Master Minimum Equipment List

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Master Minimum Equipment List

Revision: 2

Date: 01/15/2016

** FOR 14 CFR PART 91 and 135 OPERATIONS ONLY **

GULFSTREAM

G280

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) 627-5317

FAX: (562) 627-5210

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FEDERAL AVIATION ADMINISTRATION AIRCRAFT: GULFSTREAM G280 REVISION NO: 2 DATE: 01/15/2016 PAGE NO: I TABLE OF CONTENTS

SYSTEM NO. SYSTEM PAGE NO.

-- Cover Page -

-- Table of Contents I Log of Revisions II

-- Control Page III thru VI -- Highlights of Change VII, VIII

-- Definitions IX

-- Preamble X

Section One Line Replaceable Unit (LRU) Component Relief 1-1

21 Air Conditioning 21-1 thru 21-8 22 Auto Flight 22-1 thru 22-6 23 Communications 23-1 thru 23-15 24 Electrical Power 24-1 thru 24-6 25 Equipment/Furnishings 25-1 thru 25-13 26 Fire Protection 26-1 thru 26-3 27 Flight Controls 27-1 thru 27-5

28 Fuel 28-1 thru 28-6

29 Hydraulic Power 29-1 thru 29-3 30 Ice and Rain Protection 30-1 thru 30-5 31 Indicating/Recording Systems 31-1 thru 31-4 32 Landing Gear 32-1 thru 32-2

33 Lights 33-1 thru 33-6

34 Navigation 34-1 thru 34-18

35 Oxygen 35-1 thru 35-3

36 Pneumatics 36-1, 2

38 Water/Waste 38-1, 2

45 Central Maintenance Computer 45-1 46 Information Systems 46-1, 2

49 Airborne Auxiliary Power 49-1 thru 49-3

52 Doors 52-1 thru 52-4

71 Powerplant 71-1

73 Engine Fuel & Control 73-1, 2

74 Ignition 74-1 76 Engine Controls 76-1 77 Engine Indicating 77-1 78 Engine Exhaust 78-1 79 Engine Oil 79-1 80 Starting 80-1

Section Two Crew Alerting System (CAS) Message Relief 2-1

-- Statement Page 2-2

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REVISION 1 08/15/2014 COVER, TOC, LOG of REV., CONTROL PAGE, HIGHLIGHTS OF CHANGE, DEFINITIONS

21-3, 22-1, 23-2, 23-3, 23-5, 23-6, 23-7, 23-12, 23-15, 24-3, 25-12, 27-4, 27-5, 28-3, 29-2, 29-3, 30-5, 34-13, 52-4, 73-2 Section One

REVISION 2 01/15/2016 COVER, TOC, LOG of REV., CONTROL PAGE, HIGHLIGHTS OF CHANGE, DEFINITIONS

21-3, 21-4, 22-3, 23-6, 23-8, 23-9, 23-10, 23-12, 23-15, 24-3, 24-5, 25-9, 26-1, 26-2, 27-3, 30-5, 34-2, 34-3, 34-13, 34-15, 38-1, 38-2, 46-2, 49-1, 49-2, 74-1, 77-1, 78-1 REVISION 2 01/15/2016 Section Two

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FEDERAL AVIATION ADMINISTRATION AIRCRAFT: GULFSTREAM G280 REVISION NO: 2 DATE: 01/15/2016 PAGE NO: III CONTROL PAGE

System Page No. Rev. No. Current Date

Cover Page - Revision 2 01/15/2016 Table of Contents I Revision 2 01/15/2016 Log of Revisions II Revision 2 01/15/2016 Control Page III Revision 2 01/15/2016 IV Revision 2 01/15/2016 V Revision 2 01/15/2016 VI Revision 2 01/15/2016 Highlights of Change VII Revision 2 01/15/2016 VIII Revision 2 01/15/2016 Definitions IX Revision 2 01/15/2016 Preamble X Revision 2 01/15/2016 Section One Divider 1-1 Revision 2 01/15/2016 21 21-1 Original 10/16/2012 21-2 Original 10/16/2012 21-3 Revision 2 01/15/2016 21-4 Revision 2 01/15/2016 21-5 Original 10/16/2012 21-6 Original 10/16/2012 21-7 Original 10/16/2012 21-8 Original 10/16/2012 22 22-1 Revision 1 08/15/2014 22-2 Original 10/16/2012 22-3 Revision 2 01/15/2016 22-4 Original 10/16/2012 22-5 Original 10/16/2012 22-6 Original 10/16/2012 23 23-1 Original 10/16/2012 23-2 Revision 1 08/15/2014 23-3 Revision 1 08/15/2014 23-4 Original 10/16/2012 23-5 Revision 1 08/15/2014 23-6 Revision 2 01/15/2016 23-7 Revision 1 08/15/2014 23-8 Revision 2 01/15/2016 23-9 Revision 2 01/15/2016 23-10 Revision 2 01/15/2016 23-11 Original 10/16/2012 23-12 Revision 2 01/15/2016 23-13 Original 10/16/2012 23-14 Original 10/16/2012 23-15 Revision 2 01/15/2016 24 24-1 Original 10/16/2012 24-2 Original 10/16/2012 24-3 Revision 2 01/15/2016 24-4 Original 10/16/2012

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24-6 Original 10/16/2012 25 25-1 Original 10/16/2012 25-2 Original 10/16/2012 25-3 Original 10/16/2012 25-4 Original 10/16/2012 25-5 Original 10/16/2012 25-6 Original 10/16/2012 25-7 Original 10/16/2012 25-8 Original 10/16/2012 25-9 Revision 2 01/15/2016 25-10 Original 10/16/2012 25-11 Original 10/16/2012 25-12 Revision 1 08/15/2014 25-13 Original 10/16/2012 26 26-1 Revision 2 01/15/2016 26-2 Revision 2 01/15/2016 26-3 Original 10/16/2012 27 27-1 Original 10/16/2012 27-2 Original 10/16/2012 27-3 Revision 2 01/15/2016 27-4 Revision 1 08/15/2014 27-5 Revision 1 08/15/2014 28 28-1 Original 10/16/2012 28-2 Original 10/16/2012 28-3 Revision 1 08/15/2014 28-4 Original 10/16/2012 28-5 Original 10/16/2012 28-6 Original 10/16/2012 29 29-1 Original 10/16/2012 29-2 Revision 1 08/15/2014 29-3 Revision 1 08/15/2014 30 30-1 Original 10/16/2012 30-2 Original 10/16/2012 30-3 Original 10/16/2012 30-4 Original 10/16/2012 30-5 Revision 2 01/15/2016 31 31-1 Original 10/16/2012 31-2 Original 10/16/2012 31-3 Original 10/16/2012 31-4 Original 10/16/2012 32 32-1 Original 10/16/2012 32-2 Original 10/16/2012

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FEDERAL AVIATION ADMINISTRATION AIRCRAFT: GULFSTREAM G280 REVISION NO: 2 DATE: 01/15/2016 PAGE NO: V CONTROL PAGE

