NLFW Exhibit 6 Rev 26ReOpen 05152026.xlsx

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National Light Fixed Wing Multiple Award Task Order Contract Reopener
Solicitation number
1202SA26B9400
Issued by

About this file

This is a pricing/technical data template (Exhibit 6) for the National Light Fixed Wing Multiple Award Task Order Contract Reopener solicitation. The template requires offerors to provide detailed aircraft performance data across seven distinct missions (labeled 1 through 7, with some missions having sub-variants designated as "a" and "b"). Each mission section requires offerors to submit comprehensive aircraft specifications and performance metrics for a single aircraft model.

The template mandates submission of basic aircraft information including make, model, manufacturer, serial number, and FAA registration number, along with critical performance parameters such as maximum allowable zero fuel weight, maximum ramp weight, maximum takeoff gross weight, maximum landing weight, Vyse, and single-engine service ceiling. For each mission, offerors must calculate and document detailed fuel burn data, climb rates, cruise times, descent profiles, and loiter capabilities across multiple flight segments. Specific missions vary in altitude requirements (ranging from 3,000 MSL to 22,000 MSL), cruise distances (ranging from 50 to 150 nautical miles), and environmental conditions (standard day or ISA +20°C). Missions 5, 6, and 7 additionally require landing gear configuration specifications (wheels, floats, amphibious floats, or ski) and performance data for unprepared surfaces, including takeoff and landing distances over 50-foot obstacles at both sea level standard day and 4,500-foot pressure altitude conditions. All aircraft data must support the government's requirements for fixed-wing aircraft operations in support of public lands administration, fire, resource management, law enforcement, and administrative missions during the performance period of January 1, 2027, through December 31, 2033.

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Other files

File Type Posted
1202SA26B9400 0001 NLFW MATOC.pdf PDF
Exhibit 2 Vendor Information.pdf PDF
Exhibit 1 SOI 27-29.xlsx XLSX spreadsheet
Attachment 7 Past Performance.pdf PDF
Exhibit 5 Airplane Pilot Qualification record.pdf PDF
Exhibit 7 Avionics.pdf PDF
Exhibit 4 Weight and Balance.xlsx XLSX spreadsheet
E-11 52.212-3.pdf PDF
Exhibit 6 Instructions.docx DOCX document
1202SA26B9400 NLFW MATOC 2027 Reopen.pdf PDF
SF 1449.pdf PDF
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Offeror Company Name:
MissionBasic Aircraft InformationBasic Mission WeightsMission Takeoff & Climb1Cruise 1Decent 1LoiterClimb 2Cruise 2Decent 2, Approch, LandingFuel Remaining
1MakeModelManufacturer Serial NumberFAA Registration NumberAircraft Max Allowable Zero Fuel Weight (If Applicable to Aircraft)Aircraft Max Ramp WeightAircraft Max Takeoff Gross WeightAircraft Max Landing WeightVyse at Max Gross Takeoff gross weightSingle Engine Service Ceiling . If Applicable (FAA-H-8083-3A Glossary Definition)Total aircraft usable fuel in LBS.Aircraft Empty Weight with all installed contract required/mission required equipmentAircraft weight with all mission equipment plus Crew & Baggage Identified in B-1 (a through i) for specific missionTotal allowable fuel with all mission equipment plus Crew & Baggage identified in B-1 (a through i) in LBS. for specific missionActual Aircraft Takeoff weight (Mission Equip, Crew, Bags, Mission Fuel) From Departure MSL elevation and ISA TempStart, Runup, and Taxi fuel burn in LBS.Fuel burn in LBS. to 22,000 msl from 4500'MSL, at ISA +20 CTime to climb to 22,000 msl from 4500'MSL, at ISA +20 CDistance in nm to climb to 22,000 from 4500' MSL, at ISA +20CTotal fuel burn in LBS. to cruise 150 nm at 22,000 msl PAMission aircraft cruise configuration and calculated TASTime to cruise 150 nm at 22,000 msl Pressure AltFuel burn in decent to loiter, from 22,000 msl to 14,500 msl, Pressure AltTime to descend to loiter, from 22,000 msl to 14,500 msl, Pressure AltDistance in nm to descend to loiter, from 22,000 msl to 14,500 msl Pressure AltTotal fuel burn to loiter for three hours at 14,500 MSL, at Pressure AltAircraft loiter configurationVmca For loiter configurationVS1 at 30 deg AOB for loiter configuration1.3VS1 for loiter configurationFuel burn to climb from 14,500 MSL (working altitude) to 22,000 MSL PATime to climb from 14,500 MSL (working altitude) to 22,000 MSL PADistance in nm to climb from loiter at 14,500' msl at to 22,000 msl PATotal fuel burn in LBS. to cruise 150 nm at 22,000 MSL PA2Mission aircraft cruise config calculated TASTime to cruise 150 nm at 22,000 MSL PADecent 2 and Approach fuel burnDecent 2 and Approach timeDecent 2 and Approach distance in nmTotal Fuel remaining (in minutes) at landing under normal cruise configurationTotal fuel remaining at landing in LBS.
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2a

