R8_LFW_Sol_AG-43N9-S-13-0002.docx
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- Region 8 Call When Needed Light Fixed Wing AircraftServices Amendment 2 Federal contract opportunity
- Solicitation number
- AG-43-N9-S-13-0002
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Offeror's Copy of the Notice of solicitation for light fixed wing aircraft on a call when needed basis the Standard Form 1449 (SF1449) and instructions (Section E)
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Text version
| USDA Forest Service | FS-5700-20 (05/2015) |
| OMB 0596-0015 Exp. 5/2014 |
OFFEROR’S COPY
(Ref. 48 CFR 1)
Issuing Office:
U.S. FOREST SERVICE, CONTRACTING
1720 Peachtree Road, Suite 876S Atlanta, GA 30309
This solicitation can be downloaded from the following Internet site: https://www.fbo.gov/
Offers Are Solicited For:
Interagency Call-When-Needed Light Fixed Wing Aircraft - Region 8
Solicitation No:
AG-43N9-S-13-0002
Issued Date:
July 12, 2013
IMPORTANT – NOTICE TO OFFEROR
Offers will be due on 07/29/2013 @ 4:30 PM Eastern Daylight Time.
The offeror shall submit the following items in response to this solicitation:
1. SF-1449, blocks 17a - Name, Address, DUNS and TIN, 30a-30c: Complete, date, and sign.
2. Fill in the appropriate information requested under section B-1, B-2, B-3, and B-5.
3. Provide one copy of your Business proposal and 2 copies of your Technical proposal in response to Section E-2 of the solicitation.
4. Provide your responses to Section E-5, E-6, and E-7 of the solicitation.
THE SOLICITATION PACKAGE SHALL BE RETURNED TO THE FOLLOWING ADDRESS:
U.S. FOREST SERVICE, CONTRACTING
ATTN: SOLICITATION # AG-43N9-S-13-0002
1730 PEACHTREE ROAD SUITE 876S
ATLANTA, GA 30309
No facsimile (FAX) or e-mail offers will be accepted.
Bidders Questions must be submitted and received via e-mail NLT July 18, 2013.
E-mail: GRSanders@fs.fed.us With Subject line for Solicitation No. AG-43N9-S-13-0002. Mail to the Issuing Office address identified above. Offerors may contact Gloria Sanders for information at 404-347-4023.
“The policy of the United States Department of Agriculture Forest Service prohibits discrimination on the basis of race, color, national origin, age, religion, sex, disability, family status, and/or political affiliation.” Persons believing they have been discriminated against in any Forest Service related activity should write to: Chief, Forest Service, USDA, P. O. Box 96090, Washington, DC 20090-6090.
| Previous editions of this form are obsolete. |
| FS-6300-44 (11/79) |
SECTION A - SOLICITATION/CONTRACT/ORDER FOR COMMERCIAL ITEMS
STANDARD FORM 1449
SECTION B - SUPPLIES OR SERVICES AND PRICE
| B-1 | SCHEDULE OF ITEMS | B-1 |
| B-2 | GOVERNMENT FURNISHED PILOT | B-2 |
| B-3 | HOME BASE (Base from which aircraft would normally be available) | B-2 |
| B-4 | TAXES | B-2 |
| B-5 | MAINTENANCE CAPABILITY | B-3 |
| B-6 | PERFORMANCE PERIOD | B-3 |
| B-7 | CONTRACTOR PERFORMANCE ASSESSMENT REPORTING SYSTEM (CPARS) | B-3 |
SECTION C - DESCRIPTION/ SPECIFICTIONS
| C-1 | SCOPE OF AGREEMENT | C-1 |
| C-2 | GENERAL CERTIFICATIONS | C-1 |
| C-3 | GOVERNMENT FURNISHED PROPERTY | C-1 |
| C-4 | AIRCRAFT REQUIREMENTS | C-1 |
| C-5 | AIRCRAFT MAINTENANCE | C-5 |
| C-6 | AIRCRAFT AND EQUIPMENT SECURITY | C-6 |
| C-7 | AVIONICS REQUIREMENTS | C-6 |
| C-8 | FURNISHED AVIONICS SYSTEMS | C-6 |
| C-9 | AVIONICS INSTALLATION AND MAINTENANCE STANDARDS | C-18 |
| C-10 | OPERATIONS | C-18 |
| C-11 | PERSONNEL | C-21 |
| C-12 | CONDUCT AND REPLACEMENT OF PERSONNEL | C-23 |
| C-13 | SUSPENSION AND REVOCATION OF PERSONNEL | C-24 |
| C-14 | SUBSTITUTION OR REPLACEMENT OF PERSONNEL, AIRCRAFT, AND EQUIPMENT | C-24 |
| C-15 | RELIEF PILOT | C-25 |
| C-16 | FLIGHT HOUR AND DUTY LIMITATIONS | C-25 |
| C-17 | ACCIDENT PREVENTION AND SAFETY | C-26 |
| C-18 | MISHAPS | C-26 |
| C-19 | PERSONAL PROTECTIVE EQUIPMENT (PPE) | C-28 |
| C-20 | INSPECTION AND ACCEPTANCE | C-28 |
| C-21 | PRE-USE INSPECTION EXPENSES | C-29 |
| C-22 | RE-INSPECTION EXPENSES | C-30 |
| C-23 | INSPECTIONS DURING USE | C-30 |
| C-24 | PERIOD OF BASIC ORDERING AGREEMENT | C-30 |
| C-25 | AUTHORIZED ORDERING ACTIVITIES | C-30 |
| C-26 | ORDERING PROCEDURES | C-31 |
| C-27 | POINT OF HIRE | C-31 |
| C-28 | ASSIGNED WORK LOCATION(S) | C-31 |
| C-29 | ORDERED STANDBY | C-32 |
