1243N918Q0003__Region_8_LFW_CWN.pdf
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OFFEROR’S COPY
(Ref. 48 CFR 1) Issuing Office:
U.S. Forest Service, Contracting Southern Regional Office 1720 Peachtree Street NW, Ste. 876S Atlanta, GA 30309-2405
This solicitation can be downloaded from the following Internet site: https://www.fbo.gov
Solicitation No:
1243N918Q0003
Offers Are Solicited For:
Region 8 Call When Needed Light Fixed Wing Aircraft
Solicitation No:
1243N918Q0003
Issued Date:
07/16/2018
IMPORTANT – NOTICE TO OFFEROR
- Offers are due on 08/20/2018 @ 5:00 PM Eastern Standard Time.
- The offeror shall submit the following items in response to this solicitation:
1. SF-1449, block 17a and blocks 30a-30c: Complete, date, and sign.
2. Fill in the appropriate pricing information requested under Section B.1, B.2, B.3, and B.7.
3. Provide one (1) copy of your Business Proposal and two (2) copies of your Technical Proposal in response to Section
4. Provide your responses to Sections E.1, E.2, E.4, and E.5 of the solicitation.
5. Signed acknowledgement of any material amendments issued to the solicitation.
THE SOLICITATION PACKAGE SHALL BE RETURNED TO THE FOLLOWING ADDRESS:
U.S. Forest Service, Contracting Southern Region (R8) RE: Solicitation No. AG-43N9-S-17-0002 ATTN: Shundrica Daniels 1720 Peachtree Street N.W. Ste 876S Atlanta, GA 30309
Electronic offers may be submitted to shundricadaniels@fs.fed.us. No facsimile (FAX) will be accepted.
Offerors may contact Shundrica Daniels for information about this solicitation at 404-347-2348.
“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) https://www.fbo.gov/ mailto:shundricadaniels@fs.fed.us i
SECTION A - SOLICITATION/CONTRACT/ORDER FOR COMMERCIAL ITEMS
STANDARD FORM 1449
SECTION B - SUPPLIES OR SERVICES AND PRICE
B-1 SCHEDULE OF ITEMS
B-2 GOVERNMENT FURNISHED PILOT
B-3 PRINCIPAL BASE OPERATION
B-4 TAXES
B-5 STANDBY HOURS PER DAY
B-7 MAINTENANCE CAPABILITY
B-8 PERFORMANCE PERIOD
B-9 CONTRACTOR PERFORMANCE ASSESSMENT REPORTING SYSTEM (CPARS)
B-10 CONTRACTOR FURNISHED SPECIAL REQUIREMENTS
SECTION C – DESCRIPTION/SPECIFICATIONS/WORK STATEMENT
C-1 SCOPE OF AGREEMENT
C-2 GENERAL CERTIFICATIONS
C-3 GOVERNMENT FURNISHED PROPERTY
C-4 AIRCRAFT REQUIREMENTS
C-5 AIRCRAFT MAINTENANCE
C-6 AIRCRAFT AND EQUIPMENT SECURITY
C-7 AVIONICS
C-8 RESERVED
C-9 RESERVED
C-10 OPERATIONS
C-11 PERSONNEL
C-12 CONDUCT AND REPLACEMENT OF PERSONNEL
C-13 SUSPENSION AND REVOCATION OF PERSONNEL
C-14 SUBSTITUTION OR REPLACEMENT OF PERSONNEL, AIRCRAFT, AND EQUIPMENT
C-15 RELIEF PILOT
C-16 FLIGHT HOUR AND DUTY LIMITATIONS
C-17 ACCIDENT PREVENTION AND SAFETY
C-18 MISHAPS
C-19 PERSONAL PROTECTIVE EQUIPMENT (PPE)
C-20 INSPECTION AND ACCEPTANCE
C-21 PRE-USE INSPECTION EXPENSES
C-22 RE-INSPECTION EXPENSES
C-23 INSPECTIONS DURING USE
C-24 RESERVED
C-25 AUTHORIZED ORDERING ACTIVITIES
C-26 ORDERING PROCEDURES
C-27 POINT OF HIRE
C-28 ASSIGNED WORK LOCATION(S)
C-29 DAILY AVAILABILITY REQUIREMENTS
C-30 PAYMENT FOR AVAILABILITY
C-31 UNAVAILABILITY
C-32 PAYMENT FOR FLIGHT
C-33 PAYMENT FOR EXTENDED STANDBY
C-34 REIMBURSEMENT FOR MOBILIZATION AND DEMOBILIZATION COSTS
C-35 CONTRACTOR STAND-DOWN OR DEACTIVATION
ii
C-36 ADDITIONAL AIRCRAFT AFTER ESTABLISHMENT OF THE AGREEMENT
C-37 RESERVED
C-38 MISCELLANEOUS COSTS TO THE CONTRACTOR
C-39 PAYMENT FOR OVERNIGHT ALLOWANCE