Offeror Company Name:
MissionBasic Aircraft InformationBasic Mission WeightsMission Takeoff & Climb1Cruise 1Decent 1LoiterClimb 2Cruise 2Decent 2, Approch, LandingFuel Remaining
2aMakeModelManufacturer Serial NumberFAA Registration NumberAircraft Max Allowable Zero Fuel Weight (If Applicable to Aircraft)Aircraft Max Ramp WeightAircraft Max Takeoff Gross WeightAircraft Max Landing WeightVyse at Max Gross Takeoff gross weightSingle Engine Service Ceiling . If Applicable (FAA-H-8083-3A Glossary Definition)Total aircraft usable fuel in LBS.Aircraft Empty Weight with all installed contract required/mission required equipmentAircraft weight with all mission equipment plus Crew & Baggage Identified in B-1 (a through i) for specific missionTotal allowable fuel with all mission equipment plus Crew & Baggage identified in B-1 (a through i) in LBS. for specific missionActual Aircraft Takeoff weight (Mission Equip, Crew, Bags, Mission Fuel) From Departure MSL elevation and ISA TempStart, Runup, and Taxi fuel burn in LBS.Fuel burn in LBS. to 22,000 msl from 4500'MSL, at ISA +20 CTime to climb to 22,000 msl from 4500'MSL, at ISA +20 CDistance in nm to climb to 22,000 from 4500' MSL, at ISA +20CTotal fuel burn in LBS. to cruise 120 nm at 22,000 msl PAMission aircraft cruise configuration and calculated TASTime to cruise 120 nm at 22,000 msl Pressure AltFuel burn in decent to loiter, from 22,000 msl to 7,000 msl, Pressure AltTime to descend to loiter, from 22,000 msl to 7,000 msl, Pressure AltDistance in nm to descend to loiter, from 22,000 msl to 7,000 msl Pressure AltTotal fuel burn to loiter for three hours at 7,000 MSL, at Pressure AltAircraft loiter configurationVmca For loiter configurationVS1 at 30 deg AOB for loiter configuration1.3VS1 for loiter configurationFuel burn to climb from 7,000 MSL (working altitude) to 22,000 MSL PATime to climb from 7,000 MSL (working altitude) to 22,000 MSL PADistance in nm to climb from loiter at 7,000' msl at to 22,000 msl PATotal fuel burn in LBS. to cruise 120 nm at 22,000 MSL PA2Mission aircraft cruise config calculated TASTime to cruise 120 nm at 22,000 MSL PADecent 2 and Approach fuel burnDecent 2 and Approach timeDecent 2 and Approach distance in nmTotal Fuel remaining (in minutes) at landing under normal cruise configurationTotal fuel remaining at landing in LBS.
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2b

Offeror Company Name:
MissionBasic Aircraft InformationBasic Mission WeightsMission Takeoff & Climb1Cruise 1Decent 1LoiterClimb 2Cruise 2Decent 2, Approch, LandingFuel Remaining
2bMakeModelManufacturer Serial NumberFAA Registration NumberAircraft Max Allowable Zero Fuel Weight (If Applicable to Aircraft)Aircraft Max Ramp WeightAircraft Max Takeoff Gross WeightAircraft Max Landing WeightVyse at Max Gross Takeoff gross weightSingle Engine Service Ceiling . If Applicable (FAA-H-8083-3A Glossary Definition)Total aircraft usable fuel in LBS.Aircraft Empty Weight with all installed contract required/mission required equipmentAircraft weight with all mission equipment plus Crew & Baggage Identified in B-1 (a through i) for specific missionTotal allowable fuel with all mission equipment plus Crew & Baggage identified in B-1 (a through i) in LBS. for specific missionActual Aircraft Takeoff weight (Mission Equip, Crew, Bags, Mission Fuel) From Departure MSL elevation and ISA TempStart, Runup, and Taxi fuel burn in LBS.Fuel burn in LBS. to 22,000 msl from 4500'MSL, at ISA +20 CTime to climb to 22,000 msl from 4500'MSL, at ISA +20 CDistance in nm to climb to 22,000 from 4500' MSL, at ISA +20CTotal fuel burn in LBS. to cruise 120 nm at 22,000 msl PAMission aircraft cruise configuration and calculated TASTime to cruise 120 nm at 22,000 msl Pressure AltFuel burn in decent to loiter, from 22,000 msl to 7,000 msl, Pressure AltTime to descend to loiter, from 22,000 msl to 7,000 msl, Pressure AltDistance in nm to descend to loiter, from 22,000 msl to 7,000 msl Pressure AltTotal fuel burn to loiter for three hours at 7,000 MSL, at Pressure AltAircraft loiter configurationVmca For loiter configurationVS1 at 30 deg AOB for loiter configuration1.3VS1 for loiter configurationFuel burn to climb from 7,000 MSL (working altitude) to 22,000 MSL PATime to climb from 7,000 MSL (working altitude) to 22,000 MSL PADistance in nm to climb from loiter at 7,000' msl at to 22,000 msl PATotal fuel burn in LBS. to cruise 120 nm at 22,000 MSL PA2Mission aircraft cruise config calculated TASTime to cruise 120 nm at 22,000 MSL PADecent 2 and Approach fuel burnDecent 2 and Approach timeDecent 2 and Approach distance in nmTotal Fuel remaining (in minutes) at landing under normal cruise configurationTotal fuel remaining at landing in LBS.
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3a