| C-30 | PAYMENT FOR FLIGHT | C-32 |
| C-31 | PAYMENT FOR CANCELLED, DELAYED OR SHORT DURATION FLIGHT | C-32 |
| C-32 | CONTRACTOR STAND-DOWN OR DEACTIVATION | C-33 |
| C-33 | RESERVED | C-33 |
| C-34 | ADDITIONAL AIRCRAFT AFTER ESTABLISHMENT OF THE AGREEMENT | C-34 |
| C-35 | FOOD AND DRINK | C-34 |
| C-36 | MISCELLANEOUS COSTS TO THE CONTRACTOR | C-34 |
| C-37 | PAYMENT FOR OVERNIGHT ALLOWANCE | C-34 |
| C-38 | PAYMENT PROCEDURES | C-34 |
| C-39 | PERFORMANCE BY GOVERNMENT-FURNISHED PILOT | C-34 |
| C-40 | DEFINITIONS | C-37 |
| C-41 | ABBREVIATIONS | C-41 |
| ATTACHMENT 1 - WAGE DETERMINATION | C-43 | |
| ATTACHMENT 2 - PUBLIC AIRCRAFT OPERATIONS DECLARATION | C-47 | |
| ATTACHMENT 3 - CPARS EVALUATION FORM | C-48 |
SECTION D - CONTRACT CLAUSES
| D-1 | CONTRACT CLAUSES INCORPORATED BY REFERENCE | D-1 |
| D-2 | ADDENDUM TO 52.212-4 CONTRACT TERMS AND CONDITIONS - COMMERCIAL ITEMS | D-1 |
| D-3 | RESERVED | D-1 |
| D-4 | UPDATES OF PUBLICLY AVAILABLE INFORMATION REGARDING RESPONSIBILITY MATTERS | D-1 |
| D-5 | OPTION TO EXTEND SERVICES | D-2 |
| D-6 | OPTION TO EXTEND THE TERM OF THE CONTRACT | D-2 |
| D-7 | STATEMENT OF EQUIVALENT RATES FOR FEDERAL HIRES | D-3 |
| D-8 | AVAILABILITY OF FUNDS | D-3 |
| D-9 | PROPERTY AND PERSONAL DAMAGE | D-3 |
| D-10 | CONTRACT TERMS AND CONDITIONS REQUIRED TO IMPLEMENT STATUTES OR EXECUTIVE ORDERS - COMMERCIAL ITEMS | D-4 |
| D-11 | ASSURANCE REGARDING FELONY CONVICTION OR TAX DELINQUENT STATUS FOR CORPORATE APPLICANTS | D-10 |
SECTION E - INSTRUCTIONS TO OFFERORS/EXHIBITS
| E-1 | INSTRUCTIONS TO OFFERORS - COMMERCIAL ITEMS | E-1 |
| E-2 | EVALUATION-COMMERCIAL ITEMS | E-2 |
| E-3 | AWARD PROCESS | E-3 |
| E-4 | MISSION SAFETY BRIEFING BULLET TOPICS & CERTIFICATION STATEMENT | E-3 |
| E-5 | OFFEROR REPRESENTATIONS AND CERTIFICATIONS-COMMERCIAL ITEMS | E-3 |
| E-6 | CERTIFICATION REGARDING RESPONSIBILITY MATTERS | E-18 |
| E-7 | INFORMATION REGARDING RESPONSIBILITY MATTERS | E-19 |
| E-8 | REPRESENTATION BY CORPORATIONS REGARDING AN UNPAID DELINQUENT TAX LIABILITY OR A FELONY CONVICTION | E-20 |
| E-9 | INSPECTION AND ACCEPTANCE | E-21 |
| EXHIBIT 1 - PAST PERFORMANCE INFORMATION | E-21 | |
| EXHIBIT 2.- SUMMARY OF ACCIDENTS | E-23 | |
| EXHIBIT 3.- SYNOPSIS OF SAFETY PROGRAM | E-24 |
EXHIBIT 4 - AIRPLANE PILOT QUALIFICATIONS AND APPROVAL RECORD……………………..E-28
| EXHIBIT 5 - LIGHT FIXED WING MISSION SAFETY BRIEFING BULLET TOPICS | E-30 |
| Solicitation No. AG-43N9-S-13-0002 | U.S. Forest Service |
Region 8 Call When Needed Light Fixed Wing Services
TABLE OF CONTENTS
| i |
| SOLICITATION/CONTRACT/ORDER FOR COMMERCIAL ITEMS |
OFFEROR TO COMPLETE BLOCKS 12, 17, 23, 24, & 30
1. REQUISITION NUMBER
2. CONTRACT NO.
3. AWARD/EFFECTIVE
DATE
4. ORDER NUMBER
5. SOLICITATION NUMBER
AG-43N9-S-13-0002
6. SOLICITATION ISSUE DATE
7/9/2013
7. FOR SOLICITATION
INFORMATION CALL:
a. NAME Gloria Sanders
b. TELEPHONE NUMBER (No collect calls) (404)347-4023
8. OFFER DUE DATE/ LOCAL TIME
07/29/2013
4:30 PM EDT
| 9. ISSUED BY |
| CODE |
10. THIS ACQUISITION IS |_| UNRESTRICTED OR |X| SET ASIDE: 100% FOR:
U.S. FOREST SERVICE – CONTRACTING
1720 Peachtree Road Suite 876S Atlanta, GA 30309
| |X| |
| SMALL BUSINESS |
| |_| |
| WOMEN-OWNED SMALL BUSINESS |
(WOSB) ELIGIBLE UNDER THE WOMEN-OWNED
SMALL BUSINESS PROGRAM
| |_| |
| HUBZONE SMALL BUSINESS |
| |_| |
| (EDWOSB) |
| NAICS: 481212 |
| |_| |
| SERVICE-DISABLED VETERAN-OWNED SMALL BUSINESS |
| |_| |
| 8 (A) |
| SIZE STANDARD: |
1,500 Employees
11. DELIVERY FOR FOB DESTINA- TON UNLESS BLOCK IS MARKED
|X| SEE SCHEDULE
| 12. DISCOUNT TERMS |
| |_| 13a. THIS CONTRACT IS A |
| RATED ORDER UNDER |
| DPAS (15 CFR 700) |
| 13b. RATING |
| 14. METHOD OF SOLICITATION | ||
| |_| RFQ | |_| IFB | |X| RFP |
| 15. DELIVER TO |
| CODE |
| 16. ADMINISTERED BY |
| CODE |
See Block 9
| 17a. CONTRACTOR/ |
| CODE |
FACILITY
| 18a. PAYMENT WILL BE MADE BY |
| CODE |
| OFFEROR |
| CODE |
| ALBUQUERQUE SERVICE CENTER |
INCIDENT BUSINESS – CONTRACTS
101B SUN AVENUE, NE
ALBUQUERQUE, NM 87109
TELEPHONE NO. NINE-DIGIT DUNS NO. .
| |_| 17b CHECK IF REMITTANCE IS DIFFERENT AND PUT SUCH ADDRESS IN | |
| OFFER | |
| 18b. | SUBMIT INVOICES TO ADDRESS SHOWN IN BLOCK 18a UNLESS BLOCK BELOW IS CHECKED |
|_| SEE ADDENDUM
19.
ITEM NO.
20.
SCHEDULE OF SUPPLIES/SERVICES
21.
QUANTITY
22.
UNIT
23.
UNIT PRICE
24.
