Attachment 7_ASM_Aircraft Identification and Performance.xlsx
XLSX spreadsheet 14 KB Posted
- Attached to
- Aerial Supervision Module (ASM)-Leadplanes
- Solicitation number
- 1202SA23R9101
- Issued by
-
Department of Agriculture Forest Service
About this file
This document includes an attachment and federal contract opportunity related to an Aerial Supervision Module leadplane contract. The attachment provides a template for offerors to provide detailed aircraft performance specifications including make, model, weight and balance information, fuel consumption rates, climb and cruise performance, and fuel reserves. The federal contract opportunity is a solicitation from the USDA Forest Service seeking a manufacturer-built, twin-engine turbine aircraft for exclusive government use year-round. The aircraft will be used for resource management, passenger and cargo transport, law enforcement, pilot training, and administrative activities. Interested parties must submit a notice of intent by May 23, 2023 at 1300 MDT and submit any questions on a provided Microsoft form. A pre-proposal conference will be scheduled with participation information provided later. Offerors must provide company and attendee information to receive call-in details.
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Other files
| File | Type | Posted |
|---|---|---|
| Amendment6.pdf | ||
| Amendment5.pdf | ||
| Amendment4.pdf | ||
| Amendment 3.pdf | ||
| A2.1_Attendance Roster.pdf | ||
| A2.2_Offer Submission Process.pdf | ||
| A2.4_ASM_Aircraft Identification and Performance.xlsx | XLSX spreadsheet | |
| A2.3_Weight and Balance Chart.xlsx | XLSX spreadsheet | |
| Amendment 2.pdf | ||
| Amendment 1.pdf | ||
| Amendment 1.pdf | ||
| Attachment 1_ Contractor Authorized Signatures.docx | DOCX document | |
| Attachment 9_Example of Panel Preferred_Radio Configuration.pdf | ||
| 1202SA23R9101.pdf | ||
| Attachment 2_SMS Questionnaire Accident History.docx | DOCX document | |
| Attachment 6_Schedule of Items Workbook.xlsx | XLSX spreadsheet | |
| Attachment 3_Weight and Balance Charts.docx | DOCX document | |
| Attachment 4_Avionics Requirement Worksheet.docx | DOCX document | |
| Attachment 5_Past Performance.docx | DOCX document | |
| Attachment 8_Example Performance Validation.pdf |
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Text version
Offered Aircraft Performance
| Mission 1 - AIRCRAFT PERFORMANCE | |||||||||||||||||||||||||||||||||||||
| 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 | Manufactured Year | Empty Weight | Certified Max Gross Weight | Number of Seats | Pressurized? | Hourly Fuel Consumption Rate | Air Conditioning? | 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 | Vacca 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 | 2014 | 8 | Yes | 110 | Yes | 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" |
File details come from the government source that posted it. Updated .