Exhibit 6 Rev 9.1 09242024 FINAL.xlsx
XLSX spreadsheet 31 KB Posted
- Attached to
- National Light Fixed Wing - Multiple Award Task Order Contract (NLFW MATOC) Reopen Federal contract opportunity
- Solicitation number
- 1202SA25R9402
- Issued by
- Department of Agriculture Forest Service
About this file
This document appears to be an Excel spreadsheet titled "Exhibit 6 Rev 9.1 09242024 FINAL.xlsx" that contains detailed technical specifications and performance data for various aircraft that could be offered under the National Light Fixed Wing - Multiple Award Task Order Contract (NLFW MATOC) Reopen solicitation.
The spreadsheet provides detailed performance parameters for different aircraft models, including information on takeoff and landing distances, climb and cruise performance, fuel capacity and consumption, service ceiling, and other relevant technical details. This level of detailed technical information is likely required as part of the response to the NLFW MATOC Reopen solicitation, which seeks to obtain fixed-wing aircraft operated by qualified personnel to support various government missions such as fire, project, resource, law enforcement, and administrative flights on public lands. The solicitation is being issued by the U.S. Department of Agriculture Forest Service.
View the file
Other files for this federal contract opportunity
| File | Type | Posted |
|---|---|---|
| 1202SA25R9402 A00001.pdf | ||
| 1202SA25R9402 A00001.pdf | ||
| Exhibit 1 SOI.xlsx | XLSX spreadsheet | |
| 1202SA25R9402 NLFW Reopener.pdf | ||
| Exhibit 5 Airplane Pilot Qualification record.pdf | ||
| Exhibit 7 Avionics.pdf | ||
| Exhibit 1 SOI.xlsx | XLSX spreadsheet | |
| Exhibit 4 Weight and Balance.xlsx | XLSX spreadsheet |
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Text version
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| Mission | Basic Aircraft Information | Basic Mission Weights | Mission Takeoff & Climb1 | Cruise 1 | Decent 1 | Loiter | Climb 2 | Cruise 2 | Decent 2, Approch, Landing | Fuel Remaining | |||||||||||||||||||||||||||||||
| 1 | Make | Model | Manufacturer Serial Number | FAA Registration Number | Aircraft Max Allowable Zero Fuel Weight (If Applicable to Aircraft) | Aircraft Max Ramp Weight | Aircraft Max Takeoff Gross Weight | Aircraft Max Landing Weight | Vyse at Max Gross Takeoff gross weight | Single Engine Service Ceiling | Total aircraft usable fuel in LBS. | Aircraft Empty Weight with all installed contract required/mission required equipment | Aircraft weight with all mission equipment plus Crew & Baggage Identified in B-1 (a through i) for specific mission | Total allowable fuel with all mission equipment plus Crew & Baggage identified in B-1 (a through i) in LBS. for specific mission | Actual Aircraft Takeoff weight (Mission Equip, Crew, Bags, Mission Fuel) From Departure MSL elevation and ISA Temp | Start, Runup, and Taxi fuel burn in LBS. | Fuel burn in LBS. to 22,000 msl from 4500'MSL, at ISA +20 C | Time to climb to 22,000 msl from 4500'MSL, at ISA +20 C | Distance in nm to climb to 22,000 from 4500' MSL, at ISA +20C | Total fuel burn in LBS. to cruise 150 nm at 22,000 msl PA | Mission aircraft cruise configuration and calculated TAS | Time to cruise 150 nm at 22,000 msl Pressure Alt | Fuel burn in decent to loiter, from 22,000 msl to 14,500 msl, Pressure Alt | Time to descend to loiter, from 22,000 msl to 14,500 msl, Pressure Alt | Distance in nm to descend to loiter, from 22,000 msl to 14,500 msl Pressure Alt | Total fuel burn to loiter for three hours at 14,500 MSL, at Pressure Alt | Aircraft loiter configuration | Vmca For loiter configuration | VS1 at 30 deg AOB for loiter configuration | 1.3VS1 for loiter configuration | Fuel burn to climb from 14,500 MSL (working altitude) to 22,000 MSL PA | Time to climb from 14,500 MSL (working altitude) to 22,000 MSL PA | Distance in nm to climb from loiter at 14,500' msl at to 22,000 msl PA | Total fuel burn in LBS. to cruise 150 nm at 22,000 MSL PA2 | Mission aircraft cruise config calculated TAS | Time to cruise 150 nm at 22,000 MSL PA | Decent 2 and Approach fuel burn | Decent 2 and Approach time | Decent 2 and Approach distance in nm | Total Fuel remaining (in minutes) at landing under normal cruise configuration | Total fuel remaining at landing in LBS. |
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2a
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| Mission | Basic Aircraft Information | Basic Mission Weights | Mission Takeoff & Climb1 | Cruise 1 | Decent 1 | Loiter | Climb 2 | Cruise 2 | Decent 2, Approch, Landing | Fuel Remaining | |||||||||||||||||||||||||||||||
