INTERSTATE AVIATION COMMITTEE
AVIATION REGISTER
MASTER MINIMUM EQUIPMENT LIST SUPPLEMENT
CESSNA CE-680
ORIGINAL REVISION
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Cessna 680
Revision: Original
Date:07/11/2008
This Master Minimum Equipment List (MMEL) Supplement is issued by request of the Interstate Aviation Committee Aviation Register (IACAR) at the above revision level and is recommended for approval as the basis for the preparation and approval of individual operator’s Minimum Equipment List (MEL) for airplanes of this type.
This IAC AR MMEL Supplement must only be used in conjunction with the FAA Approved MMEL at Revision Original (dated 31, August 2004).
Approved By:
Danilov R.
Chief of Branch
Interstate Aviation committee
Aviation Register
Correspondence concerning this document should be addressed to the office below:
Aviation register
Interstate Aviation Committee
Bolshaya Ordynka Str., 22/2/1
119017 Mowcow, Russia
Fax: (495) 953-34-51
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CESSNA CE-680
REVISION RECORD
REVISION No. / ISSUE DATE / INCORPORATED BY / DATEOriginal /
07/11/2008
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CE-680
CESSNA CE-680
TABLE OF CONTENTS
LIST OF EFFECTIVE PAGES
GUIDANCE FOR THE USE OF THIS SUPPLEMENT
22AUTO FLIGHT
23COMMUNICATIONS
27FLIGHT CONTROLS
30ICE AND RAIN PROTECTION
31INDICATING/RECORDING SYSTEMS
33LIGHTS
34NAVIGATION
35OXYGEN
49AIRBORNE AUXILLIARY POWER
73ENGINE FUEL AND CONTROL
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CESSNA CE-680
LIST OF EFFECTIVE PAGES
PageTitleRevisionDate
Title SheetOriginal11JULY2008
iiiApproval SheetOriginal11JULY2008
vRevision RecordOriginal11JULY2008
viiTable of ContentsOriginal11JULY2008
ixList of Effective PagesOriginal11JULY2008
xiGuidance for Use of this SupplementOriginal11JULY2008
S22-1Auto FlightOriginal11JULY2008
S23-1CommunicationsOriginal11JULY2008
S23-2Communications (cont.)Original11JULY2008
S27-1Flight ControlsOriginal11JULY2008
S30-2Ice and Rain ProtectionOriginal11JULY2008
S30-3Ice and Rain Protection (cont.)Original11JULY2008
S30-4Ice and Rain Protection (cont.)Original11JULY2008
S30-5Ice and Rain Protection (cont.)Original11JULY2008
S30-6Ice and Rain Protection (cont.)Original11JULY2008
S30-7Ice and Rain Protection (cont.)Original11JULY2008
S31-1Indicating/Recording SystemsOriginal11JULY2008
S31-2Indicating/Recording Systems (cont.)Original11JULY2008
S31-3Indicating/Recording Systems (cont.)Original11JULY2008
S31-4Indicating/Recording Systems (cont.)Original11JULY2008
S33-1LightsOriginal11JULY2008
S33-2Lights (cont.)Original11JULY2008
S34-1NavigationOriginal11JULY2008
S34-2Navigation (cont.)Original11JULY2008
S34-3Navigation (cont.)Original11JULY2008
S35-2OxygenOriginal11JULY2008
S49-2Airborne Auxillary PowerOriginal11JULY2008
S73-1Engine Fuel & Control
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CESSNA CE-680
GUIDANCE FOR USE OF THIS SUPPLEMENT
1.Aircraft Model Applicability
This Supplement is applicable to the Cessna CE-680 only.
2.This supplement is based upon the FAA approved Cessna CE-680 MMEL up to Revision Original dated 31 August 2004. Additional MMEL alleviation provided by later issues of the FAA MMEL must not be used until this IAC AR Supplement has been updated to confirm that issue as the base document.
3.The text presented in bold format within this document highlight parts of the IAC ARMMEL Supplement entry which differ from the FAA MMEL entry.
