
|
|
|
|
8
.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT:
REVISION NO: 1
PAGE NO:
GULFSTREAM G150
DATE: 11/12/2008
23-4
1. SYSTEM,
REPAIR CATEGORY
SEQUENCE NUMBERS &
2. NUMBER INSTALLED
ITEM
3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
23 COMMUNICATIONS
8. Crewmember Interphone
*** System (Flight Deck to
Cabin/Cabin to Flight
Deck/Flight Deck to
Ground)
9. Automatic Cabin Briefing
*** System
C
1
0
(O) May be inoperative provided alternate |
procedures are established and used.
|
D
1
0
May be inoperative provided procedures
do not require its use.
D
1
0
(O) May be inoperative provided alternate
procedures are established and used.
10. Emergency Locator
*** Transmitter
|
|
|
|
1) Survival Type ELTs
D
-
-
Any in excess of those required by 14
CFR may be inoperative or missing.
|
|
2) Fixed ELTs
A
1
0
May be inoperative or missing provided
repairs are made within 90 days.
|
|
D
1
-
Any in excess of those required by 14
CFR may be inoperative or missing.
|
|
3) ELT Remote Switch
C
1
0
(M) May be inoperative provided:
a) Remote Switch is disconnected
from ELT, and
b) ELT Switch is placed in ARM.
|
|
|
|
11. Flight Phone Systems
***
D
-
-
12. Headset Jacks
C
2
0
May be inoperative provided cockpit
speakers are operative.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT:
REVISION NO: 1
PAGE NO:
GULFSTREAM G150
DATE: 11/12/2008
23-5
1. SYSTEM,
REPAIR CATEGORY
SEQUENCE NUMBERS &
2. NUMBER INSTALLED
ITEM
3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
23 COMMUNICATIONS
13. Boom Microphones
Cockpit Voice Recorder
(CVR) with Flight Data
Recorder (FDR) Installed
1) Cockpit Voice Recorder
Equipped to Record
Boom Microphone per
FAR 121.359(g),
135.151(d) or 125.227(e)
A
-
0
May be inoperative provided:
a) Flight Data Recorder (FDR) is
operative, and
b) Repairs are made within three (3) |
flight days.
|
2) Cockpit Voice Recorder
*** not equipped to record
Boom Microphones.
D
1
0
Any in excess of those required by 14
CFR may be inoperative.
1) Cockpit Voice Recorder
Equipped to Record
Boom Microphone per
FAR 121.359(g),
135.151(d) or 125.227(e)
A
-
0
May be inoperative provided repairs are
made within three (3) flight days.
2) Cockpit Voice Recorder
*** not equipped to record
Boom Microphones.
D
|
|
Cockpit Voice Recorder
without Flight Data
Recorder Installed
|
|
-
0
Any in excess of those required by 14
CFR may be inoperative.
|
|
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT:
REVISION NO: 1
PAGE NO:
GULFSTREAM G150
DATE: 11/12/2008
23-6
1. SYSTEM,
REPAIR CATEGORY
SEQUENCE NUMBERS &
2. NUMBER INSTALLED
ITEM
3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
23 COMMUNICATIONS
14. High Frequency (HF)
Communication System
15. Headsets
D
-
-
Any in excess of those required by 14
CFR may be inoperative.
|
|
C
-
1
(O) May be inoperative while conducting
operations that require two (2) LRCS
provided:
a) SATCOM Voice or Data Link is
operative,
b) Alternate procedures are
established and used,
c) SATCOM coverage is available
over intended route of flight, and
d) If Inmarsat codes are not available
while using SATCOM voice, prior
coordination with appropriate ATS
facility is required.
|
|
|
|
|
|
|
|
|
|
|
|
|
NOTE: SATCOM is to be used only as a
backup to normal HF communications
unless otherwise authorized by
appropriate ATS facilities.
|
|
|
|
C
2
1
One pilot’s headset may be inoperative
provided operations do not require its use
and both pilot cockpit speakers are
operative.
C
2
0
Both pilot’s headsets may be inoperative,
except when required by 14 CFR (see
NOTE below), provided both pilot cockpit
speakers are operative.
|
|
|
|
NOTE: 14 CFR requires one operative
headset for:
a) 14 CFR 91 overwater flights (more
than 30 minutes or 100 nm from
shore).
b) 14 CFR 135 extended overwater
(more than 50 nm from shore).
c) 14 CFR 135 IFR.
|
|
|
|
|
|
|
|
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT:
REVISION NO: 1
PAGE NO:
GULFSTREAM G150
DATE: 11/12/2008
23-7
1. SYSTEM,
REPAIR CATEGORY
SEQUENCE NUMBERS &
2. NUMBER INSTALLED
ITEM
3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
23 COMMUNICATIONS
16. Alerting System
(Audio/Visual)
1) Passenger Configuration
a) Flight Deck Call Visual
Alerting System
B
1
0
May be inoperative provided flight deck
audio alerting system is operative.
NOTE: Flight deck audio alerting must
always be operative.
|
|
b) Flight Attendant Visual
Alerting System
Deleted in Revision 1.
|
c) Flight Attendant Audio
Alerting System
Deleted in Revision 1.
|
17. Radio Push-to-Talk
(PTT) Switches
18. Belts/No Smoke Cabin
Chime
C
6
0
Any or all may be inoperative provided an
operative Hand Held Microphone is
available to crewmember(s) on side of
failed PTT switch(es).
|
|
|
|
C
6
2
Up to two may be inoperative at each
cockpit crew position.
|
|
NOTE: Each cockpit crew position has
three radio push to talk buttons; one on
yolk, one on side console and one on
Display Control Grip.
|
|
|
|
C
-
-
May be inoperative provided:
|
a) Belts/No Smoke signs are visible |
to all passengers, and
b) A Crewmember advises
|
passengers verbally to secure
their seat belts and when smoking
is permitted.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT:
REVISION NO: 1
PAGE NO:
GULFSTREAM G150
DATE: 11/12/2008
23-8
1. SYSTEM,
REPAIR CATEGORY
SEQUENCE NUMBERS &
2. NUMBER INSTALLED
ITEM
3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
23 COMMUNIATIONS
19. Radio Tuning Controls In
Cursor Control Panels
20. Satellite Communication
*** System (SATCOM)
21. Yoke Mounted
Microphone Holder
22. Airborne Flight
*** Information System
(AFIS)
(VHF datalink and/or
Satellite XM)
C
2
1
May be inoperative provided direct tuning |
is operative on at least one FMS.
|
C
2
0
May be inoperative provided direct tuning
is operative on two FMSs.
A
2
0
May be inoperative provided:
a) Direct turning is operative on one
FMS, and
b) Repairs are made within one (1)
flight day.
C
-
0
(O) May be inoperative provided alternate |
procedures are established and used.
|
D
-
0
May be inoperative provided procedures
do not require its use.
|
|
C
2
0
One or both may be damaged, torn, or
missing provided affected microphone is
secured or removed.
|
|
|
NOTE: Reference 23-4 if microphone is
removed or rendered inaccessible.
|
|
|
|
|
|
|
C
1
0
(O) May be inoperative provided alternate |
procedures are established and used.
|
|
|
|
D
1
0
May be inoperative provided procedures
do not require its use.
|
|
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT:
REVISION NO: 1
PAGE NO:
GULFSTREAM G150
DATE: 11/12/2008
24-1
1. SYSTEM,
REPAIR CATEGORY
SEQUENCE NUMBERS &
2. NUMBER INSTALLED
ITEM
3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
24 ELECTRICAL POWER
1. Left Battery
B
1
0
(M) May be inoperative provided:
a) Both generators are operative,
b) APU generator is operative,
c) A ground power unit is used for
APU and engine starts with battery
master switch selected to ON,
d) Left battery disconnect circuit
breaker is pulled to disconnect it
from its associated bus, and
e) L BATT OFF message is
displayed.
|
|
|
|
|
NOTE: Observe APU altitude and
electrical load limitations.
2. Left Battery Temperature
Indicating System
3. Generator DC Voltage
Displays
C
C
1
2
0
1
(M) May be inoperative provided:
a) Both generators are operative,
b) APU generator is operative,
c) A ground power unit is used for
APU and engine starts, and
d) Left Battery disconnect circuit
breaker is pulled and collared to
disconnect it from its associated
bus, and
e) L BATT OFF message is
displayed.
|
NOTE 1: Observe APU altitude and
electrical load limitations.
|
|
NOTE 2: Temperature Indicating System
is not applicable / indication is not
displayed for airplanes with Concord
Valve Regulated Lead-Acid Main
Batteries installed (STC ST03511AT-D).
|
|
|
|
|
May be inoperative provided GEN OFF
message and AMPS display of
associated generating system are
operative.
|
|
|
|
|
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT:
REVISION NO: 1
PAGE NO:
GULFSTREAM G150
DATE: 11/12/2008
24-2
1. SYSTEM,
REPAIR CATEGORY
SEQUENCE NUMBERS &
2. NUMBER INSTALLED
ITEM
3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
24 ELECTRICAL POWER
4. DC External Power
System
C
1
0
5. Engine Generator
Warning Systems
C
2
1
6. Engine Generators
A
2
1
May be inoperative provided:
a) Associated Generator Volts and
AMPS displays are operative, and
b) Generator(s) output and engine
vibration is closely monitored
when airplane is operated.
(M) One may be inoperative provided:
a) APU is kept operating with its
generator selected ON throughout
flight,
b) Inoperative generator switch is left
in OFF,
c) Integrity of affected engine
starter/generator is verified safe
for starter operation, and
d) Repairs are made within one (1)
flight day.
|
|
|
|
|
|
|
|
|
|
|
|
NOTE: Observe APU altitude and
electrical load limitations.
7. Main Batteries Voltage
Displays
C
2
1
One may be inoperative provided BATT
OFF EICAS message of each battery is
verified operative before each takeoff.
8. 60Hz AC Electrical
Power System
C
1
0
(M) (O) May be inoperative provided
affected circuit breaker is pulled and
collared.
|
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT:
REVISION NO: 1
PAGE NO:
GULFSTREAM G150
DATE: 11/12/2008
24-3
1. SYSTEM,
REPAIR CATEGORY
SEQUENCE NUMBERS &
2. NUMBER INSTALLED
ITEM
3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
24 ELECTRICAL POWER
9. APU Generator
10. 50Hz AC Electrical
*** Power System
C
C
1
1
0
0
May be inoperative provided:
a) Both Batteries are operative,
b) Both Battery Temperature Indicating
Systems are operative, and
c) Both Engine Generators are
operative.
|
|
|
|
|
|
|
NOTE: Operating Battery Temperature
Indicating System is not required (not
applicable / indication is not displayed) for
airplanes with Concord Valve Regulated
Lead-Acid Main Batteries installed (STC
ST03511AT-D).
|
|
|
|
|
(M) (O) May be inoperative provided
affected circuit breaker is pulled and
collared.
|
|
|
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT:
REVISION NO: 1
PAGE NO:
GULFSTREAM G150
DATE: 11/12/2008
25-1
1. SYSTEM,
REPAIR CATEGORY
SEQUENCE NUMBERS &
2. NUMBER INSTALLED
ITEM
3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
25 EQUIPMENT/
FURNISHINGS
1. Passenger Seat(s)
D
-
-
May be inoperative provided:
a) Seat does not block an
Emergency Exit,
b) Seat does not restrict any
passenger from access to main
airplane aisle, and
c) Affected seat(s) are blocked and
placarded “DO NOT OCCUPY”.
|
|
|
NOTE 1: A seat with an inoperative
seatbelt is considered to be inoperative.