System Page No. Rev. No. Current Date

33 33-1 Original 10/16/2012 33-2 Original 10/16/2012 33-3 Original 10/16/2012 33-4 Original 10/16/2012 33-5 Original 10/16/2012 33-6 Original 10/16/2012 34 34-1 Original 10/16/2012 34-2 Revision 2 01/15/2016 34-3 Revision 2 01/15/2016 34-4 Original 10/16/2012 34-5 Original 10/16/2012 34-6 Original 10/16/2012 34-7 Original 10/16/2012 34-8 Original 10/16/2012 34-9 Original 10/16/2012 34-10 Original 10/16/2012 34-11 Original 10/16/2012 34-12 Original 10/16/2012 34-13 Revision 2 01/15/2016 34-14 Original 10/16/2012 34-15 Revision 2 01/15/2016 34-16 Original 10/16/2012 34-17 Original 10/16/2012 34-18 Original 10/16/2012 35 35-1 Original 10/16/2012 35-2 Original 10/16/2012 35-3 Original 10/16/2012 36 36-1 Original 10/16/2012 36-2 Original 10/16/2012 38 38-1 Revision 2 01/15/2016 38-2 Revision 2 01/15/2016 45 45-1 Original 10/16/2012 46 46-1 Original 10/16/2012 46-2 Revision 2 01/15/2016 49 49-1 Revision 2 01/15/2016 49-2 Revision 2 01/15/2016 49-3 Original 10/16/2012 52 52-1 Original 10/16/2012 52-2 Original 10/16/2012 52-3 Original 10/16/2012 52-4 Revision 1 08/15/2014 71 71-1 Original 10/16/2012 73 73-1 Original 10/16/2012 73-2 Revision 1 08/15/2014 74 74-1 Revision 2 01/15/2016 76 76-1 Original 10/16/2012 77 77-1 Revision 2 01/15/2016 78 78-1 Revision 2 01/15/2016 79 79-1 Original 10/16/2012 80 80-1 Original 10/16/2012

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Statement Page 2-2 Revision 2 01/15/2016 Messages 2-3 Revision 2 01/15/2016 2-4 Revision 2 01/15/2016 2-5 Revision 2 01/15/2016 2-6 Revision 2 01/15/2016 2-7 Revision 2 01/15/2016 2-8 Revision 2 01/15/2016 2-9 Revision 2 01/15/2016 2-10 Revision 2 01/15/2016 2-11 Revision 2 01/15/2016 2-12 Revision 2 01/15/2016 2-13 Revision 2 01/15/2016 2-14 Revision 2 01/15/2016 2-15 Revision 2 01/15/2016 2-16 Revision 2 01/15/2016 2-17 Revision 2 01/15/2016 2-18 Revision 2 01/15/2016 2-19 Revision 2 01/15/2016 2-20 Revision 2 01/15/2016 2-21 Revision 2 01/15/2016 2-22 Revision 2 01/15/2016 2-23 Revision 2 01/15/2016 2-24 Revision 2 01/15/2016 2-25 Revision 2 01/15/2016 2-26 Revision 2 01/15/2016 2-27 Revision 2 01/15/2016 2-28 Revision 2 01/15/2016 2-29 Revision 2 01/15/2016 2-30 Revision 2 01/15/2016 2-31 Revision 2 01/15/2016 2-32 Revision 2 01/15/2016 2-33 Revision 2 01/15/2016 2-34 Revision 2 01/15/2016 2-35 Revision 2 01/15/2016 2-36 Revision 2 01/15/2016 2-37 Revision 2 01/15/2016 2-38 Revision 2 01/15/2016 2-39 Revision 2 01/15/2016 2-40 Revision 2 01/15/2016

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FEDERAL AVIATION ADMINISTRATION AIRCRAFT: GULFSTREAM G280 REVISION NO: 2 DATE: 01/15/2016 PAGE NO: VII HIGHLIGHTS of CHANGE

This is Revision 2 to the GULFSTREAM G280 Master Minimum Equipment List (MMEL). It is the result of a public Flight Operations Evaluation Board (FOEB) meeting held on 01/15/2016 which considered all proposals by Gulfstream and Gulfstream operators for inclusion in the MMEL.

FAA Policy Letters 1 through 129 have been incorporated in this revision. For a complete listing of FAA Policy Letters and Global Changes visit fsims.faa.gov. Definitions and Preamble sections now refer to applicable Policy Letters instead of quoting the Policy Letters directly. This is to allow an operator to change the Definitions and Preamble sections in its Minimum Equipment List (MEL) when the associated Policy Letters change.

ATA 21 AIR CONDITIONING

Item 10 Page 21-3, 4 Manifold Pressure Regulator Shutoff Valves (MPRSOV), corrected Post MOD call out from G25-10032 to

G25-10022. ATA 22 AUTO FLIGHT

Item 6 Page 22-3 Takeoff/Go-Around (TOGA) Buttons, added (O) procedure. ATA 23 COMMUNICATIONS

Item 11 Page 23-6 Headset Phone Jack, corrected typo.

Item 13 Page 23-8 High Frequency (HF) Communication System, updated according to PL-106.

Item 14 Page 23-9, 10 Alerting System, (Audio/Visual), revised NOTEs. Item 19 Page 23-12 Emergency Locator Transmitter (ELT), added Survival

Type ELTs and ELT Remote Switch that were inadvertently removed in previous revision.

Item 23 Page 23-15 Controller Pilot Data Link Communications (CPDLC) – corrected typo in Remarks or Exceptions.

ATA 24 ELECTRICAL POWER

Item 10 Page 24-3 60Hz AC Electrical Power System, added circuit breaker listing.

Item 11 Page 24-3 50Hz AC Electrical Power System, added circuit breaker listing.

Item 12 Page 24-5 Electrical Power System EICAS Displays, 6) APU Generator Loadmeter, added circuit breaker listing. ATA 25 EQUIPMENT/FURNISHINGS

Item 11 Page 25-9 Storage Bins/Cabin, Galley and Lavatory Storage

Compartment/Closets, removed reference to Wheelchair Accessible Lavatories per PL-104.

ATA 26 FIRE PROTECTION

Item 2 Page 26-1 APU Bleed Leak Detection, corrected typo. Changed “Lead Detector” to “Leak Detector”.

Item 5 Page 26-2 APU Fire Detection System, added circuit breaker listing. ATA 27 FLIGHT CONTROLS

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out from G25-10032 to G25-10022. ATA 34 NAVIGATION

Item 6 Page 34-2 GNSSU WAAS (Wide Area Augmentation System or SBAS – Satellite Based Augmentation System) Function, updated acronym. Changed “Space” in acronym to “Satellite” to match AFM.

Item 10 Page 34-2 Radio Altimeter System, updated NOTE.

Item 11 Page 34-3 ATC Transponders and Automatic Altitude Reporting Systems, 2) ADS-B Squitter Transmissions, updated according to PL-076.

Item 18 Page 34-13 Integrated Standby Instrument (ISI), added circuit breaker listing to RSE.

Item 23 Page 34-15 Flight Management Systems (FMS) (CDU and Nav Computer Only), changed to category B and revised NOTEs.

ATA 38 WATER/WASTE

Item 2 Page 38-1, 2 Lavatory Waste Systems, removed reference to Wheelchair Accessible Lavatories per PL-083. ATA 46 INFORMATION SYSTEMS

Item 3 Page 46-2 Integrated Management System (IMS) relief added. ATA 49 AIRBORNE AUXILIARY POWER

Item 2 Page 49-1 APU Air Inlet Door Actuator, removed Step b), incorrect CAS message and added circuit breaker listing.