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¦ U.S. DEPARTMENT OF TRANSPORTATION ¦
¦ MASTER MINIMUM EQUIPMENT LIST ¦
¦ FEDERAL AVIATION ADMINISTRATION ¦
¦ ------¦
¦ AIRCRAFT: ¦ REVISION NO: ORIGINAL ¦ PAGE: ¦
¦ CE-680 ¦ ¦ ¦
¦ ¦ DATE: 07/11/2008 ¦ S21-1 ¦
¦ ------¦
¦ 1. ¦ 2. NUMBER INSTALLED ¦
¦ SYSTEM & ¦ ------¦
¦ SEQUENCE ITEM ¦ ¦ 3. NUMBER REQUIRED FOR DISPATCH ¦
¦ NUMBERS ¦ ¦ ------¦
¦ ------¦ ¦ ¦ 4. REMARKS OR EXCEPTIONS ¦
¦ 21 AIR CONDITIONING ¦ ¦ ¦ ¦
¦ 1. Air Cycle Machine C ¦ 1 ¦ 0 ¦ May be inoperative provided: ¦
¦ ¦ ¦ ¦ a) Flight is conducted ¦
¦ ¦ ¦ ¦ unpressurized: ¦
¦ ¦ ¦ ¦ a) CABIN PRESS MODE switches ¦
¦ ¦ ¦ ¦ set ALT SEL and AUTO, ¦
¦ ¦ ¦ ¦ b) Set Cabin Altitude ¦
¦ ¦ ¦ ¦ 14,000 feet using "A" ¦
¦ ¦ ¦ ¦ knob. ¦
¦ ¦ ¦ ¦ b) Emergency Pressurization ¦
¦ ¦ ¦ ¦ is operable, ¦
¦ ¦ ¦ ¦ c) Cabin Pressurization Source ¦
¦ ¦ ¦ ¦ Selector Switch remains OFF, ¦
¦ ¦ ¦ ¦ and ¦
¦ ¦ ¦ ¦ d) Flight is conducted at or ¦
¦ ¦ ¦ ¦ below 10,000 feet MSL. ¦
¦ ¦ ¦ ¦ NOTE: Amber CAS message CABIN ¦
¦ ¦ ¦ ¦ Altitude will illuminate when ¦
¦ ¦ ¦ ¦ Cabin Altitude exceeds 8,500 ¦
¦ ¦ ¦ ¦ feet. A Red CAS message will ¦
¦ ¦ ¦ ¦ illuminate if the Cabin ¦
¦ ¦ ¦ ¦ Altitude exceeds ¦
¦ ¦ ¦ ¦ approximately 10,000 feet. ¦
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------
¦ U.S. DEPARTMENT OF TRANSPORTATION ¦
¦ MASTER MINIMUM EQUIPMENT LIST ¦
¦ FEDERAL AVIATION ADMINISTRATION ¦
¦ ------¦
¦ AIRCRAFT: ¦ REVISION NO: ORIGINAL ¦ PAGE: ¦
¦ CE-680 ¦ ¦ ¦
¦ ¦ DATE: 07/11/2008 ¦ S21-2 ¦
¦ ------¦
¦ 1. ¦ 2. NUMBER INSTALLED ¦
¦ SYSTEM & ¦ ------¦
¦ SEQUENCE ITEM ¦ ¦ 3. NUMBER REQUIRED FOR DISPATCH ¦
¦ NUMBERS ¦ ¦ ------¦
¦ ------¦ ¦ ¦ 4. REMARKS OR EXCEPTIONS ¦
¦ 21 AIR CONDITIONING ¦ ¦ ¦ ¦
¦ 2. Mass Flow Control C ¦ 2 ¦ 1 ¦ One may be inoperative provided: ¦
¦ and Shutoff Valves ¦ ¦ ¦ a) Cabin Pressurization Source ¦
¦ ¦ ¦ ¦ Selector Switch remains on ¦
¦ ¦ ¦ ¦ the opposite source, ¦
¦ ¦ ¦ ¦ b) Flight is conducted at FL410 ¦
¦ ¦ ¦ ¦ or below(11 or less pax) or ¦
¦ ¦ ¦ ¦ at or below FL390 (12 pax), ¦
¦ ¦ ¦ ¦ and ¦
¦ ¦ ¦ ¦ c) BAGGAGE HEAT switch is ¦
¦ ¦ ¦ ¦ selected OFF. ¦
¦ C ¦ 2 ¦ 0 ¦ (M)May be inoperative provided: ¦
¦ ¦ ¦ ¦ a) Flight is conducted ¦
¦ ¦ ¦ ¦ unpressurized: ¦
¦ ¦ ¦ ¦ a) CABIN PRESS MODE switches ¦
¦ ¦ ¦ ¦ set ALT SEL and AUTO, ¦
¦ ¦ ¦ ¦ b) Set Cabin Altitude ¦
¦ ¦ ¦ ¦ 14,000 feet using "A" ¦
¦ ¦ ¦ ¦ knob. ¦
¦ ¦ ¦ ¦ b) Emergency Pressurization is ¦
¦ ¦ ¦ ¦ operable, ¦
¦ ¦ ¦ ¦ c) Cabin Pressurization Source ¦
¦ ¦ ¦ ¦ Selector remains OFF, ¦
¦ ¦ ¦ ¦ d) Both Mass Flow Control and ¦
¦ ¦ ¦ ¦ Shutoff valves are verified ¦
¦ ¦ ¦ ¦ CLOSED, and ¦
¦ ¦ ¦ ¦ e) Flight is conducted at or ¦
¦ ¦ ¦ ¦ below 10,000 feet MSL. ¦
¦ ¦ ¦ ¦ NOTE: Amber CAS message CABIN ¦
¦ ¦ ¦ ¦ Altitude will illuminate when ¦
¦ ¦ ¦ ¦ Cabin Altitude exceeds 8,500 ¦
¦ ¦ ¦ ¦ feet. A Red CAS message will ¦
¦ ¦ ¦ ¦ illuminate if the Cabin ¦
¦ ¦ ¦ ¦ Altitude exceeds ¦
¦ ¦ ¦ ¦ approximately 10,000 feet. ¦
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------
¦ U.S. DEPARTMENT OF TRANSPORTATION ¦
¦ MASTER MINIMUM EQUIPMENT LIST ¦
¦ FEDERAL AVIATION ADMINISTRATION ¦
¦ ------¦
¦ AIRCRAFT: ¦ REVISION NO: ORIGINAL ¦ PAGE: ¦
¦ CE-680 ¦ ¦ ¦
¦ ¦ DATE: 07/11/2008 ¦ S21-3 ¦
¦ ------¦
¦ 1. ¦ 2. NUMBER INSTALLED ¦
¦ SYSTEM & ¦ ------¦
¦ SEQUENCE ITEM ¦ ¦ 3. NUMBER REQUIRED FOR DISPATCH ¦
¦ NUMBERS ¦ ¦ ------¦
