Schedule of Items_Aircraft Performance Sheet.xlsx
XLSX spreadsheet 45 KB Posted
- Attached to
- National Light Fixed Wing Services MATOC Federal contract opportunity
- Solicitation number
- 1202SA22R9102
- Issued by
- Department of Agriculture Forest Service
About this file
This document contains a draft statement of work for a multiple award task order contract to obtain fixed-wing aircraft and qualified personnel for administration and protection of public lands. Services required include daily coverage for special use missions supporting fire, project, resource, law enforcement, and point-to-point administrative flights. Aircraft may support interagency and cooperative agreements for use by federal and state agencies and private landholders. The Department of Agriculture Forest Service is the contracting agency. Responses are due by September 30th and an industry day will be held on October 25th in Boise, Idaho. Contractors must agree in writing to perform law enforcement flights if requested and relief personnel may be necessary for 7-day weekly coverage during the period of performance.
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Text version
Schedule of Items
| Vendor: | ||
| Aircraft Registration-Number: | N | Aircraft Model: |
| Manufactured Year: | Aircraft Make: | |
| Empty Weight: | Certified Max Gross Weight: | |
| Number of Seats: | Pressurized? | |
| Hourly Fuel Consumption Rate: | Air Conditioning: |
| CLIN | Year | Daily Availability | Flight Rate Wet | Flight Rate Dry | Additional pilot |
| Base | 2023 | ||||
| 1 | 2024 | ||||
| 2 | 2025 | ||||
| 3 | 2026 | ||||
| 4 | 2027 |
| Mission Code (B-1) | |
| 1 | National Air Tactical - Incident Awareness and Assessment (NAT-IAA) |
| 2 a | Medium Altitude - Sensor Enhanced ATGS |
| 2 b | Low Altitude - Sensor Enhanced ATGS |
| 3 a | High Performance - ATGS |
| 3 b | Standard - ATGS |
| 4 a | Sensor Enhanced - Fire Mapping |
| 4 b | Sensor Enhanced - Fire Detection |
| 4 c | Sensor Enhanced - Resource Reconnaissance |
| 5 a | Standard - Fire Detection |
| 5 b | Standard - Resource Reconnaissance |
| 5 c | Back Country Operations |
| 6 | Point-to-Point Cargo and Passengers |
| Check the box to indicate aircraft mission codes you are bidding on |
| Additional Offered Equipment (A-2) | ||
| Description | Qty/Unit (Day, Hour, Etc.) | Unit Price |
Mission 1
| Mission 1 - National Air Tactical - Incident Awareness and Assessment | ||||||||||||||||||||||||||||||
| YOU MUST PROVIDE A LEDGIBLE COPY OF AN AFM ANNOTATED PERFORMANCE CHART TO VERIFY ALL REPORTED NUMBERS. THIS INCLUDES A FULL WEIGHT AND BALANCE WORKSHEET AS WELL AS CG ENVELOPE DIAGRAM SHOWING ALL CONDITIONS OF FLIGHT. | ||||||||||||||||||||||||||||||
| Make | Model | FAA Registration and Serial Number of Aircraft Offered | Aircraft Max Ramp Weight | Start, Runup, and Taxi fuel burn in LBS. | Aircraft Max Takeoff Gross Weight | Aircraft Max Landing Weight | Aircraft Max Allowable Zero Fuel Weight | Aircraft Weight with all installed mission equipment | Aircraft weight with all mission equipment and max payload crew configuration | Total aircraft usable fuel in LBS. | Total allowable fuel with all mission equipment and MAX mission pay load in LBS. | Fuel burn in LBS. to 22,000 msl from sea level | Time to climb to 22,000 msl from sea level | Total fuel burn in LBS. to cruise 150 nm at 22,000 msl at ISA +20 C | Mission aircraft cruise configuration and calculated TAS | Time to cruise 150 nm