C-40 PAYMENT PROCEDURES
C-41 PERFORMANCE BY GOVERNMENT-FURNISHED PILOT
C-42 DEFINITIONS
C-43 ABBREVIATIONS
ATTACHMENTS
ATTACHMENT 1- WAGE DETERMINATION
ATTACHMENT 2- PUBLIC AIRCRAFT OPERATIONS DECLARATION
ATTACHMENT 3 - CPARS EVALUATION FORM
SECTION D – CONTRACT CLAUSES
D-1 CONTRACT CLAUSES INCORPORATED BY REFERENCE (FAR 52.252-2) (FEB 1998)
D-2 ADDENDUM TO 52.212-4 CONTRACT TERMS AND CONDITIONS - COMMERCIAL
ITEMS
D-3 CONTRACT TERMS AND CONDITIONS REQUIRED TO IMPLEMENT STATUES OR
EXCUTIVE ORDERS - COMMERCIAL ITEMS (FAR 52.212-5) (AUG 2012) …………………61
D-4 Economic Price Adjustment Contract Flight Rates
D-5 UPDATES OF PUBLICLY AVAILABLE INFORMATION REGARDING RESPONSIBILITY
MATTERS (FAR 52.209-9) (FEB 2012)
D-6 OPTION TO EXTEND SERVICES (FAR 52.217-8) (NOV 1999)
D-7 OPTION TO EXTEND THE TERM OF THE CONTRACT (FAR 52.217-9) (MAR 2000)
D-8 STATEMENT OF EQUIVALENT RATES FOR FEDERAL HIRES (FAR 52.222-42) (MAY
1989)
D-9 AVAILABILITY OF FUNDS (FAR 52.232-18) (APR 1984)
D-10 PROPERTY AND PERSONAL DAMAGE
D-11 ASSURANCE REGARDING FELONY CONVICTION OR TAX DELINQUENT STATUS FOR
CORPORATE APPLICANTS (AGAR 452.209 -71) (ALTERNATE 1) (FEB 2012)
SECTION E
E-1 INSTRUCTIONS TO OFFERORS - COMMERCIAL ITEMS (FAR 52.212-1) (JAN 2017)
(TAILORED)……………………………………………………………………………………………………….74
E-2 EVALUATION-COMMERCIAL ITEMS (FAR 52.212-2) (OCT 2014) (TAILORED)…………………….…77
E-3 AWARD PROCESS ……………………………………………………………………………………………...79
E-4 Offeror Representations and Certifications—Commercial Items (52.212-3) (NOV 2017) ……….….79
E-5 CERTIFICATION REGARDING RESPONSIBILITY MATTERS (FAR 52.209-5) (OCT 2015) ………
E-6 INFORMATION REGARDING RESPONSIBILITY MATTERS (FAR 52.209-7) (JULY 2013)………….102
EXHIBITS
EXHIBIT 1 - ORGANIZATION EXPERIENCE…………………………………………..……………………….…….104
EXHIBIT 2 - PAST PERFORMANCE INFORMATION ……………………………………………………………
EXHIBIT 3 - SAFETY MANAGEMENT SYSTEM (SMS) COMPONENTS QUESTIONAIRE AND
ACCIDENT HISTORY ……………………………………………………………………………….…
SEE ADDENDUMIS CHECKED
CODE 18a. PAYMENT WILL BE MADE BY
CODE
FACILITYCODE
17b. CHECK IF REMITTANCE IS DIFFERENT AND PUT SUCH ADDRESS IN OFFER
OFFEROR
43N9CODE 16. ADMINISTERED BY
USDA FOREST SERVICE - CONTRACTING
1720 PEACHTREE ROAD
SUITE 876S
ATLANTA GA 30309-9102
CODE
X
X
X
481212
SIZE STANDARD:
100.00 % FOR:SET ASIDE:UNRESTRICTED OR43N9
RFPIFB
10. THIS ACQUISITION ISCODE
RFQ
14. METHOD OF SOLICITATION
13b. RATING
NAICS:
SMALL BUSINESS
08/20/2018 1700 ET
07/16/2018
404-347-2348 (No collect calls)
INFORMATION CALL:
FOR SOLICITATION 8. OFFER DUE DATE/LOCAL TIMEb. TELEPHONE NUMBERa. NAME
SHUNDRICA DANIELS
4. ORDER NUMBER3. AWARD/ 6. SOLICITATION 5. SOLICITATION NUMBER
1243N918Q0003
SOLICITATION/CONTRACT/ORDER FOR COMMERCIAL ITEMS 1. REQUISITION NUMBER
OFFEROR TO COMPLETE BLOCKS 12, 17, 23, 24, & 30
TELEPHONE NO.
17a. CONTRACTOR/
15. DELIVER TO
7.
2. CONTRACT NO.
EFFECTIVE DATE
1,500
18b. SUBMIT INVOICES TO ADDRESS SHOWN IN BLOCK 18a UNLESS BLOCK BELOW
ISSUE DATE
DELIVERY FOR FOB DESTINA-
TION UNLESS BLOCK IS
MARKED
11.
SEE SCHEDULE
12. DISCOUNT TERMS
THIS CONTRACT IS A
RATED ORDER UNDER
DPAS (15 CFR 700)
13a.
SERVICE-DISABLED
VETERAN-OWNED
SMALL BUSINESS
HUBZONE SMALL
BUSINESS
8(A)
9. ISSUED BY
USDA FOREST SERVICE - CONTRACTING
1720 PEACHTREE ROAD
SUITE 876S
ATLANTA GA 30309-9102
WOMEN-OWNED SMALL BUSINESS
(WOSB) ELIGIBLE UNDER THE WOMEN-OWNED
SMALL BUSINESS PROGRAM
EDWOSB
24.