¦ ------¦ ¦ ¦ 4. REMARKS OR EXCEPTIONS ¦
¦ 21 AIR CONDITIONING ¦ ¦ ¦ ¦
¦ 3. Emergency C ¦ 1 ¦ 0 ¦ May be inoperative provided: ¦
¦ Pressurization ¦ ¦ ¦ a) Flight is conducted ¦
¦ Valve ¦ ¦ ¦ unpressurized: ¦
¦ ¦ ¦ ¦ a) CABIN PRESS MODE switches ¦
¦ ¦ ¦ ¦ set ALT SEL and AUTO, ¦
¦ ¦ ¦ ¦ b) Set Cabin Altitude ¦
¦ ¦ ¦ ¦ 14,000 feet using "A" ¦
¦ ¦ ¦ ¦ knob, and ¦
¦ ¦ ¦ ¦ b) Flight is conducted at or ¦
¦ ¦ ¦ ¦ below 10,000 feet MSL. ¦
¦ ¦ ¦ ¦ NOTE: Amber CAS message CABIN ¦
¦ ¦ ¦ ¦ Altitude will illuminate when ¦
¦ ¦ ¦ ¦ Cabin Altitude exceeds 8,500 ¦
¦ ¦ ¦ ¦ feet. A Red CAS message will ¦
¦ ¦ ¦ ¦ illuminate if the Cabin ¦
¦ ¦ ¦ ¦ Altitude exceeds ¦
¦ ¦ ¦ ¦ approximately 10,000 feet. ¦
¦ 4. Temperature Control ¦ ¦ ¦ ¦
¦ System (Cockpit and ¦ ¦ ¦ ¦
¦ Cabin ¦ ¦ ¦ ¦
¦ 1) Automatic C ¦ 2 ¦ 0 ¦ May be inoperative provided the ¦
¦ ¦ ¦ ¦ Air Temperature Control System is ¦
¦ ¦ ¦ ¦ operative in the Manual mode. ¦
¦ 2) Manual C ¦ 2 ¦ 0 ¦ May be inoperative provided the ¦
¦ ¦ ¦ ¦ Air Temperature Control System is ¦
¦ ¦ ¦ ¦ operative in the Automatic Mode. ¦
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¦ U.S. DEPARTMENT OF TRANSPORTATION ¦
¦ MASTER MINIMUM EQUIPMENT LIST ¦
¦ FEDERAL AVIATION ADMINISTRATION ¦
¦ ------¦
¦ AIRCRAFT: ¦ REVISION NO: ORIGINAL ¦ PAGE: ¦
¦ CE-680 ¦ ¦ ¦
¦ ¦ DATE: 07/11/2008 ¦ S21-4 ¦
¦ ------¦
¦ 1. ¦ 2. NUMBER INSTALLED ¦
¦ SYSTEM & ¦ ------¦
¦ SEQUENCE ITEM ¦ ¦ 3. NUMBER REQUIRED FOR DISPATCH ¦
¦ NUMBERS ¦ ¦ ------¦
¦ ------¦ ¦ ¦ 4. REMARKS OR EXCEPTIONS ¦
¦ 21 AIR CONDITIONING ¦ ¦ ¦ ¦
¦ 5. Cabin Pressure ¦ ¦ ¦ ¦
¦ Control System ¦ ¦ ¦ ¦
¦ 1) Automatic C ¦ 1 ¦ 0 ¦ May be inoperative provided: ¦
¦ Schedule Mode ¦ ¦ ¦ a) Altitude Select Mode is ¦
¦ ¦ ¦ ¦ operative, ¦
¦ ¦ ¦ ¦ b) Cabin Altimeter is ¦
¦ ¦ ¦ ¦ operative, ¦
¦ ¦ ¦ ¦ c) Cabin Vertical Speed ¦
¦ ¦ ¦ ¦ indicator is operative, ¦
¦ ¦ ¦ ¦ d) Cabin Differential Pressure ¦
¦ ¦ ¦ ¦ Gauge is operative, and ¦
¦ ¦ ¦ ¦ e) Aircraft is operated at or ¦
¦ ¦ ¦ ¦ below FL410. ¦
¦ 2) Altitude C ¦ 1 ¦ 0 ¦ May be inoperative provided: ¦
¦ Select Mode ¦ ¦ ¦ a) Automatic Schedule Mode is ¦
¦ ¦ ¦ ¦ operative, ¦
¦ ¦ ¦ ¦ b) Cabin Differential Pressure ¦
¦ ¦ ¦ ¦ Gauge is operative, ¦
¦ ¦ ¦ ¦ c) Cabin Altimeter is ¦
¦ ¦ ¦ ¦ operative, ¦
¦ ¦ ¦ ¦ d) Cabin Vertical Speed ¦
¦ ¦ ¦ ¦ indicator is operative, and ¦
¦ ¦ ¦ ¦ e) Aircraft is operated at or ¦
¦ ¦ ¦ ¦ below FL410. ¦
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------
¦ U.S. DEPARTMENT OF TRANSPORTATION ¦
¦ MASTER MINIMUM EQUIPMENT LIST ¦
¦ FEDERAL AVIATION ADMINISTRATION ¦
¦ ------¦
¦ AIRCRAFT: ¦ REVISION NO: ORIGINAL ¦ PAGE: ¦
¦ CE-680 ¦ ¦ ¦
¦ ¦ DATE: 07/11/2008 ¦ S21-5 ¦
¦ ------¦
¦ 1. ¦ 2. NUMBER INSTALLED ¦
¦ SYSTEM & ¦ ------¦
¦ SEQUENCE ITEM ¦ ¦ 3. NUMBER REQUIRED FOR DISPATCH ¦
¦ NUMBERS ¦ ¦ ------¦
¦ ------¦ ¦ ¦ 4. REMARKS OR EXCEPTIONS ¦
¦ 21 AIR CONDITIONING ¦ ¦ ¦ ¦
¦ 6. Outflow Valves C ¦ 2 ¦ 0 ¦ (M)(O)Both may be inoperative ¦
¦ ¦ ¦ ¦ provided: ¦
¦ ¦ ¦ ¦ a) Flight is conducted ¦
¦ ¦ ¦ ¦ unpressurized, ¦
¦ ¦ ¦ ¦ a) CABIN PRESS MODE switches ¦
¦ ¦ ¦ ¦ set ALT SEL and AUTO, ¦
¦ ¦ ¦ ¦ b) Set Cabin Altitude ¦
¦ ¦ ¦ ¦ 14,000 feet using "A" ¦
¦ ¦ ¦ ¦ knob. ¦
¦ ¦ ¦ ¦ b) Flight is conducted at or ¦
¦ ¦ ¦ ¦ below 10,000 feet MSL and ¦
¦ ¦ ¦ ¦ c) At least one valve is ¦
¦ ¦ ¦ ¦ secured OPEN. ¦
¦ ¦ ¦ ¦ NOTE: Amber CAS message CABIN ¦
¦ ¦ ¦ ¦ Altitude will illuminate when ¦
¦ ¦ ¦ ¦ Cabin Altitude exceeds 8,500 ¦
¦ ¦ ¦ ¦ feet. A Red CAS message will ¦