at 22,000 msl at ISA +20 C | Total fuel burn to loiter for three hours at 14,500 MSL | Aircraft loiter configuration | Vmca For loiter configuration | VS1 at 30 deg AOB for loiter configuration | 1.3VS1 for loiter configuration | Vyse at Max Gross Takeoff gross weight | Fuel burn to climb from 14,500 MSL (working altitude) to 22,000 MSL (Cruise) | Time to climb from 14,500 MSL (working altitude) to 22,000 MSL (Cruise) | Total fuel burn in LBS. to cruise 150 nm at 22,000 MSL at ISA +20 C | Column AA aircraft configuration and calculated TAS | Time to cruise 150 nm at 22,000 MSL at ISA +20 C | Approach fuel burn | Total Fuel remaining (in minutes) at landing under normal cruise configuration at 22,000 MSL ISA +20 | Total fuel remaining at landing in LBS. |
| Example | Example | N12345 / SN 12345 | 12590 | 90 | 12500 | 12500 | 11000 | 8337 | 9072 | 3562 | 3250 | 400 | 1OMIN | 400 | CLEAN 270ktas | 35 MINS | 1800 | flaps approach, props 1800 rpm @ 121 kias | 89 | 91 | 119 | 121 | 200 | 5 MIN | 350 | Clean 270 Kts | 35 mins | 200 LBS. | 30 Min | 315 |
Mission 2 A
| Mission 2 A - Medium Altitude Sensor Enhanced ATGS | ||||||||||||||||||||||||||||||
| YOU MUST PROVIDE A LEDGIBLE COPY OF AN AFM ANNOTATED PERFORMANCE CHART TO VERIFY ALL REPORTED NUMBERS. THIS INCLUDES A FULL WEIGHT AND BALANCE WORKSHEET AS WELL AS CG ENVELOPE DIAGRAM SHOWING ALL CONDITIONS OF FLIGHT. | ||||||||||||||||||||||||||||||
| Make | Model | FAA Registration and Serial Number of Aircraft Offered | Aircraft Max Ramp Weight | Start, Runup, and Taxi fuel burn in LBS. | Aircraft Max Takeoff Gross Weight | Aircraft Max Landing Weight | Aircraft Max Allowable Zero Fuel Weight | Aircraft Weight with all installed mission equipment | Aircraft weight with all mission equipment and max payload crew configuration | Total aircraft usable fuel in LBS. | Total allowable fuel with all mission equipment and MAX mission pay load in LBS. | Fuel burn in LBS. to 22,000 msl from sea level | Time to climb to 22,000 msl from sea level | Total fuel burn in LBS. to cruise 150 nm at 22,000 msl at ISA +20 C | Mission aircraft cruise configuration and calculated TAS | Time to cruise 150 nm at 22,000 msl at ISA +20 C | Total fuel burn to loiter for three hours at 10,000 MSL | Vmca For loiter configuration (if applicable) | VS1 at 30 deg AOB for loiter configuration | 1.3VS1 for loiter configuration | Vyse at Max Gross Takeoff gross weight (if applicable) | Vyse at Max Gross Takeoff gross weight | Fuel burn to climb from 10,000 MSL (working altitude) to 22,000 MSL (Cruise) | Time to climb from 10,000 MSL (working altitude) to 22,000 MSL (Cruise) | Total fuel burn in LBS. to cruise 150 nm at 22,000 MSL at ISA +20 C | Column AA aircraft configuration and calculated TAS | Time to cruise 150 nm at 22,000 MSL at ISA +20 C | Approach fuel burn | Total Fuel remaining (in minutes) at landing under normal cruise configuration at 22,000 MSL ISA +20 | Total fuel remaining at landing in LBS. |
| Example | Example | N12345 / SN 12345 | 12590 | 90 | 12500 | 12500 | 11000 | 8337 | 9072 | 3562 | 3250 | 400 | 1OMIN | 400 | CLEAN 270ktas | 35 MINS | 1800 | flaps approach, props 1800 rpm @ 121 kias | 89 | 91 | 119 | 121 | 200 | 5 MIN | 350 | Clean 270 Kts | 35 mins | 200 LBS. | 30 Min | 315 |
Mission 2 B
| Mission 2 B - Low Altitude Sensor Enhanced ATGS | ||||||||||||||||||||||||||||||
