Attachment 1 - AircraftConfigC-40A.doc

ATTACHMENT I: C-40A “Clipper” Configuration

General: The Navy C-40A (“Clipper”), a derivative of the 737-700C IGW manufactured by Boeing Military Aircraft and Missile Systems is a convertible, fixed-wing twin engine, high performance, pressurized, auto flight capable, FAA certified aircraft that can be configured to 121 passengers, 8 pallets, or a 3 pallets/70 passengers. The

C-40A is equipped with the following:

- Two high-bypass, turbofan CFM56-7B engines with FADEC;

7B24 rating; single annular combustor; CFMI

International Propulsion System; debris monitoring system; Engine Sensors – Enhanced Condition

Monitoring; Engine Vibration Monitors (EVM) - Endevco

- Installed with B737-800 wings, main landing gear, body section 44

- Cabin Pressure System capable of rate 600 ft/min for assent and 350 ft/min for descent. (This will probably change to 750 ft.min/750 ft/min due to smoke certification)

- BF Goodrich high capacity steel brakes on main landing gear; Main landing gear with BF Goodrich high gross weight wheels (not nose gear); brake temperature indication system; no 1st officer station nose gear steering tiller; nose gear taxi light (250 watt) with automatic switchoff at retraction.

- Airworthiness certification of airplane systems to support all weather operation to Category IIIa weather minimums per FAA AC 120-28 or JAA JAR AWO.

(for Navy training purposes Category II is acceptable).

- Hand pump for thrust reversers cowl C-Duct

- Hydraulics - two engine driven in-line pumps with Vespel

Spline, Vickers (10-62167); two AC electric motor drive pumps, Vickers (10-60556); The two systems are separate and independent.

- Two 90 kVA generators; Standby Power (60 min) with two

48 amp batteries and battery chargers for aircraft standby loads (#1 FMC, #1 CDU or MCDU, Captain’s Inboard

Display Unit, #1 DME, standby RMI, #1 ADF & LH GPSS, and

IFF).

- High capacity gas turbine engine Auxilliary Power Unit

(APU) that drives a third AC generator.

- Accelerometer - Allied Signal Inc

- Gaseous Oxygen System Avionics (Nav):

- Mode Annuciator

- VOR/LOC– 2 Rockwell (ARINC 711-1) Receivers, type VOR-

- Single Tactical Air Navigation (TACAN) – AN/ARN 153 with XY channel selection capability, Radio Digital Distance magnetic Indicator (RDDMI)

- Dual Distance Measuring Equip (DME) – Rockwell

Scanning Interrogator Type DME-900 (ARINC 709)

- Automatic Direction Finder (ADF) – dual system –

Rockwell ADF-900 series ADF Receiver/ADF Antenna;

Dual ADF control panel – gables – G7403-03 with tone(BFO)/switch

- ILS/GPS Multi-mode Receiver (MMR) – Rockwell, ARINC 755

Multi-Mode Receivers with ILS and GPS functions

- Heads up Guidance System (HGS) - Flight Dynamics

Capt only – partial provisions

- Heads up Display (HUD) – Supplemental installation of the HGS 4000 Annunciator - Flight Dynamics -

- Single Weather Radar System/control panel – with predictive windshear (X band)– Rockwell Transceiver

(ARINC 708)

- Inertial reference system (IRS)

- 2 Radio Altimeter (RA) – Rockwell International Corp

RA transceivers

Avionics (Coms):

- Communications Control Panels – Dual Gables Radio tuning panels capable of 2 HF and 2 VHF

- 2 HF Coms - Dual Rockwell(ARINC 719/753 data link) HF Voice data transceivers and digital HF coupler

- 2 VHF/UHF Coms (8.33 khz channel spacing) Collins

AN/AR 210 1794(v) (ARINC 716//750) VHF-900B FM-Immune

Transceivers with 8.33 KHZ channel spacing

- SATCOM system – INMARSAT AERO-I System Installations-

Honeywell MCS-7000/Canadian Marconi intermediate

Gain Antenna that is compatible with the Audio

Selector Panel

- Audio Selector Panel (ASP) and 3 basic modified 737 style Remote Electronic unit (REU) - The Avtec ASP and REU shall support communication and navigation systems, including SELCAL, SATCOM, N/ARC-210 UHF, AN/ARN-153 TACAN and TCASS/IFF