¦ ¦ ¦ ¦ illuminate if the Cabin ¦
¦ ¦ ¦ ¦ Altitude exceeds ¦
¦ ¦ ¦ ¦ approximately 10,000 feet. ¦
¦ 7. Cabin Differential C ¦ 1 ¦ 0 ¦ (O) May be inoperative provided: ¦
¦ Pressure Gauge ¦ ¦ ¦ a) Cabin Altimeter is ¦
¦ ¦ ¦ ¦ operative, and ¦
¦ ¦ ¦ ¦ b) A chart is provided to ¦
¦ ¦ ¦ ¦ convert Cabin Altitude to ¦
¦ ¦ ¦ ¦ Differential Pressure. ¦
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------
¦ U.S. DEPARTMENT OF TRANSPORTATION ¦
¦ MASTER MINIMUM EQUIPMENT LIST ¦
¦ FEDERAL AVIATION ADMINISTRATION ¦
¦ ------¦
¦ AIRCRAFT: ¦ REVISION NO: ORIGINAL ¦ PAGE: ¦
¦ CE-680 ¦ ¦ ¦
¦ ¦ DATE: 07/11/2008 ¦ S21-6 ¦
¦ ------¦
¦ 1. ¦ 2. NUMBER INSTALLED ¦
¦ SYSTEM & ¦ ------¦
¦ SEQUENCE ITEM ¦ ¦ 3. NUMBER REQUIRED FOR DISPATCH ¦
¦ NUMBERS ¦ ¦ ------¦
¦ ------¦ ¦ ¦ 4. REMARKS OR EXCEPTIONS ¦
¦ 21 AIR CONDITIONING ¦ ¦ ¦ ¦
¦ 8. Cabin Vertical C ¦ 1 ¦ 0 ¦ May be inoperative provided: ¦
¦ Speed Indicator ¦ ¦ ¦ a) Cabin Pressure Control ¦
¦ ¦ ¦ ¦ System is operative, and ¦
¦ ¦ ¦ ¦ b) Cabin Altimeter is ¦
¦ ¦ ¦ ¦ operative. ¦
¦ C ¦ 1 ¦ 0 ¦ May be inoperative provided: ¦
¦ ¦ ¦ ¦ a) Flight is conducted ¦
¦ ¦ ¦ ¦ unpressurized, ¦
¦ ¦ ¦ ¦ a) CABIN PRESS MODE switches ¦
¦ ¦ ¦ ¦ set ALT SEL and AUTO, ¦
¦ ¦ ¦ ¦ b) Set Cabin Altitude ¦
¦ ¦ ¦ ¦ 14,000 feet using "A" ¦
¦ ¦ ¦ ¦ knob. ¦
¦ ¦ ¦ ¦ and ¦
¦ ¦ ¦ ¦ b) Flight is conducted at or ¦
¦ ¦ ¦ ¦ below 10,000 feet MSL. ¦
¦ ¦ ¦ ¦ NOTE: Amber CAS message CABIN ¦
¦ ¦ ¦ ¦ Altitude will illuminate when ¦
¦ ¦ ¦ ¦ Cabin Altitude exceeds 8,500 ¦
¦ ¦ ¦ ¦ feet. A Red CAS message will ¦
¦ ¦ ¦ ¦ illuminate if the Cabin ¦
¦ ¦ ¦ ¦ Altitude exceeds ¦
¦ ¦ ¦ ¦ approximately 10,000 feet. ¦
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------
¦ U.S. DEPARTMENT OF TRANSPORTATION ¦
¦ MASTER MINIMUM EQUIPMENT LIST ¦
¦ FEDERAL AVIATION ADMINISTRATION ¦
¦ ------¦
¦ AIRCRAFT: ¦ REVISION NO: ORIGINAL ¦ PAGE: ¦
¦ CE-680 ¦ ¦ ¦
¦ ¦ DATE: 07/11/2008 ¦ S21-7 ¦
¦ ------¦
¦ 1. ¦ 2. NUMBER INSTALLED ¦
¦ SYSTEM & ¦ ------¦
¦ SEQUENCE ITEM ¦ ¦ 3. NUMBER REQUIRED FOR DISPATCH ¦
¦ NUMBERS ¦ ¦ ------¦
¦ ------¦ ¦ ¦ 4. REMARKS OR EXCEPTIONS ¦
¦ 21 AIR CONDITIONING ¦ ¦ ¦ ¦
¦ 9. Cabin Altimeter C ¦ 1 ¦ 0 ¦ (O) May be inoperative provided: ¦
¦ ¦ ¦ ¦ a) Cabin Differential Pressure ¦
¦ ¦ ¦ ¦ Gauge is operative, and ¦
¦ ¦ ¦ ¦ b) A chart is provided to ¦
¦ ¦ ¦ ¦ convert Differential ¦
¦ ¦ ¦ ¦ Pressure to Cabin Altitude. ¦
¦ C ¦ 1 ¦ 0 ¦ May be inoperative provided: ¦
¦ ¦ ¦ ¦ a) Flight is conducted ¦
¦ ¦ ¦ ¦ unpressurized: ¦
¦ ¦ ¦ ¦ a) CABIN PRESS MODE switches ¦
¦ ¦ ¦ ¦ set ALT SEL and AUTO, ¦
¦ ¦ ¦ ¦ b) Set Cabin Altitude ¦
¦ ¦ ¦ ¦ 14,000 feet using "A" ¦
¦ ¦ ¦ ¦ knob. ¦
¦ ¦ ¦ ¦ and ¦
¦ ¦ ¦ ¦ b) Flight is conducted at or ¦
¦ ¦ ¦ ¦ below 10,000 feet MSL. ¦
¦ ¦ ¦ ¦ NOTE: Amber CAS message CABIN ¦
¦ ¦ ¦ ¦ Altitude will illuminate when ¦
¦ ¦ ¦ ¦ Cabin Altitude exceeds 8,500 ¦
¦ ¦ ¦ ¦ feet. A Red CAS message will ¦
¦ ¦ ¦ ¦ illuminate if the Cabin ¦
¦ ¦ ¦ ¦ Altitude exceeds ¦
¦ ¦ ¦ ¦ approximately 10,000 feet. ¦
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------
¦ U.S. DEPARTMENT OF TRANSPORTATION ¦
¦ MASTER MINIMUM EQUIPMENT LIST ¦
¦ FEDERAL AVIATION ADMINISTRATION ¦
¦ ------¦
¦ AIRCRAFT: ¦ REVISION NO: ORIGINAL ¦ PAGE: ¦
¦ CE-680 ¦ ¦ ¦
¦ ¦ DATE: 07/11/2008 ¦ S21-8 ¦
¦ ------¦
¦ 1. ¦ 2. NUMBER INSTALLED ¦
¦ SYSTEM & ¦ ------¦
¦ SEQUENCE ITEM ¦ ¦ 3. NUMBER REQUIRED FOR DISPATCH ¦
¦ NUMBERS ¦ ¦ ------¦
¦ ------¦ ¦ ¦ 4. REMARKS OR EXCEPTIONS ¦