AMOUNT
SEE SECTION B (ATTACHED)
CALL WHEN NEEDED LIGHT FIXED WING AIRCRAFT-
SOUTHERN REGION (R8)
25. ACCOUNTING AND APPROPRIATION DATA
26. TOTAL AWARD AMOUNT (For Govt. Use Only)
|X| 27a. SOLICITATION INCORPORATES BY REFERENCE FAR 52.212-1, 52.212-4. FAR 52.212-3 AND 52.212-5 ARE ATTACHED. ADDENDA |X| ARE |_| ARE NOT ATTACHED |_| 27b. CONTRACT/PURCHASE ORDER INCORPORATES BY REFERENCE FAR 52.212-4. FAR 52.212-5 IS ATTACHED. ADDENDA |_| ARE |_| ARE NOT ATTACHED
| |X| 28. CONTRACTOR IS REQUIRED TO SIGN THIS DOCUMENT AND RETURN 1 . COPY TO ISSUING OFFICE. CONTRACTOR AGREES TO FURNISH AND DELIVER ALL ITEMS SET FORTH OR OTHERWISE IDENTIFIED ABOVE AND ON ANY ADDITIONAL SHEETS SUBJECT TO THE TERMS AND CONDITIONS SPECIFIED HEREIN. |
| |_| 29. AWARD OF CONTRACT: REF. _________________ __ OFFER |
DATED _______________ . YOUR OFFER ON SOLICITATION (BLOCK 5), INCLUDING ANY ADDITIONS OR CHANGES WHICH ARE SET FORTH HEREIN, IS ACCEPTED AS TO ITEMS:
| 30a. SIGNATURE OF OFFEROR/CONTRACTOR |
| 31a. UNITED STATES OF AMERICA (SIGNATURE OF CONTRACTING OFFICER) |
| 30b. NAME AND TITLE OF SIGNED (Type or print) |
| 30c. DATE SIGNED |
| 31b. NAME OF CONTRACTING OFFICER (Type or print) |
| 31c. DATE SIGNED |
AUTHORIZED FOR LOCAL REPRODUCTION
PREVIOUS EDITION NOT USABLE
STANDARD FORM 1449 (REV. 2/2012)
Prescribed by GSA - FAR (48 CFR) 53.212
Amendment 01
B-1 SCHEDULE OF ITEMS
This is a Basic Ordering Agreement (BOA) for fully operated and maintained light fixed wing aircraft services on a Call-When-Needed (CWN) basis. Services shall be rendered throughout the Southern Region (R 8) of the United States Forest Service (USFS). Aircraft shall meet the requirements of this schedule and the specifications included herein. Offerors shall list each aircraft to be considered for award.
Mission Codes
| A. Point-to Point |
| D. Resource Reconnaissance |
| B. Air Tactical |
| E. Other (i.e., Mountain Remote) |
C. Fire Reconnaissance
Note: Mission Codes, Weight and Fuel Charts and Equipment Codes apply to all years to include the Base Year and four (4) option years (FY 2014 through FY 2018).
Note: Region 8 will not award to offers of only Point-to-Point Aircraft services.
Note: Any aircraft offered for Air Tactical shall meet the Air Tactical Type 1 Standard. Region 8 will not award to bidders for any other type of Air tactical standards. Such aircraft will be considered for Reconnaissance only.
Solicitation No. AG-43N9-S-13-0002 U.S. Forest Service Region 8 Call When Needed Light Fixed Wing Services
SECTION B
SUPPLIES OR SERVICES AND PRICE
B-3
| AIRCRAFT | HOURLY RATES | |
| Item |
No.
Tail No.
| Make Model Year |
| Mission Codes/1 |
| Flt Rate Base Year |
| Flt Rate 2015 |
| Flt Rate 2016 |
| Flt Rate 2017 |
| Flt Rate 2018 |
| Ordered Standby Rate |
Base Year Ordered Standby Rate Ordered Standby Rate Ordered Standby Rate Ordered Standby Rate Add’l Pilot Rate
1.
2.
3.
4.
5.
6.
OFFERED AIRCRAFT
(Contractor to Complete this Chart)
| Item No. |
| Empty Weight |
| HP |
| Fuel (1) |
| Fuel Type |
J = Jet A L= Low Lead
| Maximum Certified Gross Weight |
| Equipment & Capacity Code (2) |
1.
2.
3.
4.
5.
6.
(1) Fuel consumption expressed in gallons per hour at 65% power, at 5,000 feet MSL, at ISA, as stated in Aircraft Flight Manual.
(2) Use Key Below Note: List additional aircraft on separate sheet using same format.
EQUIPMENT CAPACITY CODES
| A. |
| Single Engine – (# of seats: ____) Indicate on chart # of seats following the code. |
(i.e., A 2 = single engine with 2 seats)
| B. |
| Multi Engine – (# of seats: ____) Indicate on chart # of seats following the code |
(i.e., B 4 = multi engine with 4 seats)
| C. |
| Large Cargo Doors |
| D. |
| High Wing |
| E. |
| Low Wing |
| F. |
| Turbocharged |
| G. |
| Turboprop |
| H. |
| Jet |
| I. |
| Pressurized |
| J. |
| Non-Pressurized |
| K. |
| Oxygen |
| L. |
| Air Tactical Avionics Type 1 |
| M. |
| Air Tactical Avionics Type 2 |
| N. |
| Air Tactical Avionics Type 3 |
| O. |
| Air Tactical Avionics Type 4 |
| P. |
| Relief Pilot(s) Available |
| Q. |
| Infrared |
| R. |
| RESERVED |
| S. |
| Aerial Photography |
| T. |
| TCAS/TCAD |
| U. |
| Floats: 1. Amphibious 2. Straight |
| V. |
| Other |
| *Note: | In pressurized and non-pressurized aircraft, Pilots shall meet 14 CFR Part 135 Oxygen Requirements. |
| B-2 | GOVERNMENT FURNISHED PILOT |
Contractor will |_| will not |_| authorize performance of work under the agreement by a Government Pilot. Note Government requirements in Section C-39.
Flight rate w/o Pilot:
B-3 HOME BASE (Base from which aircraft would normally be available) Offeror shall enter the location of their home base. The same aircraft number will not be awarded /administered under more than one Forest Service CWN agreement within the Southern Region.
| _______________________________________ | _____________ |
| Location (Physical Address) | State |
Note: Offers for furnishing services on a “Call-When-Needed” Basis are being solicited from operators/contractors located in the USFS Region 8 (Southern Region).
B-4 TAXES
Taxes shall be included in your agreement price in accordance with FAR Clause 52.212-4(k). The contract price includes all applicable Federal, State, and local taxes and duties.
B-5 MAINTENANCE CAPABILITY
Contractor shall provide the name and address of the Director of Maintenance and the repair facility:
| Director of Maintenance (Name) |
| Business Address |
| Cell Phone No. |
| Phone No. |
Fax No.
| Repair Facility |
| Business Address |
Phone No.
Fax No.
The Government may inspect the Contractor’s operation and maintenance facilities prior to award.
B-6 PERFORMANCE PERIOD
The performance period for the CWN agreement shall be in effect for a period of up to five fiscal years. The Base year will be effective 10/1/2013, with four (4) optional year periods. The fiscal year begins October 1, and ends on September 30 each year.
