Attachment_1_C-37B_Desc.doc
DOC document 33 KB Posted
- Attached to
- Command Aircraft Crew Training (CACT) for C-37B Federal contract opportunity
- Solicitation number
- N6134020R0007
About this file
This document contains a federal contract solicitation and related performance work statement. The solicitation is for Command Aircraft Crew Training (CACT) for the C-37B aircraft. The Naval Air Systems Command is seeking proposals to provide crew training for the C-37B, which is a military version of the Gulfstream V aircraft used for transport of government personnel. Offerors must submit proposals by December 10, 2019, with the solicitation providing evaluation criteria and terms for the contract. The performance work statement provides details on the required training for pilots, crew chiefs, and flight attendants on the C-37B aircraft systems and emergency equipment.
View the file
Other files for this federal contract opportunity
| File | Type | Posted |
|---|---|---|
| N61340-20-R-0007-0001 CONFORMED.pdf | ||
| N61340-20-R-0007-0001 Amendment.pdf | ||
| N61340-20-R-0007-0001.pdf | ||
| Attachment_2_TPP.xlsx | XLSX spreadsheet | |
| N6134020R0007_06NOV19.docx | DOCX document |
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Text version
Attachment 1: C-37B
Attachment 1: C-37B Configuration
General description: The C-37B is a military version of the Gulfstream V (G-550). 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 – 91,400 LBS
Max Zero Fuel Weight – 54,500 LBS
Max Takeoff Weight – 91,000 LBS
Max Landing Weight – 75,300 LBS
Engines: The aircraft is powered by two FADEC controlled turbofan BMW/Rolls-Royce BR710C1-11 engines, each equipped with thrust reversers. Engine instrumentation includes EPR, TGT, HP, LP, FF, Oil pressure and temperature indicators, and 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
· Primus Epic System with 4 Honeywell DU-1310 Flat Panel LCD’s
· Three Honeywell MAU-913 Modular Avionics Units
· 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"
· Three Multi-Function Control Display Units
· Dual Automatic Flight Guidance System
· Enhanced Ground Proximity Warning System EGPWS(MK V) - AlliedSignal
· Honeywell RT-951 Traffic Alert and Collision Avoidance System (TCAS 2000)
· VHF Navigation System consisting of three receivers, ILS and marker beacon.
· TACAN-AN/ARN-153V Airborne TACAN System
· Honeywell Microwave Landing System (MLS)
· Two Distance Measurement Equipment transceivers
· Two ADF Receivers
· Two Mode “S” Transponders with TCAS 2000.
Communications
· Three 8.33 kHz VHF Radios
· Two Magnavox ARC-164 UHF radios
· Two HF transceivers
· HF and VHF SELCAL system - Two (2) Orbit Intercommunication Audio Interface Units P/N AL-14-2101-1
· MagnaStar Terrestrial Aeronautical Radio Telephone System
· Collins SAT-906-6 Satellite Aeronautical Radio Telephone System
· UHF Military Satcom ARC-210
· Allied Signal AFIS with VHF Satcom Link
· Tailwind 500 Satellite Television System
EMERGENCY EQUIPMENT
The C-37 is equipped with the following emergency equipment:
· Aircraft equipment includes: crash axe, halon fire extinguishers (3), water fire extinguisher (1), smoke goggles, portable Oxygen bottles, firefighting mask.
· Two thirteen man life rafts, P/N 1320FAUL-230-1-100. Each raft contains the PRC 149 radio.
File details come from the government source that posted it. Updated .