A2.4_ASM_Aircraft Identification and Performance.xlsx
XLSX spreadsheet 13 KB Posted
- Attached to
- Aerial Supervision Module (ASM)-Leadplanes
- Solicitation number
- 1202SA23R9101
- Issued by
-
Department of Agriculture Forest Service
About this file
This document contains a federal contract solicitation and related aircraft performance file. The solicitation is for a commercial firm fixed price contract to be awarded for manufacturer built, dual-engine, turbine-powered aircraft to be made available for the exclusive use of federal government or contracted pilots for aerial supervision and other activities year-round. Interested parties must submit a notice of intent by May 23, 2023 at 1300 MDT and submit any questions using a Microsoft form that will be provided. A pre-proposal conference will be held and available through Microsoft Teams, with company and attendee information due to the point of contact to receive the Teams link. The aircraft performance file provides specifications for various aircraft models, including maximum weights, payload capacities, fuel capacities and burns for takeoff, climb, cruise, loiter and landing profiles.
View the file
Other files
| File | Type | Posted |
|---|---|---|
| Amendment6.pdf | ||
| Amendment5.pdf | ||
| Amendment4.pdf | ||
| Amendment 3.pdf | ||
| A2.3_Weight and Balance Chart.xlsx | XLSX spreadsheet | |
| Amendment 2.pdf | ||
| A2.1_Attendance Roster.pdf | ||
| A2.2_Offer Submission Process.pdf | ||
| Amendment 1.pdf | ||
| Amendment 1.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 7_ASM_Aircraft Identification and Performance.xlsx | XLSX spreadsheet | |
| Attachment 8_Example Performance Validation.pdf | ||
| Attachment 1_ Contractor Authorized Signatures.docx | DOCX document | |
| Attachment 9_Example of Panel Preferred_Radio Configuration.pdf |
Show all 20
On GovTribe
Work with this file
- Download the original file
- Contacts named in this file
- Similar government files
- Ask GovTribe AI about this file
Text version
Offered Aircraft Performance
| B-1 ASM_Leadplane AIRCRAFT MISSION CONFIGURATION AND FLIGHT PROFILES | (i) (210 x 3=630) + Gear (35 x 3=105) = 735 LBS. | B-3 (a) (210 x 3=630) + Gear (55 x 3=165) = 795 LBS. | ||||||||||||||||||||||||||||
| 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. | B-5 (a) Useful Load: 1,000 lb. or greater payload when fully equipped with 4 hours plus 30-minute reserve. | |||||||||||||||||||||||||||||
| 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 4500' MSL | Time to climb to 22,000 msl from 4500' MSL | 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 |
File details come from the government source that posted it. Updated .