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COMMERCE BUSINESS DAILY ISSUE OF MAY 14,1999 PSA#2346Drug Enforcement Administration, Office of Acquisition Management, 700
Army Navy Drive, Arlington, Virginia 22202 15 -- SOURCES SOUGHT SYNOPSIS ONLY SOL DEA-99-R-0028 POC Doreen
Upshur, Contract Specialist, (202) 307-7806 Aircraft and airframe
structural components: SOURCES SOUGHT SYNOPSIS ONLY! No solicitation
will be issued as a result of this synopsis. The Drug Enforcement
Administration (DEA) is seeking to identify sources for an anticipated
fixed price, (commercial item) contract. The SIC is 3721 and the small
business size standard is 1,500 employees. The contemplated contract is
for a base period and two (2) twelve month option periods. The
Governments requirement is for one (1) Single-Engine Turboprop Utility
Aircraft (a/c) as modified; Pilot Training for four person; A/C
Maintenance Training for four person each year. At a minimum
prospective contractors must be able to provide: Aircraft Flight
Performance Requirements -- The following minimum performance
regulations are mandatory: (a) Range -1,500 NM with 60 minute reserve;
(b) Speed -- Cruise speed 240 KTAS as a minimum at altitude; (c)
Service Ceiling -- 25,000 feet min based on optimum a/c performance,
(d) Take Off -- International Standard Atmosphere (ISA) day + 300C to
ISA + 350C; High altitude airports, 8,000 to 10,000 feet, at gross
weight with no wind condition; Accelerate-stop distance 3,737 feet; (e)
Crew -- Two crew numbers (pilot/co-pilot); (f) Equipment -- Survival
gear, baggage and law enforcement equipment totaling 300 lbs.; (g)
Payload -- Up to nine passengers; Minimum of 3,000 LBS payload
capability; (h) Maximum Gross Take Off Weight -- Includes aircraft
basic empty weight, payload, crew and maximum fuel/oil/hydraulic
fluids; (i) Service Life -- 15,000 operating hours. Instrumentation
package shall have: (a) Standard EFIS; (b) Davtron 811B clock at Pilot
and Co-pilot positions; (c) Backup airspeed and altitude indicators
shall operate independent of the primary electrical Systems; (d) Backup
attitude reference indicator. Communication/Navigation Equipment shall
be the standard Collins Pro-line II or equivalent equip, to include:
(a) Dual VHF; (b) Dual VOR/NAV; (c) ADF; (d) Radio Altimeter; (e)
Encoding Altimeter; (f) Dual Compass; (g) Dual DME with Hold Functions;
(h) Dual Marker Beacons; (i) Dual RMI -- Both VOR and ADF; (j) Dual
Transponder with Mode C and S; (k) Air Data Computer; (l) ELT
(Emergency Locator Transmitter); (m) TCAS (Threat Collision Avoidance
System); (n) Wulfsburg GNSX-LS Global Positioning System.
Intercommunications System (ICS) -- (a) The Intercommunication System
shall permit two-way communication between pilot and co-pilot; (b) The
pilot and co-pilot, shall have both transmit and receive capability on
all RF communication systems; (c) A rotating selector clearly marked
with ICS, VHF 1, VHF 2, HF, and FM shall be provided for audio
selection; (d) The pilot and co-pilot shall have individual speakers;
(e) The cabin area shall have a sufficient number of speakers so that
each passenger can hear all announcements. Autopilot System shall have
a 3-axis autopilot system with the following modes of operation:
healing, navigation, approach, back course, altitude hold, altitude
select, indicated airspeed hold, vertical airspeed hold, vertical trim,
soft ride, yam damper, command roll, turn, go around, and test. (a)
Navigation mode to couple with VOR/DME, and GPS; (b) TCS, SYNC, and
disconnect available to both pilot and co-pilot; (c) Flight Director --
Pilot and Co-pilot. Instrumentation/Avionic shall have: Allied Signal
Bendix/King package or equivalent to include: (a) KFC 325 Integrated
3-axis Automatic Flight Control System with 5-tube EFIS (w/center MFD)
including: KMC 321 Mode Controller, EFS 40/50 4 inch EFIS including:
ED462 EADI, ED462 EHSI, CP 468 Control Panel, SG 564 Symbol Generator;
(b) KMA 24H Audio Control Console/Intercom; (c) KX 165 COM/NAV (2
each); (d) KN 63 DME; (e) KR 87 Digital ADF System; (f) KNI 582 RMI;
(g) KI 204 CDI; (h) KAS 297C Attitude/Vertical Speed Preselector; (i)
KR 21 Marker Receiver & Lights; (j) KT 70 Transponder; (k) KEA 130A
Encoding Altimeter; (l) KLN 90B GPS Navigation System; (m) RDS 82 VP
Weather Radar /RDR 2000; (n) CAS 66A TCAS1; (o) Engine Trend Monitoring
System; (p) Ground Proximity Warning System; (q) HF Radio; (r) ELT
(narco ELT-910); (s) Stormscope; (t) Lifef AHRS-LCR 92. All interested
sources must submit their descriptive literature by Thursday, May 27,
1999 to: U.S. Department of Justice, Drug Enforcement Administration,
700 Army Navy Drive, Arlington, VA 22202. Any questions should be
directed to Ms. Doreen Upshur, 202-307-7807 (Collected Calls Will Not
Be Accepted). DEA does not attend to award a contract on the basis of
this request for information or otherwise pay for the information
solicited. Posted 05/12/99 (I-SN330563). (0132) Loren Data Corp. http://www.ld.com (SYN# 0173 19990514\15-0011.SOL)
15 - Aircraft and Airframe Structural Components Index Page
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