Offeror Company Name:
MissionBasic Aircraft InformationBasic Mission WeightsMission Takeoff & Climb1Cruise 1Decent 1LoiterClimb 2Cruise 2Decent 2, Approch, LandingFuel Remaining
3aMakeModelManufacturer Serial NumberFAA Registration NumberAircraft Max Allowable Zero Fuel Weight (If Applicable to Aircraft)Aircraft Max Ramp WeightAircraft Max Takeoff Gross WeightAircraft Max Landing WeightVyse at Max Gross Takeoff gross weightSingle Engine Service Ceiling (FAA-H-8083-3A Glossary Definition)Total aircraft usable fuel in LBS.Aircraft Empty Weight with all installed contract required/mission required equipmentAircraft weight with all mission equipment plus Crew & Baggage Identified in B-1 (a thrugh i) for specific missionTotal allowable fuel with all mission equipment plus Crew & Baggage identified in B-1 (a through i) in LBS. for specific missionActual Aircraft Takeoff weight (Mission Equip, Crew, Bags, Mission Fuel) From Departure MSL elevation and ISA TempStart, Runup, and Taxi fuel burn in LBS.Fuel burn in LBS. to 22,000 msl from 4500'MSL, at ISA +20 CTime to climb to 22,000 msl from 4500'MSL, at ISA +20 CDistance in nm to climb to 22,000 from 4500' MSL, at ISA +20CTotal fuel burn in LBS. to cruise 120 nm at 22,000 msl PAMission aircraft cruise configuration and calculated TASTime to cruise 120 nm at 22,000 msl Pressure AltFuel burn in decent to loiter, from 22,000 msl to 7,000' msl, Pressure AltTime to decend to loiter, from 22,000 msl to 7,000' msl, Pressure AltDistance in nm to decend to loiter, from 22,000 msl to 7,000' msl Pressure AltTotal fuel burn to loiter for three hours at 7,000' MSL, at Pressure AltAircraft loiter configurationVmca For loiter configurationVS1 at 30 deg AOB for loiter configNo information required for this column. Intentionally left blankFuel burn in LBS. to 22,000 msl from 7000'MSL, at ISA +20 CTime to climb from 7,000' MSL (working altitude) to 22,000 MSL PADistance in nm to climb from loiter at 7,000' msl to 22,000 msl PATotal fuel burn in LBS. to cruise 120 nm at 22,000 MSL PA2Mission aircraft cruise config calculated TASTime to cruise 120 nm at 22,000 MSL PADecent 2 and Approach fuel burnDecent 2 and Approach timeDecent 2 and Approach distance in nmTotal Fuel remaining (in minutes) at landing under normal cruise configurationTotal fuel remaining at landing in LBS.
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3b

Offeror Company Name:
MissionBasic Aircraft InformationBasic Mission WeightsMission Takeoff & Climb1Cruise 1Decent 1LoiterClimb 2Cruise 2Decent 2, Approch, LandingFuel Remaining
3bMakeModelManufacturer Serial NumberFAA Registration NumberAircraft Max Allowable Zero Fuel Weight (If Applicable to Aircraft)Aircraft Max Ramp WeightAircraft Max Takeoff Gross WeightAircraft Max Landing WeightVyse at Max Gross Takeoff gross weight (If Applicable)Single Engine Service Ceiling . If Applicable (FAA-H-8083-3A Glossary Definition)Total aircraft usable fuel in LBS.Aircraft Empty Weight with all installed contract required/mission required equipmentAircraft weight with all mission equipment plus Crew & Baggage Identified in B-1 (a through i) for specific missionTotal allowable fuel with all mission equipment plus Crew & Baggage identified in B-1 (a through i) in LBS. for specific missionActual Aircraft Takeoff weight (Mission Equip, Crew, Bags, Mission Fuel) From Departure MSL elevation and ISA TempStart, Runup, and Taxi fuel burn in LBS.Fuel burn in LBS. to 10,500 msl from 4500'MSL, at ISA +20 CTime to climb to 10,500 msl from 4500'MSL, at ISA +20 CDistance in nm to climb to 10,500 from 4500' MSL, at ISA +20CTotal fuel burn in LBS. to cruise 75 nm at 10,500 msl PAMission aircraft cruise configuration and calculated TASTime to cruise 75 nm at 10,500 msl Pressure AltFuel burn in decent to loiter, from 10,500 msl to 7,000 msl, Pressure AltTime to descend to loiter, from 10,500 msl to 7,000 msl, Pressure AltDistance in nm to descend to loiter, from 10,500 msl to 7,000 msl Pressure AltTotal fuel burn to loiter for three hours at 7,000 MSL, at Pressure AltAircraft loiter configurationVmca For loiter configuration (If Applicable)VS1 at 30 deg AOB for loiter configuration1.3VS1 for loiter configurationFuel burn to climb from 7,000 MSL (working altitude) to 10,500 MSL PATime to climb from 7,000 MSL (working altitude) to 10,500 MSL PADistance in nm to climb from loiter at 7,000' msl at to 10,500 msl PATotal fuel burn in LBS. to cruise 75 nm at 10,500 MSL PA2Mission aircraft cruise config calculated TASTime to cruise 75 nm at 10,500 MSL PADecent 2 and Approach fuel burnDecent 2 and Approach timeDecent 2 and Approach distance in nmTotal Fuel remaining (in minutes) at landing under normal cruise configurationTotal fuel remaining at landing in LBS.
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4a

