usac airways 694, llc minimum equipment list … airways 694 llc...operator certificate 0 0 not...

USAC AIRWAYS 694, LLC

MINIMUM EQUIPMENT LIST

AIRCRAFT: BAE-125-1000

REGISTRATION: N67WE

SERIAL #: 259038

REV. NO: ORIGINAL DATE: 08/05/2016

PAGE NO: 23-1

1. SYSTEM, SEQUENCE NUMBERS & ITEM

REPAIR CATEGORY

2. NUMBER INSTALLED

3. NUMBER REQUIRED FOR DISPATCH

4. REMARKS AND EXCEPTIONS

23 COMMUNICATIONS

-05-1 Radio Management Unit (RMU) (Honeywell Equipped Aircraft Only)

C 2 1 (O) One may be inoperative provided: a) Remaining RMU is verified

operative, b) Clearance Delivery Head (CDH) is

verified operative, and c) Alternate procedures are

established and used.

Refer to OMP 23-05-01 for (O) procedure.

-10-1 Communications System (VHF & UHF)

D 3 1 Any in excess of those required by FAR may be inoperative provided it is not powered by an Emergency Power Source and not required for emergency procedures.

Refer to OMP 23-A for FAR requirements

-10-2 High Frequency (HF) Communication System

D 2 0 Any in excess of those required by FAR may be inoperative.





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23 COMMUNICATIONS

-20-1

Selective Call System (SELCAL)

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

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

Refer to OMP 23-20-1 for (O) procedures

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


-20-2

ACARS System 0 0 NOT INSTALLED ON THIS AIRCRAFT.

-20-3

AFIS (VHF/SAT) 0 0 NOT INSTALLED ON THIS AIRCRAFT.




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REPAIR CATEGORY

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23 COMMUNICATIONS

-20-4 Emergency Locator Transmitter (ELT)

-1) Survival Type ELTs D 1 0 Any in excess of those required by FAR may be inoperative or missing. One is required only for extended over water operations

Refer to OMP 23-D for more CFR detail, if desired.

-2) Fixed ELTs A 1 0 May be inoperative or missing provided repairs are made within 90 days.

Refer to OMP 23-D for FAR requirements

D 1 0 Any in excess of those required by FAR may be inoperative or missing.

Refer to OMP 23-D for FAR requirements

-30-1 Passenger Address (PA) System

-1) Passenger Configuration

C 1 0 (O) May be inoperative provided: a) Alternate normal and emergency

operating procedures and/or operating restrictions are established and used and

b) Flight Deck/Cabin Interphone System is operative.


-2) Cargo Configuration D 1 0 May be inoperative.




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SERIAL #: 259038


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2. NUMBER INSTALLED



23 COMMUNICATIONS

-30-2 Cabin Chime System C 1 0 May be inoperative provided Passenger Address System is operative.



-30-3

Pre-Recorded Passenger Announcement System

C 1 0 (O) May be inoperative provided alternate procedures are established and used. Refer to OMP 23-30-3 for (O) procedures

-30-4 Flight Deck Speakers C 2 1 May be inoperative provided both Pilot Station Headsets are installed and operative.

-40-1 Service Interphone System (Flight Deck to Cabin) (Cabin to Flight Deck) (Flight Deck to Ground)

C 1 0 (O) May be inoperative provided: a) Alternate procedures are

established and used, and b) PA System is operative.


-50-1 (Reserved)

-50-2 Headsets (Except Microphone)

C 2 1 One may be inoperative at either pilot station provided Flight Deck Speaker System is operative.




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23 COMMUNICATIONS

-50-3 Microphones (Handheld)

C 2 1 One may be inoperative at either pilot’s station provided associated headset with boom microphone is operative.

Refer to OMP 23-C for FAR requirements

-50-4 Boom Microphones (Including Headset Mic)

CVR WITH FDR INSTALLED

-1) Cockpit Voice Recorder Equipped to Record Boom Microphone Per FAR 121.359(g), 125.227(e) or 135.151(d)

0 0 NOT INSTALLED ON THIS AIRCRAFT.