Item 5 Page 49-2 APU Starter / Generator, added circuit breaker listing. ATA 74 IGNITION

Item 3 Page 74-1 Engine Ignition Systems Channels, revised to clarify wording.

ATA 77 ENGINE INDICATING

Item 2 Page 77-1 Engine Vibration Monitors, revised first proviso and added additional relief.

ATA 78 ENGINE EXHAUST

Item 1 Page 78-1 Thrust Reverser System, added NOTE. SECTION TWO

Two section MMEL authorized by PL-119. This grants relief for failure indications

presented as CAS messages on Engine Indicating and Crew Alerting Systems (EICAS), or Electronic Centralized Aircraft Monitoring (ECAM), rather than the traditional relief (Section One) for failed equipment.

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FEDERAL AVIATION ADMINISTRATION AIRCRAFT: GULFSTREAM G280 REVISION NO: 2 DATE: 01/15/2016 PAGE NO: IX DEFINITIONS

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FEDERAL AVIATION ADMINISTRATION AIRCRAFT: GULFSTREAM G280 REVISION NO: 2 DATE: 01/15/2016 PAGE NO: 1 - 1

SECTION ONE

LINE

REPLACEABLE

UNIT (LRU)

COMPONENT

RELIEF

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4. REMARKS OR EXCEPTIONS 21 AIR CONDITIONING

1. Ram Air Check Valve C 1 0 (O) May be inoperative OPEN provided: a) Airplane is operated

unpressurized, and b) Airplane is operated in

accordance with AFM Limitations.

2. 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: a) Airplane is operated

3. Manual Temperature Control Cabin

C 1 0 May be inoperative provided Automatic Temperature Control Cabin is operative.

4. Automatic Temperature Control Cockpit

C 1 0 May be inoperative provided Manual Temperature Control Cockpit is operative.

C 1 0 (O) May be inoperative provided:

a) Airplane is operated unpressurized, and

b) Airplane is operated in accordance with AFM Limitations.

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FEDERAL AVIATION ADMINISTRATION AIRCRAFT:

GULFSTREAM G280

REVISION NO: ORIGINAL DATE: 10/16/2012

PAGE NO: 21-2 1. SYSTEM,

SEQUENCE NUMBERS & ITEM

REPAIR CATEGORY

2. NUMBER INSTALLED

3. NUMBER REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS 21 AIR CONDITIONING

5. Manual Temperature Control Cockpit

C 1 0 May be inoperative provided Automatic Temperature Control Cockpit is operative.

unpressurized, and

b) Airplane is operated in accordance with AFM Limitations.

6. Air Conditioning Unit (Pack)

C 1 0 (O) May be inoperative provided airplane is operated unpressurized with the PACK switch selected OFF.

7. Cabin Pressurization Control System

1) Automatic Mode B 1 0 (O) May be inoperative provided: a) Manual Mode is operative, b) Cabin Altitude and Differential

Pressure Indicators are operative, c) Cabin Rate of Climb Indicator is

operative,

d) Autopilot is operative, and

e) Airplane is operated in accordance with AFM Limitations.

B 1 0 (O) May be inoperative provided: a) Airplane is operated

2) Manual Mode B 1 0 (O) May be inoperative provided: a) Airplane is operated

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4. REMARKS OR EXCEPTIONS 21 AIR CONDITIONING

8. Outflow Valve C 1 0 (M)(O) Except for extended over water operations, may be inoperative OPEN provided:

a) Outflow valve is secured OPEN, b) Airplane is operated

unpressurized, and c) Airplane is operated in

C 1 0 (M)(O) Except for extended over water operations, may be inoperative CLOSED provided:

a) Safety Valve is secured OPEN, b) Airplane is operated

9. Nose Cooling Fans C 2 1 May be inoperative provided AFM time limits are observed on the ground for compartment temperatures above normal.

10. Manifold Pressure Regulator Shutoff Valves (MPRSOV)

(Post MOD G25-10022)

C 2 1 (O) May be inoperative provided:

a) Alternate Pressurization System is operative,

b) Airplane is operated in icing conditions according to wing anti-ice operation with AFM single source procedures,

c) Airplane is operated in

accordance with AFM Limitations (below 26,000 ft.) when in icing conditions, and

d) Maximum cruise altitude is FL 410.

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FEDERAL AVIATION ADMINISTRATION AIRCRAFT: GULFSTREAM G280 REVISION NO: 2 DATE: 01/15/2016 PAGE NO: 21-4 1. SYSTEM,

REPAIR CATEGORY

2. NUMBER INSTALLED

10. Manifold Pressure Regulator Shutoff Valves (MPRSOV)

(cont’d)

(Pre or Post MOD G25-10022)

accordance with AFM Limitations. |

11. Pack Inlet Valve (PIV) C 1 0 (O) May be inoperative provided airplane is operated unpressurized.

NOTE: Heating and cooling will not be available with the PIV failed.

12. High Stage Valves (HSV) C 2 0 (O) May be inoperative provided: a) Airplane is operated

unpressurized,

b) Airplane is not operated in Icing Conditions, and

accordance with AFM Limitations

13. Bleed Pressure High Warning System

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4. REMARKS OR EXCEPTIONS 21 AIR CONDITIONING

14. Cabin Duct Temp HI Warning System

C 1 0 (M)(O) May be inoperative provided: a) PACK switch is selected OFF, b) Airplane is operated

unpressurized, and

c) Airplane is operated in accordance with AFM Limitations.

15. Cockpit Duct Temp HI Warning System

C 1 0 (M)(O) May be inoperative provided: a) PACK switch is selected OFF, b) Airplane is operated

unpressurized, and

c) Airplane is operated in accordance with AFM Limitations.

16. Cabin Pressurization System

B 1 0 (O) May be inoperative provided airplane is operated unpressurized.

17. Cockpit / Cabin

Temperature Indicators

D 2 0 May be inoperative provided associated Automatic or Manual Temperature Control System is operative. 18. Cabin Altitude Rate of

Climb Indication

C 1 0 _{(O) 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 the crew, and

c) Automatic and Manual Mode of Cabin Pressurization System (CPCS) is operative.

C 1 0 (O) May be inoperative provided airplane is operated unpressurized.

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FEDERAL AVIATION ADMINISTRATION AIRCRAFT:

GULFSTREAM G280

REPAIR CATEGORY

2. NUMBER INSTALLED

19. Cabin Altitude Indication C 1 0 (O) May be inoperative provided: a) Cabin Differential Pressure

Indicator is operative,

b) A Cabin Differential Pressure Chart from the AFM is used to calculate cabin altitude, and c) Calculated Cabin Altitude is

monitored during flight by crewmember.

20. Cabin Differential Pressure Indication

C 1 0 (O) May be inoperative provided: a) Cabin Altitude Indicator is

operative,

b) A Cabin Differential Pressure Chart from the AFM is used to calculate cabin differential pressure, and

c) Calculated Cabin Differential Pressure is monitored during flight by crewmember.