AMOUNT
23.
UNIT PRICE
22.
UNIT
21.
QUANTITY
20.
SCHEDULE OF SUPPLIES/SERVICES
19.
ITEM NO.
SEE SECTION B (ATTACHED)
REGION 8 - CALL WHEN NEEDED LIGHT FIXED WING
AIRCRAFT
(Use Reverse and/or Attach Additional Sheets as Necessary)
HEREIN, IS ACCEPTED AS TO ITEMS:
X
XX
DATED
SHUNDRICA T. DANIELS
. YOUR OFFER ON SOLICITATION (BLOCK 5),
INCLUDING ANY ADDITIONS OR CHANGES WHICH ARE SET FORTH
ARE
ARE
31c. DATE SIGNED
27b. CONTRACT/PURCHASE ORDER INCORPORATES BY REFERENCE FAR 52.212-4. FAR 52.212-5 IS ATTACHED. ADDENDA
31a. UNITED STATES OF AMERICA (SIGNATURE OF CONTRACTING OFFICER)
30c. DATE SIGNED 31b. NAME OF CONTRACTING OFFICER (Type or print)
27a. SOLICITATION INCORPORATES BY REFERENCE FAR 52.212-1, 52.212-4. FAR 52.212-3 AND 52.212-5 ARE ATTACHED. ADDENDA
26. TOTAL AWARD AMOUNT (For Govt. Use Only)
OFFER
STANDARD FORM 1449 (REV. 2/2012)
Prescribed by GSA - FAR (48 CFR) 53.212
ARE NOT ATTACHED.
ARE NOT ATTACHED.
AUTHORIZED FOR LOCAL REPRODUCTION
PREVIOUS EDITION IS NOT USABLE
30b. NAME AND TITLE OF SIGNER (Type or print)
30a. SIGNATURE OF OFFEROR/CONTRACTOR
28. CONTRACTOR IS REQUIRED TO SIGN THIS DOCUMENT AND RETURN 2
COPIES 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.
25. ACCOUNTING AND APPROPRIATION DATA
29. AWARD OF CONTRACT:
REF.
ALBUQUERQUE SERVICE CENTER
INCIDENT BUSINESS - CONTRACTS
101B SUN AVENUE NE
ALBUQUERQUE, NM 87109
Solicitation No.1243N918Q0003 U.S. Forest Service Region 8 Call When Needed Light Fixed Wing Services Southern Regional Office
SECTION B
SUPPLIES OR SERVICES AND PRICE
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 the 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 2019 through FY 2023).
Note: Region 8 will not award 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.
AIRCRAFT HOURLY RATES
Item No.
Tail No.
Make Model Year
Mission Codes/1
Flt Rate Base Year
Flt Rate
Flt Rate
Flt Rate
Flt Rate
Daily Availability
Rate Base Year
Daily Availability
Rate
Daily Availability
Rate
Daily Availability
Rate
Daily Availability
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 Pressure altitude, at ISA, as stated in Aircraft Flight Manual.
(2) Use Key Below Note: List additional aircraft on a separate sheet using the 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. Training Platform
W. 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: ______ ______ _______ _______ _______ 2019 2019 2020 2021 2023
B-3 PRINCIPAL BASE OPERATION
Contractor shall enter the location of the “Principle Base of Operation” in accordance with the “definitions” found in Section C for the offered aircraft. For Call-When-Needed (CWN) light fixed-wing aircraft, the location of the Contractor’s Operating Certificate is the determining factor as to where the agreement is administered. Therefore, the same aircraft number will not be awarded/administered under more than one Forest Service CWN agreement. Offers for furnishing services on a “CWN” basis for light fixed-wing aircraft are only being solicited from operators that hold 14 CFR 135 certificate in the Southern Region to include the states of Alabama, Arkansas, Florida, Georgia, Kentucky, Louisiana, Mississippi, North Carolina, Oklahoma, South Carolina, Tennessee, Texas, Virginia and Puerto Rico.
Location (Physical Address) State
B-4 TAXES
All applicable taxes (including excise taxes and segment fees) shall be included in your daily availability rate in accordance with FAR Clause 52.212-4(k). The contract price includes all applicable Federal, State, and local taxes and duties.
B-5 STANDBY HOURS PER DAY
9 hours of standby per day
B-6 EXTENDED STANDBY HOURLY RATE
(a) The extended standby rate will be reviewed on an annual basis to ensure compliance with the Service Contract Act and an adjustment will be made if needed. The extended standby rate will be computed by taking the minimum wage rate from the Department of Labor Wage Determination (current at that time), for Nationwide Pilot, times 1.5 plus 20% for benefits, overhead and profit and rounded to the nearest dollar. If needed, adjusted rates will become effective annually on February 16 of each year.
(b) Extended standby is not intended to compensate the Contractor on a one-to-one basis for all hours necessary to service and maintain the aircraft.
(c) The current rate is $51.00 per hour.
B-7 MAINTENANCE CAPABILITY
Contractor shall provide the name and address of the Director of Maintenance.