-2)

Cockpit Voice Recorder Not Equipped to Record Boom Microphone


CVR WITHOUT FDR INSTALLED

-1) Cockpit Voice Recorder Equipped to Record Boom Microphone per FAR 121.359(g) 135.151(d) or 125.227(e)

A 1 0 May be inoperative provided repairs are made within three flight days.

-2)

Cockpit Voice Recorder Not Equipped to Record Boom Microphone





REGISTRATION: N67WE

SERIAL #: 259038


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REPAIR CATEGORY

2. NUMBER INSTALLED



23 COMMUNICATIONS

-60-1 Static Dischargers C 27 26 One static discharger may be missing from the entire aircraft.

-70-1 Cockpit Voice Recorder (CVR)

-1) With Flight Data Recorder Installed


-2) Without Flight Data Recorder Installed

A 1 0 May be inoperative provided repairs are made within three flight days.

-3) CVR installed for Other Than Holder of an Air Carrier or Commercial Operator Certificate

0 0 NOT APPLICABLE TO THIS AIRCRAFT.

-70-2

Flight Phone D 2 0 May be inoperative.

-70-3

Satellite Communications Systems (SATCOM)


D 2 0 May be inoperative provided operating procedures do not require its use.

-80-1

Heads Up Checklist System





REGISTRATION: N67WE

SERIAL #: 259038


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REPAIR CATEGORY

2. NUMBER INSTALLED



34 NAVIGATION

-09-1 Distance Bearing Indicator (DBI)

C 1 0 May be inoperative provided DME, VOR/ADF bearing and compass heading displays are available at each pilot’s station.

-09-2 Distance Measuring Equipment (DME) Indicator (2nd Pilot’s Station)

C 1 0 May be inoperative provided DME displays are available at each pilot’s station.

-09-3 Non-Stabilized Magnetic Compass (Standby)

B 1 0 May be inoperative provided any combination of three Gyro or INS (IRU) Stabilized Compass Systems are operative.

B 1 0 (O) May be inoperative provided: a) Any combination of two 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 the enroute portion of the flight.


B 1 0 (O) May be inoperative for flights that are entirely within areas of magnetic unreliability provided at least two Stabilized Directional Gyro Systems are operative and used in conjunction with accepted Free Gyro Navigation Techniques.





REGISTRATION: N67WE

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REPAIR CATEGORY

2. NUMBER INSTALLED



34 NAVIGATION

-10-1 Mach/Airspeed Aural Warning Channels

B 2 1 One may be inoperative.

B 2 0 (O) May be inoperative provided: a) Both Mach/Airspeed Indicators on

the EFIS PFD’s are operative, and b) AFM Airspeed Limitations are

observed.


-10-2 Altitude Alerting System

A 2 0 (O) May be inoperative provided: a) Autopilot with Altitude Hold is

operative, b) Operations do not require its use,

and c) Repairs are made within three

flight days.


NOTE: RVSM is not authorized.

C 2 1 Any in excess of those required by FAR may be inoperative.

-10-3 Altimeter Vibrators C 2 1 One may be inoperative provided VMC exists at departure and arrival airports.

NOTE: RVSM is not authorized.

-10-5 Outside Air Temperature Indicator

C 1 0 (O) May be inoperative provided alternate Temperature Indicating System (TAT or SAT) is available and used.


-10-6 Air Temperature Indications (SAT/TAT) on FMS CDU

C 2 0 (O) May be inoperative provided: a) Outside Air Temperature Indicator

is operative, and b) Required Flight Management

System (FMS) is operative.





REGISTRATION: N67WE

SERIAL #: 259038


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REPAIR CATEGORY

2. NUMBER INSTALLED



34 NAVIGATION

-20-1 Flight Director Systems C 2 0 May be inoperative provided approach minimums do not require their use.

-20-2 Attitude/Heading Source Reversion Switches

A 2 1 (O) One may be inoperative provided: a) SG Reversion is verified operative, b) Affected switch remains selected

to normal independent source, and

c) Repairs are made within 3 flight days.