| YOU MUST PROVIDE A LEDGIBLE COPY OF AN AFM ANNOTATED PERFORMANCE CHART TO VERIFY ALL REPORTED NUMBERS. THIS INCLUDES A FULL WEIGHT AND BALANCE WORKSHEET AS WELL AS CG ENVELOPE DIAGRAM SHOWING ALL CONDITIONS OF FLIGHT. | ||||||||||||||||||||||||||||||
| Make | Model | FAA Registration and Serial Number of Aircraft Offered | Aircraft Max Ramp Weight | Start, Runup, and Taxi fuel burn in LBS. | Aircraft Max Takeoff Gross Weight | Aircraft Max Landing Weight | Aircraft Max Allowable Zero Fuel Weight | Aircraft Weight with all installed mission equipment | Aircraft weight with all mission equipment and max payload crew configuration | Total aircraft usable fuel in LBS. | Total allowable fuel with all mission equipment and MAX mission pay load in LBS. | Fuel burn in LBS. to 22,000 msl from sea level | Time to climb to 22,000 msl from sea level | Total fuel burn in LBS. to cruise 150 nm at 22,000 msl at ISA +20 C | Mission aircraft cruise configuration and calculated TAS | Time to cruise 150 nm at 22,000 msl at ISA +20 C | Total fuel burn to loiter for three hours at 7,000 MSL | Aircraft loiter configuration | Vmca For loiter configuration (if applicable) | VS1 at 30 deg AOB for loiter configuration | 1.3VS1 for loiter configuration | Vyse at Max Gross Takeoff gross weight (if applicable) | Fuel burn to climb from 7,000 MSL (working altitude) to 22,000 MSL (Cruise) | Time to climb from 7,000 MSL (working altitude) to 22,000 MSL (Cruise) | Total fuel burn in LBS. to cruise 150 nm at 22,000 MSL at ISA +20 C | Column AA aircraft configuration and calculated TAS | Time to cruise 150 nm at 22,000 MSL at ISA +20 C | Approach fuel burn | Total Fuel remaining (in minutes) at landing under normal cruise configuration at 22,000 MSL ISA +20 | Total fuel remaining at landing in LBS. |
| Example | Example | N12345 / SN 12345 | 12590 | 90 | 12500 | 12500 | 11000 | 8337 | 9072 | 3562 | 3250 | 400 | 1OMIN | 400 | CLEAN 270ktas | 35 MINS | 1800 | flaps approach, props 1800 rpm @ 121 kias | 89 | 91 | 119 | 121 | 200 | 5 MIN | 350 | Clean 270 Kts | 35 mins | 200 LBS. | 30 Min | 315 |
Mission 3 A
| Mission 3 A - High Performance - ATGS | ||||||||||||||||||||||||||||||
| YOU MUST PROVIDE A LEDGIBLE COPY OF AN AFM ANNOTATED PERFORMANCE CHART TO VERIFY ALL REPORTED NUMBERS. THIS INCLUDES A FULL WEIGHT AND BALANCE WORKSHEET AS WELL AS CG ENVELOPE DIAGRAM SHOWING ALL CONDITIONS OF FLIGHT. | ||||||||||||||||||||||||||||||
| Make | Model | FAA Registration and Serial Number of Aircraft Offered | Aircraft Max Ramp Weight | Start, Runup, and Taxi fuel burn in LBS. | Aircraft Max Takeoff Gross Weight | Aircraft Max Landing Weight | Aircraft Max Allowable Zero Fuel Weight | Aircraft Weight with all installed mission equipment | Aircraft weight with all mission equipment and max payload crew configuration | Total aircraft usable fuel in LBS. | Total allowable fuel with all mission equipment and MAX mission pay load in LBS. | Fuel burn in LBS. to 22,000 msl from sea level | Time to climb to 22,000 msl from sea level | Total fuel burn in LBS. to cruise 150 nm at 22,000 msl at ISA +20 C | Mission aircraft cruise configuration and calculated TAS | Time to cruise 150 nm at 22,000 msl at ISA +20 C | Total fuel burn to loiter for three hours at 7,000 MSL | Aircraft loiter configuration | Vmca For loiter configuration (if applicable) | VS1 at 30 deg AOB for loiter configuration | 1.3VS1 for loiter configuration | Vyse at Max Gross Takeoff gross weight (if applicable) | Fuel burn to climb from 7,000 MSL (working altitude) to 22,000 MSL (Cruise) | Time to climb from 7,000 MSL (working altitude) to 22,000 MSL (Cruise) | Total fuel burn in LBS. to cruise 150 nm at 22,000 MSL at ISA +20 C | Column AA aircraft configuration and calculated TAS | Time to cruise 150 nm at 22,000 MSL at ISA +20 C | Approach fuel burn | Total Fuel remaining (in minutes) at landing under normal cruise configuration at 22,000 MSL ISA +20 | Total fuel remaining at landing in LBS. |
