IOD_RFI_PWS.pdf

Procurement Work Statement (PWS)

King Air 350C (Wing Locker Extended Fuel Tanks)

Dry Lease

King Air 350C Dry Lease

1.0 Introduction

The U.S. Marshals Service (USMS), Investigative Operations Group (IOD) provides the USMS, other

Federal agencies, and requesting State or local law enforcement partners, with the timeliest and technologically advanced electronic surveillance (ELSur) and investigative support in the world.

1.1 Description of Services: The contractor shall provide one 2010 or newer Beechcraft King Air 350C aircraft (with wing locker extended fuel tanks) and cargo door, configured with the Garmin G-1000

Avionics Suite or Rockwell Collins Pro Line 21 Glass Panel Avionics for exclusive use by the USMS IOD.

The aircraft shall have less than 600 hours total time and be configured to accommodate an ISR and

FMV surveillance suite. The aircraft will be operated and maintained by Government personnel in accordance with FAA 14 CFR Parts 43 and 91. The aircraft shall be capable of providing multiple sorties daily and maintain an annual Operational Readiness (OR) rate of 85%. At the Governments request the aircraft will be configured to accommodate additional GFE (Government Furnished Equipment) such as air-to-ground communications and cockpit-to-cabin interphone capability. The aircraft shall meet FAA civil airworthiness certification and the contractor shall provide confirming documentation of said certification.

1.2 Scope: The contractor shall provide the required aircraft to meet IOD needs as identified in this PWS.

The period of performance shall not begin until receipt of one Beechcraft King Air 350C aircraft (with wing locker extended fuel tanks) and cargo door with approval and inspection to be at the discretion of the Contracting Officer. Aircraft utilization is estimated to be 500 flight hours annually for the duration of the lease. For scheduled maintenance planning purposes, the aircraft shall perform approximately 25 landing gear cycles per month. The Government will provide all required inspections and maintenance for the aircraft to ensure continued airworthiness and availability.

1.3 Period of Performance: The period of performance shall be one Base Year of 12 months and four

Option Years of 12 months each with the base year starting upon aircraft delivery to the Government.

2.0 Aircraft Specifications

The contractor provided King Air 350C aircraft (with wing locker extended fuel tanks) and cargo door shall meet the following specifications and requirements.

Certification Date: 2010 or newer

Airframe and Engine Hours: Less than 600 hours total time

Airframe Cycles: Less than 400 cycles

Aircraft Maintenance Status: Fresh Manufacturer Phase Inspection, Fresh Annual Aircraft Inspection

Engine Model: Pratt & Whitney PT6A-60A

Engine Serial Numbers: TBD at contract award

Propeller Model: Hartzell HC-B4MP-3

Propeller Serial Numbers: TBD at contract award

2.1 Avionics

Flight Display System: Garmin G-1000 avionics suite (pilot’s PFD, MFD and copilot’s PFD) and auto-pilot search and rescue capability or Pro Line 21 glass panel system with two (2) AFD-3010 and one (1) AFD-

3010E adaptive flight displays (pilot’s PFD, MFD and copilot’s PFD) and auto-pilot search and rescue capability; incorporates an Engine Indicating (EI) system

Comm 1: Collins VHF-4000 transceiver (118.000 to 136.975 MHz with 8.33 KHz increments), tuning through CDU or Collins RTU- 4220

Comm 2: Collins VHF-4000 transceiver (118.000 to 136.975 MHz with 8.33 KHz increments), tuning through CDU or Collins RTU- 4220

Nav 1: Collins NAV-4000 VOR/LOC/GLS/ADF/Marker Beacon receiver, tuning through CDU or RTU

Nav 2: Collins NAV-4500 VOR/LOC/GLS/ Marker Beacon receiver, tuning through CDU or RTU

AHRS: Dual Collins AHC-3000 attitude heading reference system including dual FDU-3000 flux detector units, slaved and DG heading modes are provided

GPS: Collins GPS-4000A global positioning sensor with antenna DBU - DBU-5000 database unit for navigation database loading

ADC: Dual Collins ADC-3000 air data computers (RVSM capable)

ADF: Collins NAV-4000 with ADF, including antenna

Transponders: Dual Collins (Mode S) TDR-94 non-diversity transponders with single antenna, controlled through CDU or RTU. Transponder ATC Ident button on pilot’s and copilot’s control wheels

DME: Collins DME-4000 with DME information displayed on PFD’s Audio system - dual dB 700/dB 800 systems

FMS: Collins FMS-3000 flight management system with single with 30 minute recording time. CDU-3000 and navigational inputs from GPS receiver, Navigation receivers, and DME

IFIS: Collins Integrated Flight Information System (IFIS) provides enhanced map features to traditional displays (e.g. rivers, lakes, national boundaries, airway and airspace depictions). A File Server Unit (FSU) is connected to an Ethernet capable MFD and provides the control interface using a Cursor Control

Panel (CCP).

ESIS: Electronic standby instrument system L3 Communications GH-3100 with attitude, heading, airspeed, altitude, and Nav with back-up battery

Turbulence Weather Radar: Collins TWR-850 turbulence detection (Doppler) weather radar (RTA-852 receiver/transmitter/12” antenna) with display capability on any AFD

Radio altimeter: Collins ALT-4000 radio altimeter, measures altitude up to 2,500 feet AGL, displayed on

PFD

Maintenance Diagnostics Computer: Collins MDC-3110 maintenance diagnostics computer, displays maintenance information on MFD and downloads through the DBU-5000 (shared with the FMS) or through the PCD-3100 interface

ACSS TAWS (Terrain Awareness and Warning System): Displayed on either PFD or MFD

TCAS 1: Traffic alert and collision avoidance system (level 1) using L3 Communications Skywatch HP displayed on MFD in normal mode, PFD in reversionary mode

Checklist display capability: Normal and emergency checklists displayed on the MFD

Cabin paging: Cockpit to cabin paging with five cabin speakers

Emergency Locator Transmitter: Artex ELT C406-2

3.0 Terms and Conditions

The required aircraft is anticipated to be procured utilizing FAR Part 12. The Government intends to award to the responsible party to avoid the significant duplication of cost. Delivery required FOB

Destination to (TBD ISR/FMV installer), 15 days from the date of Award. This is a firm fixed price (FFP) contract. The North American Industry Classification System (NAICS) Code for this procurement is

481211 and the size standard is 1500 employees.