-20-3

Angle of Attack (AOA) System

C 2 0 (O) May be inoperative provided stall warning systems are operative.


-20-4 Inertial Reference System (IRS)

C 2 0 As required by FAR Refer to OMP 34-A for FAR requirements.

-20-5

3rd Inertial Reference System


-20-6 Air Data Computer Source Reversion Switches

A 2 1 (O) One may be inoperative provided: a) SG Reversion is verified operative, b) Affected switch remains selected

to normal independent source,and Repairs are made within 3 flight days.





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SERIAL #: 259038


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REPAIR CATEGORY

2. NUMBER INSTALLED



34 NAVIGATION

-20-7 Symbol Generator Reversion Switches

A 2 1 (O) One may be inoperative provided: a) ATT/HDG reversion is operative, b) ADC reversion is operative, c) Affected switch remains selected

to normal independent source, and

d) Repairs are made within 3 flight day.


-20-8 Standby Attitude Indicator

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.

-30-1 Instrument Landing Systems (ILS)

C 1 0 May be inoperative provided: a) Not required by FAR, and b) Operations do not require its use.

-1) Glide Slope C 3 0 May be inoperative provided: c) Not required by FAR, and d) Operations do not require its use.




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SERIAL #: 259038


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REPAIR CATEGORY

2. NUMBER INSTALLED



34 NAVIGATION

-30-2 Marker Beacon System C 2 0 May be inoperative provided: a) Not required by FAR, and b) Operations do not require its use.

-30-3

Microwave Landing System (MLS)


-40-1 Radio Altimeter System A 2 0 (M)(O) May be inoperative provided: a) TAWS/GPWS is considered

inoperative, b) TCAS is considered inoperative, c) Approach minimums or operating

procedures do not require its use, d) Alternate procedures are

established and used, and e) Repairs are made within two flight

days.

Refer to OMP 34-40-1 for (M/O) procedures

-40-2 Weather Radar Systems

C 1 0 As required by FAR Refer to OMP 34-F for FAR requirements.

-1) Windshear Detection and Avoidance System (Predictive)


NOTE: Flight crew’s alternate procedures should include reviewing windshear avoidance and windshear recovery procedures.

-40-3

VTA (Voice Terrain Advisory System)





REGISTRATION: N67WE

SERIAL #: 259038


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REPAIR CATEGORY

2. NUMBER INSTALLED



34 NAVIGATION

-40-4 Terrain Awareness and Warning System-TAWS

-A. Class A TAWS Equipment Required

-1) Ground Proximity Warning System (GPWS)

A 1 0 (O) May be inoperative provided: a) Alternate procedures are

established and used, and b) Repairs are made within two flight

days.


-a) Modes 1-4 A 4 0 (O) May be inoperative provided: a) Alternate procedures are


days.


-b) Test Mode A 1 0 May be inoperative provided: a) GPWS is considered inoperative,

and b) Repairs are made within two flight

days.

-c) Glideslope Deviation(s) (Mode 5)

C 2 1

B 2 0 May be inoperative.

-d) Advisory Callouts B 6 0 (O) May be inoperative provided alternate procedures are established and used.


(Continued) C 6 0 (O) May be inoperative provided: a) Advisory callout not required by

FAR, and b) Alternate procedures are

established and used. Refer to OMP 34-40-4 for (O) procedures




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34 NAVIGATION

-40-4 Terrain Awareness and Warning System (TAWS) (Continued)

-A. Class A TAWS Equipment (Continued)

-1) GPWS (Continued)

-e)

Windshear Mode (Reactive)

B 1 0 (O) May be inoperative provided alternate procedures are established and used. Refer to OMP 34-40-4 for (O) procedures NOTE: Flight crew’s alternate procedures

should include reviewing windshear avoidance and windshear recovery procedures.

C 1 0 (O) May be inoperative provided: a) Alternate procedures are

established and used, and b) Windshear Detection and

Avoidance System (Predictive) operates normally.