Director of Maintenance (Name) Business Address
Cell Phone No.
Phone No.
Fax No.
The Government may inspect the Contractor’s operation and maintenance facilities prior to award.
B-8 PERFORMANCE PERIOD
It is contemplated that any Basic Ordering Agreement (BOA) resulting from this solicitation will be in effect for a period of up to five fiscal years. The Base year will be effective 10/1/2018, with four (4) optional year periods. The fiscal year begins October 1 and ends on September 30 each year.
B-9 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/
B-10 CONTRACTOR FURNISHED SPECIAL REQUIREMENTS
All items checked below are required and must comply with Section C, an Exhibit and/or Federal Regulations.
Resource Recon Avionics, FM Option 4 or higher (See C-7 (a)(3)) Fire Recon Avionics, FM Option 3 or higher (See C-7 (a)(4)) Air Tactical Avionics, Type 1 or better (See C-7 (a)(5)) Additional VHF-AM Radios: Total A/C Qty: (See C-7 (b)(1)(i)) VHF-FM Radio in lieu of the Aux FM requirement: Total A/C VHF-FM Qty: (See C-7 (b)(1)(ii))
Additional VHF-FM Radios: Total A/C Qty: (See C-7 (b)(1)(ii)) VHF-FM Programming Ports (See C-7 (b)(5)(xi)) Non-Standard Radio, Type: (See C-7 (b)(1)(iv)) Satellite Communications System: Minutes/Month____ (See C-7 (b)(1)(v)) Drop Cord for SIC/observer (See C-7 (b)(2)(ii)(B)) Drop Cord for aft Instructor position (See C-7 (b)(2)(ii)(B)) Push-To-Talk (PTT) cord for SIC/observer (TELEX PT-300 with VOX or equivalent) Push-To-Talk (PTT) cord for aft Instructor (TELEX PT-300 with VOX or equivalent) Aft Audio Control System (See C-7 (b)(2)(ii)(C)) Aeronautical GPS in lieu of a portable GPS (See C-7 (b)(3)(i)(A)) GPS with Moving Map (See C-7 (b)(3)(i)(C)) GPS Data connector (See C-7 (b)(5)(xii)) External Portable Aviation GPS Antenna, GPS Model: (See C-7 (b)(5)(xiii))
Traffic Advisory System (TAS) (See C-7 (b)(4)(v)) Autopilot (See C-7 (b)(5)(i)) Radar Altimeter (See C-7 (b)(5)(ii)) Multi-Function Display (MFD) (See C-7 (b)(5)(iii))
Auxiliary Power Source (3 Pin) (See C-7 (b)(5)(v)) Dual USB charging ports, Qty: 1 Users: (See C-7 (b)(5)(xiv)) Supplemental Antennas, Qty: /Band: (See C-7 (b)(5)(vi)) Supplemental Radio Kit Provisions (See C-7 (b)(5)(vii)) Supplemental Air Attack Kit Provisions (See C-7 (b)(5)(viii)) TSO approved VOR/Localizer, Qty: .
TSO approved Glideslope, Qty: .
TSO approved DME, Qty: {Not required if GPS is IFR with current database} TSO approved Three Light Marker Beacon System, Qty: .
Satellite Weather system with XM Aviator subscription or equivalent Provisions for IFR operation meeting 14 CFR 135.163 & 135.165
SECTION C
DESCRIPTION/ SPECIFICTIONS
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) All aircraft must be current or former manufacturer built production aircraft. No experimental, amateur or manufacturer built kit aircraft shall be used.
(b) All aircraft shall be FAA certificated as Normal, Standard, or Utility category airplanes and certified for single-pilot operation.
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) All aircraft shall be equipped and operated in accordance with the applicable requirements set forth in 14 CFR Part 91 and 135.
(2) Single engine, piston-powered aircraft shall meet the following performance requirements:
(a) Aircraft shall have a power loading of not more than 13.5 pounds per horsepower.
(b) At least a 200 horsepower engine; any engine under 230 horsepower must be turbo or supercharged.
(c) Minimum useful load of, 500 pounds plus 4.5 hours of fuel, when equipped for the mission.
a. Capable of a minimum 130 KTAS in cruise flight at 5000 Pressure altitude and ISA plus 20.
(3) Single engine, turbine-powered aircraft shall meet or exceed the requirements of C4(a)(2)(a) through (c) and the following performance requirements:
(a) At least a 500 shaft horsepower engine.
(4) Multiengine, piston-powered aircraft shall meet the following performance requirements:
(a) At least a 200 horsepower engine per side; any engine under 240 horsepower must be turbo or supercharged.
(b) Minimum useful load of, 700 pounds plus 4.5 hours of fuel, when equipped for the mission.
a. Capable of a minimum 165 KTAS in cruise flight at 8000 Pressure altitude and ISA plus 20.
b. Be able to maintain a positive rate of climb, with one engine inoperative, at 5000 pressure altitude and ISA plus 33, when equipped for the mission with a 200-pound pilot, 220-pound observer, and 4.5 hours of fuel onboard.
(c) Minimum Controllable Airspeed (Vmca) of 100 KIAS or less.
(5) Multiengine, turbine-powered aircraft shall meet or exceed the requirements of C4(a)(4)(a) through (c) and the following additional performance requirements:
(a) At least a 500 shaft horsepower engine per side.