| 2a | Make | Model | Manufacturer Serial Number | FAA Registration Number | Aircraft Max Allowable Zero Fuel Weight (If Applicable to Aircraft) | Aircraft Max Ramp Weight | Aircraft Max Takeoff Gross Weight | Aircraft Max Landing Weight | Vyse at Max Gross Takeoff gross weight | Single Engine Service Ceiling | Total aircraft usable fuel in LBS. | Aircraft Empty Weight with all installed contract required/mission required equipment | Aircraft weight with all mission equipment plus Crew & Baggage Identified in B-1 (a through i) for specific mission | Total allowable fuel with all mission equipment plus Crew & Baggage identified in B-1 (a through i) in LBS. for specific mission | Actual Aircraft Takeoff weight (Mission Equip, Crew, Bags, Mission Fuel) From Departure MSL elevation and ISA Temp | Start, Runup, and Taxi fuel burn in LBS. | Fuel burn in LBS. to 22,000 msl from 4500'MSL, at ISA +20 C | Time to climb to 22,000 msl from 4500'MSL, at ISA +20 C | Distance in nm to climb to 22,000 from 4500' MSL, at ISA +20C | Total fuel burn in LBS. to cruise 120 nm at 22,000 msl PA | Mission aircraft cruise configuration and calculated TAS | Time to cruise 120 nm at 22,000 msl Pressure Alt | Fuel burn in decent to loiter, from 22,000 msl to 7,000 msl, Pressure Alt | Time to descend to loiter, from 22,000 msl to 7,000 msl, Pressure Alt | Distance in nm to descend to loiter, from 22,000 msl to 7,000 msl Pressure Alt | Total fuel burn to loiter for three hours at 7,000 MSL, at Pressure Alt | Aircraft loiter configuration | Vmca For loiter configuration | VS1 at 30 deg AOB for loiter configuration | 1.3VS1 for loiter configuration | Fuel burn to climb from 7,000 MSL (working altitude) to 22,000 MSL PA | Time to climb from 7,000 MSL (working altitude) to 22,000 MSL PA | Distance in nm to climb from loiter at 7,000' msl at to 22,000 msl PA | Total fuel burn in LBS. to cruise 120 nm at 22,000 MSL PA2 | Mission aircraft cruise config calculated TAS | Time to cruise 120 nm at 22,000 MSL PA | Decent 2 and Approach fuel burn | Decent 2 and Approach time | Decent 2 and Approach distance in nm | Total Fuel remaining (in minutes) at landing under normal cruise configuration | Total fuel remaining at landing in LBS. |
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2b
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| Mission | Basic Aircraft Information | Basic Mission Weights | Mission Takeoff & Climb1 | Cruise 1 | Decent 1 | Loiter | Climb 2 | Cruise 2 | Decent 2, Approch, Landing | Fuel Remaining | |||||||||||||||||||||||||||||||
| 2b | Make | Model | Manufacturer Serial Number | FAA Registration Number | Aircraft Max Allowable Zero Fuel Weight (If Applicable to Aircraft) | Aircraft Max Ramp Weight | Aircraft Max Takeoff Gross Weight | Aircraft Max Landing Weight | Vyse at Max Gross Takeoff gross weight | Single Engine Service Ceiling | Total aircraft usable fuel in LBS. | Aircraft Empty Weight with all installed contract required/mission required equipment | Aircraft weight with all mission equipment plus Crew & Baggage Identified in B-1 (a through i) for specific mission | Total allowable fuel with all mission equipment plus Crew & Baggage identified in B-1 (a through i) in LBS. for specific mission | Actual Aircraft Takeoff weight (Mission Equip, Crew, Bags, Mission Fuel) From Departure MSL elevation and ISA Temp | Start, Runup, and Taxi fuel burn in LBS. | Fuel burn in LBS. to 22,000 msl from 4500'MSL, at ISA +20 C | Time to climb to 22,000 msl from 4500'MSL, at ISA +20 C | Distance in nm to climb to 22,000 from 4500' MSL, at ISA +20C | Total fuel burn in LBS. to cruise 120 nm at 22,000 msl PA | Mission aircraft cruise configuration and calculated TAS | Time to cruise 120 nm at 22,000 msl Pressure Alt | Fuel burn in decent to loiter, from 22,000 msl to 7,000 msl, Pressure Alt | Time to descend to loiter, from 22,000 msl to 7,000 msl, Pressure Alt | Distance in nm to descend to loiter, from 22,000 msl to 7,000 msl Pressure Alt | Total fuel burn to loiter for three hours at 7,000 MSL, at Pressure Alt | Aircraft loiter configuration | Vmca For loiter configuration | VS1 at 30 deg AOB for loiter configuration | 1.3VS1 for loiter configuration | Fuel burn to climb from 7,000 MSL (working altitude) to 22,000 MSL PA | Time to climb from 7,000 MSL (working altitude) to 22,000 MSL PA | Distance in nm to climb from loiter at 7,000' msl at to 22,000 msl PA | Total fuel burn in LBS. to cruise 120 nm at 22,000 MSL PA2 | Mission aircraft cruise config calculated TAS | Time to cruise 120 nm at 22,000 MSL PA | Decent 2 and Approach fuel burn | Decent 2 and Approach time | Decent 2 and Approach distance in nm | Total Fuel remaining (in minutes) at landing under normal cruise configuration | Total fuel remaining at landing in LBS. |