NOTE2: Inoperative seats do not affect
the required number of flight attendants.
NOTE 3: Affected seat(s) may include the
seat(s) behind and/or adjacent outboard
seats.
1) Recline Mechanism
2) Underseat Baggage
*** Restraining Bars
(continued)
D
-
-
(M) May be inoperative and seat occupied |
provided seat is secured in the full upright |
position.
C
-
-
(M) May be inoperative and seat occupied |
provided seat back is immovable in full
|
upright position.
|
C
-
-
Deleted in Revision 1.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT:
REVISION NO: 1
PAGE NO:
GULFSTREAM G150
DATE: 11/12/2008
25-2
1. SYSTEM,
REPAIR CATEGORY
SEQUENCE NUMBERS &
2. NUMBER INSTALLED
ITEM
3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
25 EQUIPMENT/
FURNISHINGS
1. Passenger Seat(s)
(continued)
3) Armrest
C
-
-
(M) May be inoperative or missing and
seat occupied provided:
a) Armrest does not block an
Emergency Exit,
b) Armrest does not restrict any
passenger from access to main
airplane aisle, and
c) For an armrest with a recline
mechanism, seat is secured in the
full upright position.
4) Swivel Mechanism
***
C
-
-
(M) May be inoperative and occupied
provided:
a) Associated seat does not block an
Emergency Exit,
b) Associated seat does not restrict
any passenger from access to the
main airplane aisle, and
c) Associated seat remains in takeoff
position.
5) Divan High Back Seat(s)
***
C
-
-
May be inoperative and occupied
provided:
a) Associated seat does not block an
Emergency Exit,
b) Associated seat does not restrict
any passenger from access to the
main airplane aisle, and
c) Associated seat remains in takeoff
position.
6) Divan Berthing
*** Mechanism
C
-
-
May be inoperative and seat occupied
provided associated seat is secured in
the takeoff position.
(continued)
|
|
|
|
|
|
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT:
REVISION NO: 1
PAGE NO:
GULFSTREAM G150
DATE: 11/12/2008
25-3
1. SYSTEM,
REPAIR CATEGORY
SEQUENCE NUMBERS &
2. NUMBER INSTALLED
ITEM
3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
25 EQUIPMENT/
FURNISHINGS
1. Passenger Seat(s)
(continued)
7) Electrical/Electronic
*** Systems/Components
C
-
-
(M) May be inoperative and seat
occupied provided associated
component(s) is deactivated.
2. Emergency Medical
Equipment
1) Automatic External
*** Defibrillator (AED) and/or
Associated Equipment
2) Emergency Medical Kit
*** (EMK) and/or Associated
Equipment
(continued)
|
|
A
-
0
(O) May be incomplete, missing or
inoperative provided:
a) AED is resealed in a manner
that will identify it as a unit that
cannot be mistaken for a fully
serviceable unit, and
b) Repairs or replacements are
made within three (3) flight
cycles.
|
|
|
|
|
|
|
|
|
D
-
-
Any in excess of those required by 14
CFR may be incomplete, missing or
inoperative.
|
|
|
A
-
0
(O) May be incomplete, missing or
inoperative provided:
a) EMK is resealed in a manner
that will identify it as a unit that
cannot be mistaken for a fully
serviceable unit, and
b) Repairs or replacements are
made within three (3) flight
cycles.
|
|
|
|
|
|
|
|
|
D
-
-
Any in excess of those required by 14
CFR may be incomplete, missing or
inoperative.
|
|
|
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT:
REVISION NO: 1
PAGE NO:
GULFSTREAM G150
DATE: 11/12/2008
25-4
1. SYSTEM,
REPAIR CATEGORY
SEQUENCE NUMBERS &
2. NUMBER INSTALLED
ITEM
3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
25 EQUIPMENT/
FURNISHINGS
2. Emergency Medical
Equipment (continued)
3) First Aid Kit (FAK) and/or
Associated Equipment
A
-
-
(O) If more than one is required by 14
CFR, only one of the required first aid
kits may be incomplete, missing or
inoperative provided:
a) FAK is resealed in a manner
that will identify it as a unit that
cannot be mistaken for a fully
serviceable unit, and
b) Repairs or replacements are
made within three (3) flight
cycles.
|
|
|
|
|
|
|
|
|
|
|
D
-
-
Any in excess of those required by 14
CFR may be incomplete, missing or
inoperative.
|
|
|
3. Overwater Survival
Equipment
D
-
-
Any in excess of those required by 14
CFR may be inoperative or missing.
|
|
4. Non-Essential
Equipment & Furnishings
(NEF)
D
-
0
May be inoperative, damaged or
missing provided item(s) is deferred in
accordance with operator’s (insert
name) Manual. (M) and (O) procedures,
if required, must be available to flight
crew and included in appropriate
operator’s document.
|
|
|
|
|
|
|
NOTE: Exterior lavatory door ash trays
are not considered NEF items.
|
|
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT:
REVISION NO: 1
PAGE NO:
GULFSTREAM G150
DATE: 11/12/2008
25-5
1. SYSTEM,
REPAIR CATEGORY
SEQUENCE NUMBERS &
2. NUMBER INSTALLED
ITEM
3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
25 EQUIPMENT/
FURNISHINGS
5. “Fasten Seat Belt While
Seated” Sign or Placard
C
-
-
One or more signs or placards may be
illegible or missing provided a legible
sign or placard is visible from each
occupied passenger seat.
6. Cargo Restraint Systems
C
-
-
(M) May be inoperative, or missing
provided acceptable cargo loading limits
from an approved source, i.e., an
approved Cargo Loading Manual,
Cargo Handling Manual, or Weight and
Balance Document are observed.
C
-
-
May be inoperative or missing provided |
cargo compartment remains empty.
|
7. Pilot Seats
C
-
-
1) Vertical Adjustment
C
-
-
2) Armrest(s)
3) Recline Adjustment
(continued)
C
C
-
-
-
-
(M) (O) May be inoperative provided:
a) Seat is secured in a position
acceptable to affected
crewmember, and
b) Seat is able to move Fore-Aft on
its track.
(M) (O) May be inoperative provided:
a) Armrest is secured in full up
position, and
b) Seat is acceptable to affected
crewmember.
(M) (O) May be inoperative provided:
a) Seat is secured in a position
acceptable to affected
crewmember, and
b) Seat is able to move Fore-Aft on
its track.
|
|
|
|
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT:
REVISION NO: 1
PAGE NO:
GULFSTREAM G150
DATE: 11/12/2008
25-6
1. SYSTEM,
REPAIR CATEGORY
SEQUENCE NUMBERS &
2. NUMBER INSTALLED
ITEM
3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
25 EQUIPMENT/
FURNISHINGS
7. Pilot Seats (continued)
4) Lumbar Adjustment
C
-
-
May be inoperative provided seat is
acceptable to affected crewmember.
|
|
5) Thigh Adjustment
C
-
-
May be inoperative provided seat is
acceptable to affected crewmember.
|
|
6) Inertial Reel
C
-
-
May be inoperative provided inertial reel
lock handle engages and locks shoulder
straps securely and is acceptable to
affected crewmember.
|
|
|
|
7) Vertical Back Rest
Adjustment
C
-
-
May be inoperative provided seat is
acceptable to affected crewmember.
|
|
8) Headrests
C
-
-
May be inoperative provided seat is
acceptable to affected crewmember.
|
|
8. Rudder PedalAdjustment
9. Crash Axe
***
Moved to ATA 27.15 Flight Controls in- |
Revision 1.
|
B
-
-
Any in excess of those required by 14
CFR may be missing.
|
|
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT:
REVISION NO: 1
PAGE NO:
GULFSTREAM G150
DATE: 11/12/2008
25-7
1. SYSTEM,
REPAIR CATEGORY
SEQUENCE NUMBERS &
2. NUMBER INSTALLED
ITEM
3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
25 EQUIPMENT/
FURNISHINGS
10. Overhead Storage
*** Bin(s)/Cabin and Galley
Storage
Compartment/Closets
C
-
-
(M) May be inoperative provided:
a) Procedures are established to
secure compartment CLOSED,
b) Associated bin or compartment is
prominently placarded DO NOT
USE,
c) Any emergency equipment located
in affected compartment is
considered inoperative, and
d) Affected compartment is not used
for storage of any item(s) except
for those permanently affixed.
|
|
|
|
|
|
|
|
|
|
NOTE: If no partitions are installed,
|
entire overhead storage compartment is |
considered one bin or compartment.
|
C
-
-
(M) (O) May be inoperative provided:
a) Affected door(s) is removed,
b) Associated bin or compartment is
not used for storage of any items,
except those permanently affixed,
c) Associated bin or compartment is
prominently placarded DO NOT
USE,
d) Procedures are established and
used to alert crew members and
passengers of inoperative bins,
and
e) Passengers are briefed that
associated bin or compartment is
not used.
|
|
|
|
|
|
|
|
|
|
|
|
|
NOTE 1: If no partitions are installed,
|
entire overhead storage compartment is |
considered one bin or compartment.
|
(continued)
NOTE 2: Any emergency equipment
located in associated compartment
(permanently affixed) is available for
use.
|
|
|
|
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT:
REVISION NO: 1
PAGE NO:
GULFSTREAM G150
DATE: 11/12/2008
25-8
1. SYSTEM,
REPAIR CATEGORY
SEQUENCE NUMBERS &
2. NUMBER INSTALLED
ITEM
3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
25 EQUIPMENT/
FURNISHINGS
10. Overhead Storage
*** Bin(s)/Cabin and Galley
Storage
Compartment/Closets
(continued)
|
|
|
1) Storage Compartment
*** Key Locks
D
-
0
(M) May be inoperative in unlocked
|
position provided doors can be secured |
by other means.
|
11. Galley Waste
*** Receptacles Access
Doors / Covers
C
-
-
(M) (O) May be inoperative provided:
a) Container is empty and access is |
secured to prevent waste
|
introduction into compartment, and |
b) Procedures are established to
ensure that sufficient galley waste
receptacles are available to
accommodate all waste that may
be generated on a flight.
12. Exterior Lavatory Door
Ashtray
A
1
0
May be missing provided it is replaced
within three (3) calendar days.
13. Emergency Vision
*** Assurance System
(EVAS)
C
-
0
|
14. Cockpit Convenience
Items
Deleted in Revision 1.
15. Crewmember Flashlight
Holder Assemblies
(Including Flashlight)
C
-
0
May be inoperative or missing provided
crewmember has a flashlight of
equivalent characteristics readily
available.