¦ 21 AIR CONDITIONING ¦ ¦ ¦ ¦
¦ 10. Cabin Dump Function C ¦ 1 ¦ 0 ¦ May be inoperative provided: ¦
¦ ¦ ¦ ¦ a) Flight is conducted ¦
¦ ¦ ¦ ¦ unpressurized: ¦
¦ ¦ ¦ ¦ a) CABIN PRESS MODE switches ¦
¦ ¦ ¦ ¦ set ALT SEL and AUTO, ¦
¦ ¦ ¦ ¦ b) Set Cabin Altitude ¦
¦ ¦ ¦ ¦ 14,000 feet using "A" ¦
¦ ¦ ¦ ¦ knob. ¦
¦ ¦ ¦ ¦ and ¦
¦ ¦ ¦ ¦ b) Flight is conducted at or ¦
¦ ¦ ¦ ¦ below 10,000 feet MSL ¦
¦ ¦ ¦ ¦ NOTE: Amber CAS message CABIN ¦
¦ ¦ ¦ ¦ Altitude will illuminate when ¦
¦ ¦ ¦ ¦ Cabin Altitude exceeds 8,500 ¦
¦ ¦ ¦ ¦ feet. A Red CAS message will ¦
¦ ¦ ¦ ¦ illuminate if the Cabin ¦
¦ ¦ ¦ ¦ Altitude exceeds ¦
¦ ¦ ¦ ¦ approximately 10,000 feet. ¦
¦ 11. Pilot Gaspers C ¦ 2 ¦ 0 ¦ ¦
¦ (WEMACS) ¦ ¦ ¦ ¦
¦ 12. DUCT O'TEMP Cockpit C ¦ 2 ¦ 1 ¦ One may be failed ON provided: ¦
¦ Amber CAS Message ¦ ¦ ¦ a) Associated Cockpit ¦
¦ ¦ ¦ ¦ Temperature Control Panel ¦
¦ ¦ ¦ ¦ Temperature Indicator is ¦
¦ ¦ ¦ ¦ operative and monitored, ¦
¦ ¦ ¦ ¦ b) Supply Air Temperature is ¦
¦ ¦ ¦ ¦ maintained below 250 degrees ¦
¦ ¦ ¦ ¦ F, and ¦
¦ ¦ ¦ ¦ c) Automatic Cockpit and Cabin ¦
¦ ¦ ¦ ¦ Temperature Control Systems ¦
¦ ¦ ¦ ¦ are operative. ¦
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------
¦ U.S. DEPARTMENT OF TRANSPORTATION ¦
¦ MASTER MINIMUM EQUIPMENT LIST ¦
¦ FEDERAL AVIATION ADMINISTRATION ¦
¦ ------¦
¦ AIRCRAFT: ¦ REVISION NO: ORIGINAL ¦ PAGE: ¦
¦ CE-680 ¦ ¦ ¦
¦ ¦ DATE: 07/11/2008 ¦ S21-9 ¦
¦ ------¦
¦ 1. ¦ 2. NUMBER INSTALLED ¦
¦ SYSTEM & ¦ ------¦
¦ SEQUENCE ITEM ¦ ¦ 3. NUMBER REQUIRED FOR DISPATCH ¦
¦ NUMBERS ¦ ¦ ------¦
¦ ------¦ ¦ ¦ 4. REMARKS OR EXCEPTIONS ¦
¦ 21 AIR CONDITIONING ¦ ¦ ¦ ¦
¦ 13. DUCT O'TEMP Cabin C ¦ 2 ¦ 1 ¦ One may be failed ON provided: ¦
¦ Amber CAS Message ¦ ¦ ¦ a) Associated Cabin ¦
¦ ¦ ¦ ¦ Temperature Control Panel ¦
¦ ¦ ¦ ¦ Temperature Indicator is ¦
¦ ¦ ¦ ¦ operative and monitored, ¦
¦ ¦ ¦ ¦ b) Supply Air Temperature is ¦
¦ ¦ ¦ ¦ maintained below 250 degrees ¦
¦ ¦ ¦ ¦ F, and ¦
¦ ¦ ¦ ¦ c) Automatic Cockpit and Cabin ¦
¦ ¦ ¦ ¦ Temperature Control Systems ¦
¦ ¦ ¦ ¦ are operative. ¦
¦ 14. Cockpit/Cabin C ¦ 2 ¦ 0 ¦ ¦
¦ Recirculation Blowers ¦ ¦ ¦ ¦
¦ 15. Cabin Door C ¦ 1 ¦ 0 ¦ May be inoperative provided the ¦
¦ Acoustic Seal ¦ ¦ ¦ acoustic seal does not interfere ¦
¦ ¦ ¦ ¦ with door operation. ¦
¦ 16. Cabin Temperature C ¦ 1 ¦ 0 ¦ (O)May be inoperative provided ¦
¦ Indicator ¦ ¦ ¦ other means are available to ¦
¦ ¦ ¦ ¦ determine cabin temperature when ¦
¦ ¦ ¦ ¦ carrying passengers. ¦
¦ C ¦ 1 ¦ 0 ¦ (O)may be inoperative provided ¦
¦ ¦ ¦ ¦ the aircraft is operated at or ¦
¦ ¦ ¦ ¦ below FL250 when carrying ¦
¦ ¦ ¦ ¦ passengers. ¦
¦ C ¦ 1 ¦ 0 ¦ May be inoperative provided no ¦
¦ ¦ ¦ ¦ passenger are carried. ¦
¦ 17. Cockpit Temperature C ¦ 1 ¦ 0 ¦ ¦
¦ Indicator ¦ ¦ ¦ ¦
¦ 18. Cabin Temperature C ¦ 1 ¦ 0 ¦ ¦
¦ Remote Controller ¦ ¦ ¦ ¦
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------
¦ U.S. DEPARTMENT OF TRANSPORTATION ¦
¦ MASTER MINIMUM EQUIPMENT LIST ¦
¦ FEDERAL AVIATION ADMINISTRATION ¦
¦ ------¦
¦ AIRCRAFT: ¦ REVISION NO: ORIGINAL ¦ PAGE: ¦
¦ CE-680 ¦ ¦ ¦
¦ ¦ DATE: 07/11/2008 ¦ S21-10 ¦
¦ ------¦
¦ 1. ¦ 2. NUMBER INSTALLED ¦
¦ SYSTEM & ¦ ------¦
¦ SEQUENCE ITEM ¦ ¦ 3. NUMBER REQUIRED FOR DISPATCH ¦
¦ NUMBERS ¦ ¦ ------¦
¦ ------¦ ¦ ¦ 4. REMARKS OR EXCEPTIONS ¦
¦ 21 AIR CONDITIONING ¦ ¦ ¦ ¦
¦ 19. Baggage Heat C ¦ 1 ¦ 0 ¦ (M)(O)May be inoperative provided: ¦
¦ System ¦ ¦ ¦ a) The Baggage Heat Valve is ¦