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3a
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| Mission | Basic Aircraft Information | Basic Mission Weights | Mission Takeoff & Climb1 | Cruise 1 | Decent 1 | Loiter | Climb 2 | Cruise 2 | Decent 2, Approch, Landing | Fuel Remaining | |||||||||||||||||||||||||||||||
| 3a | Make | Model | Manufacturer Serial Number | FAA Registration Number | Aircraft Max Allowable Zero Fuel Weight (If Applicable to Aircraft) | Aircraft Max Ramp Weight | Aircraft Max Takeoff Gross Weight | Aircraft Max Landing Weight | Vyse at Max Gross Takeoff gross weight | Single Engine Service Ceiling | Total aircraft usable fuel in LBS. | Aircraft Empty Weight with all installed contract required/mission required equipment | Aircraft weight with all mission equipment plus Crew & Baggage Identified in B-1 (a thrugh i) for specific mission | Total allowable fuel with all mission equipment plus Crew & Baggage identified in B-1 (a through i) in LBS. for specific mission | Actual Aircraft Takeoff weight (Mission Equip, Crew, Bags, Mission Fuel) From Departure MSL elevation and ISA Temp | Start, Runup, and Taxi fuel burn in LBS. | Fuel burn in LBS. to 22,000 msl from 4500'MSL, at ISA +20 C | Time to climb to 22,000 msl from 4500'MSL, at ISA +20 C | Distance in nm to climb to 22,000 from 4500' MSL, at ISA +20C | Total fuel burn in LBS. to cruise 120 nm at 22,000 msl PA | Mission aircraft cruise configuration and calculated TAS | Time to cruise 120 nm at 22,000 msl Pressure Alt | Fuel burn in decent to loiter, from 22,000 msl to 7,000' msl, Pressure Alt | Time to decend to loiter, from 22,000 msl to 7,000' msl, Pressure Alt | Distance in nm to decend to loiter, from 22,000 msl to 7,000' msl Pressure Alt | Total fuel burn to loiter for three hours at 7,000' MSL, at Pressure Alt | Aircraft loiter configuration | Vmca For loiter configuration | VS1 at 30 deg AOB for loiter config | 1.3VS1 for loiter configuration | Fuel burn in LBS. to 22,000 msl from 7000'MSL, at ISA +20 C | Time to climb from 7,000' MSL (working altitude) to 22,000 MSL PA | Distance in nm to climb from loiter at 7,000' msl to 22,000 msl PA | Total fuel burn in LBS. to cruise 120 nm at 22,000 MSL PA2 | Mission aircraft cruise config calculated TAS | Time to cruise 120 nm at 22,000 MSL PA | Decent 2 and Approach fuel burn | Decent 2 and Approach time | Decent 2 and Approach distance in nm | Total Fuel remaining (in minutes) at landing under normal cruise configuration | Total fuel remaining at landing in LBS. |
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3b
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| Mission | Basic Aircraft Information | Basic Mission Weights | Mission Takeoff & Climb1 | Cruise 1 | Decent 1 | Loiter | Climb 2 | Cruise 2 | Decent 2, Approch, Landing | Fuel Remaining | |||||||||||||||||||||||||||||||
| 3b | Make | Model | Manufacturer Serial Number | FAA Registration Number | Aircraft Max Allowable Zero Fuel Weight (If Applicable to Aircraft) | Aircraft Max Ramp Weight | Aircraft Max Takeoff Gross Weight | Aircraft Max Landing Weight | Vyse 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 equipment | Aircraft weight with all mission equipment plus Crew & Baggage Identified in B-1 (a through i) for specific mission | Total allowable fuel with all mission equipment plus Crew & Baggage identified in B-1 (a through i) in LBS. for specific mission | Actual Aircraft Takeoff weight (Mission Equip, Crew, Bags, Mission Fuel) From Departure MSL elevation and ISA Temp | Start, Runup, and Taxi fuel burn in LBS. | Fuel burn in LBS. to 10,500 msl from 4500'MSL, at ISA +20 C | Time to climb to 10,500 msl from 4500'MSL, at ISA +20 C | Distance in nm to climb to 10,500 from 4500' MSL, at ISA +20C | Total fuel burn in LBS. to cruise 75 nm at 10,500 msl PA | Mission aircraft cruise configuration and calculated TAS | Time to cruise 75 nm at 10,500 msl Pressure Alt | Fuel burn in decent to loiter, from 10,500 msl to 7,000 msl, Pressure Alt | Time to descend to loiter, from 10,500 msl to 7,000 msl, Pressure Alt | Distance in nm to descend to loiter, from 10,500 msl to 7,000 msl Pressure Alt | Total fuel burn