B-7 CONTRACTOR PERFORMANCE ASSESSMENT REPORTING SYSTEM (CPARS)
The Contractor Performance Assessment Reporting System (CPARS) shall be used by the Forest Service to track performance. For details, please visit, http://www.cpars.gov/
| C-1 | SCOPE OF AGREEMENT |
| (a) | The Government wishes to obtain services on a call when needed (CWN) basis of light fixed wing aircraft fully operated by qualified contractor personnel and equipped to meet specifications for use in administration and protection of Public Lands throughout the Southern Region (Region 8). |
(b)The aircraft furnished shall be used for fire support, project, law enforcement, and administrative flights. If the Contractor agrees to perform law enforcement flights, such agreement shall be in writing.
| (c) | The Government has Interagency and Cooperative agreements with Federal and State Agencies and private landholders. Aircraft may be dispatched under this agreement for such use. |
| C-2 | GENERAL CERTIFICATIONS |
| (a) | Contractors shall hold a current Federal Aviation Administration (FAA) Air Carrier or Operating Certificate. Aircraft offered shall be listed by make, model, series, and registration number on the Operators 135 Certificate. |
| (b) | Aircraft shall conform to its approved type design, be maintained and operated in accordance with the requirements of the 14 CFR 135 notwithstanding the aviation regulations of the States in which the aircraft may operate except those requirements specifically waived by the CO. |
| C-3 | GOVERNMENT FURNISHED PROPERTY |
| (a) | If Government Furnished Property (GFP) is provided, the Contractor shall be required to sign a property receipt document. Upon Government request, GFP shall be returned to the Government in accordance with GFP (Short Form) FAR Clause 52.245-1 (Apr 2012). |
| C-4 | AIRCRAFT REQUIREMENTS |
| (a) | Aircraft Performance Requirements |
| (1) | Single engine aircraft shall have a power loading of not more than 13.5 pounds per horse power. |
| (2) | Each takeoff shall meet aircraft climb performance requirements of 14 CFR. |
| (a) | Positive single engine rate of climb when equipped for the contract and carrying a pilot weighing 200 lbs, one observer weighing 220 lbs, fuel for 4 hours plus a 30 minute reserve, @ 5000 ft. pressure altitude @ ISA- plus 33. |
(3) Multi engine aircraft shall be capable of at least 200 horse power per engine; any engine developing less than 240 horse power shall be turbo/super charged.
(4) Cruise speed of 165 knots True Airspeed (TAS) @ 8000 ft. – ISA plus 20
(5) Cruise endurance of 4 hours @ 8000 ft – ISA plus 20 C plus a 30 minute reserve
| (b) | Aircraft condition and equipment. The aircraft shall be in airworthy condition throughout the performance period. All equipment required for original certification shall be installed and operable or be deferrable by an FAA approved Minimum Equipment List (MEL). |
| (1) | All aircraft furnished under this agreement shall be operable, free of damage, and in good working order. Aircraft systems and components shall be free of leaks, except within limitations specified by the manufacturer. |
| (2) | The aircraft interior shall be clean and neat. There shall be no un-repaired tears, rips, cracks, or other damage to the interior. All interior materials shall meet FAA standards. |
| (3) | The aircraft exterior finish, including the paint, shall be clean, neat, and in good condition (i.e., no severe fading or large areas of flaking or missing paint etc.) Military or other low visibility paint schemes are unacceptable. Any corrosion shall be within manufacturer or FAA acceptable limits. |
| (4) | All windows and windshields shall be clean and free of scratches, cracks, crazing, distortion, or repairs, which hinder visibility. Repairs such as safety wire lacing and stop drilling of cracks are not acceptable as permanent repairs. Prior to acceptance, all temporarily repaired windows and windshields shall have permanent repairs completed or shall be replaced. |
| (5) | Fire extinguishers, as required by 14 CFR 135.155, shall be hand-held bottle(s), with a minimum of 1.5 lbs capacity and 2-B:C rating. Fire Extinguishers shall be maintained in accordance with current NFPA 10 standards and mounted with a quick release attachment accessible to the flight crew while seated. |
| (6) | Each aircraft shall carry current copies of the following: |
| (i) | Basic Ordering Agreement and all modifications. |
| (ii) | Department of Transportation (DOT) Exemption 9198, the Interagency Aviation Transport of Hazardous Materials Handbook/Guide (NFES 1068) and the Emergency Response Guide (ERG) if required. |
| (iii) | Aeronautical charts covering area of operation |
| (7) | Flight Hour Meter. Each aircraft shall be equipped with a flight hour meter, installed in a location observable by the pilot and front seat observer while seated. The meter shall measure actual flight time from takeoff to landing in hours and tenths. |
| (8) | Cargo Restraint. The Contractor shall furnish tie downs, net(s), or cargo straps meeting requirements of 14 CFR to restrain cargo while in flight. |
| (9) | Safety Belts. The aircraft furnished under this agreement shall have safety belts for all occupants and shoulder harnesses for front seat occupants meeting requirements of 14 CFR. The shoulder strap and lap belt shall fasten with a metal to metal single point quick release mechanism. Military style harnesses are acceptable. All occupants shall meet the above requirements during takeoffs and landings, when flying within 1,000 feet of the ground, and at other times as specified by the Pilot. |
Lap belt and shoulder harness condition; the following are NOT acceptable:
(i) Webbing. Webbing that is frayed 5 percent or more, torn webbing, crushed webbing, swelled webbing that results in twice the thickness of original web, or if difficult to operate through hardware, creased webbing (no structural damage allowed), and sun deterioration if it results in severe fading, brittleness, discoloration, and stiffness.
| (ii) | Hardware. Buckle or other hardware is inoperable, nylon bushing at shoulder harness-to-lap belt connection missing or damaged, fabricated bushings or tie wraps used as bushings, rust/corrosion if not minor in nature, wear beyond normal use. |
| (iii) | Stitches. Broken or missing stitches, severe fading or discoloring, inconsistent stitch pattern. |
| (iv) | Technical Standard Order (TSO) Tags (see 14 CFR 21.607). Missing or illegible tags are unacceptable unless inspection can confirm the suitability of installed equipment. |
| (v) | Age. Belts/fabric over 10 years from date of manufacture require close inspection because of the elements they are exposed to, but do not have to be replaced if it can be determined they are in serviceable condition and not life limited. |
| (10) | First Aid Kit (Aeronautical). First aid kit shall be in a dust-proof and moisture-proof container. The kit shall be readily accessible to the Pilot and passengers. At a minimum, the contents shall include the following items: |
| Item Description | |
| Quantity |
| Adhesive bandage strips (3 inches long) |
| 8 |
| Antiseptic or alcohol wipes (packets) |
| 10 |
| Bandage compresses, (4 inches) |
| 4 |
| Triangular bandage compresses, 40 inch (sling) |
| 2 |
| Roller bandage, 4 inch x 5 yards (gauze) |
| 2 |
| Adhesive tape, 1 inch x 5 yards (standard roll) |
| 1 |
| Bandage scissors |
| 1 |
| Body Fluids Barrier Kit: |
| 1 |
2-pair of non-latex surgical gloves
1-face shield
1-mouth-to-mouth barrier
1-protective gown
2-antiseptic towelettes
1-biohazard disposal bag
Note: Splints are recommended if space permits.
| Kits may be commercially available types which are FAA approved for the appropriate number of crew and passengers carried. | |
| (11) | Survival Kit. Aircraft carded for any mission designations other than point-to-point only shall have sufficient equipment to sustain personnel for a 24-hour period. As a minimum, the survival kit shall include the following: |
· Knife
· Signal Mirror
· Aviation-type Signal Flares (6-each)
· Matches (2-small boxes in waterproof containers)
· Magnesium Fire Starter
· Space Blanket (1-per occupant)
· Water (1-quart per occupant – not required when operating over areas with adequate drinking water)
· Collapsible Water Bag
· Food (2-days emergency rations per occupant)
· Candles
· Whistle
· Nylon Rope or Parachute Cord (50 feet) Suggested additional survival kit items (appropriate to the geographic area.)