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4. REMARKS OR EXCEPTIONS 21 AIR CONDITIONING

21. Cabin Altitude High Warning System

B 1 0 (O) 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, c) Automatic and Manual

Pressurization Modes are operative, and

d) Cabin altitude is monitored during flight by crewmember.

B 1 0 (O) May be inoperative provided: a) Airplane is operated

22. Safety Valve C 1 0 (O) Except for extended over water operations, may be inoperative OPEN or CLOSED provided:

a) Outflow Valve is verified OPEN, b) Airplane is operated

23. Defog System C 1 0 May be inoperative provided windshield heating system is operative.

24. Defog Switch D 1 0 May be inoperative provided windshield heating system is operative.

25. HI Flow Pushbutton D 1 0

26. Air Flow “HI/LO” Switch Light

(Light Function Only)

C 1 0

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FEDERAL AVIATION ADMINISTRATION AIRCRAFT:

GULFSTREAM G280

REPAIR CATEGORY

2. NUMBER INSTALLED

3. NUMBER REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS 21 AIR CONDITIONING 27. Cabin Temperature Remote Controllers D - 0 28. Alternate Pressurization System

29. Alternate Pressurization “ALTN PRESS” Light System

C 1 0

30. Ditch Pushbutton C 1 0 May be inoperative provided the outflow valve can be controlled by Manual Cabin Pressure operation.

31. Dump Pushbutton C 1 0 May be inoperative provided the outflow valve can be controlled by Manual Cabin Pressure operation.

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4. REMARKS OR EXCEPTIONS 22 AUTO FLIGHT

1. Flight Director Systems C 2 0 May be inoperative provided approach minimums do not require its use.

2. Autopilot Computers (AP1, AP2)

A 2 1 (O) 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

FL 250,

e) Airplane is operated in

accordance with AFM Limitations for Mach Trim and Yaw Damper, and

f) Repairs are made within one (1) flight day.

NOTE: One AP is required for MNPS, RVSM, RNP and PRNAV operations.

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FEDERAL AVIATION ADMINISTRATION AIRCRAFT:

GULFSTREAM G280

REPAIR CATEGORY

2. NUMBER INSTALLED

3. NUMBER REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS 22 AUTO FLIGHT

3. Yaw Damper System C 2 1

B 2 0 May be inoperative provided airplane is operated in accordance with AFM Limitations.

4. MACH Trim C 2 1

B 2 0 May be inoperative provided airplane is operated in accordance with AFM Limitations.

5. Control Wheel Autopilot Disconnect Buttons

C 2 1 May be inoperative on the non-flying pilot’s side provided:

a) Autopilot is not used below 1,500 feet AGL, and

b) Airplane is piloted from the side with operative button when autopilot is engaged, and c) Approach minimums do not

require the use of the autopilot.

B 2 0 May be inoperative provided the autopilot is not used.

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4. REMARKS OR EXCEPTIONS 22 AUTO FLIGHT

6. Takeoff/Go-Around (TOGA) Buttons

C 2 1 (O) May be inoperative provided approach minimums do not require its use.

|

C 2 0 (O) May be inoperative provided: a) Both power levers are operated

manually for takeoff and go-around, and

b) Autopilot and Flight Director are not used below 500 feet or MDA, whichever is higher.

NOTE: Flight Director Takeoff and Go-Around Guidance are not available with both TOGA buttons inoperative.

7. Auto Throttle System C 2 0

1) Auto Throttle Disconnect Switches (on forward side of Thrust Lever Knobs)

C 2 1 May be inoperative provided Auto Throttle Engage/Disengage Switches operate normally.

C 2 0 May be inoperative provided Auto Throttle is not used.

2) Auto Throttle Engage / Disengage Switches (on the aft side of Thrust Lever knobs)

C 2 1 May be inoperative provided Auto Throttle Disconnect Switches operate normally.

C 2 0 May be inoperative provided Auto Throttle is not used.

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FEDERAL AVIATION ADMINISTRATION AIRCRAFT:

GULFSTREAM G280

REPAIR CATEGORY

2. NUMBER INSTALLED

3. NUMBER REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS 22 AUTO FLIGHT 8. Pitch Synchronization Pushbutton C 2 0 9. Alternate Autopilot Disconnect Switches

1) Pitch Trim Switch Autopilot Disconnect Function

C 2 1 May be Inoperative provided: a) Control Wheel Autopilot

Disconnect Button is operative, and

b) Auto Pilot Gang Bar Disconnect is operative.

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4. REMARKS OR EXCEPTIONS 22 AUTO FLIGHT

10. Autopilot Coupler (XFR)

1) Left Selection C 1 0 May be inoperative provided contingency planned flight time, with one engine inoperative, does not exceed one hour cruise from a suitable airport.

2) Right Selection C 1 0 May be inoperative provided contingency planned flight time, with one engine inoperative, does not exceed one hour cruise from a suitable airport.

3) Left and Right Selections

A 2 0 (O) 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

F 250,

e) Airplane is operated in accordance with AFM Limitations, and

NOTE: Each FCC provides mach trim compensation, yaw damper, autopilot, and flight director functions independent of the other FCC. Failure of the second coupler source after dispatch would result in the complete loss of these functions, and AFM Limitations apply.

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FEDERAL AVIATION ADMINISTRATION AIRCRAFT:

GULFSTREAM G280

REPAIR CATEGORY

2. NUMBER INSTALLED

3. NUMBER REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS 22 AUTO FLIGHT

11. Flight Control Panel, Altitude 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.

3) Flight Path Angle (FPA) Mode

C 1 0 May be inoperative provided flight path angle mode is considered inoperative and not used during autopilot operations.

4) 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.

12. Flight Control Panel, Lateral Guidance Modes

1) BANK Mode Selector Switch

C 1 0 May be inoperative provided autopilot operations do not require bank selection.

2) Lateral Navigation (LNAV) Mode Selector Switch

C 1 0 May be inoperative provided LNAV mode autopilot operations are not required.

3) Heading/Track

(HDG/TRK) Mode Switch

C 1 0 May be inoperative provided navigation operations do not require its use.

4) Approach (APPR) Mode Selector Switch

C 1 0 May be inoperative provided Approach Mode operations are not conducted.

13. Performance

Management Systems (Performance & TOLD)

C 2 0 May be inoperative provided current Quick Reference Handbook is

immediately available to the flight crew

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4. REMARKS OR EXCEPTIONS 23 COMMUNICATIONS

1. Communication Systems (VHF and UHF)

D - - Any in excess of those required by 14 CFR may be inoperative provided it is not powered by the Emergency AC Bus, Emergency DC Bus, Battery Bus, Battery Direct Bus, or the DC Transfer Bus and not required for Emergency Procedures.

NOTE: Comm 1 is powered by the Emergency Bus.

2. Passenger Address (PA) System

1) Passenger Configuration B 1 0 (O) May be inoperative provided:

a) Alternate, normal and emergency procedures, and/or operating restrictions are established and used, and

b) Flight attendant alerting system (audio and visual) operates normally.

NOTE: Any station function(s) that operates normally may be used.

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 operate normally may be used.

2) Lavatory Speaker C 1 0 (O) May be inoperative provided alternate procedures are established and used.