Offeror Company Name:
MissionBasic Aircraft InformationBasic Mission WeightsMission Takeoff & Climb1Cruise 1Decent 1LoiterClimb 2Cruise 2Decent 2, Approch, LandingFuel Remaining
4aMakeModelManufacturer Serial NumberFAA Registration NumberAircraft Max Allowable Zero Fuel Weight (If Applicable to Aircraft)Aircraft Max Ramp WeightAircraft Max Takeoff Gross WeightAircraft Max Landing WeightVyse at Max Gross Takeoff gross weight (If Applicable)Single Engine Service Ceiling . If Applicable (FAA-H-8083-3A Glossary Definition)Total aircraft usable fuel in LBS.Aircraft Empty Weight with all installed contract required/mission required equipmentAircraft weight with all mission equipment plus Crew & Baggage Identified in B-1 (a through i) for specific missionTotal allowable fuel with all mission equipment plus Crew & Baggage identified in B-1 (a through i) in LBS. for specific missionActual Aircraft Takeoff weight (Mission Equip, Crew, Bags, Mission Fuel) From Departure MSL elevation and ISA TempStart, Runup, and Taxi fuel burn in LBS.Fuel burn in LBS. to 22,000 msl from 4500'MSL, at ISA +20 CTime to climb to 22,000 msl from 4500'MSL, at ISA +20 CDistance in nm to climb to 22,000 from 4500' MSL, at ISA +20CTotal fuel burn in LBS. to cruise 125 nm at 22,000 msl PAMission aircraft cruise configuration and calculated TASTime to cruise 125 nm at 22,000 msl Pressure AltFuel burn in decent to loiter, from 22,000 msl to 14,500 msl, Pressure AltTime to descend to loiter, from 22,000 msl to 14,500 msl, Pressure AltDistance in nm to descend to loiter, from 22,000 msl to 14,500 msl Pressure AltTotal fuel burn to loiter for three hours at 14,500 MSL, at Pressure AltAircraft loiter configurationVmca For loiter configuration (If Applicable)VS1 at 30 deg AOB for loiter configuration1.3VS1 for loiter configurationFuel burn to climb from 14,500 MSL (working altitude) to 22,000 MSL PATime to climb from 14,500 MSL (working altitude) to 22,000 MSL PADistance in nm to climb from loiter at 14,500' msl at to 22,000 msl PATotal fuel burn in LBS. to cruise 125 nm at 22,000 MSL PA2Mission aircraft cruise config calculated TASTime to cruise 125 nm at 22,000 MSL PADecent 2 and Approach fuel burnDecent 2 and Approach timeDecent 2 and Approach distance in nmTotal Fuel remaining (in minutes) at landing under normal cruise configurationTotal fuel remaining at landing in LBS.
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4b

Offeror Company Name:
MissionBasic Aircraft InformationBasic Mission WeightsMission Takeoff & Climb1Cruise 1Decent 1LoiterClimb 2Cruise 2Decent 2, Approch, LandingFuel Remaining
4bMakeModelManufacturer Serial NumberFAA Registration NumberAircraft Max Allowable Zero Fuel Weight (If Applicable to Aircraft)Aircraft Max Ramp WeightAircraft Max Takeoff Gross WeightAircraft Max Landing WeightVyse at Max Gross Takeoff gross weight (If Applicable)Single Engine Service Ceiling . If Applicable (FAA-H-8083-3A Glossary Definition)Total aircraft usable fuel in LBS.Aircraft Empty Weight with all installed contract required/mission required equipmentAircraft weight with all mission equipment plus Crew & Baggage Identified in B-1 (a through i) for specific missionTotal allowable fuel with all mission equipment plus Crew & Baggage identified in B-1 (a through i) in LBS. for specific missionActual Aircraft Takeoff weight (Mission Equip, Crew, Bags, Mission Fuel) From Departure MSL elevation and ISA TempStart, Runup, and Taxi fuel burn in LBS.Fuel burn in LBS. to 22,000 msl from 4500'MSL, at ISA +20 CTime to climb to 22,000 msl from 4500'MSL, at ISA +20 CDistance in nm to climb to 22,000 from 4500' MSL, at ISA +20CTotal fuel burn in LBS. to cruise 125 nm at 22,000 msl PAMission aircraft cruise configuration and calculated TASTime to cruise 125 nm at 22,000 msl Pressure AltFuel burn in decent to loiter, from 22,000 msl to 41,500 msl, Pressure AltTime to descend to loiter, from 22,000 msl to 14,500 msl, Pressure AltDistance in nm to descend to loiter, from 22,000 msl to 14,500 msl Pressure AltTotal fuel burn to loiter for three hours at 14,500 MSL, at Pressure AltAircraft loiter configurationVmca For loiter configuration (If Applicable)VS1 at 30 deg AOB for loiter configuration1.3VS1 for loiter configurationFuel burn to climb from 14,500 MSL (working altitude) to 22,000 MSL PATime to climb from 14,500 MSL (working altitude) to 22,000 MSL PADistance in nm to climb from loiter at 14,500' msl at to 22,000 msl PATotal fuel burn in LBS. to cruise 125 nm at 22,000 MSL PA3Mission aircraft cruise config calculated TASTime to cruise 125 nm at 22,000 MSL PADecent 2 and Approach fuel burnDecent 2 and Approach timeDecent 2 and Approach distance in nmTotal Fuel remaining (in minutes) at landing under normal cruise configurationTotal fuel remaining at landing in LBS.
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4c