| Example | Example | N12345 / SN 12345 | 12590 | 90 | 12500 | 12500 | 11000 | 8337 | 9072 | 3562 | 3250 | 400 | 1OMIN | 400 | CLEAN 270ktas | 35 MINS | 1800 | flaps approach, props 1800 rpm @ 121 kias | 89 | 91 | 119 | 121 | 200 | 5 MIN | 350 | Clean 270 Kts | 35 mins | 200 LBS. | 30 Min | 315 |
Mission 3 B
| Mission 3 B - Standard - ATGS | ||||||||||||||||||||||||||||||
| YOU MUST PROVIDE A LEDGIBLE COPY OF AN AFM ANNOTATED PERFORMANCE CHART TO VERIFY ALL REPORTED NUMBERS. THIS INCLUDES A FULL WEIGHT AND BALANCE WORKSHEET AS WELL AS CG ENVELOPE DIAGRAM SHOWING ALL CONDITIONS OF FLIGHT. | ||||||||||||||||||||||||||||||
| Make | Model | FAA Registration and Serial Number of Aircraft Offered | Aircraft Max Ramp Weight | Start, Runup, and Taxi fuel burn in LBS. | Aircraft Max Takeoff Gross Weight | Aircraft Max Landing Weight | Aircraft Max Allowable Zero Fuel Weight | Aircraft Weight with all installed mission equipment | Aircraft weight with all mission equipment and max payload crew configuration | Total aircraft usable fuel in LBS. | Total allowable fuel with all mission equipment and MAX mission pay load in LBS. | Fuel burn in LBS. to 10,500 msl from sea level | Time to climb to 10,500 msl from sea level | Total fuel burn in LBS. to cruise 150 nm at 10,500 msl at ISA +20 C | Mission aircraft cruise configuration and calculated TAS | Time to cruise 150 nm at 10,500 msl at ISA +20 C | Total fuel burn to loiter for three hours at 7,000 MSL | Aircraft loiter configuration | Vmca For loiter configuration (if applicable) | VS1 at 30 deg AOB for loiter configuration | 1.3VS1 for loiter configuration | Vyse at Max Gross Takeoff gross weight (if applicable) | Fuel burn to climb from 7,000 MSL (working altitude) to 10,500 MSL (Cruise) | Time to climb from 7,000 MSL (working altitude) to 10,500 MSL (Cruise) | Total fuel burn in LBS. to cruise 150 nm at 10,500 MSL at ISA +20 C | Column AA aircraft configuration and calculated TAS | Time to cruise 150 nm at 10,500 MSL at ISA +20 C | Approach fuel burn | Total Fuel remaining (in minutes) at landing under normal cruise configuration at 10,500 MSL ISA +20 | Total fuel remaining at landing in LBS. |
| Example | Example | N12345 / SN 12345 | 12590 | 90 | 12500 | 12500 | 11000 | 8337 | 9072 | 3562 | 3250 | 400 | 1OMIN | 400 | CLEAN 270ktas | 35 MINS | 1800 | flaps approach, props 1800 rpm @ 121 kias | 89 | 91 | 119 | 121 | 200 | 5 MIN | 350 | Clean 270 Kts | 35 mins | 200 LBS. | 30 Min | 315 |
Mission 4 A
| Mission 4 A - Sensor Enhanced - Fire Mapping | ||||||||||||||||||||||||||||||
| YOU MUST PROVIDE A LEDGIBLE COPY OF AN AFM ANNOTATED PERFORMANCE CHART TO VERIFY ALL REPORTED NUMBERS. THIS INCLUDES A FULL WEIGHT AND BALANCE WORKSHEET AS WELL AS CG ENVELOPE DIAGRAM SHOWING ALL CONDITIONS OF FLIGHT. | ||||||||||||||||||||||||||||||