3. Cockpit Speakers C 2 0 Cockpit speakers may be inoperative provided the affected crewmember has available an operative headset.

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FEDERAL AVIATION ADMINISTRATION AIRCRAFT: GULFSTREAM G280 REVISION NO: 1 DATE: 08/15/2014 PAGE NO: 23-2 1. SYSTEM,

REPAIR CATEGORY

2. NUMBER INSTALLED

3. NUMBER REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS 23 COMMUNICATIONS

4. Flight Deck Hand Microphones HOLDER OF AN AIR CARRIER OR COMMERCIAL OPERATOR CERTIFICATE

1) Hand Held Microphones C - 0 May be inoperative provided associated boom microphone operates normally.

D - - Any in excess of those required by 14 CFR may be inoperative. OPERATOR OTHER THAN A HOLDER OF AN AIR CARRIER OR COMMERCIAL OPERATOR CERTIFICATE

1) Hand Held Microphones C - 0 May be inoperative provided associated boom microphone operates normally.

D - - Any in excess of those required by 14 CFR may be inoperative.

(29)

4. REMARKS OR EXCEPTIONS 23 COMMUNICATIONS

5. Cockpit Voice Recorder

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. 1) *** Independent Power Source C 1 0

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.

1) *** Independent Power Source C 1 0

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 applicable 14 CFR’S. 1) *** Independent Power Source C 1 0

(30)

FEDERAL AVIATION ADMINISTRATION AIRCRAFT:

GULFSTREAM G280

REPAIR CATEGORY

2. NUMBER INSTALLED

6. ***

Selective Call System (SELCAL)

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.

1) Channels C - 0 (O) May be inoperative provided alternate procedures are established and used.

7. Static Discharge Wicks 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. ***

Automatic Cabin Briefing System

D 1 0 (O) May be inoperative provided alternate procedures are established and used.

9. ***

Flight Phone Systems D - -

(31)

4. REMARKS OR EXCEPTIONS 23 COMMUNICATIONS

10. Flight Deck Headsets Earphones/Headphones HOLDER OF AN AIR CARRIER OR COMMERCIAL OPERATOR CERTIFICATE 1) Headset Earphones / Headphones

C 2 1 May be inoperative provided associated flight deck speaker operates normally.

2) Active Noise Canceling / Reduction Function

D - 0 May be inoperative provided normal audio function of the headset is operative. OPERATOR OTHER THAN A HOLDER OF AN AIR CARRIER OR COMMERCIAL OPERATOR CERTIFICATE 1) Headset Earphones / Headphones

C 2 1 May be inoperative provided associated flight deck speaker operates normally.

2) Active Noise Canceling / Reduction Function

D - 0 May be inoperative provided normal audio function of the headset is operative.

(32)

FEDERAL AVIATION ADMINISTRATION AIRCRAFT: GULFSTREAM G280 REVISION NO: 2 DATE: 01/15/2016 PAGE NO: 23-6 1. SYSTEM,

REPAIR CATEGORY

2. NUMBER INSTALLED

11. Headset Phone Jacks HOLDER OF AN AIR CARRIER OR COMMERCIAL OPERATOR CERTIFICATE

1) Headset Phone Jack C 2 1 May be inoperative provided associated flight deck speaker operates normally. |

D - - Any in excess of those required by 14 CFR may be inoperative. OPERATOR OTHER THAN A HOLDER OF AN AIR CARRIER OR COMMERCIAL OPERATOR CERTIFICATE

1) Headset Phone Jack C 2 1 May be inoperative provided associated flight deck speaker operates normally. |

D - - Any in excess of those required by regulation may be inoperative.

(33)

4. REMARKS OR EXCEPTIONS 23 COMMUNICATIONS

12. Flight Deck Boom Microphones HOLDER OF AN AIR CARRIER OR COMMERCIAL OPERATOR CERTIFICATE 1) Headset Boom Microphones

A - 0 May be inoperative provided:

a) Associated hand microphone is installed and operates normally, and

b) Repairs are made within three (3) flight days.

D - - Any in excess of those required by 14 CFR may be inoperative. OPERATOR OTHER THAN A HOLDER OF AN AIR CARRIER OR COMMERCIAL OPERATOR CERTIFICATE 1) Headset Boom Microphones

A - 0 May be inoperative provided:

a) Associated hand microphone is installed and operates normally, and

b) Repairs are made in accordance with applicable regulations.

(34)

FEDERAL AVIATION ADMINISTRATION AIRCRAFT: GULFSTREAM G280 REVISION NO: 2 DATE: 01/15/2016 PAGE NO: 23-8 1. SYSTEM,

REPAIR CATEGORY

2. NUMBER INSTALLED

13. High Frequency (HF) Communications System

C - 1 (O) May be inoperative while conducting operations that require two LRCS

provided:

a) Aircraft SATVOICE system operates normally,

b) Alternate procedures are established and used,

c) SATVOICE services are available as a LRCS over the intended route of flight, and

d) The ICAO Flight Plan is updated (as required) to notify ATC of the communications equipment status of the aircraft. | | | | | | | |

(35)

4. REMARKS OR EXCEPTIONS 23 COMMUNICATIONS 14. 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 operates normally.

NOTE: Flight deck audio alerting must always be operative.

b) ***

Flight Attendant Visual Alerting System

B 1 0 (O) May be inoperative provided: a) PA system operates normally, b) If affected visual alerting system

is used for lavatory smoke detector alerting, an alternate lavatory smoke detector alert (audio or visual) is installed and operative, and

c) Alternate procedures for contacting flight attendants are established and used.

NOTE 1: Passenger to Attendant Call System is considered Non-Essential Equipment and Furnishing (NEF).

| |

NOTE 2: Any visual alerting system

function(s) that is operative may be used. | (continued)

(36)

FEDERAL AVIATION ADMINISTRATION AIRCRAFT: GULFSTREAM G280 REVISION NO: 2 DATE: 01/15/2016 PAGE NO: 23-10 1. SYSTEM,

REPAIR CATEGORY

2. NUMBER INSTALLED

3. NUMBER REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS 23 COMMUNICATIONS 14. *** Alerting System (Audio / Visual) (continued) c) ***

Flight Attendant Audio Alerting System

B - 0 (O) May be inoperative provided: a) PA system operates normally, b) If affected audio alerting system is

used for lavatory smoke detector alerting, an alternate lavatory smoke detector alert (visual or audio) is installed and operative, and

c) Alternate procedures for contacting flight attendants are established and used.

NOTE 1: Passenger to Attendant Call System is considered Non-Essential Equipment and Furnishing (NEF).

| |

NOTE 2: Any visual alerting system

function(s) that is operative may be used. |

(37)

4. REMARKS OR EXCEPTIONS 23 COMMUNICATIONS

15. Radio Push-to-Talk (PTT) Switches

C 7 0 May be inoperative provided an operative Hand Held Microphone is available to the crewmember on the side of the failed PTT switch.

C 7 2 May be inoperative as long as there is one operative at each cockpit crew position.

NOTE: Each cockpit crew position has three radio push-to-talk buttons; one on yoke, one on side console and one on Cursor Control Device. The co-pilot has an additional PTT switch on the left horn of the yoke.