16. Reference Eye Locator
C
1
0
May be missing or damaged.
|
|
|
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT:
REVISION NO: 1
PAGE NO:
GULFSTREAM G150
DATE: 11/12/2008
25-9
1. SYSTEM,
REPAIR CATEGORY
SEQUENCE NUMBERS &
2. NUMBER INSTALLED
ITEM
3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
25 EQUIPMENT/
FURNISHINGS
17. Passenger Underseat
*** Stowage Drawers
C
-
-
(O) May be inoperative, missing or have
broken latches provided:
a) Drawer does not block an
Emergency Exit, and
b) Drawer does not restrict any
passenger from access to main
airplane aisle, and
c) Affected drawer is emptied,
secured where possible and
placarded “DO NOT USE”.
|
|
|
|
|
|
|
|
|
|
18. Cabin Flight Information
*** System
C
1
0
(O) May be inoperative provided
alternate procedures are established
and used.
|
|
|
19. Airplane Ladder
***
D
-
0
May be inoperative, damaged, missing
or removed.
|
|
NOTE: Removal will require airplane
weight and balance considerations.
|
|
May be inoperative, damaged, missing
or removed.
|
|
NOTE: Removal will require airplane
weight and balance considerations.
|
|
20. Airplane Tow Bar
***
21. Baggage Compartment
Heating Blankets
D
D
-
2
0
0
(M) May be inoperative provided system |
is deactivated and BAGGAGE
|
COMPRT Heat Switch is OFF.
|
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT:
REVISION NO: 1
PAGE NO:
GULFSTREAM G150
DATE: 11/12/2008
26-1
1. SYSTEM,
REPAIR CATEGORY
SEQUENCE NUMBERS &
2. NUMBER INSTALLED
ITEM
3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
26 FIRE PROTECTION
1. APU Bleed Leak
Detector
2. Portable Fire
Extinguishers
3. Fire Extinguisher
Thermal Discharge Disk
D
C
4. APU Fire Detection
System
C
5. APU Fire Extinguisher
System
C
6. Entertainment System
*** Overheat Detection
System
D
-
1
1
1
1
-
0
0
0
0
Deleted in Revision 1.
|
Any in excess of those required by 14
CFR may be inoperative or missing
provided:
a) Inoperative fire extinguisher is
tagged inoperative, removed from
the installed location and placed
out of sight so it can not be
mistaken for a functional unit, and
b) Required distribution is
maintained.
|
|
|
|
May be missing provided:
a) Adequate charge is checked
during preflight inspection, and
b) Yellow EMPTY light is not
illuminated “on ARM/EMPTY
Discharge Pushbuttons.”
|
|
|
(M) May be inoperative provided:
a) APU is not used,
b) APU CONTR circuit breaker is
pulled and collared, and
c) APU Master Switch is set to OFF.
|
|
|
|
(M) May be inoperative provided:
a) APU is not used,
b) APU CONTR circuit breaker is
pulled and collared, and
c) APU Master Switch is set to OFF.
|
|
|
|
(M) May be inoperative provided
|
Entertainment System is disabled and not |
used.
|
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT:
REVISION NO: 1
PAGE NO:
GULFSTREAM G150
DATE: 11/12/2008
26-2
1. SYSTEM,
REPAIR CATEGORY
SEQUENCE NUMBERS &
2. NUMBER INSTALLED
ITEM
3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
26 FIRE PROTECTION
7. Entertainment System
*** Smoke Detection System
D
1
0
(M) May be inoperative provided
|
Entertainment System is disabled and not |
used.
|
8. Lavatory Smoke
*** Detection System
C
1
0
(M) (O) Lavatory smoke detection system
may be inoperative provided:
a) Lavatory waste receptacle is
empty,
b) Associated lavatory door is
CLOSED and placarded,
“INOPERATIVE – DO NOT
ENTER”, and
c) Lavatory is used only by
crewmembers.
|
|
|
|
|
|
|
|
|
|
|
NOTE 1: These provisos are not intended |
to prohibit lavatory use or inspections by |
crewmembers.
|
NOTE 2: Lavatory smoke detection
system is not required for all-cargo
operations.
|
|
|
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT:
REVISION NO: 1
PAGE NO:
GULFSTREAM G150
DATE: 11/12/2008
27-1
1. SYSTEM,
REPAIR CATEGORY
SEQUENCE NUMBERS &
2. NUMBER INSTALLED
ITEM
3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
27 FLIGHT CONTROLS
1. Automatic Slat Extension
System
2. Aileron Trim System
C
1
0
May be inoperative provided:
a) Airplane is not operated in known
or forecast icing conditions,
b) Airplane is operated in day VMC,
c) Flight crew extends slats before
AOA exceeding 0.70, and
d) Airplane is operated in
accordance with AFM Limitations.
|
|
|
|
C
1
0
May be inoperative provided airplane is
operated with slats extended.
|
|
B
1
0
(M) May be inoperative provided:
a) Trim is in neutral position for
takeoff,
b) System is deactivated, and
c) Rudder trim system is operative.
|
3. Aileron Trim Position
Indicator
C
1
0
May be inoperative provided:
a) Aileron trim system is verified to
be operative before each
departure, and
b) Aileron trim is properly set and
checked visually before each
departure.
4. Rudder Trim Motors
C
2
1
One may be inoperative provided trim
functions normally.
5. Rudder Trim Position
Indicator
C
1
0
May be inoperative provided:
a) Rudder Trim Control System is
operative, and
b) Rudder Trim Tab is verified to be
in the neutral position with Yaw
Damper OFF before departure.
|
|
|
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT:
REVISION NO: 1
PAGE NO:
GULFSTREAM G150
DATE: 11/12/2008
27-2
1. SYSTEM,
REPAIR CATEGORY
SEQUENCE NUMBERS &
2. NUMBER INSTALLED
ITEM
3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
27 FLIGHT CONTROLS
6. Horizontal Stabilizer
Position Indicator
B
1
0
(O) May be inoperative provided:
a) Horizontal Stabilizer system is
operative,
b) Before each takeoff the flight crew
verifies by visual inspection that
actual horizontal stabilizer
position, as indicated by the
position placard on the vertical
stabilizer, matches the setting in
AFM Section V, “Horizontal Trim
Setting for Take-Off” chart,
c) CONFIG TRIM warning system is
operative,
d) CONFIG TRIM warning message
is extinguished for takeoff, and
e) Horizontal Stabilizer Trim Audio
Signal is operational.
7. Slat/Flap Position
Indicators
1) Slat Position Indicator
(continued)
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
C
1
0
May be inoperative provided:
a) Slats are verified to be properly
positioned after each commanded
control movement, and
b) CONFIG SLATS Warning is
operative.
|
|
|
|
|
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT:
REVISION NO: 1
PAGE NO:
GULFSTREAM G150
DATE: 11/12/2008
27-3
1. SYSTEM,
REPAIR CATEGORY
SEQUENCE NUMBERS &
2. NUMBER INSTALLED
ITEM
3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
27 FLIGHT CONTROLS
7. Slat/Flap Position
Indicators (continued)
2) Flap Position Indicator
|
|
C
1
0
8. Flight Airbrakes Warning
System
May be inoperative provided:
a) Flaps are operative.
b) CONFIG FLAPS Warning is
operative, and
b) Flap setting and position
corresponds with the Horizontal
Stabilizer trim setting for take-off.
|
|
|
|
|
|
|
NOTE: Correct takeoff trim setting may be
found in Section V of AFM in
HORIZONTAL STABILIZER TRIM
SETTING FOR TAKEOFF chart.
|
|
|
|
Deleted in Revision 1.
|
9. Horizontal Stabilizer Trim
Audio Signal
C
1
0
May be inoperative provided:
a) Horizontal stabilizer trim is
operative,
b) CONFIG TRIM Warning message |
is operative,
|
c) Horizontal stabilizer position
indicator is operative, and
d) Autopilot is not used.
10. Ground Airbrakes
Indicating System
C
1
0
May be inoperative provided:
a) Ground Airbrakes are verified to
be operative,
b) Ground Airbrakes are visually
confirmed retracted before takeoff
and landing,
c) FLT A/B FAIL messages do not
come on when Ground Airbrakes
are extended, and
d) A/B T/O NOT ARMED Caution is
operative.
|
|
|
|
|
|
|
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT:
REVISION NO: 1
PAGE NO:
GULFSTREAM G150
DATE: 11/12/2008
27-4
1. SYSTEM,
REPAIR CATEGORY
SEQUENCE NUMBERS &
2. NUMBER INSTALLED
ITEM
3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
27 FLIGHT CONTROLS
11. Elevator and Rudder
Gust Lock
C
1
0
(O) May be inoperative provided:
a) Gust Lock handle is in
“RELEASED” position, and
b) Elevator and Rudder has
“Freedom of Movement”.
12. Slats System
A
1
0
May be inoperative provided:
a) Slats are fully extended,
b) FLAP/SLAT lever is not selected
UP,
c) Airplane is operated in accordance
with AFM limitations, and
d) Repairs are made within one (1)
flight day.
|
|
|
|
|
|
|
|
13. Ground Airbrakes Auto
Deploy System
B
1
0
(O) May be inoperative provided:
a) Ground airbrakes are verified
operative by selecting GROUND
A/B switch to LAND,
b) The GROUND A/B switch is OFF
for takeoff and landing.
c) Takeoff and landing distances and
V1 are adjusted in accordance
with AFM, and
d) Takeoff, abort, and landing
procedures are briefed
accordingly.
|
|
|
|
|
|
|
|
|
|
|
|
NOTE 1: A/B T/O NOT ARMED message |
will be displayed during takeoff.
|
|
NOTE 2: Takeoff and landing distances
|
must be adjusted in accordance with
|
Ground A/B Failure Before Takeoff and
|
Ground A/B Failure During Landing
|
procedures in Section III of the AFM.
|
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT:
REVISION NO: 1
PAGE NO:
GULFSTREAM G150
DATE: 11/12/2008
27-5
1. SYSTEM,
REPAIR CATEGORY
SEQUENCE NUMBERS &
2. NUMBER INSTALLED
ITEM
3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
27 FLIGHT CONTROLS
14. Ground Airbrakes
System
15. Rudder Pedal
Adjustment
B
C
1
-
0
-
(M) (O) May be inoperative provided:
a) Ground Airbrakes System is
deactivated,
b) Ground Airbrakes are confirmed
retracted before takeoff,
c) Takeoff and landing distances are
adjusted in accordance with AFM,
and
d) Takeoff, abort and landing
procedures are briefed
accordingly.
|
|
|
|
|
|
|
|
|
|
|
NOTE: Takeoff and landing distance
adjustments are documented in Ground
A/B Failure Before Takeoff and Ground
A/B Failure During Landing procedures in
Section III of the AFM.
|
|
|
|
|
(M) May be inoperative provided:
a) Rudder pedals can be secured in
a position acceptable to affected
crewmember, and
b) Position of Rudder Pedals permits
full flight control movement.
|
|
|
|
|
|
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT:
REVISION NO: 1
PAGE NO:
GULFSTREAM G150
DATE: 11/12/2008
28-1
1. SYSTEM,
REPAIR CATEGORY
SEQUENCE NUMBERS &
2. NUMBER INSTALLED
ITEM
3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
28 FUEL
1. Jettison Valves
C
2
1
One may be inoperative provided
interconnect valves operate normally.
2. Fuel Low Level Warning
System
B
1
0
May be inoperative provided:
a) All fuel quantity systems are
operative, and
b) Crew members monitor fuel
quantity during flight.
3. Fuel Tank Temperature
Indication
C
1
0
(O) May be inoperative provided flight is
conducted at a TAT at least 3 degrees C
above fuel low temperature limitation.
|
4. Pressure Fueling System
C
1
0
5. Forward (Wing)
Interconnect Valve
C
1
0
(O) May be inoperative provided:
a) Aft (collector box) interconnect
valve is operative,
b) Forward (Wing) interconnect valve
is verified CLOSED, and
c) Fuel jettison valves are operative.
|
|
|
|
|
|
6. Wing Fuel Quantity
Indicating Systems
A
2
1
(O) One may be inoperative provided:
a) Total fuel quantity is verified
before departure
b) Fuselage fuel tank has a minimum
of 1,000 lbs available for dispatch,
c) All other fuel system components
and fuel indicating systems are
operative,
d) After takeoff, power is set by
matching fuel flow indications on
both engines,
e) Flight crew maintains a log of fuel
burned, and
f) EICAS Fuel Total is placarded
inoperative.
g) Repairs are made within two (2)
flight days.