| Make | Model | FAA Registration and Serial Number of Aircraft Offered | Aircraft Max Ramp Weight | Start, Runup, and Taxi fuel burn in LBS. | Aircraft Max Takeoff Gross Weight | Aircraft Max Landing Weight | Aircraft Max Allowable Zero Fuel Weight | Aircraft Weight with all installed mission equipment | Aircraft weight with all mission equipment and max payload crew configuration | Total aircraft usable fuel in LBS. | Total allowable fuel with all mission equipment and MAX mission pay load in LBS. | Fuel burn in LBS. to 22,000 msl from sea level | Time to climb to 22,000 msl from sea level | Total fuel burn in LBS. to cruise 150 nm at 22,000 msl at ISA +20 C | Mission aircraft cruise configuration and calculated TAS | Time to cruise 150 nm at 22,000 msl at ISA +20 C | Total fuel burn to loiter for three hours at 14,500 MSL | Aircraft loiter configuration | Vmca For loiter configuration (if applicable) | VS1 at 30 deg AOB for loiter configuration | 1.3VS1 for loiter configuration | Vyse at Max Gross Takeoff gross weight (if applicable) | Fuel burn to climb from 14,500 MSL (working altitude) to 22,000 MSL (Cruise) | Time to climb from 14,500 MSL (working altitude) to 22,000 MSL (Cruise) | Total fuel burn in LBS. to cruise 150 nm at 22,000 MSL at ISA +20 C | Column AA aircraft configuration and calculated TAS | Time to cruise 150 nm at 22,000 MSL at ISA +20 C | Approach fuel burn | Total Fuel remaining (in minutes) at landing under normal cruise configuration at 22,000 MSL ISA +20 | Total fuel remaining at landing in LBS. |
| Example | Example | N12345 / SN 12345 | 12590 | 90 | 12500 | 12500 | 11000 | 8337 | 9072 | 3562 | 3250 | 400 | 1OMIN | 400 | CLEAN 270ktas | 35 MINS | 1800 | flaps approach, props 1800 rpm @ 121 kias | 89 | 91 | 119 | 121 | 200 | 5 MIN | 350 | Clean 270 Kts | 35 mins | 200 LBS. | 30 Min | 315 |
Mission 4 B
| Mission 4 A - Sensor Enhanced - Fire Mapping | ||||||||||||||||||||||||||||||
| YOU MUST PROVIDE A LEDGIBLE COPY OF AN AFM ANNOTATED PERFORMANCE CHART TO VERIFY ALL REPORTED NUMBERS. THIS INCLUDES A FULL WEIGHT AND BALANCE WORKSHEET AS WELL AS CG ENVELOPE DIAGRAM SHOWING ALL CONDITIONS OF FLIGHT. | ||||||||||||||||||||||||||||||
| Make | Model | FAA Registration and Serial Number of Aircraft Offered | Aircraft Max Ramp Weight | Start, Runup, and Taxi fuel burn in LBS. | Aircraft Max Takeoff Gross Weight | Aircraft Max Landing Weight | Aircraft Max Allowable Zero Fuel Weight | Aircraft Weight with all installed mission equipment | Aircraft weight with all mission equipment and max payload crew configuration | Total aircraft usable fuel in LBS. | Total allowable fuel with all mission equipment and MAX mission pay load in LBS. | Fuel burn in LBS. to 22,000 msl from sea level | Time to climb to 22,000 msl from sea level | Total fuel burn in LBS. to cruise 150 nm at 22,000 msl at ISA +20 C | Mission aircraft cruise configuration and calculated TAS | Time to cruise 150 nm at 22,000 msl at ISA +20 C | Total fuel burn to loiter for three hours at 14,500 MSL | Aircraft loiter configuration | Vmca For loiter configuration (if applicable) | VS1 at 30 deg AOB for loiter configuration | 1.3VS1 for loiter configuration | Vyse at Max Gross Takeoff gross weight (if applicable) | Fuel burn to climb from 14,500 MSL (working altitude) to 22,000 MSL (Cruise) | Time to climb from 14,500 MSL (working altitude) to 22,000 MSL (Cruise) | Total fuel burn in LBS. to cruise 150 nm at 22,000 MSL at ISA +20 C | Column AA aircraft configuration and calculated TAS | Time to cruise 150 nm at 22,000 MSL at ISA +20 C | Approach fuel burn | Total Fuel remaining (in minutes) at landing under normal cruise configuration at 22,000 MSL ISA +20 | Total fuel remaining at landing in LBS. |