to loiter for three hours at 7,000 MSL, at Pressure Alt | Aircraft loiter configuration | Vmca For loiter configuration (If Applicable) | VS1 at 30 deg AOB for loiter configuration | 1.3VS1 for loiter configuration | Fuel burn to climb from 7,000 MSL (working altitude) to 10,500 MSL PA | Time to climb from 7,000 MSL (working altitude) to 10,500 MSL PA | Distance in nm to climb from loiter at 7,000' msl at to 10,500 msl PA | Total fuel burn in LBS. to cruise 75 nm at 10,500 MSL PA2 | Mission aircraft cruise config calculated TAS | Time to cruise 75 nm at 10,500 MSL PA | Decent 2 and Approach fuel burn | Decent 2 and Approach time | Decent 2 and Approach distance in nm | Total Fuel remaining (in minutes) at landing under normal cruise configuration | Total fuel remaining at landing in LBS. |
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4a
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| Mission | Basic Aircraft Information | Basic Mission Weights | Mission Takeoff & Climb1 | Cruise 1 | Decent 1 | Loiter | Climb 2 | Cruise 2 | Decent 2, Approch, Landing | Fuel Remaining | |||||||||||||||||||||||||||||||
| 4a | Make | Model | Manufacturer Serial Number | FAA Registration Number | Aircraft Max Allowable Zero Fuel Weight (If Applicable to Aircraft) | Aircraft Max Ramp Weight | Aircraft Max Takeoff Gross Weight | Aircraft Max Landing Weight | Vyse 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 equipment | Aircraft weight with all mission equipment plus Crew & Baggage Identified in B-1 (a through i) for specific mission | Total allowable fuel with all mission equipment plus Crew & Baggage identified in B-1 (a through i) in LBS. for specific mission | Actual Aircraft Takeoff weight (Mission Equip, Crew, Bags, Mission Fuel) From Departure MSL elevation and ISA Temp | Start, Runup, and Taxi fuel burn in LBS. | Fuel burn in LBS. to 22,000 msl from 4500'MSL, at ISA +20 C | Time to climb to 22,000 msl from 4500'MSL, at ISA +20 C | Distance in nm to climb to 22,000 from 4500' MSL, at ISA +20C | Total fuel burn in LBS. to cruise 125 nm at 22,000 msl PA | Mission aircraft cruise configuration and calculated TAS | Time to cruise 125 nm at 22,000 msl Pressure Alt | Fuel burn in decent to loiter, from 22,000 msl to 14,500 msl, Pressure Alt | Time to descend to loiter, from 22,000 msl to 14,500 msl, Pressure Alt | Distance in nm to descend to loiter, from 22,000 msl to 14,500 msl Pressure Alt | Total fuel burn to loiter for three hours at 14,500 MSL, at Pressure Alt | Aircraft loiter configuration | Vmca For loiter configuration (If Applicable) | VS1 at 30 deg AOB for loiter configuration | 1.3VS1 for loiter configuration | Fuel burn to climb from 14,500 MSL (working altitude) to 22,000 MSL PA | Time to climb from 14,500 MSL (working altitude) to 22,000 MSL PA | Distance in nm to climb from loiter at 14,500' msl at to 22,000 msl PA | Total fuel burn in LBS. to cruise 125 nm at 22,000 MSL PA2 | Mission aircraft cruise config calculated TAS | Time to cruise 125 nm at 22,000 MSL PA | Decent 2 and Approach fuel burn | Decent 2 and Approach time | Decent 2 and Approach distance in nm | Total Fuel remaining (in minutes) at landing under normal cruise configuration | Total fuel remaining at landing in LBS. |
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4b
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| Mission | Basic Aircraft Information | Basic Mission Weights | Mission Takeoff & Climb1 | Cruise 1 | Decent 1 | Loiter | Climb 2 | Cruise 2 | Decent 2, Approch, Landing | Fuel Remaining | |||||||||||||||||||||||||||||||
| 4b | Make | Model | Manufacturer Serial Number | FAA Registration Number | Aircraft Max Allowable Zero Fuel Weight (If Applicable to Aircraft) | Aircraft Max Ramp Weight | Aircraft Max Takeoff Gross Weight | Aircraft Max Landing Weight | Vyse 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 equipment | Aircraft weight with all mission equipment plus Crew & Baggage Identified in B-1 (a through i) for specific mission | Total allowable fuel with all mission equipment plus Crew & Baggage identified in B-1 (a through i) in LBS. for specific mission | Actual Aircraft Takeoff weight (Mission Equip, Crew, Bags, Mission Fuel) From Departure MSL elevation and ISA Temp | Start, Runup, and Taxi fuel burn in LBS. | Fuel burn in LBS. to 22,000 msl from 4500'MSL, at ISA +20 C | Time to climb to 22,000 msl from 4500'MSL, at ISA +20 C | Distance in nm to climb to 22,000 from 4500' MSL, at ISA +20C | Total fuel burn in LBS. to cruise 125 nm at 22,000 