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT:
REVISION NO: 1
PAGE NO:
GULFSTREAM G150
DATE: 11/12/2008
28-2
1. SYSTEM,
REPAIR CATEGORY
SEQUENCE NUMBERS &
2. NUMBER INSTALLED
ITEM
3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
28 FUEL
7. Fuel Total Indication
C
1
0
(O) May be inoperative provided:
a) Total fuel quantity is verified
before departure, and
b) All other fuel system components
and fuel indicating systems are
operative, and
c) Flight crew maintains a log of fuel
burned.
8. Tank Fuel Quantity
Indicating Systems
1) Fuselage Tank Fuel
Quantity Indicating
System
|
|
|
|
|
|
|
|
|
|
C
1
0
(O) May be inoperative provided:
a) Total fuel quantity is verified
before departure,
b) All other fuel system components
and fuel indicating systems are
operative,
c) Flight crew maintains a log of fuel
burned, and
d) EICAS Fuel Total Indication is
placarded inoperative.
|
|
|
|
|
|
|
|
|
|
C
1
0
(O) May be inoperative provided:
a) Total fuel quantity is verified
before departure to be less than
3600 lbs. (i.e. Fuselage Tank is
empty), and
b) All other fuel components and
indications are operative.
|
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|
|
|
|
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT:
REVISION NO: 1
PAGE NO:
GULFSTREAM G150
DATE: 11/12/2008
28-3
1. SYSTEM,
REPAIR CATEGORY
SEQUENCE NUMBERS &
2. NUMBER INSTALLED
ITEM
3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
28 FUEL
8. Tank Fuel Quantity
Indicating Systems
(continued)
2) Center Tank Fuel
Quantity Indicating
System
C
1
0
(O) May be inoperative provided:
a) Total fuel quantity is verified
before departure,
b) All other fuel system components
and fuel indicating systems are
operative,
c) Flight crew maintains a log of fuel
burned, and
d) EICAS Fuel Total Indication is
placarded inoperative.
|
|
|
|
|
|
|
|
|
|
C
1
0
(O) May be inoperative provided:
a) Total fuel quantity is verified
before departure to be less than
4900 lbs. (i.e. Center Tank is
empty), and
b) All other fuel system components
and fuel indicating systems are
operative.
|
|
|
|
|
|
|
|
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT:
REVISION NO: 1
PAGE NO:
GULFSTREAM G150
DATE: 11/12/2008
28-4
1. SYSTEM,
REPAIR CATEGORY
SEQUENCE NUMBERS &
2. NUMBER INSTALLED
ITEM
3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
28 FUEL
9. Standby Fuel Pumps
10. Fuel Flow Indicating
Systems
Deleted in Revision 1.
B
2
1
One may be inoperative provided:
a) All other engine indications are
operative,
b) All Fuel Quantity Indication
systems are operative, and
c) ITT, N1 and N2 indicators are
compared with those of other
engine.
11. Fuel Used Indicating
System
C
1
0
May be inoperative provided:
a) All other engine indications are
operative, and
b) All Fuel Tank Quantity Indication
systems are operative.
12. Pressure Fueling Cap
A
1
0
May be missing provided replacement is
installed within three (3) flight days.
13. Pressure Defueling
System
Deleted in Revision 1.
14. Fluid Quantity
Measurement Computer
(FQMC) Fail Warning
Systems
A
2
0
Both may be inoperative provided:
a) Both Fuel Quantity Measurement
Computers (FQMC) are operative
before each flight, and
b) Repairs are made within one (1)
flight day.
15. APU Fuel Shutoff Valve
C
1
0
(M) May be inoperative provided:
a) APU is not used,
b) APU CONTR circuit breaker is
pulled and collared, and
c) APU Master Switch is set to OFF.
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|
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U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT:
REVISION NO: 1
PAGE NO:
GULFSTREAM G150
DATE: 11/12/2008
28-5
1. SYSTEM,
REPAIR CATEGORY
SEQUENCE NUMBERS &
2. NUMBER INSTALLED
ITEM
3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
28 FUEL
16. Refuel Pushbutton
C
1
0
17. Pressure Refueling Cap
Chain
C
1
0
|
May be broken or missing.
|
|
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT:
REVISION NO: 1
PAGE NO:
GULFSTREAM G150
DATE: 11/12/2008
29-1
1. SYSTEM,
REPAIR CATEGORY
SEQUENCE NUMBERS &
2. NUMBER INSTALLED
ITEM
3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
29 HYDRAULIC POWER
1. Engine Driven Hydraulic
Pump Pressure Warning
Systems
C
2
1
(O) One may be inoperative provided:
a) AUX Hydraulic pump is verified to
be operative before each flight,
b) Ground air brakes, wheel brakes
and ailerons are cycled
simultaneously before each flight
to ensure no associated hydraulic
messages are triggered or
displayed,
c) Main hydraulic pressure indicating
system is operative, and
d) Engine driven hydraulic pump with
inoperative pressure warning
system is verified operative before
each flight.
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
2. Main Hydraulic Level
Low Warning System
A
1
0
(O) May be inoperative provided:
a) Hydraulic system is operative,
b) Fluid Quantity is visually checked
by reservoir indicator before each
departure, and
c) Repairs are made within one (1)
flight day.
|
|
|
|
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT:
REVISION NO: 1
PAGE NO:
GULFSTREAM G150
DATE: 11/12/2008
29-2
1. SYSTEM,
REPAIR CATEGORY
SEQUENCE NUMBERS &
2. NUMBER INSTALLED
ITEM
3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
29. HYDRAULIC POWER
3. Aux Hydraulic Pressure
Warning System
4. Accumulator Pressure
Gauge
A
C
1
1
0
0
(O) May be inoperative provided:
a) AUX HYD LEVEL LOW and AUX
HYD TEMP HI messages are
operative,
b) AUX pump is verified operative
before each flight,
c) Main hydraulic system is operative,
d) Emergency brakes, T/R, and
ailerons are cycled simultaneously
with the AUX pump ON, prior to
engine start, before each flight to
ensure that no associated hydraulic
messages are triggered or
displayed,
e) Hydraulic pressure indication is
constantly displayed and
monitored.
f) Repairs are made within one (1)
flight day.
(M) May be inoperative provided
accumulator pressure is verified before
each flight.
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|
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U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT:
REVISION NO: 1
PAGE NO:
GULFSTREAM G150
DATE: 11/12/2008
29-3
1. SYSTEM,
REPAIR CATEGORY
SEQUENCE NUMBERS &
2. NUMBER INSTALLED
ITEM
3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
29 HYDRAULIC POWER
5. Hydraulic Tank Pressure
Low Warning System
6. Hydraulic Tank
Pressurization
7. AUX Hydraulic Level
Low Warning System
B
C
A
1
1
1
0
0
0
May be inoperative provided:
a) All other hydraulic components are
operative, and
b) Airplane is not operated above
FL350.
|
|
|
|
|
NOTE: Landing gear extension above
8,000 ft MSL is not recommended.
|
|
May be inoperative provided:
a) All other hydraulic components are
operative, and
|
b) Airplane is not operated above
|
FL350.
|
NOTE: Landing gear extension above
8,000 ft is not recommended.
|
|
(O) May be inoperative provided:
a) Hydraulic system is operative,
b) Fluid Quantity is visually checked
by reservoir indicator before each
departure, and
c) Repairs are made within one (1)
flight day.
|
|
|
|
|
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|
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT:
REVISION NO: 1
PAGE NO:
GULFSTREAM G150
DATE: 11/12/2008
30-1
1. SYSTEM,
REPAIR CATEGORY
SEQUENCE NUMBERS &
2. NUMBER INSTALLED
ITEM
3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
30 ICE AND RAIN
PROTECTION
1. Pitot Heaters
B
2
1
Except where en route operations require
their use, one may be inoperative
provided:
a) Flight is conducted in day VMC
only,
b) Flight is not conducted in visible
moisture of any form, and
c) Airplane is not operated in known
or forecast icing conditions.
2. Probe Heat Warning
Systems
C
3
0
May be inoperative provided airplane is
not operated in known or forecast icing
conditions.
|
NOTE: Applies to Pitot, AOA and
SAT/TAT Heat Warning Systems.
|
|
Except where en route operations require
their use, two (2) may be inoperative
provided:
a) Airplane is not operated in known
or forecast icing conditions, and
b) Two inoperative static ports do not
support same Air Data System
(i.e. Pilot, Co-pilot, or Standby
system).
|
|
|
|
|
|
|
3. Static Port Heating
Systems
C
6
4
4. Pneumatic Boot Deicing
System
C
1
0
(M) May be inoperative provided:
a) Airplane is not operated in known
or forecast icing conditions, and
b) System is secured to ensure boots
will remain deflated by suction.
5. Angle of Attack Sensor
Heating System
C
1
0
May be inoperative provided airplane is
not operated in known or forecast icing
conditions.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT:
REVISION NO: 1
PAGE NO:
GULFSTREAM G150
DATE: 11/12/2008
30-2
1. SYSTEM,
REPAIR CATEGORY
SEQUENCE NUMBERS &
2. NUMBER INSTALLED
ITEM
3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
30 ICE AND RAIN
PROTECTION
6. Deicing System Timers
C
2
1
One may be inoperative provided other
timer, normal or alternate, is operative.
7. Engine Anti-Ice Systems
B
2
0
(O) May be inoperative provided airplane |
is not operated in known or forecast icing |
conditions.
|
B
2
0
(O) May be inoperative provided:
a) Affected system(s) are verified
continuously ON,
b) Takeoff and landing field
temperatures do not exceed +15
degrees C,
c) Airplane is operated in accordance
with AFM Engine Anti-ice ON
Limitations and Performance
corrections, and
d) System is selected ON in icing
conditions.
C
1
0
May be inoperative provided:
a) Both Forward Windshield Heating
Systems are operative, and
b) Both Side Window Heating
Systems are operative.
8. Cockpit Defog System
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U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT:
REVISION NO: 1
PAGE NO:
GULFSTREAM G150
DATE: 11/12/2008
30-3
1. SYSTEM,
REPAIR CATEGORY
SEQUENCE NUMBERS &
2. NUMBER INSTALLED
ITEM
3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
30 ICE AND RAIN
PROTECTION
9. Windshield Ice Detection
Lights
C
2
1
One may be inoperative provided:
a) Both Forward Windshield Heating
Systems are operative, and
b) Windshield heat systems are
operated in accordance with AFM
procedures.
|
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|
|
|
|
|
|
|
|
|
|
C
2
0
(O) May be inoperative provided:
a) Both Forward Windshield Heating
Systems are operative,
b) Windshield heat systems are
operated in accordance with AFM
procedures, and
c) Crew uses other available light
sources to detect ice on windshield.
10. Forward Windshield
Heating Systems
C
2
1
One may be inoperative provided:
a) Windshield Defogging System is
operative,
b) Inoperative system is selected
|
OFF, and
c) Airplane is not operated in visible
|
moisture, or known or forecast icing
conditions.
1) High/Low Switches
C
2
1
One position of the switch may be
inoperative provided other position of
same switch is operative.
30 ICE AND RAIN
PROTECTION
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT:
REVISION NO: 1
PAGE NO:
GULFSTREAM G150
DATE: 11/12/2008
30-4
1. SYSTEM,
REPAIR CATEGORY
SEQUENCE NUMBERS &
2. NUMBER INSTALLED
ITEM
3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
30 ICE AND RAIN
PROTECTION
11. Side Window Heating
Systems
|
|
1) Right Side Window
Heating System
C
1
0
|
|
2) Left Side Window
Heating System
C
1
0
May be inoperative provided:
a) Windshield Defogging System is
operative,
b) Airplane is not operated in visible
moisture of any form, and
c) Airplane is not operated in known
or forecast icing conditions.