- Passenger Telephone System – None installed

- Cabin, crew, ground crew Coms (provisions only)– ARINC

539A-1 pre-recorded announcement/boarding music system;

two interphone systems; Flight Interphone and Cabin

Interphone

- Selective Calling Equipment – SELCAL Motorola (ARINC

714) Five Channel Decoder

- Aircraft Communications Addressing and Reporting

System (ACARS) – ACARS Management Unit ARINC 724B

Upgradable to CMU – Rockwell installed into existing partial provision for single ARINC 724B ACARS – Dual

- VHF; ARINC 716 VHF Voice Mode Protection Dual VHF

- Emergency Locator Transmitter(ELT) – ARTEX 3- Freq automatic-fixed

- Voice Recorders – ED56A Allied Signal (2 hr recording time)

- TCAS II – Allied Signal TPA-81A System

- Ground Proximity Warning System(GPWS)/windshear -with 1000, 500 and “minimums” altitude callouts and 35, 40, 45 degrees and “bank angle” callouts enabled; 500

Smart callout inhibited

- Identification Friend or Foe (IFF) System – AN/APX-100S

(Mode 4 and S for TCAS ops); No commercial ATC transponder system

- Indicating/Recording Systems

Digital Flight Data Recorder ED56A Allied Signal Inc

256 words/sec max data rate.

Digital Flight Data Acquisition Unit (DFDAU) with ACMS

Capablity and integrated optical diskette drive –

Teledyne Controls

Airborne Data Loader/Recorder – ARINC 615- Teledyne-

02230666-020C

Data Loader Selector Switch Module – 12 positions-SFE

Narrow Format Multi-input Printer – due to change to ARC 210 (1794).

Modified Aft Electronic Panel Arrangement - due to ARC 210 (1794) change.

Avionics (Flight Controls):

- Digital Flight Control System

Dual Flight Management Computer System (FMCS) –

4 MCU (Modular Concept Unit); Activation – QNH/QFE selectable reference for TO/Ldg; Color LCD multipurpose control display units (MCDU) with fans compatible keyboards in lieu of std MCDU keyboards. Mode Control Panel (MCP) – Push-button MCP with speed altitude intervention; Approaching 900 ft of MCP setting, both altitude lights and momentary sounds; less than 200 ft, momentary tone sounds and altitude alert lights lights extinguish; upon deviation of > 200 ft for selected altitude, momentary tone sound and altitude alert lights flash. FMC option that allows selection of thrust reduction altitude (TO to climb thrust reduction). FMC System includes the following: QRH Takeoff Speeds- Enable; Runway Distance- Units of Feet; Speed and Altitude Intervention- Enable; Vertical Navigation Profile- VNAV ALT- Enable; Navigational Database- Customer Supplied; Flight Number Entry via the Router Page- Enable; Alternate Destination Predictions- Inhibit; Retention of Waypoints after Direct to- Inhibit;

Message Recall- Inhibit Flight Control Computer (FCC) (ILS flt warning)

Auto pilot control (2 channel)

Auto Pilot Flight Director (inhibits glide slope capture prior to localizer capture.

Flight Director (FD) Guidance; provides FD roll commands during TO mode to maintain selected heading

ACMS – Optional Engine Parameters – Four ARINC 429 busses from the Common Display System (CDS) Display Electronic Units (DEU) to the DFDAU (two from the DEU). These busses provide AMCS access to all of the parameters from both channels of the Electrical Engine Control (EEC). CDS has the over and under engine presentation.

- Description of CDS Display – over and under Engine presentation:

Display flight and navigation data in the Primary Flight Display (PFD)/Navigation Display (ND) format. Display primary engine indications on the upper display unit and secondary engine indications on the lower display unit. Engine data is be displayed in a format similar to that used on the Boeing 757, 767, and 777 airplanes.

Secondary engine parameters are displayed when selected by the flight crew via the ENG switch on the engine control panel or automatically in the event of a parameter exceedance.