msl PA | Mission aircraft cruise configuration and calculated TAS | Time to cruise 125 nm at 22,000 msl Pressure Alt | Fuel burn in decent to loiter, from 22,000 msl to 41,500 msl, Pressure Alt | Time to descend to loiter, from 22,000 msl to 14,500 msl, Pressure Alt | Distance in nm to descend to loiter, from 22,000 msl to 14,500 msl Pressure Alt | Total fuel burn to loiter for three hours at 14,500 MSL, at Pressure Alt | Aircraft loiter configuration | Vmca For loiter configuration (If Applicable) | VS1 at 30 deg AOB for loiter configuration | 1.3VS1 for loiter configuration | Fuel burn to climb from 14,500 MSL (working altitude) to 22,000 MSL PA | Time to climb from 14,500 MSL (working altitude) to 22,000 MSL PA | Distance in nm to climb from loiter at 14,500' msl at to 22,000 msl PA | Total fuel burn in LBS. to cruise 125 nm at 22,000 MSL PA3 | Mission aircraft cruise config calculated TAS | Time to cruise 125 nm at 22,000 MSL PA | Decent 2 and Approach fuel burn | Decent 2 and Approach time | Decent 2 and Approach distance in nm | Total Fuel remaining (in minutes) at landing under normal cruise configuration | Total fuel remaining at landing in LBS. |
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4c
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| Mission | Basic Aircraft Information | Basic Mission Weights | Mission Takeoff & Climb1 | Cruise 1 | Decent 1 | Loiter | Climb 2 | Cruise 2 | Decent 2, Approch, Landing | Fuel Remaining | |||||||||||||||||||||||||||||||
| 4c | Make | Model | Manufacturer Serial Number | FAA Registration Number | Aircraft Max Allowable Zero Fuel Weight (If Applicable to Aircraft) | Aircraft Max Ramp Weight | Aircraft Max Takeoff Gross Weight | Aircraft Max Landing Weight | Vyse 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 equipment | Aircraft weight with all mission equipment plus Crew & Baggage Identified in B-1 (a through i) for specific mission | Total allowable fuel with all mission equipment plus Crew & Baggage identified in B-1 (a through i) in LBS. for specific mission | Actual Aircraft Takeoff weight (Mission Equip, Crew, Bags, Mission Fuel) From Departure MSL elevation and ISA Temp | Start, Runup, and Taxi fuel burn in LBS. | Fuel burn in LBS. to 10,500 msl from Sea Level, Standard Day | Time to climb to 10,500 msl from Sea Level, Standard Day | Distance in nm to climb to 10,500 from Sea Level, Standard Day | Total fuel burn in LBS. to cruise 75 nm at 10,500 msl PA | Mission aircraft cruise configuration and calculated TAS | Time to cruise 75 nm at 10,500 msl Pressure Alt | Fuel burn in decent to loiter, from10,500 msl to 7,500 msl, Pressure Alt | Time to descend to loiter, from 10,500 msl to 7,500 msl, Pressure Alt | Distance in nm to descend to loiter, from10,500 msl to 7,500 msl Pressure Alt | Total fuel burn to loiter for three hours at 7,500 MSL, at Pressure Alt | Aircraft loiter configuration | Vmca For loiter configuration (If Applicable) | VS1 at 30 deg AOB for loiter configuration | 1.3VS1 for loiter configuration | Fuel burn to climb from 7,500 MSL (working altitude) to 10,500 MSL PA | Time to climb from 7,500 MSL (working altitude) to 10,500 MSL PA | Distance in nm to climb from loiter at 7,500' msl at to 10,500 msl PA | Total fuel burn in LBS. to cruise 150 nm at 10,500 MSL PA | Mission aircraft cruise config calculated TAS | Time to cruise 75 nm at 10,500 MSL PA | Decent 2 and Approach fuel burn | Decent 2 and Approach time | Decent 2 and Approach distance in nm | Total Fuel remaining (in minutes) at landing under normal cruise configuration | Total fuel remaining at landing in LBS. |
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5a
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| Mission | Basic Aircraft Information | Basic Mission Weights | Mission Takeoff & Climb1 | Cruise 1 | Descent 1 | Loiter | Climb 2 | Cruise 2 | Descent 2, Approch, Landing | Fuel Remaining | |||||||||||||||||||||||||||||||||||||