16. Seat Belt/No Smoke Cabin Chime

C - - May be inoperative provided:

a) Seat Belt/No Smoke signs are visible to all passengers, and b) A Crewmember must advise

passengers verbally to secure their seat belts and when smoking is permitted. 17. *** Satellite Communication System (SATCOM)

18. ***

Yoke Mounted Microphone Holder

C 2 0 (O) May be damaged, torn, or missing provided affected microphone is secure or removed.

(38)

FEDERAL AVIATION ADMINISTRATION AIRCRAFT: GULFSTREAM G280 REVISION NO: 2 DATE: 01/15/2016 PAGE NO: 23-12 1. SYSTEM,

REPAIR CATEGORY

2. NUMBER INSTALLED

3. NUMBER REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS 23 COMMUNICATIONS 19. Emergency Locator Transmitter (ELT) 1) ***

Survival Type ELTs D - 0 Any in excess of those required by 14 CFR may be inoperative or missing.

| |

2) Fixed ELT A 1 0 (M) May be inoperative provided: a) System is deactivated, and b) Repairs are made within 90 days.

A 1 0 May be missing provided repairs are made within 90 days.

D - - (M) Any in excess of those required by 14 CFR may be inoperative provided system is deactivated.

D - - Any in excess of those required by 14 CFR may be missing.

3) ELT Remote Switch C 1 0 (M) May be inoperative provided: a) Remote switch is disconnected

from the ELT, and b) ELT Switch is in ARM.

| | | |

(39)

4. REMARKS OR EXCEPTIONS 23 COMMUNICATIONS 20. *** Crewmember Interphone System(s) 1) *** Passenger Configuration a) ***

Flight Deck to Cabin, Cabin to Flight Deck Functions

B - - (O) May be inoperative provided; a) Flight deck to cabin and cabin to

flight deck interphone functions operate normally on at least fifty percent of the cabin handsets, and

b) Alternate communications procedures between the affected flight attendants station(s) are established and used.

b) ***

Cabin to Cabin Functions B - - (O) May be inoperative provided alternate communication procedures between the affected flight attendant station(s) are established and used.

B - - (O) May be inoperative provided: a) Cabin to cabin interphone

functions operate normally on at least fifty percent of the cabin handsets, and

b) Alternate communications procedures between the affected flight attendants stations are established and used.

NOTE: Any station function(s) that operates normally may be used. (continued)

(40)

FEDERAL AVIATION ADMINISTRATION AIRCRAFT:

GULFSTREAM G280

REPAIR CATEGORY

2. NUMBER INSTALLED

3. NUMBER REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS 23 COMMUNICATIONS 20. *** Crewmember Interphone System(s) (continued) 1) *** Passenger Configuration (continued) c) ***

Flight Deck to Ground Functions

1) All Other Aircraft / Operations

21. *** Handset System(s) 1) *** Passenger Configuration a) ***

Flight Deck C - 0 (O) May be inoperative provided: a) Flight deck to cabin

communication operates normally, and

b) Alternate procedures are established and used.

b) ***

Cabin B - 0 (O) May be inoperative provided: a) Fifty percent of cabin handsets

operate normally, and b) Alternate communications

procedures between the affected flight attendants station(s) are established and used.

(41)

4. REMARKS OR EXCEPTIONS 23 COMMUNICATIONS 21. *** Handset System(s) (continued) 1) *** Passenger Configuration (continued) b) *** Cabin (continued)

NOTE 1: An operative handset at an inoperative flight attendant seat shall not be counted to satisfy the fifty percent requirement.

NOTE 2: Any handset(s) function(s) that operates normally may be used.

22. ***

Datalink System C 1 0 (O) May be inoperative provided alternate procedures are established and used.

D 1 0 May be inoperative provided routine procedures do not require its use.

23. ***

Controller Pilot Data Link Communications (CPDLC) 1) *** ATN B1 (PM-CPDLC/Link 2000+)

D 1 0 (O) May be inoperative provided en route operations do not require its use.

| | 2) *** FANS 1/A (ADS-C/CPDLC)

D 1 0 (O) May be inoperative provided en route operations do not require its use.

(42)

FEDERAL AVIATION ADMINISTRATION AIRCRAFT:

GULFSTREAM G280

REPAIR CATEGORY

2. NUMBER INSTALLED

3. NUMBER REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS 24 ELECTRICAL POWER

1. Left Battery B 1 0 (O) May be inoperative provided: a) Both generators are operative, b) APU is kept operating with its

generator selected ON throughout the flight,

c) Airplane is operated at or below FL 400,

d) A ground power unit is used for APU starts, and

e) Left battery is selected OFF.

NOTE 1: If APU S/G is loaded, observe altitude and electrical load limitations. NOTE 2: L BATT Switch OFF message

is displayed.

2. Left Battery Temperature Indication

C 1 0 (O) May be inoperative provided: a) Both generators are operative, b) APU generator is operative, c) A ground power unit is used for

APU starts,

d) Left battery is selected OFF, and e) L BATT Switch OFF message is

displayed.

NOTE: Observe during flight Left Battery voltage (28.5 ±0.5Vand current about 0A).

3. Right Battery

Temperature Indication

C 1 0 (O) May be inoperative provided: a) Both generators are operative, b) APU generator is operative, c) A ground power unit is used for

APU starts,

d) Right battery is selected OFF, and e) R BATT Switch OFF message is

displayed.

NOTE: Observe during flight Right Battery voltage (28.5 ±0.5Vand current about 0A).

(43)

4. REMARKS OR EXCEPTIONS 24 ELECTRICAL POWER

4. Left Battery Heating System

A 1 0 (O) May be inoperative provided: a) Both generators are operative, b) APU is kept operating with its

c) Airplane is operated at or below FL 400, and

d) Repairs are made within one (1) flight day.

NOTE: If APU S/G is loaded, observe altitude and electrical load limitations.

5. Right Battery Heating System

A 1 0 (O) May be inoperative provided: a) Both generators are operative, b) APU is kept operating with its

c) Airplane is operated at or below FL 400, and

d) Repairs are made within one (1) flight day.

NOTE: If APU S/G is loaded, observe altitude and electrical load limitations.

6. DC External Power System

C 1 0 (O) May be inoperative provided both batteries are operative.

7. Main Batteries Voltage Display

C 2 1 May be inoperative provided associated battery ammeter is operative.

(44)

FEDERAL AVIATION ADMINISTRATION AIRCRAFT: GULFSTREAM G280 REVISION NO: 2 DATE: 01/15/2016 PAGE NO: 24-3 1. SYSTEM,

REPAIR CATEGORY

2. NUMBER INSTALLED

8. Engine Generators A 2 1 May be inoperative provided:

a) APU is kept operating with its generator selected ON throughout the flight,

b) Contingency planned flight time does not exceed one hour from a suitable airport,

c) Left and right batteries and STBY battery are operative,

d) Inoperative generator switch is left in OFF,

e) Airplane is operated at or below FL 400, and

NOTE: Observe APU altitude and electrical load limitations.

9. APU Starter/Generator C 1 0 May be inoperative provided:

a) Both Engine Driven Generators are operative, and

b) Contingency planned flight time does not exceed one hour from a suitable airport.