-2) Terrain System-Forward Looking Terrain Avoidance (FLTA) and Premature Descent Alert (PDA) Functions

B 1 0 (O) May be inoperative provided alternate procedures are established and used. Refer to OMP 34-40-4 for (O) procedures

-3) Terrain Displays C 3 1

B 3 0

-4)

Runway Awareness and Advisory System (RAAS)

C 1 0

(continued)




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34 NAVIGATION


-B. Class B TAWS Equipment Required

-1) Ground Proximity Warning System (GPWS)

A 1 0 (O) May be inoperative provided: a) Alternate procedures are


days.


-a) Modes 1 & 3 A 2 0 (O) May be inoperative provided: a) Alternate procedures are


days.


-b) Test Mode A 1 0 May be inoperative provided: a) GPWS is considered inoperative,

and b) Repairs are made within two flight

days.

-c)

Modes 2, 4 & 5


-d) Advisory Callouts B 6 0 (O) May be inoperative provided alternate procedures are established and used.


(Continued) C 6 0 (O) May be inoperative provided: a) Advisory callout not required

by FAR, and b) Alternate procedures are

established and used. Refer to OMP 34-40-4 for (O) procedures

(continued)




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2. NUMBER INSTALLED



34 NAVIGATION


-B. Class B TAWS Equipment Required (Continued)

-1) GPWS (Continued)

-e)

Windshear Mode (Reactive)



-2) Terrain System-Forward Looking Terrain Avoidance (FLTA) and Premature Descent Alert (PDA) Functions

B 1 0

-3)

Terrain Displays C 1 0

-4)

Runway Awareness & Advisory System (RAAS)

C 1 0

-C. Class C TAWS Equipment

-1)

TAWS/GPWS


NOTE 1: Any Mode that operates normally may be used.

NOTE 2: If Test Mode is inoperative, the GPWS must be considered inoperative.




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2. NUMBER INSTALLED



34 NAVIGATION

-40-5

Lightning Sensor System


-50-1 Flight Management Systems (FMS)(RNAV)

C 3 1

-1) Navigation Databases C 2 0 (O) May be out of currency provided: a) Current Aeronautical Charts are

used to verify Navigation Fixes prior to dispatch,

b) Procedures are established and used to verify status and suitability of Navigation Facilities used to define route of flight,

c) Approach Navigation Radios are manually tuned and identified, and

d) RNAV Departures, Arrivals, Instrument Approaches and published RNAV Routes based on RNAV guidance are not used.


-50-2 Distance Measuring Equipment (DME)






REGISTRATION: N67WE

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2. NUMBER INSTALLED



34 NAVIGATION

-50-3 ATC Transponder and Automatic Altitude Reporting System

B 2 0 May be inoperative provided: a) Enroute operations do not require

its use, and b) Prior to flight, approval is obtained

from ATC facilities having jurisdiction over the route of flight.

NOTE: RVSM is not authorized


Refer to OMP 34-B for FAR requirements

-1) Elementary and Enhanced Downlink Aircraft Reportable Parameters Not Required by FAR

A 1 0 May be inoperative provided: a) Enroute operations do not require

its use, and b) Repairs are made prior to

completion of the next heavy maintenance visit.

-2) ATC Transponder Ident Buttons

C 2 2 May be inoperative provided one is operative at each pilot position.




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34 NAVIGATION

-50-4 VOR Navigation Receivers


-50-5 ADF System D 2 0 May be inoperative provided operations do not require its use.

-50-6

Global Positioning System (GPS)


-50-7 Omega/VLF Sensor DELETED, MMEL Revision 3.

50-8 Automatic Dependent Surveillance-Broadcast (ADS-B) System





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2. NUMBER INSTALLED



34 NAVIGATION

-60-1 Traffic Collision and Avoidance System (TCASII)

B 1 0 (M) May be inoperative provided: a) System is deactivated and

secured, and b) Enroute or approach procedures

do not require its use.