· Individual First Aid Kit
· Container w/carrying Handle or Straps
· Large Plastic Bags
· Signal Panels
· Flashlight with Spare Batteries
· Hand Saw or Wire Saw
· Collapsible Shovel
· Sleeping Bag (1-per two occupants)
· Survival Manual
· Snowshoes
· Axe or Hatchet
· Insect Repellant
· Insect Head net (1-per occupant)
· Gill Net/Assorted Fishing Tackle
· Personal ELT
· Sunscreen Note: A hand-held 760 channel VHF transceiver radio or satellite phone is recommended. It should be located on a crewmember rather than placed in the aircraft survival kit.
| C-5 | AIRCRAFT MAINTENANCE |
| (a) | All aircraft shall be maintained to 14 CFR Part 43, 91, and 135 standards. The Contractor shall provide or arrange for sufficient maintenance capability to keep the aircraft in airworthy condition. |
| (b) | The Contractor shall identify the maintenance facilities and/or maintenance personnel used to fulfill the requirements of this agreement. |
| (c) | Aircraft operated with components and accessories on FAA approved Time Between Overhaul (TBO) extension programs are acceptable, provided the Contractor who provides the aircraft is the holder of the approved extension authorization (not the owner if the aircraft is leased), and shall operate in accordance with the extension. |
| (d) | Compliance with applicable mandatory manufacturer's service bulletins, alert service bulletins, and safety of flight bulletins as required by FAA Operations Specifications; FAA Airworthiness Directives (AD); and the correction of maintenance deficiencies shall be accomplished prior to delivery and continue during agreement period of performance. If referenced in Section B, schedule of items, additional mandatory manufacturer's service bulletins, alert service bulletins or safety of flight bulletins shall be required. |
| (e) | All maintenance shall be accomplished in accordance with the standards established by 14 CFR Part 43, 91, and 135, and the manufacturer's instructions and in accordance with those procedures established in the Contractor's maintenance program approved under 14 CFR Part 135 Operations Specifications. |
| (f) | A copy of the current maintenance record required by 14 CFR 91.417 shall be kept at the Home Base or maintenance facility. |
| (g) | A functional check flight shall be performed at the Contractor's expense following overhaul, repair, and replacement of any engine (installations of reciprocating engines that are new, rebuilt, or overhauled shall accumulate 3-hours of operation, including 2 hours in flight, prior to Government use), power train, or control equipment, and following any adjustment of the flight control systems before the aircraft resumes service. The result of any test flight shall be logged in the aircraft flight records by the Pilot. Results of test flights shall be reported to the U.S. Forest Service Aircraft Maintenance Inspector (AMI) before the aircraft is returned to service. |
| (h) | When any non-scheduled maintenance or repairs are performed due to mechanical or equipment deficiencies, an AMI and the Contracting Officer (CO) shall be notified before the aircraft performs any ordered services. |
| (i) | The Interagency Airplane Data Record Card or Point-to-Point Aircraft Data Card shall be posted inside the aircraft. |
| (j) | The aircraft’s required weight and balance data shall be determined by actual weighing of the aircraft every 36 calendar months for multi-engine aircraft. Mission Use Only single engine aircraft shall be weighed within the previous 5 years. |
All weighing of aircraft shall be performed on scales that have been certified within the previous 12 months. The certifying agency may be any accredited weights and measures laboratory.
| C-6 | AIRCRAFT AND EQUIPMENT SECURITY |
| (a) | The security of Contractor provided aircraft and equipment is the responsibility of the Contractor. |
| (b) | Aircraft shall be electrically and/or mechanically disabled by two independent security systems whenever the aircraft is unattended. Deactivating security systems shall be incorporated into preflight checklists to prevent accidental damage to the aircraft or interfere with safety of flight. |
| (c) | Examples of Unacceptable disabling systems are: |
| (1) | Locked door/windows; and/or |
| (2) | Fenced parking areas. |
| C-7 | AVIONICS REQUIREMENTS |
Required avionics systems and Contractor offered avionics/communication equipment shall meet the performance specifications as specified in FS/AMD A-24 at: www.nifc.gov/NIICD/documents.html
C-8 FURNISHED AVIONICS SYSTEMS
The following required avionics systems shall be furnished, installed, and maintained by the Contractor in accordance with the manufacturer’s specifications and the installation and maintenance standards. Point-to-point flights require no additional systems other than those required by 14 CFR Part 135.
| (a) | Aircraft Avionics. The use of VHF-FM mobile (vehicle type) radios in aircraft is prohibited. |
| (b) | Aircraft operating to or from airfields or airstrips designated as Category 4 and are not otherwise conducting a type of reconnaissance flight, Resource Reconnaissance, Fire Reconnaissance, and other special mission aircraft shall be configured as required by use defined in this section. The operating capabilities of this equipment shall be that as defined below. |
| (1) | All aircraft operating to or from airfields or airstrips designated as Category 4 (Mountain/Remote), Resource Reconnaissance, Fire Reconnaissance, and other special mission aircraft will have as a minimum the following basic avionics listed in (1) & (2), for air tactical missions the avionics listed in (c) (1) through (5) apply: |
| (i) | An Emergency Locator Transmitter (ELT). |
| (ii) | An Aeronautical VHF-AM Radio Transceiver (VHF-1). |
| (iii) | Instruments and lighting for 14 CFR Part 135 night VFR operations (135.159 & 135.161). |
| (iv) | A GPS Unit. |
| (v) | An Automated Flight Following (AFF) system. |
and
(vi) One (minimum) VHF-FM Aeronautical Antenna.
or
(vii) Provisions for one (minimum) Auxiliary VHF-FM Portable Radio (AUX-FM).
or the following three (3) items.
| (viii) | An Audio Control System. |
| (ix) | An Aeronautical P25 Digital VHF-FM Radio Transceiver (FM-1). Only FHP aircraft may use certain analog aeronautical VHF-FM radio transceivers |
| (x) | An Intercommunications System. |
| (2) | Additional Fire Reconnaissance Requirements. Fire Reconnaissance aircraft shall have a dedicated Air Guard receiver. |
| (c) | Air Tactical Aircraft. All Air Tactical aircraft shall be configured as required by Type(s) defined in this section. The operating capabilities of this equipment shall be that as defined below. |
| (1) | All Air Tactical Types: |
| (i) | An Emergency Locator Transmitter (ELT). |
| (ii) | Two 760 channel Aeronautical VHF-AM Radio Transceivers (VHF-1 & VHF-2). |
| (iii) | Instruments and lighting for 14 CFR Part 135 night VFR operations (135.159 & 135.161). |
| (iv) | A Transponder, Altitude Encoder and Static Systems. |
| (v) | An Automated Flight Following (AFF) system. |
| Note: | Regardless of available aircraft equipment or capabilities, Supplemental Air Attack Kit installations in any Type shall not elevate the aircraft’s capability beyond that Type for which the aircraft would normally be carded, if the supplemental radio kit were removed. |
| Note: | If an approved Traffic Advisory System (TAS) is furnished, the aircraft shall be identified as a “Type I with TAS” or a “Type II with TAS”. |
| (2) | Type I: |
| (i) | A Panel Mounted GPS Unit. |
| (ii) | Separate Audio Control Systems for the PIC and SIC/ATGS. |
| (iii) | A set of audio/mic jacks with PTT capability in the rear seat for an ATGS instructor connected to the SIC/ATGS’s audio control system. A separate Audio Control System for the instructor is acceptable. |
| (iv) | Two permanently installed Aeronautical P25 Digital VHF-FM Radio Transceivers (FM-1 & FM-2). |
| (v) | An Intercommunication System |
and either
(vi) Provisions for an Auxiliary VHF-FM Portable Radio (AUX-1).