(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 (PMS 513) and the Emergency Response Guide (ERG).
(iii) Aeronautical charts covering the area of operation
Note: The use of electronic flight bags (EFB) is authorized providing the following conditions are met:
- EFB’s used are approved and procedures listed in the operators 135 opspecs.
- All other contract items are readily available to the vendor and agency crew (tablet-style devices only, no laptops). A minimum screen size for the EFB shall be 7” inches.
- Vendors must keep the device adequately charged to allow normal use and have a means of charging the device readily available without reliance on the government.
(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 single metal 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 the 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 inches (sling)
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 at a minimum 1,000 calories per day, 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.
(12) Aircraft designated as a training platform as noted in section B must have the required additional avionics as noted in C-7, in addition to the following aircraft equipment:
(a) Aircraft offered must be a turbine engine equipped aircraft.
(b) A fixed and flat (worktop/desk) horizontal with the floor or the aircraft with enough room for a laptop. Workstation shall be located behind the co-pilots seat. Any bulkheads between the flight deck and passenger compartment shall be removed to facilitate a better view (looking forward) for the ATGS trainer.
(c) A 3rd FM P25 compliant radio mounted on the fixed training station.
(d) RAM Mounts on top of the workstation to facilitate the inflight mounting of an iPad and portable GPS.
(e) A dual USB charging port certified to FAA TSO C71 and capable of providing at least 2 amps of power to each port simultaneously with an output voltage 5VDC.
USB port must be installed according to 14CFR Part 43 on the designated workstation described below.
(f) Headset Jack at the workstation
(g) A push to talk (PTT) button on the workstation
(h) One 3.5 mm audio plug on workstation.
C-5 AIRCRAFT MAINTENANCE
(a) Offered aircraft shall be maintained in accordance with the OEM’s (original equipment manufacturer) most recent revision of inspection program applicable to the serial number of the aircraft being inspected or an inspection program approved by the FAA under the contractor’s 14 CFR 135 operations specification. All maintenance shall be accomplished in accordance with the standards established by 14 CFR Part 43, 91, and 135 standards and this contract.
(b) The Contractor shall identify the maintenance facilities and/or maintenance personnel used to fulfill the requirements of this agreement, including those covered under 14 CFR 135.426.
(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) Offered aircraft shall be in compliance with all applicable Federal Aviation Administration (FAA) Airworthiness Directives (AD’s) as per 14 CFR 91.417 (a)(2)(v), and Service Bulletins (SB’s) with a time compliance requirement, referenced in an FAA Special Airworthiness Information Bulletin (SAIB) or are designated mandatory by the manufacturer.
Each aircraft’s maintenance schedule shall include mandatory component retirement, Replacement, or overhaul time as specified in the OEM Airworthiness Limitations Section or equivalent OEM document and shall be in compliance with them.
Each aircraft shall be in compliance with all OEM (recommended or mandatory) programs, documents and resultant inspections from programs such as Continued Airworthiness Programs (CAP), Structural Inspection Documents (SID), Supplemental Structural Inspection Documents (SSID) Corrosion Prevention and Control Programs (CPCP) and Electrical Wiring
Interconnection Systems (EWIS) programs.
(e) All maintenance shall be accomplished in accordance with the standards established by 14 CFR Part 43, 91, and 135; Advisory Circular (AC) 43.13; 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. Additionally, aircraft maintenance record entries and aircraft flight logs shall be transmitted to the operator’s home base (the location the certificate is held) every 12 flight hours or 7 days- whichever occurs first.
(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), powertrain, 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 Aviation 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 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. Data shall include an accurate and updated equipment list.
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.
(k) Reserved
(l) Mechanics assigned to work on aircraft shall have appropriate FAA certification, and ratings or if at a 145 Repair Station shall at all times be working in the presence of one so certified and rated.
Additionally,
(a) Pilots without FAA airframe and power plant (A&P) certifications are authorized to perform only the preventative maintenance tasks detailed under 14 CFR 43 Appendix A, Section (c), provided they have been properly trained under the direct supervision of an appropriately rated mechanic and designated in writing by the contractor as proficient in each task to be performed. Pilots will have this documentation available for review by government representatives. Pilots performing preventative maintenance shall have current maintenance manuals available and make logbook entries that document their work was performed in accordance with 14 CFR 43.9.
(b) When the aircraft is not available due to required unscheduled maintenance, a pilot may function as a mechanic only if they possess a valid FAA mechanic certificate with the appropriate airframe and/or power plant ratings or if they are performing preventative maintenance in accordance with 14 CFR 43.3.
(c) Only a certificated mechanic (holding an airframe and power-plant rating) may perform scheduled maintenance and inspections. The primary or relief pilot on duty as a pilot must not perform scheduled maintenance and inspections.
a. All mechanics shall maintain the aircraft in accordance with requirements specified within this contract and shall meet the requirements of 14 CFR Part 43.7(b).
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 interference with the safety of flight.
(c) Examples of Unacceptable disabling systems are:
(1) Locked door/windows; and/or
(2) Fenced parking areas.