Offeror Company Name:
MissionBasic Aircraft InformationBasic Mission WeightsMission Takeoff & Climb1Cruise 1Decent 1LoiterClimb 2Cruise 2Decent 2, Approch, LandingFuel Remaining
4cMakeModelManufacturer Serial NumberFAA Registration NumberAircraft Max Allowable Zero Fuel Weight (If Applicable to Aircraft)Aircraft Max Ramp WeightAircraft Max Takeoff Gross WeightAircraft Max Landing WeightVyse at Max Gross Takeoff gross weight (If Applicable)Single Engine Service Ceiling . If Applicable (FAA-H-8083-3A Glossary Definition)Total aircraft usable fuel in LBS.Aircraft Empty Weight with all installed contract required/mission required equipmentAircraft weight with all mission equipment plus Crew & Baggage Identified in B-1 (a through i) for specific missionTotal allowable fuel with all mission equipment plus Crew & Baggage identified in B-1 (a through i) in LBS. for specific missionActual Aircraft Takeoff weight (Mission Equip, Crew, Bags, Mission Fuel) From Departure MSL elevation and ISA TempStart, Runup, and Taxi fuel burn in LBS.Fuel burn in LBS. to 10,500 msl from Sea Level, Standard DayTime to climb to 10,500 msl from Sea Level, Standard DayDistance in nm to climb to 10,500 from Sea Level, Standard DayTotal fuel burn in LBS. to cruise 75 nm at 10,500 msl PAMission aircraft cruise configuration and calculated TASTime to cruise 75 nm at 10,500 msl Pressure AltFuel burn in decent to loiter, from10,500 msl to 7,500 msl, Pressure AltTime to descend to loiter, from 10,500 msl to 7,500 msl, Pressure AltDistance in nm to descend to loiter, from10,500 msl to 7,500 msl Pressure AltTotal fuel burn to loiter for three hours at 7,500 MSL, at Pressure AltAircraft loiter configurationVmca For loiter configuration (If Applicable)VS1 at 30 deg AOB for loiter configuration1.3VS1 for loiter configurationFuel burn to climb from 7,500 MSL (working altitude) to 10,500 MSL PATime to climb from 7,500 MSL (working altitude) to 10,500 MSL PADistance in nm to climb from loiter at 7,500' msl at to 10,500 msl PATotal fuel burn in LBS. to cruise 150 nm at 10,500 MSL PAMission aircraft cruise config calculated TASTime to cruise 75 nm at 10,500 MSL PADecent 2 and Approach fuel burnDecent 2 and Approach timeDecent 2 and Approach distance in nmTotal Fuel remaining (in minutes) at landing under normal cruise configurationTotal fuel remaining at landing in LBS.
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5a