or
| (vii) | A third Aeronautical P25 Digital VHF-FM Radio Transceiver (FM-3). |
| (d) | Selected Additional Avionics Requirements. The following additional items may be required to meet local needs. When the option block |_| is checked, the operator shall install and maintain the checked equipment. If an item is checked and already is a required item, then the checked item is an additional requirement. The operating capabilities of this equipment shall be that as defined below. |
| |_| | An Accessory Power Source. |
| |_| | A second Aeronautical VHF-AM 760 Channel Radio Transceiver (VHF-2). |
| |_| | A third Aeronautical VHF-AM 760 Channel Radio Transceiver (VHF-3). |
| |_| | An Aeronautical P25 Digital VHF-FM Radio Transceiver (FM-1). |
| |_| | A second Aeronautical P25 Digital VHF-FM Radio Transceiver (FM-2). |
| |_| | A third Aeronautical P25 Digital VHF-FM Radio Transceiver (FM-3). |
| |_| | Provisions for an Auxiliary VHF-FM Portable Radio (AUX). |
| |_| | VHF-FM Programming Port. |
| |_| | A UHF Aeronautical Radio Transceiver (UHF). |
| |_| | A Low Band Aeronautical Radio Transceiver (LB). |
| |_| | A Non-Standard VHF-FM Aeronautical Transceiver (FM) for communications with the Forest Service. |
| |_| | A Non-Standard UHF Aeronautical Transceiver (UHF) for communications with the Forest Service. |
| |_| | A Non-Standard 700-800 MHz Aeronautical Transceiver (800) for communications with the Forest Service. |
| |_| | A VHF-FM Aeronautical Antenna. |
| |_| | A UHF Aeronautical Antenna. |
| |_| | A Low Band Aeronautical Antenna. |
| |_| | A Panel Mounted GPS Unit in lieu of a Handheld GPS Unit. |
| |_| | A GPS with Moving Map. |
| |_| | A GPS Data Connector. |
| |_| | A panel mounted VOR receiver system. |
| |_| | Provisions for IFR operation meeting 14 CFR Parts 135.163 & 135.165. |
| |_| | The floor space between the Pilot and Co-Pilot/observer seats shall be free of all obstructions for supplemental radio kit installation. |
| |_| | A Transponder, Altitude Encoder and Static Systems (Reconnaissance). |
| |_| | A DME system. |
| |X| | A Traffic Advisory System (TAS)(For Type I Air Tactical Platforms) |
| |_| | An Audio Control System. |
| |_| | A separate Audio Control System for the ATGS instructor. |
| |_| | An Intercommunication System for the PIC and SIC/observer. |
| |_| | An Intercommunication System for the PIC, SIC/observer and all passengers. |
(e) Specifications. These are the definitions of acceptable equipment for those configurations defined above.
All required avionics systems shall be furnished, installed, and maintained by the Contractor in accordance with the manufacturer’s specifications and the installation and maintenance standards of this section.
| (1) | ACCESSORY POWER SOURCE. A power connector (MS3112E12-3S) protected by a 10 amp circuit breaker directly connected to the avionics or aircraft power buss. The connector shall be permanently mounted in a location convenient to the SIC/observer. Pin A shall be +24 VDC in 24 volt aircraft, Pin B shall be aircraft ground, and Pin C shall be +12 VDC in 12 VDC aircraft. NEVER apply power to both Pins A and C simultaneously. See FS/AMD-A16 available at: www.nifc.gov/NIICD/documents.html |
| (2) | COMMUNICATION SYSTEMS |
| (i) | Emergency Locator Transmitter (ELT). An automatic-portable/automatic-fixed or automatic-fixed ELT utilizing an external antenna and meeting the same requirements as those detailed for airplanes in 14 CFR 91.207 (excluding section f.), shall be installed per the manufacturer’s installation manual, in a conspicuous or marked location. ELTs certified under TSO-91 are not acceptable. |
Note: After January 31, 2009, only ELTs transmitting on 406 MHz (TSO-C126 type) will be detected by satellites. The FAA recommends that any new ELT be a TSO-C126 type with a GPS/FMS interface and be registered with the National Oceanic and Atmospheric Administration (NOAA).
| (ii) | Aeronautical VHF-AM Radio Transceiver (VHF). A panel mounted aeronautical VHF-AM radio transceiver operating in the frequency band of 118.000 to 136.975 MHz, with a minimum of 760 channels in no greater than 25 kHz increments, and a minimum of 5 watts carrier output power. For aircraft operating to or from airfields or airstrips designated as Category 4, Resource Reconnaissance, and Fire Reconnaissance aircraft where a second VHF-AM radio is required (VHF-2), the second radio may be a 720 channel transceiver. All Air Tactical aircraft shall utilize only 760 channel transceivers. All Air Tactical aircraft shall utilize only 760 channel transceivers. |
| (iii) | Aeronautical P25 Digital VHF-FM Radio Transceiver (FM). For a list of currently acceptable VHF-FM radios, visit: www.nifc.gov/NIICD/documents.html |
| (A) | The transceiver shall operate from 150 to 174 MHz, permit the operator to program any usable frequency within that band while in flight, provide operator selection of wide-band (25 kHz bandwidth/5 kHz modulation), narrow-band (12.5 kHz bandwidth/2.5 kHz modulation) and P25 digital operation by channel for MAIN and AIR GUARD operation. Transceivers shall be set to operate in the narrowband mode (typically indicated with a lower case “n”) unless local requirements dictate otherwise. |
| (B) | Carrier output power shall be 6 to 10 watts nominal. The transceiver shall be capable of displaying receiver and transmitter operating frequency. Transceivers shall provide both receiver and transmitter activation indicators for MAIN and AIR GUARD. Simultaneous monitoring of both MAIN and AIR GUARD (168.6250 MHz) is required. Scanning of AIR GUARD is not acceptable. AIR GUARD communications may only be used for: Emergencies; initial call; recall; and redirection. |
| (C) | A CTCSS sub-audible tone encoder with a minimum of 32 standards selectable tones, meeting the current TIA/EIA-603 standard, shall interface with the above transceiver. The encoder shall encode a 110.9 Hz tone on all AIR GUARD transmissions. |
| (D) | The transceiver’s operational controls shall be mounted in a location that is convenient to both PIC and SIC/observer. |
| (E) | Aircraft having two or more Aeronautical P25 Digital VHF-FM Radio Transceivers (FM-1 & FM-2) need only have an AIR GUARD receiver in one transceiver. This paragraph is not applicable to Air Tactical aircraft. |
| (F) | The following Aeronautical P25 Digital VHF-FM Radio Transceivers are known to be acceptable. |
| Technisonic Industries | TDFM-136 |
| TDFM-136A | |
| Northern Airborne Technology | NPX136D-070 |
| (G) | All VHF-FM transceivers (aeronautical, mobile, and portable) furnished to meet the requirements of this agreement shall be P25 digital. Only P25 digital compliant transceivers will be acceptable. Aeronautical P25 Digital VHF-FM Radio Transceivers shall meet FS/AMD A-19. The requirements can be found at: www.nifc.gov/NIICD/documents.html. |
(H) All P25 digital radios will operate with current software as listed on www.nifc.gov/NIICD/hotsheet/hotsheet.html. Software versions identified on this website by October 1st will be acceptable for the following year. The only exception is more up-to-date software versions as released by the manufacturer. P25 digital radios without a software version listing will be upgraded to the current version within six months of release by the manufacturer.