C-7 AVIONICS
(a) MINIMUM REQUIREMENTS
All avionics used to meet this agreement shall comply with the requirements of paragraph (b) AVIONICS SPECIFICATIONS and paragraph (c) AVIONICS INSTALLATION AND MAINTENANCE STANDARDS. The following are the minimum avionics which shall be installed.
Additional avionics may be required in section B of this agreement.
(1) Point to Point Aircraft
Point to Point flights shall meet the requirements of 14 CFR 135. No additional avionics are required.
(2) Back Country Aircraft
Aircraft operating to or from airfields or airstrips designated as Category 4 and not otherwise conducting special use missions shall meet the requirements of paragraph (a)(3) excluding (a)(3)(ii).
(3) Resource Reconnaissance Aircraft (All aircraft which are not used for fire operations or covered by paragraphs (a)(1) or (a)(2))
(i) One VHF-AM Radio (COM)
(ii) One Global Positioning System (GPS)
(iii) An Emergency Locator Transmitter (ELT)
(iv) An Automated Flight Following system (AFF) {Not required for aircraft only used for Law Enforcement}
(v) Equipment and lighting for night VFR operations in accordance with 14 CFR 135.159 and 14 CFR 135.161.
(vi) One of the following options for FM communications
(A) Option 1
(1) One Supplemental VHF-FM Antenna
(B) Option 2
(1) An Intercom System (ICS)
(2) An Audio Control system
(3) One Auxiliary FM system (AUX FM)
(C) Option 3
(1) Provisions for a Supplementary Radio Kit
(D) Option 4
(1) An Intercom System (ICS)
(2) An Audio Control system
(3) One VHF-FM Radio (FM)
(4) Fire Reconnaissance Aircraft
(i) Two VHF-AM Radios (COM 1 and COM 2)
(ii) One Global Positioning System (GPS)
(iii) An Emergency Locator Transmitter (ELT)
(iv) An Automated Flight Following system (AFF)
(v) Equipment and lighting for night VFR operations in accordance with 14 CFR 135.159 and 14 CFR 135.161.
(vi) One of the following options for FM communications
(A) Option 1
(1) Two Supplemental VHF-FM Antennas
(B) Option 2
(1) Provisions for a Supplementary Radio Kit
(C) Option 3
(1) An Intercom System (ICS)
(2) An Audio Control system
(3) One VHF-FM Radio (FM)
(5) Air Tactical Aircraft
(i) Type 1
(A) Two VHF-AM Radios (COM 1 & COM 2)
(B) Two VHF-FM Radios (FM 1 & FM 2)
(C) One Auxiliary FM system (AUX FM)
(D) An Intercom System (ICS)
(E) Separate Audio Control systems for the PIC and SIC/observer
(F) Audio jacks with ICS and radio transmit capability in the rear seat connected to the SIC/observer Audio Control system. An Aft Audio Control system for this position is acceptable.
(G) One Global Positioning System (GPS)
(H) An Emergency Locator Transmitter (ELT)
(I) An Automated Flight Following system (AFF)
(J) One Transponder
(K) One Altimeter and Automatic Pressure Altitude Reporting system
(L) Equipment and lighting for night VFR operations in accordance with 14 CFR
135.159 and 14 CFR 135.161.
(ii) Type 2
(A) Two VHF-AM Radios (COM 1 & COM 2)
(B) One VHF-FM Radio (FM)
(C) One Auxiliary FM system (AUX FM)
(D) An Intercom System (ICS)
(E) Separate Audio Control systems for the PIC and SIC/observer
(F) Audio jacks with ICS and radio transmit capability in the rear seat connected to the SIC/observer Audio Control system. An Aft Audio Control system for this position is acceptable.
(G) One Global Positioning System (GPS)
(H) An Emergency Locator Transmitter (ELT)
(I) An Automated Flight Following system (AFF)
(J) One Transponder
(K) One Altimeter and Automatic Pressure Altitude Reporting system
(L) Equipment and lighting for night VFR operations in accordance with 14 CFR
135.159 and 14 CFR 135.161.
(iii) Type 3
(A) Two VHF-AM Radios (COM 1 & COM 2)
(B) One VHF-FM Radio (FM)
(C) An Intercom System (ICS)
(D) An Audio Control system
(E) One Global Positioning System (GPS)
(F) An Emergency Locator Transmitter (ELT)
(G) An Automated Flight Following system (AFF)
(H) One Transponder
(I) One Altimeter and Automatic Pressure Altitude Reporting system
(J) Equipment and lighting for night VFR operations in accordance with 14 CFR
135.159 and 14 CFR 135.161.
(iv) Type 4
(A) Two VHF-AM Radios (COM 1 & COM 2)
(B) An Audio Control system
(C) One Global Positioning System (GPS)
(D) An Emergency Locator Transmitter (ELT)
(E) An Automated Flight Following system (AFF)
(F) One Transponder
(G) One Altimeter and Automatic Pressure Altitude Reporting system
(H) Provisions for a Supplemental Air Attack Kit
(I) Equipment and lighting for night VFR operations in accordance with 14 CFR
135.159 and 14 CFR 135.161.
Note 1: Air Tactical aircraft equipped with an approved TAS shall be identified “w/TAS” on the aircraft approval card.
Note 2: If a Supplemental Radio Kit is provided with the aircraft, “with radio kit” shall be identified on the aircraft approval card.