Offeror Company Name:
MissionBasic Aircraft InformationBasic Mission WeightsMission Takeoff & Climb1Cruise 1Descent 1LoiterClimb 2Cruise 2Descent 2, Approch, LandingFuel Remaining
5aMakeModelManufacturer Serial NumberFAA Registration NumberLanding gear configuration - Wheels, Straight Floats, Anphib Floats, or Ski. (If Multiple Configs offered complete a separate line for each config)Gravel, Grass, Unimproved airstrip capable and configuredTakeoff distance over 50 foot tall obstacle at Max Gross Weight Standard Day Sea levelLanding distance over 50 foot tall obstacle at Max Gross Weight Standard Day Sea levelTakeoff distance over 50 foot tall obstacle at Max Gross Weight 4,500 Ft PA ISA +20Landing distance over 50 foot tall obstacle at Max Gross Weight 4,500 Ft PA ISA +20Aircraft Max Allowable Zero Fuel Weight (If Applicable to Aircraft)Aircraft Max Ramp WeightAircraft Max Takeoff Gross WeightAircraft Max Landing WeightVyse at Max Gross Takeoff gross weight (If Applicable) KIASSingle Engine Service Ceiling (If Applicable)Total aircraft usable fuel in LBS.Aircraft Empty Weight with all installed contract required/mission required equipmentAircraft weight with all mission equipment plus Crew & Baggage Identified in B-1 (a through i) for specific missionTotal allowable fuel with all mission equipment plus Crew & Baggage identified in B-1 (a through i) in LBS. for specific missionActual Aircraft Takeoff weight (Mission Equip, Crew, Bags, Mission Fuel) From Departure MSL elevation and ISA TempStart, Runup, and Taxi fuel burn in LBS.Fuel burn in LBS. to 10,500 msl from 4500'MSL, at ISA +20 CTime to climb to 10,500 msl from 4500'MSL, at ISA +20 CDistance in nm to climb to 10,500 from 4500' MSL, at ISA +20CTotal fuel burn in LBS. to cruise 50 nm at 10,500 msl PAMission aircraft cruise configuration and calculated TASTime to cruise 50 nm at 10,500 msl Pressure Alt (min)Fuel burn in Descent to loiter, from 10,500 msl to 7,000 msl, Pressure AltTime to descend to loiter, from 10,500 msl to 7,000 msl, Pressure AltDistance in nm to descend to loiter, from 10,500 msl to 7,000 msl Pressure AltTotal fuel burn to loiter for three hours at 7,000 MSL, at Pressure AltAircraft loiter configurationVmca For loiter configuration (If Applicable)VS1 at 30 deg AOB for loiter config (KIAS)1.3VS1 for loiter configurationFuel burn to climb from 7,000 MSL (working altitude) to 10,500 MSL PATime to climb from 7,000 MSL (working altitude) to 10,500 MSL PADistance in nm to climb from loiter at 7,000' msl at to 10,500 msl PATotal fuel burn in LBS. to cruise 50 nm at 10,500 MSL PA2Mission aircraft cruise config calculated TASTime to cruise 50 nm at 10,500 MSL PADescent 2 and Approach fuel burnDescent 2 and Approach timeDescent 2 and Approach distance in nmTotal Fuel remaining (in minutes) at landing under normal cruise configurationTotal fuel remaining at landing in LBS.
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5b

Offeror Company Name:
MissionBasic Aircraft InformationBasic Mission WeightsMission Takeoff & Climb1Cruise 1Descent 1LoiterClimb 2Cruise 2Descent 2, Approch, LandingFuel Remaining
5bMakeModelManufacturer Serial NumberFAA Registration NumberLanding gear configuration - Wheels, Straight Floats, Anphib Floats, or Ski. (If Multiple Configs offered complete a separate line for each config)Gravel, Grass, Unimproved airstrip capable and configuredTakeoff distance over 50 foot tall obstacle at Max Gross Weight Standard Day Sea levelLanding distance over 50 foot tall obstacle at Max Gross Weight Standard Day Sea levelTakeoff distance over 50 foot tall obstacle at Max Gross Weight 4,500 Ft PA ISA +20Landing distance over 50 foot tall obstacle at Max Gross Weight 4,500 Ft PA ISA +20Aircraft Max Allowable Zero Fuel Weight (If Applicable to Aircraft)Aircraft Max Ramp WeightAircraft Max Takeoff Gross WeightAircraft Max Landing WeightVyse at Max Gross Takeoff gross weight (If Applicable)Single Engine Service Ceiling (If Applicable)Total aircraft usable fuel in LBS.Aircraft Empty Weight with all installed contract required/mission required equipmentAircraft weight with all mission equipment plus Crew & Baggage Identified in B-1 (a through i) for specific missionTotal allowable fuel with all mission equipment plus Crew & Baggage identified in B-1 (a through i) in LBS. for specific missionActual Aircraft Takeoff weight (Mission Equip, Crew, Bags, Mission Fuel) From Departure MSL elevation and ISA TempStart, Runup, and Taxi fuel burn in LBS.Fuel burn in LBS. to 10,500 msl from 4500'MSL, at ISA +20 CTime to climb to 10,500 msl from 4500'MSL, at ISA +20 CDistance in nm to climb to 10,500 from 4500' MSL, at ISA +20CTotal fuel burn in LBS. to cruise 50 nm at 10,500 msl PAMission aircraft cruise configuration and calculated TASTime to cruise 50 nm at 10,500 msl Pressure Alt (min)Fuel burn in Descent to loiter, from 10,500 msl to 7,000 msl, Pressure AltTime to descend to loiter, from 10,500 msl to 7,000 msl, Pressure AltDistance in nm to descend to loiter, from 10,500 msl to 7,000 msl Pressure AltTotal fuel burn to loiter for three hours at 7,000 MSL, at Pressure AltAircraft loiter configurationVmca For loiter configuration (If Applicable)VS1 at 30 deg AOB for loiter configuration1.3VS1 for loiter configurationFuel burn to climb from 7,000 MSL (working altitude) to 10,500 MSL PATime to climb from 7,000 MSL (working altitude) to 10,500 MSL PADistance in nm to climb from loiter at 7,000' msl at to 10,500 msl PATotal fuel burn in LBS. to cruise 50 nm at 10,500 MSL PA3Mission aircraft cruise config calculated TASTime to cruise 50 nm at 10,500 MSL PADescent 2 and Approach fuel burnDescent 2 and Approach timeDescent 2 and Approach distance in nmTotal Fuel remaining (in minutes) at landing under normal cruise configurationTotal fuel remaining at landing in LBS.
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5b