As an example, Technisonic releases a new software version for their TDFM-136 radio on August 1st. The above website lists this new software version on September 15th. Therefore, all TDFM-136 radios must operate with this new software by January 1st. However, if the website did not list this new software until October 10th, the software would not be required until the end of the following year.
| (iv) | Provisions for Auxiliary VHF-FM Portable Radio (AUX-FM): |
| (A) | The Contractor shall provide the necessary interface for installing and properly operating an auxiliary VHF-FM portable radio through the aircraft's audio control system(s) (AUX). The interface shall consist of the appropriate wiring from the audio control system, terminate in an MS3112E12-10S type connector and utilizing the contact assignments as specified by drawing FS/AMD-17 ; AUX-FM RADIO INTERFACE, at the following website: www.nifc.gov/NIICD/documents.html |
| (B) | A weatherproof, external, broadband antenna (Comant type CI-177-1 or equal) covering the 150-174 MHz band, with associated RG-58A/U (or equivalent) coaxial cable and connector, terminated in a bulkhead-mounted, female BNC connector adjacent to the above 10-pin connector. |
| (C) | Mounting facilities, in accordance with the specifications of FAA Advisory Circular AC 43.13-2A, for secure installation of the auxiliary VHF-FM portable radio in the cockpit shall be provided (Field Support Services (www.helifire.com) AUX-EPH-RB or equivalent). |
The location of the mounting facilities shall be such that, when connected with an 18-inch adapter cable, allows the SIC/observer full and unrestricted movement of the radio's controls.
| (D) | Positive-polarity microphone excitation voltage shall be provided to the AUX-FM system from the aircraft DC power system through a suitable resistor network. A blocking capacitor shall be provided to prevent the portable radio microphone excitation voltage from entering the system. Sidetone for the AUX-FM shall also be provided (NAT AA34, Premier PA-34, or equivalent). |
| (E) | In lieu of the above AUX-FM requirements, the Contractor may substitute an Aeronautical P25 Digital VHF-FM Radio Transceiver (FM-2). On Type I air attack platforms the AUX FM may be substituted by an additional P25 FM radio. |
| (F) | If the AUX-FM specifications are intended for 700-800 MHz, UHF, or Low Band use, the appropriate antenna shall be used (see specifications below) and the audio control(s) shall be labeled accordingly (800/UHF/LB). |
| (v) | VHF-FM Programming Port |
| (A) | Each required Aeronautical P25 Digital VHF-FM Radio Transceiver shall be equipped with a conveniently located programming port to facilitate programming via a Government owned laptop computer. The port(s) shall be protected from accidental damage via contact, be hard-wired to the transceiver(s), not require the reconnection of any cables for utilization, and must be conveniently located for ease of use (typically by the SIC/observers position). Use of a FM-1/FM-2 programming switch is permitted. |
| (B) | The contractor shall also furnish appropriate cables of adequate length, and/or any necessary adapters, to interconnect the aircraft programming port(s) to the serial and/or USB port(s) of the Government laptop computer as required. The Government is responsible for providing their own radio programming software. |
| Note: | The “DIN” type connector on the front panel of TDFM-136 and early models of TDFM-136A radios are part of an encryption feature and cannot function as a programming port. The DIN connector on TDFM-136A radios, serial number FDA1200 and higher, can be utilized for radio programming. |
| (vi) | Automated Flight Following (AFF) |
| (A) | An Automated Flight Following (AFF) system compatible with the government’s AFF tracking network (Webtracker) is required. Not all available AFF systems are compatible with Webtracker nor meet Webtracker’s requirements. The Contractor shall ensure that the AFF system offered is compatible with Webtracker. To view Webtracker’s current compatibility requirements refer to https://www.aff.gov. |
| (B) | The AFF system shall be powered by the aircraft’s electrical system, installed per the manufacturer’s installation manual, and operational in all phases of flight. AFF equipment shall utilize as a minimum: Satellite communications, an internally or externally mounted antenna, provide data to the Government’s Webtracker software, use aircraft power via a dedicated circuit breaker for power protection, and be mounted so as to not endanger any occupant from AFF equipment during periods of turbulence. Antennas should be placed where they have the best view of the overhead sky as possible. Externally mounted antennas are recommended to improve system performance. Any AFF manufacturer required pilot display(s) or control(s) shall be visible / selectable by the PIC. Remote equipment having visual indicators should be mounted in such a manner as to allow visual indicators to be easily visible. |
| (C) | AFF communications shall be fully operational in the lower 48 states. Contractors accepting dispatches to the State of Alaska, Southern Canada, or Western Canada shall have an AFF system capable of being tracked in these locations at all times. Not all manufacturers’ AFF equipment communication links will operate effectively in all geographic areas. |
| (D) | The Contractor shall maintain a subscription service through the AFF equipment provider allowing AFF position reporting for satellite tracking via Webtracker. The position-reporting interval shall be every two minutes while the aircraft is in flight. The Contractor shall register their AFF equipment with the Fire Applications Help Desk (FAHD) Help Desk providing: Complete tail number, manufacturer and serial number of the AFF transceiver; aircraft make and model; and Contractor contact information. |
If the Contractor relocates previously registered AFF equipment into another aircraft, then the Contractor shall contact the FAHD making the appropriate changes prior to aircraft use.