| 5a | Make | Model | Manufacturer Serial Number | FAA Registration Number | Landing 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 configured | Takeoff distance over 50 foot tall obstacle at Max Gross Weight Standard Day Sea level | Landing distance over 50 foot tall obstacle at Max Gross Weight Standard Day Sea level | Takeoff distance over 50 foot tall obstacle at Max Gross Weight 4,500 Ft PA ISA +20 | Landing distance over 50 foot tall obstacle at Max Gross Weight 4,500 Ft PA ISA +20 | Aircraft Max Allowable Zero Fuel Weight (If Applicable to Aircraft) | Aircraft Max Ramp Weight | Aircraft Max Takeoff Gross Weight | Aircraft Max Landing Weight | Vyse at Max Gross Takeoff gross weight (If Applicable) KIAS | Single Engine Service Ceiling (If Applicable) | Total aircraft usable fuel in LBS. | Aircraft Empty Weight with all installed contract required/mission required equipment | Aircraft weight with all mission equipment plus Crew & Baggage Identified in B-1 (a through i) for specific mission | Total allowable fuel with all mission equipment plus Crew & Baggage identified in B-1 (a through i) in LBS. for specific mission | Actual Aircraft Takeoff weight (Mission Equip, Crew, Bags, Mission Fuel) From Departure MSL elevation and ISA Temp | Start, Runup, and Taxi fuel burn in LBS. | Fuel burn in LBS. to 10,500 msl from 4500'MSL, at ISA +20 C | Time to climb to 10,500 msl from 4500'MSL, at ISA +20 C | Distance in nm to climb to 10,500 from 4500' MSL, at ISA +20C | Total fuel burn in LBS. to cruise 50 nm at 10,500 msl PA | Mission aircraft cruise configuration and calculated TAS | Time 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 Alt | Time to descend to loiter, from 10,500 msl to 7,000 msl, Pressure Alt | Distance in nm to descend to loiter, from 10,500 msl to 7,000 msl Pressure Alt | Total fuel burn to loiter for three hours at 7,000 MSL, at Pressure Alt | Aircraft loiter configuration | Vmca For loiter configuration (If Applicable) | VS1 at 30 deg AOB for loiter config (KIAS) | 1.3VS1 for loiter configuration | Fuel burn to climb from 7,000 MSL (working altitude) to 10,500 MSL PA | Time to climb from 7,000 MSL (working altitude) to 10,500 MSL PA | Distance in nm to climb from loiter at 7,000' msl at to 10,500 msl PA | Total fuel burn in LBS. to cruise 50 nm at 10,500 MSL PA2 | Mission aircraft cruise config calculated TAS | Time to cruise 50 nm at 10,500 MSL PA | Descent 2 and Approach fuel burn | Descent 2 and Approach time | Descent 2 and Approach distance in nm | Total Fuel remaining (in minutes) at landing under normal cruise configuration | Total fuel remaining at landing in LBS. |
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5b
| Offeror Company Name: | |||||||||||||||||||||||||||||||||||||||||||||||
| Mission | Basic Aircraft Information | Basic Mission Weights | Mission Takeoff & Climb1 | Cruise 1 | Descent 1 | Loiter | Climb 2 | Cruise 2 | Descent 2, Approch, Landing | Fuel Remaining | |||||||||||||||||||||||||||||||||||||
| 5b | Make | Model | Manufacturer Serial Number | FAA Registration Number | Landing 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 configured | Takeoff distance over 50 foot tall obstacle at Max Gross Weight Standard Day Sea level | Landing distance over 50 foot tall obstacle at Max Gross Weight Standard Day Sea level | Takeoff distance over 50 foot tall obstacle at Max Gross Weight 4,500 Ft PA ISA +20 | Landing distance over 50 foot tall obstacle at Max Gross Weight 4,500 Ft PA ISA +20 | Aircraft Max Allowable Zero Fuel Weight (If Applicable to Aircraft) | Aircraft Max Ramp Weight | Aircraft Max Takeoff Gross Weight | Aircraft Max Landing Weight | Vyse 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 equipment | Aircraft weight with all mission equipment plus Crew & Baggage Identified in B-1 (a through i) for specific mission | Total allowable fuel with all mission equipment plus Crew & Baggage identified in B-1 (a through i) in LBS. for specific mission | Actual Aircraft Takeoff weight (Mission Equip, Crew, Bags, Mission Fuel) From Departure MSL elevation and ISA Temp | Start, Runup, and Taxi fuel burn in LBS. | Fuel burn in LBS. to 10,500 msl from 4500'MSL, at ISA +20 C | Time to climb to 10,500 msl from 4500'MSL, at ISA +20 C | Distance in nm to climb to 10,500 from 4500' MSL, at ISA +20C | Total fuel burn in LBS. to cruise 50 nm at 10,500 msl PA | Mission aircraft cruise configuration and calculated TAS | Time 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 Alt | Time to descend to loiter, from 10,500 msl to 7,000 msl, Pressure Alt | Distance in nm to descend to loiter, from 10,500 msl to 7,000 msl Pressure Alt | Total fuel burn to loiter for three hours at 7,000 MSL, at Pressure Alt | Aircraft loiter configuration | Vmca For loiter configuration (If Applicable) | VS1 at 30 deg AOB for loiter configuration | 1.3VS1 for loiter configuration | Fuel burn to climb from 7,000 MSL (working altitude) to 10,500 MSL PA | Time to climb from 7,000 MSL (working altitude) to 10,500 MSL PA | Distance in nm to climb from loiter at 7,000' msl at to 10,500 msl PA | Total fuel burn in LBS. to cruise 50 nm at 10,500 MSL PA3 | Mission aircraft cruise config calculated TAS | Time to cruise 50 nm at 10,500 MSL PA | Descent 2 and Approach fuel burn | Descent 2 and Approach time | Descent 2 and Approach distance in nm | Total Fuel remaining (in minutes) at landing under normal cruise configuration | Total fuel remaining at landing in LBS. |