6a

Offeror Company Name:
MissionBasic Aircraft InformationBasic Mission WeightsMission Takeoff & Climb1Cruise 1Descent 1LoiterClimb 2Cruise 2Descent 2, Approch, LandingFuel Remaining
6aMakeModelManufacturer Serial NumberFAA Registration NumberLanding gear configuration - Wheels, Straight Floats, Anphib Floats, or Ski. (If Multiple Configs offered complete a separate line for each config)Gravel, Grass, Unimproved airstrip capable and configuredTakeoff distance over 50 foot tall obstacle at Max Gross Weight Standard Day Sea levelLanding distance over 50 foot tall obstacle at Max Gross Weight Standard Day Sea levelTakeoff distance over 50 foot tall obstacle at Max Gross Weight 4,500 Ft PA ISA +20Landing distance over 50 foot tall obstacle at Max Gross Weight 4,500 Ft PA ISA +20Aircraft Max Allowable Zero Fuel Weight (If Applicable to Aircraft)Aircraft Max Ramp WeightAircraft Max Takeoff Gross WeightAircraft Max Landing WeightVyse at Max Gross Takeoff gross weight (If Applicable)Single Engine Service Ceiling (If Applicable)Total aircraft usable fuel in LBS.Aircraft Empty Weight with all installed contract required/mission required equipmentAircraft weight with all mission equipment plus Crew & Baggage Identified in B-1 (a through i) for specific missionTotal allowable fuel with all mission equipment plus Crew & Baggage identified in B-1 (a through i) in LBS. for specific missionActual Aircraft Takeoff weight (Mission Equip, Crew, Bags, Mission Fuel) From Departure MSL elevation and ISA TempStart, Runup, and Taxi fuel burn in LBS.Fuel burn in LBS. to 10,500 msl from 4500'MSL, at ISA +20 CTime to climb to 10,500 msl from 4500'MSL, at ISA +20 CDistance in nm to climb to 10,500 from 4500' MSL, at ISA +20CTotal fuel burn in LBS. to cruise 75 nm at 10,500 msl PAMission aircraft cruise configuration and calculated TASTime to cruise 75 nm at 10,500 msl Pressure AltFuel burn in Descent to loiter, from 10,500 msl to 7,000 msl, Pressure AltTime to descend to loiter, from 10,500 msl to 7,000 msl, Pressure AltDistance in nm to descend to loiter, from 10,500 msl to 7,000 msl Pressure AltTotal fuel burn to loiter for three hours at 7,000 MSL, at Pressure AltAircraft loiter configurationVmca For loiter configuration (If Applicable)VS1 at 30 deg AOB for loiter configuration1.3VS1 for loiter configurationFuel burn to climb from 7,000 MSL (working altitude) to 10,500 MSL PATime to climb from 7,000 MSL (working altitude) to 10,500 MSL PADistance in nm to climb from loiter at 7,000' msl at to 10,500 msl PATotal fuel burn in LBS. to cruise 75 nm at 10,500 MSL PA2Mission aircraft cruise config calculated TASTime to cruise 75 nm at 10,500 MSL PADescent 2 and Approach fuel burnDescent 2 and Approach timeDescent 2 and Approach distance in nmTotal Fuel remaining (in minutes) at landing under normal cruise configurationTotal fuel remaining at landing in LBS.
6a
6a
6a
6a
6a
6a
6a
6a
6a
6a
6a
6a
6a
6a
6a
6a
6a
6a
6a
6a
6a

