Attachment 10_Performance data chart.xlsx
XLSX spreadsheet 58 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 solicitation to obtain fixed-wing aircraft services. The Forest Service intends to award indefinite delivery, indefinite quantity contracts to qualified offerors to provide aircraft and flight crews for fire, resource, project, law enforcement, and administrative missions supporting various federal and state land management agencies. Aircraft must meet specifications and be operated by proficient personnel. Contractors may be required to provide daily coverage during mandatory availability periods specified in task orders. The solicitation number is 1202SA22R9102 and comments on the draft statement of work are due by September 30th, with an industry day scheduled for October 25th in Boise, Idaho.
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Text version
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 |
| *Note* When completing tabs for response N/A is not an acceptable response. |
| **Note** When completing tabs for response if information is unknown please write "UNK" and if it is unavailable please write "UA" |
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 120 nm at 22,000 msl at ISA +20 C | Mission aircraft cruise configuration and calculated TAS | Time to cruise 120 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 | 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 120 nm at 22,000 MSL at ISA +20 C | Column AA aircraft configuration and calculated TAS | Time to cruise 120 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 120 nm at 22,000 msl at ISA +20 C | Mission aircraft cruise configuration and calculated TAS | Time to cruise 120 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 | 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 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 120 nm at 22,000 MSL at ISA +20 C | Column AA aircraft configuration and calculated TAS | Time to cruise 120 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 120 nm at 22,000 msl at ISA +20 C | Mission aircraft cruise configuration and calculated TAS | Time to cruise 120 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 | 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 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 120 nm at 22,000 MSL at ISA +20 C | Column AA aircraft configuration and calculated TAS | Time to cruise 120 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 75 nm at 10,500 msl at ISA +20 C | Mission aircraft cruise configuration and calculated TAS | Time to cruise 75 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 75 nm at 10,500 MSL at ISA +20 C | Column AA aircraft configuration and calculated TAS | Time to cruise 75 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 - Back Country Operations | ||||||||||||||||||||||||||||||
| 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 6 A
| Mission 6 A - High Performance Resource Reconniassance | ||||||||||||||||||||||||||||||
| 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 6 B
| Mission 6 B - Standard Resource Reconniassance | ||||||||||||||||||||||||||||||
| 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 5,500 msl from sea level | Time to climb to 5,500 msl from sea level | Total fuel burn in LBS. to cruise 50 nm at 5,500 msl at ISA +20 C | Mission aircraft cruise configuration and calculated TAS | Time to cruise 50 nm at 5,500 msl at ISA +20 C | Total fuel burn to loiter for three hours at 3,000 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 3,000 MSL (working altitude) to 5,500 MSL (Cruise) | Time to climb from 3,000 MSL (working altitude) to 5,500 MSL (Cruise) | Total fuel burn in LBS. to cruise 50 nm at 5,500 MSL at ISA +20 C | Column AA aircraft configuration and calculated TAS | Time to cruise 50 nm at 5,500 MSL at ISA +20 C | Approach fuel burn | Total Fuel remaining (in minutes) at landing under normal cruise configuration at 5,500 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 7
| Mission 7 - Other Special Use Non-Fire light fixed wing operations | |||||||||||||||||||||||||||||||
| 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 | Gear Configuration (Fill out a line for each configuration i.e. Ski, Float, Wheel) | 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 5,000 msl from sea level | Time to climb to 5,000 msl from sea level | Total fuel burn in LBS. to cruise 50 nm at 5,000 msl at ISA +20 C | Mission aircraft cruise configuration and calculated TAS | Time to cruise 50 nm at 5,000 msl at ISA +20 C | Total fuel burn to loiter for three hours at 1,500 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 1,500 MSL (working altitude) to 5,000 MSL (Cruise) | Time to climb from 1,500 MSL (working altitude) to 5,000 MSL (Cruise) | Total fuel burn in LBS. to cruise 50 nm at 5,000 MSL at ISA +20 C | Column AA aircraft configuration and calculated TAS | Time to cruise 50 nm at 5,000 MSL at ISA +20 C | Approach fuel burn | Total Fuel remaining (in minutes) at landing under normal cruise configuration at 5,000 MSL ISA +20 | Total fuel remaining at landing in LBS. |
| Example | Example | N12345 / SN 12345 | Float | 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 |
| Example2 | Example2 | N12345 / SN 12345 | Ski | 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 |
File details come from the government source that posted it. Updated .