| Example | Example | N12345 / SN 12345 | 12590 | 90 | 12500 | 12500 | 11000 | 8337 | 9072 | 3562 | 3250 | 400 | 1OMIN | 400 | CLEAN 270ktas | 35 MINS | 1800 | flaps approach, props 1800 rpm @ 121 kias | 89 | 91 | 119 | 121 | 200 | 5 MIN | 350 | Clean 270 Kts | 35 mins | 200 LBS. | 30 Min | 315 |
Mission 4 C
| Mission 4 C - Sensor Enhanced - Resource Reconnaissance | ||||||||||||||||||||||||||||||
| YOU MUST PROVIDE A LEDGIBLE COPY OF AN AFM ANNOTATED PERFORMANCE CHART TO VERIFY ALL REPORTED NUMBERS. THIS INCLUDES A FULL WEIGHT AND BALANCE WORKSHEET AS WELL AS CG ENVELOPE DIAGRAM SHOWING ALL CONDITIONS OF FLIGHT. | ||||||||||||||||||||||||||||||
| Make | Model | FAA Registration and Serial Number of Aircraft Offered | Aircraft Max Ramp Weight | Start, Runup, and Taxi fuel burn in LBS. | Aircraft Max Takeoff Gross Weight | Aircraft Max Landing Weight | Aircraft Max Allowable Zero Fuel Weight | Aircraft Weight with all installed mission equipment | Aircraft weight with all mission equipment and max payload crew configuration | Total aircraft usable fuel in LBS. | Total allowable fuel with all mission equipment and MAX mission pay load in LBS. | Fuel burn in LBS. to 22,000 msl from sea level | Time to climb to 22,000 msl from sea level | Total fuel burn in LBS. to cruise 150 nm at 22,000 msl at ISA +20 C | Mission aircraft cruise configuration and calculated TAS | Time to cruise 150 nm at 22,000 msl at ISA +20 C | Total fuel burn to loiter for three hours at 14,500 MSL | Aircraft loiter configuration | Vmca For loiter configuration (if applicable) | VS1 at 30 deg AOB for loiter configuration | 1.3VS1 for loiter configuration | Vyse at Max Gross Takeoff gross weight (if applicable) | Fuel burn to climb from 14,500 MSL (working altitude) to 22,000 MSL (Cruise) | Time to climb from 14,500 MSL (working altitude) to 22,000 MSL (Cruise) | Total fuel burn in LBS. to cruise 150 nm at 22,000 MSL at ISA +20 C | Column AA aircraft configuration and calculated TAS | Time to cruise 150 nm at 22,000 MSL at ISA +20 C | Approach fuel burn | Total Fuel remaining (in minutes) at landing under normal cruise configuration at 22,000 MSL ISA +20 | Total fuel remaining at landing in LBS. |
| Example | Example | N12345 / SN 12345 | 12590 | 90 | 12500 | 12500 | 11000 | 8337 | 9072 | 3562 | 3250 | 400 | 1OMIN | 400 | CLEAN 270ktas | 35 MINS | 1800 | flaps approach, props 1800 rpm @ 121 kias | 89 | 91 | 119 | 121 | 200 | 5 MIN | 350 | Clean 270 Kts | 35 mins | 200 LBS. | 30 Min | 315 |
Mission 5 A
| Mission 5 A - Standard - Fire Detection | ||||||||||||||||||||||||||||||
| YOU MUST PROVIDE A LEDGIBLE COPY OF AN AFM ANNOTATED PERFORMANCE CHART TO VERIFY ALL REPORTED NUMBERS. THIS INCLUDES A FULL WEIGHT AND BALANCE WORKSHEET AS WELL AS CG ENVELOPE DIAGRAM SHOWING ALL CONDITIONS OF FLIGHT. | ||||||||||||||||||||||||||||||
| Make | Model | FAA Registration and Serial Number of Aircraft Offered | Aircraft Max Ramp Weight | Start, Runup, and Taxi fuel burn in LBS. | Aircraft Max Takeoff Gross Weight | Aircraft Max Landing Weight | Aircraft Max Allowable Zero Fuel Weight | Aircraft Weight with all installed mission equipment | Aircraft weight with all mission equipment and max payload crew configuration | Total aircraft usable fuel in LBS. | Total allowable fuel with all mission equipment and MAX mission pay load in LBS. | Fuel burn in LBS. to 10,500 msl from sea level | Time to climb to 10,500 msl from sea level | Total fuel burn