10. 60Hz AC Electrical Power System

D 1 0 (M) (O) May be inoperative provided affected 60 Hz (B1) circuit breaker is pulled and collared.

| 11. *** 50Hz AC Electrical Power System

D 1 0 (M) (O) May be inoperative provided affected 50 Hz (B1) circuit breaker is pulled and collared.

|

(45)

4. REMARKS OR EXCEPTIONS 24 ELECTRICAL POWER

12. Electrical Power System EICAS Displays

1) Main Generators Voltmeter

C 2 1 May be inoperative provided associated generator LOAD display is operative.

NOTE 1: Observe during flight that generator load is more than 0%,

NOTE 2: Observe on Synoptic electrical page associated main bus green color.

2) Main Generators Loadmeter

A 2 1 May be inoperative provided:

a) Associated generator voltage indications are available, b) Non affected generator and its

readout are operative,

c) Galley and Cabin Non-essential are disconnected manually in case of right generator loadmeter failure,

d) Inverter 60Hz is disconnected manually in case of left generator loadmeter failure, and

e) Repairs are made within one (1) flight day.

NOTE: Observe during flight that generator voltage is 28.5 ±0.5V.

3) Batteries Voltmeter C 2 1 May be inoperative provided associated battery ammeter indications are available.

NOTE 1: Battery Fail message is displayed.

NOTE 2: Observe during flight that affected battery current is equal or more than 0 Amps.

(continued)

(46)

FEDERAL AVIATION ADMINISTRATION AIRCRAFT: GULFSTREAM G280 REVISION NO: 2 DATE: 01/15/2016 PAGE NO: 24-5 1. SYSTEM,

REPAIR CATEGORY

2. NUMBER INSTALLED

12. Electrical Power

System EICAS Displays (continued)

4) Batteries Ammeter C 2 1 May be inoperative provided associated battery voltage indications are available.

NOTE: Observe during flight that generator voltage is 28.5 ±0.5V.

5) APU Generator Voltmeter

C 1 0 May be inoperative provided APU generator ammeter indications are available.

NOTE 1: When APU generator is connected to left or right side instead of failed engine generator:

1. Observe during flight that generator load is more than 0% and

2. Observe on Synoptic electrical page associated main bus GREEN color.

NOTE 2: When APU generator is

operated as backup observe on Synoptic electrical page Tie bus GREEN color.

6) APU Generator Loadmeter

C 1 0 May be inoperative provided:

a) Both Engine Driven Generators are operative,

b) Contingency planned flight time does not exceed one hour from a suitable airport, and

c) APU GCU (B19) circuit breaker is pulled and collared.

| 7) Ext DC Pwr Voltmeter C 1 0 8) Ext DC Pwr Loadmeter C 1 0

(47)

4. REMARKS OR EXCEPTIONS 24 ELECTRICAL POWER

13. APU GEN “ON/OFF” Switch Light

C 1 0 May be inoperative provided APU Generator operation is verified.

14. BATT “ON” Switch Light (Light Function Only)

C 2 0 May be inoperative provided battery ammeter indications are available.

15. GEN “ON/OFF” Switch Light (Light Function Only)

C 2 0

16. EXT PWR “AVAIL/ON” Switch Light (Light Function Only)

C 1 0

(48)

FEDERAL AVIATION ADMINISTRATION AIRCRAFT:

GULFSTREAM G280

REPAIR CATEGORY

2. NUMBER INSTALLED

3. NUMBER REQUIRED FOR DISPATCH 4. REMARKS OR 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 the main airplane aisle, and

c) Affected seat(s) are blocked and placarded “DO NOT OCCUPY”.

NOTE 1: A seat with an inoperative seat belt is considered inoperative.

NOTE 2: 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 to outboard seats.

1) Recline Mechanism D - - (M) May be inoperative and seat

occupied provided seat back is secured in full upright position.

D - - May be inoperative and seat occupied provided seat back is immovable in full upright position.

(49)

4. REMARKS OR EXCEPTIONS 25 EQUIPMENT/ FURNISHINGS 1. Passenger Seat(s) (continued) 2) Armrests

a) Armrests with Recline Mechanism

D - - (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) If armrest is missing, seat is secured in full upright position.

b) Armrests without Recline Mechanism

D - - May be inoperative or missing and seat occupied provided:

a) Armrest does not block an Emergency Exit, and

b) Armrest does not restrict any passenger from access to main aircraft aisle.

3) ***

Swivel Mechanism C - - (M) May be inoperative and seat occupied provided:

a) Associated seat does not block an Emergency Exit,

b) Associated seat does not restrict any passenger from access to main airplane aisle, and c) Associated seat remains in

takeoff position. (continued)

(50)

FEDERAL AVIATION ADMINISTRATION AIRCRAFT:

GULFSTREAM G280

REPAIR CATEGORY

2. NUMBER INSTALLED

3. NUMBER REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS 25 EQUIPMENT/ FURNISHINGS 1. Passenger Seat(s) (continued) 4) ***

Divan High Back Seat(s) C - - May be inoperative and seat occupied provided:

a) Associated seat does not block an Emergency Exit,

b) Associated seat does not restrict any passenger from access to main airplane aisle, and c) Associated seat remains in

takeoff position. 5) *** Divan Berthing Mechanism

C - - (M) May be inoperative and seat occupied provided associated seat is secured in takeoff position.

6) ***

Electrical / Electronic Systems / Components

C - - (M) May be inoperative and seat occupied provided associated component(s) is deactivated.

(51)

4. REMARKS OR EXCEPTIONS 25 EQUIPMENT/ FURNISHINGS 2. Emergency Medical Equipment 1) *** Automatic External Defibrillator (AED) and/or Associated Equipment

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 can not be mistaken for a fully serviceable unit, and

b) Repairs or replacements are made within one (1) flight.

D - - Any in excess of those required by 14 CFR may be incomplete, missing, or inoperative.

2) ***

Emergency Medical Kit (EMK) and/or Associated Equipment

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 can not be mistaken for a fully serviceable unit, and

(52)

FEDERAL AVIATION ADMINISTRATION AIRCRAFT:

GULFSTREAM G280

REPAIR CATEGORY

2. NUMBER INSTALLED

3. NUMBER REQUIRED FOR DISPATCH 4. REMARKS OR 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 can not be mistaken for a fully serviceable unit, and

3. Overwater Survival Equipment

D - - Any in excess of those required by 14 CFR may be inoperative or missing.

4. “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.

5. 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.

(53)

4. REMARKS OR EXCEPTIONS 25 EQUIPMENT/ FURNISHINGS 6. Pilot Seats

1) Vertical Adjustment 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.

2) Armrest(s) C - - (M) (O) May be inoperative provided: a) Armrest is secured in full up

position, and

b) Seat is acceptable to affected crewmember.

3) Recline Adjustment C - - (M) (O) May be inoperative provided: a) Seat is secured in a position

acceptable to the affected crewmember, and

b) Seat is able to move Fore-Aft on its track.

4) Lumbar Adjustment C - - May be inoperative provided the seat is acceptable to the affected crewmember. (continued)

(54)

FEDERAL AVIATION ADMINISTRATION AIRCRAFT:

GULFSTREAM G280

REPAIR CATEGORY

2. NUMBER INSTALLED

FURNISHINGS

6. Pilot Seats (continued)

5) Thigh Adjustment C - - May be inoperative provided the seat is acceptable to affected crewmember.