12. Windshield Surface Seal
Protection Systems
D
2
0
May be inoperative provided airplane is
not operated in precipitation within 5NM
of the airport of takeoff or intended
landing.
13. Drain Mast Heating
System
C
1
0
(O) May be inoperative provided:
a) Associated galley service basin,
ice drawer and lavatory basin are
not used,
b) Any ice or liquid is removed from
galley service drawer, and
c) Water tanks are empty.
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|
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|
|
|
|
14. Pnuematic Boot Deice
Low Pressure Warning
System
C
1
0
May be inoperative provided
a) Pneumatic Deicing System is
confirmed operative before each
departure, and
b) At least one engine is operated at
65% N1 or above whenever
Pneumatic Deicing System is on.
|
|
|
|
|
|
|
C
1
0
May be inoperative provided airplane is
not operated in known or forecast icing
conditions.
|
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|
|
|
|
|
|
|
|
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT:
REVISION NO: 1
PAGE NO:
GULFSTREAM G150
DATE: 11/12/2008
30-5
1. SYSTEM,
REPAIR CATEGORY
SEQUENCE NUMBERS &
2. NUMBER INSTALLED
ITEM
3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
30 ICE AND RAIN
PROTECTION
15. Total Air Temperature
(TAT) Probe Heating
System
B
1
0
May be inoperative provided:
a) Airplane is operated in day VMC
only,
b) Airplane is not operated in visible
moisture, and
c) Airplane is not operated in known
or forecast icing conditions.
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|
|
|
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|
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT:
REVISION NO: 1
PAGE NO:
GULFSTREAM G150
DATE: 11/12/2008
31-1
1. SYSTEM,
REPAIR CATEGORY
SEQUENCE NUMBERS &
2. NUMBER INSTALLED
ITEM
3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
31 INDICATING/
RECORDING SYSTEMS
1. Flight Hours Recorder
C
1
0
May be inoperative provided flight crew
records airplane flight time.
|
|
2. Flight Data Recorder
(FDR) System
C
-
-
Any in excess of those required by 14
CFR may be inoperative.
|
|
A
-
0
May be inoperative provided:
a) Cockpit Voice Recorder (CVR) is
operative,
b) Airplane is not dispatched from a
designated airport as listed in
operator’s MEL unless:
1) FDR failure occurs after
pushback but before takeoff, or
2) FDR repair was attempted but
was not successful.
c) In those cases where repair is
attempted but not successful,
airplane may be dispatched on a
flight or series of flights until next
designated airport where repair
must be accomplished before
dispatch, and
d) Repairs are made within three (3)
flight days.
1) FDR Recording
Parameters required by
FAR
A
-
-
May be inoperative provided:
a) Cockpit Voice Recorder (CVR) is
operative, and
b) Repairs are made within 20
calendar days.
2) FDR Recording
Parameters not required
by FAR
A
-
-
May be inoperative provided repairs are
made before the completion of the next
heavy maintenance visit.
(continued)
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|
|
|
|
|
|
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT:
REVISION NO: 1
PAGE NO:
GULFSTREAM G150
DATE: 11/12/2008
31-2
1. SYSTEM,
REPAIR CATEGORY
SEQUENCE NUMBERS &
2. NUMBER INSTALLED
ITEM
3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
31 INDICATING/
RECORDING SYSTEMS
2. Flight Data Recorder
(FDR) System
(continued)
Flight Data Recorder
(FDR) Installed for an
Operator Other Than a
Holder of an Air Carrier
or Commercial Operator
Certificate
C
-
1
Any in excess of those required by 14
CFR may be inoperative.
|
|
A
-
0
May be inoperative provided repairs are
made in accordance with 14 CFR.
|
3. Master Warning Lights
System
A
2
1
One flasher may be inoperative provided:
a) All remaining warning lights and
indications are operative, and
b) Repairs are made within two (2)
flight days.
4. Master Caution Lights
System
A
2
1
One flasher may be inoperative provided:
a) All remaining warning lights,
caution lights, and indications are
operative, and
b) Repairs are made within three (3)
flight days.
5. Clocks
C
-
1
Any in excess of those required by 14
CFR may be inoperative.
6. Security Systems
***
D
-
-
|
|
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT:
REVISION NO: 1
PAGE NO:
GULFSTREAM G150
DATE: 11/12/2008
31-3
1. SYSTEM,
REPAIR CATEGORY
SEQUENCE NUMBERS &
2. NUMBER INSTALLED
ITEM
3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
31 INDICATING/
RECORDING SYTEMS
7. Verbal Aural Warning
System
A
1
0
May be inoperative provided:
a) STALL Verbal Warning is
operative,
b) Associated warning message is
operative,
c) Associated aural tones are
operative,
d) Associated visual indications are
operative, and
e) Repairs are made within two (2)
flight days.
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|
|
|
|
|
|
|
|
|
|
NOTE: Verbal Aural Warnings are
STALL, ENGINE FIRE,
ENGINE OVERHEAT, APU FIRE,
CONFIGURATION,
CABIN ALTITUDE, GEAR.
|
|
|
|
|
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT:
REVISION NO: 1
PAGE NO:
GULFSTREAM G150
DATE: 11/12/2008
32-1
1. SYSTEM,
REPAIR CATEGORY
SEQUENCE NUMBERS &
2. NUMBER INSTALLED
ITEM
3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
32 LANDING GEAR
1. Anti-Skid System
2. Parking Brake Warning
System
B
C
1
1
0
0
(O) May be inoperative provided:
a) Appropriate AFM procedures and
performance charts are used, and
b) Take off is not made from a
contaminated runway.
(O) May be inoperative provided:
a) Crewmembers confirm operation
of Parking and Emergency Brake
before airplane is operated, and
b) Crewmembers confirm Parking
Brake is released before taxi,
takeoff and landing.
|
|
|
|
|
|
NOTE: Parking Brake is not meant to take |
the place of wheel chocks for maintaining
the airplane in its parked position.
3. Nose Wheel Steering
System
A
1
0
May be inoperative provided:
a) Airplane is towed to/from
congested areas, and
b) Repairs are made within one (1)
flight day.
NOTE: A congested area is considered
to be other airplanes or obstacles within
50 feet.
4. Rudder Pedal Steering
B
1
0
(O) May be inoperative provided:
a) All takeoff and landings are made
from left seat, and
b) Tiller Nose Wheel Steering system
is operative and Nose Wheel
Steering Switch is placed in ON.
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|
|
|
|
|
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT:
REVISION NO: 1
PAGE NO:
GULFSTREAM G150
DATE: 11/12/2008
32-2
1. SYSTEM,
REPAIR CATEGORY
SEQUENCE NUMBERS &
2. NUMBER INSTALLED
ITEM
3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
32 LANDING GEAR
5. Nose Landing Gear
(NLG) Towing Adapter
D
1
0
(M) May be inoperative, damaged or
missing provided:
a) Towing adapter is removed, and
b) Towing adapter and associated
hardware are stowed.
|
|
|
|
|
6. Wheel Despin System
D
1
0
(O)
|
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT:
REVISION NO: 1
PAGE NO:
GULFSTREAM G150
DATE: 11/12/2008
33-1
1. SYSTEM,
REPAIR CATEGORY
SEQUENCE NUMBERS &
2. NUMBER INSTALLED
ITEM
3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
33 LIGHTS
1. Cockpit/Flight Deck/
Flight Compartment and
Instrument Lighting
System
C
-
-
Individual lights may be inoperative
provided remaining lights are:
a) Sufficient to clearly illuminate all
required instruments, controls, and
other devices for which it is
provided,
b) Positioned so that direct rays are
shielded from flight crewmembers
eyes, and
c) Lighting configuration and intensity
is acceptable to flight crew.
|
2. Cabin Interior Lights
C
-
-
May be inoperative provided:
a) Cabin emergency lighting is
operative,
b) Sufficient lighting is operative for
crew to perform required duties,
and
c) Lighting configuration at dispatch
is acceptable to flight crew.
3. Passenger Notice
System (No
Smoking/Fasten Seat
Belt Signs)
B
2
1
(O) One may be inoperative and
|
associated passenger seat(s) occupied
provided:
a) Passenger Address system is
|
operative and can be clearly heard
throughout cabin during flight, and |
b) Procedures are established and
used to alert and notify
passengers when seat belts
should be fastened or smoking is
prohibited.
4. Baggage Compartment
Lighting System
(Interior/Exterior Pylon)
C
2
0
One or both lights may be inoperative
provided battery cover installation is
visually confirmed using an alternate light
source.
|
|
|
|
5. Navigation Lights
System
C
1
0
May be inoperative provided airplane is
operated day only.
|
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|
|
|
|
|
|
|
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT:
REVISION NO: 1
PAGE NO:
GULFSTREAM G150
DATE: 11/12/2008
33-2
1. SYSTEM,
REPAIR CATEGORY
SEQUENCE NUMBERS &
2. NUMBER INSTALLED
ITEM
3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
33 LIGHTS
6. Landing Lights
C
2
1
One may be inoperative for night
operations provided taxi lights are
operative.
C
2
0
Both may be inoperative for day
operations.
1) Pulse Light Function
D
1
0
May be inoperative provided both Landing
Lights are operative.
7. Taxi Lights
C
2
0
Both may be inoperative for night
operations provided both landing lights
are operative.
C
2
0
Both may be inoperative for day
operations.
C
2
0
(O) Both may be inoperative provided a
portable lamp/light of adequate capacity
for wing inspections is available for night
operations in icing conditions.
C
2
0
Both may be inoperative for day
operations.
9. Exterior Emergency
*** Lighting System
C
1
0
May be inoperative for day operations.
10. Logo Lights
***
D
2
0
11. Flashlight Charging
System
D
-
0
8. Wing Inspection Lights
Note: Flashlight requirements remain as |
per 14 CFR.
|
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT:
REVISION NO: 1
PAGE NO:
GULFSTREAM G150
DATE: 11/12/2008
33-3
1. SYSTEM,
REPAIR CATEGORY
SEQUENCE NUMBERS &
2. NUMBER INSTALLED
ITEM
3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
33 LIGHTS
12. Floor Proximity
Emergency Lighting
System
C
-
-
Individual lights may be inoperative
provided it is verified that FAA approved
minimum acceptable lighting levels
specified in one of following documents
are complied with:
a) FAA engineering approval letter,
b) FAA approved report of type
design holder,
c) Limitations and conditions of
applicable STC, or
d) FAA approved report incorporated
in Master Drawing List for
applicable STC.
|
|
|
|
NOTE: Applicable document from above
must accompany the airplane MEL.
13. Wing Tip Navigation
Light Elements
14. Tail Navigation Light
Bulbs
15. Beacon
C
10
6
Up to two (2) LED elements may be
inoperative per wing tip assembly
provided:
a) Only one (1) of the three (3)
forward (inboard) LED elements is
inoperative, and
b) Only one (1) of the two (2) aft
(outboard) LED elements is
inoperative.
C
10
0
All LED elements may be inoperative
provided airplane is not operated at night.
C
2
1
C
2
0
C
1
0
|
|
|
|
|
|
|
|
|
Both bulbs may be inoperative provided
airplane is not operated at night.
|
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT:
REVISION NO: 1
PAGE NO:
GULFSTREAM G150
DATE: 11/12/2008
33-4
1. SYSTEM,
REPAIR CATEGORY
SEQUENCE NUMBERS &
2. NUMBER INSTALLED
ITEM
3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
33 LIGHTS
16. Cockpit Dome Lights
C
2
0
May be inoperative provided:
a) Sufficient lighting is operative for
crew to perform required duties, and
b) Lighting configuration at dispatch is
acceptable to flight crew.