¦ ¦ ¦ ¦ verified CLOSED, and ¦
¦ ¦ ¦ ¦ b) The BAGGAGE HEAT switch is ¦
¦ ¦ ¦ ¦ OFF. ¦
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------
¦ U.S. DEPARTMENT OF TRANSPORTATION ¦
¦ MASTER MINIMUM EQUIPMENT LIST ¦
¦ FEDERAL AVIATION ADMINISTRATION ¦
¦ ------¦
¦ AIRCRAFT: ¦ REVISION NO: ORIGINAL ¦ PAGE: ¦
¦ CE-680 ¦ ¦ ¦
¦ ¦ DATE: 07/11/2008 ¦ S22-1 ¦
¦ ------¦
¦ 1. ¦ 2. NUMBER INSTALLED ¦
¦ SYSTEM & ¦ ------¦
¦ SEQUENCE ITEM ¦ ¦ 3. NUMBER REQUIRED FOR DISPATCH ¦
¦ NUMBERS ¦ ¦ ------¦
¦ ------¦ ¦ ¦ 4. REMARKS OR EXCEPTIONS ¦
¦ 22 AUTO FLIGHT ¦ ¦ ¦ ¦
¦ 1. Autopilot -¦- ¦- ¦ As required by Operational Rules. ¦
¦ Channels ¦ ¦ ¦¦ ¦ ¦ ¦ ¦ Note: An automatic altitude control ¦ ¦ ¦ ¦ ¦ system is required to be ¦ ¦ ¦ ¦ ¦ operative for RVSM operations. ¦
¦ 2. Yaw Damper C ¦ 2 ¦ 1 ¦ NOTE: Corresponding AP channel will ¦
¦ Channels ¦ ¦ ¦ also be inop. ¦
¦ C ¦ 2 ¦ 0 ¦ NOTE: AP will be inop. Use AP inop ¦
¦ ¦ ¦ ¦ MMEL item. ¦
¦ 3. Autopilot C ¦ 2 ¦ 1 ¦ Either the pilot's or copilot's ¦
¦ Disengage Switches ¦ ¦ ¦ control switch may be inoperative ¦
¦ (AP/TRIM/NWS ¦ ¦ ¦ provided: ¦
¦ DISC Buttons) ¦ ¦ ¦ a) The autopilot is not ¦
¦ ¦ ¦ ¦ utilized at less than ¦
¦ ¦ ¦ ¦ initial approach altitude, ¦
¦ ¦ ¦ ¦ b) NWS is verified operative, ¦
¦ ¦ ¦ ¦ c) Pitch trim is verified ¦
¦ ¦ ¦ ¦ operative,and ¦
¦ ¦ ¦ ¦ d) Flying pilot must have the ¦
¦ ¦ ¦ ¦ operative autopilot ¦
¦ ¦ ¦ ¦ disengage switch. ¦
¦ 4. Go-Around Buttons C ¦ 2 ¦ 0 ¦ Both may be inoperative provided: ¦
¦ ¦ ¦ ¦ a) Flight Director is not used ¦
¦ ¦ ¦ ¦ during a go-around, and ¦
¦ ¦ ¦ ¦ b) Autopilot must be ¦
¦ ¦ ¦ ¦ disconnected for go arounds. ¦
¦ ¦ ¦ ¦ NOTE: FMS Missed Approach Procedure ¦
¦ ¦ ¦ ¦ must be activated via the MCDU. ¦
¦ 5. Mach Trim C ¦ 1 ¦ 0 ¦ (O)May be inoperative provided ¦
¦ ¦ ¦ ¦ operations are conducted in ¦
¦ ¦ ¦ ¦ accordance with AFM procedures for ¦
¦ ¦ ¦ ¦ failed Mach trim. ¦
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¦ U.S. DEPARTMENT OF TRANSPORTATION ¦
¦ MASTER MINIMUM EQUIPMENT LIST ¦
¦ FEDERAL AVIATION ADMINISTRATION ¦
¦ ------¦
¦ AIRCRAFT: ¦ REVISION NO: ORIGINAL ¦ PAGE: ¦
¦ CE-680 ¦ ¦ ¦
¦ ¦ DATE: 07/11/2008 ¦ S22-2 ¦
¦ ------¦
¦ 1. ¦ 2. NUMBER INSTALLED ¦
¦ SYSTEM & ¦ ------¦
¦ SEQUENCE ITEM ¦ ¦ 3. NUMBER REQUIRED FOR DISPATCH ¦
¦ NUMBERS ¦ ¦ ------¦
¦ ------¦ ¦ ¦ 4. REMARKS OR EXCEPTIONS ¦
¦ 22 AUTO FLIGHT ¦ ¦ ¦ ¦
¦ 6. Flight Guidance B ¦ 1 ¦ - ¦ Individual functions except for ¦
¦ Controller ¦ ¦ ¦ ALT Selector, Heading Mode Switch, ¦
¦ ¦ ¦ ¦ and Heading Selector may be ¦
¦ ¦ ¦ ¦ inoperative provided procedures do ¦
¦ ¦ ¦ ¦ not require their use. ¦
¦ 7. Autopilot/Flight C ¦ 2 ¦ 0 ¦ ¦
¦ Director Touch ¦ ¦ ¦ ¦
¦ ControlSteering (TCS) ¦ ¦ ¦ ¦
¦ Switches ¦ ¦ ¦ ¦
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¦ U.S. DEPARTMENT OF TRANSPORTATION ¦
¦ MASTER MINIMUM EQUIPMENT LIST ¦
¦ FEDERAL AVIATION ADMINISTRATION ¦
¦ ------¦
¦ AIRCRAFT: ¦ REVISION NO: ORIGINAL ¦ PAGE: ¦
¦ CE-680 ¦ ¦ ¦
¦ ¦ DATE: 07/11/2008 ¦ S23-1 ¦
¦ ------¦
¦ 1. ¦ 2. NUMBER INSTALLED ¦
¦ SYSTEM & ¦ ------¦
¦ SEQUENCE ITEM ¦ ¦ 3. NUMBER REQUIRED FOR DISPATCH ¦
¦ NUMBERS ¦ ¦ ------¦
¦ ------¦ ¦ ¦ 4. REMARKS OR EXCEPTIONS ¦
¦ 23 COMMUNICATIONS ¦ ¦ ¦ ¦
¦ 1. Communications ¦ ¦ ¦ ¦
¦ Systems ¦ ¦ ¦ ¦
¦ 1) VHF 2 C ¦ 1 ¦ 0 ¦ ¦
¦ 2) HF B ¦ - ¦ - ¦ As required by Operational Rules.¦
¦ ¦ ¦ ¦ ¦
¦ 2. Passenger Address B ¦ 1 ¦ 0 ¦ (O)May be inoperative provided ¦
¦ System ¦ ¦ ¦ alternate normal and emergency ¦