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6a
| Offeror Company Name: | |||||||||||||||||||||||||||||||||||||||||||||||
| Mission | Basic Aircraft Information | Basic Mission Weights | Mission Takeoff & Climb1 | Cruise 1 | Descent 1 | Loiter | Climb 2 | Cruise 2 | Descent 2, Approch, Landing | Fuel Remaining | |||||||||||||||||||||||||||||||||||||
| 6a | Make | Model | Manufacturer Serial Number | FAA Registration Number | Landing 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 configured | Takeoff distance over 50 foot tall obstacle at Max Gross Weight Standard Day Sea level | Landing distance over 50 foot tall obstacle at Max Gross Weight Standard Day Sea level | Takeoff distance over 50 foot tall obstacle at Max Gross Weight 4,500 Ft PA ISA +20 | Landing distance over 50 foot tall obstacle at Max Gross Weight 4,500 Ft PA ISA +20 | Aircraft Max Allowable Zero Fuel Weight (If Applicable to Aircraft) | Aircraft Max Ramp Weight | Aircraft Max Takeoff Gross Weight | Aircraft Max Landing Weight | Vyse 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 equipment | Aircraft weight with all mission equipment plus Crew & Baggage Identified in B-1 (a through i) for specific mission | Total allowable fuel with all mission equipment plus Crew & Baggage identified in B-1 (a through i) in LBS. for specific mission | Actual Aircraft Takeoff weight (Mission Equip, Crew, Bags, Mission Fuel) From Departure MSL elevation and ISA Temp | Start, Runup, and Taxi fuel burn in LBS. | Fuel burn in LBS. to 10,500 msl from 4500'MSL, at ISA +20 C | Time to climb to 10,500 msl from 4500'MSL, at ISA +20 C | Distance in nm to climb to 10,500 from 4500' MSL, at ISA +20C | Total fuel burn in LBS. to cruise 75 nm at 10,500 msl PA | Mission aircraft cruise configuration and calculated TAS | Time to cruise 75 nm at 10,500 msl Pressure Alt | Fuel burn in Descent to loiter, from 10,500 msl to 7,000 msl, Pressure Alt | Time to descend to loiter, from 10,500 msl to 7,000 msl, Pressure Alt | Distance in nm to descend to loiter, from 10,500 msl to 7,000 msl Pressure Alt | Total fuel burn to loiter for three hours at 7,000 MSL, at Pressure Alt | Aircraft loiter configuration | Vmca For loiter configuration (If Applicable) | VS1 at 30 deg AOB for loiter configuration | 1.3VS1 for loiter configuration | Fuel burn to climb from 7,000 MSL (working altitude) to 10,500 MSL PA | Time to climb from 7,000 MSL (working altitude) to 10,500 MSL PA | Distance in nm to climb from loiter at 7,000' msl at to 10,500 msl PA | Total fuel burn in LBS. to cruise 75 nm at 10,500 MSL PA2 | Mission aircraft cruise config calculated TAS | Time to cruise 75 nm at 10,500 MSL PA | Descent 2 and Approach fuel burn | Descent 2 and Approach time | Descent 2 and Approach distance in nm | Total Fuel remaining (in minutes) at landing under normal cruise configuration | Total fuel remaining at landing in LBS. |
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6b
| Offeror Company Name: | |||||||||||||||||||||||||||||||||||||||||||||||
| Mission | Basic Aircraft Information | Basic Mission Weights | Mission Takeoff & Climb1 | Cruise 1 | Descent 1 | Loiter | Climb 2 | Cruise 2 | Descent 2, Approch, Landing | Fuel Remaining | |||||||||||||||||||||||||||||||||||||
| 6b | Make | Model | Manufacturer Serial Number | FAA Registration Number | Landing 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 configured | Takeoff distance over 50 foot tall obstacle at Max Gross Weight Standard Day Sea level | Landing distance over 50 foot tall obstacle at Max Gross Weight Standard Day Sea level | Takeoff distance over 50 foot tall obstacle at Max Gross Weight 4,500 Ft PA ISA | Landing distance over 50 foot tall obstacle at Max Gross Weight 4,500 Ft PA ISA | Aircraft Max Allowable Zero Fuel Weight (If Applicable to Aircraft) | Aircraft Max Ramp Weight | Aircraft Max Takeoff Gross Weight | Aircraft Max Landing Weight | Vyse 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 equipment | Aircraft weight with all mission equipment plus Crew & Baggage Identified in B-1 (a through i) for specific mission | Total allowable fuel with all mission equipment plus Crew & Baggage