These parameters are shown on the outboard and inboard display units: Attitude parameters:

- Pitch

- Roll

- Slip/skid indication

- Flight director indication

- Pitch limit indication

- TCAS resolution advisories (if applicable)

Airspeed parameters:

- Airspeed

- Selected airspeed

- Mach number

- Maximum operating speeds

- V1, VR and V2+15 speeds

- Stick shaker speed range

- High speed buffet range

- Selected Mach number

- Airspeed trend

- VMO

- MMO

- Flap extension and retraction speeds

- Landing reference speed V REF and V REF + 15

Barometric Altitude Parameters:

- Barometric altitude

- Selected altitude

- Selected minimum barometric altitude

- Barometric correction setting

- Pre-selected barometric correction setting

- Altitude reference annunciation and FMC prompt

- Vertical speed indication

- Selected vertical speed

- MCP selected altitude as metric digital readout (when selected on the EFIS control panel)

- Current metric digital altitude (when selected on the EFIS control panel)

Radio Altitude Parameter

- Radio altitude

- Selected radio altitude approach minimums

Heading Parameters:

- Drift angle

- Heading

- Selected heading

- Track

- MAG/TRUE indication

- Selected course

Landing Aids Parameters:

- Localizer deviation

- Glideslope deviation

- ILS deviation warnings

- Marker beacon indication

Flight Mode Annunciation:

- Autopilot/flight director mode indication

- Autothrottle mode indication

The inboard display has these modes of operation:

- MAP

- VOR/APP

- PLN (planning) The MAP and VOR/APP modes can be shown with the airplane reference at the center or at the bottom of the display.

This information is included in MAP mode:

- Airplane track and heading

- Trend vector

- Vertical path deviations

- Distance to next active waypoint

- Estimated time of arrival at next active waypoint

- Navigation aids

- Flight plan waypoints

- Active LNAV route

- Airports

- Waypoints

- Altitude range arc

- Fix point and radials

- ADF bearing pointer

- Ground speed

- True airspeed

- Wind direction and speed

- Weather radar returns

- Inertial position

- Selected VOR radials

- VOR radials and DME vectors

- VOR bearing pointers

- ADF frequency or identifier

- VOR frequencies or identifier

- ILS frequencies or identifier

- ILS course

- DNE distance

- Weather radar mode, gain and tilt annunciations

- TCAS traffic display

- TCAS traffic alerts and mode annunciations

- Failure flags

- Navigation advisory messages

The PLN mode uses a north-up presentation. This information is included in PLN mode:

- Distance to next active waypoint

- Estimated time of arrival to next active waypoint

- Flight plan waypoints

- Flight plan path line

- Moving airplane symbol

- TCAS traffic alert messages and mode annunciations

- Wind direction and speed

- Navigation aids

- Groundspeed

The VOR/APP mode uses a heading-up presentation. This information is included in VOR/APP mode:

- Airplane heading and track

- Course pointer and deviation scale

- To/From indication

- DME distance

- VOR frequency or identifier

- VOR bearing pointers

- ADF bearing pointer

- ADF frequency or identifier

- Selected course

- Ground speed

- True airspeed

- Wind speed and bearing

- Weather radar (only in expanded mode)

- TCAS traffic display

- TCAS traffic alerts and mode annunciations

- Glideslope deviation

- Localizer deviation

- Selected runway heading

- ILS frequency or identifier

- ILS course

Note: This option is contingent on successful certification of the 737-800.

- Flight Director Command Display – Split axis – Display FD command as split axis command bars on the Attitude

- Director Indicator (ADI). Pitch command bar is horizontal bar that moves up/down relative to fixed airplane reference and roll command is a vertical bar that moves left/right relative to airplane reference.

- Radio Altimeter – Below ADI

- Landing altitude reference bar – Primary Flight Display

(PFD) - white bar [1000 to 500ft] and amber bar [500 to 0 ft] on the PFD above the TDZ/FE bug.

- Baro Minimums Pointer – PFD – Display the triangle portion of the bar minimums pointer on the PFD altitude tape when the mins reference “MINS” selector on the EFIS control panel is in the “radio” position

- ILS Localizer Deviation Expanded scale – Auto Pilot mode only

- Map Mode Orientation - Track up – navigation display