Refer to OMP 34-60-1 for (M) procedures

C 1 0 (M) May be inoperative provided: a) Not required by FAR, b) System is deactivated and

secured, and c) Enroute or approach procedures


Refer to OMP 34-60-1 for (M) procedures

-1) Combined Traffic Alert (TA) and Resolution Advisory (RA) Dual Display

C 2 1 (O) May be inoperative on the 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 the flying pilot side.


(continued)




REGISTRATION: N67WE

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2. NUMBER INSTALLED



34 NAVIGATION

-60-1 Traffic Collision and Avoidance System (TCASII) (Continued)

-2) Resolution Advisory (RA) Display System(s)

C 2 1 (O) One may be inoperative on the non-flying pilot side.


C 2 0 (O) May be inoperative provided: a) TA visual display and audio

functions are operative, b) TA ONLY Mode is selected, and c) Enroute or approach procedures



-3) Traffic Alert (TA) Display System(s)


-4) Audio Functions B 1 0 May be inoperative provided enroute or approach procedures do not require use of TCAS.

-5)

Airspace Selection Function

C 1 0 May be inoperative.

-70-1 EFIS Cooling Fans (Honeywell EDZ-818 EFIS equipped only)

A 3 2 (O) One may be inoperative provided: a) Standby Attitude Indicator is

operative, b) DBI and Standby Magnetic

Compass are operative, c) Cabin temperature can be

maintained below 35 degrees C, and

d) Repairs are made within three flight days.





REGISTRATION: N67WE

SERIAL #: 259038


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REPAIR CATEGORY

2. NUMBER INSTALLED



34 NAVIGATION

-70-2 EFIS Overheat Warning Annunciators (Honeywell EDZ-818 EFIS equipped only)

C 3 0 (M)(O) May be inoperative provided: a) All EFIS Cooling Fans are verified

operative before each departure, and

b) EFIS Fan Fail Warning System is operative.

Refer to OMP 34-70-2 for (M/O) procedure.

-70-3 EFIS “Fan Fail” Annunciators (Honeywell EDZ-818 EFIS equipped only)

C 3 0 (M) May be inoperative provided: a) All EFIS Cooling Fans are

operative, and b) EFIS Overheat Warning System is

operative.

Refer to OMP 34-70-3 for (M) procedure.

-70-4 Electronic Flight Displays (EFD) (Honeywell EDZ-818 EFIS equipped only)

C 4 3 (O) One Unit may be inoperative provided an independent PFD is available at each pilot’s station. Refer to OMP 34-70-4 for (O) procedure.

-70-5 Symbol Generators (SG) (Honeywell EDZ-818 EFIS equipped only)

C 2 1 (M)(O) Right-side may be inoperative provided:

a) The required number of EFDs show correct displays,

b) Each pilot’s EFIS is driven by an operative independent symbol generator unit, and

c) Multifunction Symbol Generator is verified operative.


C 2 1 (M)(O) One may be inoperative provided: a) The required number of EFDs

show correct displays, b) Each pilot’s EFIS is driven by an

operative independent symbol generator unit, and

c) Multifunction Symbol Generator is verified operative, and

d) Aircraft is operated Day VMC only.





REGISTRATION: N67WE

SERIAL #: 259038


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2. NUMBER INSTALLED



34 NAVIGATION

-70-6 Multifunction Symbol Generator (MSG) (Honeywell EDZ-818 EFIS equipped only)

C 1 0 (M)(O) May be inoperative provided: a) Both SG’s are operative, b) Standby Attitude Indicator is

operative, and c) Multifunction Display (MFD) and

all Electronic Flight Displays (EFDs) are operative.


NOTE: MSG must remain installed to ensure that the cross side symbol generator reversion is operative.

-70-7 Multifunction Display (MFD) (Honeywell EDZ-818 EFIS equipped only)

C 1 0 May be inoperative provided all 4 EFDs are operative.

(Honeywell Primus CDS/R equipped only)


-70-8 Integrated Avionics Computer (IC-1080) (Honeywell Primus CDS/R equipped only)


-80-1

Airborne Flight Information System (AFIS)


usac airways 694, llc minimum equipment list … airways 694 llc...operator certificate 0 0 not...

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