17. Entry Lights
C
-
0
May be inoperative provided an alternate |
means is used to illuminate entry area.
|
NOTE: An alternate means is only
required when ambient lighting does not
adequately illuminate entry area.
18. Main Entry Door Step
Boarding Lights
C
4
0
|
|
|
|
|
|
|
|
May be inoperative provided an alternate |
means is used to illuminate entry area.
|
NOTE: An alternate means is only
required when ambient lighting does not
adequately illuminate entry area.
I
I
I
19. Lavatory Lights
C
-
0
|
20. Vanity Lights
C
-
0
|
21. Reading Lights
C
-
0
22. Flashlights
D
2
1
May be inoperative, damaged or missing |
provided flashlights on board meet 14
|
CFR requirements.
|
NOTE: Flashlight used to meet dispatch
requirements does not have to be one of
the installed flashlights.
|
|
|
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT:
REVISION NO: 1
PAGE NO:
GULFSTREAM G150
DATE: 11/12/2008
34-1
1. SYSTEM,
REPAIR CATEGORY
SEQUENCE NUMBERS &
2. NUMBER INSTALLED
ITEM
3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
34 NAVIGATION
1. Non-stabilized Magnetic
Compass (Standby
Compass)
2. VMO/MMO Aural
Warning Systems
B
1
0
(O) May be inoperative provided any
combination of three (3) gyro or INS (IRU)
stabilized compass systems are
operative.
B
1
0
(O) May be inoperative provided:
a) Any combination of two (2) gyro or
INS (IRU) stabilized compass
|
systems are operative, and
b) Airplane is operated with dual
independent navigation capability
and under positive radar control by
ATC on en route portion of flight. |
B
1
0
(O) May be inoperative for flights that are |
entirely within areas of magnetic
unreliability provided at least two (2)
stabilized directional gyro systems are
installed, operative and used in
conjunction with accepted free gyro
|
navigation techniques.
B
2
1
One may be inoperative provided both
primary Mach/Airspeed Indicators are
operative.
3. Flight Information
System
4. Altitude Alerting System
|
|
|
|
|
Moved to Section 23 (Communications) |
and renamed “Airborne Flight Information |
System” in Revision 1.
|
-
-
0
May be inoperative provided it is not
required by 14 CFR.
|
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT:
REVISION NO: 1
PAGE NO:
GULFSTREAM G150
DATE: 11/12/2008
34-2
1. SYSTEM,
REPAIR CATEGORY
SEQUENCE NUMBERS &
2. NUMBER INSTALLED
ITEM
3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
34 NAVIGATION
5. Navigation Systems
(VOR/ILS, ADF)
D
-
-
Any in excess of those required by 14
CFR may be inoperative.
|
|
6. Long Range Navigation
Systems (IRS & GPS)
C
-
0
May be inoperative provided:
a) Affected system is not required for |
attitude or heading data, and
b) 14 CFR does not require system |
for operations conducted.
7. Distance Measuring
Equipment (DME)
D
-
-
Any in excess of those required by 14
CFR may be inoperative.
|
|
8. Weather Radar System
C
-
-
As required by 14 CFR.
|
9. Storm Scope
***
C
-
0
10. Radio Altimeter System
A
1
0
May be inoperative provided:
a) Approach minimums are not
dependent on its use, and
b) Repairs are made within two (2)
flight days.
NOTE: Inoperative Radio Altimeter will
affect the Ground Proximity Warning
System (GPWS) and Traffic Collision and
Avoidance System (TCAS).
11. ATC Transponders and
Automatic Altitude
Reporting System
(continued)
B
-
-
May be inoperative provided:
a) Operations do not require its use,
and
b) Before airplane is operated,
approval is obtained from ATC
facilities having jurisdiction over
the planned route of flight.
|
D
1
0
Any in excess of those required by 14
CFR may be inoperative.
|
|
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT:
REVISION NO: 1
PAGE NO:
GULFSTREAM G150
DATE: 11/12/2008
34-3
1. SYSTEM,
REPAIR CATEGORY
SEQUENCE NUMBERS &
2. NUMBER INSTALLED
ITEM
3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
34 NAVIGATION
11. ATC Transponders and
Automatic Altitude
Reporting System
(continued)
1) Elementary and
*** Enhanced Downlink
Aircraft Reportable
Parameters not Required
by 14 CFR
A
-
0
May be inoperative provided:
a) Operations do not require its use,
and
b) Repairs are made before
completion of next heavy
maintenance visit.
|
|
|
|
|
|
2) ADS-B Squitter
*** Transmissions
A
-
0
May be inoperative provided:
a) Operations do not require its use,
and
b) Repairs are made before
completion of next heavy
maintenance visit.
|
|
|
|
|
|
12. Automatic Direction
Finding Equipment
(ADF)
D
-
-
Any in excess of those required by 14
CFR may be inoperative.
|
|
13. Marker Beacon
Receivers
C
-
-
May be inoperative provided approach
minimums do not require its use.
14. Adaptive Flight Displays
(AFD) (PFD & MFD
Display Units)
C
4
3
One inboard AFD may be inoperative
provided EICAS is operative and always
displayed.
|
|
|
1) ILS/VOR Deviation
Indicator
C
4
0
May be inoperative provided approach
minimums do not require its use.
|
2) Speed Trend
C
2
0
(M) May be inoperative provided trend
information is removed from display.
|
(continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT:
REVISION NO: 1
PAGE NO:
GULFSTREAM G150
DATE: 11/12/2008
34-4
1. SYSTEM,
REPAIR CATEGORY
SEQUENCE NUMBERS &
2. NUMBER INSTALLED
ITEM
3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
34 NAVIGATION
14. Adaptive Flight Displays
(AFD) (PFD & MFD
Display Units)
(continued)
3) Mach Indicators
|
|
|
|
C
2
1
4) Accel/Decel Indication
5) DH Set
(M) One may be inoperative provided:
a) Associated Mach information is
removed from the display, and
b) Both VMO/MMO Aural Warnings
are operative.
Deleted in Revision 1.
C
2
0
|
Both may be inoperative provided
approach minimums do not require its
use.
6) Selected Heading
|
a) Heading Bug
C
4
0
b) Heading Readout
C
4
1
May be inoperative provided selected
heading readout is displayed on at least
one (1) Primary Flight Display.
|
|
|
7) Selected Course
Readout
C
2
0
May be inoperative provided navigation
does not require its use.
|
8) Bearing Indicators
C
8
2
May be inoperative provided both bearing |
indicators (#1 and #2 needles) can be
|
displayed on at least one AFD.
|
9) Groundspeed/Time to
Go
C
4
0
|
10) Elapsed Time
C
2
0
11) TAS Indications
C
4
0
(continued)
|
|
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT:
REVISION NO: 1
PAGE NO:
GULFSTREAM G150
DATE: 11/12/2008
34-5
1. SYSTEM,
REPAIR CATEGORY
SEQUENCE NUMBERS &
2. NUMBER INSTALLED
ITEM
3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
34 NAVIGATION
14. Adaptive Flight Displays
(AFD) (PFD & MFD
Display Units)
(continued)
|
|
|
|
12) Vertical Speed
Indications
C
2
1
May be inoperative for day VMC
operations only.
|
|
13) Electronic Checklist
***
C
-
0
May be inoperative provided accepted
checklist is available for use.
|
|
14) 3-D Map Display
***
C
-
0
|
|
15) Graphical Weather
***
C
-
0
|
|
16) Enhanced Map Displays
*** (geo-political, airways)
C
-
0
|
|
15. Vertical Speed
Indications (PFD)
Deleted in Revision 1. (Moved under
Adaptive Flight Displays.)
|
|
16. Multi-Function Display
(MFD)
Deleted in Revision 1. (Included in
Adaptive Flight Displays.)
|
|
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT:
REVISION NO: 1
PAGE NO:
GULFSTREAM G150
DATE: 11/12/2008
34-6
1. SYSTEM,
REPAIR CATEGORY
SEQUENCE NUMBERS &
2. NUMBER INSTALLED
ITEM
3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
34. NAVIGATION
17. Traffic Collision and
Avoidance System II
(TCAS II)
B
-
0
(M) May be inoperative provided:
a) System is deactivated and
secured, and
b) En route or approach procedures
do not require its use.
C
-
0
(M) May be inoperative provided:
|
a) It is not required by 14 CFR,
|
b) System is deactivated and
secured, and
c) En route and approach
procedures do not require its use.
1) Combined Traffic Alert
(TA) and Resolution
Advisory (RA) Dual
Display System(s)
C
2
1
May be inoperative on non-flying pilot
side provided:
a) TA and RA visual display is
operative on flying pilot side, and
b) TA and RA audio function is
operative on flying pilot side.
|
|
2) Resolution Advisory (RA)
Display System(s)
C
2
1
May be inoperative on non-flying pilot
side.
|
C
-
0
(O) May be inoperative provided:
a) Traffic Alert (TA) visual display
and audio functions are operated,
b) TA only mode is selected by crew, |
and
c) En route or approach procedures
do not require its use.
(continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT:
REVISION NO: 1
PAGE NO:
GULFSTREAM G150
DATE: 11/12/2008
34-7
1. SYSTEM,
REPAIR CATEGORY
SEQUENCE NUMBERS &
2. NUMBER INSTALLED
ITEM
3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
34 NAVIGATION
17. Traffic Collision and
Avoidance System II
(TCAS II)
(continued)
3) Traffic Alert Display
System(s)
C
-
0
(O) May be inoperative provided:
a) RA visual display and audio
functions are operative, and
b) En route or approach procedures
do not require its use.
4) Audio Functions
B
1
0
May be inoperative provided en route or
approach procedures do not require use
of TCAS.
5) Airspace Selection
Function
C
-
0
1) GPWS
A
1
0
(O) May be inoperative provided:
a) Alternate procedures are
established and used, and
b) Repairs are made within two (2)
flight days.
|
a) Modes 1-4
A
4
0
(O) May be inoperative provided:
a) Alternate procedures are
established and used, and
b) Repairs are made within two (2)
flight days.
|
|
|
|
|
|
18. Terrain Awareness and
Warning System (TAWS)
Class A TAWS
Equipment Required
(continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT:
REVISION NO: 1
PAGE NO:
GULFSTREAM G150
DATE: 11/12/2008
34-8
1. SYSTEM,
REPAIR CATEGORY
SEQUENCE NUMBERS &
2. NUMBER INSTALLED
ITEM
3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
34 NAVIGATION
18. Class A TAWS
(continued)
|
b) Test Mode
A
1
0
c) Glideslope Deviation
(Mode 5)
C
-
1
B
-
0
B
-
0
(O) May be inoperative provided alternate
procedures are established and used.
C
-
0
(O) May be inoperative provided:
a) Advisory callout not required by 14 |
CFR, and
|
b) Alternate procedures are
established and used.
B
1
0
(O) May be inoperative provided alternate
procedures are established and used.
d) Advisory Callouts
e) Windshear Mode
*** (Reactive)
May be inoperative provided:
a) GPWS is considered inoperative,
and
b) Repairs are made within two (2)
flight days.
NOTE: Operator’s alternate procedures
should include reviewing windshear
avoidance and windshear recovery
procedures.