Note 3: Supplemental Air Attack Kit installations shall not elevate the aircraft’s capability beyond the type for which it would otherwise be approved.
Note 4: Automatic Dependent Surveillance-Broadcast Out (ADS-B OUT) will be required for
Air Tactical Aircraft beginning January 1st 2020.
(b) AVIONICS SPECIFICATIONS
All avionics used to meet this agreement shall comply with the following requirements and paragraph (c) AVIONICS INSTALLATION AND MAINTENANCE STANDARDS.
(1) Communications systems
Transmitters shall not open squelch on, or interfere with, other AM or FM transceivers on the aircraft which are monitoring different frequencies. Transmit interlock functions shall not be used with communication transceivers.
(i) VHF-AM Radios
VHF-AM radios shall be TSO approved aeronautical transceivers, permanently installed, and operate in the frequency band of 118.000 to 136.975 MHz with a minimum of 760 channels in no greater than 25 KHz increments. Transmitters shall have a minimum of 5 Watts carrier output power.
(ii) VHF-FM Radios
All aircraft approved for fire operations shall use P25 Digital VHF-FM transceivers meeting the specifications of FS/OAS A-19. FM radios used in all aircraft shall be agency approved. FS/OAS A-19 and a list of currently approved FM radios can be found on the following website: http://www.nifc.gov/NIICD/documents.html . The following requirements shall be met.
(A) VHF-FM radios shall be aeronautical transceivers, permanently installed in a location that is convenient to the PIC and SIC/observer, and operate in the frequency band of 138 to 174 MHz. All usable frequencies shall be programmable http://www.nifc.gov/NIICD/documents.html in flight. Narrowband and digital operation shall be selectable by channel for both MAIN and GUARD operation. Carrier output power shall be 6-10 Watts nominal.
(B) Transceivers shall have a GUARD capability constantly monitoring 168.625 MHz and have a tone of 110.9 on all GUARD transmissions. Simultaneous monitoring of MAIN and GUARD is required. Scanning of GUARD is not acceptable. Aircraft not approved for Air Tactical operation only requires one FM GUARD receiver.
(C) Transceivers shall have the capability of encoding CTCSS subaudible tones on all channels. A minimum of 32 tones meeting the current TIA/EIA-603A standards shall be selectable.
(D) Transceivers shall have the capability to display both receiver and transmitter frequencies. Activation indicators for transmit and receive shall be provided for both MAIN and GUARD operation.
(E) The radio shall use an external broadband antenna covering the frequency band of 138 to 174 MHz (Comant CI-177-1 or equivalent).
(iii) Auxiliary FM systems (AUX FM)
An interface to properly operate a portable FM radio through the aircraft audio control systems shall be provided using an MS3112E12-10S type bulkhead mounted connector with contact assignments as specified by FS/AMD A-17 available at the following website:
http://www.nifc.gov/NIICD/documents.html .Sidetone for the portable radio shall be provided (AEM AA34 or equivalent). The following applies to all AUX FM installations.
(A) An external broadband antenna covering the frequency band of 138 to 174 MHz (Comant CI-177-1 or equivalent) shall be installed with the associated coax terminated in a bulkhead mounted BNC connector adjacent to the above 10 pin connector.
(B) A portable radio mount (Field Support Services AUX-EPH-RB or equivalent) shall be installed providing the unrestricted crew operation of the radio controls when connected with an 18-inch adapter cable.
(C) A VHF-FM radio meeting the requirements of paragraph 2.A.2) may be installed, in addition to the radios already required, in lieu of the AUX FM system.
(iv) Non-Standard Radios
Non-standard radios shall be aeronautical transceivers interfaced to the aircraft audio control systems and a compatible antenna via an approved installation. The radio shall be compatible with the requesting unit.
(v) Satellite Communications System (SatCom)
(A) SatCom systems shall be FAA approved, powered by the aircraft electrical system via a dedicated circuit breaker, interfaced to the aircraft audio system as a communication transceiver, permit direct-dial operation, and be operational in all phases of flight.
(B) All manufacturer required displays and controls shall be easily visible and selectable by the PIC and SIC/Observer.
(C) The contractor shall maintain a subscription providing uninterrupted service during the contract period, and a minimum amount of minutes per month as identified in Section B. The Government will reimburse the contractor for actual costs incurred when using more than the required amount of minutes specified.
(2) Audio Systems
(i) Intercom systems (ICS)
ICS shall integrate with the aircraft audio control systems and mix with selected receiver audio. An ICS volume control and a “hot mic” capability shall be provided for the PIC and SIC/observer. Passenger volume adjustments shall not affect the PIC. Hot mic may be voice activated (VOX) or controlled via an activation switch. The PIC shall have an isolation capability.
(ii) Audio Control systems
(A) General
Controls for transmitter selection and independent receiver selection of all required radios shall be provided for each required audio control system. Each system shall have the capability to simultaneously select and utilize a different transceiver (and PA if required). Sidetone shall be provided for the user as well as for cross-monitoring by all installed systems. Receiver audio shall be automatically selected when the corresponding transmitter is selected. Receiver audio shall be provided to each position which requires ICS. Aft audio control systems are not required to provide NAV audio.
