Attachment 1 - C-40AConfig.pdf

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.

- Installed with B737-800 wings and main landing gear.

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

(Navy training purposes Category II is acceptable).

- Gaseous Oxygen System

Avionics (Nav):

- Mode Annuciator

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

- Single Tactical Air Navigation (TACAN) – AN/ARN 153 with XY channel selection capability.

- Dual Distance Measuring Equip (DME) – Rockwell

Scanning Interrogator Type DME-900 (ARINC 709)

- Automatic Direction Finder (ADF).

- 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

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

(ARINC 708)

- Inertial reference system (IRS)

- Radio Altimeter (RA) – 2 Rockwell International Corp

RA transceivers

Avionics (Coms):

- 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.

- Aircraft Communications Addressing and Reporting

System (ACARS).

- Emergency Locator Transmitter(ELT).

- 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 “mimumums” altitude callouts and 35, 40, 45 degrees and “bank angle” callouts enabled.

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

(Mode 4 and S for TCAS ops).

Avionics (Flight Controls):

- Digital Flight Control System

Dual Flight Management Computer System (FMCS) –

Navigational Database- Customer Supplied

Flight Director (FD) Guidance.