C
(continued)
1
0
(O) May be inoperative provided:
a) Alternate procedures are
established and used, and
b) Windshear Detection and
Avoidance System (Predictive) is
operative.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT:
REVISION NO: 1
PAGE NO:
GULFSTREAM G150
DATE: 11/12/2008
34-9
1. SYSTEM,
REPAIR CATEGORY
SEQUENCE NUMBERS &
2. NUMBER INSTALLED
ITEM
3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
34 NAVIGATION
18. Class A TAWS
(continued)
|
2) Terrain System –
Forward Looking Terrain
Avoidance (FLTA) and
Premature Descent Alert
(PDA) Functions
B
1
0
3) Terrain Displays
C
-
1
B
-
0
C
1
0
1) GPWS
A
1
0
(O) May be inoperative provided:
a) Alternate procedures are
established and used, and
b) Repairs are made within two (2)
flight days.
a) Modes 1 & 3
A
2
0
(O) May be inoperative provided:
a) Alternate procedures are
established and used, and
b) Repairs are made within two (2)
flight days.
b) Test Mode
A
1
0
May be inoperative provided:
a) GPWS is considered inoperative,
and
b) Repairs are made within two (2)
flight days.
4) Runway Awareness &
*** Advisory System (RAAS)
(O) May be inoperative provided alternate
procedures are established and used.
|
Class B TAWS
Equipment Required
(continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
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AIRCRAFT:
REVISION NO: 1
PAGE NO:
GULFSTREAM G150
DATE: 11/12/2008
34-10
1. SYSTEM,
REPAIR CATEGORY
SEQUENCE NUMBERS &
2. NUMBER INSTALLED
ITEM
3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
34 NAVIGATION
18. Class B TAWS
(continued)
c) Modes 2, 4 & 5
***
C
3
0
d) Advisory Callouts
B
-
0
(O) May be inoperative provided alternate
procedures are established and used.
C
-
0
(O) May be inoperative provided:
a) Advisory callout not required by 14 |
CFR, and
|
b) Alternate procedures are
established and used.
e) Windshear Mode
*** (Reactive)
C
1
0
(O) May be inoperative provided alternate
procedures are established and used.
2) Terrain System –
Forward Looking Terrain
Avoidance (FLTA) and
Premature Descent Alert
(PDA) Functions
B
1
0
3) Terrain Displays
***
C
-
0
4) Runway Awareness &
*** Advisory System (RAAS)
C
1
0
(continued)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT:
REVISION NO: 1
PAGE NO:
GULFSTREAM G150
DATE: 11/12/2008
34-11
1. SYSTEM,
REPAIR CATEGORY
SEQUENCE NUMBERS &
2. NUMBER INSTALLED
ITEM
3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
34 NAVIGATION
18. TAWS (continued)
Class C TAWS
Equipment
1) TAWS/GPWS
***
C
1
0
(O) May be inoperative provided alternate
procedures are established and used.
NOTE: Any mode that is operative may
be used.
19. Automatic Dependent
*** Surveillance - Broadcast
(ADS-B) System
D
-
0
May be inoperative provided it is not
required by 14 CFR.
|
NOTE: If ADS-B is installed in lieu of or
as a replacement for 14 CFR required
equipment, repair category in operator’s
MEL will be the same as that of 14 CFR
required equipment.
|
|
|
|
|
1) Link and Display
*** Processor Unit (LDPU)
D
-
0
NOTE: Cockpit Display Traffic
Information (CDTI) display of data from
other airplane systems may be used.
2) Cockpit Display and
*** Traffic Information
(CDTI)
D
-
0
NOTE: ADS-B data transmissions may
continue.
3) CDTI Control Panel
***
D
-
0
May be inoperative provided:
a) Flight ID can be set, and
b) Screen display is acceptable to
flight crew.
4) Data Link Transmitter(s)
***
D
-
0
5) Data Link Receivers
***
D
-
0
|
|
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT:
REVISION NO: 1
PAGE NO:
GULFSTREAM G150
DATE: 11/12/2008
34-12
1. SYSTEM,
REPAIR CATEGORY
SEQUENCE NUMBERS &
2. NUMBER INSTALLED
ITEM
3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
34 NAVIGATION
20. Compass System Flux
Valves
C
2
1
One may be inoperative provided:
a) All reference systems are
operative (includes IRSs and/or
AHRS), and
b) Affected compass system can be
slewed to correct heading.
21. Attitude Heading and
Reference System
(AHRS)
A
2
1
(O) One may be inoperative provided:
a) Airplane is operated in VMC
conditions,
b) Standby Attitude and Standby
Compass Systems are operative,
and
c) Repairs are made within one (1)
flight day.
22. Data Loader
B
2
1
D
1
0
NOTE: Loss of a single AHRS without an
IRS installed results in loss of yaw
damper and autopilot functions. The flight
director is still available when coupled to
side with operable AHRS.
|
|
|
|
|
(O) One may be inoperative provided:
a) IRS provides Attitude Indicating
System for inoperative AHRS, and
b) Standby Attitude Indicator and
Standby Compass Systems are
operative.
|
|
|
|
|
|
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT:
REVISION NO: 1
PAGE NO:
GULFSTREAM G150
DATE: 11/12/2008
34-13
1. SYSTEM,
REPAIR CATEGORY
SEQUENCE NUMBERS &
2. NUMBER INSTALLED
ITEM
3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
34 NAVIGATION
23. Flight Management
Systems (FMS) (CDU
and Nav Computer only)
C
-
0
May be inoperative provided:
a) Affected system is not required for
IRS alignment,
b) Long Range Navigation is not
dependent on it’s use,
c) Procedures do not require its use,
and
d) Both radio tuning controls in the
curser control panels are
operative.
NOTE: Two (2) systems are required for
dispatch into MNPS or RNP-10 airspace.
1) Navigation Database
C
-
-
May be out of currency provided:
a) Current Aeronautical Charts are
used to verify Navigation fixes
before dispatch,
b) Procedures are established and
used to verify status and suitability
of Navigation Facilities used to
define route of flight, and
c) Approach Navigation Radios are
manually tuned and identified.
24. Integrated Electronic
Standby Instrument
(IESI)
C
1
0
May be inoperative provided not required |
by 14 CFR.
|
B
1
0
May be inoperative provided:
a) Operations are conducted in Day
VMC only, and
b) Operations are not conducted into
known or forecast over-the-top
conditions.
|
|
|
|
|
|
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT:
REVISION NO: 1
PAGE NO:
GULFSTREAM G150
DATE: 11/12/2008
34-14
1. SYSTEM,
REPAIR CATEGORY
SEQUENCE NUMBERS &
2. NUMBER INSTALLED
ITEM
3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
34 NAVIGATION
25. Courser Control Panels
(CCP)
B
2
1
One may be inoperative provided
corresponding Display Control Panel
(DCP) is operative.
|
|
|
B
2
1
One may be inoperative provided
corresponding Display Control Grip
(DCG) is operative.
|
|
|
B
2
1
One may be inoperative provided
corresponding Cursor Control Panel
(CCP) is operative.
|
|
|
B
2
1
One may be inoperative provided
corresponding Display Control Grip
(DCG) is operative.
|
|
|
27. Display Control Grips
(DCG)
C
2
0
Any or all functions may be inoperative
provided inoperative function is available
via other means such as the DCP, CCP,
other push to talk buttons.
|
|
|
|
28. Charts Function
***
D
-
0
May be inoperative provided current
aeronautical charts are carried onboard
and are available to flight crew.
|
|
|
1) Charts Database
C
-
0
May be out of currency provided terminal
charts for origin, destination, and
alternate airports are verified to be
current.
|
|
|
|
26. Display Control Panels
(DCP)
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT:
REVISION NO: 1
PAGE NO:
GULFSTREAM G150
DATE: 11/12/2008
34-15
1. SYSTEM,
REPAIR CATEGORY
SEQUENCE NUMBERS &
2. NUMBER INSTALLED
ITEM
3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
34 NAVIGATION
29. Enhanced Vision System
*** (EVS)
D
1
0
|
1) EVS Window Heat
D
1
0
|
2) EVS MFD Display
D
1
0
May be inoperative provided procedures
are not dependent on its use.
|
|
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT:
REVISION NO: 1
PAGE NO:
GULFSTREAM G150
DATE: 11/12/2008
35-1
1. SYSTEM,
REPAIR CATEGORY
SEQUENCE NUMBERS &
2. NUMBER INSTALLED
ITEM
3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
35 OXYGEN
1. Oxygen Blow Out Disc
C
1
0
(M) May be missing provided adequate
oxygen is available for number of people
on board including crew.
|
2. Passenger Oxygen
System
C
1
0
As required by 14 CFR.
|
3. Automatic Passenger
Oxygen Deployment
System
C
1
0
May be inoperative provided:
a) Manual deployment (Bypass
function) is operative,
b) Flight is conducted at or below
FL250, and
c) Cabin Altitude Warning System is
operative.
|
|
|
|
|
|
|
C
1
0
One or more passenger service units may
be inoperative provided:
a) Associated seats are BLOCKED
and placarded “DO NOT
OCCUPY”, and
b) Units are operative at lavatory
location.
|
|
|
|
|
|
|
4. Therapeutic Oxygen
***
C
-
-
5. Lavatory Oxygen Drop
Out Panel
C
-
0
May be inoperative provided lavatory is
BLOCKED and placarded “DO NOT
OCCUPY”.
6. Protective Breathing
*** Equipment
D
-
-
Any in excess of those required by 14
CFR may be inoperative.
7. Oxygen Service Panel
Pressure Gauge
C
-
0
(M) (O) May be inoperative provided
Oxygen Pressure Indication on EICAS is
operative and monitored.
|
|
|
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT:
REVISION NO: 1
PAGE NO:
GULFSTREAM G150
DATE: 11/12/2008
35-2
1. SYSTEM,
REPAIR CATEGORY
SEQUENCE NUMBERS &
2. NUMBER INSTALLED
ITEM
3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
35 OXYGEN
8. Passenger Oxygen ON
Warning Light
9. Oxygen Cylinder Service
Adaptor
C
1
0
(O) May be inoperative provided:
|
a) Both Automatic and Manual
|
Modes of Cabin Pressurization
Control system (CPCS) are
operative,
b) Cabin Altitude and Differential
Pressure Indicators are operative,
and
c) Cabin Altitude High Warning
|
System is operative.
C
1
0
May be inoperative provided airplane is
operated unpressurized.
D
1
0
May be inoperative, damaged or missing. |
|
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT:
REVISION NO: 1
PAGE NO:
GULFSTREAM G150
DATE: 11/12/2008
38-1
1. SYSTEM,
REPAIR CATEGORY
SEQUENCE NUMBERS &
2. NUMBER INSTALLED
ITEM
3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
38 WATER / WASTE
1. Lavatory Waste System
C
-
-
(M) Individual components may be
inoperative provided:
a) Associated components are
deactivated or isolated, and
b) Associated system components
are verified not to have leaks.
NOTE: Any portion of the system which is
operative may be used.
C
2. Potable Water Systems
C
-
-
-
-
(M) Associated lavatory system(s) may be |
|
inoperative provided:
a) Associated components are
deactivated or isolated to prevent
leaks, and
b) Lavatory Door is secured
CLOSED and placarded
“INOPERATIVE – DO NOT
ENTER”.
NOTE: These provisions are not
intended to prohibit inspections by
crewmembers.
|
|
|
(M) Individual components may be
inoperative provided:
a) Associated components are
deactivated or isolated, and
b) Associated system components
are verified not to have leaks.
|
|
|
|
|
|
NOTE: Any portion of the system which is |
|
operative may be used.