In all cases, the Contractor shall ensure that the correct aircraft information is indicated within Webtracker. The Contractor shall contact the FAHD of system changes, scheduled maintenance, and planned service outages.
| (E) | Registration contact information, a web accessible feedback form, and additional information is available at: https://www.aff.gov. The FAHD can be reached at 866-224-7677. |
| (F) | Prior to the aircraft’s annual agreement inspection, the Contractor shall ensure compliance with all AFF systems requirements. The Contractor shall additionally perform an operational check of the system. As a minimum, the operational check shall consist of confirming the aircraft being tested is displayed in Webtracker (indicating it is currently transmitting data to Webtracker) and that all information displayed in Webtracker is current. A username and password is required to access Webtracker. Log on to the AFF website at https://www.aff.gov to request a username and password, or contact the FAHD. |
| (G) | This clause incorporates Specification Section Supplement available at: https://www.aff.gov/contract.asp with the same force and effect as if they were presented as full text herein. |
| (vii) | VHF-FM Aeronautical Antenna. A broadband aeronautical antenna (Comant CI-177-1 or equivalent) operating from 150 to 174 MHz with coaxial cable (RG-58 A/U or better) terminated on a male BNC connector. The antenna cable in the cabin shall have the ability to connect to a unit mounted between the PIC and SIC/observer's seats plus 4 feet (minimum). Antenna VSWR shall be better than 3.0 to 1. |
| (ix) | A conventional UHF Aeronautical Transceiver (UHF) operating in the frequency range of 406 to 512 MHz, which provides selection of either narrow-band (12.5 kHz) or wide-band (25.0 kHz) channel spacing operation on each channel. The transceiver shall meet applicable specifications provided in FS/AMD A-24; AVIONICS OPERATIONAL TEST STANDARDS. For a copy of FS/AMD A-24, visit www.nifc.gov/NIICD/documents.html |
| (x) | VHF Low Band Aeronautical Transceiver (LB) operating in the frequency range of 32 to 50 MHz, with channel spacing of 20 kHz. The transceiver shall meet applicable specifications provided in FS/AMD A-24; AVIONICS OPERATIONAL TEST STANDARDS. For a copy of FS/AMD A-24, visit www.nifc.gov/NIICD/documents.html |
| (xi) | Non-Standard Aeronautical Radio Transceivers. There are too many types of radio systems available to create specifications for each type. Therefore, when a Non-Standard Aeronautical VHF-FM, UHF, or 700-800 MHz Radio Transceiver is required, the Contractor shall provide the appropriate panel mounted aeronautical radio, with appropriate externally mounted antenna, connected to the aircraft audio control system(s) for the PIC and SIC/observer. |
The Non-Standard Aeronautical Radio Transceiver shall fully communicate (excluding encryption) with the listed agency on the specified frequency band. The transceiver shall meet applicable specifications provided in FS/AMD A-24; AVIONICS OPERATIONAL TEST STANDARDS. For a copy of FS/AMD A-24, visit www.nifc.gov/NIICD/documents.html
| (xii) | 700-800 MHz Aeronautical Antenna. A broadband aeronautical antenna (Comant CI-285 or equivalent) operating from 721 to 898 MHz with coaxial cable (RG-58 A/U or better) terminated on a male BNC connector. The antenna cable in the cabin shall have the ability to connect to a unit mounted between the PIC and SIC/observer's seats plus 4 feet (minimum). Antenna VSWR shall be better than 3.0 to 1. |
| (xiii) | UHF Aeronautical Antenna. A broadband aeronautical antenna (Comant CI-275 or equivalent) operating from 406 to 512 MHz with coaxial cable (RG-58 A/U or better) terminated on a male BNC connector. |
The antenna cable in the cabin shall have the ability to connect to a unit mounted between the PIC and SIC/observer's seats plus 4 feet (minimum). Antenna VSWR shall be better than 3.0 to 1.
| (xiv) | Low Band Aeronautical Antenna. A broadband aeronautical antenna (Dayton-Granger 720061 or equivalent) operating from 32 to 50 MHz with coaxial cable (RG-58 A/U or better) terminated on a male BNC connector. The antenna cable in the cabin shall have the ability to connect to a unit mounted between the PIC and SIC/observer's seats plus 4 feet (minimum). Antenna VSWR shall be better than 3.0 to 1. |
| (3) | NAVIGATION SYSTEMS |
| (i) | Global Positioning System (GPS) |
| (A) | Panel Mounted GPS Unit. A panel-mounted TSO’d GPS shall be permanently installed in the aircraft where the PIC and SIC/observer can clearly view the display. |
The GPS shall: utilize WGS-84 datum; reference latitude and longitude coordinates in the DM (degrees/minutes/decimal minutes) mode; utilize an approved, fixed, external aircraft antenna; and be powered by the aircraft electrical system. The GPS unit shall have the ability for manual entry of waypoints in flight. The GPS shall have a data base (VFR and in route units not over one (1) year old and IFR approach units not over 28 days old) covering the continental United States and Alaska. Handheld and/or marine type equipment is not acceptable.
Aviation portable GPS units (Garmin GPSMAP 296/396/496 or equivalent) are acceptable provided they use remote antennas, are securely mounted, powered by the aircraft electrical system, present information from an overhead orientation (not a drive along the road type), installation approved via FAA Form 337, and meet all previously stated GPS requirements for TSO’d GPS units.
| (B) | GPS with Moving Map. In addition to the above Panel Mounted GPS Unit requirements, the moving map’s display shall be at least three inches wide, 1.5 inches high, and show the aircraft’s present position relative to user selected waypoints and geographical features (i.e. coastlines, cities, railroads, roads, lakes, rivers, etc.). If the moving map display is a separate unit from the GPS receiver, it shall utilize GPS data from the GPS or (if utilizing an internal GPS receiver) shall adhere to the GPS data requirements for the above listed GPS unit. |
| (D) | GPS Data Connector. A GPS data connector shall be installed for the purpose of external data retrieval by a GIS laptop computer. The connector shall be a DB-9F type D sub-connector and shall be wired for RS-232C serial format for laptop computers (pin 2-transmit data, pin 3-receive data if applicable, and pin 5-ground) and shall be mounted in a location convenient to the observer. |
| (ii) | Transponder and Altitude Encoder. An ATC transponder and altitude reporting system meeting the requirements of 14 CFR 91.215(a) and (b) and tested and inspected per 14 CFR 91.413. |
| (iii) | Static Systems. Although the aircraft to be provided may not be certified for IFR flight, the aircraft's static pressure system, altimeter instrument system, and automatic pressure altitude reporting system shall be maintained in accordance with the IFR requirements of 14 CFR 91.411 and inspected and tested every 24 calendar months as specified by 14 CFR Part 43, appendices E and F. |
| (iv) | Traffic Advisory System (TAS). An active TAS shall be installed in the aircraft. The system shall be a TSO certified system using active surveillance interrogation and meet the following minimum requirements: |
| (A) | The system shall have antennas providing a 360-degree view while minimizing airframe shadowing. The system must be capable of receiving targets both above and below the aircraft. |
| (B) | The system shall allow operator range selection of 2 NM or less. The maximum range shall be at least 10 NM. |
| (C) | The system shall utilize a panel mounted multifunction display (MFD) or the systems own display unit situated for convenient scan reference by the PIC and SIC. Ryan and Avidyne units shall utilize a MFD. |
| (D) | The system shall be connected to the aircraft's audio control system(s) providing traffic alert audio to (minimally) the PICs audio control system. |
| (4) | AUDIO CONTROL SYSTEM(S) |
| (i) | General |
The audio control system shall provide the specified operator(s) with controls for selection of receiver audio outputs and transmitter microphone/PTT audio inputs for each required system (e.g. VHF-1, VHF-2, FM-1, FM-2, AUX, etc.).
(ii) Transmitter Selection and Operation Transmitter selection controls shall be provided to the specified operator(s) for microphone/PTT inputs. Whenever a transmitter is selected, the companion receiver audio shall automatically be selected for the corresponding earphone. Transmitter sidetone audio shall be provided for the operator as well as for cross-monitoring via the corresponding receiver selection switch on other audio control systems (if required).
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