6b

Offeror Company Name:
MissionBasic Aircraft InformationBasic Mission WeightsMission Takeoff & Climb1Cruise 1Descent 1LoiterClimb 2Cruise 2Descent 2, Approch, LandingFuel Remaining
6bMakeModelManufacturer Serial NumberFAA Registration NumberLanding gear configuration - Wheels, Straight Floats, Anphib Floats, or Ski. (If Multiple Configs offered complete a separate line for each config)Gravel, Grass, Unimproved airstrip capable and configuredTakeoff distance over 50 foot tall obstacle at Max Gross Weight Standard Day Sea levelLanding distance over 50 foot tall obstacle at Max Gross Weight Standard Day Sea levelTakeoff distance over 50 foot tall obstacle at Max Gross Weight 4,500 Ft PA ISALanding distance over 50 foot tall obstacle at Max Gross Weight 4,500 Ft PA ISAAircraft Max Allowable Zero Fuel Weight (If Applicable to Aircraft)Aircraft Max Ramp WeightAircraft Max Takeoff Gross WeightAircraft Max Landing WeightVyse at Max Gross Takeoff gross weight (If Applicable)Single Engine Service Ceiling (If Applicable)Total aircraft usable fuel in LBS.Aircraft Empty Weight with all installed contract required/mission required equipmentAircraft weight with all mission equipment plus Crew & Baggage Identified in B-1 (a through i) for specific missionTotal allowable fuel with all mission equipment plus Crew & Baggage identified in B-1 (a through i) in LBS. for specific missionActual Aircraft Takeoff weight (Mission Equip, Crew, Bags, Mission Fuel) From Departure MSL elevation and ISA TempStart, Runup, and Taxi fuel burn in LBS.Fuel burn in LBS. to 5,500 msl from Sea Level, at ISA +20 CTime to climb to 5,500 msl from Sea Level at ISA +20 CDistance in nm to climb to 5,500 from Sea Level, at ISA +20CTotal fuel burn in LBS. to cruise 50 nm at 5,500 msl PAMission aircraft cruise configuration and calculated TASTime to cruise 50 nm at 5,500 msl Pressure AltFuel burn in Descent to loiter, from 5,500 msl to 3,000 msl, Pressure AltTime to descend to loiter, from 5,500 msl to 3,00msl, Pressure AltDistance in nm to descend to loiter, from 5,500 msl to 3,000 msl Pressure AltTotal fuel burn to loiter for three hours at 3,000 MSL, at Pressure AltAircraft loiter configurationVmca For loiter configuration (If Applicable)VS1 at 30 deg AOB for loiter configuration1.3VS1 for loiter configurationFuel burn to climb from 3,000 MSL (working altitude) to 5,500 MSL PATime to climb from 3,000 MSL (working altitude) to 5,500 MSL PADistance in nm to climb from loiter at 3,000' msl at to 5,500 msl PATotal fuel burn in LBS. to cruise 50 nm at 5,500 MSL PA2Mission aircraft cruise config calculated TASTime to cruise 50 nm at 5,500 MSL PADescent 2 and Approach fuel burnDescent 2 and Approach timeDescent 2 and Approach distance in nmTotal Fuel remaining (in minutes) at landing under normal cruise configurationTotal fuel remaining at landing in LBS.
6b
6b
6b
6b
6b
6b
6b
6b
6b
6b
6b
6b
6b
6b
6b
6b
6b
6b
6b
6b
6b
Offeror Company Name:
MissionBasic Aircraft InformationBasic Mission WeightsMission Takeoff & Climb1Cruise 1Descent 1LoiterClimb 2Cruise 2Descent 2, Approch, LandingFuel Remaining
7MakeModelManufacturer Serial NumberFAA Registration NumberLanding gear configuration - Wheels, Straight Floats, Anphib Floats, or Ski. (If Multiple Configs offered complete a separate line for each config)Gravel, Grass, Unimproved airstrip capable and configuredTakeoff distance over 50 foot tall obstacle at Max Gross Weight Standard Day Sea levelLanding distance over 50 foot tall obstacle at Max Gross Weight Standard Day Sea levelTakeoff distance over 50 foot tall obstacle at Max Gross Weight 4,500 Ft PA ISALanding distance over 50 foot tall obstacle at Max Gross Weight 4,500 Ft PA ISAAircraft Max Allowable Zero Fuel Weight (If Applicable to Aircraft)Aircraft Max Ramp WeightAircraft Max Takeoff Gross WeightAircraft Max Landing WeightVyse at Max Gross Takeoff gross weight (If Applicable)Single Engine Service Ceiling (If Applicable)Total aircraft usable fuel in LBS.Aircraft Empty Weight with all installed contract required/mission required equipmentAircraft weight with all mission equipment plus Crew & Baggage Identified in B-1 (a through i) for specific missionTotal allowable fuel with all mission equipment plus Crew & Baggage identified in B-1 (a through i) in LBS. for specific missionActual Aircraft Takeoff weight (Mission Equip, Crew, Bags, Mission Fuel) From Departure MSL elevation and ISA TempStart, Runup, and Taxi fuel burn in LBS.Fuel burn in LBS. to 5,500 msl from Sea Level, Standard DayTime to climb to 5,500 msl from Sea Level at Standard DayDistance in nm to climb to 5,500 from Sea Level, Standard DayTotal fuel burn in LBS. to cruise 50 nm at 5,500 msl PAMission aircraft cruise configuration and calculated TASTime to cruise 50 nm at 5,500 msl Pressure AltFuel burn in Descent to loiter, from 5,500 msl to 3,000 msl, Pressure AltTime to descend to loiter, from 5,500 msl to 3,00msl, Pressure AltDistance in nm to descend to loiter, from 5,500 msl to 3,000 msl Pressure AltTotal fuel burn to loiter for three hours at 3,000 MSL, at Pressure AltAircraft loiter configurationVmca For loiter configuration (If Applicable)VS1 at 30 deg AOB for loiter configuration1.3VS1 for loiter configurationFuel burn to climb from 3,000 MSL (working altitude) to 5,500 MSL PATime to climb from 3,000 MSL (working altitude) to 5,500 MSL PADistance in nm to climb from loiter at 3,000' msl at to 5,500 msl PATotal fuel burn in LBS. to cruise 50 nm at 5,500 MSL PA2Mission aircraft cruise config calculated TASTime to cruise 50 nm at 5,500 MSL PADescent 2 and Approach fuel burnDescent 2 and Approach timeDescent 2 and Approach distance in nmTotal Fuel remaining (in minutes) at landing under normal cruise configurationTotal fuel remaining at landing in LBS.
7
7
7
7
7
7
7
7
7
7
7
7
7
7
7
7
7
7
7
7
7

File details come from the government source that posted it. Updated .