6) Seat Belt 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) Fore and Aft Adjustment C 2 0 (M)(O) May be inoperative provided seat is secured in a position acceptable to affected crewmember.

9) Headrests C 2 0 May be inoperative provided seat is acceptable to affected crewmember.

7. Rudder Pedal Adjustment

C - - (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.

(55)

4. REMARKS OR EXCEPTIONS 25 EQUIPMENT/ FURNISHINGS 8. *** Observer Seat

1) Primary Observer Seat (including associated equipment)

A - - May be inoperative provided:

a) A passenger seat in passenger cabin is made available to an FAA Inspector for the

performance of official duties, and b) Repairs are made within

two (2) flight days.

A - - May be inoperative provided: a) Required minimum safety

equipment (safety belt and oxygen) is available, b) Seat is acceptable to

FAA inspector for performance of official duties, and

c) Repairs are made within two (2) flight days.

NOTE 1: These provisos are intended to provide for occupancy of the above seats by an FAA inspector when the minimum safety equipment (oxygen and safety belt) is functional and the inspector determines the conditions to be acceptable.

NOTE 2: The pilot-in-command will determine if the minimum safety

equipment is functional for other persons authorized to occupy any observer seat(s).

2) ***

Observer Seat Not Required by 14 CFR (including associated equipment)

D - 0

NOTE: The pilot-in-command will determine if the minimum safety

equipment is functional for other persons authorized to occupy any observer seat(s).

(56)

FEDERAL AVIATION ADMINISTRATION AIRCRAFT: GULFSTREAM G280 REVISION NO: 2 DATE: 01/15/2016 PAGE NO: 25-9 1. SYSTEM,

REPAIR CATEGORY

2. NUMBER INSTALLED

3. NUMBER REQUIRED FOR DISPATCH 4. REMARKS OR EXCEPTIONS 25 EQUIPMENT/ FURNISHINGS 9. ***

Megaphones D - - Any in excess of those required by 14 CFR may be inoperative or missing provided:

a) Inoperative megaphone is removed from passenger cabin, b) Associated placard is removed or

obscured, and c) Required distribution is maintained. 10. ***

Crash Axe D - - Any in excess of those required by 14 CFR may be missing.

11. ***

Storage Bins/Cabin, Galley and Lavatory Storage Compartment / Closets

C - - (M) May be inoperative provided: a) Procedures are established to

secure the affected bin, compartment or closet in the closed position,

b) Affected bin, compartment or closet is prominently placarded DO NOT USE,

c) Any emergency equipment

located in affected compartment is considered inoperative, and d) Affected bin, compartment or

closet is not used for storage of any item(s) except for those permanently affixed.

| | |

NOTE: For overhead bins, if no partitions are installed, the entire overhead bin is considered inoperative.

(57)

4. REMARKS OR EXCEPTIONS 25 EQUIPMENT/ FURNISHINGS 11. *** Storage Bins/Cabin, Galley and Lavatory Storage Compartment / Closets (continued)

C - - (M)(O) May be inoperative provided: a) For non-retractable doors,

affected door is removed, b) For retractable doors, affected

door is removed or secured in the retracted (fully open) position, c) Affected bin, compartment or

closet is not used for storage of any items, except those

permanently affixed,

d) Affected bin, compartment or closet is prominently placarded DO NOT USE,

e) Procedures are established and used to alert crew members and passengers of inoperative bins, compartments or closets and f) Passengers are briefed that

affected bin, compartment or closet is not used.

NOTE 1: For overhead bins, if no partitions are installed, the entire overhead bin is considered inoperative. NOTE 2: Any emergency equipment located in the affected bin, compartment or closet (permanently affixed) is

available for use. 1)

***

Storage Compartment Key Locks

D - - (M) May be inoperative in the unlocked position provided doors can be secured by other means.

NOTE: Storage Compartment Key Locks pertain to interior key locks only.

(58)

FEDERAL AVIATION ADMINISTRATION AIRCRAFT:

GULFSTREAM G280

REPAIR CATEGORY

2. NUMBER INSTALLED

FURNISHINGS 12.

***

Galley / Cabin 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 the compartment, and

b) Procedures are established to ensure that sufficient galley/cabin waste receptacles are available to accommodate all waste that may be generated on a flight.

13. Exterior Lavatory Door Ashtray

A 1 0 May be missing or inoperative for ten (10) days. 14. *** Baggage Compartment Shelves

D - - May be removed or inoperative provided the shelves are in the down position.

15. Restraint Straps (Aft Coat Closet)

D - - May be inoperative or removed provided the shelves are not used.

16. ***

External Camera System D - 0 17. *** Emergency Vision Assurance System (EVAS)

D - 0 May be inoperative or missing.

18. Reference Eye Locator C 1 0 May be missing or damaged.

19. ***

Passenger Under Seat Stowage Drawers

C 1 0 (O) May be inoperative, missing, or have broken latches provided:

a) Drawer does not block an Emergency Exit,

b) Drawer does not restrict any passenger from access to the main airplane aisle, and c) Affected drawer is emptied,

secured and placarded “DO NOT USE”.

(59)

4. REMARKS OR EXCEPTIONS 25 EQUIPMENT/ FURNISHINGS 20. *** Cabin Management System

C 1 0 (O) May be inoperative provided alternate procedures are established and used.

1) CabinView System D 1 0

21. ***

Airplane Ladder D - 0 May be inoperative, damaged, missing or removed.

NOTE: Removal will require airplane weight and balance considerations.

22. ***

Airplane Tow Bar D - 0 May be inoperative, damaged, missing or removed.

NOTE: Removal will require airplane weight and balance considerations.

23. Non-Essential Equipment & Furnishings (NEF)

- - 0 _{May be inoperative, damaged or missing} provided that the item(s) is deferred in accordance with the NEF deferral program. The NEF program, procedures and processes are outlined in the

operator’s (insert name) Manual.

(M) and (O) procedures, if required, must be available to the flight crew and

included in the operator’s appropriate document.

NOTE: Exterior lavatory door ash trays are not NEF items.

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FEDERAL AVIATION ADMINISTRATION AIRCRAFT:

GULFSTREAM G280

REPAIR CATEGORY

2. NUMBER INSTALLED

FURNISHINGS

24. Flotation Devices D - - Any in excess of those required by 14 CFR may be inoperative. Inoperative equipment will be removed from airplane.

25. Crewmember Shoulder Harnesses

B - - Any in excess of those required by flight deck crew members (including official observer in observer’s seat) may be inoperative.

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4. REMARKS OR EXCEPTIONS 26 FIRE PROTECTION 1. Baggage Compartment 1) Baggage Compartment Smoke Detector System

C 1 0 (O) May be inoperative provided: a) Baggage compartment is not

used,

b) Internal baggage door remains CLOSED, and

2) Baggage Compartment Dump Valve

B 1 0 (O) May be inoperative provided: a) It is verified OPEN, b) Airplane is operated

3) Baggage Compartment Isolation Valve

(electrical operation)

C 1 0 (O) May be inoperative provided: a) It is verified OPEN, b) Airplane is operated

NOTE: The valve can be operated manually.

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