MODIFICATION
99 -- (UPDATED) Multi-Engine Jet Aircraft
- Notice Date
- 6/17/2003
- Notice Type
- Modification
- Contracting Office
- FEDERAL AVIATION ADMINISTRATION, ACX-51 W.J. Hughes Tech Center (ACT)
- ZIP Code
- 00000
- Solicitation Number
- DTFACT-03-R-00021
- Response Due
- 6/10/2003
- Point of Contact
- Kevin Dillon, 609.485.6911
- E-Mail Address
-
Email your questions to kevin.dillon@faa.gov
(kevin.dillon@faa.gov)
- Description
- *** THIS ANNOUNCEMENT IS HEREBY CANCELLED. A revised announcement will be forthcoming.*** In accordance with the FAA AMS Paragraph 3.2.1.3.12, the purpose of this announcement is to inform industry that the FAA William J. Hughes Technical Center intends to issue a firm fixed price contract for the purchase a new or used Multi-Engine Jet Aircraft to support FAA airborne Research and Development. The not-to-exceed ceiling price for this requirement is $14.9 million dollars. Minimum Specification: The following are the Minimum Requirements established for consideration as a eligible aircraft for this procurement. These requirements are Inclusive; all must be met for further consideration. The final selection will be made based on selection criteria in the Screening Information Request (SIR), and upon physical inspection of the aircraft and aircraft documents of highly ranked candidates. A. The aircrafts certification basis must be compliant with Code of Federal Regulations Title 14, Part 25. B. The aircraft must hold a valid and current US Airworthiness Certificate. C. The aircraft must be a multi-engine, turbofan jet. D. The aircraft must be equipped with a Electronic Flight Instrumentation System E. The aircraft must have Fully Digital Navigation, including: Dual Flight Management Systems, Dual Digital Air Data Computers, and Digital (Autopilot) Flight Guidance System. F. The Flight Management System must be capable of accepting the following navigation signals: GPS, VOR, DME, IRS and/or INS, MLS G. The aircraft must, in addition to the above, be equipped with at least the following avionics equipment: a. (2) VHF communication radios b. (2) VOR/DME/ILS navigation radios c. (1) ADF system d. (1) HF communication radio e. Voice Data Recorder f. Flight Data Recorder g. TCAS II h. GPWS H. The aircraft must be compliant with Code of Federal Regulations, Title 14, Part 36, Stage 3 Noise Levels, and the International Civil Aviation Organizations, Annex 16, Volume I, Noise Standards without the use of hush kits . I. The aircraft must be compliant with Code of Federal Regulations, Title 14, Part 91.706, Operations within airspace designated as Reduced Vertical Separation Minimum Airspace , and Part 91 Appendix G, section 91.2, Aircraft Approval . J. The aircraft must come equipped with, or, there must exist a current Supplemental Type Certificate, for the aircraft proposed, for a GPS navigation system. K. The aircraft must come equipped with an functioning Auxiliary Power Unit L. The aircraft interior must be fully furnished with sound deadening, headliner, sidewalls, seat tracks, heating and air conditioning distribution system, passenger service units (oxygen, lighting and air outlet), and at least one enclosed, flushing, externally serviced lavatory, as well as seating for at least 8 passengers. The interior must be a good condition with no obvious damage. M. The aircraft must have a maximum certificated ceiling of at least 41,000 feet. N. The aircraft must have an IFR range (no wind, ISA), with a payload of 3,200 pounds, of no less than 3000 nautical miles, with NBAA IFR fuel reserve criteria with 200 NM alternate. O. The aircraft must have a cabin length, from aft cockpit bulkhead to aft cabin bulkhead, of no less than 25 feet and a cabin height, from floor to ceiling, of no less than 6 feet. P. The aircraft must come equipped with, or, there must exist, a current Supplemental Type Certificate, for the aircraft proposed, for a self-contained method for boarding/deplaning passengers. Q. The aircraft must be current on all applicable required corrosion inspection, intervention or control programs, all aging aircraft inspections and repairs as specified in the manufacturers maintenance planning documents (MPD) or manufacturers approved maintenance schedules and/or all required maintenance actions as detailed in FAA ADs. R. The aircraft records must include a listing and suitable documentation for all major modifications and/or alterations accomplished on the aircraft. S. Maximum take off gross weight of the aircraft cannot be greater than 275,000 lbs.. Inspections: Offerors must permit FAA personnel and its contractors access to the aircraft for physical inspections, as well as, access to all aircraft records and documents. Documentation: The successful offeror must provide an approved Airplane Flight Manual, Log Books and all other aircraft records to the FAA William J. Hughes Technical Center, upon delivery of the aircraft. Delivery: The successful offeror will deliver the aircraft to the FAA William J. Hughes Technical Center, in Atlantic City, NJ and provide any assistance required to transfer ownership to the FAA. Certification The offerors will, as part of its proposal, certify for each aircraft offered that the aircraft: a. Has an accident free history with full ownership history b. Is availability for sale with a free and clear title c. Has no litigation pending that may impede the transfer d. Has been offered for sale by the legal owner or legally authorized agent e. Has never carried live animals, except domestic pets. Has a complete maintenance record. Award of this requirement will result in a Firm Fixed Price Contract based on Best Value Criteria. The solicitation will be posted on this website on or about June 10,2003. This is a competitive solicitation. This is not a request for sources.
- Web Link
-
FAA Contract Opportunities
(http://www.asu.faa.gov/faaco/index.htm)
- Record
- SN00349463-W 20030619/030617213316 (fbodaily.com)
- Source
-
FedBizOpps.gov Link to This Notice
(may not be valid after Archive Date)
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