in LBS. to cruise 150 nm at 10,500 msl at ISA +20 C | Mission aircraft cruise configuration and calculated TAS | Time to cruise 150 nm at 10,500 msl at ISA +20 C | Total fuel burn to loiter for three hours at 7,000 MSL | Aircraft loiter configuration | Vmca For loiter configuration (if applicable) | VS1 at 30 deg AOB for loiter configuration | 1.3VS1 for loiter configuration | Vyse at Max Gross Takeoff gross weight (if applicable) | Fuel burn to climb from 7,000 MSL (working altitude) to 10,500 MSL (Cruise) | Time to climb from 7,000 MSL (working altitude) to 10,500 MSL (Cruise) | Total fuel burn in LBS. to cruise 150 nm at 10,500 MSL at ISA +20 C | Column AA aircraft configuration and calculated TAS | Time to cruise 150 nm at 10,500 MSL at ISA +20 C | Approach fuel burn | Total Fuel remaining (in minutes) at landing under normal cruise configuration at 10,500 MSL ISA +20 | Total fuel remaining at landing in LBS. |
| Example | Example | N12345 / SN 12345 | 12590 | 90 | 12500 | 12500 | 11000 | 8337 | 9072 | 3562 | 3250 | 400 | 1OMIN | 400 | CLEAN 270ktas | 35 MINS | 1800 | flaps approach, props 1800 rpm @ 121 kias | 89 | 91 | 119 | 121 | 200 | 5 MIN | 350 | Clean 270 Kts | 35 mins | 200 LBS. | 30 Min | 315 |
Mission 5 B
| Mission 5 A - Standard - Resource Reconnaissance | ||||||||||||||||||||||||||||||
| YOU MUST PROVIDE A LEDGIBLE COPY OF AN AFM ANNOTATED PERFORMANCE CHART TO VERIFY ALL REPORTED NUMBERS. THIS INCLUDES A FULL WEIGHT AND BALANCE WORKSHEET AS WELL AS CG ENVELOPE DIAGRAM SHOWING ALL CONDITIONS OF FLIGHT. | ||||||||||||||||||||||||||||||
| Make | Model | FAA Registration and Serial Number of Aircraft Offered | Aircraft Max Ramp Weight | Start, Runup, and Taxi fuel burn in LBS. | Aircraft Max Takeoff Gross Weight | Aircraft Max Landing Weight | Aircraft Max Allowable Zero Fuel Weight | Aircraft Weight with all installed mission equipment | Aircraft weight with all mission equipment and max payload crew configuration | Total aircraft usable fuel in LBS. | Total allowable fuel with all mission equipment and MAX mission pay load in LBS. | Fuel burn in LBS. to 10,500 msl from sea level | Time to climb to 10,500 msl from sea level | Total fuel burn in LBS. to cruise 150 nm at 10,500 msl at ISA +20 C | Mission aircraft cruise configuration and calculated TAS | Time to cruise 150 nm at 10,500 msl at ISA +20 C | Total fuel burn to loiter for three hours at 7,000 MSL | Aircraft loiter configuration | Vmca For loiter configuration (if applicable) | VS1 at 30 deg AOB for loiter configuration | 1.3VS1 for loiter configuration | Vyse at Max Gross Takeoff gross weight (if applicable) | Fuel burn to climb from 7,000 MSL (working altitude) to 10,500 MSL (Cruise) | Time to climb from 7,000 MSL (working altitude) to 10,500 MSL (Cruise) | Total fuel burn in LBS. to cruise 150 nm at 10,500 MSL at ISA +20 C | Column AA aircraft configuration and calculated TAS | Time to cruise 150 nm at 10,500 MSL at ISA +20 C | Approach fuel burn | Total Fuel remaining (in minutes) at landing under normal cruise configuration at 10,500 MSL ISA +20 | Total fuel remaining at landing in LBS. |
| Example | Example | N12345 / SN 12345 | 12590 | 90 | 12500 | 12500 | 11000 | 8337 | 9072 | 3562 | 3250 | 400 | 1OMIN | 400 | CLEAN 270ktas | 35 MINS | 1800 | flaps approach, props 1800 rpm @ 121 kias | 89 | 91 | 119 | 121 | 200 | 5 MIN | 350 | Clean 270 Kts | 35 mins | 200 LBS. | 30 Min | 315 |
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