¦ ¦ ¦ ¦ operations briefing procedures are ¦
¦ ¦ ¦ ¦ established and used. ¦
¦ C ¦ 1 ¦ 0 ¦ May be inoperative provided: ¦
¦ ¦ ¦ ¦ a) PA System is not required ¦
¦ ¦ ¦ ¦ by Operational Rules, and ¦
¦ ¦ ¦ ¦ (O) May be inoperative provided: ¦
¦ ¦ ¦ ¦ a) PA system is not required ¦
¦ ¦ ¦ ¦ by Operational Rules, and ¦
¦ ¦ ¦ ¦ b) Alternate, normal and ¦
¦ ¦ ¦ ¦ emergency operations ¦
¦ ¦ ¦ ¦ briefing procedures are ¦
¦ ¦ ¦ ¦ established and used. ¦
¦ 3. Cockpit Voice A ¦ 1 ¦ 0 ¦ May be inoperative provided: ¦
¦ Recorder (CVR) ¦ ¦ ¦ a) Flight Data Recorder is ¦
¦ System ¦ ¦ ¦ operating normally and ¦
¦ (With Flight Data ¦ ¦ ¦ b) the aircraft may be dispatched ¦
¦ Recorder installed) ¦ ¦ ¦ on a flight or series of ¦ ¦ ¦ ¦ ¦ flights until the next ¦ ¦ ¦ ¦ ¦ designated airport where ¦ ¦ ¦ ¦ ¦ repair must be accomplished ¦ ¦ ¦ ¦ ¦ prior to dispatch. ¦
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------
¦ U.S. DEPARTMENT OF TRANSPORTATION ¦
¦ MASTER MINIMUM EQUIPMENT LIST ¦
¦ FEDERAL AVIATION ADMINISTRATION ¦
¦ ------¦
¦ AIRCRAFT: ¦ REVISION NO: ORIGINAL ¦ PAGE: ¦
¦ CE-680 ¦ ¦ ¦
¦ ¦ DATE: 07/11/2008 ¦ S23-2 ¦
¦ ------¦
¦ 1. ¦ 2. NUMBER INSTALLED ¦
¦ SYSTEM & ¦ ------¦
¦ SEQUENCE ITEM ¦ ¦ 3. NUMBER REQUIRED FOR DISPATCH ¦
¦ NUMBERS ¦ ¦ ------¦
¦ ------¦ ¦ ¦ 4. REMARKS OR EXCEPTIONS ¦
¦ 23 COMMUNICATIONS ¦ ¦ ¦ ¦
¦ 4. Reserved ¦ ¦ ¦ ¦
¦ ¦ ¦ ¦ ¦
¦ 5. Boom Microphone ¦ ¦ ¦ ¦
¦ ¦ ¦ ¦ ¦
¦ 1) Cockpit Voice A ¦ - ¦ 0 ¦ May be inoperative provided the ¦
¦ Recorder ¦ ¦ ¦ aircraft may be dispatched on a ¦
¦ equipped to ¦ ¦ ¦ flight or series of flights until ¦
¦ record Boom ¦ ¦ ¦ the next designated airport where ¦
¦ Microphone per ¦ ¦ ¦ repair must be accomplished prior ¦
¦ FAR 121.359(g), ¦ ¦ ¦ to dispatch. ¦
¦ 135.151(d) or ¦ ¦ ¦ ¦
¦ 125.227(e) ¦ ¦ ¦ ¦
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------
¦ U.S. DEPARTMENT OF TRANSPORTATION ¦
¦ MASTER MINIMUM EQUIPMENT LIST ¦
¦ FEDERAL AVIATION ADMINISTRATION ¦
¦ ------¦
¦ AIRCRAFT: ¦ REVISION NO: ORIGINAL ¦ PAGE: ¦
¦ CE-680 ¦ ¦ ¦
¦ ¦ DATE: 07/11/2008 ¦ S23-3 ¦
¦ ------¦
¦ 1. ¦ 2. NUMBER INSTALLED ¦
¦ SYSTEM & ¦ ------¦
¦ SEQUENCE ITEM ¦ ¦ 3. NUMBER REQUIRED FOR DISPATCH ¦
¦ NUMBERS ¦ ¦ ------¦
¦ ------¦ ¦ ¦ 4. REMARKS OR EXCEPTIONS ¦
¦ 23 COMMUNICATIONS ¦ ¦ ¦ ¦
¦ 5. Static Wicks C ¦ 17 ¦ 13 ¦ One static wick may be missing or ¦
¦ ¦ ¦ ¦ broken from each of the following ¦
¦ ¦ ¦ ¦ areas: ¦
¦ ¦ ¦ ¦ a) Right hand wingtip or ¦
¦ ¦ ¦ ¦ aileron, ¦
¦ ¦ ¦ ¦ b) Left hand wingtip or ¦
¦ ¦ ¦ ¦ aileron, ¦
¦ ¦ ¦ ¦ c) Rudder, and ¦
¦ ¦ ¦ ¦ d) Elevators. ¦
¦ 6. Flight Phone D ¦ - ¦ 0 ¦ ¦
¦ *** ¦ ¦ ¦ ¦
¦ 7. Headsets C ¦ - ¦ 0 ¦ May be inoperative provided: ¦
¦ ¦ ¦ ¦ a) Associated Hand-Held ¦
¦ ¦ ¦ ¦ Microphone is operative, and ¦
¦ ¦ ¦ ¦ b) Cockpit Specakers are ¦
¦ ¦ ¦ ¦ operative. ¦
¦ 8. Recorded Passenger D ¦ - ¦ 0 ¦ (O) May be inoperative provided ¦
¦ Briefing System ¦ ¦ ¦ alternate procedures are used for ¦
¦ ¦ ¦ ¦ passenger briefings. ¦
¦ 9. Selective Call C ¦ - ¦ 0 ¦ May be inoperative provided ¦
¦ System (SELCAL) ¦ ¦ ¦ procedures do not require its use. ¦
¦ ¦ ¦ ¦ its use, ¦
¦ C ¦ - ¦ 0 ¦ May be inoperative provided flight ¦
¦ ¦ ¦ ¦ crew monitors HF or VHF frequency. ¦
¦ 10. Flight Deck Speaker C ¦ 2 ¦ 0 ¦ May be inoperative provided: ¦
¦ System ¦ ¦ ¦ a) Procedures do not require ¦
¦ ¦ ¦ ¦ its use, and ¦
¦ ¦ ¦ ¦ b) Headsets are installed, ¦
¦ ¦ ¦ ¦ operational and used. ¦
