Attachment_2_-_C-37A_AC_Description_(27FEB19).doc

Attachment 2 C-37A

Attachment 2: C-37A Configuration

General description: The C-37A is a military version of the Gulfstream V (G-V). It is a two engine, swept wing, long range, high altitude, high speed, special mission aircraft. The normal crew consists of two pilots, crew chief, and flight attendant and is capable of carrying 14 passengers.

Max Ramp Weight – 90,900 LBS

Max Zero Fuel Weight – 54,500 LBS

Max Takeoff Weight – 90,500 LBS

Max Landing Weight – 75,300 LBS

Engines: The aircraft is powered by two FADEC controlled turbofan BMW/Rolls-Royce BR710A1-10 engines, each equipped with thrust reversers. Engine instrumentation includes EPR, TGT, HP, LP, FF, Oil pressure and temperature indicators, fuel tank and fuel temperature indicators.

Electrical: Two engine driven Integrated Drive Generators(IDG) and one APU driven IDG. Each IDG provides 40 KVA three phase power at 115 volts, 400 HZ. The DC power is developed by two 24 VDC, 53 amp hour 21 cell NICAD batteries.

Avionics:

Navigation

· Two Honeywell IC-800E Flight Guidance Computers

· North Atlantic Minimum Navigation Performance Specification(NAT MNPS)

· Reduced Vertical Separation Minimums (RVSM) compliant

· Basic RNAV(BRNAV) and RNP-5 capable

· RNP 0.3 RNAV approach capable

· Category II ILS capable

· Heads Up Display (HUD) – Honeywell HUD-2020

· Enhanced Vision System (EVS) - Kollsman "All Weather Window"

· Two Flight Management Systems with three 820 CDUs - Honeywell

· Auto-pilot-Sperry SPZ-8500

· Enhanced Ground Proximity Warning System EGPWS(MK V) - AlliedSignal

· Traffic Alert and Collision Avoidance System(TCAS II ch.7) - Honeywell

· Two Honeywell HG-2021 GPS receivers

· VHF Navigation System consisting of two VIR-432 receivers and two RMI’s.

· TACAN-AN/ARN-153V Airborne TACAN System

· Honeywell Microwave Landing System (MLS)

· Two Collins Distance Measurement Equipment units - DME-422

· Two Collins ADF-462 Receivers

· Two Collins TDR-94D mode “S” Transponders

Communications

· Two Collins RTU-4280 Radio Frequency Management Units (8.33khz capable)

· Two Collins VHF-422D Radios

· Two Magnavox ARC-164 UHF radios

· Two Collins HF-9034A HF Communication radios

· HF and VHF SELCAL system - Two (2) Orbit Intercommunication Audio Interface Units P/N AL-14-2101-1

· MagnaStar C-2000 Terrestrial Aeronautical Radio Telephone System

· Collins SAT-906-6 Satellite Aeronautical Radio Telephone System

· Raytheon APX-100 IFF system

· UHF Military Satcomm -Motorola LST-5D

· Allied Signal AFIS with VHF Satcom Link

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