identified in B-1 (a through i) in LBS. for specific mission | Actual Aircraft Takeoff weight (Mission Equip, Crew, Bags, Mission Fuel) From Departure MSL elevation and ISA Temp | Start, Runup, and Taxi fuel burn in LBS. | Fuel burn in LBS. to 5,500 msl from Sea Level, at ISA +20 C | Time to climb to 5,500 msl from Sea Level at ISA +20 C | Distance in nm to climb to 5,500 from Sea Level, at ISA +20C | Total fuel burn in LBS. to cruise 50 nm at 5,500 msl PA | Mission aircraft cruise configuration and calculated TAS | Time to cruise 50 nm at 5,500 msl Pressure Alt | Fuel burn in Descent to loiter, from 5,500 msl to 3,000 msl, Pressure Alt | Time to descend to loiter, from 5,500 msl to 3,00msl, Pressure Alt | Distance in nm to descend to loiter, from 5,500 msl to 3,000 msl Pressure Alt | Total fuel burn to loiter for three hours at 3,000 MSL, at Pressure Alt | Aircraft loiter configuration | Vmca For loiter configuration (If Applicable) | VS1 at 30 deg AOB for loiter configuration | 1.3VS1 for loiter configuration | Fuel burn to climb from 3,000 MSL (working altitude) to 5,500 MSL PA | Time to climb from 3,000 MSL (working altitude) to 5,500 MSL PA | Distance in nm to climb from loiter at 3,000' msl at to 5,500 msl PA | Total fuel burn in LBS. to cruise 50 nm at 5,500 MSL PA2 | Mission aircraft cruise config calculated TAS | Time to cruise 50 nm at 5,500 MSL PA | Descent 2 and Approach fuel burn | Descent 2 and Approach time | Descent 2 and Approach distance in nm | Total Fuel remaining (in minutes) at landing under normal cruise configuration | Total fuel remaining at landing in LBS. |
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| Mission | Basic Aircraft Information | Basic Mission Weights | Mission Takeoff & Climb1 | Cruise 1 | Descent 1 | Loiter | Climb 2 | Cruise 2 | Descent 2, Approch, Landing | Fuel Remaining | |||||||||||||||||||||||||||||||||||||
| 7 | Make | Model | Manufacturer Serial Number | FAA Registration Number | Landing 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 configured | Takeoff distance over 50 foot tall obstacle at Max Gross Weight Standard Day Sea level | Landing distance over 50 foot tall obstacle at Max Gross Weight Standard Day Sea level | Takeoff distance over 50 foot tall obstacle at Max Gross Weight 4,500 Ft PA ISA | Landing distance over 50 foot tall obstacle at Max Gross Weight 4,500 Ft PA ISA | Aircraft Max Allowable Zero Fuel Weight (If Applicable to Aircraft) | Aircraft Max Ramp Weight | Aircraft Max Takeoff Gross Weight | Aircraft Max Landing Weight | Vyse 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 equipment | Aircraft weight with all mission equipment plus Crew & Baggage Identified in B-1 (a through i) for specific mission | Total allowable fuel with all mission equipment plus Crew & Baggage identified in B-1 (a through i) in LBS. for specific mission | Actual Aircraft Takeoff weight (Mission Equip, Crew, Bags, Mission Fuel) From Departure MSL elevation and ISA Temp | Start, Runup, and Taxi fuel burn in LBS. | Fuel burn in LBS. to 5,500 msl from Sea Level, Standard Day | Time to climb to 5,500 msl from Sea Level at Standard Day | Distance in nm to climb to 5,500 from Sea Level, Standard Day | Total fuel burn in LBS. to cruise 50 nm at 5,500 msl PA | Mission aircraft cruise configuration and calculated TAS | Time to cruise 50 nm at 5,500 msl Pressure Alt | Fuel burn in Descent to loiter, from 5,500 msl to 3,000 msl, Pressure Alt | Time to descend to loiter, from 5,500 msl to 3,00msl, Pressure Alt | Distance in nm to descend to loiter, from 5,500 msl to 3,000 msl Pressure Alt | Total fuel burn to loiter for three hours at 3,000 MSL, at Pressure Alt | Aircraft loiter configuration | Vmca For loiter configuration (If Applicable) | VS1 at 30 deg AOB for loiter configuration | 1.3VS1 for loiter configuration | Fuel burn to climb from 3,000 MSL (working altitude) to 5,500 MSL PA | Time to climb from 3,000 MSL (working altitude) to 5,500 MSL PA | Distance in nm to climb from loiter at 3,000' msl at to 5,500 msl PA | Total fuel burn in LBS. to cruise 50 nm at 5,500 MSL PA2 | Mission aircraft cruise config calculated TAS | Time to cruise 50 nm at 5,500 MSL PA | Descent 2 and Approach fuel burn | Descent 2 and Approach time | Descent 2 and Approach distance in nm | Total Fuel remaining (in minutes) at landing under normal cruise configuration | Total fuel remaining at landing in LBS. |
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File details come from the government source that posted it. Updated .