¦ 11. Hand-Held C ¦ - ¦ 0 ¦ May be inoperative provided the ¦
¦ Microphone(s) ¦ ¦ ¦ associated Headset Microphone ¦
¦ ¦ ¦ ¦ is operative. ¦
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------
¦ U.S. DEPARTMENT OF TRANSPORTATION ¦
¦ MASTER MINIMUM EQUIPMENT LIST ¦
¦ FEDERAL AVIATION ADMINISTRATION ¦
¦ ------¦
¦ AIRCRAFT: ¦ REVISION NO: ORIGINAL ¦ PAGE: ¦
¦ CE-680 ¦ ¦ ¦
¦ ¦ DATE: 07/11/2008 ¦ S23-4 ¦
¦ ------¦
¦ 1. ¦ 2. NUMBER INSTALLED ¦
¦ SYSTEM & ¦ ------¦
¦ SEQUENCE ITEM ¦ ¦ 3. NUMBER REQUIRED FOR DISPATCH ¦
¦ NUMBERS ¦ ¦ ------¦
¦ ------¦ ¦ ¦ 4. REMARKS OR EXCEPTIONS ¦
¦ 23 COMMUNICATIONS ¦ ¦ ¦ ¦
¦ 12. Datalink C ¦ - ¦ - ¦ May be inoperative provided ¦
¦ *** ¦ ¦ ¦ procedures do not require its use. ¦
¦ 13. SATCOM D ¦ - ¦ - ¦ May be inoperative provided ¦
¦ ¦ ¦ ¦ procedures do not require its use. ¦
¦ 14. Push-to-Talk (PTT) ¦ ¦ ¦ ¦
¦ Switches ¦ ¦ ¦ ¦
¦ 1)Side Panel PTT C ¦ 2 ¦ 0 ¦ May be inoperative provided ¦
¦ Switches ¦ ¦ ¦ associated Yoke PTT switch ¦
¦ ¦ ¦ ¦ operates normally. ¦
¦ 2)Yoke PTT C ¦ 2 ¦ 0 ¦ May be inoperative provided ¦
¦ Switches ¦ ¦ ¦ associated Side Panel PTT Switch ¦
¦ ¦ ¦ ¦ operates normally. ¦
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------
¦ U.S. DEPARTMENT OF TRANSPORTATION ¦
¦ MASTER MINIMUM EQUIPMENT LIST ¦
¦ FEDERAL AVIATION ADMINISTRATION ¦
¦ ------¦
¦ AIRCRAFT: ¦ REVISION NO: ORIGINAL ¦ PAGE: ¦
¦ CE-680 ¦ ¦ ¦
¦ ¦ DATE: 07/11/2008 ¦ S24-1 ¦
¦ ------¦
¦ 1. ¦ 2. NUMBER INSTALLED ¦
¦ SYSTEM & ¦ ------¦
¦ SEQUENCE ITEM ¦ ¦ 3. NUMBER REQUIRED FOR DISPATCH ¦
¦ NUMBERS ¦ ¦ ------¦
¦ ------¦ ¦ ¦ 4. REMARKS OR EXCEPTIONS ¦
¦ 24 ELECTRICAL POWER ¦ ¦ ¦ ¦
¦ 1. Windshield Anti-Ice B ¦ 2 ¦ 1 ¦ May be inoperative provided ¦
¦ AC Generator ¦ ¦ ¦ aircraft is not operated in known ¦
¦ (Alternator) ¦ ¦ ¦ or forecast icing conditions. ¦
¦ ¦ ¦ ¦ NOTE: Defog capability is also ¦
¦ ¦ ¦ ¦ affected. ¦
¦ 2. External Power C ¦ 1 ¦ 0 ¦ One may be inoperative provided ¦
¦ ¦ ¦ ¦ alternate electrical power is ¦
¦ ¦ ¦ ¦ available for aircraft starts. ¦
¦ 1) External Power D ¦ 1 ¦ 0 ¦ One may be inoperative provided ¦
¦ Switch ¦ ¦ ¦ alternate electrical power is ¦
¦ (EXT PWR) ¦ ¦ ¦ available for aircraft starts. ¦
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------
¦ U.S. DEPARTMENT OF TRANSPORTATION ¦
¦ MASTER MINIMUM EQUIPMENT LIST ¦
¦ FEDERAL AVIATION ADMINISTRATION ¦
¦ ------¦
¦ AIRCRAFT: ¦ REVISION NO: ORIGINAL ¦ PAGE: ¦
¦ CE-680 ¦ ¦ ¦
¦ ¦ DATE: 07/11/2008 ¦ S25-1 ¦
¦ ------¦
¦ 1. ¦ 2. NUMBER INSTALLED ¦
¦ SYSTEM & ¦ ------¦
¦ SEQUENCE ITEM ¦ ¦ 3. NUMBER REQUIRED FOR DISPATCH ¦
¦ NUMBERS ¦ ¦ ------¦
¦ ------¦ ¦ ¦ 4. REMARKS OR EXCEPTIONS ¦
¦ 25 EQUIPMENT/FURNISHINGS ¦ ¦ ¦ ¦
¦ 1. Flotation D ¦ - ¦ 0 ¦ Any in excess of those required by ¦
¦ Equipment ¦ ¦ ¦ FAR may be inoperative. ¦
¦ (Crew and ¦ ¦ ¦ ¦
¦ Passenger) ¦ ¦ ¦ ¦
¦ 2. Passenger Seats C ¦ - ¦ - ¦ May be inoperative provided: ¦
¦ ¦ ¦ ¦ a) Seat does not block an ¦
¦ ¦ ¦ ¦ Emergency Exit, ¦
¦ ¦ ¦ ¦ b) Seat does not restrict any ¦
¦ ¦ ¦ ¦ passenger from access to the ¦
¦ ¦ ¦ ¦ main aisle, and ¦
¦ ¦ ¦ ¦ c) The affected seat(s) are ¦
¦ ¦ ¦ ¦ blocked and placarded "DO ¦
¦ ¦ ¦ ¦ NOT OCCUPY". ¦
¦ ¦ ¦ ¦ NOTE 1: A seat with an inoperative ¦
¦ ¦ ¦ ¦ seatbelt is considered ¦
¦ ¦ ¦ ¦ inoperative. ¦
¦ ¦ ¦ ¦ NOTE 2: Affected seat(s) may ¦
¦ ¦ ¦ ¦ include the seat(s) behind ¦
¦ ¦ ¦ ¦ and/or adjacent outboard ¦
¦ ¦ ¦ ¦ seats. ¦
¦ 1) Recline C ¦ - ¦ - ¦ May be inoperative and seat ¦