All required passenger positions shall utilize the SIC/observer’s audio control system unless an aft audio control system is installed. Drop cords may be used provided MS3112E10-6S type 6-pin connectors are installed adjacent to the required passenger headset jacks and wired for compatibility with an appropriate drop cord (Alpine Aerotech AAL280 series or equivalent).
Audio controls shall be labeled as COM-1, FM-1, AUX, PA, etc.… as appropriate or as COM-1, COM-2, COM-3, etc.… with the corresponding transceiver labeled to match. Audio shall be free of distortion, noise, or crosstalk. The system shall be designed for use with 600-ohm earphones and carbon equivalent, noise canceling, boom type microphones. All required positions shall have JJ-033 and JJ-034 type microphone and headphone jacks separated by no more than 4 inches. Cockpit speakers shall be sufficiently amplified for use in flight.
Crew positions shall have radio Push-To-Talk (PTT) switches on their respective flight controls. A PTT switch shall be provided to allow the SIC/observer to transmit without touching the flight controls.
(B) Drop Cord Requirements
(1) Coil cord with sufficient length to provide unrestricted movement according to mission requirements (Minimum 3 feet retracted)
(2) 6-Pin MS3476L10-6P type connector on the coil cord
(3) JJ-033 and JJ-034 type headset jacks at the housing
(4) Large clip
(5) Volume control
(6) ICS switch with momentary and lock positions
(7) Radio PTT switch (only for positions which require radio transmit)
(C) Aft Audio Control systems
The audio controller shall be installed in a location that provides the operator directly behind the SIC/observer unobstructed access to the controls while seated.
Aft passengers shall utilize the aft audio control system(s).
(D) Required Audio Control systems
The following audio control systems are required based on mission type
(1) Type I and Type II Air Tactical airplanes
(a) Two separate audio control systems (which may be combined in a single unit) for the PIC and SIC/observer
(b) The instructor position (directly behind the SIC/observer) shall have radio transmit capability. This position shall follow the SIC/observer system or have an aft audio control system.
(2) Type III and Type IV Air Tactical airplanes
A single audio control system for the PIC and SIC/observer
(3) Reconnaissance airplanes (when required)
A single audio control system for the PIC and SIC/observer
(3) Navigation systems
(i) Global Positioning Systems (GPS)
(A) Aeronautical GPS
Each required GPS shall be TSO approved, permanently installed where both the PIC and SIC/observer can clearly view the display, use an approved external aircraft antenna, and be powered by the aircraft electrical system. The GPS shall utilize the WGS-84 datum, reference coordinates in the DM (degrees/minutes/decimal minutes) format and have the ability to enter waypoints in flight manually. The GPS navigation database shall be updated annually covering the geographic areas where the aircraft will operate.
(B) Portable Aviation GPS
Portable aviation GPS units (Garmin GPSMAP, aera, or equivalent) are acceptable when an Aeronautical GPS is not specified. They shall be securely mounted via an approved installation using the aircraft electrical system and a remote antenna.
The GPS shall present information from an overhead perspective. The PIC shall have a clear view of the display and unrestricted access to the controls. The SIC/observer shall also have a clear view of the display in Air Tactical aircraft. The GPS shall meet the above datum, coordinate, and database requirements for an aeronautical GPS. Portable GPS units are not acceptable for aircraft performing IFR or NVG operations.
(C) GPS with Moving Map
The GPS providing data to the moving map shall meet all of the above GPS requirements. The moving map’s display shall be 3 inches wide, 1.5 inches high, and show the aircraft’s present position relative to user selected waypoints and geographical features. The map may be integrated with the GPS.
(4) Surveillance systems
(i) Emergency Locator Transmitters (ELT)
Emergency locator transmitters shall be automatic-fixed, installed in a conspicuous or marked location, and meet the requirements detailed in 14 CFR 91.207 (excluding section f). ELT antennas shall be mounted externally to the aircraft unless installed in a location approved by the aircraft manufacturer. TSO C91a or newer ELTs are required. TSO C126 and newer ELTs require documentation of current registration from the national authority for which the aircraft is registered.
(ii) Automated Flight Following systems (AFF)
Automated flight following systems shall be compatible with the government’s tracking program (AFF.gov), utilize satellite communications, and use aircraft power via a dedicated circuit breaker. AFF shall be functional in all phases of flight and in all geographic areas where the aircraft will operate. The following additional requirements shall be met.
(A) A subscription service shall be maintained through the equipment provider allowing position reporting via the Government AFF Program. The reporting interval must be every two minutes while aircraft power is on.
(B) AFF equipment must be registered with AFF.gov providing all requested information. Changes to equipment and registration information shall be reported to AFF.gov ensuring the program is current prior to aircraft use. For assistance, the Fire Applications Help Desk (FAHD) may be reached at (866) 224-7677 or (616) 323-1667.
(C) An AFF operational test shall be performed by the vendor no less than seven calendar days prior to the annual compliance inspection. This test must ensure that the system meets all requirements and is displayed in the AFF viewer with the correct information. A username and password are required. Registration and additional information are available at https://www.aff.gov/. If the aircraft is not displaying properly, the vendor shall notify AFF.gov.
(D) If AFF becomes unreliable, the aircraft may, at the…
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