C
-
-
(M) May be inoperative provided:
a) System is drained, and
b) Procedures are established to
ensure system is not serviced.
|
|
|
|
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT:
REVISION NO: 1
PAGE NO:
GULFSTREAM G150
DATE: 11/12/2008
38-2
1. SYSTEM,
REPAIR CATEGORY
SEQUENCE NUMBERS &
2. NUMBER INSTALLED
ITEM
3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
38 WATER / WASTE
3. Lavatory External
Service Cap
C
1
0
May be inoperative or missing provided:
a) Waste valve is verified closed
before each flight, and
b) No leakage can be detected after
each servicing.
|
|
|
|
|
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT:
REVISION NO: 1
PAGE NO:
GULFSTREAM G150
DATE: 11/12/2008
45-1
1. SYSTEM,
REPAIR CATEGORY
SEQUENCE NUMBERS &
2. NUMBER INSTALLED
ITEM
3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
45 CENTRAL
MAINTENANCE
COMPUTER
1. Maintenance Diagnostic
Computer (MDC)
D
1
0
|
|
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT:
REVISION NO: 1
PAGE NO:
GULFSTREAM G150
DATE: 11/12/2008
46-1
1. SYSTEM,
REPAIR CATEGORY
SEQUENCE NUMBERS &
2. NUMBER INSTALLED
ITEM
3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
46 INFORMATION
SYSTEMS
1. Electronic Flight Bag
*** Systems (EFBs)
1) Class 3 EFBs
***
2) Data Connectivity
*** (Class 2)
3) Power Connection
*** (Class 1 & 2)
4) Mounting Device
*** (Class 2)
|
|
C
-
-
(O) May be inoperative provided alternate |
procedures are established and used.
|
NOTE: Any function, program or
document which operates normally may
be used.
|
|
|
|
|
D
-
0
May be inoperative provided procedures
do not require its use.
C
-
-
(O) May be inoperative provided alternate |
procedures are established and used.
|
D
-
0
May be inoperative provided procedures
do not require its use.
C
-
-
(O) May be inoperative provided alternate |
procedures are established and used.
|
D
-
0
May be inoperative provided procedures
do not require its use.
|
|
C
-
0
(M) (O) May be inoperative provided:
a) Associated EFB and hardware is
secured by an alternate means or
removed from airplane, and
b) Alternate procedures are
established and used.
|
|
|
|
|
|
|
|
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT:
REVISION NO: 1
PAGE NO:
GULFSTREAM G150
DATE: 11/12/2008
46-2
1. SYSTEM,
REPAIR CATEGORY
SEQUENCE NUMBERS &
2. NUMBER INSTALLED
ITEM
3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
46 INFORMATION
SYSTEMS
2. Integrated Flight
*** Information System
(IFIS) File Server Units
(FSU)
C
-
-
(O) May be inoperative provided alternate |
procedures are established and used.
|
NOTE 1: Any function, program or
document which operates normally may
be used.
|
|
|
NOTE 2: Two File Server Units are
required to meet the operational
requirements of FAA Advisory Circular
120-76A for paperless charts.
|
|
|
|
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT:
REVISION NO: ORIGINAL
PAGE NO:
GULFSTREAM G150
DATE: 12/07/2005
49-1
1. SYSTEM,
REPAIR CATEGORY
SEQUENCE NUMBERS &
2. NUMBER INSTALLED
ITEM
3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
49 AIRBORNE AUXILIARY
POWER
1. Auxiliary Power Unit
(APU)
C
1
0
(O) May be inoperative provided its use is
not required by other inoperative items.
2. APU Bleed Shutoff Valve
A
1
0
May be inoperative provided:
a) APU is operated for electrical
power only, and
b) Repairs are made within three (3)
flight days.
3. APU External Fire
Warning Horn
C
1
0
May be inoperative provided APU
operation is monitored from the cockpit.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT:
REVISION NO: 1
PAGE NO:
GULFSTREAM G150
DATE: 11/12/2008
52-1
1. SYSTEM,
REPAIR CATEGORY
SEQUENCE NUMBERS &
2. NUMBER INSTALLED
ITEM
3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
52 DOORS
1. Cabin Door Warning
System
C
1
0
May be inoperative provided:
a) Latching and LOCKING marks are
aligned,
b) Inner handle is securely LOCKED,
and
c) Pressurization is verified in Manual
Mode before departure and
remains in Manual Mode.
2. Cabin Door Assist
Handle
C
1
0
May be inoperative provided it does not
interfere with normal door operations.
3. Cabin Door Interior
Railing
C
1
0
May be inoperative provided it does not
interfere with normal door operations.
|
4. Baggage / Fuel Door
Warning System
C
1
0
EICAS message may be inoperative or
displayed provided baggage, fuel and
service compartment doors are visually
verified CLOSED, LATCHED and
LOCKED before each flight.
|
|
|
5. Keyed Locks
***
C
-
-
Except for baggage compartment door
and service compartment door locks, all
other keyed locks may be inoperative
provided associated door, compartment
or cover is verified secured before each
flight.
|
|
|
|
|
|
6. Nose Compartment
External Access Door
Hold Open Support Rods
and Attachment Points
C
2
0
(M) May be missing or inoperative
provided:
a) Door can be properly CLOSED
and latched, and
b) Rod is removed or secured for
flight.
|
|
|
|
|
|
7. Main Entry Door, Primary
Door Seal
C
1
0
(O) May be inoperative provided:
a) Primary seal does not interfere
with door operation, and
b) Airplane is operated in an
unpressurized configuration.
|
|
|
|
|
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT:
REVISION NO: 1
PAGE NO:
GULFSTREAM G150
DATE: 11/12/2008
52-2
1. SYSTEM,
REPAIR CATEGORY
SEQUENCE NUMBERS &
2. NUMBER INSTALLED
ITEM
3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
52 DOORS
8. Acoustic Seal Curtain
(Main Entry Door &
Cockpit)
D
2
0
|
|
|
9. Main Entry Door Steps
Hinged Flapper Sill
Spring
D
1
0
May be inoperative provided flight crew
|
verifies flapper sill is down in place before |
entering or exiting airplane.
|
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT:
REVISION NO: ORIGINAL
PAGE NO:
GULFSTREAM G150
DATE: 12/07/2005
71-1
1. SYSTEM,
REPAIR CATEGORY
SEQUENCE NUMBERS &
2. NUMBER INSTALLED
ITEM
3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
71 POWERPLANT
1. Automatic Power
Reserve (APR) System
C
1
0
May be inoperative provided:
a) APR is not armed, and
b) AFM takeoff limitations and
performance for APR OFF are
observed.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT:
REVISION NO: 1
PAGE NO:
GULFSTREAM G150
DATE: 11/12/2008
73-1
1. SYSTEM,
REPAIR CATEGORY
SEQUENCE NUMBERS &
2. NUMBER INSTALLED
ITEM
3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
73 ENGINE FUEL &
CONTROL
1. Fuel Flow EICAS
Indicators
B
2
1
One may be inoperative provided:
a) Associated N1 and N2 Indicating
Systems are operative,
b) Fuel Quantity Indicating Systems
are operative, and
c) Fuel Flow Indications can be
verified on the Flight Management
System (FMS).
2. Fuel Pressure Low
Warning Systems
B
2
1
(O) One may be inoperative provided:
a) Associated standby fuel pump is
operative in AUTO, and
b) Airplane is operated at or below
16,000 feet.
B
2
1
(O) One may be inoperative provided:
a) Associated standby fuel pump is
operative,
b) Airplane is operated with
associated standby fuel pump ON,
and
c) Airplane is operated at or below
16,000 feet.
3. Fuel Filter Warning
Systems
A
2
1
(M) One may be inoperative provided:
|
a) Fuel Low Pressure System for
|
affected engine is operative,
b) Fuel Flow Indications are
operative
c) Associated Filter is verified free of
clogging before each flight, and
d) Repairs are made within three (3)
flight days.
4. Fuel Used Indications
C
2
0
May be inoperative provided fuel
remaining indications are operative.
|
|
|
|
|
|
|
|
|
|
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT:
REVISION NO: ORIGINAL
PAGE NO:
GULFSTREAM G150
DATE: 12/07/2005
74-1
1. SYSTEM,
REPAIR CATEGORY
SEQUENCE NUMBERS &
2. NUMBER INSTALLED
ITEM
3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
74 IGNITION
1. Ignition “ON” Indications
C
2
1
One may be inoperative provided:
a) Automatic Ignition System is
operative during engine start, and
b) Crew monitors engine start for
normal indications.
2. Automatic Ignition
System
C
2
1
One may be inoperative provided manual
Ignition is operative.
3. Igniters
C
4
2
(O) One may be inoperative on each
engine.
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT:
REVISION NO: 1
PAGE NO:
GULFSTREAM G150
DATE: 11/12/2008
76-1
1. SYSTEM,
REPAIR CATEGORY
SEQUENCE NUMBERS &
2. NUMBER INSTALLED
ITEM
3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
76 ENGINE CONTROLS
1. Engine Synchronizer
C
2
0
|
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT:
REVISION NO: 1
PAGE NO:
GULFSTREAM G150
DATE: 11/12/2008
77-1
1. SYSTEM,
REPAIR CATEGORY
SEQUENCE NUMBERS &
2. NUMBER INSTALLED
ITEM
3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
77 ENGINE INDICATING
1. ITT Digital Indications
C
2
1
One may be inoperative provided:
a) All other engine indications are
operative, and
b) Associated analog display is
operative.
2. Engine Vibration Monitor
System
C
2
1
Indicator on one engine may be
inoperative provided all other engine
indications are operative.
|
|
|
C
2
0
Both indicators may be inoperative
provided:
a) All other engine indications are
operative, and
b) Operations are not conducted in
known or forecast icing conditions.
|
|
|
|
|
|
C
1
0
(O) May be inoperative provided alternate |
procedures are established and used.
|
3. Engine Event Recording
System
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT:
REVISION NO: 1
PAGE NO:
GULFSTREAM G150
DATE: 11/12/2008
78-1
1. SYSTEM,
REPAIR CATEGORY
SEQUENCE NUMBERS &
2. NUMBER INSTALLED
ITEM
3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
78 ENGINE EXHAUST
1. Thrust Reverser (T/R)
ARM Lights
D
2
0
One or both may be inoperative provided:
a) T/R operation is verified before
|
departure,
|
b) T/R indication in N1 display is
operative,
c) Both L T/R FAIL and R T/R FAIL |
Caution messages are operative,
and
d) Associated power lever is not
LOCKED from reverser range
before flight.
2. Thrust Reverser System
D
2
0
(M) May be inoperative provided
inoperative thrust reverser system(s) is
secured in forward thrust position.
|
|
|
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT:
REVISION NO: 1
PAGE NO:
GULFSTREAM G150
DATE: 11/12/2008
79-1
1. SYSTEM,
REPAIR CATEGORY
SEQUENCE NUMBERS &
2. NUMBER INSTALLED
ITEM
3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
79 ENGINE OIL
1. Engine Oil Level Low
Warning Systems
2. Oil Filter Warning
System
C
2
0
Deleted in Revision 1.
|
|
(M) Both may be inoperative provided:
a) Oil Low Pressure System for
affected engine is operative, and
b) Associated Filter is verified free of
clogging before each flight.
|
|
|
|
|
U.S. DEPARTMENT OF TRANSPORTATION
MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION
AIRCRAFT:
REVISION NO: ORIGINAL
PAGE NO:
GULFSTREAM G150
DATE: 12/07/2005
80-1
1. SYSTEM,
REPAIR CATEGORY
SEQUENCE NUMBERS &
2. NUMBER INSTALLED
ITEM
3. NUMBER REQUIRED FOR DISPATCH
4. REMARKS AND EXCEPTIONS
80 STARTING
1. Automatic Starter Cutout
Features
C
2
0
Both may be inoperative provided starter
is disengaged manually at 50% N2 during
engine start.